A method for operating a gas turbine engine having a starter-electric generator driven by one of a plurality of shafts of the gas turbine engine is provided. The method includes determining a desired amount of thrust to be produced by the gas turbine engine, as well as a desired amount of electrical power to be generated by the starter-electric generator of the gas turbine engine. The method operates the gas turbine engine to produce the desired amount of thrust, while producing less than the desired amount of electrical power using the starter-electric generator. Producing less than the desired amount of electrical power using the starter-electric generator allows for the desired amount of thrust production, or allows for the desired amount of thrust production more quickly.


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    Title :

    GAS TURBINE ENGINE STALL MARGIN MANAGEMENT



    Publication date :

    2021-08-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H02P CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS , Steuern oder Regeln von elektrischen Motoren, elektrischen Generatoren, dynamoelektrischen Umformern



    GAS TURBINE ENGINE STALL MARGIN MANAGEMENT

    GEMIN PAUL ROBERT / ADIBHATLA SRIDHAR / RADUN ARTHUR VORWERK et al. | European Patent Office | 2017

    Free access

    Stall margin indication

    HOADLEY, ARTHUR W. / VANDERBOK, RAYMOND S. | AIAA | 1988


    Stall margin indication

    HOADLEY, A. / VANDERBOK, R. | AIAA | 1986


    Stall margin indicator development

    HOADLEY, A. / VANDERBOK, R. | AIAA | 1986


    Stall and Margin System

    L. Pauze / B. Howard | NTIS | 1966