Supersonic Transport Development Program. Phase Iii. Boeing Model 2707. Flight Deck Subsystem Specification PDF Download
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Author: George G. Burton
Publisher:
ISBN:
Category :
Languages : en
Pages : 163
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Book Description
Author: George G. Burton
Publisher:
ISBN:
Category :
Languages : en
Pages : 163
Get Book Here
Book Description
Author: George G. Burton
Publisher:
ISBN:
Category :
Languages : en
Pages : 126
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Book Description
This specification defines the objectives, criteria and configuration and establishes the requirements for performance, design, test, and qualification of the flight deck subsystem as applicable to the prototype supersonic transport airplane. Differences between the prototype and production airplanes are described in Supplement I. (Author).
Author: BOEING CO SEATTLE WA SUPERSONIC TRANSPORT DIV.
Publisher:
ISBN:
Category :
Languages : en
Pages : 139
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Book Description
This specification defines objectives, criteria and configuration, and establishes requirements for performance, operation, design, test and qualification of the air induction control subsystem (hereinafter called the control subsystem) as applied to the prototype model supersonic transport airplane. Differences between the prototype and production airplanes are described in Supplement I. This subsystem is used to provide automatic and manual control of the air induction subsystem, (hereinafter called the inlet). There shall be one independent control subsystem for each of the four inlets. Each control subsystem changes the geometry of an inlet centerbody and operates its bypass louvers and takeoff doors to provide efficient inlet airflow diffusion and high performance inlet-engine airflow match. The subsystems include necessary hydraulic power generation, hydraulic power distribution equipment, and flight deck controls and displays. Power from the airplane electrical system and from each of the engines is required by the subsystem in order to accomplish its intended function. (Author).
Author: Grant W. Ort
Publisher:
ISBN:
Category :
Languages : en
Pages : 41
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Book Description
This specification defines the objectives, criteria, and configuration, and establishes the requirements for performance, design, test and qualification of the starting subsystem (SS) for the prototype model supersonic transport airplane. Differences between the prototype and production airplanes are described in Supplement I. The SS provides for starting and windmill braking of the engine, drives the accessory drive subsystem (ADS) and its attached accessories in the engine disconnect mode, and supplies ground source or engine bleed air to the environmental control subsystem (ECS).
Author: E. See
Publisher:
ISBN:
Category :
Languages : en
Pages : 143
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Book Description
This specification defines the objectives, criteria, and configuration and establishes the requirements for performance, design, test, and qualification of the flight controls and hydraulic subsystem for the B-2707 supersonic transport airplane. Differences between the prototype and production airplanes are described in Supplement I. This subsystem shall provide control of the airplane in response to pilot or guidance-navigation commands and furnish hydraulic power to the landing gear subsystem. This subsystem shall consist of primary flight controls, secondary flight controls, automatic flight controls and hydraulic power. (Author).
Author: George M. Burton
Publisher:
ISBN:
Category :
Languages : en
Pages : 76
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Book Description
Contents: Requirements; Performance; Subsystem Definition; Design and Construction; Quality Assurance Provisions; Engineering Test and Evaluation; Preliminary Qualification Tests; Formal Qualification/Certification Tests; and Reliability Test and Analysis.
Author: W. H. Burrell
Publisher:
ISBN:
Category :
Languages : en
Pages : 33
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Book Description
This specification defines the objectives, criteria and configuration and establishes the requirements for performance, design, test, and qualification of the Aircraft Integrated Data System (AIDS) for the prototype model supersonic transport airplane. The primary purpose of AIDS is to reduce maintenance cost and to improve aircraft availability and dispatch reliability. It accomplishes fault detection during flight and identifies aircraft system component failures. This information is presented as a readable output on board the airplane for use by the flight crew during flight and maintenance crew upon termination of the flight. The AIDS data may be further used to accomplish failure prediction by analyzing flight recorded system performance data with a ground based computer.
Author: John Katzinski
Publisher:
ISBN:
Category :
Languages : en
Pages : 76
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Book Description
This specification establishes the requirements for performance, design, test, and qualification for the Airframe Subsystem as applied to the prototype model supersonic transport airplanes. The airframe subsystem consists of the fuselage, empennage, wing and control surfaces.
Author: Howard G. Barton
Publisher:
ISBN:
Category :
Languages : en
Pages : 395
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Book Description
This specification defines the objectives, criteria, and configuration, and establishes the requirements for performance, design, test, and qualification of the navigation and communication subsystem for the prototype model supersonic transport airplane. (Author).
Author: S. E. Lindstrom
Publisher:
ISBN:
Category :
Languages : en
Pages : 47
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Book Description
This specification defines the objectives, criteria, and configuration and establishes the requirements for performance, design, test, and qualification of the fuel subsystem for the prototype model supersonic transport airplane. This subsystem provides for the storage, distribution and management of fuel.
