ACOUSTIC PANEL AND METHOD FOR MAKING THE SAME

    公开(公告)号:US20200049075A1

    公开(公告)日:2020-02-13

    申请号:US16059338

    申请日:2018-08-09

    发明人: Egbert Geertsema

    摘要: An acoustic panel comprises a face sheet comprising a plurality of openings; a back sheet opposite to the face sheet; and an intermediate layer comprising a plurality of cells each comprising a cavity and a plurality of walls extending between the face sheet and the back sheet and surrounding the cavity. The plurality of walls can comprise at least one and possibly a plurality of slots for drainage. A method for making the acoustic panel is also described.

    Acoustic liner for gas turbine engine components

    公开(公告)号:US10174675B2

    公开(公告)日:2019-01-08

    申请号:US14984767

    申请日:2015-12-30

    摘要: A single degree of freedom (SDOF) acoustic liner includes a porous face sheet, a substantially imperforate back sheet generally parallel to and opposing said porous face sheet and defining a thickness therebetween, and an acoustic core layer of contiguous adjacent resonant cavities disposed between the porous face sheet and the imperforate back sheet. The acoustic core layer includes a first resonant cell having a first internal volume therein and a second resonant cell having a second internal volume therein different than the first internal volume. A cell partition wall extends between the porous face sheet and the imperforate back sheet, and separates and seals the first resonant cell from the second resonant cell. In a thickness direction, and perpendicular to a plane generally parallel with the porous face sheet and the substantially imperforate back sheet, the first internal volume overlaps the second internal volume over the cell partition wall.

    Turbofan blade blocking apparatus
    10.
    发明授权

    公开(公告)号:US11788549B2

    公开(公告)日:2023-10-17

    申请号:US17493600

    申请日:2021-10-04

    IPC分类号: F04D29/52 F04D19/00

    CPC分类号: F04D29/522 F04D19/002

    摘要: Turbofan blade blocking apparatus are disclosed. An example turbofan engine includes a containment casing, a fan, at least one of a trench filler or an abradable layer at least partially aligned with the fan in an axial direction defined by the turbofan engine, at least one of the trench filler or the abradable layer fixed to an inner radial surface of the containment casing, and a metal blocker coupled to the containment casing forward of the fan, an aft end of the metal blocker interfacing with at least one of the trench filler or the abradable layer.