Lubricant Evaluation and Systems Design for Aircraft Gas Turbine Engines Rolls-Royce, Limited

Format:

Conference/Event

Author/Creator:

Edge, R. G., 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:

Design of the oil system of aircraft gas turbine engines must keep pace with the ever improving performance which results in temperatures within the engine being continually raised. It is necessary to prevent the increased temperatures from causing rapid deterioration of the oil or failures of the bearings. Some of the design features of the Rolls-Royce RB 211 which are relevant to this requirement are presented, together with methods used to evaluate and predict the performance of lubricants under operational conditions

Notes:

Vendor supplied data

Publisher Number:

690424

Access Restriction:

Restricted for use by site license