An acoustic panel for an aircraft comprising: a sound attenuating sheet having a plurality of cavities, a sound attenuating sheet having a first surface, a second surface opposite to the first surface and an end surface connecting the first and second surfaces, a first sheet extending over at least a portion of the first surface and over the end surface, and a second sheet extending over the second surface and the end surface, wherein the first and the second sheets are connected such that a tensile force can be transferred therebetween.


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    Titel :

    Acoustic panel


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

    Erscheinungsdatum :

    02.02.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



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