Aircraft cabin interior noise treatment

• US 6,260,660 B1
• Filed: 12/18/1998
• Issued: 07/17/2001
• Est. Priority Date: 12/18/1998
• Status: Expired due to Fees

• Current Assignee: Sikorsky Aircraft Corporation (Martin Marietta Corporation)
• Original Assignee: Sikorsky Aircraft Corporation (Martin Marietta Corporation)
• Inventors: Yoerkie, Charles A. Jr., Wadey, Bryan T.
• Primary Examiner(s): Dang, Khanh
• Application Number:
  US09/215,076
• Time in Patent Office: 942 Days
• Field of Search: 181/207, 181/208, 181/286, 181/288, 181/290, 181/291, 181/292, 181/294, 181/295
• US Class Current: 181/290
• CPC Class Codes: B64C 1/40 Sound or heat insulation , e.g. using insulation blankets
• CPC Class Codes: Y02T 50/40 Weight reduction

Abstract

A noise reducing blanket for use in an aircraft cabin for reducing acoustic noise transmission from an aircraft airframe to a cabin interior. The blanket includes a mass barrier portion, a foam portion having at least one cavity formed in it, and a vapor barrier which is disposed about the foam portion The mass barrier portion includes a plurality of vinyl layers that are attached to one another at spaced apart locations. The spaced attachment allows the layers to move substantially independently from one another. The layers are preferably attached to one another by stitching that includes between approximately three to five stitches per inch. There are preferably at least two layers in the mass barrier portion, and, more preferably, between 2 and 4 layers in the mass barrier portion. The cavities in the foam portion are designed to increase the noise absorptive properties of the blanket. Preferably at least one of the dimensions of the cavities in the foam portion is approximately ¼ the wavelength of the dominant noise frequency to provide a resonant chamber within the foam portion. In one embodiment of the invention, the foam portion is attached to the mass barrier portion with an adhesive. In a second embodiment of the invention the foam portion is mounted to the aircraft separate from the mass barrier portion.

Claims

1. A noise reducing blanket for use in an aircraft cabin for reducing acoustic noise transmission from an aircraft airframe to a cabin interior, the blanket comprising:

a mass barrier portion that includes a plurality of vinyl layers attached to one another at spaced apart locations so as to move substantially independently from one another between attachment locations;

a foam portion, the foam portion having at least one cavity formed in it; and

a vapor barrier disposed about the foam portion.

2. A noise reducing blanket according to claim 1 wherein the foam portion is attached to the mass barrier portion.

3. A noise reducing blanket according to claim 1 wherein the layers are attached to one another by stitching.

4. A noise reducing blanket according to claim 3 wherein there are between approximately three to five stitches per inch.

5. A noise reducing blanket according to claim 1 wherein the layers are loaded with material to increase their mass.

6. A noise reducing blanket according to claim 5 wherein the material is selected from a group consisting of mica and barium sulfate.

7. A noise reducing blanket according to claim 1 wherein there are at least two layers in the mass barrier portion.

8. A noise reducing blanket according to claim 7 wherein there are between 2 and 4 layers in the mass barrier portion.

9. A noise reducing blanket according to claim 1 wherein the foam portion is at least ¾

inch thick.

10. A noise reducing blanket according to claim 1 wherein the vapor barrier is made from a polyvinyl fluoride material.

11. A noise reducing blanket according to claim 1 wherein there are a plurality of cavities formed in the foam portion.

12. A noise reducing blanket for use in an aircraft cabin for reducing acoustic noise transmission from an aircraft airframe to a cabin interior, the blanket comprising:

a mass barrier portion;

a foam portion having at least one cavity formed in it; and

a vapor barrier disposed about the foam portion;

wherein at least one of the dimensions of the at least one cavity in the foam portion is approximately ¼

the wavelength of the dominant noise frequency to provide a resonant chamber within the foam portion.

13. A noise reducing blanket for use in an aircraft cabin for reducing acoustic noise transmission from an aircraft airframe to a cabin interior, the blanket comprising:

a mass barrier portion including a plurality of vinyl layers attached to one another at spaced apart locations so as to move substantially independently from one another between attachment locations;

a foam portion having a plurality of cavities formed in it, at least one of the dimensions of the cavities in the foam portion being approximately ¼

the wavelength of the dominant noise frequency to provide a resonant chamber within the foam portion; and

a vapor barrier disposed about the foam portion.

14. A noise reducing blanket according to claim 13 wherein there are between 2 and 4 layers in the mass barrier portion.

15. A noise reducing blanket according to claim 13 wherein the layers are loaded with material to increase their mass.

16. A noise reducing blanket according to claim 13 wherein the vapor barrier is made from a polyvinyl fluoride material.

17. A noise reducing blanket for use in an aircraft cabin for reducing acoustic noise transmission from an aircraft airframe to a cabin interior, the blanket comprising:

a foam portion having at least one cavity formed in it;

a vapor barrier completely surrounding the foam portion;

a mass barrier portion disposed outside the vapor barrier so as to move substantially independently from the vapor barrier, the combination of the mass barrier and the foam portion providing reduction in acoustic noise transmission.