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公开(公告)号：US20110030390A1
公开(公告)日：2011-02-10
申请号：US12753824
申请日：2010-04-02
申请人： Serguei Charamko , Balaji Maniam
发明人： Serguei Charamko , Balaji Maniam
IPC分类号： F25B9/04
摘要： A vortex tube allowing for control of the velocities, flow, and pressure differentials otherwise present in a free vortex like that found in a tornado is disclosed. The presently disclosed vortex tube may be used for the control and implementation of the otherwise chaotic aspects of a true tornado and vortex (i.e., with less energy and a narrowed and more focused and intense vortex) when implementing the critical flow regime in a fluid flow system.
摘要翻译： 公开了一种允许控制如在龙卷风中发现的自由涡旋中存在的速度，流量和压力差的涡流管。 当在流体流中实现临界流动状态时，目前公开的涡流管可用于控制和实施真正的龙卷风和涡流（即，具有更少的能量和更窄的和更集中和强烈的涡流）的混沌方面 系统。
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公开(公告)号：US20110051549A1
公开(公告)日：2011-03-03
申请号：US12843834
申请日：2010-07-26
申请人： Kristian Debus , Thomas Gielda , Serguei Charamko , Balaji Maniam
发明人： Kristian Debus , Thomas Gielda , Serguei Charamko , Balaji Maniam
IPC分类号： B01F13/00
CPC分类号： F15D1/02
摘要： 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.
摘要翻译： 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。
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公开(公告)号：US20120260676A1
公开(公告)日：2012-10-18
申请号：US13088593
申请日：2011-04-18
申请人： Serguei Charamko
发明人： Serguei Charamko
CPC分类号： F25B23/00
摘要： Cooling via acceleration of a compressible fluid is disclosed. The fluid is accelerated by a rotatable body to a velocity that may be equal to or greater than the speed of sound in the fluid. No conventional mechanical pump is required to accelerate the fluid. A phase change of the fluid may be utilized to transfer heat from an element to be cooled.
摘要翻译： 公开了通过可压缩流体的加速冷却。 流体通过旋转体加速至可等于或大于流体中的声速的速度。 不需要常规的机械泵来加速流体。 流体的相变可用于从要冷却的元件传递热量。
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公开(公告)号：US20120118538A1
公开(公告)日：2012-05-17
申请号：US12945799
申请日：2010-11-12
申请人： Thomas Gielda , Kristian Debus , Serguei Charamko
发明人： Thomas Gielda , Kristian Debus , Serguei Charamko
IPC分类号： F28D15/00
CPC分类号： F25B1/06 , F28D11/04 , F28D2021/0028 , F28F2250/08
摘要： A method of cooling that accelerates a compressible working fluid without the use of a pump. The method accelerates the fluid to a velocity equal to or greater than the speed of sound in the compressible fluid selected to be used in the method. The fluid is accelerated to a supersonic velocity in a rotating evaporator tube. A phase change of the fluid due to a pressure differential may be utilized to transfer heat from an element to be cooled.
摘要翻译： 一种冷却方法，可以在不使用泵的情况下加速可压缩的工作流体。 该方法将流体加速至等于或大于选择用于该方法的可压缩流体中的声速。 流体在旋转的蒸发器管中被加速到超音速。 可以利用由于压力差导致的流体的相变来从要冷却的元件传递热量。
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公开(公告)号：US20120260673A1
公开(公告)日：2012-10-18
申请号：US13087062
申请日：2011-04-14
申请人： Serguei Charamko , Kristian Debus , Tom Gielda
发明人： Serguei Charamko , Kristian Debus , Tom Gielda
IPC分类号： F25B9/00
CPC分类号： F25B1/00
摘要： Cooling in the supersonic region of a compressible fluid is disclosed. The fluid is accelerated by a reciprocating piston to a velocity equal to or greater than the speed of sound in the fluid in an evaporator. No conventional mechanical pump is required to accelerate the fluid. A phase change of the fluid due to a pressure differential may be utilized to transfer heat from an element to be cooled.
摘要翻译： 公开了可压缩流体的超音速区域中的冷却。 流体通过往复式活塞加速至等于或大于蒸发器中流体中的声速的速度。 不需要常规的机械泵来加速流体。 可以利用由于压力差导致的流体的相变来从要冷却的元件传递热量。
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公开(公告)号：US5676536A
公开(公告)日：1997-10-14
申请号：US532209
申请日：1995-11-13
申请人： Andreas Ruhl , Patrick McGehee , Kim Anderson , Serguei Charamko
发明人： Andreas Ruhl , Patrick McGehee , Kim Anderson , Serguei Charamko
CPC分类号： F23G7/065 , F23D14/62 , F23G2207/102 , F23G2207/20
摘要： Raw gas burner that maximizes fuel efficiency of the burner, minimizes residence time, and reduces or eliminates flame contact with the process air or gas in order to minimize NOx formation. Process air flow such as from the cold side of a heat exchanger associated with thermal oxidizer apparatus is directed into and around the burner. The amount of process air flowing into the burner is regulated based upon the pressure drop created by the burner assembly. The pressure drop is, in turn, regulated by one or more of an external damper assembly, an internal damper assembly, and movement of the burner relative to the apparatus in which it is mounted. To ensure thorough mixing of the fuel and process air, process air entering the burner is caused to spin by the use of a swirl generator. The fuel/process air mixture proceeds into the combustion section of the burner, where the swirling flow is caused to recirculate to ensure complete combustion of the fuel in the combustion chamber. The mixture of burned fuel and process gas transfers its energy flamelessly to the process gas circulating outside the burner combustion chamber, and is hot enough to ignite the process gas there, which then burns separately from the burner combustion chamber, such as in the main combustion enclosure of the thermal post-combustion device.
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公开(公告)号：US20120000631A1
公开(公告)日：2012-01-05
申请号：US13039121
申请日：2011-03-02
申请人： Serguei Charamko , Kristian Debus , Tom Gielda
发明人： Serguei Charamko , Kristian Debus , Tom Gielda
CPC分类号： F25B1/06 , F28D11/04 , F28D2021/0028 , F28F2250/08 , F28F2265/14
摘要： Disclosed herein is a cooling system that utilizes a supersonic cooling cycle. The cooling system includes accelerating a compressible working fluid, and may not require the use of a conventional mechanical pump. The cooling system accelerates the fluid to a velocity equal to or greater than the speed of sound in the compressible fluid selected to be used in the system. A phase change of the fluid due at least in part to a pressure differential cools a working fluid that may be utilized to transfer heat from a heat intensive system.
摘要翻译： 本文公开了利用超音速冷却循环的冷却系统。 冷却系统包括加速可压缩的工作流体，并且可以不需要使用传统的机械泵。 冷却系统将流体加速至等于或大于选择用于系统中的可压缩流体中的声速。 至少部分地由压力差导致的流体的相变使得可用于从热密集系统传递热量的工作流体冷却。
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8.发明授权
公开(公告)号：US5609833A
公开(公告)日：1997-03-11
申请号：US532210
申请日：1995-09-22
申请人： Andreas R uhl , Gert Rentzel , Patrick McGehee , Serguei Charamko , Kim Anderson
发明人： Andreas R uhl , Gert Rentzel , Patrick McGehee , Serguei Charamko , Kim Anderson
摘要： Process and apparatus for burning combustible constituents in process gas in a main combustion enclosure, preferably a thermal post-combustion device, whereby the main combustion enclosure is separated from a combustion chamber, into which oxygenic gas and gaseous fuel are fed, mixed and burnt. The fuel for the apparatus is fed through a lance which opens into a mixing chamber supplied with oxygenic gas, which is either itself the combustion chamber or merges with it, and the outer surface of the combustion chamber is exposed at least partially to the process gas. The fuel is burned completely or nearly completely in the burner combustion chamber and the mixture of burned fuel and gas leaving the combustion chamber oxidizes the combustible constitutes in the process gas flowing outside of the combustion chamber by yielding flameless heat energy to them.
摘要翻译： 用于燃烧主燃烧外壳中的工艺气体中的可燃组分的方法和装置，优选热后燃烧装置，由此主燃烧外壳与燃气室分离，氧气和气体燃料进入燃烧室，混合燃烧。 用于该设备的燃料通过喷枪进入，该喷枪通向供应有氧气的混合室，该混合室本身是燃烧室或与其合并，并且燃烧室的外表面至少部分暴露于工艺气体 。 燃料在燃烧器燃烧室中被完全燃烧或几乎完全燃烧，并且燃烧的燃料和离开燃烧室的气体的混合物氧化了在燃烧室外面流动的工艺气体中构成的可燃物通过向它们产生无焰的热能。
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9.发明授权Raw gas burner and process for burning oxygenic constituents in process gas 失效原燃气燃烧器和燃烧过程气体中含氧成分的方法
公开(公告)号：US5601789A
公开(公告)日：1997-02-11
申请号：US356601
申请日：1994-12-15
申请人： Andreas Ruhl , Patrick McGehee , Kim Anderson , Serguei Charamko
发明人： Andreas Ruhl , Patrick McGehee , Kim Anderson , Serguei Charamko
CPC分类号： F23G7/065 , F23D14/62 , F23G2207/102 , F23G2207/20
摘要： Raw gas burner that maximizes fuel efficiency of the burner, minimizes residence time, and reduces or eliminates flame contact with the process air or gas in order to minimize NOx formation. Process air flow such as from the cold side of a heat exchanger associated with thermal oxidizer apparatus is directed into and around the burner. The amount of process air flowing into the burner is regulated based upon the pressure drop created by the burner assembly. The pressure drop is, in turn, regulated by one or more of an external damper assembly, an internal damper assembly, and movement of the burner relative to the apparatus in which it is mounted. To ensure thorough mixing of the fuel and process air, process air entering the burner is caused to spin by the use of a swirl generator. The fuel/process air mixture proceeds into the combustion section of the burner, where the swirling flow is caused to recirculate to ensure complete combustion of the fuel in the combustion chamber. The mixture of burned fuel and process gas transfers its energy flamelessly to the process gas circulating outside the burner combustion chamber, and is hot enough to ignite the process gas there, which then burns separately from the burner combustion chamber, such as in the main combustion enclosure of the thermal post-combustion device.
摘要翻译： 原燃气燃烧器使燃烧器的燃油效率最大化，最小化停留时间，并减少或消除与过程空气或气体的火焰接触，以最小化NOx的形成。 来自与热氧化装置相关联的热交换器的冷侧的处理空气流被引导到燃烧器中和周围。 基于由燃烧器组件产生的压降来调节流入燃烧器的过程空气量。 压降又由一个或多个外部阻尼器组件，内部阻尼器组件和燃烧器相对于其安装的装置的运动来调节。 为了确保燃料和处理空气的充分混合，通过使用涡流发生器使进入燃烧器的进程空气旋转。 燃料/过程空气混合物进入燃烧器的燃烧部分，在该燃烧器的燃烧部分中，使涡旋流再循环以确保燃料在燃烧室中完全燃烧。 燃烧燃料和处理气体的混合物将其能量无火焰地转移到在燃烧器燃烧室外循环的过程气体，并且足够高以点燃那里的工艺气体，然后该燃烧器与燃烧器燃烧室分开燃烧，例如主燃烧 热后燃烧装置的外壳。
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公开(公告)号：US08820114B2
公开(公告)日：2014-09-02
申请号：US13039121
申请日：2011-03-02
申请人： Serguei Charamko , Kristian Debus , Tom Gielda
发明人： Serguei Charamko , Kristian Debus , Tom Gielda
CPC分类号： F25B1/06 , F28D11/04 , F28D2021/0028 , F28F2250/08 , F28F2265/14
摘要： Disclosed herein is a cooling system that utilizes a supersonic cooling cycle. The cooling system includes accelerating a compressible working fluid, and may not require the use of a conventional mechanical pump. The cooling system accelerates the fluid to a velocity equal to or greater than the speed of sound in the compressible fluid selected to be used in the system. A phase change of the fluid due at least in part to a pressure differential cools a working fluid that may be utilized to transfer heat from a heat intensive system.
摘要翻译： 本文公开了利用超音速冷却循环的冷却系统。 冷却系统包括加速可压缩的工作流体，并且可以不需要使用传统的机械泵。 冷却系统将流体加速至等于或大于选择用于系统中的可压缩流体中的声速。 至少部分地由压力差导致的流体的相变使得可用于从热密集系统传递热量的工作流体冷却。
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