Acoustic liner for gas turbine engine components

Patent metadata

Field	Value
Publication number	US-10174675-B2
Application number	US-201514984767-A
Country	US
Kind code	B2
Filing date	Dec 30, 2015
Priority date	Dec 30, 2015
Publication date	Jan 8, 2019
Grant date	Jan 8, 2019

Abstract

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.

First claim

What is claimed is:

1. 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:
a central hexagonal tube comprising six lateral walls arranged evenly about a central tube axis, said six lateral walls each extending along said central tube axis from a first opposing tube end to a second opposing tube end, said six lateral walls defining a first central hexagonal base opening disposed at said first opposing tube end and a second central hexagonal base opening disposed at said second opposing tube end; and
six adjacent hexagonal tubes radially surrounding said central hexagonal tube about said central tube axis, each of said six adjacent hexagonal tubes extending from said first opposing tube end to said second opposing tube end and including a first adjacent hexagonal base opening disposed at said first opposing tube end and a second adjacent hexagonal base opening disposed at said second opposing tube end,
wherein said first central hexagonal base opening is generally parallel to said second central hexagonal base opening,
wherein said first adjacent hexagonal base opening is generally parallel to said second adjacent hexagonal base opening, wherein said second central hexagonal base opening is larger than said first central hexagonal base opening,
wherein each of said six lateral walls is commonly shared with a respective one of said six adjacent hexagonal tubes; and
wherein said six lateral walls each comprise a first rectangular wall portion and a second rectangular wall portion.

2. The acoustic honeycomb structure as claimed in claim 1 , wherein said second rectangular wall portion is disposed at a greater radial distance from said central tube axis than said first rectangular wall portion.

3. The acoustic honeycomb structure as claimed in claim 2 , wherein each of said six lateral walls further comprises a radial shelf connecting said first rectangular wall portion with said second rectangular wall portion.

4. The acoustic honeycomb structure as claimed in claim 3 , wherein said at least one heptad comprises a first heptad and a second heptad disposed adjacent said first heptad in said hexagonal grid formation.

5. The acoustic honeycomb structure as claimed in claim 4 , wherein said first heptad shares one of said six adjacent hexagonal tubes in common with second heptad.

6. The acoustic honeycomb structure as claimed in claim 5 , wherein said in common one of said six adjacent hexagonal tubes comprises at least two separate radial shelves of two separate central hexagonal tubes, respectively.

7. The acoustic honeycomb structure as claimed in claim 3 , wherein said central hexagonal tube comprises a central interior volume, said each adjacent hexagonal tube comprises an adjacent interior volume, and said central interior volume is greater than said adjacent interior volume.

8. The acoustic honeycomb structure as claimed in claim 7 , wherein said central interior volume corresponds to a first suppression frequency.

9. The acoustic honeycomb structure as claimed in claim 8 , wherein said adjacent interior volume corresponds to a second suppression frequency different from said first suppression frequency.

10. The acoustic honeycomb structure as claimed in claim 7 , wherein said central interior volume and said adjacent interior volume overlap over said radial shelf in the direction of said central tube axis.

11. The acoustic honeycomb structure as claimed in claim 1 , wherein said first central hexagonal base opening and said first adjacent hexagonal base opening comprise regular hexagonal shapes.

12. The acoustic honeycomb structure as claimed in claim 8 , wherein said first central hexagonal base opening has substantially the same dimensions as said first adjacent hexagonal base opening.

13. The acoustic honeycomb structure as claimed in claim 1 , wherein said first adjacent hexagonal base opening is larger than said second adjacent hexagonal base opening.

14. The acoustic honeycomb structure as claimed in claim 1 , wherein said second adjacent hexagonal base opening comprises an irregular convex hexagonal shape.

Assignees

• Gen Electric
• Mra Systems Inc

Inventors

• Martinez Michael Moses
• Majjigi Rudramuni Kariveerappa
• Davies Steven Thomas
• Geertsema Egbert

Classifications

• F05D2240/40

  Use of a multiplicity of similar components · CPC title

• F04D29/664

  by means of sound absorbing material · CPC title

• G10K11/172

  using resonance effects · CPC title

• F05D2250/132

  hexagonal · CPC title

• F05D2250/283

  honeycomb · CPC title