A nacelle for a turbofan engine includes a fan case, an inner barrel and a nose lip generally concentrically disposed about an axis. The inner barrel projects forward from and is engaged to the fan case at a first split line. The nose lip is engaged to the inner barrel at a second split line, and extends substantially radially outward directly from the second split line, then substantially axially rearward to the fan cowl as one unitary piece.


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    Title :

    Inlet assembly for a turbofan engine


    Contributors:

    Publication date :

    2018-12-25


    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



    INLET ASSEMBLY FOR A TURBOFAN ENGINE

    CRAWFORD SARA CHRISTINE | European Patent Office | 2017

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    Turbofan engine assembly methods

    COFFIN JAMES B / PESCOSOLIDO ALESSIO | European Patent Office | 2018

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