自主形状记忆铰链,用于太阳能驱动的空间应用

Arvind Gurusekaran, Hugo de Souza Oliveira, V. Benedetti, M. Baratieri, N. Münzenrieder, M. Ciocca, P. Lugli, L. Petti
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引用次数: 0

摘要

这项工作展示了用于部署卫星散热器的概念验证自主铰链。由于使用了形状记忆合金(SMA),铰链利用了形状记忆效应(SME)。首先,将基于镍钛的SMA钢丝嵌入Ecoflex聚合物材料中,随后进行固化。铰链的弯曲是由印在10 μ m$厚聚醚醚酮(PEEK)基板上并嵌入SMA结构顶部的银基加热器提供的热刺激引起的。加热器供电是通过市售太阳能电池实现的。加热后,铰链由平面水平结构转变为铰链两侧弯曲角度约为45°的弯曲结构。在这项工作中,我们首先描述了铰链的工作原理,然后展示了铰链是如何设计和原型的,以及概念验证装置的实现。最后,对自主铰链样机进行了实验室测试,研究了其运动性能和能耗性能。在通过关闭加热器降低SMA电线的温度后,铰链以10°的弯曲角度返回其原始位置。结果证明,铰链能够根据温度弯曲和不弯曲,同时由太阳能电池供电,例如利用空间太阳辐射。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Autonomous shape memory hinge for space applications powered via solar energy
This work demonstrates a proof-of-concept autonomous hinge for the deployment of satellite radiators. The hinge utilizes the shape memory effect (SME), thanks to the use of a shape memory alloy (SMA). First SMA wires based on Nickel-Titanium are embedded into an Ecoflex polymeric material and subsequently solidified. The bending of the hinge is induced by a thermal stimulus provided by a silver-based heater printed on a $10\mu m$ thick Polyether ether ketone (PEEK) substrate and embedded on top of the SMA structure. Heater powering is achieved via commercially available solar cells. Upon heating, the hinge transforms from a flat horizontal configuration to a curved bent one with approximately 45° bending angle on both sides of the hinge. In this work, we first describe the working principle of the hinge, to then show how the hinge is designed and prototyped, along with the realization of the proof-of-concept-device. Finally, laboratory testing of the autonomous hinge prototype is shown to investigate its motion and energy consumption performance. Upon reducing the temperature of the SMA wires by switching off the heater, the hinge returns to its original position with a 10° bending angle. The results prove that the hinge is capable of bending and unbending depending on the temperature, while being powered through solar cells using e.g., space solar radiation.
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