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.


    Access

    Download


    Export, share and cite



    Title :

    Variable cycle compensation in a gas turbine engine


    Contributors:

    Publication date :

    2021-11-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    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



    Variable cycle compensation in a gas turbine engine

    TERWILLIGER NEIL / BENGEA SORIN | European Patent Office | 2024

    Free access

    VARIABLE CYCLE COMPENSATION IN A GAS TURBINE ENGINE

    TERWILLIGER NEIL / BENGEA SORIN | European Patent Office | 2022

    Free access

    VARIABLE CYCLE COMPENSATION IN A GAS TURBINE ENGINE

    TERWILLIGER NEIL / BENGEA SORIN | European Patent Office | 2020

    Free access

    Turbine engine variable cycle selection program summary

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


    Turbine Engine Variable Cycle Selection Program Summary

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