In order to reduce the risks of movable nacelle cowlings opening, the invention provides a nacelle (11) for an aircraft engine assembly (1) comprising a fixed nacelle structure (42) as well as at least one jointed movable cowling (38) on the fixed structure (42), the cowling (38) being jointed at its front end (38a) on the fixed structure so that, upon closing the movable cowling, a rear end (38b) of this cowling moves towards the rear and radially towards the inside.


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    Titel :

    NACELLE FOR AN AIRCRAFT ENGINE ASSEMBLY COMPRISING AT LEAST ONE JOINTED NACELLE COWLING AT ITS FRONT END


    Beteiligte:

    Erscheinungsdatum :

    2016-09-15


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / F02K JET-PROPULSION PLANTS , Strahltriebwerke



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