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公开(公告)号：US07823390B2
公开(公告)日：2010-11-02
申请号：US11711306
申请日：2007-02-27
IPC分类号： F02C6/04
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。
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公开(公告)号：US20080202092A1
公开(公告)日：2008-08-28
申请号：US11711306
申请日：2007-02-27
IPC分类号： F02C7/12
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。
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公开(公告)号：US08505310B2
公开(公告)日：2013-08-13
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
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。
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4.发明授权Ejectors with separably secured nozzles, adjustable size nozzles, or adjustable size mixing tubes 有权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
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。
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公开(公告)号：US08142169B2
公开(公告)日：2012-03-27
申请号：US12348923
申请日：2009-01-06
申请人： Kenneth Neil Whaling , Dean Matthew Erickson , Hua Zhang , David Wesley Ball , Christina Renee Pompey
发明人： Kenneth Neil Whaling , Dean Matthew Erickson , Hua Zhang , David Wesley Ball , Christina Renee Pompey
IPC分类号： F04F5/48
CPC分类号： F02C6/08 , F01D25/12 , F02C3/32 , F05D2260/601
摘要： An ejector for a turbine engine is described herein. The ejector may include a variable geometry motive nozzle and a variable geometry mixing tube positioned downstream of the variable geometry motive nozzle.
摘要翻译： 这里描述了一种用于涡轮发动机的喷射器。 喷射器可以包括可变几何运动喷嘴和位于可变几何运动喷嘴下游的可变几何形状混合管。
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公开(公告)号：US20100170265A1
公开(公告)日：2010-07-08
申请号：US12348923
申请日：2009-01-06
申请人： Kenneth Neil Whaling , Dean Matthew Erickson , Hua Zhang , David Wesley Ball , Christina Renee Pompey
发明人： Kenneth Neil Whaling , Dean Matthew Erickson , Hua Zhang , David Wesley Ball , Christina Renee Pompey
CPC分类号： F02C6/08 , F01D25/12 , F02C3/32 , F05D2260/601
摘要： An ejector for a turbine engine is described herein. The ejector may include a variable geometry motive nozzle and a variable geometry mixing tube positioned downstream of the variable geometry motive nozzle.
摘要翻译： 这里描述了一种用于涡轮发动机的喷射器。 喷射器可以包括可变几何运动喷嘴和位于可变几何运动喷嘴下游的可变几何形状混合管。
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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
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。
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8.发明申请EJECTORS WITH SEPARABLY SECURED NOZZLES, ADJUSTABLE SIZE NOZZLES, OR ADJUSTABLE SIZE MIXING TUBES 有权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
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。
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9.发明授权Method and system for controlling a set point for extracting air from a compressor to provide turbine cooling air in a gas turbine 有权用于控制用于从压缩机抽取空气以在燃气轮机中提供涡轮机冷却空气的设定点的方法和系统公开(公告)号：US08240153B2
公开(公告)日：2012-08-14
申请号：US12120621
申请日：2008-05-14
申请人： Priscilla Childers , Mark Disch , Curtis Newton, III , David Wesley Ball, Jr. , Kenneth Neil Whaling , Alan Meier Truesdale
发明人： Priscilla Childers , Mark Disch , Curtis Newton, III , David Wesley Ball, Jr. , Kenneth Neil Whaling , Alan Meier Truesdale
摘要： A method for controlling the generation of turbine cooling air from air extracted from a compressor of a gas turbine including: extracting compressed air from a low pressure and a high pressure stage of the compressor; adding in an ejector the compressed air from the low pressure stage to the air from the high pressure stage and discharging the combined air as turbine cooling air; bypassing the ejector with a bypass portion of the extracted compressed air from the high pressure stage; in response to turning on the flow of extracted compressed air from the low pressure stage, changing a set point for an actual pressure ratio that includes a pressure of the turbine cooling air, and adjusting the bypass flow in response to the changed set point to cause the actual pressure ratio to approach the changed set point.
摘要翻译： 一种用于控制从燃气轮机压缩机抽出的空气产生涡轮机冷却空气的方法，包括：从压缩机的低压级和高压级抽出压缩空气; 将压缩空气从低压级喷射到来自高压级的空气并将组合的空气作为涡轮冷却空气排出; 绕过来自高压级的提取的压缩空气的旁路部分的喷射器; 响应于从低压级引起提取的压缩空气的流动，改变包括涡轮机冷却空气的压力的实际压力比的设定点，并且响应于改变的设定点来调节旁路流，导致 实际压力比接近改变的设定点。
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10.发明申请METHOD AND SYSTEM FOR CONTROLLING A SET POINT FOR EXTRACTING AIR FROM A COMPRESSOR TO PROVIDE TURBINE COOLING AIR IN A GAS TURBINE 有权用于控制从压缩机提取空气以在气体涡轮机中提供涡轮冷却空气的设定点的方法和系统公开(公告)号：US20120117977A1
公开(公告)日：2012-05-17
申请号：US12120621
申请日：2008-05-14
申请人： Priscilla Childers , Mark Disch , Curtis Newton, III , David Wesley Ball, JR. , Kenneth Neil Whaling , Alan Meier Truesdale
发明人： Priscilla Childers , Mark Disch , Curtis Newton, III , David Wesley Ball, JR. , Kenneth Neil Whaling , Alan Meier Truesdale
IPC分类号： F02C6/08
摘要： A method for controlling the generation of turbine cooling air from air extracted from a compressor of a gas turbine including: extracting compressed air from a low pressure and a high pressure stage of the compressor; adding in an ejector the compressed air from the low pressure stage to the air from the high pressure stage and discharging the combined air as turbine cooling air; bypassing the ejector with a bypass portion of the extracted compressed air from the high pressure stage; in response to turning on the flow of extracted compressed air from the low pressure stage, changing a set point for an actual pressure ratio that includes a pressure of the turbine cooling air, and adjusting the bypass flow in response to the changed set point to cause the actual pressure ratio to approach the changed set point.
摘要翻译： 一种用于控制从燃气轮机压缩机抽出的空气产生涡轮机冷却空气的方法，包括：从压缩机的低压级和高压级抽出压缩空气; 将压缩空气从低压级喷射到来自高压级的空气并将组合的空气作为涡轮冷却空气排出; 绕过来自高压级的提取的压缩空气的旁路部分的喷射器; 响应于从低压级引起提取的压缩空气的流动，改变包括涡轮机冷却空气的压力的实际压力比的设定点，并且响应于改变的设定点来调节旁路流，导致 实际压力比接近改变的设定点。
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