IP Library › Granted Patent US 7,345,616
Granted Patent B2
US 7,345,616 · App. 11/628,824 · Granted Mar 18, 2008

Method and apparatus for reducing the infrared and radar signature of a vehicle

Assignee: Bell Helicopter Textron Inc.
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Quick Facts
Patent No.
US 7,345,616
App. No.
11/628,824
Granted
Mar 18, 2008
Kind
B2
Abstract

A radar-absorbing panel ( 9 ) includes a honeycomb core ( 11 ) and a lower skin ( 13 ), where the lower skin ( 13 ) is attached to the bottom of the honeycomb core ( 11 ). The honeycomb core ( 11 ) is made up of individual cells ( 15 ), which may be filled with aerogel. The individual cells ( 15 ) are approximately ½ of an inch in size with polygonal shape.

Claims (40)

1. A panel for a vehicle comprising:

a first skin;

a second skin;

a honeycomb structure disposed between the first skin and the second skin and formed from an array of large cells, each cell having a selected volume disposed between the first skin and the second skin; and

wherein the honeycomb structure is adapted for attenuating an electromagnetic signature of the vehicle.

2. The panel according to claim 1 further comprising:

a thermally insulative material disposed within the cells of the honeycomb structure and wherein the thermally insulative material reduces an electromagnetic signature of the vehicle.

3. The panel according to claim 2 , wherein the thermally insulative material is an aerogel.

4. The panel according to claim 3 , wherein at least a portion of the aerogel is treated with an opacification coating.

5. The panel according to claim 4 , wherein the aerogel is arranged within the cells so as to selectively create an electrical gradient within the cells.

6. The panel according to claim 1 , wherein the cells have a hexagon cross-sectional shape.

7. The panel according to claim 1 wherein the honeycomb structure is formed from a prepreg material.

8. The panel according to claim 7 , wherein the prepreg material is pre-impregnated with a radar absorptive material.

9. The panel according to claim 1 , wherein the cells are at least ⅜ of an inch in size.

10. The panel according to claim 1 , further comprising:

a second honeycomb structure disposed between the first skin and the second skin.

11. The panel according to claim 1 , further comprising a ground plane disposed within the first skin.

12. A panel for a vehicle comprising:

a first skin;

a second skin;

a first honeycomb structure formed from an array of cells, each cell having a selected volume disposed between the first skin and the second skin;

a second honeycomb structure formed from an array of cells, each cell having a selected volume disposed between the first skin and the second skin;

a thermally insulative material disposed within the cells of the first honeycomb structure and the cells of the second honeycomb structure; and

wherein each of the first honeycomb structure, the second honeycomb structure, and the thermally insulative material are adapted to attenuate an electromagnetic signature of the vehicle.

13. The panel according to claim 12 , wherein the first honeycomb structure and second honeycomb structure have substantially the same thickness.

14. The panel according to claim 12 , wherein the cells of the first honeycomb structure and the cells of the second honeycomb structure are substantially aligned.

15. The panel according to claim 12 , wherein the cells of the first honeycomb structure and the cells of the second honeycomb structure are selectively filled with an opacified aerogel to create a gradient of conductivity.

16. The panel according to claim 12 , wherein the first skin is constructed of a carbon and epoxy composite material.

17. The panel according to claim 12 , wherein first honeycomb structure and second honeycomb structure are constructed of a prepreg material.

18. The panel according to claim 17 , wherein the prepreg material is impregnated with a radar absorptive material.

19. A method of simultaneously attenuating the radar signature and the infrared signature of a vehicle comprising the steps of:

providing a first skin;

providing a second skin;

forming a honeycomb structure from a prepreg material, the honeycomb structure having an array of cells;

disposing the honeycomb structure between the first skin and the second skin; and

disposing a thermally insulative material within the cells of the honeycomb structure.

20. The method according to claim 19 , wherein the cells are large.

21. The method according to claim 19 , further comprising the steps of:

forming a second honeycomb structure from a prepreg material, the second honeycomb structure having an array of cells; and

disposing the second honeycomb structure between the first skin and the second skin.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 30, 2009
From: BELL HELICOPTER TEXTRON INC.
To: TEXTRON INNOVATIONS INC.
Reel/Frame 022182/0068 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 28, 2006
From: WILLIAMS, RANDY B.
To: BELL HELICOPTER TEXTRON INC.
Reel/Frame 018686/0652 →
Continuity (1)
Related Publication 20070268173A1 · Nov 22, 2007