Patent ID: 11878808
Assignee: ROHR, INC.
Field: Transport (Mechanical engineering)
Classification: CPC B  F | IPC B  F

Claim 18:
19. An assembly for an aircraft propulsion system, comprising:
a nacelle inlet structure extending axially along a centerline between a forward end and an aft end, the nacelle inlet structure including an inlet lip, an inner barrel, an outer barrel, a bulkhead and a fitting;
the inlet lip at the forward end;
the inner barrel connected to the inlet lip;
the outer barrel connected to the inlet lip and circumscribing the inner barrel;
the bulkhead extending radially between and connected to the inner barrel and the outer barrel; and
the fitting at the aft end and connected to the bulkhead, the fitting including a locator clip and a hoist bracket, the locator clip comprising a receptacle configured to receive a locator for a nacelle cowl, and the hoist bracket configured to provide a structural lift point for connecting to a hoist system during nacelle assembly and/or nacelle disassembly.