An aspect includes a variable cycle system of a gas turbine engine. The variable cycle system includes an actuation system, an electric component, and a controller. The actuation system is configured to adjust a variable cycle of turbomachinery of the gas turbine engine. The electric component is operable to provide a shaft power supply or a load corresponding respectively to an adjustment of the turbomachinery. The controller is operable to adjust an output of either or both of the actuation system and the electric component for separate control of thrust and cycle responses.


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    Titel :

    VARIABLE CYCLE COMPENSATION IN A GAS TURBINE ENGINE


    Beteiligte:
    TERWILLIGER NEIL (Autor:in) / BENGEA SORIN (Autor:in)

    Erscheinungsdatum :

    12.03.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES



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    VARIABLE CYCLE COMPENSATION IN A GAS TURBINE ENGINE

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    Turbine engine variable cycle selection program summary

    Glaser, F.C. / Weber, W.B. | Tema Archiv | 1977


    Turbine Engine Variable Cycle Selection Program Summary

    F. C. Glaser / W. B. Weber | NTIS | 1977