A latch assembly for selectively preventing a relative movement between first and second components of an aircraft cabin monument, including a latch having a first connection member and a striker plate having a second connection member complementary to and selectively engageable with the first connection member. The engaged latch and striker plate in use are subjected to a load having a use threshold value and a decompression threshold value. The striker plate is designed to have a failure load higher than the use threshold value and lower than the decompression threshold value. The latch has a failure load higher than the use threshold value and higher than the decompression threshold value. A method of tailoring a failure of a latch assembly selectively preventing a relative movement between first and second components of an aircraft cabin monument is also discussed.


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    Titel :

    LATCH ASSEMBLY FOR AIRCRAFT MONUMENT


    Beteiligte:
    RICCI MICHAEL (Autor:in) / TANASE ANDREEA (Autor:in) / KONRAD WILFRIED (Autor:in)

    Erscheinungsdatum :

    2020-08-13


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    E05B LOCKS , Schlösser / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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