Deployable reflector antenna system

• US 10,516,216 B2
• Filed: 01/12/2018
• Issued: 12/24/2019
• Est. Priority Date: 01/12/2018
• Status: Active Grant

• Current Assignee: Eagle Technology, LLC (L3Harris Technologies, Inc.)
• Original Assignee: Eagle Technology, LLC (L3Harris Technologies, Inc.)
• Inventors: Harless, Richard I., Feys, Joshuo
• Primary Examiner(s): Phan, Tho G
• Application Number:
  US15/870,063
• Publication Number:
  US 20190221944A1
• Time in Patent Office: 711 Days
• CPC Class Codes: H01Q 1/1235 Collapsible supports; Means for erecting a rigid antenna
• CPC Class Codes: H01Q 1/28 Adaptation for use in or on aircraft, missiles, satellites, or balloons
• CPC Class Codes: H01Q 15/161 Collapsible reflectors
• CPC Class Codes: H01Q 7/02 Collapsible antennas; Retractable antennas

Abstract

Reflector antenna system includes a hoop assembly comprising a plurality of link elements which are rigid and extend between a plurality of hinge members, the hoop assembly expandable between a collapsed condition where the link elements are substantially parallel to one another and an expanded condition wherein the link elements define a circumferential hoop around a central axis. The hoop assembly defines a plurality of N rectangular sides, each comprised of an X-member including first and a second link element in a crossed configuration. A plurality of tension elements extend around the periphery of the side and apply tension between opposing ends of the first and second link elements in directions aligned with the top, bottom and two opposing sides.

Claims

1. A reflector antenna system, comprising:

a hoop assembly comprising a plurality of link elements which are rigid and extend between a plurality of hinge members, the hoop assembly configured to expand between a collapsed condition wherein the link elements extend substantially parallel to one another and an expanded condition wherein the link elements define a circumferential hoop around a central axis;

a reflector surface comprised of a collapsible web and secured to the hoop assembly such that when the hoop assembly is in the expanded condition, the reflector surface is expanded to a shape that is configured to concentrate RF energy in a desired pattern;

wherein the hoop assembly in the expanded condition is defined by a plurality of N sides, each defining a rectangle, including a top, a bottom, and two opposing edges aligned with the central axis, said N sides disposed edge to edge circumferentially around a periphery of the hoop assembly whereby each opposing edge extends substantially the full axial depth of the hoop assembly in a direction aligned with the hoop central axis; and

wherein each of the N sides is comprised of

an X-member comprised of a plurality of the link elements including a first and a second link element respectively disposed on opposing diagonals of the rectangle in a crossed configuration, and a pivot member connected at a medial pivot point of the first and second link elements, the pivot member facilitating pivot motion of the first link element relative to the second link element on a pivot axis when the hoop assembly transitions between the collapsed condition and the expanded condition;

at least one top cord which extends along the top of the side between top ends of the first and second link elements, at least one bottom cord which extends along the bottom of the side between bottom ends of the first and second link elements; and

first and second edge tension elements which extend respectively along the two opposing edges of the side; and

at least one deployment cable to provide a force needed to transition the hoop assembly from the collapsed condition to the expanded condition by reducing a length of each opposing edge.

2. The reflector antenna system according to claim 1, wherein each of the first and second link elements include a top end which extends to a top corner of the rectangle defined by the side, and a bottom end which extends to a bottom corner of the rectangle defined by the side.

3. The reflector antenna system according to claim 2, wherein the hinge members connect adjoining ones of the X-members associated with adjacent sides at the top and bottom corners associated with each edge.

4. The reflector antenna system according to claim 2, wherein the first link element of each X-member is connected at the top end to the second link element of a first one of the X-members associated with a first adjacent side, and at a bottom end to the second link element of a second one of the X-members associated with a second adjacent side.

5. The reflector antenna system according to claim 1, wherein the second link element is comprised of a plurality of elongated structural members which extend in parallel respectively on an inner and outer side of the first link element.

6. The reflector antenna system according to claim 5, wherein the pivot member pivotally connects each of the plurality of elongated structural members to the first link element.

7. The reflector antenna system according to claim 5, wherein the plurality of elongated structural members which comprise the second link element are connected to a top hinge at a top end of the second link element, and connected to a bottom hinge at a bottom end of the second link element.

8. The reflector antenna system according to claim 7, wherein the top hinge is connected to a top end of the first link element comprising the X-member in a first adjacent side, and the bottom hinge is connected to a bottom end of the first link element comprising the X-member in a second adjacent side.

9. The reflector antenna system according to claim 1, wherein each of the top cord and the bottom cord are exclusively tension elements.

10. The reflector antenna system according to claim 1, wherein the deployment cable extends along a length of each of the edge tension elements, and diagonally along the length of the first link element of the side.

11. The reflector antenna system according to claim 10, further comprising top and bottom cord guide elements respectively disposed at the top and bottom ends of the first link element, the top and bottom cord guide elements configured to transition an alignment of the deployment cable from directions aligned with the opposing edges of each side, to a diagonal direction aligned with the first link element.

12. The reflector antenna system according to claim 10, further comprising at least one actuator configured to vary a length of the opposing edges of the side by controlling an extended length of the deployment cable extending around a periphery of the hoop assembly.

13. The reflector antenna system according to claim 1, further comprising at least one latching element configured to latch the X-members in a fixed pivot position after the hoop assembly is in the expanded condition, whereby a force applied to the first link element by the deployment cable can be reduced while maintaining the hoop assembly in the expanded condition.

14. The reflector antenna system according to claim 1, further comprising a resistance mechanism configured to resist the transition of the hoop assembly from the collapsed condition to the expanded condition.

15. A reflector antenna system, comprising:

a hoop assembly comprising a plurality of link elements which are rigid and extend between a plurality of hinge members, the hoop assembly configured to expand between a collapsed condition wherein the link elements extend substantially parallel to one another and an expanded condition wherein the link elements define a circumferential hoop around a central axis;

a reflector comprised of a flexible web material secured to the hoop assembly such that when the hoop assembly is in the expanded condition, the flexible web material is expanded to a shape that is configured to concentrate RF energy in a desired pattern;

wherein the hoop assembly in the expanded condition defines a plurality of N rectangular sides, each of which includes a top, a bottom, and two opposing edges aligned with the central axis, the rectangular sides disposed side to side circumferentially around a periphery of the hoop assembly, and each opposing edge substantially extending the full axial depth of the hoop assembly in a direction aligned with the hoop central axis; and

wherein each of the N rectangular sides is comprised of

an X-member comprised of a plurality of the link elements including a first and a second link element which respectively extend substantially between opposing top and bottom corners of the rectangular side in a crossed configuration; and

a plurality of tension elements which extend around the periphery of the side and apply tension between opposing ends of the first and second link elements in directions aligned with the top, bottom and two opposing edges.

16. The reflector antenna system according to claim 15, wherein the hinge members connect adjoining ones of the X-members associated with adjacent sides at the top and bottom corners of each rectangular side.

17. The reflector antenna system according to claim 15, wherein the second link element is comprised of a plurality of elongated rigid structural members which respectively extend in parallel on an inner and outer side of the first link element.

18. The reflector antenna system according to claim 15, further comprising a pivot member which is connected to the first and second link elements, the pivot member facilitating pivot motion of the first link element relative to the second link element on a pivot axis when the hoop assembly transitions between the collapsed condition and the expanded condition.

19. The reflector antenna system according to claim 18, wherein the plurality of tension elements include first and second edge tension cords which are also deployment cables configured to transition the hoop assembly from the collapsed condition to the expanded condition by reducing a length of the two opposing edges associated with each rectangular side.

20. The reflector antenna system according to claim 19, further comprising at least one latching element configured to latch the X-members in a fixed pivot position after the hoop assembly is in the expanded condition.

21. The reflector antenna system according to claim 20, wherein the plurality of tension elements include a top cord which extends along a top of the rectangular side and a bottom cord which extends along a bottom of the rectangular side.

22. A reflector antenna system, comprising:

a hoop assembly comprising a plurality of link elements which are rigid and extend between a plurality of hinge members, the hoop assembly configured to expand between a collapsed condition wherein the link elements extend substantially parallel to one another and an expanded condition wherein the link elements define a circumferential hoop around a central axis;

a reflector surface comprised of a collapsible web and secured to the hoop assembly such that when the hoop assembly is in the expanded condition, the reflector surface is expanded to a shape that is configured to concentrate RF energy in a desired pattern;

wherein the hoop assembly in the expanded condition defines a plurality of N rectangular sides, each of which includes a top, a bottom, and two opposing edges aligned with a central axis of the hoop assembly, the rectangular sides disposed circumferentially side to side around a periphery of the hoop assembly; and

wherein each of the N rectangular sides is comprised of

an X-member comprised of a plurality of the link elements including a first and a second link element which respectively extend substantially between opposing top and bottom corners of the rectangular side in a crossed configuration;

a top tension cord which extends along the top of the rectangular side between top ends of the first and second link elements, and a bottom tension cord which extends along the bottom of the rectangular side between bottom ends of the first and second link elements; and

a first side tension element which extends along a first one of the opposing edges of the rectangular side between a top end of the first link element and a bottom end of the second link element, and a second edge tension element which extends along a second one of the opposing sides of the rectangular side between a bottom end of the first link element and a top end of the second link element.

23. The reflector antenna according to claim 22, wherein the top tension cord is substantially aligned with a top plane of the hoop assembly and the bottom tension cord is substantially aligned with a bottom plane of the hoop assembly.