A method of monitoring a gas turbine engine includes the steps of: (a) receiving information from actual flights of an aircraft including an engine to be monitored, and including at least one of the ambient temperature at takeoff, and internal engine pressures, temperatures and speeds; (b) evaluating the damage accumulated on an engine component given the data received in step (a); (c) storing the determined damage from step (b); (d) repeating steps (a)-(c); (e) recommending a suggested future use for the component based upon steps (a)-(d). A system is also disclosed.


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    Titel :

    Gas Turbine Engine with Lifing Calculations Based Upon Actual Usage


    Beteiligte:
    SCHWARZ FREDERICK M (Autor:in) / RIZO MARNIE A (Autor:in) / HOUSTON DAVID P (Autor:in) / NISSLEY DAVID M (Autor:in) / HIESTER PAUL J (Autor:in) / DALE TIMOTHY (Autor:in) / WINFIELD TIMOTHY B (Autor:in) / CAMPBELL MADELINE N (Autor:in) / MIDGLEY JAMES R (Autor:in)

    Erscheinungsdatum :

    23.11.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G01M TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES , Prüfen der statischen oder dynamischen Massenverteilung rotierender Teile von Maschinen oder Konstruktionen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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