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
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