A thrust reverser (130) of a nacelle (100) may include an translating sleeve (134) and an inner fixed structure (132) a pressure relief assembly (420). A pressure relief mechanism may include a pressure relief door (522) coupled via a hinge (524) and a latch (622) to the inner fixed structure (132). The pressure relief assembly (420) may limit deflections between the thrust reverser (134) and a pylon (140) in response to a burst duct. The pressure relief door (522) may release from the latch (622) automatically in response to an over pressurization event.


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    Title :

    PRESSURE RELIEF ASSEMBLY


    Additional title:

    DRUCKENTLASTUNGSANORDNUNG
    ENSEMBLE DE DÉCHARGE DE PRESSION


    Contributors:

    Publication date :

    2022-08-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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