A gas turbine engine nacelle includes an inner skin surrounded by a radially outer skin. The inner skin terminates at an exhaust outlet. The outer skin terminates at a recess in the inner skin extending into a closed cavity under the outer skin.


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    Title :

    RECESSED ENGINE NACELLE


    Additional title:

    AUSGESPARTE TRIEBWERKSGONDEL
    CARTER-MOTEUR EN RETRAIT


    Contributors:

    Publication date :

    2016-09-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64C AEROPLANES , Flugzeuge



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