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.


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    Title :

    Nacelle bifurcation with leading edge structure


    Contributors:

    Publication date :

    2020-09-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



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