Deployment mechanism for reflector antenna system

Patent metadata

Field	Value
Publication number	US-11319093-B2
Application number	US-201916403893-A
Country	US
Kind code	B2
Filing date	May 6, 2019
Priority date	May 6, 2019
Publication date	May 3, 2022
Grant date	May 3, 2022

Abstract

Deployable reflector system includes a boom which is extended from a rigid base. A reflector support structure is secured to a carrier end of the boom opposed from the base. The reflector support structure is configured to transition from a collapsed configuration to an expanded configuration. A tension element coupled at one end to the reflector support structure extends along a length of the boom to the base. The tension element is tensioned as a result of extending the boom, whereby a tension force is provided. The reflector support structure is transitioned from the collapsed configuration to the expanded configuration responsive to the tension force, whereby the same actuator mechanism that extends the boom also expands the reflector support structure.

First claim

We claim:

1. A deployable reflector system, comprising:
a boom configured to transition from a stowed condition in which the boom is compactly arranged for stowage, to a deployed condition in which the boom is extended to define an elongated boom length, the boom including a base tube and a carrier end which is disposed distal from the base tube when the boom is extended;
a reflector support structure secured to the carrier end, the reflector support structure configured to transition from a collapsed configuration in which the reflector support structure is arranged for compact stowage, to an expanded configuration in which the reflector support structure supports a reflector surface in accordance with a predetermined reflector shape;
an actuator configured to concurrently (i) urge the boom from the compact stowed condition to the deployed condition and (ii) facilitate deployment of the reflector support structure; and
a tension element coupled at a first end to the reflector support structure and secured at a second opposing end by an anchor located adjacent to the base tube of the boom, the tension element automatically urgable from a condition of slack to a condition of tension as the actuator urges the boom to the deployed condition;
wherein the reflector support structure is configured to automatically transition from the collapsed configuration to the expanded configuration when the tension element is being urged from the condition of slack to the condition of tension.

2. The deployable reflector system of claim 1 , wherein the tension element is configured to extend along a length of the boom to a tension guide element disposed at the carrier end of the boom, the tension guide element is configured to cause the tension element to extend away from the boom in a direction angled relative to the length of the boom.

3. The deployable reflector system of claim 2 , wherein the tension guide element is selected from the group consisting of a pulley and a cam.

4. The deployable reflector system of claim 1 , wherein the tension element is selected from the group consisting of a cord and a tape.

5. The deployable reflector system of claim 1 , wherein the actuator is comprised of a motor.

6. The deployable reflector system of claim 1 , wherein the boom is comprised of a plurality of sections which are nested together in the stowed condition, and which extend substantially end to end in the deployed condition.

7. The deployable reflector system of claim 1 , wherein the boom is comprised of a plurality of sections which are configured to operate in accordance with a scissoring action.

8. The deployable reflector system of claim 1 , wherein the extendable boom is comprised of a member extensible from a spool.

9. The deployable reflector system of claim 1 , wherein the reflector support structure is a perimeter truss assembly comprising a plurality of link members which define a pantograph.

10. The deployable reflector system of claim 1 , wherein the reflector support structure is a comprised of a plurality of foldable ribs which, when unfolded are disposed radially with respect to a central axis of the reflector support structure.

11. A method for deploying a reflector system, comprising:
using an actuator to concurrently (i) urge a boom from a stowed configuration to an extended configuration and (ii) facilitate deployment of a reflector support structure;
urging a tension element to a condition of tension by taking up a slack in the tension element as the actuator urges the boom to the extended configuration; and
using the condition of tension to urge the reflector support structure to transition from a collapsed configuration in which the reflector support structure is arranged for compact stowage, to an expanded configuration in which the reflector support structure supports a reflector surface in accordance with a predetermined reflector shape;
wherein the tension element includes a first portion disposed in alignment with a boom central axis, and a second portion extending along a part of the reflector support structure, the method further comprising increasing a length of the first portion and decreasing a length of the second portion, responsive to extending the boom.

12. The method according to claim 11 , further comprising using the decreased length of the second portion to urge the reflector support structure to the expanded configuration.

13. The method according to claim 11 , further comprising anchoring the tension element to a rigid structural base which supports the boom.

14. A method for deploying a reflector system, comprising:
using an actuator to concurrently (i) urge a boom from a stowed configuration to an extended configuration and (ii) facilitate deployment of a reflector support structure;
urging a tension element to a condition of tension by taking up a slack in the tension element as the actuator urges the boom to the extended configuration;
using the condition of tension to urge the reflector support structure to transition from a collapsed configuration in which the reflector support structure is arranged for compact stowage, to an expanded configuration in which the reflector support structure supports a reflector surface in accordance with a predetermined reflector shape; and
transitioning the reflector to an expanded configuration by controlling relative positions of a plurality of pantographic link members which form a pantograph hoop.

15. The method according to claim 11 , further comprising transitioning the reflector to the expanded configuration by unfolding a plurality of foldable ribs so that they extend radially with respect to a central axis of the reflector support structure.

16. The method according to claim 11 , further comprising extending the boom by urging a plurality of coaxially disposed sliding sections so that they are disposed substantially end to end.

17. The method according to claim 11 , further comprising extending the boom by unspooling an extensible member.

Assignees

• Eagle Tech Llc

Inventors

• Rose Christopher L
• Apotsos Greg

Classifications

• B64G1/66 Primary

  Arrangements or adaptations of apparatus or instruments, not otherwise provided for · CPC title

• B64G1/2226

  Telescoping · CPC title

• B64G1/2229

  characterised by the deployment actuating mechanism (inflating B64G1/2227) · CPC title

• B64G1/2223

  via scissor linkage · CPC title

• H01Q1/08

  Means for collapsing antennas or parts thereof (collapsible loop antennas H01Q7/02; means for collapsing H-antennas or Yagi antennas H01Q19/04) · CPC title