Synchronously deployable double fold beam and planar truss struc

Static structures (e.g. – buildings) – Openwork; e.g. – truss – trellis – grille – screen – frame – or... – Components adjustably or collapsibly connected

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403 72, E04H 1218

Patent

active

050164180

ABSTRACT:
A deployable structure that synchronously deploys in both length and width is disclosed which is suitable for use as a structural component for orbiting space stations or large satellites. The structure is designed with maximum packing efficiency so that large structures may be collapsed and transported in the cargo bay of the Space Shuttle. The synchronous deployment feature allows the structure to be easily deployed in space without a complex deployment mechanism. The structure is made up of interconnected structural units, each generally in the shape of a parallelepiped. The structural units are constructed of structural members connected with hinged and fixed connections at connection nodes in each corner of the parallelepiped. Diagonal members along each face of the parallelepiped provide structural rigidity and are equipped with mid-length, self-locking hinges to allow the structure to collapse. The structure is designed so that all hinged connections may be made with simple clevis-type hinges requiring only a single degree of freedom, and each hinge pin is located along the centerline of its structural member for high strength and stiffness.

REFERENCES:
patent: 4475323 (1984-10-01), Schwartzberg
patent: 4482900 (1984-11-01), Bilek
patent: 4578920 (1986-04-01), Bush
patent: 4667451 (1987-05-01), Onoda
Deployable Structures for Large Space Platform Systems pp. 1-39 .COPYRGT.NASA Aug. 1982.

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