Hull or fuselage integrated antenna

• US 20080316124A1
• Filed: 02/29/2008
• Published: 12/25/2008
• Est. Priority Date: 03/02/2007
• Status: Active Grant

• Current Assignee: Saab AB
• Original Assignee: Saab AB
• Inventors: Hook, Anders
• Granted Patent: US 7,760,149 B2
• Time in Patent Office: Days
• US Class Current: 343/705
• CPC Class Codes: H01Q 1/286 substantially flush mounted with the skin of the craft
• CPC Class Codes: H01Q 21/061 Two dimensional planar arrays
• CPC Class Codes: H01Q 21/062 using dipole aerials; H01Q21/067, H01Q21/068 take precedence
• CPC Class Codes: H01Q 21/064 using horn or slot aerials slotted waveguides arrays H01Q21/005

Abstract

An antenna structure integrated in a hull or fuselage. The hull or fuselage can be the outer surface of an aircraft, artillery shell, missile or ship. The antenna structure includes an array antenna. The array antenna includes a number of antenna elements. Each antenna element includes a radiator and an RF feed. The antenna elements are arranged in a lattice within an antenna area including a central antenna area and a transition region outside the central antenna area wherein a number of the antenna radiators as well as resistive sheets are arranged in substantially the same plane as a surrounding outer surface of the hull or fuselage.

Claims

1. An antenna structure integrated in a hull or fuselage, the antenna structure comprising:

an array antenna comprising a number of antenna elements, each antenna element comprising a radiator and an RF-feed, the antenna elements being arranged in a lattice within an antenna area comprising a central antenna area and a transition region outside the central antenna area, the array antenna further comprising a plurality of resistive sheets, wherein a number of the antenna radiators and resistive sheets are arranged in substantially a same plane as a surrounding outer surface of the hull or fuselage.

2. The antenna structure according to claim 1, wherein the resistive sheets have a high conductivity in a transition region close to the hull or fuselage and wherein a conductivity of the sheets decreases in a direction towards the central antenna area, thus providing a tapered adjustment in a reflection coefficient over a wide frequency interval.

3. The antenna structure according to claim 1, wherein the antenna radiators within the transition region outside the central antenna area are covered with the resistive sheets.

4. The antenna structure according to claim 1, wherein the antenna radiators each comprise a slot radiator filled with dielectric material and fed via a probe in a cavity and wherein the slots are made directly in the hull or fuselage.

5. The antenna structure according to claim 1, wherein the antenna radiators each comprise a slot radiator filled with dielectric material and fed via a probe in a cavity and wherein the slots are made in a plate inserted into the hull or fuselage such that a surface of the plate conforms to the surface of the hull or fuselage.

6. The antenna structure according to claim 5, the plate has a curved surface.

7. The antenna structure according to claim 1, wherein the plate comprises metal or carbon reinforced composite.

8. The antenna structure according to claim 4, wherein the cavity is filled with a dielectric material.

9. The antenna structure according to claim 8, wherein the slot radiator and the cavity are filled with the same dielectric material.

10. The antenna structure according to claim 4, wherein a conductivity of walls of the slots is increased by suitable surface treatment.

11. The antenna structure according to claim 4, wherein the slot radiators in the transition region outside the central antenna area are covered with the resistive sheets, wherein the sheets are slot shaped.

12. The antenna structure according to claim 1, wherein the transition region outside the central antenna area comprises one ring of antenna radiators covered with the resistive sheets, wherein the sheets are slot shaped.

13. The antenna structure according to claim 1, wherein the transition region outside the central antenna area comprises at least two rings of radiators covered with the resistive sheets, wherein the sheets are slot shaped, wherein a first ring closest to the hull or fuselage comprises resistive sheets with a low resistance and following rings have slots covered with resistive sheets having a resistance becoming higher the closer the ring is to the central antenna area.

14. The antenna structure according to claim 1, wherein the antenna radiators comprise conductive elements surrounded by strips of resistive sheets in the transition region outside the central antenna area and mounted on a dielectric substrate having a top surface conforming to the outer surface of the hull or fuselage and a bottom surface to which a separate antenna ground plane is applied.

15. The antenna structure according to claim 1, wherein:

the antenna radiators comprise conductive elements mounted on at least two layers of dielectric substrates having a top layer with a top surface and a bottom layer with a bottom surface to which a separate antenna ground plane is applied,

the top surface conforms to the outer surface of the of the hull or fuselage, and

the antenna radiators in the top layer and within the transition region outside the central antenna area are surrounded by strips of resistive sheets.

16. The antenna structure according to claim 14, wherein the separate antenna ground plane comprises a conductive material of high mechanical strength.

17. The antenna structure according to claim 14, wherein the antenna radiators in the transition region outside the central antenna area are surrounded by one ring of the strips of resistive sheets.

18. The antenna structure according to claim 1, wherein the transition region outside the central antenna area comprises at least two rings of antenna radiators, the radiators being surrounded by the strips of resistive sheets, wherein a first ring closest to the hull or fuselage comprises resistive sheet strips with a low resistance and following rings comprises strips of resistive sheets having a resistance becoming higher the closer the ring is to the central antenna area.

19. The antenna structure according to claim 1, wherein the dielectric substrate under a part of the transition region outside the central antenna area is replaced by bulk absorbers or vertically oriented resistive cards.

20. The antenna structure according to claim 1, wherein the radiators comprise metal.

21. The antenna structure according to claim 1, wherein at least one of the dielectric substrate or the separate antenna ground plane comprise high mechanical strength materials.

22. The antenna structure according to claim 1, wherein the hull or fuselage has a curved surface.

23. The antenna structure according to claim 1, wherein at least one of the antenna radiators in the transition region outside the central antenna area is inactive.

24. The antenna structure according to claim 1, wherein the antenna area is covered with a thin environmental protection skin.

25. The antenna structure according to claim 1, wherein the hull or fuselage is the outer surface of an aircraft, artillery shell, missile or ship.

26. The antenna structure according to claim 1, wherein the antenna is integrated in a hatch covering an opening in the hull or fuselage.