发明名称 |
Conductive shape memory metal deployment latch hinge deployment method |
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. |
申请公布号 |
US2002195177(A1) |
申请公布日期 |
2002.12.26 |
申请号 |
US20010886417 |
申请日期 |
2001.06.21 |
申请人 |
THE AEROSPACE CORPORATION |
发明人 |
HINKLEY DAVID A.;SIMBURGER EDWARD J. |
分类号 |
C22F1/00;E05D1/02;F03G7/06;(IPC1-7):C21D1/00;C21D8/00 |
主分类号 |
C22F1/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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