Installation Effects on the CF6-50 in the YC-14 Aircraft Aircraft Engine Group, Div., General Electric Company

Format:

Conference/Event

Author/Creator:

Tuten, Richard K., author.

Conference Name:

National Air Transportation Meeting (1975-05-06 : Hartford, Connecticut, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1975

Summary:

Design of the YC-14 over-the-wing nacelle, utilizing the CF6-50D engines, presented unique engine installation conditions which have been accommodated with very minor impact to the baseline commercial engine design. Major installation features which affect the engine are reviewed including engine mounting, engine/aircraft deflections and nacelle sealing, effect of the confluent-flow exhaust nozzle on engine cycle matching, and inlet/thrust reverser/engine compatibility. Design solutions and planned testing to evaluate the installation are discussed

Notes:

Vendor supplied data

Publisher Number:

750607

Access Restriction:

Restricted for use by site license