Conformal high frequency antenna

• US 8,791,868 B2
• Filed: 07/18/2013
• Issued: 07/29/2014
• Est. Priority Date: 10/26/2009
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: McCarthy, Dennis K., Tornberg, Neal E., Lavin, Ronald O., Valle, Michael J.
• Primary Examiner(s): PHAN, THO GIA
• Application Number:
  US13/945,130
• Publication Number:
  US 20130300617A1
• Time in Patent Office: 376 Days
• Field of Search: 343/700.MS, 343/705, 343/708, 343/767, 343/770
• US Class Current: 343/705
• CPC Class Codes: H01Q 1/28 Adaptation for use in or on aircraft, missiles, satellites, or balloons
• CPC Class Codes: H01Q 1/286 substantially flush mounted with the skin of the craft
• CPC Class Codes: H01Q 1/38 formed by a conductive layer on an insulating support patch antennas H01Q9/0407; microstrip dipole antennas H01Q9/065; microstrip slot antennas H01Q13/106; transmission line microstrip antennas H01Q13/206; manufacturing reflecting surfaces using insulating material for supporting the reflecting surface H01Q15/142
• CPC Class Codes: H01Q 13/08 Radiating ends of two-conductor microwave transmission lines, e.g. of coaxial lines, of microstrip lines
• CPC Class Codes: H01Q 13/10 Resonant slot antennas
• CPC Class Codes: H01Q 5/357 using a single feed point
• CPC Class Codes: Y10T 29/49016 Antenna or wave energy "plumbing" making

Abstract

An integrated driveshaft cover antenna includes a driveshaft cover including a conductive layer and having a generally curved cross-section. The driveshaft cover is hingeably secured and electrically coupled to a helicopter tail boom section to cover a driveshaft access opening. The integrated drive shaft cover includes a dielectric layer including a first surface shaped to conform to a curved outer surface of the driveshaft cover and a second surface opposite the first surface. The first surface of the dielectric layer is positioned over the curved outer surface of the driveshaft cover. The first surface is secured to the curved outer surface of the driveshaft cover. The integrated drive shaft cover includes a slotted patch high frequency (HF) antenna layer having an inner slot and extends a majority of a length of the dielectric layer. The slotted patch HF antenna layer is secured to the second surface of the dielectric layer.

Claims

1. An integrated driveshaft cover antenna, comprising:

a driveshaft cover including a conductive layer, the driveshaft cover configured to be hingeably secured and electrically coupled to a helicopter tail boom section to cover a driveshaft access opening, wherein the driveshaft cover has a generally curved cross-section;

a dielectric layer including a first surface shaped to conform to a curved outer surface of the driveshaft cover and a second surface opposite the first surface, wherein the first surface of the dielectric layer is positioned over the curved outer surface of the driveshaft cover, and wherein the first surface is secured to the curved outer surface of the driveshaft cover; and

a slotted patch high frequency (HF) antenna layer having an inner slot, wherein the slotted patch HF antenna layer extends a majority of a length of the dielectric layer, and wherein the slotted patch HF antenna layer is secured to the second surface of the dielectric layer.

2. The integrated driveshaft cover antenna of claim 1, further comprising a pair of antenna leads, wherein a first end of each of the antenna leads is received at an opposing inner edge of the inner slot, and wherein a second end of each of the antenna leads is configured to be coupled to an HF transceiver.

3. The integrated driveshaft cover antenna of claim 2, wherein each of the antenna leads extends through a first thickness of the driveshaft cover and through a second thickness of the dielectric layer to the opposing inner edge of the inner slot.

4. The integrated driveshaft cover antenna of claim 2, wherein the antenna leads include a balun and a high power electrical connector to couple the antenna leads to the HF transceiver.

5. The integrated driveshaft cover antenna of claim 1, wherein the dielectric layer covers a majority of an area of the curved outer surface of the driveshaft cover.

6. The integrated driveshaft cover antenna of claim 1, wherein a shape and dimensions of the inner slot are selected to enable the slotted patch HF antenna layer to emit HF radiation that is vertically-polarized and to emit HF radiation that is horizontally-polarized, and wherein the HF radiation spans at least a portion of an HF band between 1.8 megahertz and 30 megahertz.

7. The integrated driveshaft cover antenna of claim 1, further comprising a protective outer layer covering at least the slotted patch HF antenna layer.

8. The integrated driveshaft cover antenna of claim 7, wherein the protective outer layer includes a low dielectric loss quartz fiber composite material.

9. The integrated driveshaft cover antenna of claim 1, further comprising a lightning strike appliqué

covering exposed outer surfaces of the slotted patch HF antenna layer, the dielectric layer, and the driveshaft cover.

10. A method, comprising:

coupling an antenna to a helicopter tail boom section, the antenna including;

a driveshaft cover including a conductive layer, the driveshaft cover configured to be hingeably secured and electrically coupled to the helicopter tail boom section to cover a driveshaft access opening, wherein the driveshaft cover has a generally curved cross-section;

a dielectric layer including a first surface shaped to conform to a curved outer surface of the driveshaft cover and a second surface opposite the first surface, wherein the first surface of the dielectric layer is positioned over the curved outer surface of the driveshaft cover, and wherein the first surface is secured to the curved outer surface of the driveshaft cover; and

a slotted patch high frequency (HF) antenna layer having an inner slot, wherein the slotted patch HF antenna layer extends a majority of a length of the dielectric layer, and wherein the slotted patch HF antenna layer is secured to the second surface of the dielectric layer; and

coupling first ends of transceiver leads to opposing edges of the inner slot at a midpoint of the slotted patch HF antenna layer.

11. The method of claim 10, further comprising positioning a protective outer layer over the slotted patch HF antenna layer.

12. The method of claim 11, further comprising positioning a lightning strike appliqué

over the protective layer, wherein the lightning strike appliqué

is configured disperse an electrical charge associated with a lightning strike.

13. The method of claim 12, wherein the lightning strike appliqué

comprises one of an expanded mesh and a nonconductive substrate supporting a plurality of patches of conductive material.

14. The method of claim 10, further comprising coupling second ends of the transceiver leads to a transceiver.

15. The method of claim 14, wherein the second ends of the transceiver leads are coupled to the transceiver using electrical connectors, wherein the electrical connectors include a current balancing structure.

16. The method of claim 10, wherein the slotted patch HF antenna layer is curved such that a first antenna face matches the curved cross section of the driveshaft cover.

17. The method of claim 10, wherein the slotted patch HF antenna layer is configured to radiate vertically polarized signals at a first range of frequencies and to radiate horizontally polarized signals at a second range of frequencies that is different than the first range of frequencies, wherein the first range of frequencies is between 3 megahertz and 30 megahertz, and wherein the second range of frequencies is between 1.8 megahertz and 15 megahertz.

18. The method of claim 10, wherein the inner slot has a rectangular shape.

19. The method of claim 10, wherein the inner slot has a bow-tie shape.

20. The method of claim 10, wherein a thickness between the first surface and the second surface of the dielectric layer is between one half inch to two inches.