An assembly is provided for an aircraft propulsion system. This assembly includes a nacelle inlet structure, a thrust reverser and a fan cowl. The thrust reverser includes a forward portion and a translating sleeve. The fan cowl is axially between the nacelle inlet structure and the translating sleeve. The fan cowl axially covers the forward portion of the thrust reverser. The fan cowl is axially structurally tied to the nacelle inlet structure. The fan cowl is radially and circumferentially structurally tied to the forward portion of the thrust reverser.


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    Titel :

    Fan cowl mounted to thrust reverser


    Beteiligte:

    Erscheinungsdatum :

    30.06.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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