An example method includes: determining a throttle command for a servomotor configured to control a position of a throttle lever, where the position of the throttle lever indicates a commanded thrust for the first engine of the aircraft; determining a trim command for the first engine to equalize the thrust of the first engine with the respective thrust of the second engine; determining that a magnitude of the throttle command is less than a magnitude of a threshold throttle command indicative of a dead zone of the servomotor, where the servomotor is irresponsive to a given throttle command within the dead zone; modifying the trim command based on the throttle command to generate a modified trim command that compensates for irresponsiveness of the servomotor to the throttle command; and changing the thrust generated by the first engine based on the modified trim command.


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    Titel :

    LOW THROTTLE RATE COMMAND COMPENSATION VIA FULL AUTHORITY ENGINE TRIM


    Weitere Titelangaben:

    FEINKOMPENSATION DES TRIEBWERKLEISTUNGSSTEUERUNGSSIGNALS DURCH FADEC-TRIMMEINGABE
    RÉGLAGE FIN DU SIGNAL DE COMMANDE DE VITESSE PAR LE BIAIS D'UN TRIM DE LA POUSSÉE MOTEUR MOYENNANT LE FADEC


    Beteiligte:

    Erscheinungsdatum :

    2022-01-12


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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