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Conductive shape memory metal deployment latch hinge deployment method

机译:导电形状记忆金属展开闩锁铰链展开方法

摘要

A conductive hinge is made of a superelastic shape memory alloy such as nitinol (NiTi) having a large elastic strain limit for enabling the hinge to bend to a small radius during stowage for flexible return to a trained rigid hinge position by training the shape memory alloy to assume a predetermined deployed configuration when released from a stowage configuration. The hinge is trained by forging at a temperature above a training temperature. The hinge is released to deploy solar cell panels as the hinges unfold to the forged trained deployed configuration.
机译:导电铰链由诸如镍钛诺(NiTi)之类的超弹性形状记忆合金制成,该合金具有较大的弹性应变极限,可在存放期间使铰链弯曲至较小的半径,从而通过训练形状记忆合金而灵活地返回到经过训练的刚性铰链位置从存放配置中释放时,将采用预定的部署配置。通过在高于训练温度的温度下锻造来训练铰链。当铰链展开到锻造的经过训练的展开结构时,释放铰链以展开太阳能电池板。

著录项

  • 公开/公告号US2002195177A1

    专利类型

  • 公开/公告日2002-12-26

    原文格式PDF

  • 申请/专利权人 THE AEROSPACE CORPORATION;

    申请/专利号US20010886417

  • 发明设计人 EDWARD J. SIMBURGER;DAVID A. HINKLEY;

    申请日2001-06-21

  • 分类号C21D1/00;C21D8/00;

  • 国家 US

  • 入库时间 2022-08-22 00:09:30

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