Flush-mounted low-profile resonant hole antenna

• US 8,836,589 B2
• Filed: 09/10/2009
• Issued: 09/16/2014
• Est. Priority Date: 09/12/2008
• Status: Active Grant

• Current Assignee: Advanced Automotive Antennas, S.L. (Panasonic Holdings Corporation)
• Original Assignee: Advanced Automotive Antennas, S.L. (Panasonic Holdings Corporation)
• Inventors: Monsalve Carcelen, Beatriz, Quintero Illera, Ramiro, Sanz Arronte, Alfonso, Martinez Ortigosa, Enrique
• Primary Examiner(s): Haupt, Kristy A
• Application Number:
  US13/063,506
• Publication Number:
  US 20120038525A1
• Time in Patent Office: 1,832 Days
• Field of Search: 343/705
• US Class Current: 343/705
• CPC Class Codes: H01Q 1/286 substantially flush mounted with the skin of the craft
• CPC Class Codes: H01Q 13/18 the slot being backed by, or formed in boundary wall of, a resonant cavity longitudinally slotted cylinder H01Q13/12 ; Open cavity antennas
• CPC Class Codes: H01Q 9/0442 with particular tuning means
• CPC Class Codes: H01Q 9/0457 electromagnetically coupled to the feed line
• CPC Class Codes: H01Q 9/0464 Annular ring patch

Abstract

The invention relates to a flush-mounted aircraft, UAV or missile antenna system, which is an integral part of the fuselage (3) of an aircraft, UAV or missile. The antenna system comprises a surface (3) made of a conductive material and a resonant recess (4) formed in said conducting surface, wherein said recess is conformed to provide a resonant behavior in a selected operating frequency, the antenna system further comprising a radiating element (2) located within said recess and a feeding element (5) within said recess coupled to said radiating element.

Claims

1. A portion of a fuselage of a flying artifact, the portion of the fuselage comprising:

a conducting surface;

a resonant hole antenna system comprising

a resonant recess formed in the conducting surface, the resonant recess comprising an aperture in the conducting surface, the resonant recess filled at least partially with a dielectric material,

a radiating element supported by the dielectric material, the radiating element having a top surface and a perimeter, the radiating element being disposed in the aperture, the top surface being mounted flush with the conducting surface, the perimeter being spaced from an peripheral edge of the aperture by a gap, the gap extending around the perimeter of the radiating element,

a feeding element housed in the resonant recess and spaced from the radiating element, the feeding element being electromagnetically coupled with the radiating element for exciting the radiating element with an electromagnetic signal;

wherein the resonant recess comprises a first shape and the radiating element comprises a second shape, the first shape and the second shape being resonant in a predetermined operating frequency.

2. The portion of the fuselage of claim 1, wherein the feeding element is capacitively coupled to said radiating element.

3. The portion of the fuselage of claim 1, wherein the conducting surface comprises a conductive material, the conductive material being carbon fiber, aluminum, or titanium.

4. The portion of the fuselage of claim 1, wherein the first shape comprises a substantially circular configuration or a substantially polygonal configuration.

5. The portion of the fuselage of claim 1, wherein the first shape comprises a circular shape with a radius smaller than 1.5 wavelengths.

6. The portion of the fuselage of claim 1, wherein the antenna system is configured to provide a vertical polarization behaviour.

7. The portion of the fuselage of claim 1, wherein the antenna system is configured to have an omnidirectional pattern on the horizontal plane.

8. The portion of the fuselage of claim 1, wherein the radiating element is circular.

9. The portion of the fuselage of claim 1, wherein the radiating element comprises a planar or curved surface.

10. The portion of the fuselage of claim 1, wherein the radiating element is electrically isolated from the conducting surface.

11. The portion of the fuselage of claim 1, wherein the radiating element comprises a laminar body.

12. In combination, a portion of a fuselage of a flying artifact and a resonant hole antenna system;

the portion of the fuselage comprising a conducting surface;

the resonant hole antenna system comprising

a resonant recess formed in the conducting surface, the resonant recess comprising an aperture in the conducting surface, the resonant recess filled at least partially with a dielectric material,

a radiating element supported by the dielectric material, the radiating element having a top surface and a perimeter, the radiating element being disposed in the aperture, the top surface being mounted flush with the conducting surface, the perimeter being spaced from an peripheral edge of the aperture by a gap, the gap extending around the perimeter of the radiating element,

a feeding element housed in the resonant recess and spaced from the radiating element, the feeding element being electromagnetically coupled with the radiating element for exciting the radiating element with an electromagnetic signal;

wherein the resonant recess comprises a first shape and the radiating element comprises a second shape, the first shape and the second shape being resonant in a predetermined operating frequency.

13. The combination of claim 12, wherein the radiating element comprises a laminar body.

14. A flying artifact comprising:

a fuselage comprising a conducting surface;

a resonant hole antenna system comprising

a resonant recess formed in the conducting surface, the resonant recess comprising an aperture in the conducting surface, the resonant recess filled at least partially with a dielectric material,

a radiating element supported by the dielectric material, the radiating element having a top surface and a perimeter, the radiating element being disposed in the aperture, the top surface being mounted flush with the conducting surface, the perimeter being spaced from an peripheral edge of the aperture by a gap, the gap extending around the perimeter of the radiating element,

a feeding element housed in the resonant recess and spaced from the radiating element, the feeding element being electromagnetically coupled with the radiating element for exciting the radiating element with an electromagnetic signal;

wherein the resonant recess comprises a first shape and the radiating element comprises a second shape, the first shape and the second shape being resonant in a predetermined operating frequency;

wherein the flying artifact is an airplane, an helicopter, a missile or an UAV vehicle.

15. The flying artifact of claim 14, wherein the radiating element comprises a laminar body.