Download or read book Supersonic Transport Development Program Phase Iii Boeing Model 2707 Engine Inlet Anti icing Subsystem Specification written by J. N. R. Hall and published by . This book was released on 1966 with total page 23 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification defines the objectives, criteria, and configuration and establishes the requirements for performance, design, test, and qualification of the Inlet Anti-icing Subsystem (hereinafter called IAIS), for the prototype model supersonic transport airplane. Differences between the prototype and the production airplanes are described.
Download or read book Supersonic Transport Development Program Phase Iii Proposal Boeing Model 2707 Engine Inlet Anti icing Subsystems Specification written by N. R. Hall and published by . This book was released on 1966 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt: The primary design objective of the IAIS shall be the control of ice accrual on the selected supersonic inlet surfaces to the level required to limit inlet airflow distortion, prevent damage to the engine in event of ice ingestion, and prevent blockage of the air data sensors. Failure of an anti-icing shutoff valve in the open position shall not prevent dispatch or continuation of normal flight. (Author).
Download or read book ENGINE INLET ANTI ICING SUBSYSTEM SPECIFICATION SST BOEING MODEL 2707 SUPERSONIC TRANSPORT PROGRAM PHASE II C REPORT written by and published by . This book was released on 1966 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Supersonic Transport Development Program Phase Iii Boeing Model 2707 Air Induction Subsystem Specification written by L. J. Kimer and published by . This book was released on 1966 with total page 79 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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. The air induction subsystem shall provide the engine with the quantity of air demanded at high-pressure recovery within the flow distortion limits of the engine. This subsystem requires a control subsystem and an anti-icing subsystem. The installation of the subsystem is defined by specification D6A10113-1. Four independent subsystems are required per airplane.
Download or read book Supersonic Transport Program Phase Ii c Report Air Induction Subsystem Specification Sst Boeing Model 2707 written by R. E. Ensley and published by . This book was released on 1966 with total page 21 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification establishes the requirements for performance, design, test and qualification of the Air Induction Subsystem. This subsystem shall provide the engine with the quantity of air demanded within the flow distortion limits of the engine. This subsystem requires a control subsystem and an anti-icing subsystem, and provides for high pressure recovery within the flow. The installation of the subsystem is defined by the Aircraft Engine Installation Subsystem Specification (D6A10113-1).
Download or read book Supersonic Transport Development Program Phase Iii Proposal Boeing Model 2707 Air Induction Control Subsystem Specification written by BOEING CO SEATTLE WA SUPERSONIC TRANSPORT DIV. and published by . This book was released on 1966 with total page 139 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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).
Download or read book Supersonic Transport Development Program Phase Iii Proposal Boeing Model 2707 Air Induction Subsystem Specification written by L. J. Kimer and published by . This book was released on 1966 with total page 94 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Download or read book Supersonic Transport Development Program Phase Iii Boeing Model 2707 Flight Deck Subsystem Specification written by George G. Burton and published by . This book was released on 1966 with total page 163 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Supersonic Transport Development Program Phase Iii Boeing Model 2707 Propulsion Performance Specification general Electric written by Paul E. Johnson and published by . This book was released on 1966 with total page 85 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification establishes the requirement for the performance and method of calculation of the 2707-100 (GE) propulsion system. The General Electric GE4/J5P engine performance data is the primary data for the propulsion performance specification. The body of this specification, together with Supplement I, defines the prototype propulsion subsystem performance and method of calculation. The body of this specification, together with Supplement II, defines the production propulsion subsystem performance.
Download or read book Supersonic Transport Development Program Phase Iii Proposal Boeing Model 2707 Coordinated Inlet engine Test Plan general Electric written by BOEING CO SEATTLE WASH SUPERSONIC TRANSPORT DIV. and published by . This book was released on 1966 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt: A preliminary plan outlining the test program for the full-scale SST inlet and controller with the GE4/J5P engine is presented in this document. This plan will be prepared in greater detail as the B-2707 Program advances. The over-all scope of the test consists of the following two major test programs: Testing in the full-scale SST inlet and controller without the engine in the supersonic tunnel, and Testing the full-scale inlet/engine combination with flight-type inlet and engine control systems in the supersonic and transonic tunnels simulating, to the maximum degree possible, the B-2707 flight envelope.
Download or read book Supersonic Transport Development Program Phase Iii Proposal Boeing Model 2707 Training Equipment Specifications written by Lewis H. Gray and published by . This book was released on 1966 with total page 29 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification establishes the performance, design, test, and qualification requirements for the flight simulator of Boeing Model 2707 production airplane (B-2707). The simulator will be used for training flight crews in both ground and flight operations.
Download or read book Supersonic Transport Program Phase Ii c Report Air Induction Control Subsystem Specification Sst Boeing Model 2707 written by BOEING CO SEATTLE WA SUPERSONIC TRANSPORT DIV. and published by . This book was released on 1966 with total page 43 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification establishes the requirements for performance, design, test and qualification of one type of equipment identified as the Air Induction Control Subsystem (hereinafter called the control subsystem). 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 for each of the four inlets. The control subsystem effects changes in the geometry of the inlet centerbody and operates the bypass doors to provide efficient inlet airflow diffusion and high performance inlet-engine airflow match. The subsystems include necessary hydraulic power generation, distribution equipment, and flight deck controls and displays. Power from the airplane electrical system and from each of the engines is required by the subsystems in order to accomplish their intended missions. (Author).
Download or read book Supersonic Transport Program Phase Ii c Report Fuel Subsystem Specification Sst Boeing Model 2707 written by Stanley E. Lindstrom and published by . This book was released on 1966 with total page 37 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification establishes the requirements for performance design, test and qualification of the fuel system as applied to the prototype airplanes. This subsystem will provide for the storage, distribution and management of fuel. (Author).
Download or read book Commercial Supersonic Transport Program Phase Ii c Interim Aircraft Performance Assessment Report Engine Inlet Anti icing Performance Specification written by BOEING CO RENTON WA. and published by . This book was released on 1965 with total page 13 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification describes the engine inlet anti-icing system and establishes its requirements, and testing objectives. System performance requirements established herein are design objectives to be applied to the prototype airplanes. Application of these requirements to production airplane design will be determined after prototype flight testing.
Download or read book Commercial Supersonic Transport Program Phase Iib Report Engine Inlet Anti icing System Performance Specification written by BOEING CO RENTON WA. and published by . This book was released on 1965 with total page 12 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification describes the engine inlet anti-icing system and establishes its requirements and testing objectives. (Author).
Download or read book Technical Abstract Bulletin written by Defense Documentation Center (U.S.) and published by . This book was released on 1967 with total page 784 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book SUPERSONIC TRANSPORT DEVELOPMENT PROGRAM PHASE 3 PROPSAL BOEING MODEL 2707 VOLUME 2 8 AIRFRAME DESIGN REPORT PART D MATERIALS AND PROCESSES written by and published by . This book was released on 1966 with total page 223 pages. Available in PDF, EPUB and Kindle. Book excerpt: The materials and processes for the B-2707 have been evaluated by tests that reflect the new operational environment (defined in D6A10107-1) and incorporate improvements developed for subsonic airplanes. This document describes the materials and processes for the particular applications and the reasons for selection together with supporting data. Details of much of the development work leading to final selection of materials and processes are reported in the bimonthly progress reports D6-18110 and are not repeated in this document. Particular emphasis is placed on new materials and requirements. Those material applications with long history of satisfactory use on commercial and military airplanes are identified, but are not discussed in detail.
