公开(公告)号：US20110088878A1

公开(公告)日：2011-04-21

申请号：US12961342

申请日：2010-12-06

Applicant: Jayden Harman ,  Thomas Gielda

Inventor： Jayden Harman ,  Thomas Gielda

IPC: F28D15/00 ,  F28F13/00

CPC classification number: F25B1/00

Abstract: A supersonic cooling system operates by pumping liquid. Because the supersonic cooling system pumps liquid, the compression system does not require the use of a condenser. The compression system utilizes a compression wave. An evaporator of the compression system operates in the critical flow regime where the pressure in an evaporator tube will remain almost constant and then ‘jump’ or ‘shock up’ to the ambient pressure.

Abstract translation: 超音速冷却系统通过泵送液体进行操作。 由于超音速冷却系统泵送液体，压缩系统不需要使用冷凝器。 压缩系统利用压缩波。 压缩系统的蒸发器在临界流动状态下工作，其中蒸发器管中的压力将保持几乎恒定，然后“环绕”或“缓冲”到环境压力。

公开(公告)号：US20110088419A1

公开(公告)日：2011-04-21

申请号：US12960979

申请日：2010-12-06

Applicant: Jayden Harman ,  Thomas Gielda

Inventor： Jayden Harman ,  Thomas Gielda

IPC: F25B1/00

CPC classification number: F25B1/00

Abstract: A supersonic cooling system operates by pumping liquid. Because the supersonic cooling system pumps liquid, the compression system does not require the use of a condenser. The compression system utilizes a compression wave. An evaporator of the compression system operates in the critical flow regime where the pressure in an evaporator tube will remain almost constant and then ‘jump’ or ‘shock up’ to the ambient pressure.

Abstract translation: 超音速冷却系统通过泵送液体进行操作。 由于超音速冷却系统泵送液体，压缩系统不需要使用冷凝器。 压缩系统利用压缩波。 压缩系统的蒸发器在临界流动状态下工作，其中蒸发器管中的压力将保持几乎恒定，然后“环绕”或“缓冲”到环境压力。

公开(公告)号：US20110051549A1

公开(公告)日：2011-03-03

申请号：US12843834

申请日：2010-07-26

Applicant: Kristian Debus ,  Thomas Gielda ,  Serguei Charamko ,  Balaji Maniam

Inventor： Kristian Debus ,  Thomas Gielda ,  Serguei Charamko ,  Balaji Maniam

IPC: B01F13/00

CPC classification number: F15D1/02

Abstract: A central insert causes maximum fluid velocity to shift away from an external tube wall reducing friction losses at the tube wall. Centrifugal forces pull fluid away from a central insert wall minimizing friction at the insert wall. The insert may be used in the context of nozzles, flow tubes, vortex tubes, and other fluid pathways. In a nozzle, grooves may be added to the nozzle wall. By introducing these grooves at the exit or end of a nozzle, nucleation may be improved and cavitation may be triggered prior to a fluid entering an expansion tube. The nucleation ring may also be placed at the beginning of a nozzle such that cavitation starts within the nozzle.

Abstract translation: 中央插入件使最大流体速度从外管壁移开，减少管壁处的摩擦损失。 离心力将流体从中心插入物壁拉出，从而最小化插入壁处的摩擦力。 插入物可以在喷嘴，流量管，涡流管和其它流体通路的上下文中使用。 在喷嘴中，可以向喷嘴壁添加凹槽。 通过在喷嘴的出口或端部引入这些凹槽，可以改善成核，并且在流体进入膨胀管之前可以触发空化。 成核环也可以放置在喷嘴的开始处，使得在喷嘴内开始空化。

公开(公告)号：US20100287954A1

公开(公告)日：2010-11-18

申请号：US12732171

申请日：2010-03-25

Applicant: Jayden Harman ,  Thomas Gielda

Inventor： Jayden Harman ,  Thomas Gielda

IPC: F25B9/02 ,  F25B1/00

CPC classification number: F25B1/00

Abstract: A supersonic cooling system operates by pumping liquid. Because supersonic cooling system pumps liquid, the compression system does not require the use a condenser. Compression system utilizes a compression wave. The evaporator of compression system operates in the critical flow regime where the pressure in an evaporator tube will remain almost constant and then ‘jump’ or ‘shock up’ to the ambient pressure.

Abstract translation: 超音速冷却系统通过泵送液体进行操作。 因为超音速冷却系统泵送液体，所以压缩系统不需要使用冷凝器。 压缩系统利用压缩波。 压缩系统的蒸发器在临界流动状态下工作，其中蒸发器管中的压力将保持几乎恒定，然后“环绕”或“缓冲”到环境压力。