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1. 发明申请

US20110056212A1 SYSTEM AND METHOD FOR APPLYING ENERGY EXTERNALLY FOR FUEL GAS FOR DEW POINT HEATING IN GAS TURBINE POWER PLANT 有权
标题翻译：用于燃气涡轮发电厂柴油机加热能源的系统和方法
公开(公告)号：US20110056212A1
公开(公告)日：2011-03-10
申请号：US12556153
申请日：2009-09-09
申请人： Hua Zhang , Dean Erickson , David Wesley Ball, JR.
发明人： Hua Zhang , Dean Erickson , David Wesley Ball, JR.
IPC分类号： F02C7/26 , H05B3/06
CPC分类号： F02C7/22 , F02C3/22 , F05D2260/20 , F05D2260/85
摘要： In a gas turbine power plant, pressurized fuel gas undergoes pressure reduction and gas expansion before being provided to a gas turbine. Condensations, which can damage the turbine, can form as the fuel gas cools when the fuel gas undergoes the pressure reduction and expansion. An electric startup heater is used to superheat the fuel gas to substantially prevent the condensations from forming. The electric startup heater includes band heaters wrapped externally to a fuel gas pipe to heat the fuel gas from outside in. Compared to conventional heaters which provide superheating through internal heating elements, the electric startup heater reduces costs and provides increased safety, flexibility, operational efficiency and ability to adapt to varying fuel gas characteristics.
摘要翻译：在燃气轮机发电厂中，加压燃料气体在提供给燃气轮机之前经历减压和气体膨胀。当燃料气体经历减压和膨胀时，当燃料气体冷却时，可能形成可能损坏涡轮机的冷凝物。使用电启动加热器来使燃料气体过热，从而基本上防止冷凝物形成。电启动加热器包括从外部包裹的燃气管道的带式加热器，以从外部加热燃料气体。与通过内部加热元件提供过热的常规加热器相比，电启动加热器降低成本并提供增加的安全性，灵活性，运行效率以及适应不同燃料气体特性的能力。

2. 发明授权

US08490403B2 System and method for applying energy externally for fuel gas for dew point heating in gas turbine power plant 有权
标题翻译：燃气轮机发电厂露天采暖燃料气外部应用能量的系统和方法
公开(公告)号：US08490403B2
公开(公告)日：2013-07-23
申请号：US12556153
申请日：2009-09-09
申请人： Hua Zhang , Dean Erickson , David Wesley Ball, Jr.
发明人： Hua Zhang , Dean Erickson , David Wesley Ball, Jr.
IPC分类号： F02C1/00
CPC分类号： F02C7/22 , F02C3/22 , F05D2260/20 , F05D2260/85
摘要： In a gas turbine power plant, pressurized fuel gas undergoes pressure reduction and gas expansion before being provided to a gas turbine. Condensations, which can damage the turbine, can form as the fuel gas cools when the fuel gas undergoes the pressure reduction and expansion. An electric startup heater is used to superheat the fuel gas to substantially prevent the condensations from forming. The electric startup heater includes band heaters wrapped externally to a fuel gas pipe to heat the fuel gas from outside in. Compared to conventional heaters which provide superheating through internal heating elements, the electric startup heater reduces costs and provides increased safety, flexibility, operational efficiency and ability to adapt to varying fuel gas characteristics.
摘要翻译：在燃气轮机发电厂中，加压燃料气体在提供给燃气轮机之前经历减压和气体膨胀。当燃料气体经历减压和膨胀时，当燃料气体冷却时，可能形成可能损坏涡轮机的冷凝物。使用电启动加热器来使燃料气体过热，从而基本上防止冷凝物形成。电启动加热器包括从外部包裹的燃气管道的带式加热器，以从外部加热燃料气体。与通过内部加热元件提供过热的常规加热器相比，电启动加热器降低成本并提供增加的安全性，灵活性，运行效率以及适应不同燃料气体特性的能力。

3. 发明授权

US07823390B2 Mixer for cooling and sealing air system of turbomachinery 失效
标题翻译：涡轮机冷却和密封空气系统混合器
公开(公告)号：US07823390B2
公开(公告)日：2010-11-02
申请号：US11711306
申请日：2007-02-27
申请人： Ravi Praveen S. Eluripati , David Wesley Ball, Jr. , Kenneth Neil Whaling , Hua Zhang
发明人： Ravi Praveen S. Eluripati , David Wesley Ball, Jr. , Kenneth Neil Whaling , Hua Zhang
IPC分类号： F02C6/04
CPC分类号： F02C7/185 , F01D11/04 , F01D25/12 , F02C3/06 , F02C3/32
摘要： A system is provided for directing air from plural compressor ports to provide cooling and/or sealing air to an associated turbine site. A first flow from a pressure stage of the compressor has a first pressure and temperature. A second flow from another pressure stage of the compressor has a second pressure and temperature. The first and second pressures/temperatures are different. An ejector has two inlets for receiving the first and second flows, and output for combining the first and second flows into a third flow. The pressure and temperature of the third flow are different from the first and second pressures and temperatures. A bypass line is connected between the first flow and the third flow, and provides a bypass flow. A mixer combines the bypass flow and the third flow into a fourth flow. The fourth flow has a pressure and temperature intermediate the pressure and temperature of the bypass flow and the third flow. The mixer comprises inner and outer sections. The inner section is generally cylindrical in cross section and has a plurality of holes therein. The angle between the direction of the bypass flow and the direction of the third flow, when the bypass flow meets the third flow in the mixer, is less than about 90 degrees.
摘要翻译：提供一种用于引导来自多个压缩机端口的空气以向相关联的涡轮机位置提供冷却和/或密封空气的系统。来自压缩机的压力级的第一流量具有第一压力和温度。来自压缩机的另一压力级的第二流量具有第二压力和温度。第一和第二压力/温度是不同的。喷射器具有用于接收第一和第二流的两个入口，并且输出用于将第一和第二流合并成第三流。第三流量的压力和温度与第一和第二压力和温度不同。旁路管线连接在第一流和第三流之间，并提供旁路流。混合器将旁路流和第三流合并成第四流。第四流量的压力和温度介于旁路流量和第三流量的压力和温度之间。混合器包括内部和外部部分。内部截面通常为圆柱形，其中具有多个孔。当旁通流量与混合器中的第三流量相交时，旁路流动方向与第三流动方向之间的角度小于约90度。

4. 发明申请

US20100024424A1 CONDENSER FOR A COMBINED CYCLE POWER PLANT 审中-公开
标题翻译：一个组合循环电厂的冷凝器
公开(公告)号：US20100024424A1
公开(公告)日：2010-02-04
申请号：US12181741
申请日：2008-07-29
申请人： Hua Zhang , Jatila Ranasinghe , David Wesley Ball, JR.
发明人： Hua Zhang , Jatila Ranasinghe , David Wesley Ball, JR.
IPC分类号： F01K13/00
CPC分类号： F01K9/00 , F01K11/02 , F01K23/106 , F28B1/00 , F28D15/02 , Y02E20/16
摘要： A combined cycle power plant includes a steam turbine section having an inlet section and an outlet section. The steam turbine section passes steam from the inlet section toward the outlet section. The combined cycle power plant also includes a condenser fluidly connected to the outlet section of the steam turbine section. The condenser includes a plurality of heat pipes configured to extract latent heat from steam passing from the steam turbine section to form condensed water.
摘要翻译：联合循环发电厂包括具有入口部分和出口部分的汽轮机部分。蒸汽轮机部分将来自进口部分的蒸汽传送到出口部分。联合循环发电厂还包括流体连接到蒸汽涡轮机部分的出口部分的冷凝器。冷凝器包括多个热管，其构造成从蒸汽涡轮机部分抽出的蒸气中提取潜热，形成冷凝水。

5. 发明授权

US08157512B2 Heat pipe intercooler for a turbomachine 有权
标题翻译：用于涡轮机的热管中冷器
公开(公告)号：US08157512B2
公开(公告)日：2012-04-17
申请号：US12181756
申请日：2008-07-29
申请人： Hua Zhang , Jatila Ranasinghe , David Wesley Ball, Jr.
发明人： Hua Zhang , Jatila Ranasinghe , David Wesley Ball, Jr.
IPC分类号： F01D17/00
CPC分类号： F02C7/143 , F05D2260/208 , F05D2260/211
摘要： A turbomachine includes a compressor having an intake portion and an outlet portion. The compressor compresses air received at the intake portion to form a compressed airflow that is passed from the outlet portion. The turbomachine also includes an intercooler operatively connected downstream from the compressor. The intercooler includes a plurality of heat pipes that are configured to extract heat from the compressed airflow.
摘要翻译：涡轮机包括具有进气部分和出口部分的压缩机。压缩机压缩容纳在进气部分处的空气，以形成从出口部分通过的压缩空气流。涡轮机还包括可操作地连接在压缩机下游的中间冷却器。中间冷却器包括被配置为从压缩空气流中提取热量的多个热管。

6. 发明申请

US20100096474A1 Gas Turbine Ejector and Method of Operation 有权
标题翻译：燃气轮机喷射器及操作方法
公开(公告)号：US20100096474A1
公开(公告)日：2010-04-22
申请号：US12255723
申请日：2008-10-22
申请人： Hua Zhang , David Wesley Ball, JR. , Ravi Praveen Eluripati , Christina Renee Pompey , Kenneth Neil Whaling
发明人： Hua Zhang , David Wesley Ball, JR. , Ravi Praveen Eluripati , Christina Renee Pompey , Kenneth Neil Whaling
IPC分类号： F02K1/36 , F04F5/44 , F02C3/32
CPC分类号： F02C6/08 , F01D9/065 , F01D25/12
摘要： An ejector system and method of operation for combining high and low pressure fluid flow streams is disclosed. A nozzle chamber communicates with a high pressure fluid flow stream and a suction chamber communicates with a low pressure fluid flow stream. The outlet of the nozzle chamber exit into the suction chamber and include multiple nozzles such that the high pressure flow stream exits the nozzle chamber in multiple flow streams having multiple surface areas for interlayer drag between the flows. The low pressure fluid flow stream is entrained by the high pressure fluid flow streams exiting the multiple nozzles to define an intermediate pressure flow stream.
摘要翻译：公开了一种用于组合高压和低压流体流动的喷射器系统和操作方法。喷嘴室与高压流体流相通，吸入室与低压流体流动相通。喷嘴室的出口离开吸入室并且包括多个喷嘴，使得高压流动流以多个流动流离开喷嘴室，该多个流动流具有用于流动之间的夹层拖动的多个表面区域。低压流体流动由离开多个喷嘴的高压流体流动夹带以限定中间压力流动流。

7. 发明申请

US20100040482A1 EJECTORS WITH SEPARABLY SECURED NOZZLES, ADJUSTABLE SIZE NOZZLES, OR ADJUSTABLE SIZE MIXING TUBES 有权
标题翻译：具有分离式安全喷嘴，可调节尺寸喷嘴或可调节尺寸混合管的喷枪
公开(公告)号：US20100040482A1
公开(公告)日：2010-02-18
申请号：US12191748
申请日：2008-08-14
申请人： Kenneth Neil Whaling , Dean Matthew Erickson , Hua Zhang , David Wesley Ball, JR. , James L. Davis , Michael Savale , Douglas S. Byrd
发明人： Kenneth Neil Whaling , Dean Matthew Erickson , Hua Zhang , David Wesley Ball, JR. , James L. Davis , Michael Savale , Douglas S. Byrd
IPC分类号： F04F5/44 , B05B7/04 , F02C7/18
CPC分类号： F04F5/20 , F02C7/222 , F02K9/52 , F04F5/461 , F05D2240/36
摘要： An ejector comprising a motive inlet, a motive nozzle separably secured to the motive inlet, a suction chamber about the motive nozzle, a suction fluid inlet to the suction chamber, a mixing tube in fluid communication with the suction chamber and the motive nozzle, a diffuser in fluid communication with the mixing tube and distal the suction chamber and the motive nozzle, and an outlet from the diffuser is provided. A nozzle comprising at least two concentric arc nozzle portions is also provided. An ejector comprising a mixing tube including a flexible layer adapted to compress or stretch, thereby allowing a mixing tube diameter to change is further provided.
摘要翻译：喷射器，包括动力入口，可分离地固定到动力入口的动力喷嘴，围绕运动喷嘴的抽吸室，到吸入室的抽吸流体入口，与吸入腔和动力喷嘴流体连通的混合管，扩散器与混合管流体连通并且远离吸入室和动力喷嘴，并且提供来自扩散器的出口。还提供了包括至少两个同心弧形喷嘴部分的喷嘴。提供一种喷射器，其包括混合管，其包括适于压缩或拉伸的柔性层，从而允许混合管直径改变。

8. 发明授权

US08083495B2 Ejectors with separably secured nozzles, adjustable size nozzles, or adjustable size mixing tubes 有权
标题翻译：具有可分离固定喷嘴，可调节尺寸喷嘴或可调节尺寸混合管的喷射器
公开(公告)号：US08083495B2
公开(公告)日：2011-12-27
申请号：US12191748
申请日：2008-08-14
申请人： Kenneth Neil Whaling , Dean Matthew Erickson , Hua Zhang , David Wesley Ball, Jr. , James L. Davis , Michael Savale , Douglas S. Byrd
发明人： Kenneth Neil Whaling , Dean Matthew Erickson , Hua Zhang , David Wesley Ball, Jr. , James L. Davis , Michael Savale , Douglas S. Byrd
IPC分类号： F04F5/46 , F04F5/48 , F04F5/00 , F04F5/44
CPC分类号： F04F5/20 , F02C7/222 , F02K9/52 , F04F5/461 , F05D2240/36
摘要： An ejector comprising a motive inlet, a motive nozzle separably secured to the motive inlet, a suction chamber about the motive nozzle, a suction fluid inlet to the suction chamber, a mixing tube in fluid communication with the suction chamber and the motive nozzle, a diffuser in fluid communication with the mixing tube and distal the suction chamber and the motive nozzle, and an outlet from the diffuser is provided. A nozzle comprising at least two concentric arc nozzle portions is also provided. An ejector comprising a mixing tube including a flexible layer adapted to compress or stretch, thereby allowing a mixing tube diameter to change is further provided.
摘要翻译：喷射器，包括动力入口，可分离地固定到动力入口的动力喷嘴，围绕运动喷嘴的抽吸室，到吸入室的抽吸流体入口，与吸入腔和动力喷嘴流体连通的混合管，扩散器与混合管流体连通并且远离吸入室和动力喷嘴，并且提供来自扩散器的出口。还提供了包括至少两个同心弧形喷嘴部分的喷嘴。提供一种喷射器，其包括混合管，其包括适于压缩或拉伸的柔性层，从而允许混合管直径改变。

9. 发明授权

US08083466B2 Turbomachine inlet heating system 有权
标题翻译：涡轮机进气加热系统
公开(公告)号：US08083466B2
公开(公告)日：2011-12-27
申请号：US12403444
申请日：2009-03-13
申请人： Hua Zhang , David Wesley Ball, Jr. , Valery Ivanovich Ponyavin , Douglas Scott Byrd
发明人： Hua Zhang , David Wesley Ball, Jr. , Valery Ivanovich Ponyavin , Douglas Scott Byrd
IPC分类号： F01D21/12
CPC分类号： F02C9/18 , F01D25/10 , F02C7/08 , F05D2260/221 , F05D2270/101
摘要： A turbomachine system includes a compressor having a compressor intake and a compressor extraction outlet, and an inlet system fluidly connected to the compressor intake and the compressor extraction outlet. The inlet system includes a plenum having a first end portion that extends to a second end portion through an intermediate portion. The inlet system also includes a heating system having a plurality of conduits extending horizontally through the intermediate portion of the plenum and arranged in a vertical relationship. Heated air from the compressor extraction outlet passes through the plurality of conduits and raises a temperature of ambient air passing through the plenum and into the compressor intake.
摘要翻译：涡轮机系统包括具有压缩机进气口和压缩机排出口的压缩机，以及与压缩机进气口和压缩机排出口流体连接的入口系统。入口系统包括具有通过中间部分延伸到第二端部的第一端部的增压室。入口系统还包括加热系统，其具有水平延伸通过气室的中间部分并以垂直关系布置的多个管道。来自压缩机排出口的加热空气通过多个管道，并且使经过集气室的环境空气的温度升高并进入压缩机进气口。

10. 发明申请

US20100054926A1 SYSTEM AND METHOD FOR THERMAL MANAGEMENT OF A GAS TURBINE INLET 审中-公开
标题翻译：一种气体涡轮机入口热管理系统及方法
公开(公告)号：US20100054926A1
公开(公告)日：2010-03-04
申请号：US12201491
申请日：2008-08-29
申请人： Hua Zhang , David Wesley Ball, JR.
发明人： Hua Zhang , David Wesley Ball, JR.
IPC分类号： F02C7/141
CPC分类号： F02C7/10
摘要： A thermal management system includes: a turbine assembly including an inlet housing, a compressor in fluid communication with the inlet housing, a power turbine in fluid communication with the compressor, and an exhaust assembly in fluid communication with the power turbine; and at least one heat pipe having a first portion disposed in thermal communication with the inlet housing and a second portion disposed in thermal communication with the exhaust assembly, the at least one heat pipe configured to transfer thermal energy from the exhaust assembly to at least one of input gas entering the inlet housing and at least one component of the inlet housing.
摘要翻译：热管理系统包括：涡轮组件，其包括入口壳体，与入口壳体流体连通的压缩机，与压缩机流体连通的动力涡轮机和与动力涡轮机流体连通的排气组件; 以及至少一个热管，其具有设置成与所述入口壳体热连通的第一部分和设置成与所述排气组件热连通的第二部分，所述至少一个热管被配置为将热能从所述排气组件传递到至少一个输入气体进入入口壳体和入口壳体的至少一个部件。

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