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WWW.CROUZET-AEROSPACE.COM
ELECTRICAL PROTECTION
& DISTRIBUTION
AEROSPACE & DEFENSE
TECHNICAL GUIDE
›› Electromechanics
›› Mechatronics
›› Electronics
|| WWW.CROUZET-AEROSPACE.COM || 2 || ELECTRICAL PROTECTION|| WWW.CROUZET-AEROSPACE.COM || 2 || ELECTRICAL PROTECTION & DISTRIBUTION
Crouzet Aerospace has been producing High
Performance Aerospace components for over
fifty years and has secured a leading role in three
Product lines dedicated to aerospace applications:
››  Detection and Sensing: Limit switches, Proximity
switches and sensors
››  Electrical Protection and Distribution: Circuit
Breakers  Circuit Breaker Panels, Solid State
Power Controllers
››  Cockpit Equipment: Control Wheels, Helicopter
Grips, Pushbuttons.
Today Crouzet Aerospace’s components can be
found on most major fixed wing programs around the
world.To ensure the necessary quality, all Crouzet
Aerospace High Performance components are
manufactured in Valence, France, and Casablanca,
Morocco and are fully certified to EN 9100,
ISO 9001, ISO 14001, EASA part 21/G and part 145.
With more than 50 years of
presence in the aerospace market,
Crouzet Aerospace is a specialist
providing customized solutions for
electromechanical switches, inductive
sensors, electrical protection and
cockpit equipment backed up by a
loyal and experienced team of experts
available worldwide.
Crouzet Aerospace is a brand of
InnoVista Sensors™.
ABOUT
CROUZET AEROSPACE
InnoVista Sensors™: your trusted
partner of choice to face industrial
challenges of today and tomorrow.
InnoVista Sensors™ is a worldwide
industrial specialist of sensors,
controllers and actuators for automated
systems.
Through its brands, Crouzet Aerospace,
Crouzet Automation, Crouzet Control,
Crouzet Motors, Crouzet Switches and
Systron Donner Inertial,
InnoVista Sensors™ offers a wide range
of reliable, efficient and customizable
components dedicated to the Aerospace
 Defence, Transportation and Industrial
market and segments.
Thanks to the recognized expertise of
its teams and a strong innovation policy,
InnoVista Sensors™ brings performance
enhancing solutions to its customers
worldwide.
www.innovistasensors.com
For
Aerospace
 Defense
Transportation Industry
With commercial brands
Designs  Manufactures
|| WWW.CROUZET-AEROSPACE.COM || 3 || ELECTRICAL PROTECTION  DISTRIBUTION
CONTENTS
	 Pages
Topology 	 4
Components 	 5
Arc Fault Protection 	 8
Ground Fault Circuit Breaker (GFCB)  Arc Fault Interrupter 	 10
From SSCB to SSPC 	 12
High Shock and Vibration Breakers 	 13
Circuit Breaker panels 	 14
The «do it your self» kit 	 15
Remote Control Contactor  Circuit Breaker 	 16
ELECTRICAL PROTECTION
Selection Guide (standard, ratings) 	 17
Small Model Circuit Breaker Single Pole 	 18
Small Model Circuit Breaker Three Pole 	 20
Big Model Circuit Breaker Single Pole 	 22
Big Model Circuit Breaker Three Pole 	 24
Frog legs Terminals 	 26
Frog legs Connection 	 27
Push-pull Push-fit 6.35 mm Blade 	 28
Push-push  Flying Leads Version	 30
GFCB  AFCB 	 32
Dummy  Simulator CB 	 34
Accessories 	 36
ELECTRICAL DISTRIBUTION
Selection guide 	 37
PCB kit for Faston CB 	 38
RCCB 115/200 VAC 360-800 Hz 	 40
SSPC 28 VDC  115 VAC  GFI 	 42
INNOVATION  FUTURE PRODUCTS 	 44
FREQUENTLY ASKED QUESTIONS	 45
ACRONYMS 	 51
|| WWW.CROUZET-AEROSPACE.COM || 4 || ELECTRICAL PROTECTION  DISTRIBUTION
An electrical network can be split between primary distribution and secondary distribution.
ELECTRICAL NETWORK
TOPOLOGY
Contactor AFCB CB Fuse SSCB-SSPC RCCB
Primary Electric Distribution encompasses the logic of power management (bus shedding in accordance with the
Generator Control Unit (GCU), reconfiguration of contactors for ground power unit, or auxiliary power sources, cockpit
specific orders…) and Secondary Electric Distribution encompasses the way to bring energy to most of the loads
(lights, computers, actuators…) through Circuit Breaker panels or Solid State Protection devices.
|| WWW.CROUZET-AEROSPACE.COM || 5 || ELECTRICAL PROTECTION  DISTRIBUTION
ELECTRICAL NETWORK
COMPONENTS
Thermal trip curve
Crouzet Aerospace offers different components for different type of electrical protections:
›› Electromechanical Circuit Breakers (CB) with several different terminals (frog legs, FASTON, EN, MIL…) and accessories
›› Single channel Solid-state Circuit Breakers (SSCB) (i.e. an electronic switch with logical Inputs, thus a one
channel SSPC)
›› Remote Control Circuit Breakers (RCCB) for bus shedding or temporary power ON of equipments and loads
›› Power Distribution Boxes (PDB) designed to customer specifications
›› A Circuit Breaker Panel Kit (qualified to severe environment)
The goal of electric protection is to protect the cables, the installation and in some cases the load from smoking or igniting
or damage due to excessive current or arcing.
Thermal Circuit Breakers protect the wire downstream of the Circuit Breaker. They do not protect the load. To
do this, a Circuit Breaker must sense the current and break open the line (wire conveying the current) when the
current surges ( if the current is above the authorized value for too long).
›› Arc Fault Circuit Breakers protect aluminum structures, composite structures, hydraulic tubes, wires and
bundles from the damages of arcing and reduce occurrences of fuel vapor ignition.
›› Ground Fault Interrupters protect humans against electrical shock (with a threshold around 30 mA) and
reduce fuel vapor ignition occurrences (with a threshold around 1 A).
›› Solid State Power Controllers protect the wire downstream of the SSPC, they can control the power going to
the load and they can protect the load if they are connected to the load’s heat sensors or security output.
›› Remote Control Contactor and Circuit Breakers protect the wire downstream of the RCCB and they can
protect the load if they are connected to the load’s heat sensors or security output.
Trip range
Curve of circuit opening
caused by damage
Cable smoke curve
Current
Time
Thermal Circuit Breakers have a trip curve which is defined
in relation to the cable smoke curves for the entire operating
temperature range (-60 °C to +125 °C).
Thermal protection based on i2t monitoring is a simple and
therefore very reliable concept.
It is not sensitive to electromagnetic emission and has the
advantage of not tripping on normal transient currents such as
current surge caused by motor inertia, a capacitor inrush or a
cold incandescent lamp filament etc...
For this purpose Circuit Breakers are composed of a latch, a
spring, contacts and a current sensor (see next page).
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«LIGHT, SIMPLE AND SAFE»
Light:
Our single phase EN2495 and MIL MS33201 V compliant model is the lightest in the world
(20 g with screws, washers and nut).
Simple:
›› Designed to be reused several times, spare components are not required
›› Can sometimes be used as a switch (within the defined endurance limits),
they therefore perform a dual function of switching and protecting
Safe:
›› Our intrinsic fail safe** and trip free* conception enable a high level of safety
(generally 10-9
 Flight Hours (FH) of not opening on a short circuit)
›› The temperature compensation ensures high performance over a wide temperature range
(usually -60°C to +125°C)
›› Excellent resistance to mechanical stress
›› High current level peeks and high current flows tolerance
ELECTROMECHANICAL CIRCUIT BREAKERS
In this type of Circuit Breaker, the current sensing is done by a bi-metal. The bi-metal is also part of the actuator
that will open the line: the bi-metal is bent by heat coming from the current, the bi-metal moves the key lock,
releases the latch and opens the line.
ELECTRICAL PROTECTION
HOW DOES IT WORK?
Button
Spring
Load terminal Power terminal
bi-metal
Key lock
Compensation bi-metal
Power terminal
Contacts
* Trip free: even if the pushbutton is maintained in the closed position, the opening of the contacts (and therefore of the electric circuit) is ensured in the
event of a current surge or short-circuit.
** Intrinsic safety (Fail safe): the Circuit Breaker has been designed with a fuse element to ensure that the electric circuit is opened in the extreme case
of a blocked mechanism or glued contacts.
The Circuit Breaker bi-metal bends and releases the latch according to the overload current
value and the overload duration (the bending is independant of the current direction).
If any, the auxiliary contact are galvanically isolated from the power and gives the state
of the contacts (open or closed).
* *
* The current direction can be inverted.
|| WWW.CROUZET-AEROSPACE.COM || 7 || ELECTRICAL PROTECTION  DISTRIBUTION
SOLID STATE CIRCUIT BREAKERS (SSCB)
In this type of Circuit Breaker, the current sensing is done by a shunt or a Hall sensor in DC or a Current Transformer (CT)
in AC. A microcontroller or FPGA acquires the current and simulates the i²t curve, the switch function is often done by
MOSFETS, bipolar transistors, SCR (i.e. thyristors).
Elementary Solid State Circuit Breaker
The patented fuse F gives a 10-9
FH safety level (equivalent to mechanical Circuit Breakers)
and still gives the possibility of reprogramming the Rated Current value by software.
«MORE THAN A THERMAL SWITCH»
A SSCB is more than a thermal switch because when it is connected to a data bus, it provides
intrinsically functions such as:
›› A remote switching ability (useful in application: contactor or relay function)
›› Dimmer or chopper function (useful in applications such as: motor speed control, light dimming,
soft start)
›› Current monitoring (prognostic applications, load failure detection)
Also,
›› They are not susceptible to vibrations (useful in applications with high acceleration (Gs): aircraft,
guns…)
›› They generate no audio noise (useful in applications such as: submarines, electric tanks,
medical…)
›› The micro controller can run the arc fault protection algorithm
›› They can become a PLD with a protected power output (see p. 37)
›› They can protect the load (see p. 37).
The microcontroller will integrate the current going through the shunt and will open the MOSFET
according to the current value and overload duration.
|| WWW.CROUZET-AEROSPACE.COM || 8 || ELECTRICAL PROTECTION  DISTRIBUTION
Wet arc
The associated Advisory Circular (AC) gives guidance for subpart H
compliancy and indicates that a safety analysis of the Electric Wiring
Interconnection Systems (EWIS) has to be done.
To certify the EWIS, the constructor must show a proactive approach
to mitigate risks and perform a zonal analysis (EZAP).
When performing this analysis, it is very important to keep in mind that
«regardless of probability, any single arcing failure should be
assumed for any power carrying line» (page 31 of the AC) because
the traditional way of thinking which was: «optional systems, like in
flight entertainment, cannot cause a catastrophic failure condition» is
not a valid assumption.
Locations where arcing must be mitigated:
A 	In flight entertainment area
B 	Cargo and baggage compartment door actuators
C 	Fuel tanks
D SWAMP area (Severe Wind And Moisture Problem area) such as
wires in landing gear well or cockpit window heater or wing defrost
heaters
E Galleys to protect electrical socket appliances such as: Cooktop
ovens, waste compacting machines, coffee machines etc…
F Places where due to vibration, heat, aging or after an incorrect 	
maintenance operation there is a risk of a power line touching:
	 1. a critical hydraulic actuator line
	 2. pressurized air line (air duct) or flight critical data line
	 3. mechanical control system cable
	 4. oxygen lines
	 5. fuel lines
	 6. water and water/waste line (and below them in case of dripping)
	 7. hot air ducts
In case of an arc inside a bundle, arc fault technology will preclude a
chain reaction in the bundle from inducing the loss of the complete
bundle. Instead there will be a «controlled» deterioration of the wire(s)
giving time for maintenance to be aware of the fault (by using the
information coming from the circuit breaker) and thus avoiding a
potential catastrophic situation.
ELECTRICAL PROTECTION
ARC FAULT PROTECTION
EWIS PROTECTION
The new FAA Part 25 subpart H requirements asks aircraft OEM
to consider the electrical wiring interconnection as a system.
This means that the airworthiness of the wiring must be guaranteed
for the complete lifetime of the aircraft.
By incorporating AFCBs in your electrical network, you will be
compliant to this new rule.
|| WWW.CROUZET-AEROSPACE.COM || 9 || ELECTRICAL PROTECTION  DISTRIBUTION
HOW DOES ARC FAULT PROTECTION WORK?
AFCBs combine the safety of standard Circuit Breakers and high
accuracy electronics to mitigate arcing. Each standard thermal Circuit
Breaker is equipped with an electronic board in order to analyze the
current waveform
in real time to detect if arcing is occurring.
CARBON COMPOSITE (CFRP) PROTECTION
Carbon Fibres Reinforced Polymer (CFRP) can be damaged (delamination) and can ignite in case of arcing.
The use of arc fault protection will mitigate damage and risk significantly as illustrated below:
The algorithm in the electric board works faster
than the thermal bi-metal function as shown on
the adjacent chart.
In case of an electric hazard, the arcing
energy (thus mechanical damage) is divided
by a magnitude (generally 10) as shown in
the adjacent chart.
Developped in accordance with DO178B,
the AFCB delivers effective arcing mitigation
while keeping the robust and proven
mechanical EN2995 thermal protection.
Current (Amp)
Energy(J)
10000
1000
100
10
1
1 5A 10 100 1000
parallel
arc area
series
arc
area
Upper limit of
released arc
energy with a
thermal CB
(400J..70J)
Upper limit of
released arc
energy
with an AFCB
(6J..30J)
Electronic
board
Thermal
breaker
Cosmetic
damage
Delamination
Single pole AFCB
230 VAC Fault with arc fault protection:
only cosmetic damages appears
230 VAC Fault without arc fault protection:
delamination of the fibers
|| WWW.CROUZET-AEROSPACE.COM || 10 || ELECTRICAL PROTECTION  DISTRIBUTION
FUEL TANK PROTECTION
Following SFAR88 recommendation, the FAA and EASA have compelled PART 25 aircrafts to
protect fuel tanks with Ground Fault. The purpose of these Ground Fault products is to mitigate
fuel tank ignition by reducing the amount of leakage current to the airframe inside the fuel tank.
Documents AC2025_981_1C and EASA CS-25 AMC25.981(a) state that:
«any components located in or adjacent to a fuel tank must be qualified to meet standards that
assure, during both normal and failure conditions, ignition of flammable fluid vapors will not
occur».
The above is a concern for:
›› Pylons  nacelles and small dimension aircraft where power line are routed near data buses
or hydraulic tubes.
›› Wings where torque tube disconnections can cause severe damage to the wiring.
›› Composite wings with high power electric actuators (EHA, EBHA) in the vicinity of fuel tanks.
AC2025_981_1C states:
Page 17:
«A practical means to achieve this is to provide sleeving of the wiring and an independent means
such as a GFI or arc fault circuit breaker».
Page 20:
«(f) Circuit Breakers Service experience has indicated that thermal mechanical circuit breakers
installed in the fuel pump circuits have not been shown to preclude arcing […] Arc Fault Circuit
Breakers and Ground Fault Interrupters may be needed to provide fail safe features necessary
to demonstrate compliance».
THE GFCB: A CIRCUIT BREAKER WITH AN ENHANCED GFI
Traditional GFI do not capture series arcing or line to line arcing because these two faults do not
create a leakage current to the ground (i.e. the CT that measures the homopolar current will still
read «zero» with those 2 faults). By adding arc fault detection on each line, Crouzet Aerospace's
GFCB is a GFI and a circuit breaker that detects these failure modes.
ELECTRICAL PROTECTION
GROUND FAULT CIRCUIT BREAKER (GFCB)
A
triangle load
ground fault
detector
arcfault
detector
B
C
line to ground fault ➔ detected
line to line fault ➔ detected
series arc fault ➔ detected
Ground fault
 arc fault
interrupter
THE GFCB LAYOUT
|| WWW.CROUZET-AEROSPACE.COM || 11 || ELECTRICAL PROTECTION  DISTRIBUTION
ARC FAULT INTERRUPTER
HOW DOES THE GFCB WORK?
›› Built in test
The GFCB provides built-in test features that allow aircraft
maintenance personal to verify that ground fault protection
is functional, or that a ground fault has occurred: data
issued from the led on the flat of the threaded barrel gives
this information.
›› Severed wire detection
The GFCB includes «severed wire detection» (ie broken
or cut wire) to preclude the heating of a motor if it is stalled
(blocked) or running on only 2 phase (typical time detection
is 1 second).
The above has been implemented because
AC2025_981_1C states page 34:
( c) «[…] Automatic protective means, such as arc/ground
fault interrupters or other means, should be provided to
shut down the pump when a single electrical phase failure
occurs. Periodic inspections or maintenance of these
features may be required».
ON A «STAR» (WYE) LOAD, WITH GROUNDED CENTER, THE BEHAVIOR OF THE GFCB IS THE FOLLOWING
ON A «DELTA» (TRIANGLE) LOAD, THE BEHAVIOR OF THE GFCB IS THE FOLLOWING
A
star load
«normal» leakage current
ground fault
detector
B
C
A
delta load
ground fault
detector
B
C
Electronic
board
Thermal
breaker
›› The Crouzet Aerospace GFCB has 2 thresholds:
–– fault time confirmation
–– maximum ground fault current.
This enables Crouzet Aerospace to deliver products
adapted to you load configuration. For instance, GFCB can
be targeted either toward Delta (triangle) motor or star (wye)
motor configuration.
The star configuration is specific because leakage current
from the star center to the airframe is possible without being
an anomaly (if the center of the star is grounded).
|| WWW.CROUZET-AEROSPACE.COM || 12 || ELECTRICAL PROTECTION  DISTRIBUTION
ELECTRICAL DISTRIBUTION
FROM SSCB TO SSPC
FROM SSCB TO SSPC
Using the most recent solid state technology, Crouzet Aerospace has developed 2 generic Solid
State Circuit Breakers (SSCB): One for 28 VDC applications, the other for 115 VAC applications.
A Solid State Circuit Breaker is composed of a microcontroller, a switch and a data bus.
This enables a SSCB to provide more than just thermal protection; its role encompasses electrical
functions such as: relay, gradator, chopper, ground fault, soft start, current measurement.
These functions can be used for light dimming, motor speed control, intermittent load command
(on/off), inrush current limitation, sequential power ON of loads, load failure detection.
This is why they become Solid State Power Controllers (SSPC).
WHEN DO I NEED A SSPC?
Cost efficiency will depend on the ability to encompass several of the previous functions.
When thinking of an SSPC solution the following chart must be kept in mind:
EASY TO OPERATE
Both 115 VAC and 28 VDC SSPC components are delivered with a
laptop/tablet interface that enables a quick appropriation of SSPC
features. Command from the laptop are transferred through CAN
bus. The laptop/tablet interface can be replaced by a MCU or Utilities
Management System (UMS) that sends and receives data frames
through CAN2.0B.
The typical set of orders/queries is:
ON/OFF 	 : Powers ON/OFF the load
RESET 	 : RESETS the elementary switch after arc or thermal trip
STATUS 	 : Asks for trip reason
CURRENT 	: Asks for current (A) value
BACKUP	 : Programs the behavior when data bus is disconnected
WHAT I NEED MUST I THINK OF
AN SSPC SOLUTION?
TRIP INFORMATION
ON/OFF I²t
High Inrush (8X)
SECURE OPEN Arc Fault
GFI
TRIP ACKNOWLEDGE
Laptop-tablet interface
|| WWW.CROUZET-AEROSPACE.COM || 13 || ELECTRICAL PROTECTION  DISTRIBUTION
ELECTRICAL PROTECTION
HIGH SHOCK AND VIBRATION BREAKERS
Typical circuit protection on following military platforms:
›› Fighter Aircraft
›› Military Helicopters
›› Ground Air Defense Systems
›› Military Land Tracked and Wheeled Vehicles
›› Missile Launchers
›› Naval Shipboard Applications
MIL-STD-202G
Sinusoidal (MIL STD 202 method 204 D) 20 g-PK: condition D under 71 °C and RC
Random (MIL STD 202 method 214 A) 23.91 Gms: condition G under 71° C and RC
Shock (MIL STD 202 method 213B) 75 g 3 halfsine 6 msec: condition B
Our High-Performance Thermal Circuit Breakers exceed the standard for shock and vibration for
military applications.
It has allways been troublesome for electrical systems engineers to find the best suitable circuit
breakers for harsh environments. Crouzet Aerospace has developed a specific series of circuit
breakers which go far beyond the current standards.
When used in the vicinity of cannons or missile launchers and in circuit breaker panels installed
next to machine guns (e.g. helicopters, jet fighters or armored vehicles) the high «shock and
vibration» family avoids installing silent blocs on panels or on circuit breakers (while maintaining
top circuit protection performance).
For the single pole circuit breaker the High Shock and Vibration products multiply by three the
endurance level to random and sinus vibrations, compared to AS58091 level or basic MS33201
levels.
AS58091  AS33201 basic level
Vibration frequency in Hz
New level
Test condition
letter
Power spectral
density
Overall
rms G
A .02 5.35
B .04 7.56
C .06 9.26
D .1 11.95
E .2 16.91
F .3 20.71
G .4 23.91
H .6 29.28
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OUR KNOW HOW
As a manufacturer of CB panels we will optimise your needs:
›› Geometry, connection and mounting as specified by your requirements and constraints
›› Customised marking of the front panel
›› Labelling of Circuit Breaker functions by engraving or easily-modified labels
›› Reduced weight due in part to our specially developed light weight Circuit Breaker and busbars
›› Expertise in mechanical and thermal limits (wire gauges, suitable sizes for Circuit Breakers,
optimum distribution of Circuit Breaker, …)
›› Expertise in busbars and connections with all the safety requirements (segregation,
protection, …)
›› ATP performed by automatic test benches
PREDICTABLE PANEL MASS FOR PANELS CONTAINING ONLY CBs
SUPPLIER OF CIRCUIT BREAKER PANELS
ON SEVERAL JET AND HELICOPTER PROGRAMS
Crouzet Aerospace has extensive experience in the design, development and production of
illuminated and non-illuminated Circuit Breaker panels in Push/Pull or Push/Push versions,
wire or PCB-FASTON version.
ELECTRICAL DISTRIBUTION
CIRCUIT BREAKER PANELS
56 CB military helicopter panel
(wire +casing)
55 CB search and rescue helicopter panel
(PCB + casing)
100 CB regional jet panel
(wire + casing)
25 CB offshore helicopter panel
(wire +casing)
X
X
X
grams/protected line
Technology
Constraints
Wire + casing
None
56 CB military helicopter panel 
100 CB regional jet panel
55 CB search and rescue
helicopter panel
16 CB PCB panel kit
= World Record !
43
38
0
33
PCB + casing
Rear or side
connector
PCB + no casing
Side connector
|| WWW.CROUZET-AEROSPACE.COM || 15 || ELECTRICAL PROTECTION  DISTRIBUTION
PREQUALIFICATION
To reduce development time the kit is qualified to harsh
environnement.
The use of the panel or its sub-sets enables the quick fielding
of a qualified solution. If the assembly recommendation
and Circuit Breaker locations are respected,
Crouzet Aerospace guarantees the electrical and vibrational
behavior of the kit:
›› Temperature and electrically from -55°C to 71°C with a 100%
utility factor (150 A output)
›› Vibrations: Random and Sinusoidal rays (Harsh Helicopter
Level)
›› Crash, fungus, sand and dust.
KIT CONSTITUTION
The kit is composed of spacers, a PCB board, FASTON Circuit
Breakers, and positionning rings. A front panel with removable
plate is also available. The removable plate is compatible with
accessories (Circuit Breaker gags and obturators).
WORLD RECORD
The above kit assembly conveys 150 A at 71°C, it weighs
528 g with 16 Circuit Breakers and thus gives a panel
efficiency ratio of 528 g=33g/CB ➔ a world record!
Ring
Distance tube
Spacer tube
Power feeder
EN4165Vertical take off UAV
(PCB + no casing)
The «Do it your self» kit
A STANDARD PCB CARRYING FASTON CBS
Crouzet Aerospace is the first company to invent the concept of «do it yourself» Circuit Breaker
panels
and with this technique, it has created the lightest extractible Circuit Breaker panel in the
world!
The concept is based on a generic PCB carrying 16 FASTON CBs that you can duplicate
(if several bus bars are needed or if more Circuit Breakers are needed).
ELECTRICAL DISTRIBUTION
THE «DO IT YOUR SELF» KIT
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Electric or hydraulic actuator
FIN Design Bus bar P/N
12C GALLEY A 84 354 335
1X BULK FAN HEATER A 84 354 335
3 RECIRC FAN B 84 354 350
3JV1 HYD PUMP B 84 354 350
6XN1 L INDB ELEVATOR POWER SPLY C 84 354 350
1XX R INDB ELEVATOR POWER SPLY C 84 354 350
3XX GND SUPPLY A 84 354 350
3XX1HG1 RECIRC FAN A 84 354 350
51N 107XP (IFE) A 84 354 360
1MC L-MID AILERON POWER SPLY A 84 354 350
3J2 L-MID AILERON POWER SPLY A 84 354 350
3J1 HYD PUMP GND SUPPLY A 84 354 360
3C2 HYD PUMP B 84 354 350
1HG Y UPPER RUDDER POWER SUPPLY A 84 354 350
5X G UPPER RUDDER POWER SUPPLY B 84 354 350
23MC L SPOILERS POWER SUPPLY A 84 354 350
3MC R SPOILERS POWER SUPPLY B 84 354 350
24M SLAT E-MOT POWER 1 A 84 354 350
6N2 SLAT E-MOT POWER 2 B 84 354 350
2X 212XP GND SUPPLY C 84 354 350
ELECTRICAL DISTRIBUTION
REMOTE CONTROL CONTACTOR  CIRCUIT BREAKER
The RCCB’s primary use is to power loads that do not need to be permanently ON (to optimize energy).
This is why it is used:
›› For powering hydraulic actuators of cargo bay doors
›› For powering Electro Hydraulic Actuators (EHA) and Electro Backup Hydraulic Actuators (EBHA)
›› For powering ON and OFF the galleys or In Flight Entertainment (IFE)
The RCCB contacts are CLOSED and OPENED (load is set ON and OFF) only once or twice during the flight; it is designed
to commute at least 100,000 times, giving the aircraft a minimum of 50,000 cycles (take off and landing).
The RCCB merges a contactor function and a circuit breaker function in a single unit. The contactor is closed when 28 V is
applied on the command input. The RCCB has a status display window and a mechanical «TRIP indicator».
When the CB has tripped, the mechanical «TRIP indicator» is «popped out» and must be pushed back in manually to
RESET the circuit breaker.
Our real MTBF figure of 300,000 Flight Hours (field value) during 20 years of service have convinced our customers to
mount the RCCB successively on:
›› Galleys feeders
›› Cargo doors actuation motors
›› Flight control power packs (EHA and EBHA) of primary flight control actuators(spoilers; ailerons; rudder)
Hereafter is an illustration of the main aircraft locations of the RCCB:
Status window
or
Reset button
(trip indicator)
|| WWW.CROUZET-AEROSPACE.COM || 17 || ELECTRICAL PROTECTION  DISTRIBUTION
ELECTRICAL PROTECTION
SELECTION GUIDE
AS5692 EN2495 EN2592 EN2665 EN2794 EN2995
Rate (A) single Code M Code U Code M Code U 003 004 003 004 004 005
DPMU DMPU DPMU DMPT DPMT DGMT DGMT DGMU DGMU DPMU DPMU
1 84 402 001 84 401 001 84 412 001 84 411 001 84 401 801 84 401 601
2 84 402 002 84 401 002 84 412 002 84 411 002 84 401 802 84 401 602
2.5 84 402 012 84 401 012 84 412 012 84 411 012 84 401 812 84 401 612
3 84 401 503 84 402 003 84 401 003 84 412 003 84 411 003 84 401 803 84 401 603
4 84 412 004
5 84 401 505 84 402 005 84 401 005 84 412 005 84 411 005 84 401 805 84 401 605
7.5 84 401 507 84 402 007 84 401 007 84 412 007 84 411 007 84 401 807 84 401 607
10 84 401 510 84 402 010 84 401 010 84 412 010 84 411 010 84 401 810 84 401 610
15 84 401 515 84 402 015 84 401 015 84 412 015 84 411 015 84 313 015 84 306 015 84 401 815 84 401 615
20 84 401 520 84 402 020 84 401 020 84 412 020 84 411 020 84 313 020 84 313 036 84 306 020 84 306 016 84 401 820 84 401 620
25 84 401 525 84 402 025 84 401 025 84 412 025 84 411 025 84 313 025 84 313 037 84 306 025 84 306 017 84 401 825 84 401 625
30 84 306 030
35 84 313 035 84 313 038 84 306 035 84 306 018
41 84 313 041
50 84 313 050 84 313 058 84 306 050 84 306 019
60
Page 32 18 18 20 20 24 24 22 22 18 18
MS26574 FROG EN3773 EN3774 BACC AS5692
Rate (A) «like» 45° 60° 45° 60° 006 006 extended trip extended trip AFCB GF-AFCB
DPMU DMPU DPMU DPMT DPMT DPMU DPMT DGMU DGMT DPMT DPMT
1 84 406 001 84 437 001 84 437 201 84 417 001 84 417 201 84 408 001 84 418 001
2 84 406 002 84 437 002 84 437 202 84 417 002 84 417 202 84 408 002 84 418 002
2.5 84 406 012 84 437 012 84 437 212 84 417 012 84 417 212 84 408 012 84 418 012
3 84 406 003 84 437 003 84 437 203 84 417 003 84 417 203 84 408 003 84 418 003 84 411 103 84 411 136
4 84 406 004
5 84 406 005 84 437 005 84 437 205 84 417 005 84 417 205 84 408 005 84 418 005 84 411 105 84 411 137
6 84 406 006
7.5 84 406 007 84 437 007 84 437 207 84 417 007 84 417 207 84 408 007 84 418 007 84 411 107 84 411 138
10 84 406 010 84 437 010 84 437 210 84 417 010 84 417 210 84 408 010 84 418 010 84 411 110 84 411 139
15 84 406 015 84 437 015 84 437 215 84 417 015 84 417 215 84 408 015 84 418 015 84 411 115 84 411 140
20 84 406 020 84 437 020 84 437 220 84 417 020 84 417 220 84 408 020 84 418 020 84 411 120 84 411 141
25 84 406 025 84 437 025 84 437 225 84 417 025 84 417 225 84 408 025 84 418 025 84 306 825 84 313 825 84 411 125 84 411 142
30 84 406 030 84 437 030 84 437 230 84 417 030 84 417 230 84 306 830 84 313 830
35 84 306 835 84 313 835
40 84 306 840 84 313 840
50 84 306 850 84 313 850
60 84 306 860 84 313 860
Page 26 26 26 26 26 28 28 22 24 32 32
EN2996 EN3661 EN3662 EN3773 EN3774
Rate (A) 004 005 004 005 006 004 005 006 004 003 004
DPMT DPMT DGMU DGMU DGMU DGMT DGMT DGMT DPMU DPMT DPMT
1 84 411 801 84 411 601 84 401 050 84 413 001 84 411 001
2 84 411 802 84 411 602 84 401 051 84 413 002 84 411 002
2.5 84 411 812 84 411 612 84 401 052 84 413 012 84 411 012
3 84 411 603 84 401 053 84 413 003 84 411 003
5 84 411 805 84 411 605 84 401 054 84 413 005 84 411 005
7.5 84 411 807 84 411 607 84 401 055 84 413 007 84 411 007
10 84 411 810 84 411 610 84 401 056 84 413 010 84 411 010
15 84 411 815 84 411 615 84 313 315 84 401 057 84 413 015 84 411 015
20 84 411 820 84 411 620 84 306 320 84 306 620 84 306 655 84 313 320 84 313 620 84 313 631 84 401 058 84 413 020 84 411 020
25 84 411 825 84 411 625 84 306 325 84 306 625 84 306 653 84 313 325 84 313 625 84 313 632 84 401 059 84 413 025 84 411 025
35 84 306 335 84 306 635 84 306 654 84 313 335 84 313 635 84 313 633
50 84 306 350 84 306 650 84 306 652 84 313 350 84 313 650 84 313 634
60
Page 20 20 22 22 22 24 24 24 18 20 20
GAM
TI-TII-40 / Air
6.625-403
LN29886
/
LN29887
MS3320
AS33201
MS3320
AS33201
QPL
MS14154
AS14154A
MS14154
AS14154A
QPL
MS26574 VG 95345-TEIL 6 VG 95345-TEIL 11
Rate (A) DPMU DPMU DPMU DMPT DMPT DMPU DPMU DPMU DPMT DPMT
1 84 405 001
LN 29886
see
EN2495 M
LN29887
see
EN2592 M
84 400 001 84 400 048 84 410 001 84 414 001 84 406 001 84 402 001 84 402 801 84 412 001 84 412 801
2 84 405 002 84 400 002 84 400 049 84 410 002 84 414 002 84 406 002 84 402 002 84 402 802 84 412 002 84 412 802
2.5 84 405 012 84 400 012 84 400 050 84 410 012 84 414 012 84 406 012 84 402 012 84 402 812 84 412 012 84 412 812
3 84 405 003 84 400 003 84 400 051 84 410 003 84 414 003 84 406 003 84 402 003 84 402 803 84 412 003 84 412 803
4 84 400 061 84 412 004 84 412 804
5 84 405 005 84 400 005 84 400 052 84 410 005 84 414 005 84 406 005 84 402 005 84 402 805 84 412 005 84 412 805
7.5 84 405 007 84 400 007 84 400 053 84 410 007 84 414 007 84 406 007 84 402 007 84 402 807 84 412 007 84 412 807
10 84 405 010 84 400 010 84 400 054 84 410 010 84 414 010 84 406 010 84 402 010 84 402 810 84 412 010 84 412 810
15 84 405 015 84 400 015 84 400 055 84 410 015 84 414 015 84 406 015 84 402 015 84 402 815 84 412 015 84 412 815
20 84 405 020 84 400 020 84 400 056 84 410 020 84 414 020 84 406 020 84 402 020 84 402 820 84 412 020 84 412 820
25 84 405 025 84 400 025 84 410 025 84 406 025 84 402 025 84 402 825 84 412 025 84 412 825
30 84 400 060 84 402 830
Page 30 18 18 20 20 26 18 18 20 20
CHOICE BY STANDARD/RATING
|| WWW.CROUZET-AEROSPACE.COM || 18 || ELECTRICAL PROTECTION  DISTRIBUTION
Rating No signal contact Non polarised / polarised signal contact
1 A 84 400 001 84 400 048/148 84 402 001 84 400 248 84 401 001 84 401 050 84 440 001 84 400 801/601 84 401 801/601 84 402 801/601
2 A 84 400 002 84 400 049/149 84 402 002 84 400 249 84 401 002 84 401 051 84 440 002 84 400 802/602 84 401 802/602 84 402 802/602
2.5 A 84 400 012 84 400 050/150 84 402 012 84 400 250 84 401 012 84 401 052 84 440 012 84 400 812/612 84 401 812/612 84 402 812/612
3 A 84 400 003 84 400 051/151 84 402 003 84 400 251 84 401 003 84 401 053 84 440 003 84 400 803/603 84 401 803/603 84 402 803/603
4 A 84 400 061/161 84 400 261
5 A 84 400 005 84 400 052/152 84 402 005 84 400 252 84 401 005 84 401 054 84 440 005 84 400 805/605 84 401 805/605 84 402 805/605
6 A 84 402 006 84 402 806/606
7.5 A 84 400 007 84 400 053/153 84 402 007 84 400 253 84 401 007 84 401 055 84 440 007 84 400 807/607 84 401 807/607 84 402 807/607
10 A 84 400 010 84 400 054/154 84 402 010 84 400 254 84 401 010 84 401 056 84 440 010 84 400 810/610 84 401 810/610 84 402 810/610
15 A 84 400 015 84 400 055/155 84 402 015 84 400 255 84 401 015 84 401 057 84 440 015 84 400 815/615 84 401 815/615 84 402 815/615
20 A 84 400 020 84 400 056/156 84 402 020 84 400 256 84 401 020 84 401 058 84 440 020 84 400 820/620 84 401 820/620 84 402 820/620
25 A 84 400 025 84 402 025 84 400 225 84 401 025 84 401 059 84 440 025 84 400 825/625 84 401 825/625 84 402 825/625
30 A 84 400 060 84 402 030 84 400 230 84 440 030 84 400 860/660 84 401 830/630 84 402 830/630
Ratings 0.5; 0.75; 1.5 A are available.
REFERENCES
Mounting hardware HV
Threaded
barrel
M12-0.75
M12-100 • • • • •
7/16 • • • • •
Terminal
Screw
8-32 UNC • • • • • • • •
M4 • •
Terminal Offset Offset Offset Offset Aligned Aligned Aligned Offset Aligned Offset
Conformity standard HV
EN 2495 M U
EN 2995 004
EN 3773 004
AS33201 - MS3320 • QPL QPL
VG 95345 TEIL 6 • •
BACC 18Z18AD like •
Mass / MTBF / Vibration / Technical file HV
Weight without mounting hardware  18  18  18  18  18  18  20  20
Weight with mounting hardware  21  20  20  20  20  20  22  22
MTBF FH (Typical)  7.2 M  7.2 M  7.2 M  7.2 M  7.2 M  7.2 M  7.2 M  3.6 M
MIL vibration Sinus/Random A  C A  C A  C G  H A  C A  C A  C A  C
Technical File SP4374 SP9930 SP4356
Button HV
Green color • • •
Black color • • • • • • •
Long neck option •
Electrical
28 VDC 115 VAC (400 Hz) 115 VAC 60 Hz-230 VAC 50 Hz
Breaking current 1co + 2OCO 6000 A 2500 A
CONTACT CROUZET AEROSPACE
Dielectric 1500 V 1500 V
Endurance cycles 5000 (with L/R: 5 ms) 5000 (with cos fi: 0.7)
Insulation resistance above 100 MΩ above 100 MΩ
Working life (endurance) at 5x RC 50 cycles 50 cycles
Auxiliary contact current 0.1..0.2 A 0.1..0.2 A
Voltage drop compliance EN2495/2995/MS3320/AS33201 EN2495/2995/MS3320/AS33201
GENERAL CHARACTERISTICS
DPMU
SMALL MODEL CIRCUIT BREAKER SINGLE POLE
Environmental
Salt spray 48h 5% NaCl
Humidity: Test b RTCA DO160 10 cycles
Operating temperature -60°C +125°C for all ratings except 30 A: - 60°C + 90°C
Acceleration (centrifugal) up to 40 g
Vibrations EN QPL (MS AS33201) High Vibration (HV)
Sinusoidal (MIL STD202 method 204D) 10 g-PK: condition A 15 g-PK: condition C 20 g-PK: condition D
Random (MIL STD202 method 214A) 9.26 Grms: condition C under 71°C and RC 16.91 Grms: condition E under 71°C and RC 23.91 Grms: condition G under 71°C and RC
Shock 50 g 3 halfsine 11 msec 75 g 3 halfsine 6 msec above 75 g 3 halfsine 6 msec
Mechanical
Operating force 3,5N push45N / 5Npull30N
Endurance without load: 5000 cycles resistive load: 2500 cycles
Tightening torque barrel nut: recommended: 4 ± 0.25 N.m maximum : 5.0 N.m terminal screw: recommended: 1.6 ± 0.1 N.m maximum : 2.0 N.m
|| WWW.CROUZET-AEROSPACE.COM || 19 || ELECTRICAL PROTECTION  DISTRIBUTION
DIMENSIONS
CURVES
PANEL CUTOUT RECOMMENDATION
84 400 0
84 402 0
84 401 084 400 6-8
84 402 6-8
84 401 6-8
› Thickness: 1.6 mm ➞ 3 mm
20
10
5
4
3
2
In
10 2
-2
3 45 10-1
2 3 45 1 2 3 45 2 3 45 2 3 4510 100 1000
+125C +25C
-55C
84 400 0 - 6 - 8
84 400 0 - 6 - 8
84 400 0 - 6 - 8
84 405 0
-60
-20
-40
0
20
40
60
80
100
120
0,8 In 1,2 1,4 1,6 1,8 2
84 400 0 - 6 - 8
84 400 0 - 6 - 8
84 400 0 - 6 - 8
84 405 0
Non-trip threshold
Trip threshold
Current
(as percentage of In)
Ambiant
temperature
°C
31
2,5max
1,5
19max
28max.
12,5
38max
4,6
m
in
84 400 0
24 max
19,5 max
2
9,5
14,3max
84 401 0
18
31 max
84 401 0
18
31 max
31
2,5max
1,5
19max
28max
12,5
38max
4,6
m
in
19,5max
16,3 max
26 max
2
9,5
14,3max
84 400 6-8
ø10
12,8
6,35
3max
5
10
84 401 6-8
18 12
10
31,5 max
84 401 6-8
18 12
10
31,5 max
Versions 84 400 0
30min.
9,5
Ø11,5
20 min.
Ø3,5
Versions 84 402 0
30min.
9,5
Ø12,5
20 min.
Ø3
Versions 84 401 0 - 6 - 8
Versions 84 400 1xx
35min.
22.5±0.5
(.886±.019)
28.6max.
Trip times envelope for temperature from -55°C to
125°C (direct overload) Rating 1.5 ➞ 5 A 7.5 ➞ 25 A
Non tripping
point at 25°C
1.15 * RC 1.15 * RC
Tripping point
at 25°C
1.4 * RC 1.4 * RC
Tripping time
at 2 * RC
2 s ➞ 15 s 4 s ➞ 20 s
Non tripping
point at 125°C
1 * RC 1 * RC
Maximum and minimum limit of ultimate trip
|| WWW.CROUZET-AEROSPACE.COM || 20 || ELECTRICAL PROTECTION  DISTRIBUTION
Rating No signal contact Non polarised/polarised signal contact
1 A 84 410 001 84 411 001 84 412 001 84 413 001 84 414 001 84 450 001 84 410 801/601 84 411 801/601 84 412 801/601
2 A 84 410 002 84 411 002 84 412 002 84 413 002 84 414 002 84 450 002 84 410 802/602 84 411 802/602 84 412 802/602
2.5 A 84 410 012 84 411 012 84 412 012 84 413 012 84 414 012 84 450 012 84 410 812/612 84 411 812/612 84 412 812/612
3 A 84 410 003 84 411 003 84 412 003 84 413 003 84 414 003 84 450 003 84 410 803/603 84 411 803/603 84 412 803/603
4 A 84 412 004 84 412 804/604
5 A 84 410 005 84 411 005 84 412 005 84 413 005 84 414 005 84 450 005 84 410 805/605 84 411 805/605 84 412 805/605
6 A 84 412 006 84 412 806/606
7.5 A 84 410 007 84 411 007 84 412 007 84 413 007 84 414 007 84 450 007 84 410 807/607 84 411 807/607 84 412 807/607
10 A 84 410 010 84 411 010 84 412 010 84 413 010 84 414 010 84 450 010 84 410 810/610 84 411 810/610 84 412 810/610
15 A 84 410 015 84 411 015 84 412 015 84 413 015 84 414 015 84 450 015 84 410 815/615 84 411 815/615 84 412 815/615
20 A 84 410 020 84 411 020 84 412 020 84 413 020 84 414 020 84 450 020 84 410 820/620 84 411 820/620 84 412 820/620
25 A 84 410 025 84 411 025 84 412 025 84 413 025 84 414 025 84 450 025 84 410 825/625 84 411 825/625 84 412 825/625
30 A 84 412 030 84 413 030 84 450 030
Button
Green color • • •
Black color • • • • •
Long neck
Mounting hardware
Threaded
barrel
M12-0.75 •
M12-100 • • • •
7/16 • • • •
Terminal
Screw
8-32 UNC • • • • • •
M4 • • •
Terminal Offset Offset Offset Offset Offset Aligned Offset Offset Offset
REFERENCES
Mass / MTBF / Vibration / Technical file
Without mounting hardware  46  51
With mounting hardware  55  60
MTBF FH (Typical)  1,2 M  700 000
MIL vibration condition Sinus/Random A  C A  C
Technical File - - - - - -
Conformity standard
EN 2592 U M
EN 3774 004 003
EN 2996 004/005
VG 95345 TEIL 11 • •
AS 14154B/MS14154 • QPL
BACC 18AC18AE like •
Electrical
115/200 VAC (400 Hz) 115/200 VAC 60 Hz-230/400 VAC 50 Hz
Breaking current 1CO + 2OCO 2000 A
CONTACT CROUZET AEROSPACE
Dielectric 1500 V
Endurance (electrical overloads) 5000 (with cos fi: 0.7)
Insulation resistance above 100 MΩ
Working life (endurance) at 5xRC 50 cycles
Auxiliary contact current 0.1..0.2 A
Voltage drop compliance MS14154/AS14154A/EN2592/2996/3774
Environmental
Salt spray 48h : 5% NaCl
Humidity: Test b RTCA DO160 : 10 cycles
Operating temperature (1 to 15 A) -60°C +125°C
Operating temperature (20 and 25 A) -60°C.+90°C
Acceleration (centrifugal) 17g
Shock 50 g 3 halfsine 11 msec 6 directions
Vibration (sinusoidal) 10 g-PK from 70 to 20000 Hz (MIL STD202 method 204 D condition A with 90 % of RC)
Vibration (random at RC) 9.26 Grms (MIL STD202 method 214 A condition C with 90 % of RC)
Mechanical
Operating force 8Npush80N / 5Npull30N
Endurance (manual open/close)
no load / 5000 cycles
on resistive load / 5000 cycles
Tightening torque barrel nut: recommended: 4 ± 0.25 N.m maximum : 5.0 N.m terminal screw: recommended: 1.6 ± 0.1 N.m maximum : 2.0 N.m
GENERAL CHARACTERISTICS
DPMT
SMALL MODEL CIRCUIT BREAKER THREE POLE
|| WWW.CROUZET-AEROSPACE.COM || 21 || ELECTRICAL PROTECTION  DISTRIBUTION
DIMENSIONS
CURVES
Trip times envelope for temperature from -55°C to
125°C (direct overload) Rating 1.5 ➞ 5 A 7.5 ➞ 25 A
Non tripping
point at 25°C
1.15 * RC 1.15 * RC
Tripping point
at 25°C
1.4 * RC 1.4 * RC
Tripping time
at 2 * RC
2 s ➞ 15 s 4 s ➞ 20 s
Non tripping
point at 125°C
1 * RC 1 * RC
Maximum and minimum limit of ultimate trip
20
10
5
4
3
2
In
10 2
-2
3 45 10-1
2 3 45 1 2 3 45 2 3 45 2 3 4
1.10
1.40
1.60
510 100 1000
+23C
-55C
+125C
84 310 0 - 3 - 6
84 314 2
-60
-20
-40
0
20
40
60
80
100
120
0,8 In 1,2 1,4 1,6 1,8
Non-trip threshold
Trip threshold
Current
(as percentage of In)
Ambiant
temperature
°C
2
84 310 0 - 3 - 6
84 314 2
PANEL CUTOUT RECOMMENDATION
› Thickness: 1.6 mm ➞ 3 mm
84 411 0	 84 412 0
84 413 0	
30min.
9,5
Ø12,5
50 min.
Ø3
84 414 0
30min.
9,5
Ø11,5
50 min.
Ø3
84 411 6 	 84 411 8	
84 412 8	 84 413 6
35min.
9,5
Ø12,5
50 min.
Ø3
84 411 0	 84 412 0
84 413 0	 84 414 0
84 411 6 	 84 411 8	
84 412 8	 84 413 6
|| WWW.CROUZET-AEROSPACE.COM || 22 || ELECTRICAL PROTECTION  DISTRIBUTION
Rating
No signal
contact
No signal contact
long trip time
Non polarised/polarised
signal contact
Polarised
signal contact
15 A 84 306 015
20 A 84 306 020 84 306 016 84 306 320/620 84 306 316/616 84 306 645/655
25 A 84 306 025 84 306 017 84 306 325/625 84 306 317/617 84 306 643/653
30 A 84 306 030 84 306 330/630
35 A 84 306 035 84 306 018 84 306 835 84 306 335/635 84 306 318/618 84 306 644/654
40 A 84 306 080 84 306 340/640
50 A 84 306 050 84 306 019 84 306 850 84 306 350/650 84 306 319/619 84 306 642/652
60 A 84 306 860
REFERENCES
Button
Green color • • • •
Black color • •
Conformity standard
EN 2794 003 004
EN 3661 004 005 005 006
BACC 18R18X like •
Mass / MTBF / Vibration / Technical file
Without mounting hardware 61 61 66
With mounting hardware 65 65 70
MTBF FH (Typical)  10 M  10 M  6 M
MIL vibration condition Sinus/Random A  C A  C A  C
Technical File - SP4393 - - SP4339 SP9300
Environmental
Salt spray 48h / 5% NaCl
Humidity: Test b RTCA DO160 / 10 cycles
Operating temperature -60°C +125°C
Acceleration (centrifugal) up to 17g
Shock 50 g 3 halfsine 11 msec 6 directions
Vibration (sinusoidal) 10 g-PK from 70 to 20000 Hz (MIL STD202 method 204 D condition A with 90 % of RC)
Vibration (random at RC) 9.26 Grms (MIL STD202 method 214 A condition C with 90 % of RC)
Mechanical
Operating force 3,5Npush55N / 5Npull40N
Endurance (manual open/close)
no load : 5 000 cycles
on resistive load : 2 500 cycles
Tightening torque barrel nut: recommended: 4 ± 0.25 N.m maximum : 5.5 N.m terminal screw: recommended: 2.35 ± 0.15 N.m maximum : 2.5 N.m
Electrical
28 VDC 115 VAC (400 Hz) 115 VAC 60 Hz-230 VAC 50Hz
Breaking current 1co + 2OCO 4000 A ; 2000 A long trip 2000 A ; 1500 A long trip
CONTACT CROUZET AEROSPACE
Dielectric 1500 V 1500 V
Endurance (electric overloads) 5000 (with L/R: 5 ms) 5000 (with cos fi: 0.7)
Insulation resistance above 100 MΩ above 100 MΩ
Working life (endurance) at 5xRC 50 cycles 50 cycles
Voltage drop compliance EN2794/3661 EN2794/3661
GENERAL CHARACTERISTICS
DGMU
BIG MODEL CIRCUIT BREAKER SINGLE POLE
Mounting hardware
Threaded
barrel
M12-0.75 • • • • • •
M12-100
7/16
Terminal
Screw
8-32 UNC • • • •
M4 • •
Hole ø5.5 for Bus-Bar •
|| WWW.CROUZET-AEROSPACE.COM || 23 || ELECTRICAL PROTECTION  DISTRIBUTION
DIMENSIONS
CURVES
Standard trip time (EN compliant) Long trip time (BACC compliant)
20
10
5
4
3
2
In
10 2
-2
3 45 10-1
2 3 45 1 2 3 45 2 3 45 2 3 4510 100 1000
-55C
84 306 0 - 6 - 8
+125C
+23C
0,90
1.10
1.45
1.65
20
10
5
4
3
2
In
10 2-2
3 45 10-1
2 3 45 1 2 3 45 2 3 45 2 3 4510 100 1000
-55C
84 306 835
+125C
+25C
55max
4823
22
34 max.
21
M12 x 0,75
9,5
3
m
ax.
7
m
in.
Ø2
19,5max.
1 2
84 306 0
3min.
6,6
1-3max.
18
10 min.
Ø10,4
84 306 0  84 406 8
55max
26,5
1-3max.
18
4823
22
28max.
34 max.
10 min.
10 min.
Ø10,4
21
25 max.
M12 x 0,75
42 max.
9,5
3
m
ax.
7
m
in.
Ø2
19,5max.
4
1 2
3
84 306 3
3min.
6,6
84 306 3
55max
26,5
1-3max.
18
4823
22
28max.
34 max.
10 min.
10 min.
Ø10,4
21
25 max.
M12 x 0,75
42 max.
9,5
3
m
ax.
7
m
in.
Ø2
19,5max.
1 2
84 306 6
3min.
6,6
5 3
84 306 6
84 306 6 Bus-Bar EN 3661-006 PANEL CUTOUT RECOMMENDATION
› Thickness 1.6 mm ➞ 3 mm
Versions 84 306 0 - 3 - 6
45min.
9,5
Ø12,5
25 min.
Ø3
84 306 6 Bus-Bar EN 3661-006
|| WWW.CROUZET-AEROSPACE.COM || 24 || ELECTRICAL PROTECTION  DISTRIBUTION
Conformity standard
EN 2665 003 004
EN 3662 004 005 005 006
10-60806 like •
Weight (g)
Without mounting hardware 156 156 161
With mounting hardware 165 165 170
MTBF FH (Typical)  5 M  5 M  26 M
MIL vibration condition Sinus/Random A  C A  C A  C
Technical File - SP4393 ASNE459 - - SP4340 SP4346
Button
Green color • • • •
Black color • • •
Rating No signal contact
No signal contact
long trip time
Non polarised/polarised signal
contact
Polarised signal
contact
15 A 84 313 015
20 A 84 313 020 84 313 036 84 313 061 84 313 820 84 313 320/620 84 313 316/613 84 313 621/631
25 A 84 313 025 84 313 037 84 313 062 84 313 825 84 313 325/625 84 313 317/617 84 313 622/632
30 A 84 313 330/630
35 A 84 313 035 84 313 038 84 313 063 84 313 840 84 313 335/635 84 313 318/618 84 313 623/633
41 A 84 313 041
50 A 84 313 050 84 313 058 84 313 066 84 313 850 84 313 350/650 84 313 319/619 84 313 624/634
60 A 84 313 860
REFERENCES
Electrical
115/200 VAC (400 Hz) 115/200 VAC 60 Hz-230/400 VAC 50 Hz
Breaking current 1CO + 2OCO 2000 A ; 1500 A long trip
CONTACT CROUZET AEROSPACE
Dielectric 1500 V
Endurance (electric overloads) 5000 (with cos fi: 0.7)
Insulation resistance above 100 MΩ
Working life (endurance) at 5xRC 50 cycles
Auxiliary contact current 0.1..0.2 A
Voltage drop compliance EN2665/3662
Environmental
Salt spray 48h / 5% NaCl
Humidity: Test b RTCA DO160 / 10 cycles
Operating temperature -55°C +90°C
Acceleration up to 40 g
Shock 50 g 3 halfsine 11 msec 6 directions
Vibration (sinusoidal) 10 g-PK from 70 to 20000 Hz (MIL STD202 method 204 D condition A with 90 % of RC)
Vibration (random at RC) 9.26 Grms (MIL STD202 method 214 A condition C with 90 % of RC)
Mechanical
Operating force 20Npush80N / 5Npull45N
Endurance (manual open/close)
no load : 5000 cycles
on resistive load : 2500 cycles
Tightening torque barrel nut: recommended: 4 ± 0.25 N.m maximum: 5.5 N.m terminal screw: recommended: 2.35 ± 0.15 N.m maximum : 2.5 N.m
GENERAL CHARACTERISTICS
DGMT
BIG MODEL CIRCUIT BREAKER THREE POLE
Mounting hardware
Threaded
barrel
M12-0.75 • • • • • • •
M12-100
7/16
Terminal
Screw
8-32 UNC • • • • • •
M4 •
Hole ø5.5 for Bus-Bar • •
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DIMENSIONS
CURVES
Standard trip time (EN compliant) Long trip time (BACC compliant)
20
10
5
4
3
2
In
10 2
-2
3 45 10-1
2 3 45 1 2 3 45 2 3 45 2 3 4510 100 1000
-55C
84 313 0 - 6 - 8
+90C
1.10
1.40
1.60
+23C
20
10
5
4
3
2
In
10 2
-2
3 45 10-1
2 3 45 1 2 3 45 2 3 45 2 3 4510 100 1000
-55C
84 306 835
+90C
+25C
84 313 0
1 2
55max
4823
22
21
M12 x 0,75
3
m
ax.
7
m
in.
3min.
6,6
C1
C2 B2 A2
C1 A1
B1 A1
34max.
1-3max.
18
Ø10,4
10 min.
17,5 17,5
54 max.
B1
9,5
2
84 313 0
84 313 3
1 2
55max
4823
22
28max.
21
25 max.
M12 x 0,75
3
m
ax.
7
m
in.
3min.
6,6
C1
C2 B2 A2
C1 A1
B1 A1
26,5
34max.
42max.
1-3max.
18
10 min.
Ø10,4
10 min.
17,5 17,5
54 max.
B1
9,5
2
19,5 max.
4 3
84 313 3 - 84 313 6
PANEL CUTOUT RECOMMENDATION
› Thickness 1.6 mm ➞ 3 mm
Versions 84 313 0 - 3 - 6
45min.
9,5
Ø12,5
60 min.
Ø3
Versions Bus-Bar EN 3662-006
45min.
9,5
9,5 9,5
Ø12,5
60 min.
Ø3
84 313 6
1 2
55max
4823
22
28max.
21
25 max.
M12 x 0,75
3
m
ax.
7
m
in.
3min.
6,6
5 3
C1
C2 B2 A2
C1 A1
B1 A1
26,5
34max.
42max.
1-3max.
18
10 min.
Ø10,4
10 min.
17,5 17,5
54 max.
B1
9,5
2
19,5 max.
84 313 6 Bus-Bar EN 3662-006
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Button color
Green
Black • • • • •
Rating 1 pole 45° 1 pole 45° 1 pole 60° 3 pole 45° 3 pole 60°
0.5 A 84 406 011
1 A 84 406 001 84 437 001 84 437 201 84 417 001 84 417 201
2 A 84 406 002 84 437 002 84 437 202 84 417 002 84 417 202
2.5 A 84 406 012 84 437 012 84 437 212 84 417 012 84 417 212
3 A 84 406 003 84 437 003 84 437 203 84 417 003 84 417 203
4 A*
5 A 84 406 005 84 437 005 84 437 205 84 417 005 84 417 205
6 A*
7.5 A 84 406 007 84 437 007 84 437 207 84 417 007 84 417 207
10 A 84 406 010 84 437 010 84 437 210 84 417 010 84 417 210
15 A 84 406 015 84 437 015 84 437 215 84 417 015 84 417 215
20 A 84 406 020 84 437 020 84 437 220 84 417 020 84 417 220
25 A 84 406 025 84 437 025 84 437 225 84 417 025 84 417 225
30 A 84 437 030 84 437 230 84 417 030 84 417 230
Mounting hardware
Threaded
barrel
M12-0.75
M12-100 • • • •
7/16 •
Terminal
Screw
6-32 UNC •
M4 • • • •
REFERENCES
Conformity standard
EN 2495* • • •
EN 2995* • • •
EN 2592* • •
EN 2996* • •
EN 3774* • •
MS26574 ** •
* for performance ** for terminal configuration
Mass/MTBF/technical file
Weight without mounting hardware (g)  18  18  19  54  56
Weight with mounting hardware (g)  20  20  21  63  65
MTBF FH (Typical)  7.2 M  7.2 M  7.2 M  1.7 M  1.7 M
Technical file SP 990100 SP 991700 SP 992000 SP 991900 SP 992100
Environmental
Salt spray 48h 5% NaCl
Humidity: Test b RTCA DO160 10 cycles
Operating temperature -60°C +125°C for all ratings except 30 A: - 60°C + 90°C
Acceleration (centrifugal) up to 40 g
Shock 50 g 3 halfsine 11 msec
Vibration (sinusoidal) single pole 15 g-PK from 70 to 2000 Hz (MIL STD 202 method 214G condition B with 90% of RC) at 23°C
Vibration (random) single pole 16.91 Grms (MIL STD 202 method 204D condition E with 90% of RC) at 23°C
Mechanical
Operating force 3,5N push45N / 5Npull30N 8Npush80N / 5Npull80N
Endurance
mechanical (no load) 5 000 cycles mechanical (no load) 5000 cycles
on resistive load 2 500 cycles on resistive load 2500 cycles
Tightening torque (barrel nut) recommended: 4 ± 0.25 N.m maximum : 5.0 N.m recommended: 4±0.25 N.m maximum: 5.0 N.m
Tightening torque (terminal screw) recommended: 1.6 ± 0.1 N.m maximum : 2.0 N.m recommended: 1.6±0.1 N.m maximum: 2.0 N.m
Electrical Single Pole Three pole
28 VDC 115 VAC (400 Hz) 115/200 VAC (400 Hz)
Breaking current 1CO + 2OCO 6000 A 2500 A 2000 A
Dielectric 1500 V 1500 V 1500 V
Endurance cycles 5000 (with L/R: 5 ms) 5000 (with cos fi: 0.7) 5000 (with cos fi: 0.7)
Insulation resistance above 100 MΩ above 100 MΩ above 100 MΩ
Working life (endurance) at 5xRC 50 cycles 50 cycles 50 cycles
Auxiliary contact current (if present) 0.1..0.2 A 0.1..0.2 A 0.1..0.2 A
Voltage drop compliance EN2495/2995/MS3320/AS33201 EN2495/2995/MS3320/AS33201 MS14154/AS14154A/EN2592/2996/3774
GENERAL CHARACTERISTICS
SMALL MODEL CIRCUIT BREAKER
FROG LEGS TERMINALS
* contact Crouzet Aerospace for this rating
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FROG LEGS CONNECTION
three pole
20
10
5
4
3
2
In
10 2
-2
3 45 10-1
2 3 45 1 2 3 45 2 3 45 2 3 4
1.10
1.40
1.60
510 100 1000
+23C
-55C
+125C
84 310 0 - 3 - 6
84 314 2
DIMENSIONS
PANEL CUTOUT RECOMMENDATION
CURVES
Trip times envelope for temperature from -55°C to 125°C (direct overload)
Rating 1.5 ➞ 5 A 7.5 ➞ 25 A
Non tripping
point at 25°C
1.15 * RC 1.15 * RC
Tripping point
at 25°C
1.4 * RC 1.4 * RC
Tripping time
at 2 * RC
2 s ➞ 15 s 4 s ➞ 20 s
Non tripping
point at 125°C
1 * RC 1 * RC
Maximum and minimum limit
of ultimate trip
20
10
5
4
3
2
In
10 2
-2
3 45 10-1
2 3 45 1 2 3 45 2 3 45 2 3 4510 100 1000
+125C +25C
-55C
84 400 0 - 6 - 8
84 400 0 - 6 - 8
84 400 0 - 6 - 8
84 405 0
single pole
84 406 0 - 84 437 0 - 84 437 1
84 437 2 84 417 2
84 417 0 - 84 417 1
› Thickness 1.6 mm ➞ 3 mm
Versions 84 406 0
30min.
9,5
Ø11,5
20 min.
Ø3,5
Versions	 84 437 0
84 437 1 - 84 437 2
30min.
9,5
Ø12,5
20 min.
Ø3
Versions	 84 417 0 - 84 417 1
84 417 20
30min.
9,5
Ø12,5
50 min.
Ø3
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Button
Green color •
Black color • • •
Long neck (long button) • •
Rating no auxiliary contacts no auxiliary contacts no polarised/polarised         no auxiliary contacts
0.5 A 84 408 111 84 418 011
1 A 84 408 001 84 408 101 84 408 601/801 84 418 001
2 A 84 408 002 84 408 102 84 408 602/802 84 418 002
2.5 A 84 408 012 84 408 112 84 408 612/812 84 418 012
3 A 84 408 003 84 408 103 84 408 603/803 84 418 003
4 A 84 408 004 84 408 104 84 408 604/804 84 418 004
5 A 84 408 005 84 408 105 84 408 605/805 84 418 005
6 A 84 408 006 84 408 106 84 408 606/806 84 418 006
7.5 A 84 408 007 84 408 107 84 408 607/807 84 418 007
10 A 84 408 010 84 408 110 84 408 610/810 84 418 010
15 A 84 408 015 84 408 115 84 408 615/815 84 418 015
20 A 84 408 020 84 408 120 84 408 620/820 84 418 020
25 A 84 408 025 84 408 125
84 408 625/825
available in 2016
84 418 025
Mounting hardware
Straight terminals without screws • • • •
Barrel threadings
Conical barrel • • • •
SMALL MODEL CIRCUIT BREAKER FASTON CONNECTION
PUSH-PULL PUSH-FIT 6.35 MM BLADE
REFERENCES
Conformity standard
EN 2495* • •
EN 2995* 004 005
EN3773-006 • •
EN3774-006 •
AS 33201 • • •
* for thermal performance and auxiliary contact performance
Mass/MTBF / Technical file
No mounting hardware  14,5  15,5  16,5  51
MTBF FH (Typical)  7.2 M  7.2 M  3.6 M  1.7 M
Technical file SP 991600 SP 991800 SP 991800 SP 991500
Environmental
Salt spray 48h 5% NaCl
Humidity: Test b RTCA DO160 10 cycles
Operating temperature -60°C +125°C for all ratings except 30 A: - 60°C + 90°C
Acceleration (centrifugal) up to 40 g
Shock 50 g 3 halfsine 11 msec
Vibration (sinusoidal) single pole 10 g-PK from 70 to 2000 Hz (MIL STD 202 method 204 D condition B with 90% of RC)
Vibration (random) single pole 9.26 Grms (MIL STD 202 method 214 A condition E with 90% of RC)
Mechanical
Operating force 3,5N push45N / 5Npull30N 8Npush80N / 5Npull80N
Endurance
mechanical (no load) 5 000 cycles mechanical (no load) 5000 cycles
on resistive load 2 500 cycles on resistive load 2500 cycles
Tightening torque (barrel nut) recommended: 4 ± 0.25 N.m maximum : 5.0 N.m recommended: 4 ± 0.25 N.m maximum : 5.0 N.m
Tightening torque (terminal screw) recommended: 1.6 ± 0.1 N.m maximum : 2.0 N.m recommended: 1.6 ± 0.1 N.m maximum : 2.0 N.m
Electrical Single pole Three pole
28 VDC 115 VAC (400 Hz) 115/200 VAC (400 Hz)
Breaking current 1CO + 2OCO 6000 A 2500 A 2000 A
Dielectric 1500 V 1500 V 1500 V
Endurance cycles 5000 (with L/R: 5 ms) 5000 (with cos fi: 0.7) 5000 (with cos fi: 0.7)
Insulation resistance above 100 MΩ above 100 MΩ above 100 MΩ
Working life (endurance) at 5xRC 50 cycles 50 cycles 50 cycles
Auxiliary contact current (if present) 0.1..0.2 A 0.1..0.2 A 0.1..0.2 A
Voltage drop compliance EN2495/2995/MS3320/AS33201 EN2495/2995/MS3320/AS33201 MS14154/AS14154A/EN2592/2996/3774
GENERAL CHARACTERISTICS
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PUSH-FIT 0.25 INCH TAB
DIMENSIONS
› Thickness: 1.6 mm for ring gasket
PANEL CUTOUT RECOMMENDATION
CURVES
Trip times envelope for temperature from -55°C to
125°C (direct overload) Rating 1.5 ➞ 5 A 7.5 ➞ 25 A
Non tripping
point at 25°C
1.15 * RC 1.15 * RC
Tripping point
at 25°C
1.4 * RC 1.4 * RC
Tripping time
at 2 * RC
2 s ➞ 15 s 4 s ➞ 20 s
Non tripping
point at 125°C
1 * RC 1 * RC
Maximum and minimum limit of ultimate trip
20
10
5
4
3
2
In
10 2
-2
3 45 10-1
2 3 45 1 2 3 45 2 3 45 2 3 4510 100 1000
+125C +25C
-55C
84 400 0 - 6 - 8
84 400 0 - 6 - 8
84 400 0 - 6 - 8
84 405 0
-60
-20
-40
0
20
40
60
80
100
120
0,8 In 1,2 1,4 1,6 1,8 2
84 400 0 - 6 - 8
84 400 0 - 6 - 8
84 400 0 - 6 - 8
84 405 0
Non-trip threshold
Trip threshold
Current
(as percentage of In)
Ambiant
temperature
°C
84 408 1
84 418 0
84 408 0
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Rating Faston Flying leads
1 A 84 405 001
1.5 A 84 405 040
2 A 84 405 002
2.5 A 84 405 012
3 A 84 405 003
5 A 84 405 005 84 405 045
7.5 A 84 405 007
10 A 84 405 010
15 A 84 405 015
20 A 84 405 020
25 A 84 405 025
REFERENCES
Button color
White • •
Mounting hardware
Faston terminal Barrel nut M12-100 + 500mm flying leads
Conformity standard
Air 6 625-403 • •
GAM TI-II-40 • •
EN 3773-3774* • •
* our equipment complies with EN standards
Mass / MTBF / Technical file
Weight  15  25
MTBF FH (Typical)  3.6 M  3.6 M
Technical file SP 4397  SP 9925
Environmental
Salt spray 48h 5% NaCl
Humidity: Test b RTCA DO160 10 cycles
Operating temperature -60°C +125°C
Acceleration up to 20 g
Shock up to 50 g (11 ms)
Vibration (sinusoidal) 10 g-PK from 10 to 2000 Hz
Vibration (random at RC) up to 9.26 Grms from 10 to 2000 Hz
Mechanical
Operating force
Endurance
no load 40 000 cycles
on resistive load 40 000 cycles
Tightening torque (barrel nut) recommended: 4 N.m ; Max.: 5 N.m
Tightening torque (terminal screw) 1.7 N.m +-0.1
Electrical
28 VDC 115 VAC (400 Hz) 115 VAC 60 Hz-230 VAC 50 Hz
Breaking current 1CO + 2OCO 3000 A 1500 A
CONTACT Crouzet Aerospace
Dielectric 1500 V 1500 V
Endurance cycles 5000 5000
Insulation resistance above 100 MΩ above 100 MΩ
Working life (endurance) at 5° RC 1000 cycles 1000 cycles
Auxiliary contact current 0.1..0.2 A 0.1..0.2 A
Voltage drop compliance EN2495/2995/MS3320/AS33201 EN2495/2995/MS3320/AS33201
GENERAL CHARACTERISTICS
SINGLE POLE SMALL MODEL CIRCUIT BREAKER
PUSH-PUSH  FLYING LEADS VERSION
Read also p. 46
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1,5
12,8
28max.
9,2
84 405 0
19,8 max.
2
9,5
14,3max.
Ø8,4
0,8
Ø11
17,4
6,35
6,3
5,9
DIMENSIONS
PANEL CUTOUT RECOMMENDATION
84 405 0 84 405 040
Version 84 405 0 Version 84 405 04X
› Thickness 1.6 mm ➞ 3 mm
9,5
Ø3,1
Ø12,5
30min.
9,5
Ø12,5
20 min.
Ø3
CURVES
Trip times envelope for temperature from -55°C to
125°C (direct overload)
Maximum and minimum limit of ultimate trip
20
10
5
4
3
2
In
10 2
-2
3 45 10-1
2 3 45 1 2 3 45 2 3 45 2 3 4510 100 1000
+125C +25C
-55C
84 400 0 - 6 - 8
84 400 0 - 6 - 8
84 400 0 - 6 - 8
84 405 0
-60
-20
-40
0
20
40
60
80
100
120
0,8 In 1,2 1,4 1,6 1,8 2
84 400 0 - 6 - 8
84 400 0 - 6 - 8
84 400 0 - 6 - 8
84 405 0
Non-trip threshold
Trip threshold
Current
(as percentage of In)
Ambiant
temperature
°C
Rating 1 ➞ 3 A 5 ➞ 25 A 5 ➞ 25 A
Non tripping
point at 25°C
1.15 In 1.15 In 1.15 In
Tripping point
at 25°C
1.4 In 1.4 In 1.4 In
Tripping time
at 2 * RC
2 s ➞ 15 s 4 s ➞ 16 s 6 s ➞ 20 s
Non tripping
point at 125°C
In In In
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Button color
Green •
Black • •
Rating GFCB (star)** Three pole AFCB Single pole AFCB
1 A
3 A 84 411 136 84 411 103 84 401 503
5 A 84 411 137 84 411 105 84 401 505
7.5 A 84 411 138 84 411 107 84 401 507
10 A 84 411 139 84 411 110 84 401 510
15 A 84 411 140 84 411 115 84 401 515
20 A 84 411 141 84 411 120 84 401 520
25 A 84 411 142 84 411 125 84 401 525
** on request the GFCB is available in star or triangle configuration with different thresholds
Mounting hardware
Threaded
barrel
M12-0.75
M12-100 • • •
7/16
Terminal
Screw
8-32 UNC • • •
M4
REFERENCES
Conformity standard
EN 2592 - EN 2996* • •
EN 2495* •
AS 5692 • • •
* for thermal part
Mass / MTBF / Technical file
Without mounting hardware  141  141  31
With mounting hardware  150  150  33
MTBF FH (Typical)  150 000  150 000  450 000
Environmental
Salt spray According DO160 section 14 category B
Humidity According DO160 section 6 category B
Operating temperature (1 to 15 A) -60°C +125°C
Operating temperature (20 and 25 A) -60°C +90°C
Operating temperature (Arc fault and ground fault detection) -40°C +71°C
Acceleration (centrifugal) 17g
Shock up to 50 g (11 ms) -1/2 sine
Vibration (sinusoidal) 10 g-PK from 5 to 2000 Hz
Vibration (random at RC) 5.82 Grms from 10 to 2000 Hz
Mechanical
Operating force 8Npush80N 5Npull30N
Endurance
no load 5 000 cycles
on resistive load 5 000 cycles
Tightening torque (barrel nut) recommended: 4 N.m ; Max.: 5 N.m
Tightening torque (terminal screw) 1.7 N.m +-0.1
Electrical
115/200 VAC (400 Hz)
Breaking current 1CO + 2OCO 2000 A
Dielectric 1500 V
Endurance cycles 5000 (with cos fi: 0.7)
Insulation resistance above 100 MΩ
Working life (endurance) at 5° RC 50 cycles
Auxiliary contact current 0.1..0.2 A
Voltage drop compliance MS14154/AS14154A/EN2592/2996/3774
GENERAL CHARACTERISTICS
GROUND FAULT  ARC FAULT CIRCUIT BREAKER
GFCB AND AFCB
Read also p. 8-11
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DIMENSIONS
PANEL CUTOUT RECOMMENDATION
CURVES
84 401 5
84 401 5
84 411 1
84 411 1
› Thickness 1.6 mm ➞ 2.4 mm
› Thermal trip
› Arc fault trip: Compliant with AS5692
› Ground fault trip thresholds
Trip times envelope for temperature from -60°C
to 125°C (direct overload)
20
10
5
4
3
2
In
10 2-2
3 45 10-1
2 3 45 1 2 3 45 2 3 45 2 3 4
1.10
1.40
1.60
510 100 1000
+23C
-55C
+125C
84 310 0 - 3 - 6
84 314 2
-60
-20
-40
0
20
40
60
80
100
120
0,8 In 1,2 1,4 1,6 1,8
Non-trip threshold
Trip threshold
Current
(as percentage of In)
Ambiant
temperature
°C
2
84 310 0 - 3 - 6
84 314 2
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84 404 011 84 404 004 84 313 626 84 404 00784 411 860
Small Model Single Pole
Description Aux. contact Ref. Conformity
Barrel threadings Terminal screw
Control button
M12-0.75 M12-100 7/16 H8-32 CB M4
DPMU Yes 84 404 002 E0486A01 • Pushed in
Push push faston No 84 404 003 • Without
DPMU No 84 404 004 • • Pushed in
DPMU No 84 404 005 • • Popped out
DPMU Yes 84 404 006 E0486B01 • Without
Frog legs No 84 404 009 • 6-32UNC2A Without
Frog legs Yes 84 404 010 • 6-32UNC2A Without
One terminal DPMU No 84 404 011 • • Pushed in
Frog legs Yes 84 404 013 • • Without
Small Model Three Pole
Description Aux. contact Ref. Conformity
Barrel threadings Terminal screw
Control button
M12-0.75 M12-100 7/16 H8-32 CB M4
DPMT Yes 84 404 007 E0486B03 • Without
DPMT Yes 84 411 860 E0486A03 • Pushed in
Big Model Single Pole
Description
Aux.
contact
Ref. Conformity
Barrel threadings Terminal screw
Control button
M12-0.75 M12-100 7/16 H8-32 CB M4
84 306 xxx
Big Model Three Pole
Description Aux. contact Ref. Conformity
Barrel threadings Terminal screw
Control button
M12-0.75 M12-100 7/16 Bus-bar CB M4
DGMT Yes 84 313 626 E0486A04 • • Pushed in
DGMT No 84 313 044 E0486A04 • Pushed in
REFERENCES
DUMMY CIRCUIT BREAKER
DUMMY  SIMULATOR CB
Based on «standard» or «catalog CBs» (in the light blue column) the dark grey column gives the references of the Simulator CBs:
Standard Simulator Standard Simulator Standard Simulator Standard Simulator Standard Simulator
Rate (A)
EN3661-004
green button
same with
black button
844006
green button
same with
black button
844026
green button
same with
black button
844006
green button
same with
black button
rotated 180°
EN2495-M
0.5 A Rating
same with
different
button value
DGMU DGMU DPMU DPMU DPMU DPMU DPMU DPMU DPMU DPMU
0.5 84400611 84400650 84400611 84400636 84402011
0.75 84400637
1 84400601 84400651 84400601 84400638
1.5 84400652 84400639
2 84400640
2.5 84400612 84402612 84402712 84400612 84400641
3 84400603 84400653 84402603 84402703 84400603 84400642 84402036
4 84400604 84400654 84400604 84400643
5 84400605 84400655 84402605 84402705 84400605 84400644 84402037
7.5 84400607 84400656 84402607 84402707 84400607 84400645 84402038
10 84400610 84400657 84402610 84402710 84400610 84400646 84402039
15 84400615 84400658 84402615 84402715 84400615 84400647 84402040
20 84400620 84400659 84402620 84402720 84400620 84400648 84402041
25 84306325 84306353 84400625 84400661 84402625 84402725 84400625 84400649 84402042
30 84400630 84400662
35 84306335 84306352 84402043
50 84306350 84306351
no marking 84402044
mounting hw mounting hardware on CB mounting hardware in bag mounting hardware on CB mounting hardware on CB mounting hardware on CB
CHOICE BY STANDARD/RATING
Read also p. 46
and p. 49
SELECTION GUIDE FOR SIMULATOR CBs
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PANEL CUTOUT RECOMMENDATION
DIMENSIONS
84 404 001
84 404 01184 404 006
84 404 007
› Thickness 1.6 mm ➞ 3 mm
Please, refer to the according technical file.
|| WWW.CROUZET-AEROSPACE.COM || 36 || ELECTRICAL PROTECTION  DISTRIBUTION
Rating
red gag 23 422 009
grey cap panel hole diam 12.5mm 24 323 003
brown cap panel hole diam 12.5mm 24 323 005
opaque
covers
Barrel M12*1 79 254 157
Barrel M12*0.75 79 254 154
Barrel 15/32 79 254 155
Barrel 7/16 79 254 156
clear covers
(see
through)
Barrel M12*1 79 254 150
Barrel M12*0.75 79 254 151
Barrel 15/32 79 254 152
Barrel 7/16 79 254 153
male pin EN 3155 -016M 2018 25 637 611
Other information
crimping tool for pin 25637611: crimp tool: M22520/1-01 and crimp locator: M22520/1-02
insertion extraction tool: Ref. Deutsch: 020-0008-20
male pin Ref. Deutsch: 006-0912-20
Conformity Standard
IPX7 •
VG 95345 chap. 23 •
Gag Caps Covers Auxiliary contact pin
REFERENCES
ACCESSORIES
ACCESSORIES
DIMENSIONS
79 254 150-153-156-157 24 323 003	 24 323 005	
23 422 009
EC 79 25 40 85
25 637 611
79 254 150
Safety guard
Nut
Seal
Connector pins for auxiliary contacts:
EN 3155 - 016 M2018
Wire gage: 18 to 24 (0.21 to 0.93mm2
)
Caution: For good water proofness: the CB pannel must be
2.5 mm thick and positioning key hole must be «blind». Torque
of 4 N.m must be applied to the nut ; not on the cover.
Extraction tool
not supplied
Crimped
pin
|| WWW.CROUZET-AEROSPACE.COM || 37 || ELECTRICAL PROTECTION  DISTRIBUTION
ELECTRICAL DISTRIBUTION
SELECTION GUIDE
Crouzet Aerospace is proud to contribute towards the “greener Aircraft” through its bus connected components and
through its never ending quest for more compact and lighter solutions.
Crouzet Aerospace delivers 3 standard distribution components:
›› RCCB
›› A Circuit Breaker panel Kit
›› Solid State Circuit Breakers
With smart management, loads can be powered off during some flight phases and in rush current can be reduced. This
technique will decrease the electrical network complexity and weight. Using information provided by the load, SSCB and
RCCB’s role can encompass wire protection and load protection
LOAD AND WIRE PROTECTION WITH SSPC
LOAD AND WIRE PROTECTION WITH RCCB
|| WWW.CROUZET-AEROSPACE.COM || 38 || ELECTRICAL PROTECTION  DISTRIBUTION
CIRCUIT BREAKER PANEL KIT
PCB KIT FOR FASTON CB
complete panel PCB rings and spacers
complete panel 84 341 072
bottom spacer 79 2194 30
lateral spacer 79 219 431
central spacer 79 219 432
centring ring 79 219 333
EN 4165 connector support 79 219 440
PCB with 16 receptacles 79 219 439
front plate 79 219 441/42
Circuit Breaker type	
Faston without auxiliary contact (conical barrel) 84 406 039..84 406 048
Faston with auxiliary contact non polarised (conical barrel)	 XB 406 839..XB406 848
Faston without auxiliary contact polarised (conical barrel)	 XB 406 639..XB406 648
Weight (g)
Without standard CB (only mechanichal panel)  351
Panel with 16 Circuit Breakers  528
MTBF FH (Typical)  60 000
REFERENCES
Spacer kit
5 short spacers	
79 219 443one central spacer
five short spacer (below)
Connection possibilities
EN4165 (2 modules of 8 size 16 pins) with pins soldered on the vertical PCB
EN4165 (2 modules of 8 size 16 pins)	 held by 79219440 with crimped contact pins
Flying leads soldered on the vertical PCB	
Environmental
DO160 section Test category method
4 Altitude similarity
5 Temperature from -60°C..71°C (with power) test
6 Humidity test
7 Crash MIL STD 810E test
80 ms 1/2 sine (20 g on all axes)
8 Vibration MIL STD 810E helicopter test
random wide band+ sine strips
9 Explosion proofness demonstration
10 Waterproof N/A
11 Fluids N/A
12 Sand and dust similarity
13 Fungus resistance no tested
14 Salt spray 48h no power + 48h dry test
15 Magnetic effect demonstration
16 ➔ 23 EMI N/A
25 Inflammability FAR 25853 demonstration
Mechanical
torque (max) N.m
Power stud (M6) 3.9
Every screw/spacer (M3) 2
Locktite on every screw/spacer (not on power stud nut)
Electrical
Vehiculated current 15*4+6*10+6*5=150 A from -60°C to 71°C
Vehiculated power 150*28=4200 W
Prospective current (blocked mechanism) 1800 A 28 VDC (no copper tracks destruction)
Dielectric 700 VDC between 2 copper tracs and between each track and power feeder
GENERAL CHARACTERISTICS
Read also page 15
|| WWW.CROUZET-AEROSPACE.COM || 39 || ELECTRICAL PROTECTION  DISTRIBUTION
DIMENSIONS AND SPECIFIC ZONES FOR CB RATINGS CENTRING RING
PANEL CUTOUT RECOMMENDATION AND CIRCUIT BREAKER TYPE
PIN TO CB AFFECTATIONS
HOW DOES IT WORK?	
The assembly is qualified and distributes securely up to 150 A under 71°C with a configuration carrying four 15 A,
six 10 A and six 5 A Circuit Breakers (thus a total of 16 CBs).
The distribution connector can be mounted on the vertical PCB or distribution leads can be soldered on the vertical PCB.
EN4165
84 406 0XX	 XB406839 XB406639
connector EN 4165 8T16
› Thickness: 1.6 mm
Module A CB#
1 F6
2 F2
3 F1
4 F7
5 F3
6 F8
7 F5
8 F4
vertical PCB
to solder
connector
or flying
leads
power
feeder
›› If EN 4165 is soldered and used with leads the size 16 pins
limit the current to 13 A:
	
			
Max output:
			 4*13+6*10+6*5=142 A
›› If leads are soldered directly on the vertical PCB,
the maximum currents are:
Red zone: 15 A max
Yellow zone: 10 A max
} Max output:
Green zone: 5 A max
4*15+6*10+6*5=150 A
A B
Module B CB#
1 F9
2 F10
3 F14
4 F11
5 F15
6 F12
7 F13
8 F16
breakers up to 15 A breakers up to 10 A breakers up to 5 A
Layout 0816: 8 contacts size 16 x 2
|| WWW.CROUZET-AEROSPACE.COM || 40 || ELECTRICAL PROTECTION  DISTRIBUTION
REMOTE CONTROL CONTACTOR  CIRCUIT BREAKER
RCCB 115/200 VAC 360-800 HZ
Environmental
Salt spray 48h at 5% NaCl 48h at 5% NaCl
Operating temperature -40°C to +85°C -40°C to +85°C
Acceleration (centrifugal) up to 10 g up to 10 g
Shock 25 g - 11 ms 25 g - 11 ms
Vibration (sinusoïdal) 10 g from 5 to 2000 Hz 10 g from 5 to 2000 Hz
Vibration (random) 5.8 g from 10 to 2000 Hz 5.8 g from 10 to 2000 Hz
Mechanical
Operating force (R push button)  10 N  10 N
Max. admissible force (R push button) 50 N 50 N
Tightening torque (barrel nut) 3 +/- 0.2 Nm 3 +/- 0.2 Nm
Tightening torque (terminal screw) 2.3 +/-0.1 Nm 2.3 +/-0.1 Nm
Weight  550 g  700 g
MTBF FH (Typical)  300 000  300 000
Mounting hardware
Fixing screws (to panel or closet wall) 3 screws 10-32 UNF-3B 3 screws 10-32 UNF-3B
Connexion screws (to power feeders lugs) 6 screws 8-32 UNC-3A 6 screws 8-32 UNC-3A
Matched connector for control signals Air LB00 1748-120.00 Sub D 15 Female
Connector retaining screw M3x0.5 -
Contactor Function
Actuating voltage 17 V= ≤U≤32 V (a2 - a1 pins) 17 V= ≤U≤32 V (10 - 2 pins)
Max Pull-in current 3A during max 50 ms 3A during max 50 ms
Max. continuous hold-in current 300 mA 300 mA
Min. Hold-in voltage 10 V= 10 V=
Response time (off to on)  60 ms  60 ms
Release time ( on to off)  60 ms  50 ms
Direct visual indication of contacts position on front plate OPEN / CLOSE OPEN / CLOSE
Auxiliary contact n°1 SPDT type
Intermediate current level
Common/NC/NO: b1/c1/d1
28 VDC 3A (L/R 5 ms) - 5 VAC 250 mA
Common/NC/NO: 3/4/5
28 VDC 3A (L/R 5 ms) - 5 VAC 250 mA
Auxiliary contact n°2 SPDT type
Low level current
Common/NC/NO: b2/c2/d2
3 VDC 0 to 20 mA resistive
28 VDC 200 mA (L/R 5 ms)
Common/NC/NO: 6/7/8
3 VDC 0 to 20 mA resistive
28 VDC 200 mA (L/R 5 ms)
Dielectric stength I leakage  1 mA @ 1500 V~ I leakage  1 mA @ 1500 V~
Insulation resistance ≥ 100 MΩ ≥ 100 MΩ
Contactor Endurance cycles with RC at 40°C cos Fi=0.7 100 000 cycles 100 000 cycles
Current measurement  Breaker function
Current transformer ratio - 0.5 Volt rms for 10 A rms
Integrated load resistance (on current trasformer output) - 50 Ω
Breaking at 115 VAC 360-800 Hz 2000 A 2000 A
Trip status auxiliary contact (incorporated diode) 28 VDC 10 to 200 mA 28 VDC 10 to 200 mA
Visual indication of trip status by R button on front plate Yes Yes
Operating circuit disable after break Yes Yes
Resetting after trip By push on front R button By push on front R button
Endurance at 2*RC 1 000 cycles 1 000 cycles
GENERAL CHARACTERISTICS
Rating Without current transformer With current transformer
35 A 84 354 335 84 354 435
50 A 84 354 350 84 354 450
60 A 84 354 360 84 354 460
REFERENCES
C1 c2 b2 d2 c1 b1 d1 d3 c3 b3 a3 a2 a1B1 A1
C2 B2 A2
C1 c2 b2 d2 c1 b1 d1 d3 c3 b3 a3 a2B1 A1
Load
terminals
Output (current transformer)
Thermal detection by bimetal strips
Visual status
Indication
Block circuit diagram
Reset and
visual trip
Indication
Line
terminals
Auxiliary
contacts Trip
Command
a2:0V a1:28V
Management
part
Contactor
function
Circuit Breaker
function
Outputs to connector
Block circuit diagram
C1 7 6 8 411 12 13 14
QA QB QC
3 5 1 9 2 10B1 A1
C2 B2 A2
Current
transformer
Load
terminals
Thermal detection by bimetal strips
Visual status
Indication
Reset and
visual trip
Indication
Line
terminals
Auxiliary
contacts Trip
Command
2:0V 10:28V
Management
part
Contactor
function
Circuit Breaker
function
Outputs to connector Sub D1584 354 3XX 84 354 4XX
Read also page 16
|| WWW.CROUZET-AEROSPACE.COM || 41 || ELECTRICAL PROTECTION  DISTRIBUTION
DIMENSIONS
TRIPPING CHARACTERISTICS
HOW DOES IT WORK?
The RCCB merges a contactor function and a circuit breaker function in a single unit. This association gives the following
unique advantages:
›› Reduction of the length of generally large cross-sections wires (mass reduction and harness simplification)
›› Reduction of voltage drop (reduced number of contacts)
›› Reduction of volume
›› Improved reliability (less components)
The contactor is closed when 28 V is applied on the command input.
The RCCB has a status display window and a mechanical «TRIP
indicator». When the CB has tripped, the mechanical
«TRIP indicator» is «popped out» and must be pushed back
in manually to RESET the circuit breaker (see page 16).
The «protection function» overrides the «contactor function».
After tripping, the RCCB must therefore be reset manually,
this avoids any risk of spurious restarting.
Without current transformer With current transformer
-60
-20
-40
0
20
40
60
80
100
120
0,8 In 1,2 1,4 1,6 1,8
Non-trip threshold
Trip threshold
Current
(as percentage of In)
Ambiant
temperature
°C
2
84 310 0 - 3 - 6
84 314 2
20
10
5
4
3
2
In
10 2
-2
3 45 10-1
2 3 45 1 2 3 45 2 3 45 2 3 4
1.10
1.40
1.60
510 100 1000
+23C
-55C
+125C
84 310 0 - 3 - 6
84 314 2
40
5354,8
62
51
87,5
A2B2C2
Current transformer
casing
SUB D15
connector
Closet wall
mounting surface
10,2
6
1717
26,5
53
2
40
5354,8
62
57
34
53
66
76
88
A1B1C1
A2B2C2
Female connector
Air LB 00 1748 - 120.00
M3 x 0.6-6H
Minimum air gap for
ventilation
3 holes for bus bars: 5.5mm
3 lug connection
Range
indication
Status
indication
Closet wall
mounting surface
Manual Reset
Inputside
Outputside
3 floating nuts
for panel mounting
10-32 UNF-3B
Contactor
(3 phases)
Circuit breaker
(3 phases)
RCCB
(3 phases)
ALL IN ONE
To load
To load
Control
Control
333
3 3
|| WWW.CROUZET-AEROSPACE.COM || 42 || ELECTRICAL PROTECTION  DISTRIBUTION
SOLID STATE CIRCUIT BREAKER
SSPC 28 VDC  115 VAC  GFI
Environmental
DO160-G section Test 28 VDC 115 VAC
4 Operating temperature range -55 °C to +85 °C -55 °C to +85 °C
4 Storage temperature range -55 °C to +125 °C -55 °C to +125 °C
5 Temperature variation
8 Vibration
11 Contamination fluids
12 Sand and dust
13 Fungus resistance
14 Salt spray
17 Voltage spikes Category A Category A
18 Audio frequency conducted susceptibility Category R Category R
20 Conducted radio frequency susceptibility Category M Category M
20 Radiated radio frequency susceptibility Category B Category B
21 Emission of radio frequency energy Category M Category M
22 Lightning induced transient susceptibility Category B3H3L3 Category B3H2L2
25 Electrostatic discharges Category A Category A
Mass / MTBF / Other
Weight (g)  170  250
MTBF FH (Typical)  20 000  20 000
30 mA GFI option •
Electrical (overall) 28 VDC 115 VAC
Power supply 28 VDC (17 ➞ 46) 115 VAC / 380 ➞ 420 Hz
Maintenance supply 28 VDC (17 ➞ 46) 28 VDC (17 ➞ 46)
Maximum current consumption (SSPC Off) ≤ 40 mA ≤ 1 mA on 115 VAC
Maximum current consumption (SSPC On) ≤ 50 mA ≤ 100 mA on 28 VDC
Turn ON or turn OFF time ≤ 10 ms ≤ 10 ms
Guarantee no trip limit 1.15 x rating current 1.15 x rating current
Guarantee trip limit 1.40 x rating current 1.40 x rating current
Overload trip delay See curve next page See curve next page
Short circuit trip delay (8 x rated current) ≤ 3 ms  2 ms
Short circuit trip delay (20 x rated current) ≤ 0.5 ms ≤ 0.2 ms
Leakage current in Off state ≤ 10 µA ≤ 150 µA
Residual voltage in Off state ≤ 200 mV ≤ 7 V
GENERAL CHARACTERISTICS
Rating SSCB 28 VDC SSCB 115 VAC
2 84 332 052
3 84 332 053
5 84 332 043 84 332 054
10 84 332 040
15 84 332 044
20 84 332 041
REFERENCES
Conformity standard
EN 2592* • •
EN 2495* • •
AS 5692** •
AS 6019** •
* for thermal protection
** possible contact Crouzet Aerospace
Read also p.12  37
EASY TO INSTALL
1 - Power from feeder
2 - Power to the load
3 - In house ground (0 Volts)
4 - CAN BUS
5 - Optional Battery 28 V
1 - 115 VAC feeder
2 - 115 VAC Power to the load
3 - In house ground (0 Volts)
4 - CAN BUS
5 - Optional Battery 28 V
6 - 0 VAC feeder return (neutral)
7 - 0 VAC load return
28 VDC
LOAD LOAD
CAN 2.0B
1
5
5
3 3
6
2
4
1 2
7
4
CAN 2.0B
115 VAC28 VDC
LOAD LOAD
CAN 2.0B
1
5
5
3 3
6
2
4
1 2
7
4
CAN 2.0B
115 VAC
Small current
a few mA for
in house
power
Small current
a few mA for
in house
power
Current returns path inside chassis or fuselage
|| WWW.CROUZET-AEROSPACE.COM || 43 || ELECTRICAL PROTECTION  DISTRIBUTION
136 mm Max.
27mmMax.58mmMax.
11mm41.2mm
121.2 mm
A1 28V from feeder
8
1 GND
9 28 V optional
2 SPARE_IN_4
10 GND
3 SPARE_IN_1
11 CANH
4 SPARE_IN_2
12 CANL
5
12 GND
6 SPARE_IN_3
14 reserved
7 GND
15 reserved
A2 28 V LOAD
1 115 VAC to load
9 115 VAC from feeder
2 0 VAC feeder return
10
3 0 VAC feeder return (neutral)
11
4
12
5 SPARE_IN_1
13 SPARE_IN_2
6 SPARE_IN_3
14 CAN_L
7 CAN_H
15 GND
8 28 V optional
136 mm Max.
27mmMax.83mmMax.
11mm66.2mm
121.2 mm
DIMENSIONS AND PIN ASSIGNEMENT
CURVES
84 332 04X 84 332 05X
›› Connector is a Sub-D 17W2 male connector with 15
signal contacts and 2 power contacts.
›› Optional battery is used if the master controlling the CAN bus needs a reply from the SSCB even if feeder power is OFF.
Spare inputs (SPARE_IN_X) can be used for limit switch inputs or GROUND/FLIGHT information.
›› Connector is a Sub-D 15 contacts male connector.
The signal positions are given below.
› Trip delay versus current 28 VCD › Trip delay versus current 115 VAC
Fixation holes diameter: 5.2 mm Fixation holes diameter: 5.2 mm
0
2
4
6
8
10
12
14
16
18
20
1,E-04 1,E-03 1,E-02 1,E-01 1,E+00 1,E+01 1,E+02
I/In
Time (s)
0
2
4
6
8
10
12
14
16
18
20
1,E-04 1,E-03 1,E-02 1,E-01 1,E+00 1,E+01 1,E+02
I/In
Time (s)
|| WWW.CROUZET-AEROSPACE.COM || 44 || ELECTRICAL PROTECTION
Secondary network simulator Primary network simulator
INNOVATION  FUTURE PRODUCTS
TIME STAMPING CIRCUIT BREAKER FOR MAINTENANCE COST EVALUATION
Using a specific software, the electronic board included in the Circuit Breaker can measure the time an equipment has been
powered ON and transmit it to a portable device. This can be used to measure the real MTBF of the equipment.
The time stamping products give same thermal protection as a standard Circuit Breaker.
›› Can most often replace a standard Circuit Breaker
›› Will give «hours ON» figures to check «predictable maintenance costs» (for power by the hour applications)
DESIGN DEPARTMENT
Crouzet Aerospace engineers and technicians develop new mechatronic components using all state of the art tools and
methods.
›› COSMOS design for mechanical and thermal simulation
›› ProEngineer for mechanical conception and drawing
›› Altium and Pspice for electrical and electronic design and simulation
›› VISULA and ALTIUM for PCB design and routing
›› C_Compilers and VHDL for embedded software
FPGA and microcontroller software are developed according to DO178 and D0254 up to level A
Behavior of «prototypes» can be verified in our electrical lab environment that simulates primary and secondary aircraft
distributions with «real loads». Available power sources are 28 VDC and 115 VAC and 230 VAC.
|| WWW.CROUZET-AEROSPACE.COM || 45 || ELECTRICAL PROTECTION  DISTRIBUTION
FREQUENTLY ASKED QUESTIONS
1 HOW TO USE CIRCUIT BREAKERS WITH LOADS USING VERY LITTLE CURRENT
(EXAMPLE 100 mA):
Definition of wetting current: it is the minimum current needed to flow through a mechanical switch while it is operated
in order to break through any film of oxidation that may have been deposited on the switch contacts. It is the minimum
current that enables 20-25 years operation of the circuit breaker.
Example:
If you want to power a load that has a 100 mA current consumption. You cannot use a single AWG20 wire and a
0.5 A or a 1 A circuit breaker to protect the AWG20 wire because the wetting current of a circuit breaker is
250 mA ➞ it will not operate properly after 5-10 years in the field (voltage drop will be incorrect).
You must find another load (with a higher consumption than 250 mA; for instance a 2.3 A load) in the vicinity of your
100 mA load and use the circuit breaker and wire of «higher current load» in the following manner:
Junction blocs (from Amphenol AIR-LB):
Note:
You must ensure that by unpowering both loads
(i.e. by opening the breaker), you do not create a safety
hazard.
2 STORAGE DURATION  CIRCUIT BREAKER CYCLING (EXTRACT OF EN3773-001)
The storage duration under conditions of §13.2 shall be three years maximum. After a longer period, the following tests shall be
conducted before use:
›› Voltage drop at 2*RC
›› Tripping time at 2*RC
at the ambient temperature of 23 °C.
NOTE: Three to five switchings (cycling) shall be performed prior to check. If the second voltage drop measurement fails, the
circuit breakers have to be scrapped.
|| WWW.CROUZET-AEROSPACE.COM || 46 || ELECTRICAL PROTECTION
3 WHEN DO YOU NEED PUSH-PUSH CIRCUIT BREAKER?
With gloves it can be easier to use only one finger to open or close a protected line (rather than capture the button with index
and thumb and pull/push on it).
5 WHY USE FAKE (DUMMY) CIRCUIT BREAKERS?
When making a Circuit Breaker panel, you can require «Space» provisions for future loads (this is very frequent for helicopters
where configurations are modified just before customer delivery or in the field).
To reduce the delay time, OEM can want a pre-wired bus-bar and a pre-wired distribution wire and a fake Circuit Breaker.
The ‘fake’ or dummy Circuit Breaker will hold in place the bus bar and hold in place the distribution wire so that they do not
create shorts or hazards due to them being pre-wired and «loose» in the Circuit Breaker Panel. Such dummy Circuit Breakers
can also bare signal contacts if required.
›› They are lighter than normal breakers because they are «empty».
›› They do not convey current between their terminals.
›› The button can be permanently pushed in or popped out.
30min.
20 min.
20min.
17 min.
Push/Push
30min.
20 min.
20min.
17 min.
Push/Pull Activated Deactivated
Auxillary contacts galvanically isolated
from the power give information on the status
of the primary contacts.
6 HOW DO YOU USE AUXILIARY CONTACTS TO DETECT TRIPPED BREAKERS?
4 3
non polarised
5 3
polarised
The auxiliary contacts are closed when primary
contacts are open:
Power
Aux Aux
Load
34
21
Power
Aux Aux
Load
34
21
Diode type: 1N 4007
4 WIRE GAGE CIRCUIT BREAKER RATING ASSOCIATION
Small aircraft /helicopter
Calibre/ratedcurrent LUG color
Below or equal to 1 AWG 22 grey
1.5 ➞ 6 AWG 20 orange
7 ➞ 10 AWG 18 orange
11 ➞ 15 AWG 16 white
16 ➞ 20 AWG 14 white
21 ➞ 50 AWG 12 black
Large aircraft
Calibre/rated current LUG color
Below or equal to 1 AWG 20 grey
1.5 ➞ 6 AWG 18 orange
7 ➞ 10 AWG 16 orange
11 ➞15 AWG 14 white
16 ➞ 20 AWG 12 white
21 ➞ 50 AWG 10 black
Tripped
/popped out
Engaged
/pushed in
FREQUENTLY ASKED QUESTIONS
|| WWW.CROUZET-AEROSPACE.COM || 47 || ELECTRICAL PROTECTION  DISTRIBUTION
This implementation requires: 6 outputs +
1 ground going through a connector.
The information is processed by a computer
or connected to LEDs.
SETBACK: you need n+1 wires to monitor
n Circuit Breakers
A) SOLUTION FOR 6 CB (WITH NON POLARIZED AUXILIARY CONTACTS): DAISY CHAIN
B) SOLUTION FOR 6 CB (WITH NON POLARIZED AUXILIARY CONTACTS):
This implementation requires: 1 output + 1
ground =2 wires going through a connector.
SETBACK: you only know that one CB has
tripped but you do not know which one.
The information is processed by a computer
or connected to LEDs.
By duplicating the above grid layout:
›› 16 Circuit Breakers can be monitored with 4+4 lines = 8 lines (4 in - 4 out)= 24
›› 256 Circuit Breakers can be monitored with 8+8 = 16 lines (8 in - 8 out)= 28
›› 2n
Circuit Breakers can be monitored with n+n = 2xn lines (n input lines and n output lines
SETBACK: the information has to be processed by a microcontroller or an FPGA (or a CBMU).
represented this way:
C) SOLUTION FOR 16 TO 256 CB (WITH POLARIZED AUXILIARY CONTACTS):
By using auxiliary contacts with diodes
and a keyboard type interrogation:
|| WWW.CROUZET-AEROSPACE.COM || 48 || ELECTRICAL PROTECTION
7 HOW TO ASSOCIATE A LOAD WITH A CIRCUIT BREAKER AND A WIRE?
You must persuade yourself that a thermal Circuit Breaker protects the wire from smoking and igniting; it does not protect
the load. The following information is similar to EN3197.
STEP 1
Chose a CB rating between 15 % and 20 % above the nominal current to be carried through the wire. This provision is
needed because in the future, if you want to change for a more powerful load, or add new loads on the same line, or your
mechanical load has more friction you will need margin on the CB rating.
Generally military aircrafts CB will be loaded around 80% or 90% of RC, civilian aircrafts around 60% of RC.
You must know the inrush current profile of your load (generally the worst case is when temperature is low) and check the
compatibility of the inrush current with the chosen CB’s trip curve (see example next page).
STEP 2
Select a wire gage that will ensure no more than 40 °C temperature rise when it is run through by your nominal current.
For example (EN3841-100):
Current rating A Cross section mm2
AWG* EN code
Up to 1 0,6 20 2083-006
1.5 to 6 1 18 2083-010
7 to 10 1,2 16 2083-012
11 to 15 2 14 2083-020
16 to 20 3 12 2083-030
21 to 25 5 10 2083-050
26 to 40 5 10 2083-050
41 to 50 5 10 2083-050
* AWG = American Wire Gage
STEP 3
You need to know the «final» routing of the wire because if it travels through a non-pressurized zone or is «buried inside
a bundle» it will heat more and will «fume or ignite» quicker than expected. You will perhaps need to decrease AWG value
(i.e. specify a larger cable size) to insure step 2 rule.
STEP 4
The voltage drop from the generator’s point of regulation to the load or equipment must be compatible with the operating
voltage of the load or equipment. In general:
›› In 28 VDC the voltage drop must not be more than 1 V between generator output and load input.
›› In 115 VAC the voltage drop must not be more than 5 V between generator output and load input.
If your wire is very long, you will perhaps need to decrease AWG value (i.e. specify a larger cable size) to insure the above
voltage drop.
STEP 5
Verify that the minimum short-circuit current allows the tripping of the protection device in case of a fault near the load or
equipment.
Table 1
FREQUENTLY ASKED QUESTIONS
|| WWW.CROUZET-AEROSPACE.COM || 49 || ELECTRICAL PROTECTION  DISTRIBUTION
40
Amp
sec
30
20
10
0
1 3 9
EXAMPLE:
I have a 28 VDC motor of 180W. The motor requires 180/28 = 6,4 A nominal current (when torque is high).
Step 1 says that the correct rating for the circuit breaker could be a 7.5 A (around 20% above nominal current).
Step 2 says that a AWG16 wire is suitable for a 6.4 A nominal current (with 6.4 A the temperature rise of the wire will be less
than 40 °C).
Unfortunately, when you connect the motor and power on the motor, the CB trips. This is due to the inrush current of the motor.
If you look at the inrush current of your motor (with an oscilloscope for instance) it looks like the figure on the left:
CONCLUSION:
You must choose a 10A CB to be able to pass the inrush current.
Also: the wire powering the motor is not in a pressurized zone (in a pressurized zone air is a heat sink) or it is imbedded inside
a bundle. In this situation, it will not be cooled down by the surrounding air and will deteriorate with time.
In accordance with Step 3, to reduce wire heating you finally must use a AWG14 wire.
Motor inrush current Circuit Breaker trip envelope
AWG16 wire heated by the adjacent
wires in pressurized zone
You notice that your motor stays above 15 A
(2 times Rated Current) for 3 seconds
➔ this «collides» with the trip envelope of your
Circuit Breaker
Indeed, the above curve shows that at 2 times rated
current (here 15 A for a 7.5 A CB) the CB will trip before
3 seconds.
CONCLUSION: you must use a 10A CB with a AWG14 wire.
8 WHEN DO YOU NEED SIMULATOR CIRCUIT BREAKERS?
Simulator Circuit Breakers can be connected to computer inputs. There are two ways to do this:
1 - Use the auxiliary contacts of a CB (adapted to convey 100 to 200 mA). If your «in the field CB» has a black button, you
will require that your simulator CB (with auxiliary contacts) bares also a black button. For this reason the simulator family
8440227xx is a «black button» version derived from the 844026xx family (which has a green button).
2 - Use the power therminals of a 0.5 A CB (low resistor) and change the button marking to your need: 3A, 5A ➔ 35A etc...
An example of such a solution is the simulator family 84402036 ➔ 84402044 which is internally 0.5 A CB (the 84402011)
but bares a button marking of 3 to 35 A.
AWG16 wire in non
pressurized zone
Non pressurized area
(i.e. bad heat sink)
|| WWW.CROUZET-AEROSPACE.COM || 50 || ELECTRICAL PROTECTION
9 CROSS REFERENCE WITH OLDER CIRCUIT BREAKER MODELS
10 PART NUMBER CONSTRUCTION
For DPMU, DPMT, DGMU, DGMT components, you can construct the article code with the following logic (some exceptions exist):
OLD
Threaded
barrel
Terminals
e=
d= Screw= NEW
Threaded
barrel
Terminals
e=
d= Screw=
PUSH/PULL
84 301 --- Stopped in 1993 No equivalency
84 303 0-- M12x075 12 7.2 M4
84 303 3-- M12x075 12 7.2 M4
84 305 0-- 7/16 12,8 5 8/32 84 400 0-- 7/16 12.5 5 8/32
84 305 3-- 7/16 12,8 5 8/32 84 400 8-- 7/16 12.5 5 8/32
84 305 51- M12x1 18 0 8/32 84 401 0-- M12X1 18 0 8/32
84 305 52- M12x1 18 0 8/32 84 401 8-- M12X1 18 0 8/32
84 305 6-- M12x1 18 0 8/32 84 401 6-- M12X1 18 0 8/32
84 402 0 M12X1 12.5 5 M4/L=8mm
85 402 8 M12X1 12.5 5 M4/L=8mm
86 402 6 M12X1 12.5 5 M4/L=8mm
PUSH/PUSH
84 307 2-- diam=11.6 9.2 5.9 - 84 405 --- diam=11.6 9.2 5.9 -
1995 CROSS REF
e=
screw
84 400 6-8
barrel
d=
e: longitudinal entrax
d: transversal entrax
screw: threading
barrel: threading
Quid ref. creation 8 4 X X X X
rating
digit 1
rating
digit 2
Small model 4
Big model 3
Single pole 0
Three pole 1
Barrel and screw* 1 to 6
Without auxiliary contacts 0
With polarised auxiliary contacts 6
With non polarised auxiliary contacts 8 or 3
Longreck 1
High vibration 2
Rating X X
CIRCUIT BREAKER ARTICLE CODE
* 1: barrel M12-100 terminal screw H8-32. 2: barrel M12-100 terminal screw CB-M4. Others: specific
Example:
Big model
Three pole
25 A
With polarised auxiliary contacts
84 313 625
FREQUENTLY ASKED QUESTIONS
|| WWW.CROUZET-AEROSPACE.COM || 51 || ELECTRICAL PROTECTION  DISTRIBUTION
11 UNDERSTANDING THE MIL SPEC MARKING (PART NUMBER)
Each time CROUZET manufactures a MS3320 circuit breaker, the Circuit Breaker is able to pass
›› High sine vibration levels as described in AS5809 i.e. (using method 204 of MIL STD 202), allowing the stamping of «V»
on the product
›› Random vibration level C as described in AS5809 (using method 214 of MIL STD 202), allowing the stamping of «C» on
the product
Thus every MS33201/AS33201 product that we produce can be stamped as follows:
MS3320-CXV (C = random vibration level, X = current rating, V = condition BC sine vibration)
When V is not present it means that the Circuit Breakers passes level A of sine vibrations
When C is not present it means random vibration level is not a required characteristic
Also when a Circuit Breaker passes level B and C of sine vibration, it is able to pass level A of sine vibration as they
are lower than B and C levels, thus, our ability to produce Circuit Breakers with the MS3320-CXV characteristics
encompasses the following versions:
MS3320-CXV 	 of course, but also
MS3320-CX 	 and,
MS3320-XV 	 and,
MS3320-X
ENGLISH
AC: 	 Alternative Current
AIC: 	 Aircraft Inhabited Cargo
AFCB: 	 Arc Fault Circuit Breaker
ATP: 	 Acceptance Test Procedure
AWG:	 American Wire Gage
CB: 	 Circuit Breaker
CBMU: 	Circuit Breaker Management Unit
CFRP: 	Carbon Fibre Reinforced Polymer (carbon
composite)
CT: 	 Current Transformer
DC: 	 Direct Current
EHA: 	 Electro Hydraulic Actuator
EBHA: 	 Electrical Backup Hydraulic Actuator
EASA: 	 European Aviation Safety Authority
EWIS: 	 Electrical Wiring Interconnect System
FAA: 	 Federal Aviation Authority
FH: 	 Flight Hours
FPGA: 	 Field Programmable Gate Array
GFCB: 	 Ground Fault Circuit Breaker
IFE: 	 In Flight Entertainment
IPX7: 	 Ingress Proctection marking X7
LED: 	 Light Emitting Diode
LMU: 	 Load Management Unit
LRU: 	 Line Replaceable Unit
MTBF: 	 Mean Time Between Failure
OCO/CO:	Open Close Open / Close Open
OEM: 	 Original Equipment Manufacturer
PCB: 	 Printed Circuit Board
PLD: 	 Program Logic Device
QPL: 	 Qualified Part List (Navair)
RMS: 	 Root Mean Square
RC: 	 Rated Current
RCCB: 	 Remote Control Circuit Breaker
REACH: 	Registration, Evaluation and Authorization of
Chemicals
ROHS:	 Restriction of Hazardous Substances
SiC:	 Silicium Carbide
SSCB: 	Single Solidstate Circuit breaker (an electronic
circuit breaker = a single channel SSPC)
SSPC: 	 Solid State Power Controller
UAV: 	 Unmanned Aerial Vehicle
FRENCH
DPMU:	 Disjoncteur Petit Modèle Unipolaire
DGMU:	 Disjoncteur Grand Modèle Unipolaire
DPMT: 	 Disjoncteur Petit Modèle Tripolaire
DGMT:	 Disjoncteur Grand Modèle Tripolaire
ACRONYMS
Pushbutton
if no letter ➔ normal length
if L present ➔ Longneck pushbutton
Sine Vibration level (method 204 of MIL-STD-202)
if no letter ➔ condition A (10 g peak)
if V present ➔ condition B  C (15 g peak)
Amperage Rating
Random Vibration (method 214 of MIL-STD-202) level C thru K
Level C = 9.26 Grms, Level D = 11,95 Grms, Level E = 16,31 Grms
MS3320 - C5VL
Warning:
The product information contained in this catalogue is given purely as information and does not constitute a representation, warrantly or any form of contractual commitment.
Crouzet Automatismes SAS and its subsidiaries reserve the right to modify their products without notice. It is imperative that we should be consulted over any particular use or application
of our products and it is the responsability of the buyer to establish, particularly through all the appropriate tests, that the product is suitable for the use or application. Under no
circumstances will our warranty apply, nor shall we be held responsible for any application (such as any modification, addition, deletion, use in conjunction with other electrical or electronic
components, circuits or assemblies, or any other unsuitable material or substance) which has not been expressly agreed by us prior to the sale of our products.
FRANCE
InnoVista Sensors™
2 rue du Docteur Henri Abel,
CS 60059
26902 Valence Cedex 9
FRANCE
Tel.: +33 (0) 475 802 101
Fax: +33 (0) 475 828 900
relationclient@crouzet.com
GERMANY / AUSTRIA /
SWITZERLAND
InnoVista Sensors™
Otto-Hahn-Str. 3
40721 Hilden
DEUTSCHLAND
Tel.: +49 (0) 2103/980-0
Fax: +49 (0) 2103/980-222
kundenservice@crouzet.com
ITALY
InnoVista Sensors™
Via Viganò De Vizzi, 93/95
20092 Cinisello Balsamo (Mi)
ITALIA
Tel.: +39 (02) 66 599 211
Fax: +39 (02) 66 599 218
assistenzaclienti@crouzet.com
USA
InnoVista Sensors™
1461 Lawrence Drive
Thousand Oaks, CA 91320
USA
Tel.: +1 (800) 677 5311
Fax: +1 (800) 677 3865
info@crouzet.com
AMERICAS EUROPE
COUNTRIES NOT LISTED
InnoVista Sensors™
2 rue du Docteur Henri Abel,
CS 60059
26902 Valence Cedex 9
FRANCE
Tel.: +33 (0) 475 802 102
Fax: +33 (0) 475 828 900
relationclient@crouzet.com
OTHER COUNTRIES
WWW.CROUZET-AEROSPACE.COM WWW.INNOVISTASENSORS.COM
Ref.:6735003AEN|02/2016-Photos:Ginko,DanielLattard,Airbus,Bombardier,Embraer,Eurocopter,Antonov,Gulfstream,©EricRaz/Eurocopter,i-Stock

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Crouzet Aerospace - Electrical Protection & Distribution

  • 1. WWW.CROUZET-AEROSPACE.COM ELECTRICAL PROTECTION & DISTRIBUTION AEROSPACE & DEFENSE TECHNICAL GUIDE ›› Electromechanics ›› Mechatronics ›› Electronics
  • 2. || WWW.CROUZET-AEROSPACE.COM || 2 || ELECTRICAL PROTECTION|| WWW.CROUZET-AEROSPACE.COM || 2 || ELECTRICAL PROTECTION & DISTRIBUTION Crouzet Aerospace has been producing High Performance Aerospace components for over fifty years and has secured a leading role in three Product lines dedicated to aerospace applications: ›› Detection and Sensing: Limit switches, Proximity switches and sensors ›› Electrical Protection and Distribution: Circuit Breakers Circuit Breaker Panels, Solid State Power Controllers ›› Cockpit Equipment: Control Wheels, Helicopter Grips, Pushbuttons. Today Crouzet Aerospace’s components can be found on most major fixed wing programs around the world.To ensure the necessary quality, all Crouzet Aerospace High Performance components are manufactured in Valence, France, and Casablanca, Morocco and are fully certified to EN 9100, ISO 9001, ISO 14001, EASA part 21/G and part 145. With more than 50 years of presence in the aerospace market, Crouzet Aerospace is a specialist providing customized solutions for electromechanical switches, inductive sensors, electrical protection and cockpit equipment backed up by a loyal and experienced team of experts available worldwide. Crouzet Aerospace is a brand of InnoVista Sensors™. ABOUT CROUZET AEROSPACE InnoVista Sensors™: your trusted partner of choice to face industrial challenges of today and tomorrow. InnoVista Sensors™ is a worldwide industrial specialist of sensors, controllers and actuators for automated systems. Through its brands, Crouzet Aerospace, Crouzet Automation, Crouzet Control, Crouzet Motors, Crouzet Switches and Systron Donner Inertial, InnoVista Sensors™ offers a wide range of reliable, efficient and customizable components dedicated to the Aerospace Defence, Transportation and Industrial market and segments. Thanks to the recognized expertise of its teams and a strong innovation policy, InnoVista Sensors™ brings performance enhancing solutions to its customers worldwide. www.innovistasensors.com For Aerospace Defense Transportation Industry With commercial brands Designs Manufactures
  • 3. || WWW.CROUZET-AEROSPACE.COM || 3 || ELECTRICAL PROTECTION DISTRIBUTION CONTENTS Pages Topology 4 Components 5 Arc Fault Protection 8 Ground Fault Circuit Breaker (GFCB) Arc Fault Interrupter 10 From SSCB to SSPC 12 High Shock and Vibration Breakers 13 Circuit Breaker panels 14 The «do it your self» kit 15 Remote Control Contactor Circuit Breaker 16 ELECTRICAL PROTECTION Selection Guide (standard, ratings) 17 Small Model Circuit Breaker Single Pole 18 Small Model Circuit Breaker Three Pole 20 Big Model Circuit Breaker Single Pole 22 Big Model Circuit Breaker Three Pole 24 Frog legs Terminals 26 Frog legs Connection 27 Push-pull Push-fit 6.35 mm Blade 28 Push-push Flying Leads Version 30 GFCB AFCB 32 Dummy Simulator CB 34 Accessories 36 ELECTRICAL DISTRIBUTION Selection guide 37 PCB kit for Faston CB 38 RCCB 115/200 VAC 360-800 Hz 40 SSPC 28 VDC 115 VAC GFI 42 INNOVATION FUTURE PRODUCTS 44 FREQUENTLY ASKED QUESTIONS 45 ACRONYMS 51
  • 4. || WWW.CROUZET-AEROSPACE.COM || 4 || ELECTRICAL PROTECTION DISTRIBUTION An electrical network can be split between primary distribution and secondary distribution. ELECTRICAL NETWORK TOPOLOGY Contactor AFCB CB Fuse SSCB-SSPC RCCB Primary Electric Distribution encompasses the logic of power management (bus shedding in accordance with the Generator Control Unit (GCU), reconfiguration of contactors for ground power unit, or auxiliary power sources, cockpit specific orders…) and Secondary Electric Distribution encompasses the way to bring energy to most of the loads (lights, computers, actuators…) through Circuit Breaker panels or Solid State Protection devices.
  • 5. || WWW.CROUZET-AEROSPACE.COM || 5 || ELECTRICAL PROTECTION DISTRIBUTION ELECTRICAL NETWORK COMPONENTS Thermal trip curve Crouzet Aerospace offers different components for different type of electrical protections: ›› Electromechanical Circuit Breakers (CB) with several different terminals (frog legs, FASTON, EN, MIL…) and accessories ›› Single channel Solid-state Circuit Breakers (SSCB) (i.e. an electronic switch with logical Inputs, thus a one channel SSPC) ›› Remote Control Circuit Breakers (RCCB) for bus shedding or temporary power ON of equipments and loads ›› Power Distribution Boxes (PDB) designed to customer specifications ›› A Circuit Breaker Panel Kit (qualified to severe environment) The goal of electric protection is to protect the cables, the installation and in some cases the load from smoking or igniting or damage due to excessive current or arcing. Thermal Circuit Breakers protect the wire downstream of the Circuit Breaker. They do not protect the load. To do this, a Circuit Breaker must sense the current and break open the line (wire conveying the current) when the current surges ( if the current is above the authorized value for too long). ›› Arc Fault Circuit Breakers protect aluminum structures, composite structures, hydraulic tubes, wires and bundles from the damages of arcing and reduce occurrences of fuel vapor ignition. ›› Ground Fault Interrupters protect humans against electrical shock (with a threshold around 30 mA) and reduce fuel vapor ignition occurrences (with a threshold around 1 A). ›› Solid State Power Controllers protect the wire downstream of the SSPC, they can control the power going to the load and they can protect the load if they are connected to the load’s heat sensors or security output. ›› Remote Control Contactor and Circuit Breakers protect the wire downstream of the RCCB and they can protect the load if they are connected to the load’s heat sensors or security output. Trip range Curve of circuit opening caused by damage Cable smoke curve Current Time Thermal Circuit Breakers have a trip curve which is defined in relation to the cable smoke curves for the entire operating temperature range (-60 °C to +125 °C). Thermal protection based on i2t monitoring is a simple and therefore very reliable concept. It is not sensitive to electromagnetic emission and has the advantage of not tripping on normal transient currents such as current surge caused by motor inertia, a capacitor inrush or a cold incandescent lamp filament etc... For this purpose Circuit Breakers are composed of a latch, a spring, contacts and a current sensor (see next page).
  • 6. || WWW.CROUZET-AEROSPACE.COM || 6 || ELECTRICAL PROTECTION DISTRIBUTION «LIGHT, SIMPLE AND SAFE» Light: Our single phase EN2495 and MIL MS33201 V compliant model is the lightest in the world (20 g with screws, washers and nut). Simple: ›› Designed to be reused several times, spare components are not required ›› Can sometimes be used as a switch (within the defined endurance limits), they therefore perform a dual function of switching and protecting Safe: ›› Our intrinsic fail safe** and trip free* conception enable a high level of safety (generally 10-9  Flight Hours (FH) of not opening on a short circuit) ›› The temperature compensation ensures high performance over a wide temperature range (usually -60°C to +125°C) ›› Excellent resistance to mechanical stress ›› High current level peeks and high current flows tolerance ELECTROMECHANICAL CIRCUIT BREAKERS In this type of Circuit Breaker, the current sensing is done by a bi-metal. The bi-metal is also part of the actuator that will open the line: the bi-metal is bent by heat coming from the current, the bi-metal moves the key lock, releases the latch and opens the line. ELECTRICAL PROTECTION HOW DOES IT WORK? Button Spring Load terminal Power terminal bi-metal Key lock Compensation bi-metal Power terminal Contacts * Trip free: even if the pushbutton is maintained in the closed position, the opening of the contacts (and therefore of the electric circuit) is ensured in the event of a current surge or short-circuit. ** Intrinsic safety (Fail safe): the Circuit Breaker has been designed with a fuse element to ensure that the electric circuit is opened in the extreme case of a blocked mechanism or glued contacts. The Circuit Breaker bi-metal bends and releases the latch according to the overload current value and the overload duration (the bending is independant of the current direction). If any, the auxiliary contact are galvanically isolated from the power and gives the state of the contacts (open or closed). * * * The current direction can be inverted.
  • 7. || WWW.CROUZET-AEROSPACE.COM || 7 || ELECTRICAL PROTECTION DISTRIBUTION SOLID STATE CIRCUIT BREAKERS (SSCB) In this type of Circuit Breaker, the current sensing is done by a shunt or a Hall sensor in DC or a Current Transformer (CT) in AC. A microcontroller or FPGA acquires the current and simulates the i²t curve, the switch function is often done by MOSFETS, bipolar transistors, SCR (i.e. thyristors). Elementary Solid State Circuit Breaker The patented fuse F gives a 10-9 FH safety level (equivalent to mechanical Circuit Breakers) and still gives the possibility of reprogramming the Rated Current value by software. «MORE THAN A THERMAL SWITCH» A SSCB is more than a thermal switch because when it is connected to a data bus, it provides intrinsically functions such as: ›› A remote switching ability (useful in application: contactor or relay function) ›› Dimmer or chopper function (useful in applications such as: motor speed control, light dimming, soft start) ›› Current monitoring (prognostic applications, load failure detection) Also, ›› They are not susceptible to vibrations (useful in applications with high acceleration (Gs): aircraft, guns…) ›› They generate no audio noise (useful in applications such as: submarines, electric tanks, medical…) ›› The micro controller can run the arc fault protection algorithm ›› They can become a PLD with a protected power output (see p. 37) ›› They can protect the load (see p. 37). The microcontroller will integrate the current going through the shunt and will open the MOSFET according to the current value and overload duration.
  • 8. || WWW.CROUZET-AEROSPACE.COM || 8 || ELECTRICAL PROTECTION DISTRIBUTION Wet arc The associated Advisory Circular (AC) gives guidance for subpart H compliancy and indicates that a safety analysis of the Electric Wiring Interconnection Systems (EWIS) has to be done. To certify the EWIS, the constructor must show a proactive approach to mitigate risks and perform a zonal analysis (EZAP). When performing this analysis, it is very important to keep in mind that «regardless of probability, any single arcing failure should be assumed for any power carrying line» (page 31 of the AC) because the traditional way of thinking which was: «optional systems, like in flight entertainment, cannot cause a catastrophic failure condition» is not a valid assumption. Locations where arcing must be mitigated: A In flight entertainment area B Cargo and baggage compartment door actuators C Fuel tanks D SWAMP area (Severe Wind And Moisture Problem area) such as wires in landing gear well or cockpit window heater or wing defrost heaters E Galleys to protect electrical socket appliances such as: Cooktop ovens, waste compacting machines, coffee machines etc… F Places where due to vibration, heat, aging or after an incorrect maintenance operation there is a risk of a power line touching: 1. a critical hydraulic actuator line 2. pressurized air line (air duct) or flight critical data line 3. mechanical control system cable 4. oxygen lines 5. fuel lines 6. water and water/waste line (and below them in case of dripping) 7. hot air ducts In case of an arc inside a bundle, arc fault technology will preclude a chain reaction in the bundle from inducing the loss of the complete bundle. Instead there will be a «controlled» deterioration of the wire(s) giving time for maintenance to be aware of the fault (by using the information coming from the circuit breaker) and thus avoiding a potential catastrophic situation. ELECTRICAL PROTECTION ARC FAULT PROTECTION EWIS PROTECTION The new FAA Part 25 subpart H requirements asks aircraft OEM to consider the electrical wiring interconnection as a system. This means that the airworthiness of the wiring must be guaranteed for the complete lifetime of the aircraft. By incorporating AFCBs in your electrical network, you will be compliant to this new rule.
  • 9. || WWW.CROUZET-AEROSPACE.COM || 9 || ELECTRICAL PROTECTION DISTRIBUTION HOW DOES ARC FAULT PROTECTION WORK? AFCBs combine the safety of standard Circuit Breakers and high accuracy electronics to mitigate arcing. Each standard thermal Circuit Breaker is equipped with an electronic board in order to analyze the current waveform in real time to detect if arcing is occurring. CARBON COMPOSITE (CFRP) PROTECTION Carbon Fibres Reinforced Polymer (CFRP) can be damaged (delamination) and can ignite in case of arcing. The use of arc fault protection will mitigate damage and risk significantly as illustrated below: The algorithm in the electric board works faster than the thermal bi-metal function as shown on the adjacent chart. In case of an electric hazard, the arcing energy (thus mechanical damage) is divided by a magnitude (generally 10) as shown in the adjacent chart. Developped in accordance with DO178B, the AFCB delivers effective arcing mitigation while keeping the robust and proven mechanical EN2995 thermal protection. Current (Amp) Energy(J) 10000 1000 100 10 1 1 5A 10 100 1000 parallel arc area series arc area Upper limit of released arc energy with a thermal CB (400J..70J) Upper limit of released arc energy with an AFCB (6J..30J) Electronic board Thermal breaker Cosmetic damage Delamination Single pole AFCB 230 VAC Fault with arc fault protection: only cosmetic damages appears 230 VAC Fault without arc fault protection: delamination of the fibers
  • 10. || WWW.CROUZET-AEROSPACE.COM || 10 || ELECTRICAL PROTECTION DISTRIBUTION FUEL TANK PROTECTION Following SFAR88 recommendation, the FAA and EASA have compelled PART 25 aircrafts to protect fuel tanks with Ground Fault. The purpose of these Ground Fault products is to mitigate fuel tank ignition by reducing the amount of leakage current to the airframe inside the fuel tank. Documents AC2025_981_1C and EASA CS-25 AMC25.981(a) state that: «any components located in or adjacent to a fuel tank must be qualified to meet standards that assure, during both normal and failure conditions, ignition of flammable fluid vapors will not occur». The above is a concern for: ›› Pylons nacelles and small dimension aircraft where power line are routed near data buses or hydraulic tubes. ›› Wings where torque tube disconnections can cause severe damage to the wiring. ›› Composite wings with high power electric actuators (EHA, EBHA) in the vicinity of fuel tanks. AC2025_981_1C states: Page 17: «A practical means to achieve this is to provide sleeving of the wiring and an independent means such as a GFI or arc fault circuit breaker». Page 20: «(f) Circuit Breakers Service experience has indicated that thermal mechanical circuit breakers installed in the fuel pump circuits have not been shown to preclude arcing […] Arc Fault Circuit Breakers and Ground Fault Interrupters may be needed to provide fail safe features necessary to demonstrate compliance». THE GFCB: A CIRCUIT BREAKER WITH AN ENHANCED GFI Traditional GFI do not capture series arcing or line to line arcing because these two faults do not create a leakage current to the ground (i.e. the CT that measures the homopolar current will still read «zero» with those 2 faults). By adding arc fault detection on each line, Crouzet Aerospace's GFCB is a GFI and a circuit breaker that detects these failure modes. ELECTRICAL PROTECTION GROUND FAULT CIRCUIT BREAKER (GFCB) A triangle load ground fault detector arcfault detector B C line to ground fault ➔ detected line to line fault ➔ detected series arc fault ➔ detected Ground fault arc fault interrupter THE GFCB LAYOUT
  • 11. || WWW.CROUZET-AEROSPACE.COM || 11 || ELECTRICAL PROTECTION DISTRIBUTION ARC FAULT INTERRUPTER HOW DOES THE GFCB WORK? ›› Built in test The GFCB provides built-in test features that allow aircraft maintenance personal to verify that ground fault protection is functional, or that a ground fault has occurred: data issued from the led on the flat of the threaded barrel gives this information. ›› Severed wire detection The GFCB includes «severed wire detection» (ie broken or cut wire) to preclude the heating of a motor if it is stalled (blocked) or running on only 2 phase (typical time detection is 1 second). The above has been implemented because AC2025_981_1C states page 34: ( c) «[…] Automatic protective means, such as arc/ground fault interrupters or other means, should be provided to shut down the pump when a single electrical phase failure occurs. Periodic inspections or maintenance of these features may be required». ON A «STAR» (WYE) LOAD, WITH GROUNDED CENTER, THE BEHAVIOR OF THE GFCB IS THE FOLLOWING ON A «DELTA» (TRIANGLE) LOAD, THE BEHAVIOR OF THE GFCB IS THE FOLLOWING A star load «normal» leakage current ground fault detector B C A delta load ground fault detector B C Electronic board Thermal breaker ›› The Crouzet Aerospace GFCB has 2 thresholds: –– fault time confirmation –– maximum ground fault current. This enables Crouzet Aerospace to deliver products adapted to you load configuration. For instance, GFCB can be targeted either toward Delta (triangle) motor or star (wye) motor configuration. The star configuration is specific because leakage current from the star center to the airframe is possible without being an anomaly (if the center of the star is grounded).
  • 12. || WWW.CROUZET-AEROSPACE.COM || 12 || ELECTRICAL PROTECTION DISTRIBUTION ELECTRICAL DISTRIBUTION FROM SSCB TO SSPC FROM SSCB TO SSPC Using the most recent solid state technology, Crouzet Aerospace has developed 2 generic Solid State Circuit Breakers (SSCB): One for 28 VDC applications, the other for 115 VAC applications. A Solid State Circuit Breaker is composed of a microcontroller, a switch and a data bus. This enables a SSCB to provide more than just thermal protection; its role encompasses electrical functions such as: relay, gradator, chopper, ground fault, soft start, current measurement. These functions can be used for light dimming, motor speed control, intermittent load command (on/off), inrush current limitation, sequential power ON of loads, load failure detection. This is why they become Solid State Power Controllers (SSPC). WHEN DO I NEED A SSPC? Cost efficiency will depend on the ability to encompass several of the previous functions. When thinking of an SSPC solution the following chart must be kept in mind: EASY TO OPERATE Both 115 VAC and 28 VDC SSPC components are delivered with a laptop/tablet interface that enables a quick appropriation of SSPC features. Command from the laptop are transferred through CAN bus. The laptop/tablet interface can be replaced by a MCU or Utilities Management System (UMS) that sends and receives data frames through CAN2.0B. The typical set of orders/queries is: ON/OFF : Powers ON/OFF the load RESET : RESETS the elementary switch after arc or thermal trip STATUS : Asks for trip reason CURRENT : Asks for current (A) value BACKUP : Programs the behavior when data bus is disconnected WHAT I NEED MUST I THINK OF AN SSPC SOLUTION? TRIP INFORMATION ON/OFF I²t High Inrush (8X) SECURE OPEN Arc Fault GFI TRIP ACKNOWLEDGE Laptop-tablet interface
  • 13. || WWW.CROUZET-AEROSPACE.COM || 13 || ELECTRICAL PROTECTION DISTRIBUTION ELECTRICAL PROTECTION HIGH SHOCK AND VIBRATION BREAKERS Typical circuit protection on following military platforms: ›› Fighter Aircraft ›› Military Helicopters ›› Ground Air Defense Systems ›› Military Land Tracked and Wheeled Vehicles ›› Missile Launchers ›› Naval Shipboard Applications MIL-STD-202G Sinusoidal (MIL STD 202 method 204 D) 20 g-PK: condition D under 71 °C and RC Random (MIL STD 202 method 214 A) 23.91 Gms: condition G under 71° C and RC Shock (MIL STD 202 method 213B) 75 g 3 halfsine 6 msec: condition B Our High-Performance Thermal Circuit Breakers exceed the standard for shock and vibration for military applications. It has allways been troublesome for electrical systems engineers to find the best suitable circuit breakers for harsh environments. Crouzet Aerospace has developed a specific series of circuit breakers which go far beyond the current standards. When used in the vicinity of cannons or missile launchers and in circuit breaker panels installed next to machine guns (e.g. helicopters, jet fighters or armored vehicles) the high «shock and vibration» family avoids installing silent blocs on panels or on circuit breakers (while maintaining top circuit protection performance). For the single pole circuit breaker the High Shock and Vibration products multiply by three the endurance level to random and sinus vibrations, compared to AS58091 level or basic MS33201 levels. AS58091 AS33201 basic level Vibration frequency in Hz New level Test condition letter Power spectral density Overall rms G A .02 5.35 B .04 7.56 C .06 9.26 D .1 11.95 E .2 16.91 F .3 20.71 G .4 23.91 H .6 29.28
  • 14. || WWW.CROUZET-AEROSPACE.COM || 14 || ELECTRICAL PROTECTION DISTRIBUTION OUR KNOW HOW As a manufacturer of CB panels we will optimise your needs: ›› Geometry, connection and mounting as specified by your requirements and constraints ›› Customised marking of the front panel ›› Labelling of Circuit Breaker functions by engraving or easily-modified labels ›› Reduced weight due in part to our specially developed light weight Circuit Breaker and busbars ›› Expertise in mechanical and thermal limits (wire gauges, suitable sizes for Circuit Breakers, optimum distribution of Circuit Breaker, …) ›› Expertise in busbars and connections with all the safety requirements (segregation, protection, …) ›› ATP performed by automatic test benches PREDICTABLE PANEL MASS FOR PANELS CONTAINING ONLY CBs SUPPLIER OF CIRCUIT BREAKER PANELS ON SEVERAL JET AND HELICOPTER PROGRAMS Crouzet Aerospace has extensive experience in the design, development and production of illuminated and non-illuminated Circuit Breaker panels in Push/Pull or Push/Push versions, wire or PCB-FASTON version. ELECTRICAL DISTRIBUTION CIRCUIT BREAKER PANELS 56 CB military helicopter panel (wire +casing) 55 CB search and rescue helicopter panel (PCB + casing) 100 CB regional jet panel (wire + casing) 25 CB offshore helicopter panel (wire +casing) X X X grams/protected line Technology Constraints Wire + casing None 56 CB military helicopter panel 100 CB regional jet panel 55 CB search and rescue helicopter panel 16 CB PCB panel kit = World Record ! 43 38 0 33 PCB + casing Rear or side connector PCB + no casing Side connector
  • 15. || WWW.CROUZET-AEROSPACE.COM || 15 || ELECTRICAL PROTECTION DISTRIBUTION PREQUALIFICATION To reduce development time the kit is qualified to harsh environnement. The use of the panel or its sub-sets enables the quick fielding of a qualified solution. If the assembly recommendation and Circuit Breaker locations are respected, Crouzet Aerospace guarantees the electrical and vibrational behavior of the kit: ›› Temperature and electrically from -55°C to 71°C with a 100% utility factor (150 A output) ›› Vibrations: Random and Sinusoidal rays (Harsh Helicopter Level) ›› Crash, fungus, sand and dust. KIT CONSTITUTION The kit is composed of spacers, a PCB board, FASTON Circuit Breakers, and positionning rings. A front panel with removable plate is also available. The removable plate is compatible with accessories (Circuit Breaker gags and obturators). WORLD RECORD The above kit assembly conveys 150 A at 71°C, it weighs 528 g with 16 Circuit Breakers and thus gives a panel efficiency ratio of 528 g=33g/CB ➔ a world record! Ring Distance tube Spacer tube Power feeder EN4165Vertical take off UAV (PCB + no casing) The «Do it your self» kit A STANDARD PCB CARRYING FASTON CBS Crouzet Aerospace is the first company to invent the concept of «do it yourself» Circuit Breaker panels and with this technique, it has created the lightest extractible Circuit Breaker panel in the world! The concept is based on a generic PCB carrying 16 FASTON CBs that you can duplicate (if several bus bars are needed or if more Circuit Breakers are needed). ELECTRICAL DISTRIBUTION THE «DO IT YOUR SELF» KIT
  • 16. || WWW.CROUZET-AEROSPACE.COM || 16 || ELECTRICAL PROTECTION DISTRIBUTION Electric or hydraulic actuator FIN Design Bus bar P/N 12C GALLEY A 84 354 335 1X BULK FAN HEATER A 84 354 335 3 RECIRC FAN B 84 354 350 3JV1 HYD PUMP B 84 354 350 6XN1 L INDB ELEVATOR POWER SPLY C 84 354 350 1XX R INDB ELEVATOR POWER SPLY C 84 354 350 3XX GND SUPPLY A 84 354 350 3XX1HG1 RECIRC FAN A 84 354 350 51N 107XP (IFE) A 84 354 360 1MC L-MID AILERON POWER SPLY A 84 354 350 3J2 L-MID AILERON POWER SPLY A 84 354 350 3J1 HYD PUMP GND SUPPLY A 84 354 360 3C2 HYD PUMP B 84 354 350 1HG Y UPPER RUDDER POWER SUPPLY A 84 354 350 5X G UPPER RUDDER POWER SUPPLY B 84 354 350 23MC L SPOILERS POWER SUPPLY A 84 354 350 3MC R SPOILERS POWER SUPPLY B 84 354 350 24M SLAT E-MOT POWER 1 A 84 354 350 6N2 SLAT E-MOT POWER 2 B 84 354 350 2X 212XP GND SUPPLY C 84 354 350 ELECTRICAL DISTRIBUTION REMOTE CONTROL CONTACTOR CIRCUIT BREAKER The RCCB’s primary use is to power loads that do not need to be permanently ON (to optimize energy). This is why it is used: ›› For powering hydraulic actuators of cargo bay doors ›› For powering Electro Hydraulic Actuators (EHA) and Electro Backup Hydraulic Actuators (EBHA) ›› For powering ON and OFF the galleys or In Flight Entertainment (IFE) The RCCB contacts are CLOSED and OPENED (load is set ON and OFF) only once or twice during the flight; it is designed to commute at least 100,000 times, giving the aircraft a minimum of 50,000 cycles (take off and landing). The RCCB merges a contactor function and a circuit breaker function in a single unit. The contactor is closed when 28 V is applied on the command input. The RCCB has a status display window and a mechanical «TRIP indicator». When the CB has tripped, the mechanical «TRIP indicator» is «popped out» and must be pushed back in manually to RESET the circuit breaker. Our real MTBF figure of 300,000 Flight Hours (field value) during 20 years of service have convinced our customers to mount the RCCB successively on: ›› Galleys feeders ›› Cargo doors actuation motors ›› Flight control power packs (EHA and EBHA) of primary flight control actuators(spoilers; ailerons; rudder) Hereafter is an illustration of the main aircraft locations of the RCCB: Status window or Reset button (trip indicator)
  • 17. || WWW.CROUZET-AEROSPACE.COM || 17 || ELECTRICAL PROTECTION DISTRIBUTION ELECTRICAL PROTECTION SELECTION GUIDE AS5692 EN2495 EN2592 EN2665 EN2794 EN2995 Rate (A) single Code M Code U Code M Code U 003 004 003 004 004 005 DPMU DMPU DPMU DMPT DPMT DGMT DGMT DGMU DGMU DPMU DPMU 1 84 402 001 84 401 001 84 412 001 84 411 001 84 401 801 84 401 601 2 84 402 002 84 401 002 84 412 002 84 411 002 84 401 802 84 401 602 2.5 84 402 012 84 401 012 84 412 012 84 411 012 84 401 812 84 401 612 3 84 401 503 84 402 003 84 401 003 84 412 003 84 411 003 84 401 803 84 401 603 4 84 412 004 5 84 401 505 84 402 005 84 401 005 84 412 005 84 411 005 84 401 805 84 401 605 7.5 84 401 507 84 402 007 84 401 007 84 412 007 84 411 007 84 401 807 84 401 607 10 84 401 510 84 402 010 84 401 010 84 412 010 84 411 010 84 401 810 84 401 610 15 84 401 515 84 402 015 84 401 015 84 412 015 84 411 015 84 313 015 84 306 015 84 401 815 84 401 615 20 84 401 520 84 402 020 84 401 020 84 412 020 84 411 020 84 313 020 84 313 036 84 306 020 84 306 016 84 401 820 84 401 620 25 84 401 525 84 402 025 84 401 025 84 412 025 84 411 025 84 313 025 84 313 037 84 306 025 84 306 017 84 401 825 84 401 625 30 84 306 030 35 84 313 035 84 313 038 84 306 035 84 306 018 41 84 313 041 50 84 313 050 84 313 058 84 306 050 84 306 019 60 Page 32 18 18 20 20 24 24 22 22 18 18 MS26574 FROG EN3773 EN3774 BACC AS5692 Rate (A) «like» 45° 60° 45° 60° 006 006 extended trip extended trip AFCB GF-AFCB DPMU DMPU DPMU DPMT DPMT DPMU DPMT DGMU DGMT DPMT DPMT 1 84 406 001 84 437 001 84 437 201 84 417 001 84 417 201 84 408 001 84 418 001 2 84 406 002 84 437 002 84 437 202 84 417 002 84 417 202 84 408 002 84 418 002 2.5 84 406 012 84 437 012 84 437 212 84 417 012 84 417 212 84 408 012 84 418 012 3 84 406 003 84 437 003 84 437 203 84 417 003 84 417 203 84 408 003 84 418 003 84 411 103 84 411 136 4 84 406 004 5 84 406 005 84 437 005 84 437 205 84 417 005 84 417 205 84 408 005 84 418 005 84 411 105 84 411 137 6 84 406 006 7.5 84 406 007 84 437 007 84 437 207 84 417 007 84 417 207 84 408 007 84 418 007 84 411 107 84 411 138 10 84 406 010 84 437 010 84 437 210 84 417 010 84 417 210 84 408 010 84 418 010 84 411 110 84 411 139 15 84 406 015 84 437 015 84 437 215 84 417 015 84 417 215 84 408 015 84 418 015 84 411 115 84 411 140 20 84 406 020 84 437 020 84 437 220 84 417 020 84 417 220 84 408 020 84 418 020 84 411 120 84 411 141 25 84 406 025 84 437 025 84 437 225 84 417 025 84 417 225 84 408 025 84 418 025 84 306 825 84 313 825 84 411 125 84 411 142 30 84 406 030 84 437 030 84 437 230 84 417 030 84 417 230 84 306 830 84 313 830 35 84 306 835 84 313 835 40 84 306 840 84 313 840 50 84 306 850 84 313 850 60 84 306 860 84 313 860 Page 26 26 26 26 26 28 28 22 24 32 32 EN2996 EN3661 EN3662 EN3773 EN3774 Rate (A) 004 005 004 005 006 004 005 006 004 003 004 DPMT DPMT DGMU DGMU DGMU DGMT DGMT DGMT DPMU DPMT DPMT 1 84 411 801 84 411 601 84 401 050 84 413 001 84 411 001 2 84 411 802 84 411 602 84 401 051 84 413 002 84 411 002 2.5 84 411 812 84 411 612 84 401 052 84 413 012 84 411 012 3 84 411 603 84 401 053 84 413 003 84 411 003 5 84 411 805 84 411 605 84 401 054 84 413 005 84 411 005 7.5 84 411 807 84 411 607 84 401 055 84 413 007 84 411 007 10 84 411 810 84 411 610 84 401 056 84 413 010 84 411 010 15 84 411 815 84 411 615 84 313 315 84 401 057 84 413 015 84 411 015 20 84 411 820 84 411 620 84 306 320 84 306 620 84 306 655 84 313 320 84 313 620 84 313 631 84 401 058 84 413 020 84 411 020 25 84 411 825 84 411 625 84 306 325 84 306 625 84 306 653 84 313 325 84 313 625 84 313 632 84 401 059 84 413 025 84 411 025 35 84 306 335 84 306 635 84 306 654 84 313 335 84 313 635 84 313 633 50 84 306 350 84 306 650 84 306 652 84 313 350 84 313 650 84 313 634 60 Page 20 20 22 22 22 24 24 24 18 20 20 GAM TI-TII-40 / Air 6.625-403 LN29886 / LN29887 MS3320 AS33201 MS3320 AS33201 QPL MS14154 AS14154A MS14154 AS14154A QPL MS26574 VG 95345-TEIL 6 VG 95345-TEIL 11 Rate (A) DPMU DPMU DPMU DMPT DMPT DMPU DPMU DPMU DPMT DPMT 1 84 405 001 LN 29886 see EN2495 M LN29887 see EN2592 M 84 400 001 84 400 048 84 410 001 84 414 001 84 406 001 84 402 001 84 402 801 84 412 001 84 412 801 2 84 405 002 84 400 002 84 400 049 84 410 002 84 414 002 84 406 002 84 402 002 84 402 802 84 412 002 84 412 802 2.5 84 405 012 84 400 012 84 400 050 84 410 012 84 414 012 84 406 012 84 402 012 84 402 812 84 412 012 84 412 812 3 84 405 003 84 400 003 84 400 051 84 410 003 84 414 003 84 406 003 84 402 003 84 402 803 84 412 003 84 412 803 4 84 400 061 84 412 004 84 412 804 5 84 405 005 84 400 005 84 400 052 84 410 005 84 414 005 84 406 005 84 402 005 84 402 805 84 412 005 84 412 805 7.5 84 405 007 84 400 007 84 400 053 84 410 007 84 414 007 84 406 007 84 402 007 84 402 807 84 412 007 84 412 807 10 84 405 010 84 400 010 84 400 054 84 410 010 84 414 010 84 406 010 84 402 010 84 402 810 84 412 010 84 412 810 15 84 405 015 84 400 015 84 400 055 84 410 015 84 414 015 84 406 015 84 402 015 84 402 815 84 412 015 84 412 815 20 84 405 020 84 400 020 84 400 056 84 410 020 84 414 020 84 406 020 84 402 020 84 402 820 84 412 020 84 412 820 25 84 405 025 84 400 025 84 410 025 84 406 025 84 402 025 84 402 825 84 412 025 84 412 825 30 84 400 060 84 402 830 Page 30 18 18 20 20 26 18 18 20 20 CHOICE BY STANDARD/RATING
  • 18. || WWW.CROUZET-AEROSPACE.COM || 18 || ELECTRICAL PROTECTION DISTRIBUTION Rating No signal contact Non polarised / polarised signal contact 1 A 84 400 001 84 400 048/148 84 402 001 84 400 248 84 401 001 84 401 050 84 440 001 84 400 801/601 84 401 801/601 84 402 801/601 2 A 84 400 002 84 400 049/149 84 402 002 84 400 249 84 401 002 84 401 051 84 440 002 84 400 802/602 84 401 802/602 84 402 802/602 2.5 A 84 400 012 84 400 050/150 84 402 012 84 400 250 84 401 012 84 401 052 84 440 012 84 400 812/612 84 401 812/612 84 402 812/612 3 A 84 400 003 84 400 051/151 84 402 003 84 400 251 84 401 003 84 401 053 84 440 003 84 400 803/603 84 401 803/603 84 402 803/603 4 A 84 400 061/161 84 400 261 5 A 84 400 005 84 400 052/152 84 402 005 84 400 252 84 401 005 84 401 054 84 440 005 84 400 805/605 84 401 805/605 84 402 805/605 6 A 84 402 006 84 402 806/606 7.5 A 84 400 007 84 400 053/153 84 402 007 84 400 253 84 401 007 84 401 055 84 440 007 84 400 807/607 84 401 807/607 84 402 807/607 10 A 84 400 010 84 400 054/154 84 402 010 84 400 254 84 401 010 84 401 056 84 440 010 84 400 810/610 84 401 810/610 84 402 810/610 15 A 84 400 015 84 400 055/155 84 402 015 84 400 255 84 401 015 84 401 057 84 440 015 84 400 815/615 84 401 815/615 84 402 815/615 20 A 84 400 020 84 400 056/156 84 402 020 84 400 256 84 401 020 84 401 058 84 440 020 84 400 820/620 84 401 820/620 84 402 820/620 25 A 84 400 025 84 402 025 84 400 225 84 401 025 84 401 059 84 440 025 84 400 825/625 84 401 825/625 84 402 825/625 30 A 84 400 060 84 402 030 84 400 230 84 440 030 84 400 860/660 84 401 830/630 84 402 830/630 Ratings 0.5; 0.75; 1.5 A are available. REFERENCES Mounting hardware HV Threaded barrel M12-0.75 M12-100 • • • • • 7/16 • • • • • Terminal Screw 8-32 UNC • • • • • • • • M4 • • Terminal Offset Offset Offset Offset Aligned Aligned Aligned Offset Aligned Offset Conformity standard HV EN 2495 M U EN 2995 004 EN 3773 004 AS33201 - MS3320 • QPL QPL VG 95345 TEIL 6 • • BACC 18Z18AD like • Mass / MTBF / Vibration / Technical file HV Weight without mounting hardware 18 18 18 18 18 18 20 20 Weight with mounting hardware 21 20 20 20 20 20 22 22 MTBF FH (Typical) 7.2 M 7.2 M 7.2 M 7.2 M 7.2 M 7.2 M 7.2 M 3.6 M MIL vibration Sinus/Random A C A C A C G H A C A C A C A C Technical File SP4374 SP9930 SP4356 Button HV Green color • • • Black color • • • • • • • Long neck option • Electrical 28 VDC 115 VAC (400 Hz) 115 VAC 60 Hz-230 VAC 50 Hz Breaking current 1co + 2OCO 6000 A 2500 A CONTACT CROUZET AEROSPACE Dielectric 1500 V 1500 V Endurance cycles 5000 (with L/R: 5 ms) 5000 (with cos fi: 0.7) Insulation resistance above 100 MΩ above 100 MΩ Working life (endurance) at 5x RC 50 cycles 50 cycles Auxiliary contact current 0.1..0.2 A 0.1..0.2 A Voltage drop compliance EN2495/2995/MS3320/AS33201 EN2495/2995/MS3320/AS33201 GENERAL CHARACTERISTICS DPMU SMALL MODEL CIRCUIT BREAKER SINGLE POLE Environmental Salt spray 48h 5% NaCl Humidity: Test b RTCA DO160 10 cycles Operating temperature -60°C +125°C for all ratings except 30 A: - 60°C + 90°C Acceleration (centrifugal) up to 40 g Vibrations EN QPL (MS AS33201) High Vibration (HV) Sinusoidal (MIL STD202 method 204D) 10 g-PK: condition A 15 g-PK: condition C 20 g-PK: condition D Random (MIL STD202 method 214A) 9.26 Grms: condition C under 71°C and RC 16.91 Grms: condition E under 71°C and RC 23.91 Grms: condition G under 71°C and RC Shock 50 g 3 halfsine 11 msec 75 g 3 halfsine 6 msec above 75 g 3 halfsine 6 msec Mechanical Operating force 3,5N push45N / 5Npull30N Endurance without load: 5000 cycles resistive load: 2500 cycles Tightening torque barrel nut: recommended: 4 ± 0.25 N.m maximum : 5.0 N.m terminal screw: recommended: 1.6 ± 0.1 N.m maximum : 2.0 N.m
  • 19. || WWW.CROUZET-AEROSPACE.COM || 19 || ELECTRICAL PROTECTION DISTRIBUTION DIMENSIONS CURVES PANEL CUTOUT RECOMMENDATION 84 400 0 84 402 0 84 401 084 400 6-8 84 402 6-8 84 401 6-8 › Thickness: 1.6 mm ➞ 3 mm 20 10 5 4 3 2 In 10 2 -2 3 45 10-1 2 3 45 1 2 3 45 2 3 45 2 3 4510 100 1000 +125C +25C -55C 84 400 0 - 6 - 8 84 400 0 - 6 - 8 84 400 0 - 6 - 8 84 405 0 -60 -20 -40 0 20 40 60 80 100 120 0,8 In 1,2 1,4 1,6 1,8 2 84 400 0 - 6 - 8 84 400 0 - 6 - 8 84 400 0 - 6 - 8 84 405 0 Non-trip threshold Trip threshold Current (as percentage of In) Ambiant temperature °C 31 2,5max 1,5 19max 28max. 12,5 38max 4,6 m in 84 400 0 24 max 19,5 max 2 9,5 14,3max 84 401 0 18 31 max 84 401 0 18 31 max 31 2,5max 1,5 19max 28max 12,5 38max 4,6 m in 19,5max 16,3 max 26 max 2 9,5 14,3max 84 400 6-8 ø10 12,8 6,35 3max 5 10 84 401 6-8 18 12 10 31,5 max 84 401 6-8 18 12 10 31,5 max Versions 84 400 0 30min. 9,5 Ø11,5 20 min. Ø3,5 Versions 84 402 0 30min. 9,5 Ø12,5 20 min. Ø3 Versions 84 401 0 - 6 - 8 Versions 84 400 1xx 35min. 22.5±0.5 (.886±.019) 28.6max. Trip times envelope for temperature from -55°C to 125°C (direct overload) Rating 1.5 ➞ 5 A 7.5 ➞ 25 A Non tripping point at 25°C 1.15 * RC 1.15 * RC Tripping point at 25°C 1.4 * RC 1.4 * RC Tripping time at 2 * RC 2 s ➞ 15 s 4 s ➞ 20 s Non tripping point at 125°C 1 * RC 1 * RC Maximum and minimum limit of ultimate trip
  • 20. || WWW.CROUZET-AEROSPACE.COM || 20 || ELECTRICAL PROTECTION DISTRIBUTION Rating No signal contact Non polarised/polarised signal contact 1 A 84 410 001 84 411 001 84 412 001 84 413 001 84 414 001 84 450 001 84 410 801/601 84 411 801/601 84 412 801/601 2 A 84 410 002 84 411 002 84 412 002 84 413 002 84 414 002 84 450 002 84 410 802/602 84 411 802/602 84 412 802/602 2.5 A 84 410 012 84 411 012 84 412 012 84 413 012 84 414 012 84 450 012 84 410 812/612 84 411 812/612 84 412 812/612 3 A 84 410 003 84 411 003 84 412 003 84 413 003 84 414 003 84 450 003 84 410 803/603 84 411 803/603 84 412 803/603 4 A 84 412 004 84 412 804/604 5 A 84 410 005 84 411 005 84 412 005 84 413 005 84 414 005 84 450 005 84 410 805/605 84 411 805/605 84 412 805/605 6 A 84 412 006 84 412 806/606 7.5 A 84 410 007 84 411 007 84 412 007 84 413 007 84 414 007 84 450 007 84 410 807/607 84 411 807/607 84 412 807/607 10 A 84 410 010 84 411 010 84 412 010 84 413 010 84 414 010 84 450 010 84 410 810/610 84 411 810/610 84 412 810/610 15 A 84 410 015 84 411 015 84 412 015 84 413 015 84 414 015 84 450 015 84 410 815/615 84 411 815/615 84 412 815/615 20 A 84 410 020 84 411 020 84 412 020 84 413 020 84 414 020 84 450 020 84 410 820/620 84 411 820/620 84 412 820/620 25 A 84 410 025 84 411 025 84 412 025 84 413 025 84 414 025 84 450 025 84 410 825/625 84 411 825/625 84 412 825/625 30 A 84 412 030 84 413 030 84 450 030 Button Green color • • • Black color • • • • • Long neck Mounting hardware Threaded barrel M12-0.75 • M12-100 • • • • 7/16 • • • • Terminal Screw 8-32 UNC • • • • • • M4 • • • Terminal Offset Offset Offset Offset Offset Aligned Offset Offset Offset REFERENCES Mass / MTBF / Vibration / Technical file Without mounting hardware 46 51 With mounting hardware 55 60 MTBF FH (Typical) 1,2 M 700 000 MIL vibration condition Sinus/Random A C A C Technical File - - - - - - Conformity standard EN 2592 U M EN 3774 004 003 EN 2996 004/005 VG 95345 TEIL 11 • • AS 14154B/MS14154 • QPL BACC 18AC18AE like • Electrical 115/200 VAC (400 Hz) 115/200 VAC 60 Hz-230/400 VAC 50 Hz Breaking current 1CO + 2OCO 2000 A CONTACT CROUZET AEROSPACE Dielectric 1500 V Endurance (electrical overloads) 5000 (with cos fi: 0.7) Insulation resistance above 100 MΩ Working life (endurance) at 5xRC 50 cycles Auxiliary contact current 0.1..0.2 A Voltage drop compliance MS14154/AS14154A/EN2592/2996/3774 Environmental Salt spray 48h : 5% NaCl Humidity: Test b RTCA DO160 : 10 cycles Operating temperature (1 to 15 A) -60°C +125°C Operating temperature (20 and 25 A) -60°C.+90°C Acceleration (centrifugal) 17g Shock 50 g 3 halfsine 11 msec 6 directions Vibration (sinusoidal) 10 g-PK from 70 to 20000 Hz (MIL STD202 method 204 D condition A with 90 % of RC) Vibration (random at RC) 9.26 Grms (MIL STD202 method 214 A condition C with 90 % of RC) Mechanical Operating force 8Npush80N / 5Npull30N Endurance (manual open/close) no load / 5000 cycles on resistive load / 5000 cycles Tightening torque barrel nut: recommended: 4 ± 0.25 N.m maximum : 5.0 N.m terminal screw: recommended: 1.6 ± 0.1 N.m maximum : 2.0 N.m GENERAL CHARACTERISTICS DPMT SMALL MODEL CIRCUIT BREAKER THREE POLE
  • 21. || WWW.CROUZET-AEROSPACE.COM || 21 || ELECTRICAL PROTECTION DISTRIBUTION DIMENSIONS CURVES Trip times envelope for temperature from -55°C to 125°C (direct overload) Rating 1.5 ➞ 5 A 7.5 ➞ 25 A Non tripping point at 25°C 1.15 * RC 1.15 * RC Tripping point at 25°C 1.4 * RC 1.4 * RC Tripping time at 2 * RC 2 s ➞ 15 s 4 s ➞ 20 s Non tripping point at 125°C 1 * RC 1 * RC Maximum and minimum limit of ultimate trip 20 10 5 4 3 2 In 10 2 -2 3 45 10-1 2 3 45 1 2 3 45 2 3 45 2 3 4 1.10 1.40 1.60 510 100 1000 +23C -55C +125C 84 310 0 - 3 - 6 84 314 2 -60 -20 -40 0 20 40 60 80 100 120 0,8 In 1,2 1,4 1,6 1,8 Non-trip threshold Trip threshold Current (as percentage of In) Ambiant temperature °C 2 84 310 0 - 3 - 6 84 314 2 PANEL CUTOUT RECOMMENDATION › Thickness: 1.6 mm ➞ 3 mm 84 411 0 84 412 0 84 413 0 30min. 9,5 Ø12,5 50 min. Ø3 84 414 0 30min. 9,5 Ø11,5 50 min. Ø3 84 411 6 84 411 8 84 412 8 84 413 6 35min. 9,5 Ø12,5 50 min. Ø3 84 411 0 84 412 0 84 413 0 84 414 0 84 411 6 84 411 8 84 412 8 84 413 6
  • 22. || WWW.CROUZET-AEROSPACE.COM || 22 || ELECTRICAL PROTECTION DISTRIBUTION Rating No signal contact No signal contact long trip time Non polarised/polarised signal contact Polarised signal contact 15 A 84 306 015 20 A 84 306 020 84 306 016 84 306 320/620 84 306 316/616 84 306 645/655 25 A 84 306 025 84 306 017 84 306 325/625 84 306 317/617 84 306 643/653 30 A 84 306 030 84 306 330/630 35 A 84 306 035 84 306 018 84 306 835 84 306 335/635 84 306 318/618 84 306 644/654 40 A 84 306 080 84 306 340/640 50 A 84 306 050 84 306 019 84 306 850 84 306 350/650 84 306 319/619 84 306 642/652 60 A 84 306 860 REFERENCES Button Green color • • • • Black color • • Conformity standard EN 2794 003 004 EN 3661 004 005 005 006 BACC 18R18X like • Mass / MTBF / Vibration / Technical file Without mounting hardware 61 61 66 With mounting hardware 65 65 70 MTBF FH (Typical) 10 M 10 M 6 M MIL vibration condition Sinus/Random A C A C A C Technical File - SP4393 - - SP4339 SP9300 Environmental Salt spray 48h / 5% NaCl Humidity: Test b RTCA DO160 / 10 cycles Operating temperature -60°C +125°C Acceleration (centrifugal) up to 17g Shock 50 g 3 halfsine 11 msec 6 directions Vibration (sinusoidal) 10 g-PK from 70 to 20000 Hz (MIL STD202 method 204 D condition A with 90 % of RC) Vibration (random at RC) 9.26 Grms (MIL STD202 method 214 A condition C with 90 % of RC) Mechanical Operating force 3,5Npush55N / 5Npull40N Endurance (manual open/close) no load : 5 000 cycles on resistive load : 2 500 cycles Tightening torque barrel nut: recommended: 4 ± 0.25 N.m maximum : 5.5 N.m terminal screw: recommended: 2.35 ± 0.15 N.m maximum : 2.5 N.m Electrical 28 VDC 115 VAC (400 Hz) 115 VAC 60 Hz-230 VAC 50Hz Breaking current 1co + 2OCO 4000 A ; 2000 A long trip 2000 A ; 1500 A long trip CONTACT CROUZET AEROSPACE Dielectric 1500 V 1500 V Endurance (electric overloads) 5000 (with L/R: 5 ms) 5000 (with cos fi: 0.7) Insulation resistance above 100 MΩ above 100 MΩ Working life (endurance) at 5xRC 50 cycles 50 cycles Voltage drop compliance EN2794/3661 EN2794/3661 GENERAL CHARACTERISTICS DGMU BIG MODEL CIRCUIT BREAKER SINGLE POLE Mounting hardware Threaded barrel M12-0.75 • • • • • • M12-100 7/16 Terminal Screw 8-32 UNC • • • • M4 • • Hole ø5.5 for Bus-Bar •
  • 23. || WWW.CROUZET-AEROSPACE.COM || 23 || ELECTRICAL PROTECTION DISTRIBUTION DIMENSIONS CURVES Standard trip time (EN compliant) Long trip time (BACC compliant) 20 10 5 4 3 2 In 10 2 -2 3 45 10-1 2 3 45 1 2 3 45 2 3 45 2 3 4510 100 1000 -55C 84 306 0 - 6 - 8 +125C +23C 0,90 1.10 1.45 1.65 20 10 5 4 3 2 In 10 2-2 3 45 10-1 2 3 45 1 2 3 45 2 3 45 2 3 4510 100 1000 -55C 84 306 835 +125C +25C 55max 4823 22 34 max. 21 M12 x 0,75 9,5 3 m ax. 7 m in. Ø2 19,5max. 1 2 84 306 0 3min. 6,6 1-3max. 18 10 min. Ø10,4 84 306 0 84 406 8 55max 26,5 1-3max. 18 4823 22 28max. 34 max. 10 min. 10 min. Ø10,4 21 25 max. M12 x 0,75 42 max. 9,5 3 m ax. 7 m in. Ø2 19,5max. 4 1 2 3 84 306 3 3min. 6,6 84 306 3 55max 26,5 1-3max. 18 4823 22 28max. 34 max. 10 min. 10 min. Ø10,4 21 25 max. M12 x 0,75 42 max. 9,5 3 m ax. 7 m in. Ø2 19,5max. 1 2 84 306 6 3min. 6,6 5 3 84 306 6 84 306 6 Bus-Bar EN 3661-006 PANEL CUTOUT RECOMMENDATION › Thickness 1.6 mm ➞ 3 mm Versions 84 306 0 - 3 - 6 45min. 9,5 Ø12,5 25 min. Ø3 84 306 6 Bus-Bar EN 3661-006
  • 24. || WWW.CROUZET-AEROSPACE.COM || 24 || ELECTRICAL PROTECTION DISTRIBUTION Conformity standard EN 2665 003 004 EN 3662 004 005 005 006 10-60806 like • Weight (g) Without mounting hardware 156 156 161 With mounting hardware 165 165 170 MTBF FH (Typical) 5 M 5 M 26 M MIL vibration condition Sinus/Random A C A C A C Technical File - SP4393 ASNE459 - - SP4340 SP4346 Button Green color • • • • Black color • • • Rating No signal contact No signal contact long trip time Non polarised/polarised signal contact Polarised signal contact 15 A 84 313 015 20 A 84 313 020 84 313 036 84 313 061 84 313 820 84 313 320/620 84 313 316/613 84 313 621/631 25 A 84 313 025 84 313 037 84 313 062 84 313 825 84 313 325/625 84 313 317/617 84 313 622/632 30 A 84 313 330/630 35 A 84 313 035 84 313 038 84 313 063 84 313 840 84 313 335/635 84 313 318/618 84 313 623/633 41 A 84 313 041 50 A 84 313 050 84 313 058 84 313 066 84 313 850 84 313 350/650 84 313 319/619 84 313 624/634 60 A 84 313 860 REFERENCES Electrical 115/200 VAC (400 Hz) 115/200 VAC 60 Hz-230/400 VAC 50 Hz Breaking current 1CO + 2OCO 2000 A ; 1500 A long trip CONTACT CROUZET AEROSPACE Dielectric 1500 V Endurance (electric overloads) 5000 (with cos fi: 0.7) Insulation resistance above 100 MΩ Working life (endurance) at 5xRC 50 cycles Auxiliary contact current 0.1..0.2 A Voltage drop compliance EN2665/3662 Environmental Salt spray 48h / 5% NaCl Humidity: Test b RTCA DO160 / 10 cycles Operating temperature -55°C +90°C Acceleration up to 40 g Shock 50 g 3 halfsine 11 msec 6 directions Vibration (sinusoidal) 10 g-PK from 70 to 20000 Hz (MIL STD202 method 204 D condition A with 90 % of RC) Vibration (random at RC) 9.26 Grms (MIL STD202 method 214 A condition C with 90 % of RC) Mechanical Operating force 20Npush80N / 5Npull45N Endurance (manual open/close) no load : 5000 cycles on resistive load : 2500 cycles Tightening torque barrel nut: recommended: 4 ± 0.25 N.m maximum: 5.5 N.m terminal screw: recommended: 2.35 ± 0.15 N.m maximum : 2.5 N.m GENERAL CHARACTERISTICS DGMT BIG MODEL CIRCUIT BREAKER THREE POLE Mounting hardware Threaded barrel M12-0.75 • • • • • • • M12-100 7/16 Terminal Screw 8-32 UNC • • • • • • M4 • Hole ø5.5 for Bus-Bar • •
  • 25. || WWW.CROUZET-AEROSPACE.COM || 25 || ELECTRICAL PROTECTION DISTRIBUTION DIMENSIONS CURVES Standard trip time (EN compliant) Long trip time (BACC compliant) 20 10 5 4 3 2 In 10 2 -2 3 45 10-1 2 3 45 1 2 3 45 2 3 45 2 3 4510 100 1000 -55C 84 313 0 - 6 - 8 +90C 1.10 1.40 1.60 +23C 20 10 5 4 3 2 In 10 2 -2 3 45 10-1 2 3 45 1 2 3 45 2 3 45 2 3 4510 100 1000 -55C 84 306 835 +90C +25C 84 313 0 1 2 55max 4823 22 21 M12 x 0,75 3 m ax. 7 m in. 3min. 6,6 C1 C2 B2 A2 C1 A1 B1 A1 34max. 1-3max. 18 Ø10,4 10 min. 17,5 17,5 54 max. B1 9,5 2 84 313 0 84 313 3 1 2 55max 4823 22 28max. 21 25 max. M12 x 0,75 3 m ax. 7 m in. 3min. 6,6 C1 C2 B2 A2 C1 A1 B1 A1 26,5 34max. 42max. 1-3max. 18 10 min. Ø10,4 10 min. 17,5 17,5 54 max. B1 9,5 2 19,5 max. 4 3 84 313 3 - 84 313 6 PANEL CUTOUT RECOMMENDATION › Thickness 1.6 mm ➞ 3 mm Versions 84 313 0 - 3 - 6 45min. 9,5 Ø12,5 60 min. Ø3 Versions Bus-Bar EN 3662-006 45min. 9,5 9,5 9,5 Ø12,5 60 min. Ø3 84 313 6 1 2 55max 4823 22 28max. 21 25 max. M12 x 0,75 3 m ax. 7 m in. 3min. 6,6 5 3 C1 C2 B2 A2 C1 A1 B1 A1 26,5 34max. 42max. 1-3max. 18 10 min. Ø10,4 10 min. 17,5 17,5 54 max. B1 9,5 2 19,5 max. 84 313 6 Bus-Bar EN 3662-006
  • 26. || WWW.CROUZET-AEROSPACE.COM || 26 || ELECTRICAL PROTECTION DISTRIBUTION Button color Green Black • • • • • Rating 1 pole 45° 1 pole 45° 1 pole 60° 3 pole 45° 3 pole 60° 0.5 A 84 406 011 1 A 84 406 001 84 437 001 84 437 201 84 417 001 84 417 201 2 A 84 406 002 84 437 002 84 437 202 84 417 002 84 417 202 2.5 A 84 406 012 84 437 012 84 437 212 84 417 012 84 417 212 3 A 84 406 003 84 437 003 84 437 203 84 417 003 84 417 203 4 A* 5 A 84 406 005 84 437 005 84 437 205 84 417 005 84 417 205 6 A* 7.5 A 84 406 007 84 437 007 84 437 207 84 417 007 84 417 207 10 A 84 406 010 84 437 010 84 437 210 84 417 010 84 417 210 15 A 84 406 015 84 437 015 84 437 215 84 417 015 84 417 215 20 A 84 406 020 84 437 020 84 437 220 84 417 020 84 417 220 25 A 84 406 025 84 437 025 84 437 225 84 417 025 84 417 225 30 A 84 437 030 84 437 230 84 417 030 84 417 230 Mounting hardware Threaded barrel M12-0.75 M12-100 • • • • 7/16 • Terminal Screw 6-32 UNC • M4 • • • • REFERENCES Conformity standard EN 2495* • • • EN 2995* • • • EN 2592* • • EN 2996* • • EN 3774* • • MS26574 ** • * for performance ** for terminal configuration Mass/MTBF/technical file Weight without mounting hardware (g) 18 18 19 54 56 Weight with mounting hardware (g) 20 20 21 63 65 MTBF FH (Typical) 7.2 M 7.2 M 7.2 M 1.7 M 1.7 M Technical file SP 990100 SP 991700 SP 992000 SP 991900 SP 992100 Environmental Salt spray 48h 5% NaCl Humidity: Test b RTCA DO160 10 cycles Operating temperature -60°C +125°C for all ratings except 30 A: - 60°C + 90°C Acceleration (centrifugal) up to 40 g Shock 50 g 3 halfsine 11 msec Vibration (sinusoidal) single pole 15 g-PK from 70 to 2000 Hz (MIL STD 202 method 214G condition B with 90% of RC) at 23°C Vibration (random) single pole 16.91 Grms (MIL STD 202 method 204D condition E with 90% of RC) at 23°C Mechanical Operating force 3,5N push45N / 5Npull30N 8Npush80N / 5Npull80N Endurance mechanical (no load) 5 000 cycles mechanical (no load) 5000 cycles on resistive load 2 500 cycles on resistive load 2500 cycles Tightening torque (barrel nut) recommended: 4 ± 0.25 N.m maximum : 5.0 N.m recommended: 4±0.25 N.m maximum: 5.0 N.m Tightening torque (terminal screw) recommended: 1.6 ± 0.1 N.m maximum : 2.0 N.m recommended: 1.6±0.1 N.m maximum: 2.0 N.m Electrical Single Pole Three pole 28 VDC 115 VAC (400 Hz) 115/200 VAC (400 Hz) Breaking current 1CO + 2OCO 6000 A 2500 A 2000 A Dielectric 1500 V 1500 V 1500 V Endurance cycles 5000 (with L/R: 5 ms) 5000 (with cos fi: 0.7) 5000 (with cos fi: 0.7) Insulation resistance above 100 MΩ above 100 MΩ above 100 MΩ Working life (endurance) at 5xRC 50 cycles 50 cycles 50 cycles Auxiliary contact current (if present) 0.1..0.2 A 0.1..0.2 A 0.1..0.2 A Voltage drop compliance EN2495/2995/MS3320/AS33201 EN2495/2995/MS3320/AS33201 MS14154/AS14154A/EN2592/2996/3774 GENERAL CHARACTERISTICS SMALL MODEL CIRCUIT BREAKER FROG LEGS TERMINALS * contact Crouzet Aerospace for this rating
  • 27. || WWW.CROUZET-AEROSPACE.COM || 27 || ELECTRICAL PROTECTION DISTRIBUTION FROG LEGS CONNECTION three pole 20 10 5 4 3 2 In 10 2 -2 3 45 10-1 2 3 45 1 2 3 45 2 3 45 2 3 4 1.10 1.40 1.60 510 100 1000 +23C -55C +125C 84 310 0 - 3 - 6 84 314 2 DIMENSIONS PANEL CUTOUT RECOMMENDATION CURVES Trip times envelope for temperature from -55°C to 125°C (direct overload) Rating 1.5 ➞ 5 A 7.5 ➞ 25 A Non tripping point at 25°C 1.15 * RC 1.15 * RC Tripping point at 25°C 1.4 * RC 1.4 * RC Tripping time at 2 * RC 2 s ➞ 15 s 4 s ➞ 20 s Non tripping point at 125°C 1 * RC 1 * RC Maximum and minimum limit of ultimate trip 20 10 5 4 3 2 In 10 2 -2 3 45 10-1 2 3 45 1 2 3 45 2 3 45 2 3 4510 100 1000 +125C +25C -55C 84 400 0 - 6 - 8 84 400 0 - 6 - 8 84 400 0 - 6 - 8 84 405 0 single pole 84 406 0 - 84 437 0 - 84 437 1 84 437 2 84 417 2 84 417 0 - 84 417 1 › Thickness 1.6 mm ➞ 3 mm Versions 84 406 0 30min. 9,5 Ø11,5 20 min. Ø3,5 Versions 84 437 0 84 437 1 - 84 437 2 30min. 9,5 Ø12,5 20 min. Ø3 Versions 84 417 0 - 84 417 1 84 417 20 30min. 9,5 Ø12,5 50 min. Ø3
  • 28. || WWW.CROUZET-AEROSPACE.COM || 28 || ELECTRICAL PROTECTION DISTRIBUTION Button Green color • Black color • • • Long neck (long button) • • Rating no auxiliary contacts no auxiliary contacts no polarised/polarised         no auxiliary contacts 0.5 A 84 408 111 84 418 011 1 A 84 408 001 84 408 101 84 408 601/801 84 418 001 2 A 84 408 002 84 408 102 84 408 602/802 84 418 002 2.5 A 84 408 012 84 408 112 84 408 612/812 84 418 012 3 A 84 408 003 84 408 103 84 408 603/803 84 418 003 4 A 84 408 004 84 408 104 84 408 604/804 84 418 004 5 A 84 408 005 84 408 105 84 408 605/805 84 418 005 6 A 84 408 006 84 408 106 84 408 606/806 84 418 006 7.5 A 84 408 007 84 408 107 84 408 607/807 84 418 007 10 A 84 408 010 84 408 110 84 408 610/810 84 418 010 15 A 84 408 015 84 408 115 84 408 615/815 84 418 015 20 A 84 408 020 84 408 120 84 408 620/820 84 418 020 25 A 84 408 025 84 408 125 84 408 625/825 available in 2016 84 418 025 Mounting hardware Straight terminals without screws • • • • Barrel threadings Conical barrel • • • • SMALL MODEL CIRCUIT BREAKER FASTON CONNECTION PUSH-PULL PUSH-FIT 6.35 MM BLADE REFERENCES Conformity standard EN 2495* • • EN 2995* 004 005 EN3773-006 • • EN3774-006 • AS 33201 • • • * for thermal performance and auxiliary contact performance Mass/MTBF / Technical file No mounting hardware 14,5 15,5 16,5 51 MTBF FH (Typical) 7.2 M 7.2 M 3.6 M 1.7 M Technical file SP 991600 SP 991800 SP 991800 SP 991500 Environmental Salt spray 48h 5% NaCl Humidity: Test b RTCA DO160 10 cycles Operating temperature -60°C +125°C for all ratings except 30 A: - 60°C + 90°C Acceleration (centrifugal) up to 40 g Shock 50 g 3 halfsine 11 msec Vibration (sinusoidal) single pole 10 g-PK from 70 to 2000 Hz (MIL STD 202 method 204 D condition B with 90% of RC) Vibration (random) single pole 9.26 Grms (MIL STD 202 method 214 A condition E with 90% of RC) Mechanical Operating force 3,5N push45N / 5Npull30N 8Npush80N / 5Npull80N Endurance mechanical (no load) 5 000 cycles mechanical (no load) 5000 cycles on resistive load 2 500 cycles on resistive load 2500 cycles Tightening torque (barrel nut) recommended: 4 ± 0.25 N.m maximum : 5.0 N.m recommended: 4 ± 0.25 N.m maximum : 5.0 N.m Tightening torque (terminal screw) recommended: 1.6 ± 0.1 N.m maximum : 2.0 N.m recommended: 1.6 ± 0.1 N.m maximum : 2.0 N.m Electrical Single pole Three pole 28 VDC 115 VAC (400 Hz) 115/200 VAC (400 Hz) Breaking current 1CO + 2OCO 6000 A 2500 A 2000 A Dielectric 1500 V 1500 V 1500 V Endurance cycles 5000 (with L/R: 5 ms) 5000 (with cos fi: 0.7) 5000 (with cos fi: 0.7) Insulation resistance above 100 MΩ above 100 MΩ above 100 MΩ Working life (endurance) at 5xRC 50 cycles 50 cycles 50 cycles Auxiliary contact current (if present) 0.1..0.2 A 0.1..0.2 A 0.1..0.2 A Voltage drop compliance EN2495/2995/MS3320/AS33201 EN2495/2995/MS3320/AS33201 MS14154/AS14154A/EN2592/2996/3774 GENERAL CHARACTERISTICS
  • 29. || WWW.CROUZET-AEROSPACE.COM || 29 || ELECTRICAL PROTECTION DISTRIBUTION PUSH-FIT 0.25 INCH TAB DIMENSIONS › Thickness: 1.6 mm for ring gasket PANEL CUTOUT RECOMMENDATION CURVES Trip times envelope for temperature from -55°C to 125°C (direct overload) Rating 1.5 ➞ 5 A 7.5 ➞ 25 A Non tripping point at 25°C 1.15 * RC 1.15 * RC Tripping point at 25°C 1.4 * RC 1.4 * RC Tripping time at 2 * RC 2 s ➞ 15 s 4 s ➞ 20 s Non tripping point at 125°C 1 * RC 1 * RC Maximum and minimum limit of ultimate trip 20 10 5 4 3 2 In 10 2 -2 3 45 10-1 2 3 45 1 2 3 45 2 3 45 2 3 4510 100 1000 +125C +25C -55C 84 400 0 - 6 - 8 84 400 0 - 6 - 8 84 400 0 - 6 - 8 84 405 0 -60 -20 -40 0 20 40 60 80 100 120 0,8 In 1,2 1,4 1,6 1,8 2 84 400 0 - 6 - 8 84 400 0 - 6 - 8 84 400 0 - 6 - 8 84 405 0 Non-trip threshold Trip threshold Current (as percentage of In) Ambiant temperature °C 84 408 1 84 418 0 84 408 0
  • 30. || WWW.CROUZET-AEROSPACE.COM || 30 || ELECTRICAL PROTECTION DISTRIBUTION Rating Faston Flying leads 1 A 84 405 001 1.5 A 84 405 040 2 A 84 405 002 2.5 A 84 405 012 3 A 84 405 003 5 A 84 405 005 84 405 045 7.5 A 84 405 007 10 A 84 405 010 15 A 84 405 015 20 A 84 405 020 25 A 84 405 025 REFERENCES Button color White • • Mounting hardware Faston terminal Barrel nut M12-100 + 500mm flying leads Conformity standard Air 6 625-403 • • GAM TI-II-40 • • EN 3773-3774* • • * our equipment complies with EN standards Mass / MTBF / Technical file Weight 15 25 MTBF FH (Typical) 3.6 M 3.6 M Technical file SP 4397 SP 9925 Environmental Salt spray 48h 5% NaCl Humidity: Test b RTCA DO160 10 cycles Operating temperature -60°C +125°C Acceleration up to 20 g Shock up to 50 g (11 ms) Vibration (sinusoidal) 10 g-PK from 10 to 2000 Hz Vibration (random at RC) up to 9.26 Grms from 10 to 2000 Hz Mechanical Operating force Endurance no load 40 000 cycles on resistive load 40 000 cycles Tightening torque (barrel nut) recommended: 4 N.m ; Max.: 5 N.m Tightening torque (terminal screw) 1.7 N.m +-0.1 Electrical 28 VDC 115 VAC (400 Hz) 115 VAC 60 Hz-230 VAC 50 Hz Breaking current 1CO + 2OCO 3000 A 1500 A CONTACT Crouzet Aerospace Dielectric 1500 V 1500 V Endurance cycles 5000 5000 Insulation resistance above 100 MΩ above 100 MΩ Working life (endurance) at 5° RC 1000 cycles 1000 cycles Auxiliary contact current 0.1..0.2 A 0.1..0.2 A Voltage drop compliance EN2495/2995/MS3320/AS33201 EN2495/2995/MS3320/AS33201 GENERAL CHARACTERISTICS SINGLE POLE SMALL MODEL CIRCUIT BREAKER PUSH-PUSH FLYING LEADS VERSION Read also p. 46
  • 31. || WWW.CROUZET-AEROSPACE.COM || 31 || ELECTRICAL PROTECTION DISTRIBUTION 1,5 12,8 28max. 9,2 84 405 0 19,8 max. 2 9,5 14,3max. Ø8,4 0,8 Ø11 17,4 6,35 6,3 5,9 DIMENSIONS PANEL CUTOUT RECOMMENDATION 84 405 0 84 405 040 Version 84 405 0 Version 84 405 04X › Thickness 1.6 mm ➞ 3 mm 9,5 Ø3,1 Ø12,5 30min. 9,5 Ø12,5 20 min. Ø3 CURVES Trip times envelope for temperature from -55°C to 125°C (direct overload) Maximum and minimum limit of ultimate trip 20 10 5 4 3 2 In 10 2 -2 3 45 10-1 2 3 45 1 2 3 45 2 3 45 2 3 4510 100 1000 +125C +25C -55C 84 400 0 - 6 - 8 84 400 0 - 6 - 8 84 400 0 - 6 - 8 84 405 0 -60 -20 -40 0 20 40 60 80 100 120 0,8 In 1,2 1,4 1,6 1,8 2 84 400 0 - 6 - 8 84 400 0 - 6 - 8 84 400 0 - 6 - 8 84 405 0 Non-trip threshold Trip threshold Current (as percentage of In) Ambiant temperature °C Rating 1 ➞ 3 A 5 ➞ 25 A 5 ➞ 25 A Non tripping point at 25°C 1.15 In 1.15 In 1.15 In Tripping point at 25°C 1.4 In 1.4 In 1.4 In Tripping time at 2 * RC 2 s ➞ 15 s 4 s ➞ 16 s 6 s ➞ 20 s Non tripping point at 125°C In In In
  • 32. || WWW.CROUZET-AEROSPACE.COM || 32 || ELECTRICAL PROTECTION DISTRIBUTION Button color Green • Black • • Rating GFCB (star)** Three pole AFCB Single pole AFCB 1 A 3 A 84 411 136 84 411 103 84 401 503 5 A 84 411 137 84 411 105 84 401 505 7.5 A 84 411 138 84 411 107 84 401 507 10 A 84 411 139 84 411 110 84 401 510 15 A 84 411 140 84 411 115 84 401 515 20 A 84 411 141 84 411 120 84 401 520 25 A 84 411 142 84 411 125 84 401 525 ** on request the GFCB is available in star or triangle configuration with different thresholds Mounting hardware Threaded barrel M12-0.75 M12-100 • • • 7/16 Terminal Screw 8-32 UNC • • • M4 REFERENCES Conformity standard EN 2592 - EN 2996* • • EN 2495* • AS 5692 • • • * for thermal part Mass / MTBF / Technical file Without mounting hardware 141 141 31 With mounting hardware 150 150 33 MTBF FH (Typical) 150 000 150 000 450 000 Environmental Salt spray According DO160 section 14 category B Humidity According DO160 section 6 category B Operating temperature (1 to 15 A) -60°C +125°C Operating temperature (20 and 25 A) -60°C +90°C Operating temperature (Arc fault and ground fault detection) -40°C +71°C Acceleration (centrifugal) 17g Shock up to 50 g (11 ms) -1/2 sine Vibration (sinusoidal) 10 g-PK from 5 to 2000 Hz Vibration (random at RC) 5.82 Grms from 10 to 2000 Hz Mechanical Operating force 8Npush80N 5Npull30N Endurance no load 5 000 cycles on resistive load 5 000 cycles Tightening torque (barrel nut) recommended: 4 N.m ; Max.: 5 N.m Tightening torque (terminal screw) 1.7 N.m +-0.1 Electrical 115/200 VAC (400 Hz) Breaking current 1CO + 2OCO 2000 A Dielectric 1500 V Endurance cycles 5000 (with cos fi: 0.7) Insulation resistance above 100 MΩ Working life (endurance) at 5° RC 50 cycles Auxiliary contact current 0.1..0.2 A Voltage drop compliance MS14154/AS14154A/EN2592/2996/3774 GENERAL CHARACTERISTICS GROUND FAULT ARC FAULT CIRCUIT BREAKER GFCB AND AFCB Read also p. 8-11
  • 33. || WWW.CROUZET-AEROSPACE.COM || 33 || ELECTRICAL PROTECTION DISTRIBUTION DIMENSIONS PANEL CUTOUT RECOMMENDATION CURVES 84 401 5 84 401 5 84 411 1 84 411 1 › Thickness 1.6 mm ➞ 2.4 mm › Thermal trip › Arc fault trip: Compliant with AS5692 › Ground fault trip thresholds Trip times envelope for temperature from -60°C to 125°C (direct overload) 20 10 5 4 3 2 In 10 2-2 3 45 10-1 2 3 45 1 2 3 45 2 3 45 2 3 4 1.10 1.40 1.60 510 100 1000 +23C -55C +125C 84 310 0 - 3 - 6 84 314 2 -60 -20 -40 0 20 40 60 80 100 120 0,8 In 1,2 1,4 1,6 1,8 Non-trip threshold Trip threshold Current (as percentage of In) Ambiant temperature °C 2 84 310 0 - 3 - 6 84 314 2
  • 34. || WWW.CROUZET-AEROSPACE.COM || 34 || ELECTRICAL PROTECTION DISTRIBUTION 84 404 011 84 404 004 84 313 626 84 404 00784 411 860 Small Model Single Pole Description Aux. contact Ref. Conformity Barrel threadings Terminal screw Control button M12-0.75 M12-100 7/16 H8-32 CB M4 DPMU Yes 84 404 002 E0486A01 • Pushed in Push push faston No 84 404 003 • Without DPMU No 84 404 004 • • Pushed in DPMU No 84 404 005 • • Popped out DPMU Yes 84 404 006 E0486B01 • Without Frog legs No 84 404 009 • 6-32UNC2A Without Frog legs Yes 84 404 010 • 6-32UNC2A Without One terminal DPMU No 84 404 011 • • Pushed in Frog legs Yes 84 404 013 • • Without Small Model Three Pole Description Aux. contact Ref. Conformity Barrel threadings Terminal screw Control button M12-0.75 M12-100 7/16 H8-32 CB M4 DPMT Yes 84 404 007 E0486B03 • Without DPMT Yes 84 411 860 E0486A03 • Pushed in Big Model Single Pole Description Aux. contact Ref. Conformity Barrel threadings Terminal screw Control button M12-0.75 M12-100 7/16 H8-32 CB M4 84 306 xxx Big Model Three Pole Description Aux. contact Ref. Conformity Barrel threadings Terminal screw Control button M12-0.75 M12-100 7/16 Bus-bar CB M4 DGMT Yes 84 313 626 E0486A04 • • Pushed in DGMT No 84 313 044 E0486A04 • Pushed in REFERENCES DUMMY CIRCUIT BREAKER DUMMY SIMULATOR CB Based on «standard» or «catalog CBs» (in the light blue column) the dark grey column gives the references of the Simulator CBs: Standard Simulator Standard Simulator Standard Simulator Standard Simulator Standard Simulator Rate (A) EN3661-004 green button same with black button 844006 green button same with black button 844026 green button same with black button 844006 green button same with black button rotated 180° EN2495-M 0.5 A Rating same with different button value DGMU DGMU DPMU DPMU DPMU DPMU DPMU DPMU DPMU DPMU 0.5 84400611 84400650 84400611 84400636 84402011 0.75 84400637 1 84400601 84400651 84400601 84400638 1.5 84400652 84400639 2 84400640 2.5 84400612 84402612 84402712 84400612 84400641 3 84400603 84400653 84402603 84402703 84400603 84400642 84402036 4 84400604 84400654 84400604 84400643 5 84400605 84400655 84402605 84402705 84400605 84400644 84402037 7.5 84400607 84400656 84402607 84402707 84400607 84400645 84402038 10 84400610 84400657 84402610 84402710 84400610 84400646 84402039 15 84400615 84400658 84402615 84402715 84400615 84400647 84402040 20 84400620 84400659 84402620 84402720 84400620 84400648 84402041 25 84306325 84306353 84400625 84400661 84402625 84402725 84400625 84400649 84402042 30 84400630 84400662 35 84306335 84306352 84402043 50 84306350 84306351 no marking 84402044 mounting hw mounting hardware on CB mounting hardware in bag mounting hardware on CB mounting hardware on CB mounting hardware on CB CHOICE BY STANDARD/RATING Read also p. 46 and p. 49 SELECTION GUIDE FOR SIMULATOR CBs
  • 35. || WWW.CROUZET-AEROSPACE.COM || 35 || ELECTRICAL PROTECTION DISTRIBUTION PANEL CUTOUT RECOMMENDATION DIMENSIONS 84 404 001 84 404 01184 404 006 84 404 007 › Thickness 1.6 mm ➞ 3 mm Please, refer to the according technical file.
  • 36. || WWW.CROUZET-AEROSPACE.COM || 36 || ELECTRICAL PROTECTION DISTRIBUTION Rating red gag 23 422 009 grey cap panel hole diam 12.5mm 24 323 003 brown cap panel hole diam 12.5mm 24 323 005 opaque covers Barrel M12*1 79 254 157 Barrel M12*0.75 79 254 154 Barrel 15/32 79 254 155 Barrel 7/16 79 254 156 clear covers (see through) Barrel M12*1 79 254 150 Barrel M12*0.75 79 254 151 Barrel 15/32 79 254 152 Barrel 7/16 79 254 153 male pin EN 3155 -016M 2018 25 637 611 Other information crimping tool for pin 25637611: crimp tool: M22520/1-01 and crimp locator: M22520/1-02 insertion extraction tool: Ref. Deutsch: 020-0008-20 male pin Ref. Deutsch: 006-0912-20 Conformity Standard IPX7 • VG 95345 chap. 23 • Gag Caps Covers Auxiliary contact pin REFERENCES ACCESSORIES ACCESSORIES DIMENSIONS 79 254 150-153-156-157 24 323 003 24 323 005 23 422 009 EC 79 25 40 85 25 637 611 79 254 150 Safety guard Nut Seal Connector pins for auxiliary contacts: EN 3155 - 016 M2018 Wire gage: 18 to 24 (0.21 to 0.93mm2 ) Caution: For good water proofness: the CB pannel must be 2.5 mm thick and positioning key hole must be «blind». Torque of 4 N.m must be applied to the nut ; not on the cover. Extraction tool not supplied Crimped pin
  • 37. || WWW.CROUZET-AEROSPACE.COM || 37 || ELECTRICAL PROTECTION DISTRIBUTION ELECTRICAL DISTRIBUTION SELECTION GUIDE Crouzet Aerospace is proud to contribute towards the “greener Aircraft” through its bus connected components and through its never ending quest for more compact and lighter solutions. Crouzet Aerospace delivers 3 standard distribution components: ›› RCCB ›› A Circuit Breaker panel Kit ›› Solid State Circuit Breakers With smart management, loads can be powered off during some flight phases and in rush current can be reduced. This technique will decrease the electrical network complexity and weight. Using information provided by the load, SSCB and RCCB’s role can encompass wire protection and load protection LOAD AND WIRE PROTECTION WITH SSPC LOAD AND WIRE PROTECTION WITH RCCB
  • 38. || WWW.CROUZET-AEROSPACE.COM || 38 || ELECTRICAL PROTECTION DISTRIBUTION CIRCUIT BREAKER PANEL KIT PCB KIT FOR FASTON CB complete panel PCB rings and spacers complete panel 84 341 072 bottom spacer 79 2194 30 lateral spacer 79 219 431 central spacer 79 219 432 centring ring 79 219 333 EN 4165 connector support 79 219 440 PCB with 16 receptacles 79 219 439 front plate 79 219 441/42 Circuit Breaker type Faston without auxiliary contact (conical barrel) 84 406 039..84 406 048 Faston with auxiliary contact non polarised (conical barrel) XB 406 839..XB406 848 Faston without auxiliary contact polarised (conical barrel) XB 406 639..XB406 648 Weight (g) Without standard CB (only mechanichal panel) 351 Panel with 16 Circuit Breakers 528 MTBF FH (Typical) 60 000 REFERENCES Spacer kit 5 short spacers 79 219 443one central spacer five short spacer (below) Connection possibilities EN4165 (2 modules of 8 size 16 pins) with pins soldered on the vertical PCB EN4165 (2 modules of 8 size 16 pins) held by 79219440 with crimped contact pins Flying leads soldered on the vertical PCB Environmental DO160 section Test category method 4 Altitude similarity 5 Temperature from -60°C..71°C (with power) test 6 Humidity test 7 Crash MIL STD 810E test 80 ms 1/2 sine (20 g on all axes) 8 Vibration MIL STD 810E helicopter test random wide band+ sine strips 9 Explosion proofness demonstration 10 Waterproof N/A 11 Fluids N/A 12 Sand and dust similarity 13 Fungus resistance no tested 14 Salt spray 48h no power + 48h dry test 15 Magnetic effect demonstration 16 ➔ 23 EMI N/A 25 Inflammability FAR 25853 demonstration Mechanical torque (max) N.m Power stud (M6) 3.9 Every screw/spacer (M3) 2 Locktite on every screw/spacer (not on power stud nut) Electrical Vehiculated current 15*4+6*10+6*5=150 A from -60°C to 71°C Vehiculated power 150*28=4200 W Prospective current (blocked mechanism) 1800 A 28 VDC (no copper tracks destruction) Dielectric 700 VDC between 2 copper tracs and between each track and power feeder GENERAL CHARACTERISTICS Read also page 15
  • 39. || WWW.CROUZET-AEROSPACE.COM || 39 || ELECTRICAL PROTECTION DISTRIBUTION DIMENSIONS AND SPECIFIC ZONES FOR CB RATINGS CENTRING RING PANEL CUTOUT RECOMMENDATION AND CIRCUIT BREAKER TYPE PIN TO CB AFFECTATIONS HOW DOES IT WORK? The assembly is qualified and distributes securely up to 150 A under 71°C with a configuration carrying four 15 A, six 10 A and six 5 A Circuit Breakers (thus a total of 16 CBs). The distribution connector can be mounted on the vertical PCB or distribution leads can be soldered on the vertical PCB. EN4165 84 406 0XX XB406839 XB406639 connector EN 4165 8T16 › Thickness: 1.6 mm Module A CB# 1 F6 2 F2 3 F1 4 F7 5 F3 6 F8 7 F5 8 F4 vertical PCB to solder connector or flying leads power feeder ›› If EN 4165 is soldered and used with leads the size 16 pins limit the current to 13 A: Max output: 4*13+6*10+6*5=142 A ›› If leads are soldered directly on the vertical PCB, the maximum currents are: Red zone: 15 A max Yellow zone: 10 A max } Max output: Green zone: 5 A max 4*15+6*10+6*5=150 A A B Module B CB# 1 F9 2 F10 3 F14 4 F11 5 F15 6 F12 7 F13 8 F16 breakers up to 15 A breakers up to 10 A breakers up to 5 A Layout 0816: 8 contacts size 16 x 2
  • 40. || WWW.CROUZET-AEROSPACE.COM || 40 || ELECTRICAL PROTECTION DISTRIBUTION REMOTE CONTROL CONTACTOR CIRCUIT BREAKER RCCB 115/200 VAC 360-800 HZ Environmental Salt spray 48h at 5% NaCl 48h at 5% NaCl Operating temperature -40°C to +85°C -40°C to +85°C Acceleration (centrifugal) up to 10 g up to 10 g Shock 25 g - 11 ms 25 g - 11 ms Vibration (sinusoïdal) 10 g from 5 to 2000 Hz 10 g from 5 to 2000 Hz Vibration (random) 5.8 g from 10 to 2000 Hz 5.8 g from 10 to 2000 Hz Mechanical Operating force (R push button) 10 N 10 N Max. admissible force (R push button) 50 N 50 N Tightening torque (barrel nut) 3 +/- 0.2 Nm 3 +/- 0.2 Nm Tightening torque (terminal screw) 2.3 +/-0.1 Nm 2.3 +/-0.1 Nm Weight 550 g 700 g MTBF FH (Typical) 300 000 300 000 Mounting hardware Fixing screws (to panel or closet wall) 3 screws 10-32 UNF-3B 3 screws 10-32 UNF-3B Connexion screws (to power feeders lugs) 6 screws 8-32 UNC-3A 6 screws 8-32 UNC-3A Matched connector for control signals Air LB00 1748-120.00 Sub D 15 Female Connector retaining screw M3x0.5 - Contactor Function Actuating voltage 17 V= ≤U≤32 V (a2 - a1 pins) 17 V= ≤U≤32 V (10 - 2 pins) Max Pull-in current 3A during max 50 ms 3A during max 50 ms Max. continuous hold-in current 300 mA 300 mA Min. Hold-in voltage 10 V= 10 V= Response time (off to on) 60 ms 60 ms Release time ( on to off) 60 ms 50 ms Direct visual indication of contacts position on front plate OPEN / CLOSE OPEN / CLOSE Auxiliary contact n°1 SPDT type Intermediate current level Common/NC/NO: b1/c1/d1 28 VDC 3A (L/R 5 ms) - 5 VAC 250 mA Common/NC/NO: 3/4/5 28 VDC 3A (L/R 5 ms) - 5 VAC 250 mA Auxiliary contact n°2 SPDT type Low level current Common/NC/NO: b2/c2/d2 3 VDC 0 to 20 mA resistive 28 VDC 200 mA (L/R 5 ms) Common/NC/NO: 6/7/8 3 VDC 0 to 20 mA resistive 28 VDC 200 mA (L/R 5 ms) Dielectric stength I leakage 1 mA @ 1500 V~ I leakage 1 mA @ 1500 V~ Insulation resistance ≥ 100 MΩ ≥ 100 MΩ Contactor Endurance cycles with RC at 40°C cos Fi=0.7 100 000 cycles 100 000 cycles Current measurement Breaker function Current transformer ratio - 0.5 Volt rms for 10 A rms Integrated load resistance (on current trasformer output) - 50 Ω Breaking at 115 VAC 360-800 Hz 2000 A 2000 A Trip status auxiliary contact (incorporated diode) 28 VDC 10 to 200 mA 28 VDC 10 to 200 mA Visual indication of trip status by R button on front plate Yes Yes Operating circuit disable after break Yes Yes Resetting after trip By push on front R button By push on front R button Endurance at 2*RC 1 000 cycles 1 000 cycles GENERAL CHARACTERISTICS Rating Without current transformer With current transformer 35 A 84 354 335 84 354 435 50 A 84 354 350 84 354 450 60 A 84 354 360 84 354 460 REFERENCES C1 c2 b2 d2 c1 b1 d1 d3 c3 b3 a3 a2 a1B1 A1 C2 B2 A2 C1 c2 b2 d2 c1 b1 d1 d3 c3 b3 a3 a2B1 A1 Load terminals Output (current transformer) Thermal detection by bimetal strips Visual status Indication Block circuit diagram Reset and visual trip Indication Line terminals Auxiliary contacts Trip Command a2:0V a1:28V Management part Contactor function Circuit Breaker function Outputs to connector Block circuit diagram C1 7 6 8 411 12 13 14 QA QB QC 3 5 1 9 2 10B1 A1 C2 B2 A2 Current transformer Load terminals Thermal detection by bimetal strips Visual status Indication Reset and visual trip Indication Line terminals Auxiliary contacts Trip Command 2:0V 10:28V Management part Contactor function Circuit Breaker function Outputs to connector Sub D1584 354 3XX 84 354 4XX Read also page 16
  • 41. || WWW.CROUZET-AEROSPACE.COM || 41 || ELECTRICAL PROTECTION DISTRIBUTION DIMENSIONS TRIPPING CHARACTERISTICS HOW DOES IT WORK? The RCCB merges a contactor function and a circuit breaker function in a single unit. This association gives the following unique advantages: ›› Reduction of the length of generally large cross-sections wires (mass reduction and harness simplification) ›› Reduction of voltage drop (reduced number of contacts) ›› Reduction of volume ›› Improved reliability (less components) The contactor is closed when 28 V is applied on the command input. The RCCB has a status display window and a mechanical «TRIP indicator». When the CB has tripped, the mechanical «TRIP indicator» is «popped out» and must be pushed back in manually to RESET the circuit breaker (see page 16). The «protection function» overrides the «contactor function». After tripping, the RCCB must therefore be reset manually, this avoids any risk of spurious restarting. Without current transformer With current transformer -60 -20 -40 0 20 40 60 80 100 120 0,8 In 1,2 1,4 1,6 1,8 Non-trip threshold Trip threshold Current (as percentage of In) Ambiant temperature °C 2 84 310 0 - 3 - 6 84 314 2 20 10 5 4 3 2 In 10 2 -2 3 45 10-1 2 3 45 1 2 3 45 2 3 45 2 3 4 1.10 1.40 1.60 510 100 1000 +23C -55C +125C 84 310 0 - 3 - 6 84 314 2 40 5354,8 62 51 87,5 A2B2C2 Current transformer casing SUB D15 connector Closet wall mounting surface 10,2 6 1717 26,5 53 2 40 5354,8 62 57 34 53 66 76 88 A1B1C1 A2B2C2 Female connector Air LB 00 1748 - 120.00 M3 x 0.6-6H Minimum air gap for ventilation 3 holes for bus bars: 5.5mm 3 lug connection Range indication Status indication Closet wall mounting surface Manual Reset Inputside Outputside 3 floating nuts for panel mounting 10-32 UNF-3B Contactor (3 phases) Circuit breaker (3 phases) RCCB (3 phases) ALL IN ONE To load To load Control Control 333 3 3
  • 42. || WWW.CROUZET-AEROSPACE.COM || 42 || ELECTRICAL PROTECTION DISTRIBUTION SOLID STATE CIRCUIT BREAKER SSPC 28 VDC 115 VAC GFI Environmental DO160-G section Test 28 VDC 115 VAC 4 Operating temperature range -55 °C to +85 °C -55 °C to +85 °C 4 Storage temperature range -55 °C to +125 °C -55 °C to +125 °C 5 Temperature variation 8 Vibration 11 Contamination fluids 12 Sand and dust 13 Fungus resistance 14 Salt spray 17 Voltage spikes Category A Category A 18 Audio frequency conducted susceptibility Category R Category R 20 Conducted radio frequency susceptibility Category M Category M 20 Radiated radio frequency susceptibility Category B Category B 21 Emission of radio frequency energy Category M Category M 22 Lightning induced transient susceptibility Category B3H3L3 Category B3H2L2 25 Electrostatic discharges Category A Category A Mass / MTBF / Other Weight (g) 170 250 MTBF FH (Typical) 20 000 20 000 30 mA GFI option • Electrical (overall) 28 VDC 115 VAC Power supply 28 VDC (17 ➞ 46) 115 VAC / 380 ➞ 420 Hz Maintenance supply 28 VDC (17 ➞ 46) 28 VDC (17 ➞ 46) Maximum current consumption (SSPC Off) ≤ 40 mA ≤ 1 mA on 115 VAC Maximum current consumption (SSPC On) ≤ 50 mA ≤ 100 mA on 28 VDC Turn ON or turn OFF time ≤ 10 ms ≤ 10 ms Guarantee no trip limit 1.15 x rating current 1.15 x rating current Guarantee trip limit 1.40 x rating current 1.40 x rating current Overload trip delay See curve next page See curve next page Short circuit trip delay (8 x rated current) ≤ 3 ms 2 ms Short circuit trip delay (20 x rated current) ≤ 0.5 ms ≤ 0.2 ms Leakage current in Off state ≤ 10 µA ≤ 150 µA Residual voltage in Off state ≤ 200 mV ≤ 7 V GENERAL CHARACTERISTICS Rating SSCB 28 VDC SSCB 115 VAC 2 84 332 052 3 84 332 053 5 84 332 043 84 332 054 10 84 332 040 15 84 332 044 20 84 332 041 REFERENCES Conformity standard EN 2592* • • EN 2495* • • AS 5692** • AS 6019** • * for thermal protection ** possible contact Crouzet Aerospace Read also p.12 37 EASY TO INSTALL 1 - Power from feeder 2 - Power to the load 3 - In house ground (0 Volts) 4 - CAN BUS 5 - Optional Battery 28 V 1 - 115 VAC feeder 2 - 115 VAC Power to the load 3 - In house ground (0 Volts) 4 - CAN BUS 5 - Optional Battery 28 V 6 - 0 VAC feeder return (neutral) 7 - 0 VAC load return 28 VDC LOAD LOAD CAN 2.0B 1 5 5 3 3 6 2 4 1 2 7 4 CAN 2.0B 115 VAC28 VDC LOAD LOAD CAN 2.0B 1 5 5 3 3 6 2 4 1 2 7 4 CAN 2.0B 115 VAC Small current a few mA for in house power Small current a few mA for in house power Current returns path inside chassis or fuselage
  • 43. || WWW.CROUZET-AEROSPACE.COM || 43 || ELECTRICAL PROTECTION DISTRIBUTION 136 mm Max. 27mmMax.58mmMax. 11mm41.2mm 121.2 mm A1 28V from feeder 8 1 GND 9 28 V optional 2 SPARE_IN_4 10 GND 3 SPARE_IN_1 11 CANH 4 SPARE_IN_2 12 CANL 5 12 GND 6 SPARE_IN_3 14 reserved 7 GND 15 reserved A2 28 V LOAD 1 115 VAC to load 9 115 VAC from feeder 2 0 VAC feeder return 10 3 0 VAC feeder return (neutral) 11 4 12 5 SPARE_IN_1 13 SPARE_IN_2 6 SPARE_IN_3 14 CAN_L 7 CAN_H 15 GND 8 28 V optional 136 mm Max. 27mmMax.83mmMax. 11mm66.2mm 121.2 mm DIMENSIONS AND PIN ASSIGNEMENT CURVES 84 332 04X 84 332 05X ›› Connector is a Sub-D 17W2 male connector with 15 signal contacts and 2 power contacts. ›› Optional battery is used if the master controlling the CAN bus needs a reply from the SSCB even if feeder power is OFF. Spare inputs (SPARE_IN_X) can be used for limit switch inputs or GROUND/FLIGHT information. ›› Connector is a Sub-D 15 contacts male connector. The signal positions are given below. › Trip delay versus current 28 VCD › Trip delay versus current 115 VAC Fixation holes diameter: 5.2 mm Fixation holes diameter: 5.2 mm 0 2 4 6 8 10 12 14 16 18 20 1,E-04 1,E-03 1,E-02 1,E-01 1,E+00 1,E+01 1,E+02 I/In Time (s) 0 2 4 6 8 10 12 14 16 18 20 1,E-04 1,E-03 1,E-02 1,E-01 1,E+00 1,E+01 1,E+02 I/In Time (s)
  • 44. || WWW.CROUZET-AEROSPACE.COM || 44 || ELECTRICAL PROTECTION Secondary network simulator Primary network simulator INNOVATION FUTURE PRODUCTS TIME STAMPING CIRCUIT BREAKER FOR MAINTENANCE COST EVALUATION Using a specific software, the electronic board included in the Circuit Breaker can measure the time an equipment has been powered ON and transmit it to a portable device. This can be used to measure the real MTBF of the equipment. The time stamping products give same thermal protection as a standard Circuit Breaker. ›› Can most often replace a standard Circuit Breaker ›› Will give «hours ON» figures to check «predictable maintenance costs» (for power by the hour applications) DESIGN DEPARTMENT Crouzet Aerospace engineers and technicians develop new mechatronic components using all state of the art tools and methods. ›› COSMOS design for mechanical and thermal simulation ›› ProEngineer for mechanical conception and drawing ›› Altium and Pspice for electrical and electronic design and simulation ›› VISULA and ALTIUM for PCB design and routing ›› C_Compilers and VHDL for embedded software FPGA and microcontroller software are developed according to DO178 and D0254 up to level A Behavior of «prototypes» can be verified in our electrical lab environment that simulates primary and secondary aircraft distributions with «real loads». Available power sources are 28 VDC and 115 VAC and 230 VAC.
  • 45. || WWW.CROUZET-AEROSPACE.COM || 45 || ELECTRICAL PROTECTION DISTRIBUTION FREQUENTLY ASKED QUESTIONS 1 HOW TO USE CIRCUIT BREAKERS WITH LOADS USING VERY LITTLE CURRENT (EXAMPLE 100 mA): Definition of wetting current: it is the minimum current needed to flow through a mechanical switch while it is operated in order to break through any film of oxidation that may have been deposited on the switch contacts. It is the minimum current that enables 20-25 years operation of the circuit breaker. Example: If you want to power a load that has a 100 mA current consumption. You cannot use a single AWG20 wire and a 0.5 A or a 1 A circuit breaker to protect the AWG20 wire because the wetting current of a circuit breaker is 250 mA ➞ it will not operate properly after 5-10 years in the field (voltage drop will be incorrect). You must find another load (with a higher consumption than 250 mA; for instance a 2.3 A load) in the vicinity of your 100 mA load and use the circuit breaker and wire of «higher current load» in the following manner: Junction blocs (from Amphenol AIR-LB): Note: You must ensure that by unpowering both loads (i.e. by opening the breaker), you do not create a safety hazard. 2 STORAGE DURATION CIRCUIT BREAKER CYCLING (EXTRACT OF EN3773-001) The storage duration under conditions of §13.2 shall be three years maximum. After a longer period, the following tests shall be conducted before use: ›› Voltage drop at 2*RC ›› Tripping time at 2*RC at the ambient temperature of 23 °C. NOTE: Three to five switchings (cycling) shall be performed prior to check. If the second voltage drop measurement fails, the circuit breakers have to be scrapped.
  • 46. || WWW.CROUZET-AEROSPACE.COM || 46 || ELECTRICAL PROTECTION 3 WHEN DO YOU NEED PUSH-PUSH CIRCUIT BREAKER? With gloves it can be easier to use only one finger to open or close a protected line (rather than capture the button with index and thumb and pull/push on it). 5 WHY USE FAKE (DUMMY) CIRCUIT BREAKERS? When making a Circuit Breaker panel, you can require «Space» provisions for future loads (this is very frequent for helicopters where configurations are modified just before customer delivery or in the field). To reduce the delay time, OEM can want a pre-wired bus-bar and a pre-wired distribution wire and a fake Circuit Breaker. The ‘fake’ or dummy Circuit Breaker will hold in place the bus bar and hold in place the distribution wire so that they do not create shorts or hazards due to them being pre-wired and «loose» in the Circuit Breaker Panel. Such dummy Circuit Breakers can also bare signal contacts if required. ›› They are lighter than normal breakers because they are «empty». ›› They do not convey current between their terminals. ›› The button can be permanently pushed in or popped out. 30min. 20 min. 20min. 17 min. Push/Push 30min. 20 min. 20min. 17 min. Push/Pull Activated Deactivated Auxillary contacts galvanically isolated from the power give information on the status of the primary contacts. 6 HOW DO YOU USE AUXILIARY CONTACTS TO DETECT TRIPPED BREAKERS? 4 3 non polarised 5 3 polarised The auxiliary contacts are closed when primary contacts are open: Power Aux Aux Load 34 21 Power Aux Aux Load 34 21 Diode type: 1N 4007 4 WIRE GAGE CIRCUIT BREAKER RATING ASSOCIATION Small aircraft /helicopter Calibre/ratedcurrent LUG color Below or equal to 1 AWG 22 grey 1.5 ➞ 6 AWG 20 orange 7 ➞ 10 AWG 18 orange 11 ➞ 15 AWG 16 white 16 ➞ 20 AWG 14 white 21 ➞ 50 AWG 12 black Large aircraft Calibre/rated current LUG color Below or equal to 1 AWG 20 grey 1.5 ➞ 6 AWG 18 orange 7 ➞ 10 AWG 16 orange 11 ➞15 AWG 14 white 16 ➞ 20 AWG 12 white 21 ➞ 50 AWG 10 black Tripped /popped out Engaged /pushed in FREQUENTLY ASKED QUESTIONS
  • 47. || WWW.CROUZET-AEROSPACE.COM || 47 || ELECTRICAL PROTECTION DISTRIBUTION This implementation requires: 6 outputs + 1 ground going through a connector. The information is processed by a computer or connected to LEDs. SETBACK: you need n+1 wires to monitor n Circuit Breakers A) SOLUTION FOR 6 CB (WITH NON POLARIZED AUXILIARY CONTACTS): DAISY CHAIN B) SOLUTION FOR 6 CB (WITH NON POLARIZED AUXILIARY CONTACTS): This implementation requires: 1 output + 1 ground =2 wires going through a connector. SETBACK: you only know that one CB has tripped but you do not know which one. The information is processed by a computer or connected to LEDs. By duplicating the above grid layout: ›› 16 Circuit Breakers can be monitored with 4+4 lines = 8 lines (4 in - 4 out)= 24 ›› 256 Circuit Breakers can be monitored with 8+8 = 16 lines (8 in - 8 out)= 28 ›› 2n Circuit Breakers can be monitored with n+n = 2xn lines (n input lines and n output lines SETBACK: the information has to be processed by a microcontroller or an FPGA (or a CBMU). represented this way: C) SOLUTION FOR 16 TO 256 CB (WITH POLARIZED AUXILIARY CONTACTS): By using auxiliary contacts with diodes and a keyboard type interrogation:
  • 48. || WWW.CROUZET-AEROSPACE.COM || 48 || ELECTRICAL PROTECTION 7 HOW TO ASSOCIATE A LOAD WITH A CIRCUIT BREAKER AND A WIRE? You must persuade yourself that a thermal Circuit Breaker protects the wire from smoking and igniting; it does not protect the load. The following information is similar to EN3197. STEP 1 Chose a CB rating between 15 % and 20 % above the nominal current to be carried through the wire. This provision is needed because in the future, if you want to change for a more powerful load, or add new loads on the same line, or your mechanical load has more friction you will need margin on the CB rating. Generally military aircrafts CB will be loaded around 80% or 90% of RC, civilian aircrafts around 60% of RC. You must know the inrush current profile of your load (generally the worst case is when temperature is low) and check the compatibility of the inrush current with the chosen CB’s trip curve (see example next page). STEP 2 Select a wire gage that will ensure no more than 40 °C temperature rise when it is run through by your nominal current. For example (EN3841-100): Current rating A Cross section mm2 AWG* EN code Up to 1 0,6 20 2083-006 1.5 to 6 1 18 2083-010 7 to 10 1,2 16 2083-012 11 to 15 2 14 2083-020 16 to 20 3 12 2083-030 21 to 25 5 10 2083-050 26 to 40 5 10 2083-050 41 to 50 5 10 2083-050 * AWG = American Wire Gage STEP 3 You need to know the «final» routing of the wire because if it travels through a non-pressurized zone or is «buried inside a bundle» it will heat more and will «fume or ignite» quicker than expected. You will perhaps need to decrease AWG value (i.e. specify a larger cable size) to insure step 2 rule. STEP 4 The voltage drop from the generator’s point of regulation to the load or equipment must be compatible with the operating voltage of the load or equipment. In general: ›› In 28 VDC the voltage drop must not be more than 1 V between generator output and load input. ›› In 115 VAC the voltage drop must not be more than 5 V between generator output and load input. If your wire is very long, you will perhaps need to decrease AWG value (i.e. specify a larger cable size) to insure the above voltage drop. STEP 5 Verify that the minimum short-circuit current allows the tripping of the protection device in case of a fault near the load or equipment. Table 1 FREQUENTLY ASKED QUESTIONS
  • 49. || WWW.CROUZET-AEROSPACE.COM || 49 || ELECTRICAL PROTECTION DISTRIBUTION 40 Amp sec 30 20 10 0 1 3 9 EXAMPLE: I have a 28 VDC motor of 180W. The motor requires 180/28 = 6,4 A nominal current (when torque is high). Step 1 says that the correct rating for the circuit breaker could be a 7.5 A (around 20% above nominal current). Step 2 says that a AWG16 wire is suitable for a 6.4 A nominal current (with 6.4 A the temperature rise of the wire will be less than 40 °C). Unfortunately, when you connect the motor and power on the motor, the CB trips. This is due to the inrush current of the motor. If you look at the inrush current of your motor (with an oscilloscope for instance) it looks like the figure on the left: CONCLUSION: You must choose a 10A CB to be able to pass the inrush current. Also: the wire powering the motor is not in a pressurized zone (in a pressurized zone air is a heat sink) or it is imbedded inside a bundle. In this situation, it will not be cooled down by the surrounding air and will deteriorate with time. In accordance with Step 3, to reduce wire heating you finally must use a AWG14 wire. Motor inrush current Circuit Breaker trip envelope AWG16 wire heated by the adjacent wires in pressurized zone You notice that your motor stays above 15 A (2 times Rated Current) for 3 seconds ➔ this «collides» with the trip envelope of your Circuit Breaker Indeed, the above curve shows that at 2 times rated current (here 15 A for a 7.5 A CB) the CB will trip before 3 seconds. CONCLUSION: you must use a 10A CB with a AWG14 wire. 8 WHEN DO YOU NEED SIMULATOR CIRCUIT BREAKERS? Simulator Circuit Breakers can be connected to computer inputs. There are two ways to do this: 1 - Use the auxiliary contacts of a CB (adapted to convey 100 to 200 mA). If your «in the field CB» has a black button, you will require that your simulator CB (with auxiliary contacts) bares also a black button. For this reason the simulator family 8440227xx is a «black button» version derived from the 844026xx family (which has a green button). 2 - Use the power therminals of a 0.5 A CB (low resistor) and change the button marking to your need: 3A, 5A ➔ 35A etc... An example of such a solution is the simulator family 84402036 ➔ 84402044 which is internally 0.5 A CB (the 84402011) but bares a button marking of 3 to 35 A. AWG16 wire in non pressurized zone Non pressurized area (i.e. bad heat sink)
  • 50. || WWW.CROUZET-AEROSPACE.COM || 50 || ELECTRICAL PROTECTION 9 CROSS REFERENCE WITH OLDER CIRCUIT BREAKER MODELS 10 PART NUMBER CONSTRUCTION For DPMU, DPMT, DGMU, DGMT components, you can construct the article code with the following logic (some exceptions exist): OLD Threaded barrel Terminals e= d= Screw= NEW Threaded barrel Terminals e= d= Screw= PUSH/PULL 84 301 --- Stopped in 1993 No equivalency 84 303 0-- M12x075 12 7.2 M4 84 303 3-- M12x075 12 7.2 M4 84 305 0-- 7/16 12,8 5 8/32 84 400 0-- 7/16 12.5 5 8/32 84 305 3-- 7/16 12,8 5 8/32 84 400 8-- 7/16 12.5 5 8/32 84 305 51- M12x1 18 0 8/32 84 401 0-- M12X1 18 0 8/32 84 305 52- M12x1 18 0 8/32 84 401 8-- M12X1 18 0 8/32 84 305 6-- M12x1 18 0 8/32 84 401 6-- M12X1 18 0 8/32 84 402 0 M12X1 12.5 5 M4/L=8mm 85 402 8 M12X1 12.5 5 M4/L=8mm 86 402 6 M12X1 12.5 5 M4/L=8mm PUSH/PUSH 84 307 2-- diam=11.6 9.2 5.9 - 84 405 --- diam=11.6 9.2 5.9 - 1995 CROSS REF e= screw 84 400 6-8 barrel d= e: longitudinal entrax d: transversal entrax screw: threading barrel: threading Quid ref. creation 8 4 X X X X rating digit 1 rating digit 2 Small model 4 Big model 3 Single pole 0 Three pole 1 Barrel and screw* 1 to 6 Without auxiliary contacts 0 With polarised auxiliary contacts 6 With non polarised auxiliary contacts 8 or 3 Longreck 1 High vibration 2 Rating X X CIRCUIT BREAKER ARTICLE CODE * 1: barrel M12-100 terminal screw H8-32. 2: barrel M12-100 terminal screw CB-M4. Others: specific Example: Big model Three pole 25 A With polarised auxiliary contacts 84 313 625 FREQUENTLY ASKED QUESTIONS
  • 51. || WWW.CROUZET-AEROSPACE.COM || 51 || ELECTRICAL PROTECTION DISTRIBUTION 11 UNDERSTANDING THE MIL SPEC MARKING (PART NUMBER) Each time CROUZET manufactures a MS3320 circuit breaker, the Circuit Breaker is able to pass ›› High sine vibration levels as described in AS5809 i.e. (using method 204 of MIL STD 202), allowing the stamping of «V» on the product ›› Random vibration level C as described in AS5809 (using method 214 of MIL STD 202), allowing the stamping of «C» on the product Thus every MS33201/AS33201 product that we produce can be stamped as follows: MS3320-CXV (C = random vibration level, X = current rating, V = condition BC sine vibration) When V is not present it means that the Circuit Breakers passes level A of sine vibrations When C is not present it means random vibration level is not a required characteristic Also when a Circuit Breaker passes level B and C of sine vibration, it is able to pass level A of sine vibration as they are lower than B and C levels, thus, our ability to produce Circuit Breakers with the MS3320-CXV characteristics encompasses the following versions: MS3320-CXV of course, but also MS3320-CX and, MS3320-XV and, MS3320-X ENGLISH AC: Alternative Current AIC: Aircraft Inhabited Cargo AFCB: Arc Fault Circuit Breaker ATP: Acceptance Test Procedure AWG: American Wire Gage CB: Circuit Breaker CBMU: Circuit Breaker Management Unit CFRP: Carbon Fibre Reinforced Polymer (carbon composite) CT: Current Transformer DC: Direct Current EHA: Electro Hydraulic Actuator EBHA: Electrical Backup Hydraulic Actuator EASA: European Aviation Safety Authority EWIS: Electrical Wiring Interconnect System FAA: Federal Aviation Authority FH: Flight Hours FPGA: Field Programmable Gate Array GFCB: Ground Fault Circuit Breaker IFE: In Flight Entertainment IPX7: Ingress Proctection marking X7 LED: Light Emitting Diode LMU: Load Management Unit LRU: Line Replaceable Unit MTBF: Mean Time Between Failure OCO/CO: Open Close Open / Close Open OEM: Original Equipment Manufacturer PCB: Printed Circuit Board PLD: Program Logic Device QPL: Qualified Part List (Navair) RMS: Root Mean Square RC: Rated Current RCCB: Remote Control Circuit Breaker REACH: Registration, Evaluation and Authorization of Chemicals ROHS: Restriction of Hazardous Substances SiC: Silicium Carbide SSCB: Single Solidstate Circuit breaker (an electronic circuit breaker = a single channel SSPC) SSPC: Solid State Power Controller UAV: Unmanned Aerial Vehicle FRENCH DPMU: Disjoncteur Petit Modèle Unipolaire DGMU: Disjoncteur Grand Modèle Unipolaire DPMT: Disjoncteur Petit Modèle Tripolaire DGMT: Disjoncteur Grand Modèle Tripolaire ACRONYMS Pushbutton if no letter ➔ normal length if L present ➔ Longneck pushbutton Sine Vibration level (method 204 of MIL-STD-202) if no letter ➔ condition A (10 g peak) if V present ➔ condition B C (15 g peak) Amperage Rating Random Vibration (method 214 of MIL-STD-202) level C thru K Level C = 9.26 Grms, Level D = 11,95 Grms, Level E = 16,31 Grms MS3320 - C5VL
  • 52. Warning: The product information contained in this catalogue is given purely as information and does not constitute a representation, warrantly or any form of contractual commitment. Crouzet Automatismes SAS and its subsidiaries reserve the right to modify their products without notice. It is imperative that we should be consulted over any particular use or application of our products and it is the responsability of the buyer to establish, particularly through all the appropriate tests, that the product is suitable for the use or application. Under no circumstances will our warranty apply, nor shall we be held responsible for any application (such as any modification, addition, deletion, use in conjunction with other electrical or electronic components, circuits or assemblies, or any other unsuitable material or substance) which has not been expressly agreed by us prior to the sale of our products. FRANCE InnoVista Sensors™ 2 rue du Docteur Henri Abel, CS 60059 26902 Valence Cedex 9 FRANCE Tel.: +33 (0) 475 802 101 Fax: +33 (0) 475 828 900 relationclient@crouzet.com GERMANY / AUSTRIA / SWITZERLAND InnoVista Sensors™ Otto-Hahn-Str. 3 40721 Hilden DEUTSCHLAND Tel.: +49 (0) 2103/980-0 Fax: +49 (0) 2103/980-222 kundenservice@crouzet.com ITALY InnoVista Sensors™ Via Viganò De Vizzi, 93/95 20092 Cinisello Balsamo (Mi) ITALIA Tel.: +39 (02) 66 599 211 Fax: +39 (02) 66 599 218 assistenzaclienti@crouzet.com USA InnoVista Sensors™ 1461 Lawrence Drive Thousand Oaks, CA 91320 USA Tel.: +1 (800) 677 5311 Fax: +1 (800) 677 3865 info@crouzet.com AMERICAS EUROPE COUNTRIES NOT LISTED InnoVista Sensors™ 2 rue du Docteur Henri Abel, CS 60059 26902 Valence Cedex 9 FRANCE Tel.: +33 (0) 475 802 102 Fax: +33 (0) 475 828 900 relationclient@crouzet.com OTHER COUNTRIES WWW.CROUZET-AEROSPACE.COM WWW.INNOVISTASENSORS.COM Ref.:6735003AEN|02/2016-Photos:Ginko,DanielLattard,Airbus,Bombardier,Embraer,Eurocopter,Antonov,Gulfstream,©EricRaz/Eurocopter,i-Stock