An electrically-powered downlock actuation system for a landing gear that does not convert rotary motor output into linear motion during the actuation process, but instead uses the rotary motor (214) output to directly drive a locking mechanism (200) coupled to upper and lower landing gear braces (202,204). The electrically-powered downlock actuation system (200) may include an electric motor (214), a gearbox (216) (optional), a clutch (optional) and a fixed link (220) to replace a hydraulically powered downlock actuation system. Further, the electrically-powered downlock actuation system (200) may be controlled with motor control electronics that cooperate with one or more sensors arranged to detect a position of an output shaft.


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    Titel :

    Electrically powered downlock actuation system


    Weitere Titelangaben:

    Elektrisch angetriebenes Sicherungsbetätigungssystem
    Système d'actionnement électrique de verrou


    Beteiligte:
    DITZLER ADAM (Autor:in)

    Erscheinungsdatum :

    2021-03-10


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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