An acoustic panel for an aircraft comprising: a sound attenuating sheet comprising 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 there between.

    一种用于飞行器的声学面板,包括:包括多个腔体的声音衰减片,声音衰减片具有第一表面、与第一表面相对的第二表面以及连接第一表面和第二表面的端部表面;在第一表面的至少一部分上方和端部表面上方延伸的第一片材;以及在第二表面和端部表面上方延伸的第二片材,其中连接第一片材和第二片材使得能够在它们之间传递拉力。


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    Title :

    ACOUSTIC PANEL


    Additional title:

    声学面板


    Contributors:
    KIRK DAVE (author) / HILL GRAEME (author) / HEBDEN DAVE (author) / FURMSTON SIMON (author)

    Publication date :

    2022-01-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    G10K Tonerzeugungsvorrichtungen , SOUND-PRODUCING DEVICES / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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