An aircraft propulsion system assembly (48) includes a nacelle (22) having an inlet structure (32) and a cowl (34). The inlet structure (32) extends axially in a first direction along a centerline (26) to an inlet structure aft end (80). The inlet structure (32) includes a clip (100) and a hoist bracket (102) integrated with the clip (100). The clip (100) is at the inlet structure (32) aft end. The clip (100) includes a locator receptacle (118). The hoist bracket (102) is configured to provide a structural lift point for the inlet structure (32) during assembly and/or disassembly of the nacelle (22). The cowl (34) extends axially in a second direction along the centerline (26) to a cowl forward end (128). The cowl (34) includes a locator at the cowl forward end (128). The locator (120) includes a protrusion (130) received by the locator receptacle (118).


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    Titel :

    NACELLE INLET STRUCTURE FITTING WITH LOCATOR CLIP AND HOIST BRACKET


    Weitere Titelangaben:

    GONDELEINLASSSTRUKTURANPASSUNG MIT POSITIONSKLAMMER UND HEBEKLAMMER
    RACCORD DE STRUCTURE D'ENTRÉE DE NACELLE AVEC ATTACHE DE POSITIONNEMENT ET SUPPORT DE LEVAGE


    Beteiligte:

    Erscheinungsdatum :

    2023-10-11


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



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