Introducing the 787. COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 1

Transcription

1 Introducing the 787 COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 1

2 787 Size Comparison ~Pax 3-Class ~Span 170 ft 197 ft 200 ft ~Length 201 ft 186 ft 242 ft ~MTGW 450,000 lbs 500,000 lbs 660,000 lbs ~Range 5,600 NM 7,650 NM 6,000 NM Cruise Mach COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 2

3 Quiet for Airport Communities 85 db Noise Contours at Heathrow London Heathrow 787 noise footprint stays in the airport property Source MS Mappoint, (c) Microsoft, Inc. 85 dba contours 3,000 nmi mission Feet Meters COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 17

4 Composite Structure By weight Composites 50% 12% - Aluminum 20% 50% Carbon laminate Carbon sandwich Fiberglass Aluminum Aluminum/steel/titanium pylons Titanium 15% Aluminum 20% Steel 10% Other 5% Composites 50% COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 3

5 COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 4

6 Partners Across the Globe are Bringing the 787 Together Wing tips Seoul, Korea U.S. Boeing Spirit GE Goodrich Australia Boeing Canada Boeing Messier-Dowty Asia Fuji Mitsubishi Kawasaki KAL-ASD Europe Messier-Dowty Rolls-Royce Latécoère Alenia Saab Fixed trailing edge Nagoya, Japan Moveable trailing edge Melbourne, Australia Wing Nagoya, Japan Nacelles Chula Vista, CA Center fuselage Grottaglie, Italy Mid forward fuselage Nagoya, Japan 41 Forward fuselage Wichita, KS Tail fin Frederickson, WA Passenger entry doors Toulouse, France Cargo access doors Linköping, Sweden Horizontal stabilizer Foggia, Italy Aft fuselage Charleston, SC Main landing gear wheel well Nagoya, Japan Center wing box Nagoya, Japan Wing/body fairing Landing gear doors Winnipeg, Canada Engines GE Evandale, Ohio Rolls Royce Derby, UK Landing gear Gloucester, UK Fixed and moveable leading edge Tulsa, OK COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 48

7 787 Structure from Asia Fuji Heavy Industries Kawasaki Heavy Industries Mitsubishi Heavy Industries Korean Air International partners providing key 787 structure COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 55

8 787 Structure from Europe Alenia Aeronautica Alenia Aeronautica Latecoere Messier-Dowty Saab International partners providing key 787 structure COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 56

9 787 Structure from North America Spirit Boeing - Charleston Boeing - Charleston International partners providing key 787 structure COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 57

10 787 Wing Flex - On-Ground On-Ground 0 ft COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 5

11 787 Wing Flex - 1G Flight 1G Flight ~12 ft On-Ground 0 ft 1G Flight COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 6

12 787 Wing Flex Ultimate-Load ~26 ft 1G Flight ~12 ft On-Ground 0 ft Max-Load COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 7

13 787 Static Load Ultimate Load COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 8

14 787 Cabin Experience COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 10

15 787 Windows COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 11

16 Cleaner Cabin Air COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 12

17 Ride Quality - Smoother Ride Vertical Gust Suppression Change in altitude (m) Time (sec) Uses the flaperons and elevators Counters light to moderate turbulence to improve ride quality Passengers have a more comfortable flight With Enhanced Gust Suppression Without Enhanced Gust Suppression COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 13

18 787 Cabin Experience Windows - Larger Pressure - Lower Humidity - Higher Air Quality - Improved Ride Quality - Improved Food Service - Unchanged (sorry) COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 14

19 787 Pax Oxygen Gaseous 3000 psi - Steel cylinder Chem Oxy Generators (2x) COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 15

20 787 Fuel Tank Inerting COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 16

21 Engine Technology Advancements No-engine-bleed-air systems architecture Higher bypass ratio Low-noise nacelles with chevrons COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 18

22 Airplane/Engine Architecture No-engine-bleed-air systems Wing LE Anti-Ice bleed air electric Air Conditioning bleed air electric Cabin Pressure bleed air electric Engine start bleed air electric Engine Generators kva 1000 kva 120 kva) 250 kva) Generators Starter/Gen s COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 19

23 Variable Frequency Power Generation VAC 400 Hz VAC Hz COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 20

24 EE vs Pneumatic Power Distribution COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 21

25 Electronic Circuit Breakers SYS MENU FLIGHT DECK CB CB BY ATA CB BY BUS NON-NORMAL CB CB BY STATE CB SEARCH CB RECENT CB BY LOCATION USED CB CUSTOM LIST CE CIRCUIT BREAKER NAME 1 TRIPPED DETAILS CONTROL No physical CBs in Flight Deck CE CIRCUIT BREAKER NAME 2 DETAILS CONTROL CE CIRCUIT BREAKER NAME 3 DETAILS CONTROL CB control and state indication are display based. CE CIRCUIT BREAKER NAME 4 CE CIRCUIT BREAKER NAME 5 CK CONTACTOR NAME 6 DETAILS CONTROL DETAILS CONTROL TRIPPED DETAILS CONTROL 1 Accessible on Multi-Function Display (MFD) and maintenance access devices CE CIRCUIT BREAKER NAME 7 CE CIRCUIT BREAKER NAME 8 CE CIRCUIT BREAKER NAME 9 CE CIRCUIT BREAKER NAME 10? UNK DO NOT CLOSE DETAILS DETAILS DETAILS DETAILS CONTROL CONTROL CONTROL CONTROL CE CIRCUIT BREAKER NAME 11 DETAILS CONTROL A few Thermal CB are located in the Fwd EE-Bay CE CIRCUIT BREAKER NAME 12 CE CIRCUIT BREAKER NAME 13 CE CIRCUIT BREAKER NAME 14? DO NOT CLOSE UNK DETAILS DETAILS DETAILS CONTROL CONTROL CONTROL 2 CK CONTACTOR NAME 15 DETAILS CONTROL CE CIRCUIT BREAKER NAME 16 DETAILS CONTROL COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 22

26 Overhead Panels - Circuit Breakers COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 23

27 Avionics Integration Surveillance WXR EGPWS TCAS ATC Integrated Surveillance System (ISS) Nav Radios VOR MB MMR DME RA RA DME Integrated Navigation Radios (INR) Comm Radios VHF HF SATCOM SATCOM HF VHF Inertial ADIRU SAARU Earth Reference System (ERS) Other LRUs WEU Others AIMS Displays DFDAC FM / TM CMF / ACMF / QAR FDCF Gateways Others Common Core Resource (CCR) Air Data Crew Alerting Comm Management Data Acquisition Displays FM / TM / AT Health Management Gateways Others COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 24

28 Integrated FCE Equivalent Channel of Flight Controls and High Lift 777 PSA PFC ACE 787 FSEU AFDC PCM ACE FCM COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 25

29 Common Core System Common Computing Resource High integrity computing resources for hosted systems applications Common Data Network High Integrity Network Open industry standard interfaces A664 Remote Data Concentrators 21 RDCs Remote I/O capability Reduces airplane wiring COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 26

30 CCS Hosted Functions Avionics Communication and Audio Avionics Flight Management and Navigation Avionics Thrust Management and Auto-throttle Avionics Primary Display Function Avionics Crew Alert/Warning and Surveillance Avionics Crew Information Services Avionics Maintenance and Data Loading Cabin Management and Air Show Environmental Control System Functions: Power Electronics and Other Equipment Liquid/forced air Cooling, Air Conditioning, Cabin Pressurization, Ice & Rain Protection, Air Distribution, Galley Refrigeration, Low Pressure Systems, Cargo Heat, Wheel Well Fire Detection and Cargo Fire Detection/Protection Electrical Utility System Control Functions Remote Power Distribution System (RPDS), Power Distribution Panels (PDPs), Generator/Bus Power Control Units (GCU/BPCU), Proximity Sensors, Window Heat, Tail Strike, Emergency Passenger Assist System (EPAS), Exterior Lighting Data Interface to Flight Controls Electronics (FCE) Interface to Flight Deck Panels and Switches Fuel Management and Fuel Quantity Indication Hydraulics Control Mechanical System Interface Functions in Brakes, Landing Gear, Nose Wheel Steering Payloads Interface Functions in Galleys, Water & Waste, Emergency Lighting Data Interface to Propulsion Controls in EEC, Engine Fire Detection/Protection, Thrust Reverser COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 27

31 Hydraulic System Architecture 25 gpm Left Engine Engine Driven Pump (EDP) Left System Electric Motor Pump (EMP) +/- 270V DC 27 gpm Center System 27 gpm Electric Motor Pump (EMP) 27 gpm +/- 270V DC 25 gpm 13 gpm Electric Motor Pump (EMP) 5000 psi systems Ram Air Turbine (RAT) Right Engine Electric Driven Pump (EDP) Right System Electric Motor Pump (EMP) +/- 270V DC 27 gpm OB Aileron IB Flaperon L Wing: OB & IB R Wing: IB L Wing: OB R Wing: OB & IB L Wing: IB R Wing: OB Spoilers IB & OB L Wing: 3 R Wing: 12 L Wing: 1, 7 R Wing: 8, 14 L Wing: 2, 6 R Wing: 9, 13 Elevator Left Left & Right Right Rudder PCU PCU PCU Thrust Reverser Left Right Trailing Edge Flaps Motor Leading Edge Flaps Motor Nose Landing Gear & Steering Normal Reserve Main Landing Gear Left & Right COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 28

32 Landing Gear Systems New Control-by-Wire Landing Gear Actuation - Electronic control and sequencing of landing gear and doors Brake System - Control-by-wire brakes, autobrake and anti-skid - Electric Brake Actuators Nose Gear Steering - Control-by-wire (pedals & dual tillers) - Hydraulic actuation COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 29

33 Cabin Air Conditioning System Heat Exchanger inlet Cabin Air Compressor Inlet (Deflector door shown deployed) Heat Exchangers Cabin Air Compressors Electric Ram Fan COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 30

34 External Air Sources Heat Exchanger Inlet Cabin Air Compressor Inlet Heat Exchanger Exhaust Doors COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 31

35 787 EAFR Enhanced Airborne Flight Recorder Dual-Combi Architecture Both recorders are same P/N - self contained acquisition function - FRED file in memory (Flight Rec. Elec. Doc. - ARINC 647) - flight data 25 hours minimum -voice - 2 hours -datalink FWD EAFR -RIPS for voice recording only AFT EAFR -no RIPS COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 32

36 Forward EAFR & RIPS COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 33

37 Aft Recorder COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 34

38 Recording Format EAFR Flight Data recording format - ARINC raw data file size ~800 MB (zips to 200 MB) - Approx equivalent to WPS recorder The 787 QAR - called "Continuous Parameter Logging" (CPL) - stored on the mass storage devices (server) - ARINC 767 recording format COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 35

39 Flight Controls / 787 Common Functionality Common 777 / 787 Fly-by-wire Functionality Stall Protection Overspeed Protection Bank Angle Protection Tail Strike Protection Thrust Asymmetry Compensation Yaw Damping, Over-yaw Protection Gust Load Alleviation Fin Load Alleviation Flap Load Relief & Autogap Lateral Gust Suppression Modal Suppression COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 36

40 Flight Controls New Features P-Beta control law Vertical Gust Suppression (turbulence) Enhanced Stall Protection - Limits high angles of attack Enhanced Thrust Asymmetry Compensation - Adds inertial yaw detection on ground - Generates rudder & steering for yaw disturbances COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 37

41 P Beta Control Law Wheel commands roll rate (P) Pedals command sideslip angle (Beta) Opposes disturbances Coordinates lateral and directional control Automatic aileron & rudder trim - No aileron trim switch COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 38

42 Air Data System Design Philosophy Federated AD & IR (Prior to 777) Voted AD & IR (777, 787) AD AD AD IR IR IR PFD Stby PFD FO Capt PFD AD SAARU AD/IR Stby AD AD AD IR FDI PFD Voted FT-ADIRU AD-IR FO Capt Fault arbitration by CREW Fault arbitration by SYSTEM AD = Air Data IR = Inertial Reference FDI = Fault Detection & Isolation PFD = Primary Flight Display COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 39

43 Air Data System - Common Mode Vulnerability Common Mode Hazards to Pitot-Static sensors - Mud Daubers - Icing - Volcanic Ash - Hail -Radomefailure -Birds - Pitot covers - Taped Static Ports - Maintenance errors (pneumatic plumbing) 787 new capabilities for protection - Synthetic airspeed - GPS altitude - Common Mode Monitor COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 40

44 787 Synthetic Airspeed Calculated from angle of attack and inertial data - AOA voted dual sensors plus inertial data - Accurate Coefficient of Lift (C L ) - Airplane Mass from FMC - Validated after Takeoff Algorithm developed for enhanced stall protection Avoid displaying data known to be bad - Loss of valid voted V CAS = Display synthetic airspeed V SYN - Loss of valid voted P STATIC = Display GPS altitude COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 41

45 Onboard Health Management Objective: Reduce schedule interruptions and maintenance costs Integrated data load and configuration reporting Electronic Distribution of Software Airplane level fault consolidation and correlation, and data collection Electronic link to maintenance manuals Fault Prediction Media-less data transfer to/from ground stations Coordinated airplane and ground processing approach COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 42

46 COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 45

47 747 Dream Lifter COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 47

48 Dreamlifter Route Structure Section 41 Wichita, KS to Everett, WA Joined Section Charleston, SC to Everett, WA Joined Section Charleston, SC to Everett, WA Section 44 Section 11/45 Nagoya, Japan to Charleston, SC Grottaglie, Italy to Charleston, SC Horizontal Stabilizer Foggia, Italy to Charleston, SC Section 46 Section 43 Nagoya, Japan to Charleston, SC Grottaglie, Italy to Charleston, SC Wing Nagoya, Japan to Everett, WA Worldwide operations, less work in process COPYRIGHT 2011 THE BOEING COMPANY COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 49

49 Dreamlifter Enables Global Operations Efficient transport of 787 major subassemblies from international partners Main deck is 65,000 cubic feet - 3x capacity of Freighter Reduced transportation times versus surface transportation - Dramatically reduced final assembly flow times - Less inventory COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 50

50 COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 51

51 COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 52

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