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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    Titel :

    LINKAGE(S) BETWEEN INNER AND OUTER COWL DOORS


    Weitere Titelangaben:

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


    Beteiligte:
    PRETTY SEAN (Autor:in) / LINDE ERIK (Autor:in) / BELL MARTIN C (Autor:in) / RAMLAOUI JIHAD (Autor:in)

    Erscheinungsdatum :

    29.05.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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