Sound attenuating structure

• US 4,035,535 A
• Filed: 02/02/1976
• Issued: 07/12/1977
• Est. Priority Date: 02/14/1975
• Status: Expired due to Term

• Current Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Original Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Inventors: Taylor, Maurice Ian
• Primary Examiner(s): Lesmes, George F.
• Assistant Examiner(s): Epstein, Henry F.
• Application Number:
  US05/654,706
• Time in Patent Office: 526 Days
• Field of Search: 428/72, 428/73, 428/116, 428/117, 428/118, 428/131, 428/132, 428/133, 428/137, 428/138, 428/139, 181/33 G, 181/33 H, 181/33 HA, 52/618
• US Class Current: 428/116
• CPC Class Codes: G10K 11/172 using resonance effects
• CPC Class Codes: Y10T 428/236 Honeycomb type cells extend perpendicularly to nonthickness layer
• CPC Class Codes: Y10T 428/24149 Honeycomb-like
• CPC Class Codes: Y10T 428/24273 including aperture

Abstract

Use of bulk sound absorber-backed spaced-cell honeycomb structures as sound attenuating liners in the flow ducts of gas turbine engines involves the disadvantage that the bulk absorber may soak up water or fuel present in the honeycomb after entry thereinto from the flow duct. In order to drain away liquid before it comes into contact with the bulk absorber, each honeycomb cell communicates with surrounding cells via apertures in the cell walls through which the liquid can drain, and a perforated sheet is provided between the honeycomb layer and the bulk absorber layer. The perforations are such that sound can enter the bulk absorber layer, but the liquid does not, each perforation being a hole having a peripheral flange which protrudes away from the bulk absorber layer into the interior of a respective cell.

Claims

1. A sound attenuating sandwich structure comprising:

a first perforate sheet member having a plurality of perforations of predetermined size therein;

a second perforate sheet member spaced from said first perforate sheet member and having a lesser plurality of perforations therein than the plurality of perforations of said first sheet member, each of the perforations of said second sheet member being greater in size than the perforations of said first sheet member, and each of the perforations of said second sheet member being defined by a flanged wall extending toward and terminating short of said first sheet member;

a spaced cell honeycomb layer disposed between said first and second sheet members, said honeycomb layer having a plurality of walls defining cells of the same, each of said cells of said honeycomb layer being disposed about a plurality of perforations of said first sheet member and only one perforation of said second sheet member, and the walls of each cell defining with said flanged wall of each perforation of said second sheet member a moat extending about the same, and apertures in the walls of each cell for providing communication between adjacent cells, the apertures in the walls of said cells being at least partially coextensive with the moats about the perforations in said second sheet member;

an impervious backing sheet member spaced from said second sheet member in a direction away from said first sheet member; and

a layer of bulk sound absorber material disposed between said second sheet member and said impervious backing sheet member.

2. A sound attenuating sandwich structure as claimed in claim 1 in which the impervious backing sheet member retains the bulk sound absorber layer in contact with the second perforate sheet member.

3. A sound attenuating sandwich structure as claimed in claim 1 in which the walls of each cell of the honeycomb layer extend spanwise between the first and second perforate sheet members and wherein each cell communicates with each adjacent cell via at least one aperture in each of its walls.

4. A sound attenuating sandwich structure as claimed in claim 1 including means for removing liquid from the structure which enters the structure through said perforations of the first sheet member and penetrates to the moats around the perforations of said second sheet member, said means comprising ducting connected to said structure for receipt of liquid flowing through said structure from the moats by the apertures in the cell walls of the honeycomb layer.

5. A sound attenuating sandwich structure forming at least a portion of an inner wall of a duct in a gas turbine engine and extending over at least a part of the circumference thereof, said sandwich structure comprising:

a first perforate sheet member forming at least a portion of the inner surface of said duct, said first perforate sheet member having a plurality of perforations of predetermined size therein;

a second perforate sheet member coextensive with and spaced radially outwardly from said first sheet member, said second sheet member having a lesser plurality of perforations therein than the plurality of perforations in said first sheet member, each of the perforations of said second sheet member being greater in size than the perforations of said first sheet member, and each of the perforations of said second sheet member being defined by a flanged wall extending radially inwardly toward the center line of said duct and terminating short of said first sheet member;

a spaced cell honeycomb layer sandwiched between said first and second sheet members and bonded thereto, said honeycomb layer having a plurality of walls defining cells of the same, each of said cells of said honeycomb layer extending between said first and second sheet members and being disposed about a plurality of perforations of said first sheet member and only one perforation of said second sheet member, and the walls of each cell defining with said flanged wall of each perforation of said second sheet member a moat extending about the same, and apertures in the walls of each cell for providing communication between adjacent cells, the apertures in the walls of said cells being at least partially coextensive with the moats about the perforations in said second sheet member;

an impervious backing sheet member spaced from said second sheet member in a direction away from said first sheet member;

a layer of bulk sound absorber material disposed between said second sheet member and said impervious backing sheet member; and

means for draining liquid penetrating to the inside of said structure by the perforations of said first sheet member and collecting in said moats, said means being located where liquid collects after drainage by gravity from the moats through the apertures in the walls of the cells of said honeycomb layer.

6. A sound attenuating sandwich structure as claimed in claim 5 in which the ends of the impervious backing sheet member overlap the ends of the bulk absorber layer and are secured to the ends of the second perforate sheet member, thereby to retain the bulk absorber layer in contact with the second perforate sheet member.

7. A sound attenuating sandwich structure as claimed in claim 5 in which the bulk absorber layer comprises a ceramic fibrous material.