Method and apparatus for reducing structural vibration and noise

Patent metadata

Field	Value
Publication number	US-2016185442-A1
Application number	US-201414276703-A
Country	US
Kind code	A1
Filing date	May 13, 2014
Priority date	May 13, 2014
Publication date	Jun 30, 2016
Grant date	—

Abstract

A conjugate damper for a structural panel includes a constraining sheet extending between a first edge and a second edge. Each of the first edge and the second edge is at least partially coupled to a first surface of the structural panel. The conjugate damper also includes a damping layer coupled between the constraining sheet and the first surface such that, when the structural panel is in a compressively deformed state, a thickness of the damping layer in a direction generally normal to the first surface is decreased relative to a baseline state. The damping layer includes a viscoelastic material.

First claim

What is claimed is:

1 . A conjugate damper for a structural panel, said conjugate damper comprising:
a constraining sheet extending between a first edge and a second edge, wherein each of said first edge and said second edge is at least partially coupled to a first surface of the structural panel; and a damping layer coupled between said constraining sheet and the first surface such that when the structural panel is in a compressively deformed state, a thickness of said damping layer in a direction generally normal to the first surface is decreased relative to a baseline state, said damping layer comprises a viscoelastic material.

2 . The conjugate damper according to claim 1 , wherein a second distance between said first edge and said second edge increases when the structural panel is in the compressively deformed state.

3 . The conjugate damper according to claim 1 , wherein said viscoelastic material comprises a polyether-based polyurethane foam.

4 . The conjugate damper according to claim 1 , wherein said viscoelastic material comprises an open-cell melamine foam.

5 . The conjugate damper according to claim 1 , wherein said constraining sheet comprises a sheet of elastic material.

6 . The conjugate damper according to claim 1 , wherein said constraining sheet comprises aluminum.

7 . The conjugate damper according to claim 1 , wherein said constraining sheet comprises a plurality of perforations each extending through said constraining sheet, said plurality of perforations have a suitable size and spacing to facilitate acoustic waves passing through said constraining layer into said damping layer.

8 . A structural panel for an aircraft, said structural panel comprising:
a first surface; and at least one conjugate damper coupled to said first surface, said at least one conjugate damper comprising:
a constraining sheet extending between a first edge and a second edge, wherein each of said first edge and said second edge is at least partially coupled to said first surface; and
a damping layer coupled between said constraining sheet and said first surface such that when said structural panel is in a compressively deformed state, a thickness of said damping layer in a direction generally normal to said first surface is decreased relative to a baseline state, said damping layer comprises a viscoelastic material.

9 . The structural panel according to claim 8 , wherein a second distance between said first edge and said second edge increases when said structural panel is in the compressively deformed state.

10 . The structural panel according to claim 8 , wherein said viscoelastic material comprises a polyether-based polyurethane foam.

11 . The structural panel according to claim 8 , wherein said viscoelastic material comprises an open-cell melamine foam.

12 . The structural panel according to claim 8 , wherein said constraining sheet comprises a sheet of elastic material.

13 . The structural panel according to claim 8 , wherein said constraining sheet comprises a thin sheet of aluminum.

14 . The structural panel according to claim 8 , wherein said constraining sheet comprises a plurality of perforations each extending through said constraining sheet, said plurality of perforations have a suitable size and spacing to facilitate acoustic waves passing through said constraining layer into said damping layer.

15 . A method of reducing structural vibration and noise transmission in a structural panel, said method comprising:
coupling a first edge of a constraining sheet at least partially to a first surface of the structural panel; coupling a second edge of the constraining sheet at least partially to the first surface; providing a damping layer with a viscoelastic material; and coupling the damping layer between the constraining sheet and the first surface such that when the structural panel is in a compressively deformed state, a thickness of the damping layer in a direction generally normal to the first surface is decreased relative to a baseline state.

16 . The method according to claim 15 , wherein said coupling the first edge and the second edge, respectively, of the constraining sheet at least partially to the first surface further comprises coupling the first edge and the second edge at least partially to the first surface such that a second distance between the first edge and the second edge increases when the structural panel is in the compressively deformed state.

17 . The method according to claim 15 , wherein said providing the damping layer with a viscoelastic material further comprises providing the damping layer with a polyether-based polyurethane foam material.

18 . The method according to claim 15 , wherein said providing the damping layer with a viscoelastic material further comprises providing the damping layer with an open-cell melamine foam material.

19 . The method according to claim 15 , wherein said coupling the first edge and the second edge, respectively, of the constraining sheet at least partially to the first surface further comprises coupling the first edge and the second edge at least partially to the first surface using an adhesive.

20 . The method according to claim 15 , further comprising providing a plurality of perforations each extending through the constraining sheet, wherein the plurality of perforations have a suitable size and spacing to facilitate acoustic waves passing through the constraining layer into the damping layer.

Assignees

• Boeing Co

Inventors

• Chin Cliff L
• Montgomery Joshua M

Classifications

• G10K11/168

  Plural layers of different materials, e.g. sandwiches · CPC title

• B64C2001/0072

  from composite materials · CPC title

• F16F9/306 Primary

  of the constrained layer type, i.e. comprising one or more constrained viscoelastic layers · CPC title

• B64C2001/0081

  from metallic materials · CPC title

• B64C1/40 Primary

  Sound or heat insulation {, e.g. using insulation blankets} · CPC title