Gas turbine engine maintenance design objectives prerequisite to increased on-wing repair are cited and discussed; major engine sections need to be of modular construction, readily separable and replaceable on aircraft; module replacement time should not exceed that normally required to change engine; inspection access should be provided to determine adequately condition of installed module components, such as all stages of compressor and turbine as well as entire burner section; aim is to replace module only when its condition warrants removal; engine, as installed, should not interfere with inspection provisions.
Maintainability design requirements for future jet engines
SAE -- Paper
SAE Meeting ; 1967 Design
1967
5 pages
Conference paper
English
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Maintainability Design Requirements for Future Jet Engines
SAE Technical Papers | 1967
|DERIVATION OF MAINTAINABILITY REQUIREMENTS
SAE Technical Papers | 1963
|