Disclosed is an actuator for varying the position of a flight control surface on an aircraft, wherein the actuator comprises a no-back device (10) including a backlash adjuster, which is arranged to select a plurality of different backlash lengths. The backlash adjuster may be a nut (20) which moves relative a housing of the no-back device (10) by rotating the nut (20). Also disclosed is a method of adjusting the backlash (B) in a flight control surface actuator, by moving the backlash adjuster axially to adjust the backlash (B) to a desired value.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    УСТРОЙСТВО БЛОКИРОВКИ ОБРАТНОГО ХОДА ДЛЯ ПРИВОДА РУЛЯ УПРАВЛЕНИЯ ПОЛЕТОМ


    Erscheinungsdatum :

    13.10.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Russisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge