Acoustic liner for gas turbine engine components
AssigneesGeneral Electric Company, MRA Systems, Inc.
InventorsMichael Moses Martinez, Rudramuni Kariveerappa Majjigi, Steven Thomas Davies, Egbert Geertsema
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AssigneesGeneral Electric Company, MRA Systems, Inc.
InventorsMichael Moses Martinez, Rudramuni Kariveerappa Majjigi, Steven Thomas Davies, Egbert Geertsema
Estimating the term…
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.
An acoustic honeycomb structure, comprising at least one heptad of contiguous adjacent resonant cavities arranged substantially parallel to one another in a hexagonal grid formation, wherein said at least one heptad comprises:
Dependencies are inferred from the claim text.