Author: BOEING CO RENTON WA.Publisher:
ISBN:
Category :
Languages : en
Pages : 15
Book Description
Airframe/engine Compatibility Plan. Pratt and Whitney Engine. Commercial Supersonic Transport Program. Phase Ii-c Report
Author: BOEING CO RENTON WA.Publisher:
ISBN:
Category :
Languages : en
Pages : 15
Book Description
Airframe/engine Compatibility Plan. General Electric Engine. Commercial Supersonic Transport Program. Phase Ii-c Report
Author: BOEING CO RENTON WA.Publisher:
ISBN:
Category :
Languages : en
Pages : 20
Book Description
Technical Abstract Bulletin
Author: Publisher:
ISBN:
Category : Science
Languages : en
Pages : 828
Book Description
Supersonic Transport Program. Phase Ii-c Report. Propulsion Subsystem Specification. Pratt and Whitney Aircraft, Sst Boeing Model 2707
Author: Paul E. JohnsonPublisher:
ISBN:
Category :
Languages : en
Pages : 52
Book Description
This specification establishes the requirements for the performance, test and qualification of the B-2707 (P and W) propulsion subsystem. The Pratt and Whitney JTF17A-20B engine performance data is the primary data for the propulsion subsystem performance specification. Subsystem performance requirements established herein are design objectives for the prototype airplane. Application of these requirements to production airplane design will be established after prototype flight testing and evaluation.
Commercial Supersonic Transport Program. Phase Ii-c. Interim Aircraft Performance Assessment Report. Model Specification. Section Ii. Performance Guarantees
Author: BOEING CO RENTON WA.Publisher:
ISBN:
Category :
Languages : en
Pages : 18
Book Description
This document describes the performance guarantees for the Boeing Model 733-390 powered by General Electric engines, the Model 733-394 powered by Pratt and Whitney engines, and the 733 prototype airplane.
Commercial Supersonic Transport Program. Phase Ii-c. Interim Aircraft Performance Assessment Report. Aircraft Engine Installation Performance Specification
Author: BOEING CO RENTON WA.Publisher:
ISBN:
Category :
Languages : en
Pages : 35
Book Description
This specification describes the aircraft engine installation. The essential physical and functional characteristics are noted and the design requirements are specified in some detail. Ground and flight tests which will ensure that the installation is satisfactory are established. The specific engine installation covered is the GE4/J5G. (Author).
Supersonic Transport Development Program. Phase 3 Proposal. Boeing Model 2707. Volume 2-14. Propulsion Report - Part C. Engine Evaluation
Author: BOEING CO SEATTLE WA SUPERSONIC TRANSPORT DIV.Publisher:
ISBN:
Category :
Languages : en
Pages : 117
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.
Supersonic Transport Aircraft Engine. Phase Ii-b. Development Program Fuel Control System Study. Appendix B
Author: PRATT AND WHITNEY AIRCRAFT GROUP EAST HARTFORD CT.Publisher:
ISBN:
Category :
Languages : en
Pages : 164
Book Description
Hamilton Standard, under contract to Pratt and Whitney Aircraft, has conducted a design and development study to conceive and optimize, within contract and time limitations, a fuel control system for the P and WA SST engine. This effort consisted of design and analytical studies, material investigations, and development efforts necessary to adapt current state-of-the-art concepts and new concepts into a fuel control system compatible with the SST environments, envelope requirements, and accuracy tolerances specified for this application. The system decided upon and studied is a hydromechanical unitized concept featuring high reliability, ease of maintenance, durability, and low overall system weight. This report covers all studies conducted under Phase 2 B of the contract for the fuel control system as well as Hamilton Standard funded elastomeric seal development work.
Commercial Supersonic Transport Program. Phase Ii-c. Interim Aircraft Performance Assessment Report. Engine Inlet Anti-icing Performance Specification
Author: BOEING CO RENTON WA.Publisher:
ISBN:
Category :
Languages : en
Pages : 13
Book Description
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.
Commercial Supersonic Transport Program. Phase Ii-c. Interim Aircraft Performance Assessment Report. Systems
Author: BOEING CO RENTON WA.Publisher:
ISBN:
Category :
Languages : en
Pages : 52
Book Description
Substantial progress has been made in all systems development essentially as outlined in the Phase II-B and II-C plans. Because of their relative importance and sensitivity to variations in airplane configuration and their effect on performance, only the development of flight control systems and flight deck vision is reported. (Author).
