A toggle release mechanism (100) comprises a base element (102), a toggle element (104) and an actuating rod (142). The toggle element (104) is rotatably mounted at a first end (112) to the base element (102) about a first axis (114) for rotation between a first, locking position and a second, release position. The actuating rod (142) has a central portion (144) extending through the toggle element (104) and first and second end portions (146, 148) projecting on opposed sides thereof for engagement with actuators (154) arranged on opposed sides of the release mechanism (100). The actuating rod (142) further comprises a mounting flange (156) projecting therefrom at a boundary between the central portion (144) and a first end portion (146). The mounting flange (156) has a first hole (158) therein for receiving a first fastener (160). A surface (162) of the toggle element (104) facing the mounting flange (156) has a bore (164) formed therein for receiving the first fastener (160). The mechanism further comprises a mounting element (166) slidably received on the second end (148) of the actuating rod (142). The mounting element (166) has a bore (168) for receiving the second end (148) of the actuator rod (142) and a second hole (170) for receiving a second fastener (176). A surface (174) of the toggle element (104) facing the mounting element (166) having a second bore (176) formed therein for receiving the second fastener (172).


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    Titel :

    RELEASE MECHANISM


    Weitere Titelangaben:

    AUSLÖSEMECHANISMUS
    MÉCANISME DE LIBÉRATION


    Beteiligte:

    Erscheinungsdatum :

    2022-04-06


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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