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F100 engine diagnostic system status to dateAn engine diagnostic system, proposed for the F100 engine, was tested in five specially modified Tactical Air Command F-15 aircraft during a 16-month flight evaluation. After more than 3300 engine operating hours encompassing almost 900 flights during the flight evaluation, these aircraft provided a data base, still being analyzed, that has shown successful demonstration of the original functional characteristics. Four general design requirements, recording engine operating time/low cycle fatigue event detection, engine trim, and trend and performance data collection were demonstrated. Also, validation of maintenance actions taken and indicated needed maintenance were successfully demonstrated.
Document ID
19810022668
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Boyless, J. A.
(Air Force Systems Command Wright-Patterson AFB, OH, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1981
Publication Information
Publication: NASA. Lewis Res. Center Aircraft Engine Diagnostics
Subject Category
Aircraft Propulsion And Power
Accession Number
81N31210
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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