A gas turbine engine inlet door control system includes an actuator, an engine controller and a door controller. The actuator opens and closes an inlet door of a gas turbine engine. The engine controller determines an intermediate door position based upon one or more engine start factors. The door controller operates the actuator to open the inlet door to the intermediate door position based on the one or more engine start factors.


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    Title :

    INLET DOOR CONTROL FOR STARTUP OF GAS TURBINE ENGINE


    Additional title:

    EINLASSKLAPPENSTEUERUNG FÜR DAS ANLAUFEN EINES GASTURBINENMOTORS
    COMMANDE DE PORTE D'ENTRÉE POUR LE DÉMARRAGE D'UN MOTEUR A TURBINE A GAZ


    Contributors:

    Publication date :

    2019-01-02


    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 / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



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