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.
NACELLE INLET STRUCTURE FITTING WITH LOCATOR CLIP AND HOIST BRACKET
02.11.2023
Patent
Elektronische Ressource
Englisch
Nacelle inlet structure fitting with locator clip and hoist bracket
Europäisches Patentamt | 2024
|NACELLE INLET STRUCTURE FITTING WITH LOCATOR CLIP AND HOIST BRACKET
Europäisches Patentamt | 2023
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