Retractable deployable structure using a tape spring

Patent metadata

Field	Value
Publication number	US-2016144984-A1
Application number	US-201514945273-A
Country	US
Kind code	A1
Filing date	Nov 18, 2015
Priority date	Nov 21, 2014
Publication date	May 26, 2016
Grant date	—

Abstract

A deployable structure comprises: a mount comprising a first point and a second point opposite and a third point, a storage reel able to rotate about an axis Z, a tape spring able to switch from a configuration in which it is wound about the axis Z in the storage reel into a configuration in which it is deployed along an axis X substantially perpendicular to the axis Z, the first and second points forming a double support with the tape spring to keep the tape spring in the deployed configuration. The third point is able to form a simple support with the tape spring, the storage reel is able to move with respect to the third point and the storage reel is pressed against the third point to guide the deployment of the tape spring.

First claim

1 . A deployable structure comprising:
a mount comprising a first point and a second point opposite and a third point, a storage reel able to rotate about an axis Z, a tape spring able to switch from a configuration in which it is wound about the axis Z in the storage reel into a configuration in which it is deployed along an axis X substantially perpendicular to the axis Z, the first and second points forming a double support with the tape spring so as to keep the tape spring in the deployed configuration, wherein the third point is able to form a simple support with the tape spring, wherein the storage reel is able to move with respect to the third point, wherein the storage reel is pressed against the third point so as to guide the deployment of the tape spring, and wherein the deployable structure comprises
a guide lever comprising two ends, a first of the two ends being pivot connected with respect to the mount, a second of the two ends being secured to the centre of the guide reel,
an elastic element arranged between the guide lever and the mount, and intended to push the guide lever so as to press the storage reel against the third point.

2 . The deployable structure according to claim 1 , wherein the mount comprises a guide device and a base, wherein the first, second and third points are secured to the guide device, and wherein the guide device is articulated with respect to the base and able to rotate about an axis parallel to the axis Z between a closed position and an open position and vice versa.

3 . The deployable structure according to claim 2 , wherein
the first end of the guide lever is pivot connected with respect to the base, the second end is secured to the centre of the guide reel, and wherein the elastic element is positioned between the guide lever and the base and intended to push the guide lever so as to press the storage reel against the third point.

4 . The deployable structure according to claim 3 , comprising a retaining system keeping the guide lever and the guide device in the wound configuration and to release the guide lever and the guide device simultaneously when the tape spring switches from the wound configuration to the deployed configuration.

5 . The deployable structure according to claim 2 , further comprising a cam positioned on the storage reel and wherein the guide device comprises a follower to be guided in such a way as to command the rotation of the guide device.

6 . The deployable structure according to claim 5 , wherein the cam comprises a nonreturn element to prevent the guide device from rotating towards the closed position.

7 . The deployable structure according to claim 1 , the tape spring having two ends, wherein a first end of the tape spring is fixed to the storage reel and wherein a second end of the tape spring is fixed to the base.

8 . The deployable structure according to claim 1 , further comprising a deployable articulated mast fixed on a platform of a satellite by a rotational-drive motor.

9 . A satellite, comprising at least one deployable structure according to claim 8 .

Assignees

• Thales Sa

Inventors

• Baudassé Yannick
• Vézain Stéphane
• Stanek Didier
• Guinot François

Classifications

• B65H75/364 Primary

  the stored material being coiled · CPC title

• B64G1/2229 Primary

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

• B64G1/222 Primary

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

• B64G1/66

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

• B64G1/44

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