发明名称 |
COOLING DEVICE FOR USE IN SPACE ENVIRONMENT |
摘要 |
A space-environment dedicated cooling device includes a first flow path to which coolant to be cooled is fed, a second flow path thermally coupled to the first flow path and a water absorbing body which is exposed to the space environment when the cooling device is used in the space environment. The second flow path is fed with feedwater. The water absorbing body is fed with the feedwater from the second flow path. The water absorbing body includes a water absorbing member made of water-absorbing material. |
申请公布号 |
US2013255303(A1) |
申请公布日期 |
2013.10.03 |
申请号 |
US201313803513 |
申请日期 |
2013.03.14 |
申请人 |
MITSUBISHI HEAVY INDUSTRIES, LTD. |
发明人 |
SATO TATSUYA;KANAZAWA RYOICHI |
分类号 |
B64G1/50;F24F5/00 |
主分类号 |
B64G1/50 |
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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