Control Concepts for a High Bypass Aircraft Turbofan Engine

Format:

Conference/Event

Author/Creator:

Evens, David A., author.

Conference Name:

National Air Transportation Meeting (1969-04-21 : New York, New York, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1969

Summary:

This paper examines the engine main fuel and geometry control design concepts and their relation to engine requirements for a large, high bypass, aircraft turbofan engine. This class of engine is representative of those powering the new "airbus" type aircraft which are currently under development. The functional design highlights of a simple, efficient, and compact control system are discussed and related to reliability, maintainability, and weight

Notes:

Vendor supplied data

Publisher Number:

690403

Access Restriction:

Restricted for use by site license