Compact, mechanically scanned cassegrain antenna system and method

• US 20060262022A1
• Filed: 05/17/2005
• Published: 11/23/2006
• Est. Priority Date: 05/17/2005
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Bien, Albert L., DeSargant, Glen J.
• Granted Patent: US 7,256,749 B2
• Time in Patent Office: Days
• US Class Current: 343/781.CA
• CPC Class Codes: H01Q 19/19 comprising one main concave reflecting surface associated with an auxiliary reflecting surface
• CPC Class Codes: H01Q 3/08 for varying two co-ordinates of the orientation

Abstract

A mechanically scanned reflector antenna system that produces a compact swept diameter and overall height, which is ideally suited for use on the external surface of a high speed mobile platform where a low profile, lightweight antenna is needed. The antenna system includes a main reflector and a subreflector both formed from composite materials. A support assembly includes a pair of arms that cantilever the main reflector forwardly of a base portion of the support assembly such that a portion of the main reflector can be positioned below an upper surface of the base portion. This enables the vertical height of the swept arc of the main reflector to be reduced when the main reflector is rotated about its elevation axis. The assembly provides an even more compact system that can be enclosed within a smaller radome when the system is employed on an external surface of a high speed mobile platform.

Claims

1. An antenna apparatus comprising:

a main reflector having a composite construction;

a subreflector supported forwardly of said main reflector and also having a composite construction;

a support platform having a base portion and at least one cantilever arm for supporting the main reflector forwardly of the base portion, the main reflector further being pivotally supported from the base portion for pivoting about an elevation axis, and further such that a portion of the main reflector can be disposed below an upper surface of the base portion and said main reflector rotated about said elevation axis without interference from said base portion; and

a rotary electrical joint disposed on said base portion to enable rotation of said support platform and said main reflector about an azimuth axis while enabling electrical coupling of said main reflector with an external electronic component.

2. The antenna apparatus of claim 1, wherein said main reflector is comprised of graphite epoxy.

3. The antenna apparatus of claim 1, wherein said support platform is comprised of a composite construction.

4. The antenna apparatus of claim 1, wherein said main reflector includes a diplexer and an orthomode transducer (OMT) supported from a rear surface thereof.

5. The antenna apparatus of claim 1, wherein said support platform includes an elevation axis motor having an output shaft with a gear;

and

wherein said main reflector includes a gear rack on a rear surface thereof for engaging said gear and enabling said motor to drive said main reflector pivotally about said elevation axis.

6. The antenna apparatus of claim 1, wherein said base portion includes an azimuth drive motor for driving said base portion rotationally about said azimuth axis.

7. The antenna apparatus of claim 1, further including an elevation axis gyroscope supported from a rear surface of said main reflector.

8. The antenna apparatus of claim 1, further comprising an azimuth axis gyroscope.

9. An antenna apparatus comprising:

a main reflector having a composite construction;

a subreflector supported from a front surface of said main reflector, said subreflector having a composite construction;

at least one of a diplexer, a low noise amplifier and an orthomode transducer supported from a rear surface of said main reflector;

a support platform assembly for supporting said main reflector for rotation about each of an azimuth axis and an elevation axis;

wherein said support platform assembly includes a base portion and a pair of arms extending forwardly of said base portion for supporting said main reflector forwardly of said base portion, and for pivoting movement about an elevation axis for enabling a portion of said main reflector to extend below an upper surface of said base portion; and

wherein said support platform assembly comprises a composite construction.

10. The antenna apparatus of claim 9, further comprising an elevation axis drive motor for driving said main reflector pivotally about said elevation axis.

11. The antenna apparatus of claim 9, further comprising a rotary coaxial joint housed in said support platform assembly for electrically coupling said components mounted on said rear surface of said main reflector with at least one electronic subsystem located externally of said antenna apparatus.

12. The antenna apparatus of claim 9, wherein said base portion comprises a composite honeycomb construction.

13. The antenna apparatus of claim 9, further comprising an elevation coaxial rotary joint disposed one of said arms for electrically coupling at least one of said components supported from said rear surface of said main reflector with an external electronics subsystem.

14. The antenna apparatus of claim 9, further comprising at least one bandpass filter supported from said rear surface of said main reflector.

15. The antenna apparatus of claim 9, further comprising at least one of an azimuth axis gyroscope and an elevation axis gyroscope supported on said support platform assembly.

16. An antenna apparatus comprising:

a main reflector having a composite construction;

a subreflector supported from a front surface of said main reflector, said subreflector having a composite construction;

at least one of a diplexer, a low noise amplifier and an orthomode transducer supported from a rear surface of said main reflector;

a toothed track supported from said rear surface of said main reflector;

a support platform assembly for supporting said main reflector for rotation about each of an azimuth axis and an elevation axis;

wherein said support platform assembly includes a base portion and a pair of arms extending forwardly of said base portion for supporting said main reflector forwardly of said base portion, and for pivoting movement about an elevation axis for enabling a portion of said main reflector to extend below an upper surface of said base portion;

a motor supported on said support platform and having a gear in engagement with said toothed track to drive said main reflector about said elevation axis; and

said support platform assembly including a composite construction.

17. The apparatus of claim 16, further comprising a coaxial rotary joint operably associated with said support platform for enabling rotation of said support platform about said azimuth axis.

18. The apparatus of claim 16, further comprising an elevation axis gyroscope supported from said support platform.

19. The apparatus of claim 16, further comprising an azimuth axis gyroscope supported from said support platform.

20. The apparatus of claim 16, wherein said main reflector and at least portions of said support platform are comprised of graphite epoxy.