Device for unfurling and refurling a flexible structure, and a flexible unfurlable structure and satellite both equipped with such a device

Patent metadata

Field	Value
Publication number	US-9718639-B2
Application number	US-201314094340-A
Country	US
Kind code	B2
Filing date	Dec 2, 2013
Priority date	Dec 5, 2012
Publication date	Aug 1, 2017
Grant date	Aug 1, 2017

Abstract

A device is provided for unfurling and refurling comprising at least one tape spring having an axis of unfurling and of refurling parallel to an axis X and a rotor capable of rotating about an axis Y perpendicular to the axis X, the tape spring being able, autonomously, to pass from a state in which it is wound around the rotor to an unwound state. The tape spring is mounted bent in two in the shape of a U and comprises a first end fixed rigidly to a first anchor point that may be secured to a stator or to the rotor and a second end wound around the rotor.

First claim

The invention claimed is:

1. A device for unfurling and refurling a flexible structure comprising at least one tape spring having an axis of unfurling and of refurling parallel to an axis X, a rotor capable of rotating about an axis Y perpendicular to the axis X, and a stator supporting the rotation axis Y of the rotor, the tape spring being able, autonomously, to pass from a state in which the tape spring is wound around the rotor to an unwound state, the tape spring being mounted bent in a transverse direction into a shape of a U with two branches, wherein the tape spring comprises a first end of a first branch fixed rigidly to a first anchor point and a second end of a second branch fixed rigidly to a second anchor point secured to the rotor, the first end of the first branch of the tape spring being mounted between two jaws of the first anchor point, wherein the first and second anchor points are different from one another, and wherein the two ends of the two branches are the respective two opposite ends of the tape spring in the longitudinal direction X.

2. The unfurling and refurling device of claim 1 , wherein the second anchor point consists of two jaws of complementing shapes mounted facing one another, the second end of the second branch of the tape spring being mounted between the two jaws of the second anchor point.

3. The unfurling and refurling device of claim 1 , further comprising at least two rollers mounted facing one another on a fixed fitting supporting the axis of rotation of the rotor, the second branch of the tape spring secured to the rotor being set in between the two rollers.

4. The unfurling and refurling device of claim 1 , further comprising an unfurling-speed regulating device coupled to the rotor.

5. The unfurling and refurling device of claim 1 , further comprising at least one two-dimensional XY flexible membrane, the tape spring being fixed to the flexible membrane parallel to the axis X of unfurling and refurling of the tape spring.

6. The unfurling and refurling device of claim 5 , comprising at least two tape springs fixed parallel to one another and parallel to the axis X on the flexible membrane, each tape spring being mounted bent in two, the first end of each tape spring being fixed rigidly to the first anchor point and the second end of each tape spring being fixed rigidly to the second anchor point secured to the rotor.

7. The unfurling and refurling device of claim 6 , wherein the flexible membrane comprises lateral battens orthogonal to the axis X, the lateral battens being respectively fixed to each tape spring.

8. The unfurling and refurling device according to claim 1 , further comprising at least one fixed stator and wherein the first anchor point is secured to the stator.

9. The unfurling and refurling device according to claim 1 , wherein the first anchor point is secured to the rotor and wherein the unfurling and refurling device comprises two first rollers mounted facing one another on a fixed fitting supporting the axis of rotation of the rotor and two second rollers mounted facing one another on the fitting, the second branch of the tape spring being set in between the two first rollers, the first branch of the tape spring being set in between the two second rollers.

10. The unfurling and refurling device of claim 8 , comprising at least two tape springs mounted in opposition on one and the same rotor, each tape spring being mounted bent in two and comprising two ends which are fixed respectively to one and the same stator by first anchor points and to said rotor by second anchor points.

11. The unfurling and refurling device of claim 8 , comprising at least three tape springs mounted in a star on one and the same rotor, each tape spring being mounted bent in two and comprising two ends fixed respectively to one and the same stator by first anchor points and to said rotor by second anchor points.

12. The unfurling and refurling device of claim 8 , comprising at least two stators parallel to the axis Y, said two stators being mounted one on either side of the rotor and two flexible structures mounted in opposition on said rotor, each flexible structure comprising a two-dimensional XY flexible membrane and at least one tape spring fixed bent in two to the flexible membrane, the tape spring comprising a first end fixed rigidly to one of the two stators and a second end fixed to the rotor.

13. The unfurling and refurling device according to claim 1 , wherein the tape spring is a corrugated sheet.

14. A flexible unfurlable structure comprising at least one unfurling and refurling device according to claim 1 .

15. The flexible unfurlable structure of claim 14 , further comprising an unfurlable articulated mast.

16. The flexible unfurlable structure of claim 15 , wherein the articulated mast is able to be fixed to a platform of a satellite via a rotational-drive motor.

17. The flexible unfurlable structure of claim 14 , comprising two solar array half-wings mounted back to back on either side of a mid-plane of the unfurlable structure, the mid-plane being perpendicular to the axis X of unfurling and of refurling of the two half-wings and two independent unfurling and refurling devices respectively dedicated to the two half-wings, the two unfurling and refurling devices comprising two respective rotors, the two rotors having mutually parallel respective axes of rotation.

18. The flexible unfurlable structure of claim 14 , comprising a first flexible membrane fixed to the first branch of the bent-in-two tape spring and a second flexible membrane fixed to the second branch of said bent-in-two tape spring, the first flexible membrane supporting first objects and the second flexible membrane supporting second objects different from the first objects.

19. The flexible unfurlable structure according to claim 18 , wherein the first objects are solar cells and the second objects are lenses that concentrate the light, and wherein the second flexible membrane is transparent to rays of light.

20. A satellite comprising at least one flexible unfurlable structure of claim 14 .

21. The unfurling and refurling device of claim 8 , further comprising an unfurling-speed regulating device coupled to the rotor.

22. The unfurling and refurling device of claim 8 , further comprising at least one two-dimensional XY flexible membrane, the tape spring being fixed to the flexible membrane parallel to the axis X of unfurling and refurling of the tape spring.

23. The unfurling and refurling device of claim 22 , comprising at least two tape springs fixed parallel to one another and parallel to the axis X on the flexible membrane, each tape spring being mounted bent in two, the first end of each tape spring being fixed rigidly to the first anchor point and the second end of each tape spring being fixed rigidly to the second anchor point secured to the rotor.

24. The unfurling and refurling device of claim 23 , wherein the flexible membrane comprises lateral battens orthogonal to the axis X, the lateral battens being respectively fixed to each tape spring.

25. The flexible unfurlable structure of claim 19 , further comprising an unfurlable articulated mast able to be fixed to a platform of a satellite.

Assignees

• Thales Sa
• Centre Nat D'Etudes Spatiales—Cnes
• Centre Nat D'Etudes Spatiales

Inventors

• Baudasse Yannick
• Vezain Stephane
• Boulanger Bernard
• Guinot Francois

Classifications

• B64G1/44

  using radiation, e.g. deployable solar arrays · CPC title

• B64G1/503

  Radiator panels · CPC title

• B65H75/34 Primary

  specially adapted or mounted for storing and repeatedly paying-out and re-storing lengths of material provided for particular purposes, e.g. anchored hoses, power cables (retractors for storing flexible hoses as accessories of dental work stands A61G15/18; vehicle safety belt retractors B60R22/34; hose-storing devices in apparatus or devices for transferring liquids from bulk storage containers or reservoirs into vehicles or portable containers B67D7/40; clothes-line supports D06F53/00; spring drums for liftable blinds with horizontal lamellae E06B9/322; spring drums or tape drums for roll-type closures or roller blinds E06B9/56; hauling- or hoisting-chains with arrangements for holding electric cables, hoses or the like F16G13/16; devices for guiding pipes, cables or protective tubing, between relatively movable points, e.g. movable channels, F16L3/01; flexible rulers or tapes with scales G01B3/10; electrical features of stored material, see the relevant subclasses, e.g. H02G) · CPC title

• B64G1/66

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

• B64G1/222

  for deploying structures between a stowed and deployed state · CPC title