A method of assembling a nacelle for a gas turbine engine that includes an inlet end, an exhaust end, and an axis that extends through the engine from the inlet end through the exhaust end is provided. The method includes providing a cowl sized to cover at least a portion of the engine and coupling the cowl to the engine such that the cowl is slideable along the axis toward at least one of the inlet end and the exhaust end.


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    Titel :

    NACELLE AND METHOD OF ASSEMBLING THE SAME


    Weitere Titelangaben:

    GONDEL UND MONTAGEVERFAHREN DAFÜR
    NACELLE ET PROCÉDÉ D'ASSEMBLAGE DE CELLE-CI


    Beteiligte:
    HOWARTH GRAHAM F (Autor:in) / CALDER DAVID P (Autor:in)

    Erscheinungsdatum :

    2017-04-05


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



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