A locking mechanism includes a linkage assembly having a first link (6a) and a second link (6b) joined at a pivot point (110). The assembly also includes a linkage assembly spring to bias the linkage assembly into a first, locked, position and a rotational rod (1) having a cam (120) formed thereon with a cam surface in engagement with the linkage assembly in the region of the pivot point (110). The assembly also includes a solenoid assembly (3) arranged, in a first mode, to rotate the rotational rod (1) such that the cam acts as a stop against the linkage assembly at the pivot point in a locked position, and, in a second mode to rotate the rotational rod such that the cam surface presses against the linkage assembly sufficiently to overcome the linkage assembly spring and to force the linkage assembly into a second, unlocked position.


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    Title :

    LOCKING AND UNLOCKING MECHANISM


    Contributors:

    Publication date :

    2020-11-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F15B SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL , Druckmittelbetriebene Systeme allgemein



    LOCKING AND UNLOCKING MECHANISM

    SOBOLAK PIOTR / PAWELEC IZABEL | European Patent Office | 2019

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    LOCKING AND UNLOCKING MECHANISM

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    LOCKING AND UNLOCKING MECHANISM

    SOBOLAK PIOTR / PAWELEC IZABELA | European Patent Office | 2019

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    LOCKING AND UNLOCKING MECHANISM

    SOBOLAK PIOTR / PAWELEC IZABELA | European Patent Office | 2017

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    Locking and unlocking mechanism

    SOBOLAK PIOTR / PAWELEC IZABELA | European Patent Office | 2020

    Free access