A thrust control assembly (10) includes a balk application arrangement which provides, in response to a received balk command to prohibit command of thrust in a balk direction, a balk force on a rotatable thrust lever (12) acting to oppose an attempt by the pilot to move the lever (129 in a direction so as to command or increase thrust in the balk direction. The balk application arrangement controls an auto-throttle actuator (20) to provide the balk force on the thrust lever (12).


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    Title :

    УСТРОЙСТВО УПРАВЛЕНИЯ ТЯГОЙ


    Publication date :

    2021-05-11


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Russian


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / F02K JET-PROPULSION PLANTS , Strahltriebwerke



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