An aircraft propulsion assembly has a hinge for articulating a first and a second of its panels. The hinge includes a yoke rigidly connected to the first panel and a counter-yoke rigidly connected to the second panel, which is received between two lugs of the yoke. The yoke and the counter-yoke are passed through by a hinge pin that is movable between an extended position between the lugs of the yoke and a retracted position outside the yoke. The hinge further includes bayonet mounting means interposed between the pin and the yoke.


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    Title :

    CHARNIERE D'ARTICULATION ENTRE DEUX PANNEAUX D'UN ENSEMBLE PROPULSIF D'AERONEF


    Additional title:

    HINGE FOR ARTICULATING TWO PANELS OF AN AIRCRAFT PROPULSION ASSEMBLY
    SCHARNIER ZUR GELENKIGEN VERBINDUNG ZWEIER PLATTEN EINER FLUGZEUGANTRIEBSANORDNUNG


    Contributors:

    Publication date :

    2023-02-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    F16C SHAFTS , Wellen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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