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May 2013
Presentado por
Angel Barrio Cardaba Head of Engineering and Technology
Engineering and Technology
• Winglets increase lift/drag ratio. Uprated engines add power in climb & cruise
• Analysis of handling qualities and performance completed May 2013 using
preliminary design
• Aircraft used for the flight trials has been the company-owned C295
development aircraft with structural reinforcements in the wings.
Summary to date
• Results have been very positive, with significant
improvement in performance
• The next phases are:
• Series solution design
• Certification (including flight trials in C295)
• Industrialization and introduction into series
design
Status
Main Characteristics
• Winglets are metallic aerostructures with composite
attachments to the wing.
• Applicable to all C-295 versions: transport, MPA, AEW…
• A maximum weight increment (payload reduction) of 90 kg is
estimated: 30 Kg due to wing reinforcements and 60 Kg due
to the two winglets (30 Kg/winglet).
• C 295Type Rating is maintained without specific training
• Fully compatible with other product improvements including
the new engine power settings
• Series aircraft solution:
• New upper panel in external and central wing (increased
thickness)
• Increased thickness in certain spars (analysis continues)
• Solution for certification trials:
• Increased thickness of upper panel only in external wing,
implemented by repair solution
Engineering solution
• Enhanced performance:
• Higher powerplant rating,
increases payload
• Increased hot and high
performance
• Already certified and offered as
customer option (independently of
winglets)
Uprated PW127 engines
• Main milestones
• Start: End May 2013.
• Design Documentation freeze: September
2013.
• Flight Trials start: January 2014.
• Certification by INTA: May 2014.
Certification
May 2013
C295 Airborne Early Warning & Command
• New flight test campaign performed with winglets fitted.
• Positive results.
May 2013
C295 Continuous Improvement
CARRIAGE AND RELEASE TRIALS
SUCCESSFULLY COMPLETED APRIL
2013.
READY TO BE OFFERED
MARTE ANTI-SHIP MISSILE
May 2013
C295 Continuous Improvement
C295 GUNNER
NEW WEAPON SYSTEMS
INTEGRATION
INSTALLATION TRADE-OFF
FOR DIFFERENT CANNONS
INSTALLATION BEING
PERFORMED:
27MM
30MM
SELECTION OF OPTIMUN
CANNON TO BE DONE 2013.
May 2013
C295 Continuous Improvement
OBIGGS: FT COMPLETED
OCT. 2012
BEING OFFERED
May 2013
NC212i
DEVELOPMENT PHASE LAUNCHED
WITH PDTI.
MAIN TECHNOLOGICAL FEATURES:
 NEW COCKPIT DISPLAYS
 NEW ADC AND AHRS
 NEW CVR, FDR AND TCAS
 NEW AUTOPILOT
 NEW INTERIOR LAY-OUT
DEVELOPMENT KEY
DATES:
PDR END MAY
CDR Q3 2013
May 2013
NC212i
COCKPIT LAY-OUT
New EFIS
New
Standby
horizon
May 2013
NC212i
INTERIOR LAY-OUT
Thunderbay Seats. 28 PAX
May 2013
Air Refuelling
In this picture everything is
real with the exception of
the aircraft
A310 MRTT FLIGHT TEST BED
 The A310 is available for Flight Test Bed for enhancements in Boom systems and
in-flight training. Is now offered for advanced boom training
BOOM INTEGRATED PROCEDURES
TRAINNER
IN-HOUSE DEVELOPMENT: SIMPLE
AND RELIABLE.
May 2013
Air Refuelling
VISION SYSTEM WIRELESS
MAINTENANCE
READY AND IN USE
ENHANCED PDL DIMMING
FUNCTION
NEW ELECTRONIC BOX
DEVELOPED BY AIRBUS
MILITARY TO IMPROVE
ORIGINAL DIMMING
FUNCTIONALITY
NEW POD LIGHT SYSTEM
INTEGRATING HOUSE
MARKINGS FUNCTION
May 2013
Technologies
Clean Sky I
Green Regional Aircraft. European project to:
• Facilitate the all-electric aircraft, reducing aircraft emissions
through lower fuel consumption
Main Achievements
• Boost maturity of technologies in electrical power generation,
distribution and usage
• New management solution to adjust the electrical sources rating
Airbus Military Activities
• Simulation Model of the Electrical Power Generation & Distribution System for the flight Demonstration
Electrical Channel
• Demo Channel Rig for validation of EPGDS Model
May 2013
Technologies
CFRP: thermoplastics,
nanotubes, integrated structures
HF integrated
antenna
PERSEUS FITS & MSC
PERSEUS (Protection of European BoRders and Seas through the IntElligent Use of
Surveillance):
CN-235 GC01 datalink capabilies enhancement.
 Platform integration in the PERSEUS network.
PROGRAM STATUS:
Development test between CN-235 GC01 and Mission Support Centre being
performed
Qualification test to be performed Q4 2013
Thank you
May 2013

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The C-295W

  • 1. May 2013 Presentado por Angel Barrio Cardaba Head of Engineering and Technology Engineering and Technology
  • 2. • Winglets increase lift/drag ratio. Uprated engines add power in climb & cruise • Analysis of handling qualities and performance completed May 2013 using preliminary design • Aircraft used for the flight trials has been the company-owned C295 development aircraft with structural reinforcements in the wings. Summary to date
  • 3. • Results have been very positive, with significant improvement in performance • The next phases are: • Series solution design • Certification (including flight trials in C295) • Industrialization and introduction into series design Status
  • 4. Main Characteristics • Winglets are metallic aerostructures with composite attachments to the wing. • Applicable to all C-295 versions: transport, MPA, AEW… • A maximum weight increment (payload reduction) of 90 kg is estimated: 30 Kg due to wing reinforcements and 60 Kg due to the two winglets (30 Kg/winglet). • C 295Type Rating is maintained without specific training • Fully compatible with other product improvements including the new engine power settings
  • 5. • Series aircraft solution: • New upper panel in external and central wing (increased thickness) • Increased thickness in certain spars (analysis continues) • Solution for certification trials: • Increased thickness of upper panel only in external wing, implemented by repair solution Engineering solution
  • 6. • Enhanced performance: • Higher powerplant rating, increases payload • Increased hot and high performance • Already certified and offered as customer option (independently of winglets) Uprated PW127 engines
  • 7. • Main milestones • Start: End May 2013. • Design Documentation freeze: September 2013. • Flight Trials start: January 2014. • Certification by INTA: May 2014. Certification
  • 8. May 2013 C295 Airborne Early Warning & Command • New flight test campaign performed with winglets fitted. • Positive results.
  • 9. May 2013 C295 Continuous Improvement CARRIAGE AND RELEASE TRIALS SUCCESSFULLY COMPLETED APRIL 2013. READY TO BE OFFERED MARTE ANTI-SHIP MISSILE
  • 10. May 2013 C295 Continuous Improvement C295 GUNNER NEW WEAPON SYSTEMS INTEGRATION INSTALLATION TRADE-OFF FOR DIFFERENT CANNONS INSTALLATION BEING PERFORMED: 27MM 30MM SELECTION OF OPTIMUN CANNON TO BE DONE 2013.
  • 11. May 2013 C295 Continuous Improvement OBIGGS: FT COMPLETED OCT. 2012 BEING OFFERED
  • 12. May 2013 NC212i DEVELOPMENT PHASE LAUNCHED WITH PDTI. MAIN TECHNOLOGICAL FEATURES:  NEW COCKPIT DISPLAYS  NEW ADC AND AHRS  NEW CVR, FDR AND TCAS  NEW AUTOPILOT  NEW INTERIOR LAY-OUT DEVELOPMENT KEY DATES: PDR END MAY CDR Q3 2013
  • 13. May 2013 NC212i COCKPIT LAY-OUT New EFIS New Standby horizon
  • 15. May 2013 Air Refuelling In this picture everything is real with the exception of the aircraft A310 MRTT FLIGHT TEST BED  The A310 is available for Flight Test Bed for enhancements in Boom systems and in-flight training. Is now offered for advanced boom training BOOM INTEGRATED PROCEDURES TRAINNER IN-HOUSE DEVELOPMENT: SIMPLE AND RELIABLE.
  • 16. May 2013 Air Refuelling VISION SYSTEM WIRELESS MAINTENANCE READY AND IN USE ENHANCED PDL DIMMING FUNCTION NEW ELECTRONIC BOX DEVELOPED BY AIRBUS MILITARY TO IMPROVE ORIGINAL DIMMING FUNCTIONALITY NEW POD LIGHT SYSTEM INTEGRATING HOUSE MARKINGS FUNCTION
  • 17. May 2013 Technologies Clean Sky I Green Regional Aircraft. European project to: • Facilitate the all-electric aircraft, reducing aircraft emissions through lower fuel consumption Main Achievements • Boost maturity of technologies in electrical power generation, distribution and usage • New management solution to adjust the electrical sources rating Airbus Military Activities • Simulation Model of the Electrical Power Generation & Distribution System for the flight Demonstration Electrical Channel • Demo Channel Rig for validation of EPGDS Model
  • 18. May 2013 Technologies CFRP: thermoplastics, nanotubes, integrated structures HF integrated antenna PERSEUS FITS & MSC PERSEUS (Protection of European BoRders and Seas through the IntElligent Use of Surveillance): CN-235 GC01 datalink capabilies enhancement.  Platform integration in the PERSEUS network. PROGRAM STATUS: Development test between CN-235 GC01 and Mission Support Centre being performed Qualification test to be performed Q4 2013