A nacelle assembly (35) for a gas turbine engine includes an integrated afterbody mount case (62). The integrated afterbody mount case (62) includes an outer ring (66) and a plurality of spokes (68) that extend radially inwardly from the outer ring (66). The outer ring (66) includes a radially outer surface (70) and a radially inner surface (72). The plurality of spokes (68) are circumferentially disposed about the radially inner surface (72) and extend radially inwardly from the radially inner surface (72).
Nacelle assembly having integrated afterbody mount case
Triebwerksgondel mit integrierter Abstützung der Schubdüse
Nacelle avec support intégral du carter d'échappement
2018-07-11
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |