Soundproofing panel with beads, and a method of manufacture

• US 7,520,369 B2
• Filed: 11/19/2004
• Issued: 04/21/2009
• Est. Priority Date: 11/21/2003
• Status: Active Grant

• Current Assignee: Ateca, Safran Aircraft Engine Company
• Original Assignee: Ateca, Snecma (Safran SA)
• Inventors: Dravet, Alain, Delverdier, Osmin, Riou, Georges, Julliard, Jacques, Vie, Philippe
• Primary Examiner(s): Benson; Walter
• Assistant Examiner(s): LUKS, JEREMY AUSTIN
• Application Number:
  US10/991,543
• Publication Number:
  US 20050109557A1
• Time in Patent Office: 1,614 Days
• Field of Search: 181/292, 181/288, 181/290, 181/293, 181/284, 181/286, 181/291
• US Class Current: 181/292
• CPC Class Codes: B64D 29/00 Power-plant nacelles, fairings, or cowlings nacelles not otherwise provided for B64C
• CPC Class Codes: G10K 11/172 using resonance effects

Abstract

A soundproofing panel having a core sandwiched between a solid wall and a porous wall. The core being connected to the walls and having partitions extending in the thickness direction between the two walls so as to form cells. Each cell containing at least one sound energy dissipating layer constituted by hollow spherical beads having mutually contacting walls that are porous and micro-perforated, and being held in position in the thickness direction between the two walls by nets that are secured to the partitions.

Claims

1. A soundproofing panel comprising:

a solid wall;

a porous wall;

a core positioned between said solid wall and said porous wall and connected to both said solid wall and said porous wall, said core including partitions extending between said solid wall and said porous wall and forming a plurality of cells, each cell containing a plurality of sound energy dissipating layers constituted by hollow spherical beads in mutual contact; and

a first net and a second net provided with each of the plurality of sound energy dissipating layers, the first and second nets are secured to the partitions,

wherein said hollow spherical beads have walls that are porous and micro-perforated and said hollow spherical beads are held in position by the first and second nets, and

wherein at least two of the plurality of sound energy dissipating layers formed in a single cell vary in thickness from each other.

2. A soundproofing panel according to claim 1, wherein said porous wall further includes perforations for increasing the viscothermal effect on the air passing therethrough.

3. A soundproofing panel according to claim 1, wherein the dissipating layers are constituted by beads of uniform diameter.

4. A soundproofing panel according to claim 1, wherein the dissipating layers are constituted by a mixture of beads having diameters varying in the range 1 mm to 3.5 mm.

5. A soundproofing panel according to claim 1, wherein the nets are of the same composition as the partitions onto which they are secured.

6. A soundproofing panel according to claim 1, wherein the micro-perforations in the walls of said hollow spherical beads include a surface dimension in the range of 200 μ

m to 400 μ

m.

7. A soundproofing panel according to claim 1, wherein the micro-perforations in the walls of said hollow spherical beads include a surface dimension that is greater than a dimension of the pores in the same walls by a factor of at least about 20.

8. A soundproofing panel according to claim 1, wherein the micro-perforations in the walls of said hollow spherical beads are substantially cylindrical having a diameter of about 200 μ

m.

9. A soundproofing panel according to claim 1, wherein the micro-perforations in the walls of said hollow spherical beads have a rectangular cross-section.

10. A soundproofing panel according to claim 9, wherein said rectangular cross-section has a width of about 200 μ

m and a length of about 500 μ

m.

11. An exhaust nozzle having a soundproofing panel according to claim 1.

12. A turbomachine having a soundproofing panel according to claim 1.

13. An airplane having a soundproofing panel according to claim 1.

14. A method of making a soundproofing panel comprising the steps of:

forming a core comprising partitions that form cells;

positioning a lower net in each cell of said core;

securing said lower nets to said partitions;

placing on said lower net a desired thickness of hollow spherical beads having porous and micro-perforated walls;

positioning an upper net in each cell while applying a small amount of pressure against said beads;

securing said upper nets to said partitions;

securing one end of the partitions forming said core to a porous wall; and

securing another end of the partitions forming said core to a solid wall,

wherein the lower and upper nets form sound energy dissipating layers,

wherein each cell includes a plurality of sound energy dissipating layers, and

wherein at least two of the plurality of sound energy dissipating layers formed in a single cell vary in thickness from each other.

15. A method according to claim 14, wherein said porous wall further includes perforations to increase the viscothermal effect of the air passing therethrough.

16. A method according to claim 14, wherein said upper and lower nets are welded to said partitions, and said ends of the partitions forming said core are welded to said walls.

17. A method according to claim 14, wherein the micro-perforations in the walls of said hollow spherical beads include a surface dimension in the range of 200 μ

m to 400 μ

m.

18. A method according to claim 14, wherein the micro-perforations in the walls of said hollow spherical beads include a surface dimension that is greater than a dimension of the pores in the same walls by a factor of at least about 20.