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Modular Engine Maintenance Concept Considerations for Aircraft Turbine Engines

David B. Edmunds (Propulsion Performance Division, Wright‐Patterson Air Force Base)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 January 1978

3436

Abstract

Maintenance on gas turbine engines results from failures in one or more of the engine's major subsections. Maintenance and support costs can be reduced if the capability exists to isolate the failures down to the lowest possible component in the engine. The modular engine maintenance concept has recently been evolved to facilitate this cost reduction. The important considerations as well as the benefits of this concept are discussed. Considerations included are: design, failure modes and isolation techniques, and implementation. The Air Force F100‐PW‐100 engine maintenance concept is used for discussion purposes.

Citation

Edmunds, D.B. (1978), "Modular Engine Maintenance Concept Considerations for Aircraft Turbine Engines", Aircraft Engineering and Aerospace Technology, Vol. 50 No. 1, pp. 14-17. https://doi.org/10.1108/eb035417

Publisher

:

MCB UP Ltd

Copyright © 1978, MCB UP Limited

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