发明名称 Supersonic Cooling Nozzle with Airfoils
摘要 A supersonic cooling system, as disclosed herein, operates by pumping liquid. Because the supersonic cooling system pumps liquid, the cooling system does not require the use of a condenser. The cooling system utilizes a compression wave to facilitate a phase change utilized in the cooling effect generated by the system. An evaporator operates in the critical flow regime in which the pressure in one or more evaporator nozzles will remain almost constant and then ‘shock up’ to the ambient pressure. The evaporator may be provided with airfoils to improve characteristics of the fluid flow, thereby increasing efficiency of the system.
申请公布号 US2012234027(A1) 申请公布日期 2012.09.20
申请号 US201113048633 申请日期 2011.03.15
申请人 HALT DAVID 发明人 HALT DAVID
分类号 F25D17/02;F25B39/02;F25B41/00 主分类号 F25D17/02
代理机构 代理人
主权项
地址