An assembly (54) is provided for an aircraft propulsion system. This assembly (54) includes a nacelle inlet structure (34) extending axially along and circumferentially about an axis (28). The nacelle inlet structure (34) includes an inlet lip (62), an inner barrel (58), an outer barrel (60) and a plurality of supports (66, 142A). The inlet lip (62) forms a leading edge (86) of the nacelle inlet structure (34). The inner barrel (58) projects axially aft away from the inlet lip (62). The outer barrel (60) projects axially aft away from the inlet lip (62). The outer barrel (60) is radially outboard of and axially overlaps the inner barrel (58). The supports (66, 142A) are arranged circumferentially about the axis (28) in an array. Each of the supports (66, 142A) extends longitudinally along the axis (28). Each of the supports (66, 142A) extends radially between and is connected to the inner barrel (58) and the outer barrel (60).
OUTER BARREL SUPPORT STRUCTURE FOR NACELLE INLET STRUCTURE
AUSSENZYLINDERSTÜTZSTRUKTUR FÜR GONDELEINLASSSTRUKTUR
STRUCTURE DE SUPPORT DE TUBE EXTERNE POUR STRUCTURE D'ENTRÉE DE NACELLE
2025-02-12
Patent
Electronic Resource
English
Outer barrel support structure for nacelle inlet structure
European Patent Office | 2025
|OUTER BARREL SUPPORT STRUCTURE FOR NACELLE INLET STRUCTURE
European Patent Office | 2025
|