An assembly is provided for an aircraft propulsion system. This aircraft propulsion system assembly includes a nacelle. The nacelle includes an inlet structure and a cowl. The inlet structure extends axially in a first direction along a centerline to an inlet structure aft end. The inlet structure includes a clip and a hoist bracket integrated with the clip. The clip is at the inlet structure aft end. The clip includes a locator receptacle. The hoist bracket is configured to provide a structural lift point for the inlet structure during assembly and/or disassembly of the nacelle. The cowl extends axially in a second direction along the centerline to a cowl forward end. The cowl includes a locator at the cowl forward end. The locator includes a protrusion received by the locator receptacle.


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    Title :

    NACELLE INLET STRUCTURE FITTING WITH LOCATOR CLIP AND HOIST BRACKET


    Contributors:

    Publication date :

    2023-11-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B66C Krane , CRANES



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