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.


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    Title :

    A NACELLE ASSEMBLY


    Additional title:

    GONDELANORDNUNG
    ENSEMBLE DE NACELLE


    Contributors:

    Publication date :

    2021-11-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    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



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