Combination bulk absorber-honeycomb acoustic panels

• US 4,235,303 A
• Filed: 11/20/1978
• Issued: 11/25/1980
• Est. Priority Date: 11/20/1978
• Status: Expired due to Term

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Schultz, William H., Dhoore, Louis G.
• Primary Examiner(s): Hix, L. T.
• Assistant Examiner(s): Fuller, Benjamin R.
• Application Number:
  US05/962,714
• Time in Patent Office: 736 Days
• Field of Search: 181/214, 181/217, 181/218, 181/222, 181/286, 181/288, 181/291, 181/292, 181/269, 181/210, 181/290, 428/116, 428/117, 428/118
• US Class Current: 181/214
• CPC Class Codes: B64D 2033/0206 comprising noise reduction means, e.g. acoustic liners
• CPC Class Codes: B64D 33/02 of combustion air intakes air intakes for gas-turbine plants or jet-propulsion plants per se F02C7/04; air intakes for combustion engines in general F02M35/00
• CPC Class Codes: F02C 7/045 having provisions for noise suppression
• CPC Class Codes: F04D 29/663 Sound attenuation
• CPC Class Codes: F05D 2250/283 honeycomb
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft
• CPC Class Codes: Y10T 428/24149 Honeycomb-like

Abstract

Combination bulk absorber-honeycomb acoustic panels particularly adapted for use in the inlet and fan air duct of a fan jet engine are disclosed. Each panel comprises a broadband noise-suppressing bulk absorber layer mounted between a back sheet and a perforated septum; and, a narrow band noise-suppressing honeycomb layer mounted between the septum and a perforated face sheet. The panels are mounted in an engine such that the perforated face sheet interfaces with airflow in the inlet or the fan air duct, as the case may be, whereby the face sheet, honeycomb layer and septum protect the bulk absorber from deterioration by isolating the high speed inlet and fan air duct airflows from the bulk absorber layer.

Claims

1. A combination bulk absorber-honeycomb acoustic panel comprising:

an impervious back sheet;

a perforated septum sheet;

a broadband noise-suppressing bulk absorber layer mounted between said back sheet and said septum sheet;

a perforated face sheet; and

a rigid noise-suppressing honeycomb layer mounted between said septum sheet and said face sheet.

2. The acoustic panel claimed in claim 1 wherein the thickness of said honeycomb layer lies in the range between about 0.125 inch and about 0.75 inch.

3. The acoustic panel claimed in claim 2 wherein the percent open area of said perforated septum lies in the range between about 10% and about 20%.

4. The acoustic panel claimed in claim 3 wherein the density of said bulk absorber layer lies in the range between about 6 and 9 pounds per cubic foot, and the thickness of said bulk absorber is greater than 0.45 inch.

5. The acoustic panel claimed in claim 4 wherein the percent open area of said perforated face sheet is greater than 19%.

6. The acoustic panel claimed in claim 1 wherein the percent open area of said perforated septum lies in the range between about 10% and about 20%.

7. The acoustic panel claimed in claim 6 wherein the density of said bulk absorber layer lies in the range between about 6 and 9 pounds per cubic foot, and the thickness of said bulk absorber is greater than 0.45 inch.

8. The acoustic panel claimed in claim 7 wherein the percent open area of said perforated face sheet is greater than 19%.

9. The acoustic panel claimed in claim 1 wherein the density of said bulk absorber layer lies in the range between about 6 and 9 pounds per cubic foot, and the thickness of said bulk absorber is greater than 0.45 inch.

10. The acoustic panel claimed in claim 9 wherein the percent open area of said perforated face sheet is greater than 19%.

11. The acoustic panel claimed in claim 1 wherein the percent open area of said perforated face sheet is greater than 19%.

12. In a fan jet engine having a fan and ducting for directing air past said fan, said ducting defined by an inlet wall located forward of said fan and fan air duct outer and inner walls located aft of said fan, the improvement comprising:

combination bulk absorber-honeycomb acoustic panels forming at least a portion of, said inlet wall and/or said fan air duct outer and inner walls for attenuating noise produced by said jet engine including buzz saw noise, forward radiated fan noise and aft radiated fan noise, each of said combination bulk absorber-honeycomb acoustic panels comprising;

an impervious back sheet;

a perforated septum sheet;

a broadband noise-suppressing bulk absorber layer mounted between said back sheet and said septum sheet;

a perforated face sheet; and

a rigid noise-suppressing honeycomb layer mounted between said septum sheet and said face sheet, said face sheet being substantially flush with said inlet wall and said fan air duct outer and inner walls.

13. The improvement claimed in claim 12 wherein the thickness of said honeycomb layer lies in the range between about 0.125 inch and about 0.75 inch.

14. The improvement claimed in claim 13 wherein the percent open area of said perforated septum lies in the range between about 10% to about 20%.

15. The improvement claimed in claim 14 wherein the density of said bulk absorber layer lies in the range between about 6 and 9 pounds per cubic foot, and the thickness of said bulk absorber is greater than 0.45 inch.

16. The improvement claimed in claim 15 wherein the open area of said perforated face sheet is greater than 19%.

17. The improvement claimed in claim 12 wherein the percent open area of said perforated septum lies in the range between about 10% to about 20%.

18. The improvement claimed in claim 17 wherein the density of said bulk absorber layer lies in the range between about 6 and 9 pounds per cubic foot, and the thickness of said bulk absorber is greater than 0.45 inch.

19. The improvement claimed in claim 18 wherein the open area of said perforated face sheet is greater than 19%.

20. The improvement claimed in claim 12 wherein the density of said bulk absorber layer lies in the range of between about 6 and 9 pounds per cubic foot, and the thickness of said bulk absorber is greater than 0.45 inch.

21. The improvement claimed in claim 20 wherein the open area of said perforated face sheet is greater than 19%.

22. The improvement claimed in claim 12 wherein the open area of said perforated face sheet is greater than 19%.