A structure for the nacelle of an aircraft propulsion unit includes a first skin and stiffeners arranged to hold acoustic treatment modules against the first skin. Each acoustic treatment module includes a honeycomb core and a second skin, such that the honeycomb core is sandwiched between the first skin and the second skin. Such a structure allows the structural reinforcement function provided by the stiffeners to be separated from the acoustic treatment function performed by the acoustic treatment modules which are simply bearing on the first skin.


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    Titel :

    ACOUSTIC TREATMENT STRUCTURE FOR AN AIRCRAFT PROPULSION UNIT NACELLE


    Beteiligte:
    BOUILLON FLORENT (Autor:in) / DUPE FRANCK (Autor:in) / CARRERE BENOÎT (Autor:in) / DESJOYEAUX BERTRAND (Autor:in)

    Erscheinungsdatum :

    2020-10-29


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / F02K JET-PROPULSION PLANTS , Strahltriebwerke



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