Supersonic Transport Development Program. Phase Iii Proposal. Boeing Model 2707. Volume Ii-13. Propulsion Report-part B. Engine Installation Fuel System Exhaust System PDF Download
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Author: BOEING CO SEATTLE WASH SUPERSONIC TRANSPORT DIV.
Publisher:
ISBN:
Category :
Languages : en
Pages : 112
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Book Description
Contents: Engine Installation; Fuel System; System Studies; Exhaust System; and Noise Suppression.
Author: BOEING CO SEATTLE WASH SUPERSONIC TRANSPORT DIV.
Publisher:
ISBN:
Category :
Languages : en
Pages : 112
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Book Description
Contents: Engine Installation; Fuel System; System Studies; Exhaust System; and Noise Suppression.
Author: BOEING CO SEATTLE WASH SUPERSONIC TRANSPORT DIV.
Publisher:
ISBN:
Category :
Languages : en
Pages : 308
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Book Description
This document includes the summary and three major sections of the propulsion report describing the engines, supersonic inlet, and the propulsion control systems. Studies conducted during Phase II C have resulted in significant improvements to the Boeing Model 2707 propulsion system. Optimum sized engines with improved thrust and fuel consumption characteristics are available from General Electric and Pratt and Whitney Aircraft. The four separate and interchangeable propulsion pods are mounted below the lower surface of the horizontal stabilizer at such a position that the engine exhaust will not impinge on any part of the airplane. The pod location and shape provides optimum lift effect on the airplane.
Author: BOEING CO SEATTLE WA SUPERSONIC TRANSPORT DIV.
Publisher:
ISBN:
Category :
Languages : en
Pages : 117
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Book Description
Throughout Phase II-C, as in earlier phases of the SST Program, The Boeing Company has maintained a program of design analysis and performance evaluation, with the coordinated participation of both engine contractors. As a result, the General Electric GE4/J5P powered B-2707 (GE) and the Pratt and Whitney Aircraft JFT17A-21B powered B-2707 (P and WA) airplanes are very competitive in terms of overall airplane performance criteria, and either would make an outstanding airline airplaned. The purpose of this document is to report the technical evaluation of the two engines. Considerations in this evaluation include engine/airplane matching and performance, engine design, installation compatibility, development plan, development risk, and growth potential.
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 812
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Book Description
Author: James W. McKee
Publisher:
ISBN:
Category :
Languages : en
Pages : 399
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Book Description
Contents: Hydraulics and Flight Controls System; Landing Gear Systems; Instruments and Displays; Passenger and Cargo Handling Provisions; Starter/Auxiliary Power Unit System; Accessory Drive System; and Fire Detection/Extinguishing System.
Author: James W. McKee
Publisher:
ISBN:
Category :
Languages : en
Pages : 237
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Book Description
The air-conditioning system includes a cabin air source and associated cooling equipment, passenger cabin and flight deck air distribution and exhaust system, cabin temperature control, cabin pressure control, equipment and compartment conditioning, and instruments to monitor ozone levels. The adverse weather systems include ice and fog protection and rain removal for the flight deck windshields. Fog protection is provided for the movable-nose side windows. Ice protection is provided for the engine inlets and air data sensors. The oxygen system includes a gaseous oxygen system for the flight crew members and portable first-air oxygen units for the passenger cabin occupants and flight crew members. The electrical system comprises all electrical equipment required for generation, control, conversion, storage, and distribution of electrical power. It also includes electrical and electronic wiring and circuit protection devices between the distribution buses and the utilization loads and the airplane internal and external lights. Radio navigation and communication design and performance requirements have generally been well-established through action by airline industry study groups; e.g. RTCA, ATA, ARINC, and are therefore discussed briefly. Inertial Navigation and Weather Radar are development items, not yet fully defined, and are discussed in detail.
Author: D. R. Donaldson
Publisher:
ISBN:
Category :
Languages : en
Pages : 138
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Book Description
This report presents the Boeing proposal for structural design loads and environment on the B-2707 commercial supersonic transport. Information on Phase III planning is included to define an efficient program necessary for first flight of the B-2707 prototype. Flight and ground loads criteria, flutter and vibration criteria, and structural design criteria are presented. The design loads and methods of analysis together with load validation data are presented in Sec. 3.0. The effects of these loads on ride comfort of the passengers and crew are also included. Structural temperature analyses that define the effects of aerodynamic and engine-induced heating on all major structure are presented in Sec. 4.0.
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 219
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Book Description
The air transportation system is comprised of the following basic elements; Airlines; Airports; Governmental facilities and agencies; Passengers and cargo; and Airplane.
Author: A. J. Mathy
Publisher:
ISBN:
Category :
Languages : en
Pages : 209
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Book Description
Contents: Summary; Wind Tunnel Program; Materials and Processes; Airframe Structures; Airframe Subsystems; Propulsion System; Product Support; System Integration; Airplane Ground Test Program; Design Assurance; Production Tests; and Certification Plan.
Author: John E. Johnson
Publisher:
ISBN:
Category :
Languages : en
Pages : 354
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Book Description
This book describes the production version of the B-2707. Minimal differences will exist between the production and prototype airplanes because of availability of materials, processes, and facilities. A general discussion is presented of the structural design. A complete description is included of structural design features of the wing, fuselage, empennage, control surfaces, and landing gear, including drawings of all major assemblies. A preliminary stress analysis discusses methods of analysis, stress levels, member sizes, allowable stresses, and analysis and description of fail-safe designs. An analysis of structure designed by sonic or high-temperature effects is included. A fatigue analysis, includes fatigue criteria and environment, analysis procedure, fatigue damage summaries, fatigue analysis results, and 1-g stress levels.
