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Diagnostics of wear in aeronautical systemsThe use of appropriate diagnostic tools for aircraft oil wetted components is reviewed, noting that it can reduce direct operating costs through reduced unscheduled maintenance, particularly in helicopter engine and transmission systems where bearing failures are a significant cost factor. Engine and transmission wear modes are described, and diagnostic methods for oil and wet particle analysis, the spectrometric oil analysis program, chip detectors, ferrography, in-line oil monitor and radioactive isotope tagging are discussed, noting that they are effective over a limited range of particle sizes but compliment each other if used in parallel. Fine filtration can potentially increase time between overhauls, but reduces the effectiveness of conventional oil monitoring techniques so that alternative diagnostic techniques must be used. It is concluded that the development of a diagnostic system should be parallel and integral with the development of a mechanical system.
Document ID
19790055792
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wedeven, L. D.
(NASA Lewis Research Center Cleveland, Ohio, United States)
Date Acquired
August 9, 2013
Publication Date
June 1, 1979
Subject Category
Mechanical Engineering
Meeting Information
Meeting: American Chemical Society, State-of-the-Art Symposium on Corrosion and Wear
Location: Washington, DC
Start Date: June 4, 1979
End Date: June 6, 1979
Sponsors: American Chemical Society
Accession Number
79A39805
Distribution Limits
Public
Copyright
Other

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