Design of a Deployable Antenna Actuated by Shape Memory Alloy Hinge

Author:

Lan Xin1,Leng Jin Song1,Du Shan Yi1

Affiliation:

1. Harbin Institute of Technology

Abstract

This paper is concerned about a design of a new deployable antenna actuated by 6 shape memory alloy (SMA) hinges. The antenna consists of 6 radial, tensioned, parabolic, deployable ribs connecting to a central hub. The hinge, located at each rib, is used of the Nitinol SMA material due to the ability to generate large strains and electrical resistive actuation. The elongated SMA wire is heated by an electrical current, caused to contract in response to a converse thermally-induced phase transformation. The resulting tension creates a moment, imparting rotary motion between two adjacent beams. The concept and operation of deployable antenna system are discussed in detail, and a dynamic simulation is presented. A series of experiments are performed on the SMA actuator to investigate the system behavior in the process of deployment. Results indicated that the hinge with low speed rotation and easy fabrication achieves reliable actuation for the deployment of the antenna, and the antenna demonstrates a high deployment-to-stowage volume ratio.

Publisher

Trans Tech Publications, Ltd.

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,General Materials Science

Reference7 articles.

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3. Gunnar Tibert, Deployable Tensegrity Structures for Space Applications, Royal Institute of Technology (Doctoral Thesis), 2002, pp.16-26.

4. Jin Mitsugi, Kazuhide Ando, Yumi Senbokuya And Akira Meguro, Deployment analysis of large space antenna using flexible multibody dynamics simulation. Acta Astronautica Vol. 47(2000), No. 1, pp.19-26.

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