An 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.


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    Titel :

    F100 engine diagnostic system status to date


    Beteiligte:
    Boyless, J. A. (Autor:in)


    Erscheinungsdatum :

    01.01.1981


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    F100 engine diagnostic system status to date

    BOYLESS, J. / BUTTS, D. | AIAA | 1981


    F15/F100 engine diagnostic system

    SPETH, R. / SCOTT, B. / ROMOSER, B. | AIAA | 1979


    F100 Engine Diagnostic System (EDS) - Summary of results

    BOYLES, J. A. / BUTTS, D. C. | AIAA | 1984


    The F100 Engine

    Lancaster, Lanny T.G. / Eshbach, Russel E. | SAE Technical Papers | 1980