COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 45
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1 COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 45
2 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
3 COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 4
4 787 Wing Flex - On-Ground On-Ground 0 ft COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 5
5 787 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
6 787 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
7 787 Static Load Ultimate Load COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 8
8 787 Cabin Experience COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 10
9 787 Windows COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 11
10 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
11 787 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
12 787 Pax Oxygen Gaseous 3000 psi - Steel cylinder Chem Oxy Generators (2x) COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 15
13 787 Fuel Tank Inerting COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 16
14 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
15 EE vs Pneumatic Power Distribution COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 21
16 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
17 Overhead Panels - Circuit Breakers COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 23
18 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
19 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
20 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
21 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
22 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
23 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
24 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
25 Air Data System Design Philosophy Federated AD & IR (all previous models) 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
26 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
27 COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 46
28 747 Dream Lifter COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 47
29 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
30 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 Grottaglie, Italy to Charleston, SC Nagoya, Japan to Charleston, SC Horizontal Stabilizer Foggia, Italy to Charleston, SC Section 43 Nagoya, Japan to Charleston, SC Section 46 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
31 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
32 COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 51
33 COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 52
34 COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 53
35 COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 54
36 787 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
37 787 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
38 787 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
Introducing the 787. COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 1
Introducing the 787 COPYRIGHT 2010 THE BOEING COMPANY Smith, 7-April-2011, ESASI-Lisbon 1 787 Size Comparison 767-400 787-8 777-300 ~Pax 3-Class 245 250 368 ~Span 170 ft 197 ft 200 ft ~Length 201 ft 186
Highlights. 787 Overview COPYRIGHT 2008 THE BOEING COMPANY COPYRIGHT 2008 THE BOEING COMPANY. Firm orders NG 737
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