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
2024-01-23
Patent
Electronic Resource
English
NACELLE INLET STRUCTURE FITTING WITH LOCATOR CLIP AND HOIST BRACKET
European Patent Office | 2023
|NACELLE INLET STRUCTURE FITTING WITH LOCATOR CLIP AND HOIST BRACKET
European Patent Office | 2023
|