Electronically scanned hemispheric antenna

• US 20080106482A1
• Filed: 11/08/2006
• Published: 05/08/2008
• Est. Priority Date: 11/08/2006
• Status: Abandoned Application

• Current Assignee: Northrop Grumman Space & Mission Systems Corporation (Northrop Grumman Corporation)
• Original Assignee: Northrop Grumman Space & Mission Systems Corporation (Northrop Grumman Corporation)
• Inventors: Goetz, Allan, Wise, Carl, Bhattacharyya, Arun, Wrobleski, Michael, Cherrette, Alan
• Application Number:
  US11/594,320
• Publication Number:
  US 20080106482A1
• Time in Patent Office: Days
• US Class Current: 343/872
• CPC Class Codes: H01Q 1/02 Arrangements for de-icing; Arrangements for drying-out ; Arrangements for cooling; Arrangements for preventing corrosion
• CPC Class Codes: H01Q 1/246 specially adapted for base stations
• CPC Class Codes: H01Q 1/28 Adaptation for use in or on aircraft, missiles, satellites, or balloons
• CPC Class Codes: H01Q 1/40 Radiating elements coated with or embedded in protective material
• CPC Class Codes: H01Q 21/065 Patch antenna array

Abstract

A low-profile, electronically scanned antenna that can scan a hemisphere is comprised of three, phased array radiators. Each radiator face has an azimuth and elevation scan angle equal to 120 degrees. The three radiator faces are arranged in a truncated 3 sided pyramid such that they prove continuous hemispherical coverage. The three radiators are mounted to cooled panels of a truncated pyramid-shaped frame such that the radiators enable a full hemisphere to be scanned by radar.

Claims

1. An antenna comprising:

first, second and third phased array radiators (hereafter “

radiators”

), each of said radiators having an axis that is normal to the radiator, each radiator having a scan angle substantially equal to ±

60 degrees relative to each radiator'"'"'s center axis, the radiators being positioned on the circumference of a geometric circle.

2. The antenna of claim 1 wherein the geometric circle lies in a substantially horizontal plane.

3. The antenna of claim 1 wherein the first, second and third phased array radiators are substantially planar.

4. The antenna of claim 2 wherein the center axes of the first, second and third phased array radiators are upwardly inclined with respect to the horizontal plane.

5. The antenna of claim 1 wherein the first, second and third phased array radiators have vertical and azimuth scan angles that are both substantially equal to ±

60 degrees relative to the radiator'"'"'s axis so that radar signals from the three radiators can be controlled to be swept over a hemisphere.

6. The antenna of claim 1 wherein the first, second and third planar phased array radiators enclose a substantially triangular shape.

7. The antenna of claim 1 wherein the first, second and third planar phased array radiators enclose a truncated pyramid.

8. The antenna of claim 1 wherein the first, second and third planar phased array radiators abut each other such that the sum of the angles they enclose equal 180 degrees.

9. The antenna of claim 1 wherein each radiator is comprised of:

electromagnetic signal radiating elements; and

a coolant that absorbs thermal energy emitted from the electromagnetic signal radiating elements.

11. The antenna of claim 9 wherein the geometric circle lies in a substantially horizontal plane.

13. The antenna of claim 9 wherein the first, second an third planar phased array radiators enclose a volume that is substantially in the shape of a truncated pyramid.

14. The antenna of claim 9 wherein the first, second an third planar phased array radiators abut each other such that the sum of the angles they enclose equal 180 degrees.

15. The antenna of claim 9 wherein each radiator is comprised of:

electromagnetic signal radiating elements; and

a coolant that absorbs thermal energy emitted from the electromagnetic signal radiating elements.

10. An antenna comprising:

first, second and third phased array planar radiators (hereafter “

radiators”

), each of said planar radiators having a center axis that is normal to the radiator, each radiator having an azimuth scan angle substantially equal to ±

60 degrees relative to each radiator'"'"'s center axis, and each radiator has a vertical scan angle substantially equal to ±

60 degrees relative to each radiator'"'"'s center axis, the radiators being positioned on the circumference of a geometric circle.

12. The antenna of claim 10 wherein the center axes of the first, second and third phased array radiators are upwardly inclined with respect to the horizontal plane, at the same angle.

16. An antenna comprising:

first, second and third planar arrays, each of said planar arrays being substantially planar and having a geometric center axis that extends substantially perpendicular from the geometric center of a radiating face of each radiator, each radiator having vertical and azimuth scan angles that are both substantially equal to ±

60 degrees relative to each radiator'"'"'s center axis, the planar arrays being positioned on the circumference of a geometric circle; and

first, second and third, radar-signal transmissive radomes extending over the radiating faces of the first, second and third planar arrays respectively such that the planar arrays are behind the radomes and the radomes are mechanically supported by the planar arrays.

17. The antenna of claim 16 wherein the geometric circle lies in a substantially horizontal plane.

18. The antenna of claim 16 wherein the first, second and third planar arrays are substantially planar and the radomes substantially conform to the planar arrays.

19. The antenna of claim 16 wherein the center axes of the first, second and third planar arrays are upwardly inclined with respect to the horizontal plane, at substantially the same angle.

20. The antenna of claim 16 wherein the first, second and third planar arrays emit electromagnetic signals from each radiator that can be swept over a hemisphere.

21. The antenna of claim 16 wherein the first, second an third planar planar arrays abut each other such that the first, second and third planar arrays enclose a substantially triangular shape.

22. The antenna of claim 16 wherein each radiator is comprised of:

electromagnetic signal radiating elements; and

a coolant that absorbs thermal energy emitted from the electromagnetic signal radiating elements.

23. An antenna comprising:

first, second and third phased array radiators (hereafter “

radiators”

), each of said radiators being substantially planar and having a electromagnetic signal radiating face having geometric center axis that extends perpendicularly from the geometric center of the radiating face of each radiator, each radiator having a vertical and azimuth scan angle substantially equal to ±

60 degrees relative to each radiator'"'"'s center axis;

first, second and third, radar-signal transmissive radomes that conform to and which extend over the radiating faces of the first, second and third radiators respectively such that the radiators are behind the radomes, the radomes being mechanically supported by the radiators; and

a three-sided, truncated-pyramidal-shaped fairing having first, second and third inclined faces that receive the first, second and third radomes.

24. The antenna of claim 23 wherein the sides of the truncated-pyramidal-shaped fairing are inclined at a first predetermined angle.

25. The antenna of claim 24 wherein the first, second and third phased array radiators are substantially planar and the radomes conform to the radiators.

26. The antenna of claim 23 wherein the center axes of the first, second and third phased array radiators are upwardly inclined with respect to the horizontal plane, at the same angle.

27. The antenna of claim 23 wherein the first, second and third phased array radiators are capable of emitting electromagnetic signals from each radiator that can be swept over a hemisphere.

28. The antenna of claim 23 wherein each radiator is comprised of:

electromagnetic signal radiating elements; and

a coolant that absorbs thermal energy emitted from the electromagnetic signal radiating elements.