airbu

Transcription

airbu
14th March 2007
Presented by:
Presented by
Frank L. Johnson
Manager Maintenance Training
Name
Thierry HARQUIN
JobTitle
Systems senior manager
Engineering
A350 Technology
Aviation Technical Education Council
Orlando, Florida 21 April 2009
Contents
Paradox of training
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document.
Programe
Product
Conclusion
(ATEC) 21 APRIL 2009 ORLANDO, FLORIDA
Contents
Paradox of training
© AIRBUS S.A.S. All rights rese
erved. Confidential and proprietary d
document.
Programe
Product
Conclusion
(ATEC) 21 APRIL 2009 ORLANDO, FLORIDA
Paradox of Training
The Paradox
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Labor in different Generations
Labor in different Generations
Cold War Generation
Generation “Y” (1977-1997)
(1940
(1940-1960)
1960)
iGeneration (1985-1995)
(ATEC) 21 APRIL 2009 ORLANDO, FLORIDA
Paradox of Training
The Paradox
M
Manual labor in a digital world
l l b i di i l
ld
Generation “Y” 1977
1977-1997
1997
Cold War Generation
iGeneration (1985-1995)
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(1940-1960)
(1940 1960)
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Paradox of Training
• iGeneration
Linked to digital technology
Digitization, virtualization, automation © AIRBUS S.A.S. All rights rese
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Old way of training not enough
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Paradox of Training
Benefits:
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Elevate participation
Increase enjoyment
Immediate understanding
(ATEC) 21 APRIL 2009 ORLANDO, FLORIDA
Paradox of Training
• Example – Information Management Systems
eLogbook
OMS
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document.
Pilot and maintenance
actions reports
Instant notification of
fault & warning messages
+ ACMS Reports
AIRMAN
Airline’s
Ai
li ’
Maintenance
Information System
ACMS:
Aircraft Condition Monitoring System
AirN@v
TSM, AMM consultation …
(ATEC) 21 APRIL 2009 ORLANDO, FLORIDA
Mr. / Ms. iGen
Contents
Paradox of training
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erved. Confidential and proprietary d
document.
Programe
Product
Conclusion
(ATEC) 21 APRIL 2009 ORLANDO, FLORIDA
A350
a wide ranging family
Capacity
- Seats
S t
A350-1000
A350
1000 MTOW 295t Thrust 95klb
350
A350-900
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300
MTOW 265t Thrust 87klb
Plus…..
Pl
A freighter variant
Ultra-long-range variant
A350-800
MTOW 245t Thrust 75klb
250
8000nm
Range
A superior family with no compromise on range
(ATEC) 21 APRIL 2009 ORLANDO, FLORIDA
Contents
P d off training
Paradox
t i i
Programe
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erved. Confidential and proprietary d
document.
Product
Cabin
Wing
Fuselage
g
Flight deck
Systems
Conclusion
(ATEC) 21 APRIL 2009 ORLANDO, FLORIDA
A350 XWB - Wing Design
64m wingspan
g p
(ICAO Category E)
442m2 wing area / All Models
35° Leading edge sweep angle
35
CFRP structure
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M 0.85 cruise speed
Advanced high lift devices
Structural adaptation per variant
(ATEC) 21 APRIL 2009 ORLANDO, FLORIDA
A350 XWB Wing Design – high lift
Advanced Dropped
Hinge Flaps
2 Inboard Droop
Nose Devices
Low Speed
Efficiency
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6 Spoilers
2 Outboard Ailerons
6 Outboard slats
Simple high-lift system
(ATEC) 21 APRIL 2009 ORLANDO, FLORIDA
erved. Confidential and proprietary d
document.
© AIRBUS S.A.S. All rights rese
Cockpit and Avionics
Advanced cockpit based on A380 design
(ATEC) 21 APRIL 2009 ORLANDO, FLORIDA
Trade Off Study with 6 Large Displays
Advantages:
erved. Confidential and proprietary d
document.
© AIRBUS S.A.S. All rights rese
OIS
PFD
ND
SFLM
VD
MB
SD
WD
MFD
MFD
New Cockpit concept
(ATEC) 21 APRIL 2009 ORLANDO, FLORIDA
• Similarity with A380 functions repartition
ED
• IntegrationND
of OIS: PFD
15’’ display on central and
OIS
external display units
VDreconfigurations
SFLM
• More flexible
since 6
identical displays
Continuous Innovation while keeping Airbus
Cockpit Philosophy
HUD provision
ATSAW
AP TCAS
Check
C
ec lists
ss
Acute
New RMP
ISIS
Mailbox
Vertical display
MFD
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OIT
Brake To Vacate
Screen interactivity
OANS
Items specific to A380/A350
(ATEC) 21 APRIL 2009 ORLANDO, FLORIDA
New Functionalities
Onboard Airport Navigation System
N i ti around
Navigating
d complex
l airports
i
t
Aircraft Traffic Situational Awareness (ATSAW)
AAL1255
+30 ↓
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In trail procedures
Enhanced visual separation in approach
Enhanced situational awareness on the airport surface
Brake To Vacate (BTV)
Minimize runway occupancy
Autopilot
p
TCAS ((APTCAS))
participates in increasing safety
level in TCAS operations
(ATEC) 21 APRIL 2009 ORLANDO, FLORIDA
OANS with BTV
HMI screenshot
example
Integrated Modular Avionics (IMA)
ARINC 429
AFDX
LRU6
•
•
•
•
LRUx
LRU1
AFDX Switch
•
•
•
•
LRU5
IOM
document.
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LRM
LRU2
CPIOM
(module)
LRU4
LRU3
CPIOM
Fewer connections, easier Maintenance & T/S
/S
Higher re-configuration flexibility
(ATEC) 21 APRIL 2009 ORLANDO, FLORIDA
IOM
Systems Highlights
2 hydraulic/ 2 electric (2H/2E) flight control architecture
Proven in A380 flight-test
g
– Weight, Maintenance, Reliability, Redundancy
Electro-Pneumatic bleed system
More efficient at aircraft level
3 tank fuel system with inerting system
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Simplified architecture.
architecture No trim tank
4 Variable frequency electrical generation system
Significant maintenance cost reduction
Interactive Cockpit with modular server systems
Enhanced functionalities
Simple single stage oleo landing gears
Secured reduced maintenance cost
(ATEC) 21 APRIL 2009 ORLANDO, FLORIDA
Hydraulics & Flight Controls
2 Hydraulics
y
- 2 Electrics architecture
erved. Confidential and proprietary d
document.
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Electrically powered Electro-Hydrostatic Actuators (EHA)
Electrically and Hydraulically powered Electrical Back-up
Hydraulic Actuators (EBHA)
Electrical motor for SLAT Power Control Unit
Electrical Wing Tip Brakes
A380 aileron
‘More Electric’ architecture and lower maintenance cost
(ATEC) 21 APRIL 2009 ORLANDO, FLORIDA
Fuel System
Key:
y
Engine Feed
Transfer
XFEED
document.
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L
R
Simple 3 tank configuration
Simple system architecture
Based on proven Airbus experience
(ATEC) 21 APRIL 2009 ORLANDO, FLORIDA
Electrical Systems
4 Generators : 150kVA each
Variable Frequency (VF)
230V
lighter + more efficient
ETOPS 350 min and beyond
Dispatch with 1 GEN inop
A380
technology
Smaller & lighter than IDG
Gen4
Gen2
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APU
Gen
Main power centers
Position either Front or Central
More power after Engine loss
System Segregation
Weight saving
(ATEC) 21 APRIL 2009 ORLANDO, FLORIDA
Gen3
Gen1
RAT
1 APU Generators : 150 Kva
Electric RAT
Landing Gear
Extensive use of Titanium - Corosion
Single stage oleo
Improved Seal design
Aft Pintle
pin
No rocking bogie
Gear Beam
Fwd Pintle
pin
Inner Rear Spar
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No shortening mechanism
14 year hard maintenance target
Aft Side-Stay
Side Stay
Fwd Side-Stay
FORWARD
Simple architecture
Improved reliability
(ATEC) 21 APRIL 2009 ORLANDO, FLORIDA
4 wheel
h lb
bogie
i A350
A350-800/900
800/900
6 wheel bogie A350-900R /1000
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document.
Contents
Programme
Product
Conclusion
(ATEC) 21 APRIL 2009 ORLANDO, FLORIDA
A350
– taking the lead
A totally new design
new cabin,
cabin new wing
wing, new materials
materials, new systems
systems, new engines
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Excellent performance
Most efficient economics
A new long-range family
For the Xtra experience
(ATEC) 21 APRIL 2009 ORLANDO, FLORIDA