A method of controlling thrust for a gas turbine engine of an aircraft is provided. The method includes determining a fan speed required for minimum thrust to achieve an aircraft operation. The method also includes determining an excess amount of thrust generated by the gas turbine engine. The method also includes reducing the amount of thrust generated by the gas turbine engine.


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    Title :

    Aircraft power setting trims for life extension


    Contributors:

    Publication date :

    2019-03-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64C AEROPLANES , Flugzeuge



    AIRCRAFT POWER SETTING TRIMS FOR LIFE EXTENSION

    SOBANSKI KURT J / MEISNER RICHARD P / BENGTSON ROBERT J | European Patent Office | 2019

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