Reliability testing is critical for new component qualification, design change validation, or field failure simulation for root cause analysis. In many cases, with tight project schedules and scarce available resources, some important critical characteristics of a component or subsystem are overlooked. This will potentially result in new failure modes after implementing changes in production. The author will explain how to develop an effective test plan using the 6σ (Six Sigma) problem solving process, IDOV (Identify, Design, Optimize and Validation), to make the testing simple but efficient.
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4. Agenda
Introduction
What and Why Reliability Testing
Effective Test Plan Development
Process Map
Case Studies
Summary
Questions?
8/24/2011 2
5. Introduction
My background
Expertise in warranty analysis, reliability modeling and testing
Work experience with home appliances (Whirlpool), commercial and
residential HVAC products ( Trane, Research Products Corp.)
Research Products Corporation: since 1938, is a leading manufacturer of
products for HVAC industry, business includes:
Aprilaire: Indoor air quality systems for temperature control, humidity
control, ventilation and filtration.
GeoSystems: Geothermal Heat Pump (ECONAR, HydroHeat)
DRI-STEEM: Humidification systems for health care, industrial, process-
critical, commercial and residential humidification applications worldwide.
Technical Services:
Authorized Qualmark testing facility: HALT, HASS, Environmental
Testing
IEC 6100 testing: Electromagnetic compatibility (EMC), Electrostatic
Discharge
Air Flow testing, ASHRAE 52.2: Air Filter testing
8/24/2011 3
6. Introduction
Reliability is probability that a device will
perform it’s intended function during a specified
period of time under stated condition
Design for Reliability
Reliability Modeling
Identify high risk components
Allocate reliability growth plan for higher reliability target
Perform root cause analysis for corrective actions
Reliability Testing
Qualification, ALT, HALT
DFMEA, FRACAS, others
8/24/2011 4
7. Reliability Test – Qualification
Qualification Test
Verify if new design/components meet design
specification – function and operation
condition, agency specification – UL or others
Functional test under expected operating
conditions specified in company engineering
standard or design specification
Comply with industry standard / regulation
Not intended to fail, not test to failure (TTF)
8/24/2011 5
8. Reliability Test – ALT
Accelerated Life Testing
Verify if the new design/components meet
design life expectation
Operational Cycling: on/off
Continuous operating under specified conditions
Elevated environmental stress
Thermal cycling / thermal shock
Corrosion resistance test
Vibration
Test to failure
Simulate field failure
Compare different designs/suppliers
Allow life prediction
8/24/2011 6
9. Reliability Test – ALT
Smaller sample size (4 – 16) depend on stress level
Pair test: test with baseline part
Current production samples
Different suppliers
Different Design
Stress Levels to simulate real failure mode
Understand failure mechanisms
Operating condition and material limit
Worse case scenarios
What “Test to Failure” Results Reveal
Same failure modes as seen in field
Operation margin
Root cause of failures
Optimize design parameters
8/24/2011 7
10. Reliability Test – HALT
HALT (Highly Accelerated Life Testing)
Identify weak links for new design or
comparison test
Temperature limits
Vibration limits
Thermal Shock
Combined Thermal Shock and Vibration
Compare different design or supplier quality
Design margin
Operating limit
8/24/2011 8
11. Testing Standards
Industry Standards
ANSI/AMCA (American National Standards Institute / The
Air Movement & Control Association International Inc)
ANSI/AMCA-204: Operation Vibration (fan motor)
ASTM (American Society for Testing and Materials)
B117: Salt Spray
NEMA (National Electrical Manufacturing)
NEMA MG-1: Motor
NEMA 4: enclosures
UL 1995: Heating and Cooling Equipment
Company Engineering Standards or
Specifications
ES (Engineering Standard)
Design Specification
8/24/2011 9
12. Reliability Testing
No industry standards available
No specifications in design documents
No testing procedures to follow
Varied from part to part, from application to
application
Each test requires unique method
Difficulties to simulate field failure in lab
Even harder if complete new design or application
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13. Test Plan Development Process
Identify (I) failure modes and failure mechanisms
Understand history – warranty performance and field feedback
Evaluate/verify under conditions for seeable misuse, not just anticipated use
condition
Failure modes: list all well known and unknown
Design (D) test method and test matrix
Develop test methods for critical failure modes
Determine failure detection, failure criteria, DOE
Optimize (O) test method and testing parameter
Run pilot tests to find out most reasonable setup
Time and cost effective
Validate (V) test method and failure modes
Validate test method
Verify testing part meet design specification – functionality and life
8/24/2011 11
14. Six Sigma Methodology: IDOV
Road Map
Success: replicate field failure and eliminate it
8/24/2011 12
15. Test Plan Contents
Functions of part
Design limit: max. temperature, pressure, current,
torque
Operational load – mechanical, electrical, thermal
Input / output signals – wiring diagram
Operating condition
Normal use condition
Customer misuse
Material properties
Failure modes
What, Where and How
Root Cause Analysis (RCA) – true reason of failures
8/24/2011 13
16. Test Plan Contents
Testing Methods
Follow industrial standard if possible: UL, ASTM,
ASHRAE
Apply correct load (stress) – thermal, mechanical,
cycling, etc
Set appropriate stress level to simulate real application
condition
ALT, HALT, functional check under certain conditions
Failure criteria
Define “Failure” for lab test setup and monitoring
Testing Duration – how long going to test
Failure detection
8/24/2011 14
17. Subject Matter Experts Input
Design Engineers have best knowledge of design functions
(design specs)
Product Engineers know customer requirement and
operating conditions (operation mapping)
Quality / Manufacturing Engineers know how it fails
during production (failure mode, weak links, installation
issue)
Service Engineers know more customer complaints (failure
mode)
Material Engineers to help on failure mechanisms
Agency Experts: like UL and material test
Reliability Engineers to complete the puzzle: collect all
inputs from different teams, develop test plan for reliability
testing
Lab Test Engineers and Technicians to make it happen
Teamwork is Essential!
8/24/2011 15
18. Case Study (1) Door Handle Improvement
Functions
Provide service access into / Identify
out of unit for service
Unit size from 3ftx3ft to 10ftx12ft
Keep door closed while unit
operating Design
Background Information
Failure mode: broken handle
High failure rate but low
warranty cost Optimize
Possible Causes
Impact load from shipping
and handling Validate
Misuse – use as ladder or
grasp as moving handle
Others
8/24/2011 16
19. Case Study (1) Door Handle Improvement
Handle Broken by Impact Load
Moving unit by fork truck or crane, collision Identify
happens, hit handle:
Split Unit Weight Range: 2500 ~ 8000lb
Moving Velocity: 1.6 ft/s (1 mile/h, 0.5 m/s)
Impact Force range will be from 2000lb to 6400lb Design
Handles, guarding, and any protrusion may
fail when encounter such huge impact force
Optimize
Force = (W*V)/time
Assume: Collision in 2s
Validate
Impact
Test
8/24/2011 17
20. Case Study (1) Door Handle Improvement
Impact Test Identify
Drop part to concrete floor
Swing a ball to hit
Design
Shoot a solid block
Free drop solid block to hit handle
How to measure impact load? Optimize
Weight
Hit velocity
Validate
Hit time
Height
8/24/2011 18
21. Case Study (1) Door Handle Improvement
Optimize
Free drop cylinder start from 1 food Identify
Measure drop height
Validate Design
Run pilot test to confirm it will produce
same failure mode
Optimize
Other Tests
Shear test: use handle as ladder
Pull test: use handle as moving tool Validate
Operating rotation test not conducted
because no prototype unit available
8/24/2011 19
22. Door Handle Qualification Test
Impact Test New HDL: 2 feet,
Apply impact load to center point of no failure
Old: HDL: broken at 1
handle foot drop
Drop throw a 10lbs cylinder, drop
distance from 1 ft, increase drop
distance until handle breaks
New HDL: base crew
Shear Test bend or pull out
Old: HDL: passed 250lb
Apply 250 lb load on top of handle for 3
minutes, repeat loading 3 times at 10
minutes interval
Inspect any damages in handle assembly
Strap Test New HDL: Not broke
until 500lb, but base
Apply shipping strap load to end of crew bend or pull out
handle for 1 minutes, increase load from Old: HDL: Broke @ 200lb
300lbs until break handle
8/24/2011 20
23. Design Change on New Handle
Increase base screw size and add hardened
washer
Re-test
Success to fix old failure mode
Approval for new product application
Reliability model was updated, claimed to have
70% improvement
However, 3 months later in prototype units…..
8/24/2011 21
24. New Failure Mode
Cam Roller Loosens
Identify
Noticed loosening handle at
production floor
Partially lost function, would
not close door properly Design
Cam Roller
Potential Causes loosening gap
Torque specification between cam
roller and striker Optimize
Insert material hardness
Bolt material
Validate
22 8/24/2011
25. Actions to Fix New Failure Mode (IDOV)
P-Diagram to identify desired functions, Identify
noise factors, design control factors, error
modes
Design
Boundary Diagram to evaluate
interferences
FMEA Optimize
Put any potential failure modes into
consideration
Validate
Potential causes
Design, material, assembly process
Recommendations on Detection and Control
8/24/2011 23
26. Test Plan for Improvement
Identify failure modes Insert Type Washer Cam Torque Identify
Cam Roller loosening Current 1 Low
Current 2 High
Difficult to rotate Current 1 Low
Base screw loosening Current 2 High
Design
Testing parameters Harder 1 High
Harder 2 High
Add 1 or 2 washers to Harder 1 Low
cam bolt Harder 2 Low
Increase hardness of No Insert 2 Low
Optimize
insert plate No Insert 1 Low
Find proper bolt Torque No Insert 1 High
No Insert 2 High
Validate
8/24/2011 24
27. Test Setup
Mount door handles on Identify
door panel
How to Rotate Handles?
Manual operation? Design
PLC control operation?
Electrical drill?
Other automaton? Optimize
Rotate handle 360 degree
through striker by a Validate
electrical drill
8/24/2011 25
28. Test Result
Old handle exhibited same failure mode Identify
at about 50 cycles operation
Samples with one washer added meet
Design
life cycle requirement
Harder insert samples showed best
result in terms of tightness and insert Optimize
plate damage
No insert sample also demonstrated
improvement on the tightness Validate
Cost benefit
Easy to assembly
8/24/2011 26
29. Whole Plastic Handle
• Impact Test Identify
Apply impact load to the center point of the handle
(drop throw a metal ball or other objects), using a
10lbs object, drop distance from 1 ft, increase the drop
Design
distance until the handle breaks:
Optimize
Validate
Current HDL after 4 ft drops Whole Plastic HDL after 1 ft drop
8/24/2011 27
30. Corrective Actions based on Test Results
Generic Corrective actions for improvement:
Material change: material used did not meet design
specification
Manufacturing assembly change: part variation or
manufacturing defect cause infant failures
Design change: design concept change
Door Handle
Use harder insert material and torque tolerance limit was
specified
Apply hardened washers on both sides of insert plate
Handle without insert material showed similar performance
in terms of rotation cycling, but failed impact test and pull
test, it is not recommended
8/24/2011 28
31. Handles in HVAC Unit
This door handle becomes one of new features that our
customers enjoy most
High perceived quality
Easy to rotate
Very robust
8/24/2011 29
32. Lessons Learned
Focus well known failure modes, but never overlook
unknown failure modes
New design may introduce new failure modes while removing
well known failure modes
Use reliability engineering tools to identify potential failure
modes before start test planning
Do not skip steps, if not possible to do it, find alternative
way
8/24/2011 30
33. Case Study (2) – Anti Spin Rod
Anti-Spin Rod field failures
Identify
Fatigue at inner groove
Design life: 30,000 cycles
Broken
Design
Mount plate
Optimize
Screw
Actuator
Validate
Bracket
Fracture Surface
8/24/2011 31
34. Case Study (2) – Anti Spin Rod
Current Design and Machining Quality
Very rough groove surface Identify
Sharp groove edge - no radius
Some samples had less 90 degree bend angle
Design
Optimize
ALT Samples
Baseline: current production samples (bend, Validate
rough surface)
Improved surface with radius
8/24/2011 32
35. Case Study (2) – Anti-Spin Rod
Test Fixture Design
Identify
How to apply stress – air cylinder, weight
blocks, actual damper?
How to measure load? Design
Optimize
Not apply torque load to actuator, achieve Optimize
desired load by using fixed Jackshaft
Simple
but effective Validate
8/24/2011 33
36. Case Study (2) – Anti-Spin Rod
Validate
Identify
Measure actuator torque which is
same as part specified
Be able to duplicate field failure – Design
fatigue at inner groove
Optimize
Validate
8/24/2011 34
37. Case Study (2) – Anti Spin Rod
Test Results
ReliaSoft W eibull++ 7 - www.ReliaSoft.com
Unreliability vs Time Plot
1.000
U nreliability
20 – 40 K cycles
Design Margin
Design Margin Baseline: Rod Baseline
Lognormal-2P
RRX SRM MED FM
82% FR F=4/ S=5
Data Points
40 K cycles
U nreliability Line
0.800
Rod Rounded
W eibull-2P
RRX RRM MED FM
F=3/ S=0
Data Points
I ntervals
U nreliability Line
0.600
Improved:
Unreliability, F(t)=1-R(t )
40% FR
0.400
0.200
100K Cycles
Keyanna Qi
Trane
11/ 22/ 2010
0.000 12:39:15 PM
0 4.E+4 8.E+4 1.E+5 2.E+5 2.E+5
Time (Cycles)
Rod Baseline: µ=10.9874, σ=0.7704, ρ=0.9594
Rod Rounded: β=6.2192, η=1.3496Ε+5, ρ=0.9557
8/24/2011 35
38. Case Study (2)– Anti Spin Rod
Observe a lot from just watching
Failure rate of the improved samples were 50% less than the
baseline @ 100,000 cycles
Rounded sample show no failures within design margin,
failed part still works
Good to go……but, can be better?
Broke rod still functional
8/24/2011 36
39. Case Study (2)– Anti Spin Rod
Worst stress load
on weakest point
Is one groove better than two grooves
Inner groove is always subjected to shear stress when actuator
moves
If only one groove (cut outer groove) then shear (bending)
stress will transfer to angle corner – much stronger
Confirm with design team: no special reason to have end
groove
8/24/2011 37
40. Case Study (2)– Anti Spin Rod
Test one groove and
Validate
One groove with worst
surface quality
Test to 120,000 cycles, no
failures
Estimated to be better than
rounded sample
Less material
Lower machining
requirement
More robust
8/24/2011 38
41. From Good to Great
Test suspended at 120,000 cycles without any failure
ReliaSoft W eibull++ 7 - www.ReliaSoft.com
Unreliabilit y vs Time Plot
1.00 U nreliability
20 – 40 K cycles
Design Margin
Design Margin Baseline: R odBas el i ne
0.82 Lognorm al -2P
R R X SR M MED FM
F=4/S=5
40 K cycles
D ata Poi nts
0.80 U nrel i abi l i ty Li ne
R odR ounded
Wei bul l -2P
R R X R R M MED FM
F=3/S=0
Unreliability, F(t)=1-R(t)
D ata Poi nts
0.60 Interval s
U nrel i abi l i ty Li ne
Rounded: R odOne Groove
Wei bul l -1P
0.40
0.40 MLE SR M MED FM
F=0/S=6
U nrel i abi l i ty Li ne
One Groove:
0.20
0.15
100K Cycles Keyanna Qi
Trane
11/ 23/ 2010
3:38:34 PM
0.00
0 4.E+4 8.E+4 1.E+5 2.E+5 2.E+5
Time (Cycle s)
RodO ne Groove : β = 6 . 0 0 0 0 , η = 1 . 6 2 1 1 Ε + 5
RodBase line : µ = 1 0 . 9 8 7 4 , σ = 0 . 7 7 0 4 , ρ = 0 . 9 5 9 4
RodRounde d: β = 6 . 2 1 9 2 , η = 1 . 3 4 9 6 Ε + 5 , ρ = 0 . 9 5 5 7
8/24/2011 39
42. Lessons Learned
Make it from Good to Great
Understand functions of components and design
requirement
Understand limit of manufacturing process
Take one more step to make design more robust and cost
effective
Lower machining tolerance requirement
Reduce material use
As reliability and testing engineer, we are able to
help more than what others thought
New perspective to ask more questions
8/24/2011 40
43. Never Skip System Validation
Component passed qualification test alone, does
not mean it works in the subsystem or system
Validation tests to verify if the new component
meets design specification and life expectation at
system level
System Validation Tests
System / Subsystem Integration
Follow normal installation process
Subject to operating condition or accelerated stress level of operating
conditions
Meet life exception or confirm the old failure modes were
removed
8/24/2011 41
44. Summary
Reliability Engineer is not particular component expert (valve,
sensor, electrical controls, or system design), but be able to
collect information and collaborate with various engineering
groups to develop comprehensive reliability test plans
Reliability test plan development follows process of Identify –
Design – Optimize – Validate
Do not overlook any potential failure modes, especially unknown
failure modes
Apply DOE for design change optimization
Always run validation test for final approval
Put enthusiasm into your work to drive it from Good to Great
8/24/2011 42
45. Where to Get More Information
Annual Book of ASTM Standards
Materials, instrumentation evaluation or testing
ASHRAE Handbook
HVAC equipments and components
MG 1-2006 by National Electrical Manufactures
Association
Motor testing
Military Handbook: Reliability Prediction of Electronic
Equipment (MIL-HDBD-217F)
Consult with subject experts in your organization
They know more than you thought
8/24/2011 43
46. Questions
Thank you for your attention.
Do you have any questions?
8/24/2011 44