Tactical high power microwave antenna pedestal

Patent metadata

Field	Value
Publication number	US-12540803-B2
Application number	US-202318357422-A
Country	US
Kind code	B2
Filing date	Jul 24, 2023
Priority date	Jul 24, 2023
Publication date	Feb 3, 2026
Grant date	Feb 3, 2026

Abstract

An antenna system comprises a reflector subsystem, a rotatable support structure and a support member. The reflector subsystem receives an input beam and reflects the input beam to produce an output beam steered in elevation by an elevation reflector and in azimuth by an azimuth reflector, towards a target. The rotatable support structure is operably coupled to the azimuth reflector and to the elevation reflector and is configured to rotate them simultaneously. The support member comprises a lengthwise portion coupled to the rotatable support structure and an offset portion coupled to the elevation reflector, the offset portion configured to offset the elevation reflector from the lengthwise portion. The offset portion is configured to enable clearance of the elevation reflector during beam steering of the output beam to extreme ends of a range of motion of the elevation reflector.

First claim

What is claimed is:

1 . An antenna system, comprising:
a reflector subsystem configured to receive an input beam and to reflect the input beam to produce an output beam towards at least one target, the reflector subsystem comprising an elevation reflector having a first range of motion and configured for steering the input beam in elevation and an azimuth reflector having a second range of motion and configured for steering the input beam in azimuth, wherein the output beam is steered in elevation and azimuth towards the target; a rotatable support structure operably coupled to the azimuth reflector and to the elevation reflector and configured to rotate the elevation reflector and the azimuth reflector simultaneously; a first support member comprising a lengthwise portion coupled to the rotatable support structure and an offset portion coupled to the elevation reflector, the offset portion configured to offset the elevation reflector from the lengthwise portion; and a second support member having a first end coupled to the rotatable support structure and a second end coupled to the azimuth reflector; and wherein, during a beam steering of the output beam, the offset portion is configured to enable clearance of the elevation reflector during beam steering of the output beam to extreme ends of the first range of motion of the elevation reflector.

2 . The antenna system of claim 1 , wherein the input beam comprises an axisymmetric beam having uniform power density distribution.

3 . The antenna system of claim 1 , wherein the first range of motion comprises a range of angles of approximately −5° to +95°.

4 . The antenna system of claim 1 wherein the elevation reflector is configured to have a deployed position and a stowed position and wherein, in the stowed position, the offset portion of the first support member is configured to position an elevation reflector steering drive next to the lengthwise portion of the first support member, wherein, in the stowed position, a positioning of the elevation reflector is configured to minimize a stowed height of the elevation reflector.

5 . The antenna system of claim 1 , further comprising a linear actuator configured to raise the elevation reflector to a deployed position and to lower the elevation reflector to a stowed position.

6 . The antenna system of claim 1 , further comprising an elevation beam steering drive operably coupled to the elevation reflector and to the rotatable support structure, the elevation beam steering drive configured to rotate the elevation reflector about an elevation rotational axis when the elevation reflector is in a deployed position.

7 . The antenna system of claim 1 , wherein the antenna system further comprises a single degree of freedom canted rotary drive operably coupled to the second support member and configured to rotate the second support member along a first end of the second support member, to position the azimuth reflector coupled to the second end into a stowed position and into a deployed position, wherein the stowed position of the azimuth reflector is configured to minimize a stowed height of the azimuth reflector.

8 . The antenna system of claim 7 , further comprising an elevation beam steering drive operably coupled to the elevation reflector and to the rotatable support structure, wherein:
the elevation beam steering drive is configured to rotate the elevation reflector about an elevation rotational axis when the elevation reflector is in its deployed position, wherein, when the azimuth reflector is in its deployed position; the rotatable support structure is configured to rotate the azimuth reflector about an azimuth rotational axis; and when the elevation reflector and the azimuth reflector are both deployed and the input beam is received, the elevation beam steering drive and the rotatable support structure are configured to cooperate to enable the antenna system to direct its output beam to any point in a full hemispherical sky dome.

9 . The antenna system of claim 8 , wherein:
the input beam comprises a high power microwave signal; the elevation reflector is configured to have a first deployed position and a first stowed position; in the first stowed position of the elevation reflector, the offset portion of the first support member is configured to position the elevation reflector next to the lengthwise portion of the first support member; and in the first stowed position of the elevation reflector, a positioning of the elevation reflector is configured to minimize a stowed height of the elevation reflector.

10 . The antenna system of claim 5 , further comprising an elevation steering head tilt actuator operably coupled to the elevation reflector and to the rotatable support structure, the elevation steering head tilt actuator configured to cooperate with the linear actuator to produce motion of the elevation reflector that is configured to stow the elevation reflector in a horizontal position.

11 . The antenna system of claim 1 , wherein the input beam comprises a high power microwave (HPM) signal and wherein the output beam that is steered towards the target is configured to direct HPM energy towards the at least one target as part of a directed energy weapon (DEW) system.

12 . The antenna system of claim 1 wherein the antenna system is in operable communication with a control subsystem that is configured to receive information about the at least one target and that is configured to automatically control, based on the information about the at least one target; at least one of:
a characteristic of the input beam;
a position of the rotatable support structure;
a position of the elevation reflector; and
a position of the azimuth reflector.

13 . The antenna system of claim 1 , wherein the input beam comprises a high power microwave (HPM) input beam, wherein the antenna system is sized for operation with the HPM input beam, and wherein the rotatable support structure is operably coupled to a movable structure, wherein the movable structure is configured with a recessed region sized to receive the elevation reflector and the first support member when the elevation reflector and the first support member are in a first stowed position.

14 . The antenna system of claim 13 , wherein:
the antenna system has a first height when the elevation reflector is in the first stowed position and the azimuth reflector is in a second stowed position; the movable structure has a second height; and the combination of the first height and the second height corresponds to an overall height that is sized to fit within a C-17 aircraft.

15 . The antenna system of claim 14 , wherein the movable structure comprises a beam generation subsystem configured to generate the HPM input beam for the antenna system.

16 . A method of directing a high power microwave (HPM) beam to a target, the method comprising:
configuring a reflector subsystem to receive a high power microwave (HPM) input beam and to reflect the HPM input beam to produce an HPM output beam towards at least one target, the reflector subsystem comprising an elevation reflector having a first range of motion and configured for steering the input beam in elevation and an azimuth reflector having a second range of motion and configured for steering the input beam in azimuth, wherein the HPM output beam is steered in elevation and azimuth towards the target; operably coupling a rotatable support structure to the azimuth reflector and to the elevation reflector; configuring the rotatable support structure to rotate the elevation

Assignees

• Raytheon Co

Inventors

• Toomey Michael A
• Marchetti Paul J
• Kemp Steven P
• Rocca Derek P
• Dressel Earl M

Classifications

• F41H13/0068 Primary

  the high-energy beam being of microwave type, e.g. for causing a heating effect in the target · CPC title

• F41A23/20

  for disappearing guns · CPC title

• H01Q1/1235 Primary

  Collapsible supports; Means for erecting a rigid antenna · CPC title

• H01Q1/3216

  where the road or rail vehicle is only used as transportation means · CPC title

• H01Q3/08

  for varying two co-ordinates of the orientation · CPC title