초록 ▼

A support structure (1) is provided comprising a plurality of curved surfaces A, B hingedly interconnected along their edges such as to provide effective deployment in two separate stages. Preferably, the structure has only two curved surfaces hingedly interconnected at a single non-planar hinge li

A support structure (1) is provided comprising a plurality of curved surfaces A, B hingedly interconnected along their edges such as to provide effective deployment in two separate stages. Preferably, the structure has only two curved surfaces hingedly interconnected at a single non-planar hinge line. In FIG. 1(a), the two sheets A, B are coplanar in that they lie in the same horizontal plane, permitting the structure to be in a flat, first stage deployment position. In Figure (b), the structure is fully deployed in a second stage deployment position by bringing sheet A out of plane through some angle in relation to the position of sheet B, resulting in both sheets becoming curved. The structure has utility in various space-based as well as terrestrial reflective and absorbing applications, and bears definite advantage in terms of weight saving, high stiffness and well-defined surface precision.

대표청구항 ▼

The invention claimed is: 1. A two-stage deployable antenna support structure comprising: a plurality of interconnected surfaces; means defining at least one curved hinge line along which said surfaces are interconnected; said surfaces being adapted and arranged to provide a package of predetermine

The invention claimed is: 1. A two-stage deployable antenna support structure comprising: a plurality of interconnected surfaces; means defining at least one curved hinge line along which said surfaces are interconnected; said surfaces being adapted and arranged to provide a package of predetermined shape and size; said package being deployable by means of a first unfolding operation of the surfaces to form a substantially flat structure; and said substantially flat structure being further deployable by means of a second unfolding operation of the surfaces to form a well-defined structure. 2. A two-stage deployable support structure comprising: four interconnected surfaces; means defining four curved hinge lines along which said surfaces are interconnected; said surfaces being movable between a first stowed position, in which the surfaces provide a package of predetermined shape and size, and a first deployed position in which two of the surfaces are folded along their respective center lines such that the four surfaces form a substantially flat structure; and said surfaces being further movable between said first deployed position and a second deployed position in which two of said surfaces are concave-shaped opposing surfaces and the other two surfaces are convex-shaped opposing surfaces, the four surfaces forming a well defined structure. 3. A deployable antenna support structure as claimed in claim 1 wherein there are only two surfaces interconnected at a single curved hinge line. 4. A deployable antenna support structure as claimed in claim 1 wherein there are four surfaces linked in a closed configuration and four curved hinge lines associated therewith, wherein in the first deployed position two of the surfaces are folded along their respective center lines and in the second deployed position two of the surfaces are concave-shaped opposing surfaces and the other two surfaces are convex-shaped opposing surfaces. 5. A deployable antenna support structure as claimed in claim 1 wherein one of the surfaces is configured to provide a reflective surface. 6. A deployable antenna support structure as claimed in claim 5 wherein said reflective surface has a parabolic shape. 7. A deployable antenna support structure as claimed in claim 1 wherein said package has a folded Z shape in stowed condition. 8. A deployable antenna support structure as claimed in claim 1 wherein said package has a coil shape in stowed condition. 9. A deployable antenna support structure as claimed in claim 1 further comprising hinge power means for application on the number of hinge lines for powering the two-stage deployment of the structure. 10. A deployable antenna support structure as claimed in claim 9 wherein said hinge power means is provided by a number of tape-spring hinges selectively added to the walls of the structure. 11. A deployable antenna support structure as claimed in claim 1 further comprising locking means for latching the structure in deployed position. 12. A deployable antenna support structure as claimed in claim 1 wherein the structure is formed of lightweight composite material. 13. A deployable antenna support structure as claimed in claim 12 wherein the lightweight composite material comprises carbon-fibre composite material. 14. A deployable antenna support structure as claimed in claim 1 wherein the surfaces are formed of thin sheet material of micron-size thickness. 15. A reflector system for space-based applications incorporating a deployable antenna support structure as claimed in claim 1. 16. A spacecraft incorporating a reflector system as claimed in claim 15. 17. A synthetic aperture radar (SAR) satellite incorporating a reflector system as claimed in claim 15. 18. A method of deploying an antenna support structure in two stages comprising the steps of: (a) providing a package of predetermined shape and size in stowed condition, which package comprises a plurality of interconnected surfaces with means defining a number of curved hinge lines along which the surfaces are interconnected; (b) unfolding the surfaces of the package so as to form a substantially flat structure for first stage deployment; and (c) unfolding the surfaces of the substantially flat structure about the curved hinge lines so as to form a well-defined structure for second stage deployment. 19. A deployable antenna support structure as claimed in claim 1 wherein one of the surfaces is configured to provide an absorbing surface.