The invention relates to a locking system (801) for an aircraft nacelle comprising a first portion (803), intended to be mounted on a first part (703) of an aircraft nacelle, and a second portion (809), intended to be mounted on a second part (709) of the aircraft nacelle. The locking system (801) is configured such that, when it is in the closed position, the first portion (803) and the second portion (809) are held together. It comprises at least one buffer part (815) and a load sensor (817) joined together and configured to compress the load sensor (817) between the buffer part (815) and another part (807) of the locking system (801) when it is in the closed position.


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    Title :

    SYSTEME DE VERROUILLAGE POUR NACELLE D'AERONEF


    Additional title:

    LOCKING SYSTEM FOR AN AIRCRAFT NACELLE
    VERRIEGELUNGSSYSTEM FÜR EINE FLUGZEUGGONDEL



    Publication date :

    2024-05-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

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



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