An aircraft nacelle air inlet comprising: a lip skin defining a curved surface of the inlet, the curved surface extending about a longitudinal axis of the inlet; a forward bulkhead; an inner barrel having a radially inner surface defining a surface of the inlet, a radially outer surface, and a sound attenuating layer arranged between the radially inner and radially outer surfaces; and a joining frame fixed to the lip skin and/or to the forward bulkhead. A first portion of the joining frame extends over at least a portion of the sound attenuating layer of the inner barrel and is fixed to the radially outer surface of the inner barrel.


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    Titel :

    AIRCRAFT NACELLE INLET


    Weitere Titelangaben:

    FLUGZEUGTRIEBWERKSGONDELEINLAUF
    ENTRÉE D'AIR DE NACELLE D'AVION


    Beteiligte:
    KIRK DAVID (Autor:in) / HILL GRAEME (Autor:in) / HEBDEN DAVID (Autor:in) / FURMSTON SIMON (Autor:in)

    Erscheinungsdatum :

    2024-04-24


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



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