An assembly is provided for an aircraft propulsion system (10). The assembly includes a fixed structure (27), an inner cowl door (32) and an outer cowl door (40). The inner cowl door (32) is pivotally connected to the fixed structure (27). The outer cowl door (40) is pivotally connected to the fixed structure (27). The outer cowl door (40) is radially outboard of and overlaps the inner cowl door (32). A linkage (46) extends between and is movably connected to the inner cowl door (32) and the outer cowl door (40).


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    Title :

    LINKAGE(S) BETWEEN INNER AND OUTER COWL DOORS


    Additional title:

    VERBINDUNG(EN) ZWISCHEN INNERER UND ÄUSSERER TRIEBWERKSVERKLEIDUNG
    LIAISON(S) ENTRE DES PORTES DE CAPOT INTERNES ET EXTERNES


    Contributors:
    PRETTY SEAN (author) / LINDE ERIK (author) / BELL MARTIN C (author) / RAMLAOUI JIHAD (author)

    Publication date :

    2024-05-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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