A control system (20) for controlling pitching stabilizer means of an aircraft, said system (20) being provided with at least one outlet shaft (21) and with a first actuator (31) and a second actuator (36). The first and second actuators (31 and 36) are different, and the first actuator (31) is a slow actuator having a first driving portion that moves at a first speed, the second actuator (36) being a fast actuator having a second driving portion that moves at a second speed faster than the first speed, said control system (20) comprising a control device (50) connected to the first actuator (31) and to the second actuator (36) in order to cause said outlet shaft (21) to be driven either by the first driving portion (32) and/or by the second driving portion (37).


    Access

    Download


    Export, share and cite



    Title :

    System and a method for controlling pitching stabilizer means of an aircraft


    Contributors:

    Publication date :

    2017-05-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F16H Getriebe , GEARING / B64C AEROPLANES , Flugzeuge



    Computer system configured to actuate pitching motion stabilizer

    LUNDIN NILS | European Patent Office | 2024

    Free access

    Pitching stabilization means and a rotary wing aircraft including such means

    GATTI JEAN-LOUP / ARNAUD REMY-ELIAN | European Patent Office | 2016

    Free access

    AIRCRAFT STABILIZER

    HOUSER PETER BENNETT / LAVIGNE JESSICA MARIE | European Patent Office | 2019

    Free access

    Engine pitching adjusting suspension structure, aircraft power system and aircraft

    ZHANG XUEHU | European Patent Office | 2024

    Free access

    The pitching vibrations of an aircraft

    Morris, J. / Green, G. S. | TIBKAT | 1948