Fuel Control System of The GE4 Engine for The Supersonic Transport

Format:

Conference/Event

Author/Creator:

Moehring, John T., author.

Conference Name:

National Aeronautic Meeting and 3rd International Simulation and Training Conference (1967-04-24 : New York, New York, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1967

Summary:

The design of the power control and fuel systems for the augmented turbojet engine selected to power the United States supersonic transport combines proved designs with technical innovation to strike a design balance meeting all the requirements for commercial airline service. Application of the integrated three-variable power control principles long in production for supersonic military service will ensure a successful transition from the simpler, single-variable power controls operating at subsonic conditions in today's airlines. The overall power control system operation of the General Electric GE4 engine is presented followed by a more detailed account of the main and augmentation fuel and control subsystems. System design and component mechanization are shown and related to the factors that influenced the design

Notes:

Vendor supplied data

Publisher Number:

670326

Access Restriction:

Restricted for use by site license