Method and apparatus for reducing structural vibration and noise

• US 9,725,154 B2
• Filed: 05/13/2014
• Issued: 08/08/2017
• Est. Priority Date: 05/13/2014
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Chin, Cliff L., Montgomery, Joshua M.
• Primary Examiner(s): Ference, James
• Application Number:
  US14/276,703
• Publication Number:
  US 20160185442A1
• Time in Patent Office: 1,183 Days
• Field of Search: 244 1 N, 244 1 R, 2441291, 244119, 244120, 244117 R, 2441732
• CPC Class Codes: B64C 1/40 Sound or heat insulation , e.g. using insulation blankets
• CPC Class Codes: B64C 2001/0072 from composite materials
• CPC Class Codes: B64C 2001/0081 from metallic materials
• CPC Class Codes: F16F 9/306 of the constrained layer type, i.e. comprising one or more constrained viscoelastic layers
• CPC Class Codes: G10K 11/168 Plural layers of different materials, e.g. sandwiches

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.

Claims

1. A conjugate damper for a structural panel, said conjugate damper comprising:

a constraining sheet extending in a first direction between a first edge and an opposite second edge, and extending in a second direction transverse to the first direction between a third edge and an opposite fourth edge, wherein at least a portion of each of said first edge and said second edge is directly coupled to a first surface of the structural panel, and said third and fourth edges are not directly coupled to the first surface; 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, wherein a second distance between said first edge and said second edge increases when the structural panel is in the compressively deformed state, said damping layer comprises a viscoelastic material.

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

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

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

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

6. 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.

7. 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 in a first direction between a first edge and an opposite second edge, and extending in a second direction transverse to the first direction between a third edge and an opposite fourth edge, wherein at least a portion of each of said first edge and said second edge is directly coupled to said first surface, and said third and fourth edges are not directly 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, wherein a second distance between said first edge and said second edge increases when said structural panel is in the compressively deformed state, said damping layer comprises a viscoelastic material.

8. The structural panel according to claim 7, wherein said viscoelastic material comprises a polyether-based polyurethane foam.

9. The structural panel according to claim 7, wherein said viscoelastic material comprises an open-cell melamine foam.

10. The structural panel according to claim 7, wherein said constraining sheet comprises a sheet of elastic material.

11. The structural panel according to claim 7, wherein said constraining sheet comprises a thin sheet of aluminum.

12. The structural panel according to claim 7, 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.

13. A method of reducing structural vibration and noise transmission in a structural panel, said method comprising:

coupling at least a portion of a first edge of a constraining sheet directly to a first surface of the structural panel;

coupling at least a portion of a second edge of the constraining sheet directly to the first surface, wherein the constraining sheet extends in a first direction between the first edge and the second edge, and extends in a second direction between a third edge and an opposite fourth edge, and wherein the third and fourth edges are not directly coupled 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, wherein a second distance between the first edge and the second edge increases when the structural panel is in the compressively deformed state.

14. The method according to claim 13, wherein said providing the damping layer with a viscoelastic material further comprises providing the damping layer with a polyether-based polyurethane foam material.

15. The method according to claim 13, wherein said providing the damping layer with a viscoelastic material further comprises providing the damping layer with an open-cell melamine foam material.

16. The method according to claim 13, wherein said coupling the first edge and the second edge, respectively, further comprises coupling the first edge and the second edge using an adhesive.

17. The method according to claim 13, 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.