Deployable satellite mast

Patent metadata

Field	Value
Publication number	US-11772825-B2
Application number	US-201816652893-A
Country	US
Kind code	B2
Filing date	Oct 1, 2018
Priority date	Oct 4, 2017
Publication date	Oct 3, 2023
Grant date	Oct 3, 2023

Abstract

A deployable satellite mast consisting of an inflatable tube, which is stored in fan-fold form before deployment and can be deployed by filling the tube with a gas, and which comprises a device for reinforcing and facilitating the deployment of the mast, which device is external to the mast and comprises one or more stays, first ends of which are wound on a reel device and second ends of which are secured to the tube, with the stays unwinding from the reel when the mast is deployed.

First claim

What is claimed is:

1. A deployable mast for a satellite consisting of an inflatable tube stored in an accordion shape before deployment and deployable by filling the inflatable tube by means of a gas, the mast including a rigidification and deployment-assist device external to the mast, said device including one or more stays, each stay is wound on a reel device at a first end and attached to the inflatable tube at a second end, said stays unwinding from the reel device upon deploying the mast, wherein said one or more stays further comprise a pair of stays disposed at 180° relative to the mast axis, wherein the pair of stays are wound on a single reel device, and wherein the pair of stays each have a second respective end attached to the inflatable tube, and wherein the pair of stays are synchronized by a connecting cable unwound from a first reel of the reel device and wound in opposition from a second reel of the reel device during unwinding of the stays.

2. The deployable mast according to claim 1 , wherein at least some of the stays are fastened to the free end of the inflatable tube becoming the apex of the mast after deployment.

3. The deployable mast according to claim 1 , wherein at least some of the stays are fastened to an intermediate part of the inflatable tube.

4. The deployable mast according to claim 1 , wherein the rigidification device comprises at least two pairs of stays disposed in planes intersecting at the mast axis.

5. The deployable mast according to claim 1 , wherein the stays are ropes a composition of which comprises polymers solidifying by UV irradiation or ropes that are rigidifiable by Joule effect polymerisation.

6. The deployable mast according to claim 1 , wherein the reel device includes a brake device for keeping the stays tensioned upon deploying the mast.

7. The deployable mast according to claim 1 , wherein at the base of the mast, the stays are held spaced from the mast by arms formed by fixed beams or foldable rods perpendicular or tilted relative to the mast.

8. The deployable mast according to claim 1 , wherein at least one spring is disposed either at the top of the stays or at the end of the stays on the reel side or on both sides.

9. The deployable mast according to claim 1 , further comprising tabs, each tab is perforated at a middle of the respective tab for passing a cable in the mast surround said cable.

Assignees

• Arianegroup Sas

Inventors

• Villemain Alexis

Classifications

• B64G1/44 Primary

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

• B64G1/2227

  Inflating · CPC title

• B64G1/222 Primary

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

• B64G2001/224

  Operations & Transport · mapped topic

• H01Q1/081

  Inflatable antennas · CPC title