DEPLOYABLE SATELLITE MAST

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.

Claims

1. A deployable mast for a satellite consisting of an inflatable tube (1) stored in an accordion shape (1a) before deployment (1b) and deployable by filling the 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 (2a, 2b) wound on a reel device (3, 31, 32, 33, 34) at a first one of their ends and attached to the tube at a second one of their ends, said stays unwinding from the reel upon deploying the mast.

2. The deployable mast according to claim 1, wherein the rigidification device comprises at least one pair of stays disposed at 180 relative to the mast axis.

3. The deployable mast according to claim 2, wherein the stays of the pair of stays are wound on a single reel device (33).

4. The deployable mast according to claim 2, wherein the reel device comprises a reel (32, 32) per stay, the reels of a pair of stays being synchronised by a connecting cable (40) arranged to be unwound from the first one (32) of the reels and wound in opposition on a second one (32) of the reels during unwinding of the stays.

5. The deployable mast according to claim 1, wherein at least some of the stays (2a) are fasten to the free end of the tube becoming the apex of the mast after deployment.

6. The deployable mast according to claim 1, wherein at least some of the stays (2b) are fastened to an intermediate part of the tube.

7. The deployable mast according to claim 1, wherein the rigidification device comprises at least two pairs of stays (21, 22, 21, 22) disposed in planes intersecting at the mast axis.

8. The deployable mast according to claim 1, wherein the stay(s) is or are ropes a composition of which comprises polymers solidifying by UV irradiation or ropes that are rigidifiable by Joule effect polymerisation.

9. The deployable mast according to claim 3, wherein the reel(s) include(s) a brake device for keeping stays tensioned upon deploying the mast.

10. The deployable mast according to claim 1, wherein at the base of the mast, stays are held spaced from the mast by arms (50) formed by fixed beams (51) or foldable rods (52) perpendicular or tilted relative to the mast.

11. The deployable mast according to claim 1, wherein at least one spring (71, 72) is disposed either at the top of the stays (71) or at the end of the stay on the reel side (72) or on both sides.

12. The deployable mast according to claim 1, wherein flexible tabs (61, 62) perforated at the middle thereof for passing a cable in the mast surround said cable.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0021] Further characteristics and advantages of the invention will appear upon reading the following description of non-limiting exemplary embodiments of the invention with reference to the drawings which represent:

[0022] in FIG. 1, a schematic representation of a mast deployment of prior art;

[0023] in FIGS. 2A-2D, schematic examples in a side view of embodiments of masts according to the invention;

[0024] in FIGS. 3A-3B, perspective views of exemplary embodiments of the invention;

[0025] in FIGS. 4A-4C, exemplary embodiments of reel means of the invention;

[0026] in FIGS. 5, 6 and 7, perspective views of reels applicable to the invention;

[0027] in FIG. 8, a particular exemplary embodiment of the mast.

DETAILED DESCRIPTION OF EMBODIMENTS OF THE INVENTION

[0028] The present invention is concerned with structures which can be deployed on a satellite such as for example a structure which can in particular support solar panels and adapted to withstand stresses and strains created by these panels such as stresses and strains created by the thermal environment and motions of the satellite. It fulfils technical needs which are assisting in guiding the mast during its deployment and bringing stiffness to the mast after deployment.

[0029] The invention relates to a deployable mast 1 such as depicted in FIG. 1 and mainly consisting of an inflatable tube 10, stored in an accordion shape 1a before deployment, and deployable by filling the tube by means of a gas according to a sequence such as represented, the deployed tube 1b forming a carrying structure.

[0030] To assist in deploying the tube and rigidify it, the invention provides stays external to the tube as represented in FIGS. 2A to 2C.

[0031] Stays are flexible structures of the cable or wire type which can be made from different materials: metal, composite, polymers, etc.

[0032] FIG. 2A represents a deployed mast provided with a pair of stays 21 which are fastened to the free end of the tube 10 becoming the apex of the mast after deployment.

[0033] FIG. 2B represents a deployed mast including a pair of stays 22 fastened to the intermediate part of the deployed tube.

[0034] FIG. 2C represents a deployed mast including two pairs of stays 21, 22. A pair of stays 21 is fastened at the top of the mast and a pair of stays 22 is fastened to the intermediate part of the deployed tube.

[0035] In the example of FIGS. 2A to 2C, the bottom part of the stays is fastened at a distance from the mast to fixed beams 51. In the example of FIG. 2D, the lower part of the stays is held spaced from the mast by foldable rods 52 possibly perpendicular to the mast and lower strands 23 of the stays are used to tension stays.

[0036] The rigidification and deployment-assist device external to the mast of the invention includes, according to FIGS. 4A to 4C, reels on which the stays are wound when the tube is stored folded and from which the stays are unwound upon deploying the mast.

[0037] In the example of FIG. 4A, a single reel 33 receives two stays 21, 21 of a pair of coplanar stays on winding cylinders or bobbins 33a, 33b with opposite winding directions and pulleys 3a at the end of beams 50 guide the stays. The reel is for example such as represented in FIG. 5. This reel is a triple reel which includes a first winding cylinder 33a for a first stay of a pair of stays, a second winding cylinder 33b for a second stay of the pair of stays and, in this embodiment, a third cylinder 33c receiving a cable internal to the tube and attached to the free end of the tube and used to control uncoiling of stays during deployment of the mast, the free end of the tube pulling on the inner cable. In this configuration, the diameter of cylinders is adapted so that unwinding stays is synchronised with deploying the mast.

[0038] In the example of FIG. 4B, each stay of the pair of stays includes a contrarotating reel 32, 32. These reels are synchronised by a connecting cable 40 connecting them which is more particularly represented in FIG. 4C. This connecting cable 40 is unwound from a first winding cylinder or bobbin on a first reel, for example the reel 32 and is wound on a second winding cylinder or bobbin on the second reel, for the reel 32 upon deploying the mast. In this case, the reels are made according to the example of FIG. 6. They include a first winding cylinder 32a receiving the stay 21, a second winding cylinder receiving the connecting cable 40.

[0039] The reel represented in FIG. 7 is an exemplary reel receiving a head stay 21 and a stay 22 attaching to an intermediate part of the mast. In this case the ratio of diameters of the winding cylinders receiving the stays is adapted to keep an identical tension for these stays upon deploying the mast.

[0040] The stays can be flexible cables of different materials, metal, composite, polymers, etc. or rigidifiable ropes such as rigidifiable ropes by Joule effect polymerisation after flowing an electric current into the rope. Another embodiment can use stays including a UV polymerisable material. In the latter case, once unwound and subjected to the sun UV irradiation, the stays can rigidify and even better contribute to hold the mast erected.

[0041] Still for the purpose of controlling the deployment of the mast, the reel(s) can include a brake device for keeping the stays tensioned during deployment of the mast.

[0042] FIG. 3A describes in a perspective view an embodiment with two pairs of coplanar stays disposed at 180 relative to the mast axis.

[0043] According to FIG. 3B, the rigidification device comprises four pairs of stays 21, 21, 22, 22 disposed in twos in planes intersecting at the mast axis. In the example, by taking a plane P defined by the mast and a straight line A perpendicular to the mast, in which plane for example the solar panels are, the plane including a first pair of stays fastened at the top of the mast and a first pair of stays fastened at an intermediate part of the mast, forms with a plane P an angle whereas the plane including the second pair of stays fastened at the top of the mast and the second pair of stays fastened at an intermediate part of the mast forms an angle with plane P.

[0044] According to the example of FIG. 9, in order to absorb thermal expansions of the stays as a function of their material, elongation thermal expansions of the mast, the slake of the stay opposed to the other which would undergo a tensile warp, a slight tension is brought at the end of deployment, without hampering plastic deformation by inflation of the mast, by adding springs either at the top of the stays, as the spring 71, or at the end of the stay, as the spring 72 on the reel side, or on both sides. Springs can be of the coil spring or elastic cable type spring at the top part of the stay. However, at the bottom part of the stay, since the spring is initially wound on the reel, an elastic cable type spring then acting after complete reeling of the stays will be preferred.

[0045] In the case a central cable is positioned inside the tube a means for preventing the cable from striking the mast after deployment has to be found. In this case, it is possible to position, as represented in FIG. 8, flexible tabs 61, 62, for example made of kapton, perforated at the middle thereof for passing the cable. These tabs which surround the cable can especially be bonded between the folded parts of the mast according to mark 63.

[0046] The invention therefore provides staying the mast which brings bending and tensile stiffness to the mast after deployment and a synchronised unwinding of the stays which brings an assistance in guiding the mast upon deploying the mast.