Herein provided are methods and systems for a method for controlling autothrottle of an engine (150). A digital power request is obtained from an autothrottle controller (204), the digital power request based on an autothrottle input (203) to the autothrottle controller (204). A manual input mode for the engine (150) is terminated, the manual input mode based on a second power request obtained from a manual input (202) associated with the engine (150). An autothrottle mode for the engine (150) is engaged to control the engine (150) based on the digital power request.


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    Title :

    AUTOTHROTTLE CONTROL SYSTEM ON TURBOPROPELLER-POWERED AIRCRAFT


    Additional title:

    SELBSTDROSSELNDES STEUERSYSTEM AN TURBOPROPELLERGETRIEBENEN FLUGZEUGEN
    SYSTÈME DE COMMANDE D'AUTOMANETTE SUR UN AÉRONEF ALIMENTÉ PAR TURBOPROPULSEUR


    Contributors:

    Publication date :

    2025-06-11


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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