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L’A380 pour Air France

L’A380 pour Air France. A3XX / A3XX-F 79.8 m 73 m 24.1 m. SPAN LENGTH HEIGHT. A3XX dimensions. Caractéristiques de l’A380. A380. Capacité passager. 555/559*. Capacité fret. 38 LD3s or 13 palettes 18 LD3s* and 5 palettes*. Rayon d’action (max pax). 8,000 nm / 6700 nm*. MDTOW.

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L’A380 pour Air France

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  1. L’A380 pour Air France

  2. A3XX / A3XX-F 79.8 m 73 m 24.1 m SPAN LENGTH HEIGHT A3XX dimensions

  3. Caractéristiques de l’A380 A380 Capacité passager 555/559* Capacité fret 38 LD3s or 13 palettes 18 LD3s* and 5 palettes* Rayon d’action (max pax) 8,000 nm / 6700 nm* MDTOW 560 t MLW 386 t 361 t MZFW OWE (masse de base) 277 t / 293.1 t * 84 t / 67.9 t * Charge marchande 310 000 l Capacité carburant Poussée moteur (slst) 302 kN * Configuration Air France

  4. Rayon d’action autour de Paris A380/GP7200 Rayon d’action avec charge marchande maximale passager (559pax) 548t/560t: 6398nm/6731nm Vents les plus défavorables- probabilité annuelle de 85% ISA Marge de 3% sur le rayon d’action

  5. L’ économie de l’ avion Ref :747-400, 416 sièges, Prix catalogue : 180 m$ 2000 Coût direct d'opération/siège* Coût carburant /siège* Prix/siège -10% -13.5% -15% A380-800, 555 sièges, Prix catalogue: 216 m$ 2000 L’A380 : un avion économiquement attractif *Comparaison basée sur un secteur de 6000 nm - coûts d ’opération standards Airbus

  6. A380 A340 A320 Nose Fuselage Dimensions

  7. Plus grand dedans 233’’ Fuselage large 160’’ 241’’ 259’’ Fuselage large L’A380 : capacité et espace • Plus grand dehors 747-400 • +35 % de capacité supplémentaire • 2 cabines distinctes (ponts principal et supérieur) Un confort et flexibilité grâce à deux très larges cabines

  8. De 4 à 9 de front DU CONFORT POUR LE PASSAGER De 4 à 11 de front Poste de repos et toilettes en soutes optionnels Palettes 2 palettes LD3s et/ou palettes La réponse A380 … ET DE LA CAPACITE CARGO

  9. Configuration A380 Air France :559 sièges Pont supérieur 78J, pas 48” 135 Y, pas 31” Pont principal 16 P, pas 82” 330 Y, pas 31”

  10. Les prochaines étapes du programme Gel de la Configuration Autorisation commerciale Clients de lancement Définition terminée Premier vol Mise en service Jan. 99 Durant 2000 Fin 2001 Mi 2004 Début 2006 Mi 2000

  11. Principales innovations • 2 Packs ( BP et HP ) • PA intégré au CDV • Génération électrique : fréquence variable. • CDV : concept EHA et EBHA • Fuel : optimisation du CG de l’ avion lors du remplissage. • Hydraulique : 5000 Psi. • LDG : 22 roues / aide au management de configuration. • Oxygéne : Systéme OBOGS ? • OIS / OMS : avion communicant / informations embarquées….. • Station de maintenance : face au pylone + possibilité d’ interrogation à distance par terminaux sans fil. • Structures : CFRP / Glare • Portes : électriques • Moteurs : surveillance enrichie ( analyse des gaz en sortie ….. )

  12. 8 identical potentially interactive displays 2 multi-functions keyboards 2 multi-functions Cursor Control Devices Control and Display System

  13. Maintenance station

  14. To be examined in the mock-up

  15. Same ladder in different positions Rear Fuselage

  16. Conventional Technology Advanced Technology BPV BPV FCV1 FCV RHX RDA ACM RDA HP - ACM RHX RDA FCV2 LP - ACM BPV FCV RHX RDA ACM BPV FCV1 RDA HP - ACM BPV RHX RDA FCV2 FCV RHX RDA ACM LP - ACM No. of Components 3 3 3 3+3* 4 2 4 4+2* *for HX-mode Air Generation pack concept - redundancy Components: FCV: Flow Control Valve RHX: Ram Heat Exchanger RDA: Ram Door Actuator BPV: Bypass Valve ACM: Air Cycle Machine Conventional: Most single failures result in loss of complete pack. Advanced: No cooling degradation due to most single failures.

  17. Variable frequency network • Objectives : • Significant improvement of the ATA24 DMC and operational reliability • Reduction of the aircraft systems DMC • Re-open industrial competition Suppliers involved • TRW-LUCAS : 120 KVA variable frequency generator on test. • HONEYWELL-ALLIED : 150 kVA generator in lab. in Feb 2001 • HAMILTON SUNDSTRAND: 150 kVA gen. in lab. in Feb 2001 Network characterization under process with EUROCAE and RTCA (DO160 update) 115 V AC network confirmed

  18. 4x150kVA VFG Engine 1 Engine 2 Engine 3 Engine 4 APU 2x120kVA CF gen Ext 4>> Ext 3>> AC3 AC4 <<Ext 2 <<Ext 1 AC1 AC2 Galley3 Galley4 Galley1 Galley 2 4x90kVA ext. connections AC network general architecture

  19. Inner Engine Feed Tank Outer Transfer Tank Vent Tanks Fuel System Fuel system provides • Protection of fuel volume following engine rotor failure (FAR 25.903(d)(1)) • Provision of wing bending relief and CG management • Embodiment of TWA800 accident recommendations Aft Center Tank Inner Transfer Tank Aft center tank- 42 400 litres (-800 R and -900 only) Inner feed Tank - 28500 litres Inner Transfer Tank - 84400 litres Outer Eng Feed Tank - 28400 litres Outer Transfer Tank - 10600 litres Trim tank - 24 000 litres • Gauging technology under evaluation • Refueling procedure under • review with the airlines Outer Engine Feed Tank Trim Tank

  20. Trade-off study (PDR) Hydraulic fluid analysis Initial actions • System weight : - 1200 kg • Feasibility confirmed • Technical risk on • Hydraulic system reduced Increased hydraulic pressure 5000 psi Kick-off (1998) : current experience potential show stoppers criteria for trade-off action list Review with the airlines - system workshop 26/28 Oct 1999 Final decision : 8 November 1999 + follow-up actions Airline questionnaire 2 Hyd. benches for endurance Definition of standards Additional benches in suppliers

  21. Gen APU Gen Gen Isolation Gen Gen Gen Gen Eng. 2 Eng. 1 Eng. 3 Eng. 4 RAT EDP EDP EDP EDP Gen EDP EDP EDP EDP EMP EMP T/R Eng. 2 T/R Eng. 3 T/R Ailerons L & R o/b & m/b L & R i/b L & R o/b L & R i/b & o/b Spoilers 6 (L & R) 4 (L & R) 1, 3, 5, 7 (L &R) 2, 4, 6, 8 (L&R) Rudder Upper & Lower Upper & Lower Upper & Lower Upper & Lower Elevators LOB & ROB LIB & RIB LOB & ROB LIB & RIB THS Pitch trim 1 Pitch trim Pitch trim 2 PMV PMV Slats/Flaps Slats Slats Flaps PMF Flaps PMF Braking Alt. Ener Body Gear Brakes Alt. Ener Wing Gear Brakes PV PV Steering Nose Body Gears Alt. Ener Gear actuation Nose & Wing Body Gears Green System Electric System 1 Electric System 2 Yellow System 2H/2E Architecture Schematic

  22. Nose gear & fuselage studies STATUS 14 STATUS 11 Frame 11 Frame 12 Frame 10 150 100

  23. Main Gear Group • 4 post main gear group for 560 & 590 t • 4 wheel Wing gear • 6 wheel Body gear • 5 post main gear group for growth 560t & 590t MTOW • bay gives extra cargo volume • with good central fuselage structure • compatible with pavement loading • (being demonstrated by PEP) growth

  24. Ethernet network AFDX Ethernet Network TACS : cameras, video switches HFDR, VDR, SATCOM CVR, DFDR SELCAL, RAMP, AMU... ACR SCI fuel&LG APU GCU LRU Cabin Intercom Data -CIDS Smoke detect. Water/waste ctl Air Gener. Temp ctl Bleed mon. Overheat detect. Cabin Pressure Ventil. Ctl Avioncs cooling Air Gene- Cabin . ration / Pressure / . . Temp Ventalation . . . . Contr . Contr . . Avionics for A380 FCGC FCSC SFCC Engines Flight control FADEC AFDX network DME ADIRU MMR VOR AWLU OMT Radio comm. Ethernet network Sensors Recorders Ctrl & Displays R/A WACS cockpit NCR SATCOM std by LEO/MEO ACMF FDIF IOM FW Surveillance FM ATC FCDC Cockpit ACAS, TAWS, W/R Avionics server energy connectors ELM IRDC LG LG LG ECM WHC PHC GCU FQI/ FQI/ BC BC CBM HSyM SC SC FuM FuM TP TP Utilities . . . Cabin server IFE Cabin

  25. On Board Information Gate Link Passenger Terminals Crew Station IFE FS Router VHF Flight Deck Info Cabin Services Maintenance Apps IFE • Charts and Maps • Weather • Electronic Library • Electronic log book • Passenger Manifest • Consumables Tracking • Financial Transactions • Cabin Logbook, Checklist • FMS Nav Data Base • Operational S/W Loading • Fault Correction Guide • Quick Access Recorder • Direct TV • Internet

  26. Terminals Cockpit, cabin, Portable Onboard Information Network Consultation Aircraft Condition Monitoring Data Loading Centralized Maintenance Link Maintenance Electronic documentation Acquisition and processing Fault acquisition Tests activation S/W and data bases loading A/C Systems and engines Ops. data BITE A3XX Onboard Maintenance System concept Uplink Downlink Control, reporting display, customisation programming Recording Printing

  27. A3XX Scenario for Advanced Materials Upper Floor Beams: CFRP for Pax version, Aluminium for freighter version Upper Fuselage Panels: Fibre Laminates (GLARE) Empennage: CFRP Outer Wing: Metal bonded Rear Pressure Bulkhead: CFRP Wing Panels: Advanced aluminium alloys Center Wing Box: CFRP Fixed Wing Leading Edge: Thermoplastic J-Nose Lower Fuselage Panels: Laser Beam Welded aluminium alloys

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