A fuel control system for an aircraft engine, comprises a fuel feed conduit including an inlet end and an outlet end. A fuel metering mechanism is disposed in the fuel feed conduit between the inlet end and the outlet end operable to regulate flow through the fuel feed conduit. A position feedback sensor is operatively connected to the fuel metering mechanism and operable to generate a signal indicative of a position of the fuel metering mechanism.


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    Title :

    CONTROLLING GASEOUS FUEL FLOW


    Additional title:

    CONTROLE DU FLUX DE CARBURANT GAZEUX


    Contributors:
    LU XUENING (author) / MESHKINFAM EZZAT (author) / DURAND SEAN (author)

    Publication date :

    2023-01-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



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