发明名称 |
Supersonic Cooling with a Pulsed Inlet |
摘要 |
A supersonic cooling system operates by pumping liquid without the need of a condenser. The compression system utilizes a compression wave in the generation of the cooling effect. An inlet of the system may be pulsed to reduce energy required of a pump. The evaporator of compression system operates in the critical flow regime where the pressure one or more evaporator tubes will remain almost constant and then ‘jump’ or ‘shock up’ to the ambient pressure. |
申请公布号 |
US2012204593(A1) |
申请公布日期 |
2012.08.16 |
申请号 |
US201113028083 |
申请日期 |
2011.02.15 |
申请人 |
GIELDA TOM;DEBUS KRISTIAN;CHARAMKO SERGUEI |
发明人 |
GIELDA TOM;DEBUS KRISTIAN;CHARAMKO SERGUEI |
分类号 |
F25D17/00 |
主分类号 |
F25D17/00 |
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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