A nacelle assembly (35) for a gas turbine engine includes an integrated afterbody mount case (62). The integrated afterbody mount case (62) includes an outer ring (66) and a plurality of spokes (68) that extend radially inwardly from the outer ring (66). The outer ring (66) includes a radially outer surface (70) and a radially inner surface (72). The plurality of spokes (68) are circumferentially disposed about the radially inner surface (72) and extend radially inwardly from the radially inner surface (72).


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    Title :

    Nacelle assembly having integrated afterbody mount case


    Additional title:

    Triebwerksgondel mit integrierter Abstützung der Schubdüse
    Nacelle avec support intégral du carter d'échappement


    Contributors:

    Publication date :

    2018-07-11


    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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