A nacelle assembly for a gas turbine engine includes an integrated afterbody mount case. The integrated afterbody mount case includes an outer ring and a plurality of spokes that extend radially inwardly from the outer ring. The outer ring includes a radially outer surface and a radially inner surface. The plurality of spokes are circumferentially disposed about the radially inner surface and extend radially inwardly from the radially inner surface.
Nacelle assembly having integrated afterbody mount case
28.11.2017
Patent
Elektronische Ressource
Englisch
Nacelle assembly having integrated afterbody mount case
Europäisches Patentamt | 2018
|Nacelle afterbody for jet engines Patent
NTRS | 1967
|