发明名称 |
Supersonic Cooling With Pulsed Inlet and Bypass Loop |
摘要 |
A supersonic cooling system operates by pumping liquid without the need of a condenser. An inlet of the system may be pulsed to reduce energy required of a pump and to increase the cooling power of the system. The supersonic cooling system utilizes a compression wave in the generation of the cooling effect. The formation of the compression wave may be assisted by a resonance chamber. An evaporator of the cooling system operates in the critical flow regime. |
申请公布号 |
US2012301268(A1) |
申请公布日期 |
2012.11.29 |
申请号 |
US201113115930 |
申请日期 |
2011.05.25 |
申请人 |
GIELDA TOM;DEBUS KRISTIAN;ASHER WILL |
发明人 |
GIELDA TOM;DEBUS KRISTIAN;ASHER WILL |
分类号 |
F01D25/12 |
主分类号 |
F01D25/12 |
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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