Supersonic Transport Development Program. Phase Iii Proposal. Boeing Model 2707. Environmental Control Subsystem Specification PDF Download
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Author: V. D. Warmbo
Publisher:
ISBN:
Category :
Languages : en
Pages : 66
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Book Description
Author: V. D. Warmbo
Publisher:
ISBN:
Category :
Languages : en
Pages : 66
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Book Description
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: 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: 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.
Author: R. G. Bush
Publisher:
ISBN:
Category :
Languages : en
Pages : 309
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Book Description
Contents: General Airplane Description; General Requirements; General Airplane Characteristics; Airframe Structures; Propulsion; Flight Deck Accommodations; Flight Controls; Hydraulic Power System; Electric Power System; Electronics; Passenger and Cargo Provisions; Environmental Control; Maintainability, and Standard Parts, Interchangeability, and Replaceability.
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: 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: 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: John Katzinski
Publisher:
ISBN:
Category :
Languages : en
Pages : 75
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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 airplenes. The airframe subsystem consists of the fuselage, empennage, wing and control surfaces. Discrete differences between the prototype model supersonic transport airplanes and production airplanes are included in Supplement I. (Author).
Author: L. J. Kimer
Publisher:
ISBN:
Category :
Languages : en
Pages : 94
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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 air induction subsystem for the prototype-model supersonic transport airplane. Differences between the prototype and production airplanes are described in Supplement I. The air induction subystem shall provide the engine with the quantity of air demanded at high-pressure recovery within the flow distortion limits of the engine. Four independent subsystems are required per airplane.
