An acoustic panel assembly includes an acoustic panel. The acoustic panel includes an acoustic core arranged along a transverse direction and a longitudinal direction. The acoustic core extends between and to an inner core side and an outer core side. The acoustic core includes a plurality of cell rows distributed transversely along the acoustic core. Each cell row of the plurality of cell rows includes a plurality of cells distributed longitudinally along the respective cell row of the plurality of cell rows. Each cell of the plurality of cells includes a first transverse panel, a second transverse panel, a first longitudinal panel, a second longitudinal panel, and an oblique panel. Each of the first transverse panel and the second transverse panel includes a plurality of apertures. The oblique panel extends transversely between and to the first transverse panel at the outer core side and the second transverse panel at the inner core side.


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    Titel :

    ACOUSTIC PANEL FOR AN AIRCRAFT PROPULSION SYSTEM


    Beteiligte:
    NOEL AARON T (Autor:in) / MALLAMPATI PRATAP (Autor:in)

    Erscheinungsdatum :

    03.07.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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