An assembly is provided for an aircraft propulsion system. The assembly includes a tubular inner housing, a tubular outer housing and a bifurcation. The bifurcation includes a leading edge structure structurally connected to the inner housing and the outer housing.
NACELLE BIFURCATION WITH LEADING EDGE STRUCTURE
2018-08-02
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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