Kỹ Thuật - Công Nghệ - Kỹ thuật - Kỹ thuật June 2008 Presented by Andy Hebborn Airbus, UK Head of Landing Gear Systems A380 Landing Gear and Systems HAW Hamburg 5th June 2008 Lecture for RAeS, DGLR, VDI and HAW Hamburg Download from: http:AeroLectures.de June 2008DGLR Hamburg Page 2 AIRBUS UK LTD. All rights reserved. Confidential and proprietary document. A380 Landing Gear Systems – An Overview Introduction Description of Landing Gears and Associated Systems – Development of Gears Layout – Highlight new functions and technologies – Overview of Systems Architectures and Equipment June 2008DGLR Hamburg Page 3 AIRBUS UK LTD. All rights reserved. Confidential and proprietary document. The A380 The A380 is a completely new, very high capacity, very long rang e commercial transport aircraft, powered by 4 RR Trent 900 or Engine Alliance GP7200 engines Standard A380-800 accommodates 555 Passengers in three - class long-range arrangement MTOW 569 tonnes, MLW 391 tonnes First flight 27 April 2005 Entry into service Oct 2007, with Singapore Airlines Delivery schedule for 2008: 13 AC to Singapore, Qantas and Emirates A380 Landing Gear Systems – An Overview The Aircraft June 2008DGLR Hamburg Page 4 AIRBUS UK LTD. All rights reserved. Confidential and proprietary document. A380 Landing Gear Systems – An Overview Major Components and Systems 4ATA Chapter 32 Landing Gear Systems 4 Gears – Nose Landing Gear (2 Wheels) – Body Landing Gear x2 (Bogie Type, 6 Wheels - 4 Braked) – Wing Landing Gear x2 (Bogie Type, 4 Wheels - 4 Braked) 4ExtensionRetraction System 4Braking Control System 4Steering Control System – Nose Wheel Steering – Body Wheel Steering 4Wheels, Tyres and Brakes (16 Braked Wheels) 4Monitoring Systems – Tyre Pressure Indication System – Brake Temperature Monitoring System – Oleo Pressure Monitoring System June 2008DGLR Hamburg Page 5 AIRBUS UK LTD. All rights reserved. Confidential and proprietary document. A380 Landing Gear Configuration Starting Point – 38 Alternatives A380 Landing Gear Systems – An Overview Evolution of Main Landing Gear Configuration June 2008DGLR Hamburg Page 6 AIRBUS UK LTD. All rights reserved. Confidential and proprietary document. Classical Bay First Down Selection: 2 Family Concepts for the gear and airframe Longitudinal Bay A380 Landing Gear Systems – An Overview Evolution of Main Landing Gear Configuration June 2008DGLR Hamburg Page 7 AIRBUS UK LTD. All rights reserved. Confidential and proprietary document. A380 Landing Gear Systems – An Overview Evolution of Main Landing Gear Configuration Baseline configuration Second Down Selection: - Family Concept Selected - Kinematic Options traded Kinematic options Bay concept selected June 2008DGLR Hamburg Page 8 AIRBUS UK LTD. All rights reserved. Confidential and proprietary document. Main Gear Group: Installation in Wing Fuselage A380 Landing Gear Systems – An Overview Evolution of Main Landing Gear Configuration June 2008DGLR Hamburg Page 9 AIRBUS UK LTD. All rights reserved. Confidential and proprietary document. Landing gear A380 Landing Gear Systems – An Overview Evolution of Gears Configuration Manoeuvring on ICAO code E and FAA group V airports 4 45m wide runways and 23m taxiways 4 U-turn on 60m wide runway possible 4 one concept philosophy for all aircraft variants 4 each variant capable of optimization 4 concept capable of development to significantly higher design weights 4 ACNs no worse than existing large aircraft 4 Nose gear to be compatible with towbarless towing Capable of growth beyond current ac definitions 4 2 wheel or 4 wheel CLG installation possible Landing Gear Configuration – Basic Requirements June 2008DGLR Hamburg Page 10 AIRBUS UK LTD. All rights reserved. Confidential and proprietary document. Wing Rear Spar (Ref) Gear Rib 9 Fitting Sidestay Assy Sidestay Fitting Fwd Pintle Fitting Retract Actuator (Ref) Locklinks Cardan Pin FORWARD OUTBOARD Main Fitting BTA Fuse Aft Pintle Pin Retract Actuator Cardan Pin VIEW LOOKING INBOARD ON PINTLE AXIS VIEW LOOKING FORWARD ON WLG SPAR PLANE Bogie Trim Actuator (BTA) Unlock Actuator (with third Downlockspring) Downlock Springs VIEW RETRACTED Lower Sidestay Lock Links TorqueLinks Slave Links Bogie Beam Assy Brake Rods SlidingPiston Drag Brace Fwd Pintle Pin Ground Locking Pin Main Fitting Retract Actuator Fuse Pin Lower Cardan Pin Upper Cardan Pin Upper Sidestay Bogie Trim Actuator Hydraulic Dressings Normal Brake System Alternate Brake System Downlock Hoses Retract Actuator Hoses Brake Hoses FWD Uplock Roller A380 Landing Gear Systems – An Overview Wing Landing Gear June 2008DGLR Hamburg Page 11 AIRBUS UK LTD. All rights reserved. Confidential and proprietary document. Upper Drag Brace Lower Panel Retract Actuator Bogie Trim Actuator (BTA) Outer Cylinder Sliding Piston Ground Locking Pin Fuse Pin Lower Drag Brace TorqueLinks Brake Rods Slave Links Upper Panel Lower Panel Uplock Roller Lock Links Bogie Beam Assy Upper Drag Brace Normal Brake System Alternate Brake System Steering System Lock Springs Normal Brake Manifold Alternate Brake Manifold SteeredAxle VIEW RETRACTED LH BLG VIEW LOOKING AFT LH BLG VIEW LOOKING INBOARD FWD UnlockActuator Knuckle Joint Link UPLOCK FITTING ‘A’ FITTING ‘H’ FITTING FR 63 ‘J’ FITTING ‘C’ FITTING ‘G1’ FITTING ‘G2’ FITTING STEERED AXLE DETAIL Steering Unlocked Steering Locked Steering Actuator and Steering Hydraulic Control Block Steering Unlock Actuator Steering Lock Springs Steering Wedge Lock A380 Landing Gear Systems – An Overview Body Landing Gear June 2008DGLR Hamburg Page 12 AIRBUS UK LTD. All rights reserved. Confidential and proprietary document. ‘Push-to-retract’ gear actuator Single stage oleo Steering Disconnect Panel HVOF-coated slider Maintenance Panel on Leg A380 Landing Gear Systems – An Overview Nose Landing Gear 6070° 6070°FWD Nose Wheel Steering (NWS): Towing Angle is +- 60° Hydraulic Steering Angle is +- 70° Mechanical Stop Angle is +- 75° J u n e 2 0 0 8D G L R H a m b ur g P a g e 1 3 AI R B U S U K L T D. All ri g ht s r e s er v e d. C o nfi d e nti al a n d pr o pri et ar y d o c u m e nt. Hi g h S t r e n g t h S t e el ( 3 0 0 M), e x c e p t: - Ti t a ni u m Al u mi ni u m W ei g ht C o st Si z e Ti m e s c al e Tr a d e -off s A 3 8 0 L a n di n g G e ar S y st e m s – A n O v er vi e w L a n di n g G e ar Str u ct ur e June 2008DGLR Hamburg Page 14 AIRBUS UK LTD. All rights reserved. Confidential and proprietary document. A380 Landing Gear Systems – An Overview Gears Retraction Animation June 2008DGLR Hamburg Page 15 AIRBUS UK LTD. All rights reserved. Confidential and proprietary document. Honeywell Wheel Brake: Braked Wheel Deep Cavity A-Frame 2014-T6 Aluminium Alloy 23 inch rim size 11 Vent Holes 11 Drive keys 22 Iconel Tie Bolts Segmented Heat-shield Stainless Steel Axle Sleeve Non-Braked Wheel Symmetric A-Frame Brake 5 Rotor Carbenix 4000 heat-sink 1.59inch wear pin 23 spline titanium torque tube Aluminium 7050 piston housing 6 x Ø1.805” pistons (split-ball adjuster) Integral Lug and steel torque pin Bridgestone Tyre 1400x530 R23 40PR Lightweight Radial A380 Landing Gear Systems – An Overview Main Wheel, Tyre and Brake June 2008DGLR Hamburg Page 16 AIRBUS UK LTD. All rights reserved. Confidential and proprietary document. Honeywell Wheel Wheel Symmetric A-Frame 2014-T6 Aluminium Alloy 22 inch rim size Iconel Tie Bolts Light-weight Aluminium Axle Sleeve Bridgestone Tyre 1270x455 R22 32PR Lightweight Radial A380 Landing Gear Systems – An Overview Nose Wheel and Tyre June 2008DGLR Hamburg Page 17 AIRBUS UK LTD. All rights reserved. Confidential and proprietary document. A380 Landing Gear Systems – An Overview Power Systems Architecture Hydraulic architecture : 45000 psi 42 AC circuit (Green Yellow) 4Segregation Between Green and Yellow : – BLGs ATA32 function on Yellow circuit only – WLGs NLG ATA32 function on Green circuit only 4 All hydraulic back-up functions ensured by local hydraulic generation system (LEHGS) owned by the function system Electrical Architecture : 4AC : 115V Variable frequency 4DC: 28V with no power transients 2 segregated Normal DC : DC1 DC2 1 Emergency DC : DC essential 1 DC Service Bus June 2008DGLR Hamburg Page 18 AIRBUS UK LTD. All rights reserved. Confidential and proprietary document. Redundancy of hydraulic power for Braking and Nose Wheel Steering provided by LEHGS Features: 4 Re-pressurises the HP accumulators to 350 bar throughout the flight 4 Low pressure reservoir with LVDT for level sensing and visual indicator 4Electric motor-pump 4 Incorporates health monitoring (fluid and motor temperature sensing, filter clog detection) A380 Landing Gear Systems – An Overview Local Hydraulic Power Generation System June 2008DGLR Hamburg Page 19 AIRBUS UK LTD. All rights reserved. Confidential and proprietary document. 1) Normal ATA32 functions controlled by shared avionics units for a ll systems 4 Core Processor Input Output Module (Integrated Modular Avionics) CPIOM-G (IMA): All ATA32 System functions – Control functions and indication management – Central monitoring functions (BITE) – Main interfaces to other AC systems 4 Remote Data Concentrator Landing Gear RDCs : ExtensionRetraction (LGERS) and Monitoring (LGMS) – Specific Systems sensors Acquisitions – ExtRet Valves and Actuators second order control – Local monitoring Iinterface RDCs : Braking and Steering (BSCS) – ASKID and pressure control loop function – Specific Systems sensors Acquisitions – Local monitoring 2) Emergency ATA32 functions controlled by specific analogue units, independent of IMA and AFDX avionics technology 4 Brake Control : Emergency Brake Control (EBCU) 4 ExtRet Free Fall : Free-Fall Control (FFCM) A380 Landing Gear Systems – An Overview System Avionics Architecture June 2008DGLR Hamburg Page 21 AIRBUS UK LTD. All rights reserved. Confidential and proprietary document. Oleo pressure is monitored simultaneously on all landing gear shock absorbers and any warning is passed on to the Flight Warning System. Prevents departure with mis-serviced Landing Gear Accurate Check - performed once per flight, after gear extension Gross Check - continuous monitoring Combined Pressure and Temperature sensor mounted on each Shock Absorber OPMS is designed to: Pr...
June 2008 Presented by Andy Hebborn Airbus, UK Head of Landing Gear Systems A380 Landing Gear and Systems HAW Hamburg 5th June 2008 Lecture for RAeS, DGLR, VDI and HAW Hamburg Download from: http://AeroLectures.de A380 Landing Gear & Systems – An Overview Introduction © AIRBUS UK LTD All rights reserved Confidential and proprietary document Description of Landing Gears and Associated Systems – Development of Gears Layout – Highlight new functions and technologies – Overview of Systems Architectures and Equipment DGLR Hamburg June 2008 Page 2 © AIRBUS UK LTD All rights reserved Confidential and proprietary document A380 Landing Gear & Systems – An Overview The Aircraft The A380 • The A380 is a completely new, very high capacity, very long rang e commercial transport aircraft, powered by 4 RR Trent 900 or Engine Alliance GP7200 engines • Standard A380-800 accommodates 555 Passengers in three- class long-range arrangement • MTOW 569 tonnes, MLW 391 tonnes • First flight 27 April 2005 • Entry into service Oct 2007, with Singapore Airlines • Delivery schedule for 2008: 13 A/C to Singapore, Qantas and Emirates DGLR Hamburg June 2008 Page 3 © AIRBUS UK LTD All rights reserved Confidential and proprietary document A380 Landing Gear Systems – An Overview Major Components and Systems ATA Chapter 32 Landing Gear Systems Gears – Nose Landing Gear (2 Wheels) – Body Landing Gear x2 (Bogie Type, 6 Wheels - 4 Braked) – Wing Landing Gear x2 (Bogie Type, 4 Wheels - 4 Braked) Extension/Retraction System Braking Control System Steering Control System – Nose Wheel Steering – Body Wheel Steering Wheels, Tyres and Brakes (16 Braked Wheels) Monitoring Systems – Tyre Pressure Indication System – Brake Temperature Monitoring System – Oleo Pressure Monitoring System DGLR Hamburg June 2008 Page 4 A380 Landing Gear & Systems – An Overview Evolution of Main Landing Gear Configuration © AIRBUS UK LTD All rights reserved Confidential and proprietary document A380 Landing Gear Configuration June 2008 Page 5 Starting Point – 38 Alternatives DGLR Hamburg A380 Landing Gear & Systems – An Overview Evolution of Main Landing Gear Configuration First Down Selection: 2 Family Concepts for the gear and airframe Longitudinal Bay © AIRBUS UK LTD All rights reserved Confidential and proprietary document Classical Bay DGLR Hamburg June 2008 Page 6 © AIRBUS UK LTD All rights reserved Confidential and proprietary document A380 Landing Gear & Systems – An Overview Evolution of Main Landing Gear Configuration Second Down Selection: - Family Concept Selected - Kinematic Options traded Kinematic options Bay concept selected Baseline configuration DGLR Hamburg June 2008 Page 7 A380 Landing Gear & Systems – An Overview Evolution of Main Landing Gear Configuration © AIRBUS UK LTD All rights reserved Confidential and proprietary document Main Gear Group: Installation in Wing & Fuselage DGLR Hamburg June 2008 Page 8 © AIRBUS UK LTD All rights reserved Confidential and proprietary document A380 Landing Gear Systems – An Overview ELvaonludtiionngofgGeeaarrs Configuration • Landing Gear Configuration – Basic Requirements one concept philosophy for all aircraft variants each variant capable of optimization concept capable of development to significantly higher design weights ACNs no worse than existing large aircraft Nose gear to be compatible with towbarless towing • Manoeuvring on ICAO code E and FAA group V airports 45m wide runways and 23m taxiways U-turn on 60m wide runway possible • Capable of growth beyond current a/c definitions 2 wheel or 4 wheel CLG installation possible DGLR Hamburg June 2008 Page 9 A380 Landing Gear Systems – An Overview Wing Landing Gear Fwd Pintle Retract Actuator Retract Actuator Uplock Roller Pin Cardan Pin Hoses Drag Brace Aft Pintle Pin Downlock Hoses Retract Actuator Lock Links Upper Sidestay Upper Cardan Pin VIEW RETRACTED Unlock Actuator (with Ground Locking Fwd Pintle third Downlockspring) Lower SidestaPy in Fitting Normal Brake System Downlock Springs Sliding Piston Fuse Pin Slave Links Bogie Trim Actuator Main Fitting Lower Cardan Hydraulic Dressings Alternate Brake Pin Bogie Trim Actuator System (BTA) Gear Torque Links Rib 9 Fitting © AIRBUS UK LTD All rights reserved Confidential and proprietary document BTA Fuse Brake Hoses Retract Actuator Cardan (Ref) VIEW LOOKING FORWARD PinSidestay ON WLG SPAR PLANE Main Fitting Fitting Bogie Beam Sidestay Assy Wing Rear Spar (Ref) Assy FWD Brake Rods VIEW LOOKING INBOARD ON PINTLE AXIS Locklinks OUTBOARD FORWARD DGLR Hamburg June 2008 Page 10