Boeing 787 System and Performance - Configurations
- 1. BOEING is a trademark of Boeing Management Company. Copyright © 2005 Boeing. All rights reserved. 787 Systems and Performance 787 Systems and Performance Tim Nelson Flight Operations Engineering Boeing Commercial Airplanes Tim Nelson Flight Operations Engineering Boeing Commercial Airplanes
- 2. NELSON.2 Copyright © 2005 Boeing. All rights reserved. Configured for Success Configured for Success Composite primary structure Advanced engines and nacelles Breakthrough passenger cabin Enhanced flight deck Advanced wing design Innovative systems technologies Large cargo capacity Overhead crew rests 787-8 Design Features 787-8 Design Features Copyright © 2005 Boeing. All rights reserved.
- 3. NELSON.3 Copyright © 2005 Boeing. All rights reserved. The 787 Is a Complete, Flexible, Efficient Family The 787 Is a Complete, Flexible, Efficient Family 787-8 223 passengers (three-class) 8,500 nmi / 15,700 km 787-8 223 passengers (three-class) 8,500 nmi / 15,700 km 787-9 259 passengers (three-class) 8,300 nmi / 15,400 km 787-9 259 passengers (three-class) 8,300 nmi / 15,400 km 787-3 296 passengers (two-class) 3,500 nmi / 6,500km 787-3 296 passengers (two-class) 3,500 nmi / 6,500km
- 4. NELSON.4 Copyright © 2005 Boeing. All rights reserved. Efficiency for Medium — and Long-Haul Markets Efficiency for Medium — and Long-Haul Markets 767-200ER 767-300ER 767-400ER 777-300 777-200ER 777-200LR 777-300ER Tri-Class Long Range Rules Tri-Class Long Range Rules Dual-Class Short Medium Range Rules Dual-Class Short Medium Range Rules 787-8 787-9 747-400 767-300 787-3 747-400ER Design range, nmi Design range, nmi Seats Seats 150 150 200 200 250 250 300 300 350 350 400 400 450 450 3000 3000 4000 4000 5000 5000 6000 6000 7000 7000 8000 8000 9000 9000 10000 10000
- 5. NELSON.5 Copyright © 2005 Boeing. All rights reserved. Creating New Non-Stop Routes Creating New Non-Stop Routes The 787 can connect more than 450 new airport pairs Possible New Airport Pairs Possible New Airport Pairs The 787 can efficiently connect more than 450 new city pairs Vancouver - Sao Paulo Seattle - Shanghai San Francisco - Manchester Boston - Athens Tel Aviv - Montreal Vancouver - Sao Paulo Seattle - Shanghai San Francisco - Manchester Boston - Athens Tel Aviv - Montreal Munich - Nairobi Geneva - Singapore Dubai - Taipei Madrid - Manila Auckland - Beijing Munich - Nairobi Geneva - Singapore Dubai - Taipei Madrid - Manila Auckland - Beijing
- 6. NELSON.6 Copyright © 2005 Boeing. All rights reserved. Quiet for Airport Communities Quiet for Airport Communities 4001041404 Feet Meters 0 5000 0 1500 Source MS Mappoint, (c) Microsoft, Inc. A330-300 787- 8 767-300 • 85 dBA contours • 3,000 nmi mission 60% less area affected than the A330 and A340 London Heathrow 787 noise footprint stays in the airport property A340-300 A330-200 85 dB Noise Contours at Heathrow 85 dB Noise Contours at Heathrow
- 7. NELSON.7 Copyright © 2005 Boeing. All rights reserved. Breakthrough Technologies Reduce Fuel Burn Per Seat by 20% Breakthrough Technologies Reduce Fuel Burn Per Seat by 20% Systems Systems Materials Materials Aerodynamics Aerodynamics Engines Engines
- 8. NELSON.8 Copyright © 2005 Boeing. All rights reserved. Engine Technology Advancements Engine Technology Advancements Engine and nacelle features (Common to RR and GE engines) • Higher bypass ratio and higher pressure ratio compressor • High-flow low-speed fan • Advanced materials and coatings • No-engine-bleed systems architecture • Low-noise nacelles with chevrons • Engine types are interchangeable at wing / pylon interface Engine and nacelle features (Common to RR and GE engines) • Higher bypass ratio and higher pressure ratio compressor • High-flow low-speed fan • Advanced materials and coatings • No-engine-bleed systems architecture • Low-noise nacelles with chevrons • Engine types are interchangeable at wing / pylon interface
- 9. NELSON.9 Copyright © 2005 Boeing. All rights reserved. Advanced Aerodynamics Advanced Aerodynamics • State of the art 3-D aerodynamic analysis and design tools provide: − Advanced transonic wing design for improved speed and lift − High performance, but mechanically simplified high lift system for high reliability and reduced maintenance cost − Multi-disciplinary optimization for best combination of weight, drag and engine performance • Tightly integrated packaging of systems to reduce the size of aerodynamic fairings for reduced weight and drag • Advanced aerodynamic features validated through extensive wind tunnel test program at both high and low Reynolds number facilities • Laminar flow nacelles • Variable camber trailing edge • State of the art 3-D aerodynamic analysis and design tools provide: − Advanced transonic wing design for improved speed and lift − High performance, but mechanically simplified high lift system for high reliability and reduced maintenance cost − Multi-disciplinary optimization for best combination of weight, drag and engine performance • Tightly integrated packaging of systems to reduce the size of aerodynamic fairings for reduced weight and drag • Advanced aerodynamic features validated through extensive wind tunnel test program at both high and low Reynolds number facilities • Laminar flow nacelles • Variable camber trailing edge Copyright © 2005 Boeing. All rights reserved.
- 10. NELSON.10 Copyright © 2005 Boeing. All rights reserved. Composite Solutions Applied Throughout the 787 Composite Solutions Applied Throughout the 787 Carbon laminate Carbon sandwich Fiberglass Aluminum Aluminum/steel/titanium pylons
- 11. NELSON.11 Copyright © 2005 Boeing. All rights reserved. Starting the Second Century of Powered Flight Starting the Second Century of Powered Flight
- 12. NELSON.12 Copyright © 2005 Boeing. All rights reserved. 787 Advanced Systems 787 Advanced Systems Efficient Airplane Systems • Advanced Energy Management – The More Electric Airplane • Flight Controls – Variable Camber Trailing Edge and Drooped Spoilers Highly Integrated Avionics • Common Core Systems open architecture • Integrated Flight Controls Electronics • Integrated Communication/Navigation/Surveillance equipment • Integrated Airplane Systems control e-Enabled Airplane • Broadband connectivity within airplane and with ground − Flight Deck − Crew Information System − Onboard Health Maintenance − Cabin systems Trade Study decisions assume Life Cycle Costs of the airplane Efficient Airplane Systems • Advanced Energy Management – The More Electric Airplane • Flight Controls – Variable Camber Trailing Edge and Drooped Spoilers Highly Integrated Avionics • Common Core Systems open architecture • Integrated Flight Controls Electronics • Integrated Communication/Navigation/Surveillance equipment • Integrated Airplane Systems control e-Enabled Airplane • Broadband connectivity within airplane and with ground − Flight Deck − Crew Information System − Onboard Health Maintenance − Cabin systems Trade Study decisions assume Life Cycle Costs of the airplane
- 13. NELSON.13 Copyright © 2005 Boeing. All rights reserved. Advanced Energy Management Advanced Energy Management Hybrid AC and DC Primary Distribution Systems (230 Vac, 115 Vac, ±270 Vdc, 28 Vdc) Hybrid AC and DC Primary Distribution Systems (230 Vac, 115 Vac, ±270 Vdc, 28 Vdc) APU with Two 225 kVA Starter/Generators APU with Two 225 kVA Starter/Generators Adjustable Speed Motors and Motor Controllers Adjustable Speed Motors and Motor Controllers Adjustable Electric Air Conditioning Adjustable Electric Air Conditioning Two 250 kVA Variable Frequency Starter/Generators per engine Two 250 kVA Variable Frequency Starter/Generators per engine Liquid Cooled Power Electronics Liquid Cooled Power Electronics Electric Wing Ice Protection Electric Wing Ice Protection Elimination of Pneumatic Bleed System Elimination of Pneumatic Bleed System Generate, Distribute, and Consume energy in an effective and efficient manner.
- 14. NELSON.14 Copyright © 2005 Boeing. All rights reserved. ATRU approx. 25 loads Electrical Systems Overview Electrical Systems Overview • ATRU – Auto Transformer Rectifier Unit • ATU – Auto Transformer Unit • TRU – Transformer Rectifier Unit • NGS – Nitrogen Generating System • EMP – Electric Motor Pump • ECS – Environmental Control System • RPDU – Remote Power Distribution Unit • CCS – Common Core System • BPCU – Bus Power Control Unit • GCU – Generator Control Unit 115 Vac Loads < 10 amps 28 Vdc Loads < 10 amps 115 Vac Loads < 10 amps 28 Vdc Loads < 10 amps Motor Controllers approx.20 loads Large loads such as: • Wing Ice Protection • Hydraulic AC Motor Pump • Fuel Pumps • Galley Ovens • Cargo Heaters • ECS Recirc Fans ENGINE Gen Gen ENGINE Gen Gen APU Gen Gen Large >10 amps: • DC Fuel Pump • Igniters • CCS • Flight Deck Displays • BPCUs/GCUs • etc Large >10 amps: • ECS Lav/Gal fans • Equipment Cooling Fans • Window Heat • etc approx. 150 loads approx. 850 loads RPDU #17 RPDU #1 Adjustable Speed Motors: • Hydraulic EMP • NGS • ECS Compressors • ECS Fans • Engine Start approx. 10 loads 230Vac Distribution ±270Vdc Distribution 28Vdc Distribution 115Vdc Distribution ATU TRU
- 15. NELSON.15 Copyright © 2005 Boeing. All rights reserved. Electronic Circuit Breakers Electronic Circuit Breakers • Display-based control and indication of breaker state • Accessible on Multi-Function Displays (MFDs) and maintenance access devices • Display-based control and indication of breaker state • Accessible on Multi-Function Displays (MFDs) and maintenance access devices NON-NORMAL CB RECENT USED CB CB SEARCH CB BY ATA CB BY BUS CB BY LOCATION CB CUSTOM LIST FLIGHT DECK CB CB BY STATE TRIPPED DETAILS CONTROL DETAILS CONTROL DETAILS CONTROL DETAILS DETAILS DETAILS DETAILS CONTROL DETAILS CONTROL DETAILS CONTROL TRIPPED DETAILS CONTROL DETAILS CONTROL DETAILS CONTROL DETAILS CONTROL DETAILS DETAILS CONTROL CONTROL CONTROL S ½ T ¾ DETAILS CONTROL ? ? UNK UNK CONTROL CONTROL DO NOT CLOSE DO NOT CLOSE 2 1 CE2100713 CIRCUIT BREAKER NAME 1 CE2100714 CIRCUIT BREAKER NAME 2 CE2100715 CIRCUIT BREAKER NAME 3 CE2100701 CIRCUIT BREAKER NAME 4 CE2100702 CIRCUIT BREAKER NAME 5 CK2100780 CONTACTOR NAME 6 CE2100716 CIRCUIT BREAKER NAME 7 CE2100717 CIRCUIT BREAKER NAME 8 CE2100718 CIRCUIT BREAKER NAME 9 CE2100719 CIRCUIT BREAKER NAME 10 CE2100703 CIRCUIT BREAKER NAME 11 CE2100721 CIRCUIT BREAKER NAME 12 CE2100722 CIRCUIT BREAKER NAME 13 CE2100723 CIRCUIT BREAKER NAME 14 CK2100724 CONTACTOR NAME 15 CE2100725 CIRCUIT BREAKER NAME 16 SYS MENU NON-NORMAL CB RECENT USED CB CB SEARCH CB BY ATA CB BY BUS CB BY LOCATION CB CUSTOM LIST FLIGHT DECK CB CB BY STATE TRIPPED DETAILS CONTROL DETAILS CONTROL DETAILS CONTROL DETAILS DETAILS DETAILS DETAILS CONTROL DETAILS CONTROL DETAILS CONTROL TRIPPED DETAILS CONTROL DETAILS CONTROL DETAILS CONTROL DETAILS CONTROL DETAILS DETAILS CONTROL CONTROL CONTROL S ½ T ¾ DETAILS CONTROL ? ? ? ? UNK UNK CONTROL CONTROL DO NOT CLOSE DO NOT CLOSE 2 1 CE2100713 CIRCUIT BREAKER NAME 1 CE2100714 CIRCUIT BREAKER NAME 2 CE2100715 CIRCUIT BREAKER NAME 3 CE2100701 CIRCUIT BREAKER NAME 4 CE2100702 CIRCUIT BREAKER NAME 5 CK2100780 CONTACTOR NAME 6 CE2100716 CIRCUIT BREAKER NAME 7 CE2100717 CIRCUIT BREAKER NAME 8 CE2100718 CIRCUIT BREAKER NAME 9 CE2100719 CIRCUIT BREAKER NAME 10 CE2100703 CIRCUIT BREAKER NAME 11 CE2100721 CIRCUIT BREAKER NAME 12 CE2100722 CIRCUIT BREAKER NAME 13 CE2100723 CIRCUIT BREAKER NAME 14 CK2100724 CONTACTOR NAME 15 CE2100725 CIRCUIT BREAKER NAME 16 SYS MENU
- 16. NELSON.16 Copyright © 2005 Boeing. All rights reserved. Environmental Control Systems Environmental Control Systems • Electric Air Conditioning* • 6,000 foot maximum cabin altitude* • Integrated galley refrigeration* • Conventional cabin pressure control – two outflow valves • Electric Air Conditioning* • 6,000 foot maximum cabin altitude* • Integrated galley refrigeration* • Conventional cabin pressure control – two outflow valves • Overhead cabin air distribution • Upper and lower air recirculation • HEPA Filters and Gaseous Air Purification* for recirculated air • Personal Air Outlet (Gasper) System* - Basic • Optional Flight Deck Humidification System • Overhead cabin air distribution • Upper and lower air recirculation • HEPA Filters and Gaseous Air Purification* for recirculated air • Personal Air Outlet (Gasper) System* - Basic • Optional Flight Deck Humidification System • Forced air cooling for essential E/E equipment • Draw-thru cooling for minor E/E equipment • Liquid cooling for Power Electronics* • Forced air cooling for essential E/E equipment • Draw-thru cooling for minor E/E equipment • Liquid cooling for Power Electronics* • Electric heating for door floor areas* • Draw-thru ventilation for Lavatories, Galleys, and Crew Rests • Electric heating for door floor areas* • Draw-thru ventilation for Lavatories, Galleys, and Crew Rests • Supplemental electric heating for Forward and Bulk Cargo compartments* • Forward* and Bulk Cargo heating and ventilation for animal carriage • Optional Forward Cargo air conditioning • Supplemental electric heating for Forward and Bulk Cargo compartments* • Forward* and Bulk Cargo heating and ventilation for animal carriage • Optional Forward Cargo air conditioning * Different from 777 * Different from 777
- 17. NELSON.17 Copyright © 2005 Boeing. All rights reserved. Cabin Air Compressor Inlet (Deflector door shown deployed) Cabin Air Compressor Inlet (Deflector door shown deployed) Heat Exchanger inlet Heat Exchanger inlet Cabin Air Compressors Cabin Air Compressors Heat Exchangers Heat Exchangers Electric Ram Fan Electric Ram Fan • Two air conditioning packs • Air source provided by cabin air compressors • Adjustable to passenger count • Two air conditioning packs • Air source provided by cabin air compressors • Adjustable to passenger count Cabin Air Conditioning System Cabin Air Conditioning System
- 18. NELSON.18 Copyright © 2005 Boeing. All rights reserved. Cabin Pressurization Schedule Cabin Pressurization Schedule Increased passenger comfort - maximum normal cabin altitude of 6000 feet at maximum cruise altitude (reduced from 8000 feet) Airplane altitude (ft) Airplane altitude (ft) Cabin altitude (ft) Cabin altitude (ft) 3000 3000 30000 30000 33000 33000 36000 36000 39000 39000 42000 42000 450000 450000 4000 4000 5000 5000 6000 6000 7000 7000 8000 8000 777 767 787 747-400
- 19. NELSON.19 Copyright © 2005 Boeing. All rights reserved. Equipment Cooling System Equipment Cooling System RAM Heat Exchanger 3-way Valve PECS Heat Load: motor controller, ATRU, or galley refrigeration unit Lav/galley vent heat exchanger PECS Heat Load: hydraulic motor controller Power Electronics Cooling System Power Electronics Cooling System Pump Package w/ reservoirs, filters, and check valves L1 ECS / MES MC L1 ATRU Basic GRU L2 ECS / MES MC L2 ATRU Left RAM Fan MC Optional GRU Left Ram Air Duct Left Ram Air Duct P700 Rack C1 HYD MC R HYD MC R1 ECS / MES MC R1 ATRU Basic GRU L HYD MC R2 ECS / MES MC Right RAM Fan MC Optional GRU Right Ram Air Duct Right Ram Air Duct P800 Rack C2 HYD MC NGS / APU Start MC
- 20. NELSON.20 Copyright © 2005 Boeing. All rights reserved. Left Engine Engine Driven Pump (EDP) Hydraulic System Architecture Hydraulic System Architecture 5000 psi systems with common pumps 5000 psi systems with common pumps Electric Motor Pump (EMP) Ram Air Turbine (RAT) L Wing: OB & IB R Wing: IB L Wing: 3 R Wing: 12 Left PCU Left Electric Motor Pump (EMP) Electric Driven Pump (EDP) Right Engine OB Aileron – IB Flaperon Spoilers IB & OB Elevator Rudder Thrust Reverser Trailing Edge Flaps Leading Edge Flaps Nose Landing Gear & Steering Main Landing Gear 25 gpm 27 gpm +/- 270V DC Left System 27 gpm +/- 270V DC Center System 13 gpm 25 gpm Right System 27 gpm +/- 270V DC Electric Motor Pump (EMP) Electric Motor Pump (EMP) 27 gpm PCU L Wing: IB R Wing: OB Right Right L Wing: 2, 6 R Wing: 9, 13 L Wing: OB R Wing: OB & IB L Wing: 1, 7 R Wing: 8, 14 Left & Right PCU Motor Motor Reserve Left & Right Normal
- 21. NELSON.21 Copyright © 2005 Boeing. All rights reserved. 787 Fly-by-Wire Flight Controls 787 Fly-by-Wire Flight Controls Leading Edge Surfaces • Inboard and outboard 3-position slats • Sealing Krueger Flap at pylon Leading Edge Surfaces • Inboard and outboard 3-position slats • Sealing Krueger Flap at pylon All Surfaces Fly-By-Wire • Eliminates cables • Reduced weight • Improved functionality All Surfaces Fly-By-Wire • Eliminates cables • Reduced weight • Improved functionality Integrated Flight Control Electronics • Reduced weight and space Integrated Flight Control Electronics • Reduced weight and space Trailing Edge Surfaces • Inboard and outboard single slotted flaps • Single outboard ailerons • Single flaperons • Seven spoiler pairs with droop function • Trailing Edge Variable Camber (TEVC) • Reduced complexity of trailing edge mechanism Trailing Edge Surfaces • Inboard and outboard single slotted flaps • Single outboard ailerons • Single flaperons • Seven spoiler pairs with droop function • Trailing Edge Variable Camber (TEVC) • Reduced complexity of trailing edge mechanism Electric Integrated Horizontal Stabilizer Trim Actuator (HSTA) • Reduced complexity • Reduced weight Electric Integrated Horizontal Stabilizer Trim Actuator (HSTA) • Reduced complexity • Reduced weight
- 22. NELSON.22 Copyright © 2005 Boeing. All rights reserved. High Lift Function High Lift Function • Leading Edge and Trailing Edge Kinematic Motion • Leading Edge and Trailing Edge Kinematic Motion Outboard Slats Gapped on Landing settings Outboard Slats Gapped on Landing settings Outboard Slats Small Gap on Takeoff (Inboard Sealed) Outboard Slats Small Gap on Takeoff (Inboard Sealed) Extended Extended UP UP Middle Middle • Spoiler Droop functionality replaces fore flaps and maintains gap and overlap requirements. • Spoilers driven down via fly-by-wire control. • Spoiler Droop functionality replaces fore flaps and maintains gap and overlap requirements. • Spoilers driven down via fly-by-wire control. Rotary Actuator Rotary Actuator Spoiler Droop Spoiler Droop Variable Camber at Cruise Variable Camber at Cruise Simple pivot dropped hinge Simple pivot dropped hinge Hinge Fairing Hinge Fairing 37-43 degrees down 37-43 degrees down
- 23. NELSON.23 Copyright © 2005 Boeing. All rights reserved. Landing Gear Systems New Control-by-Wire Landing Gear Systems New Control-by-Wire • Landing Gear Actuation − Electronic control and sequencing of landing gear and doors − Dedicated proximity sensors to monitor gear and door position, and to control sequencing − Alternate landing gear extension electrically controlled and hydro-mechanically released • Brake Control − Control-by-wire for brake, autobrake, and anti-skid functions − Electric Brake Actuators • Steering Control − Control-by-wire rudder pedals and dual tillers • Brake Temperature Monitoring System – baseline • Tire Pressure Indication System – baseline • Landing Gear Actuation − Electronic control and sequencing of landing gear and doors − Dedicated proximity sensors to monitor gear and door position, and to control sequencing − Alternate landing gear extension electrically controlled and hydro-mechanically released • Brake Control − Control-by-wire for brake, autobrake, and anti-skid functions − Electric Brake Actuators • Steering Control − Control-by-wire rudder pedals and dual tillers • Brake Temperature Monitoring System – baseline • Tire Pressure Indication System – baseline
- 24. NELSON.24 Copyright © 2005 Boeing. All rights reserved. Wing Anti-Ice System Overview Wing Anti-Ice System Overview • Electrical Power – no engine bleed air • Six heater mats in each heated slat • Aluminum cap to protect leading edge surface • Electrical Power – no engine bleed air • Six heater mats in each heated slat • Aluminum cap to protect leading edge surface The heater mats are bonded to interior surface of the composite slat leading edge skin Slats with ice protection 2, 3, 4, 5 Slats with ice protection 2, 3, 4, 5 Nose Skin Nose Skin Heater Mats Heater Mats
- 25. NELSON.25 Copyright © 2005 Boeing. All rights reserved. Final Nose Configuration Final Nose Configuration • Four windows, fewer posts • Pilot vision similar to 777 • Non-opening windows • Crew escape door • Vertically stowed wipers • Windshield washer • Four windows, fewer posts • Pilot vision similar to 777 • Non-opening windows • Crew escape door • Vertically stowed wipers • Windshield washer
- 26. NELSON.26 Copyright © 2005 Boeing. All rights reserved. Cargo Fire Protection Cargo Fire Protection Aft and Bulk Cargo Compartments Aft and Bulk Cargo Compartments Forward Cargo Compartment Forward Cargo Compartment Cargo Fire Suppression System Nozzles: Flow Valves: Optional Bottles Optional Bottles ETOPS Capability: • Basic - 180 minutes • Options (-8 and -9): − 240 minutes (one bottle) − 330 minutes (two bottles) ETOPS Capability: • Basic - 180 minutes • Options (-8 and -9): − 240 minutes (one bottle) − 330 minutes (two bottles) HRD Btl 1B HRD Btl 1B Metered Btl 2A Metered Btl 2A Metered Btl 2C Metered Btl 2C Metered Btl 2B Metered Btl 2B Metered Btl 2D Metered Btl 2D HRD Btl 1A HRD Btl 1A Metered Btl 2E Metered Btl 2E
- 27. NELSON.27 Copyright © 2005 Boeing. All rights reserved. Fuel Systems Improvements Fuel Systems Improvements • Improved Fuel Quantity availability (measuring sticks removed) • Highly capable center tank fuel scavenge system • Improved lateral balance correction without need to turn off fuel pumps • Redundant jettison path of main tank fuel • Improved anti-ignition safety using all-tank Nitrogen inerting and compliance to latest ignition prevention regulations • Improved Fuel Quantity availability (measuring sticks removed) • Highly capable center tank fuel scavenge system • Improved lateral balance correction without need to turn off fuel pumps • Redundant jettison path of main tank fuel • Improved anti-ignition safety using all-tank Nitrogen inerting and compliance to latest ignition prevention regulations
- 28. NELSON.28 Copyright © 2005 Boeing. All rights reserved. Common Core System Benefits Common Core System Benefits with robust partitioning of functions in software with robust partitioning of functions in software hierarchical layering of services hierarchical layering of services having well defined, standardized, rigidly enforced key interfaces A653 having well defined, standardized, rigidly enforced key interfaces A653 Common Computing Resource • Based on Open System Architecture Principles Common Computing Resource • Based on Open System Architecture Principles Modular Implementation Modular Implementation of common elements of common elements RDC Core Signal Condit- ioning Controller Power Supply Power Supply A/D, D/A Sys Bus IF Application API Application API Application API Application API Application API Application API Resource Control Operating System H/W Support Package ECS Ctrl. Utilities Avionics Mech /Hyd Electrical Cabin Sys Hardware Implementation Application API Application API Application API Application API Application API Application API Application API Application API Application API Application API Application API Application API Operating System ECS Ctrl. Utilities Avionics Mech /Hyd Electrical Cabin Sys Hardware Implementation A653 A653 Remote Data Concentrators • Reduces airplane wiring/weight, • Ease of system upgrade/modification • Highly reliable Remote Data Concentrators • Reduces airplane wiring/weight, • Ease of system upgrade/modification • Highly reliable Common Data Network • Open industry standard interfaces A664 • Eliminate multiple standards & protocols • Fiber Optic Network media Common Data Network • Open industry standard interfaces A664 • Eliminate multiple standards & protocols • Fiber Optic Network media
- 29. NELSON.29 Copyright © 2005 Boeing. All rights reserved. Comm Radios Comm Radios VHF VHF HF HF SATCOM SATCOM VHF VHF HF HF SATCOM SATCOM Avionics Integration Beyond 777 Avionics Integration Beyond 777 777 777 787 787 AIMS Displays DFDAC FM / TM CMF / ACMF / QAR FDCF Gateways Others AIMS Displays DFDAC FM / TM CMF / ACMF / QAR FDCF Gateways Others Nav Radios Nav Radios Integrated Navigation Radios (INR) Integrated Navigation Radios (INR) VOR VOR MB MB MMR MMR DME DME RA RA DME DME RA RA Inertial Inertial Earth Reference System (ERS) Earth Reference System (ERS) ADIRU ADIRU SAARU SAARU Other LRUs Other LRUs WEU WEU Others Others Surveillance Surveillance WXR WXR EGPWS EGPWS TCAS TCAS ATC ATC Integrated Surveillance System (ISS) Integrated Surveillance System (ISS) Common Core Resource (CCR) Air Data Crew Alerting Comm Management Data Acquisition Displays FM / TM / AT Health Management Gateways Others Common Core Resource (CCR) Air Data Crew Alerting Comm Management Data Acquisition Displays FM / TM / AT Health Management Gateways Others
- 30. NELSON.30 Copyright © 2005 Boeing. All rights reserved. Flight Deck Flight Deck • Boeing look, feel and procedures flow • Familiar Boeing controls • Familiar display formats • All 777 functions and features • Large format displays
- 31. NELSON.31 Copyright © 2005 Boeing. All rights reserved. Display Layout Comparison Display Layout Comparison 777 787
- 32. NELSON.32 Copyright © 2005 Boeing. All rights reserved. Class III EFB Overview Class III EFB Overview • One installed for each pilot – basic • Avionics quality LCD • Accessible via touchscreen, bezel keys, cursor control device and keyboard • Interfaces to: ―Other Avionics (e.g. Flight Management) ―Communication systems ―Flight Deck printer
- 33. NELSON.33 Copyright © 2005 Boeing. All rights reserved. On-board Performance Tool On-board Performance Tool • Calculates limit weights, V speeds, thrust and more • Performance optimization and flexibility − Optimum flap − Multiple intersections − Calculates assumed temperature thrust reduction − MEL and CDL item entry − Airport NOTAM entry • Data from FMC − Origin airport, QNH, OAT • Simplified weight and balance • Calculates limit weights, V speeds, thrust and more • Performance optimization and flexibility − Optimum flap − Multiple intersections − Calculates assumed temperature thrust reduction − MEL and CDL item entry − Airport NOTAM entry • Data from FMC − Origin airport, QNH, OAT • Simplified weight and balance
- 34. NELSON.34 Copyright © 2005 Boeing. All rights reserved. Crew Information System — Onboard Health Management Crew Information System — Onboard Health Management Fault Prediction Fault Prediction Objective: Reduce schedule interruptions and maintenance costs Coordinated airplane and ground processing approach Coordinated airplane and ground processing approach Electronic link to maintenance manuals Electronic link to maintenance manuals Airplane level fault consolidation and correlation, and data collection Airplane level fault consolidation and correlation, and data collection Electronic Distribution of Software Electronic Distribution of Software Integrated data load and configuration reporting Integrated data load and configuration reporting Media-less data transfer to/from ground stations Media-less data transfer to/from ground stations
- 35. NELSON.35 Copyright © 2005 Boeing. All rights reserved. 787 Program Schedule 787 Program Schedule 2002 2003 2004 2005 2006 2007 2008 First Flight First Flight Certification and Delivery Certification and Delivery Airplane Announcement Airplane Announcement Firm Configuration Firm Configuration Program Launch Program Launch Authority to Offer Authority to Offer
- 36. NELSON.36 Copyright © 2005 Boeing. All rights reserved. Thank You Thank You