Claims
- 1. A foldable structural member comprising:
- a plurality of longitudinal segments, each of said longitudinal segments having sides;
- connector means connecting said longitudinal segments, said connector means arranged so that said connector means describe a planar configuration, when the longitudinal segments are deployed in a substantially straight line, and describe a cylindrical configuration, when the segments are folded into a helical configuration for stowage; and
- tensioning means associated with the sides of said member opposite said side having said connector means causing all of said segments to simultaneously pivot about the axes of said connector means from a stowed helical configuration into a deployed substantially straight line configuration, to be held deployed by said tensioning means.
- 2. The member of claim 1 wherein each of said longitudinal segments comprises a plurality of at least three equilength rigid, lightweight tubular longerons parallel to each other and reinforced by a plurality of trusses and diagonal members.
- 3. The member of claim 2 wherein at least two of said longerons are pivotally connected by rigid diagonals to the longerons of both of the adjacent longitudinal segments corresponding to the opposite of said longerons, whereby the contraction of said tensioning means and resultant approach of adjacent longitudinal segment forces the opposite sides apart and conversely the separation of said segments pulls the sides together in a scissor-like fashion.
- 4. The member of claim 2 wherein the said longerons comprising one of the said longitudinal segments are fixedly connected; and wherein the said connector means are disposed between two of the said longerons and each of the two corresponding longerons of adjacent longitudinal segments; and wherein the said tensioning means is threaded through others of the said longerons.
- 5. The member of claim 4 wherein said connector means is a plurality of hinges; said hinges having axes all of which, while remaining parallel to each other, are canted from the normal to the axes of the longerons which they connect, whereby the path formed by the folding of successive longitudinal segments approximates a helix, so that said member may be folded into multiple revolutions.
- 6. The member of claim 2 wherein said longerons are three in number, said connector means are disposed between one of the longerons and each of the corresponding longerons of adjacent longitudinal segments; and wherein the said tensioning means is threaded through the remaining two of the said longerons.
- 7. The member of claim 7 wherein:
- the said two of the longerons with which the said tensioning means are associated have truss means pivotally connecting them to the said longeron having connector means associated therewith; and
- wherein the said two longerons are not directly connected to each other, but rather are pivotally connected by rigid diagonals to the longerons of both of the said adjacent longitudinal segments corresponding to the opposite of the said two longerons, whereby the contraction of the said tensioning means and resultant approach of adjacent longitudinal segments forces the opposite sides apart, and conversely, the separation of the longitudinal segments pulls the sides together.
- 8. The member of claim 7 wherein the said tensioning means is a cable.
ORIGIN OF THE INVENTION
The invention described herein was made in the performance of work under a NASA contract and is subject to the provisions of Section 305 of the National Aeronautics and Space Act of 1958, Public Law 85-568 (72 Stat. 435; USC 2457).
US Referenced Citations (2)
Number |
Name |
Date |
Kind |
3209508 |
Hunnebeck |
Oct 1965 |
|
3312020 |
Schuster |
Apr 1967 |
|
Foreign Referenced Citations (2)
Number |
Date |
Country |
1052362 |
Jan 1944 |
FRX |
122846 |
|
GBX |