An engine fastener includes a fixing assembly having a connection element provided with a shaft and holding two pins, which are configured to participate in the implementation of a fail-safe function, the fixing assembly including a shear pin surrounding the shaft of the connection element with a clearance , the shear pin being arranged between the two pins and being adjusted so as to be in contact with two joined fitting parts at a junction zone therebetween, the shaft of the connection element also being mounted with clearances relative to the two pins and the two fitting parts.


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    Titel :

    Aircraft engine fastener


    Beteiligte:
    DEFORET THOMAS (Autor:in) / WYSOCKI ARNOLD (Autor:in)

    Erscheinungsdatum :

    2016-12-27


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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