The present disclosure relates generally to a fan nacelle assembly (62) circumferentially surrounding a fan section (22), the fan nacelle assembly including an inner wall (82) including an inner wall axial length (87), and an outer wall (88) including an outer wall axial length (94), wherein the outer wall axial length is greater than the inner wall axial length.
A NACELLE ASSEMBLY
GONDELANORDNUNG
ENSEMBLE DE NACELLE
2021-11-03
Patent
Elektronische Ressource
Englisch
IPC: | F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS |
Assembly for nacelle of aircraft, nacelle and aircraft comprising such assembly
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