A method of controlling a propulsion system of an aircraft, the propulsion system comprising a gas turbine engine arranged to be powered by a fuel and at least one variable inlet guide vane—VIGV, comprises obtaining at least one fuel characteristic of the fuel being provided to the gas turbine engine; and making a change to scheduling of the at least one VIGV based on the at least one obtained fuel characteristic.


    Access

    Download


    Export, share and cite



    Title :

    Variable inlet guide vanes


    Publication date :

    2023-01-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English



    Constant swirl angle inlet guide vanes

    ANDRES, RICHARD M. | AIAA | 1990


    Failure Analysis of Inlet Guide Vanes

    Mcalpin, R.L. | Online Contents | 2003


    Sealing variable guide vanes

    COUTU DANIEL | European Patent Office | 2022

    Free access