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1. 发明授权

US08240153B2 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
标题翻译：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
IPC分类号： F02C7/18 , F02C9/18
CPC分类号： F02C9/18 , F02C6/08 , F02C7/18
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。

2. 发明申请

US20120117977A1 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
标题翻译：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
CPC分类号： F02C9/18 , F02C6/08 , F02C7/18
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。

3. 发明申请

US20090173078A1 Methods and Systems for Providing Real-Time Comparison with an Alternate Control Strategy for a Turbine 有权
标题翻译：提供与涡轮机替代控制策略实时比较的方法和系统
公开(公告)号：US20090173078A1
公开(公告)日：2009-07-09
申请号：US11971007
申请日：2008-01-08
申请人： Jonathan Carl Thatcher , Scott Schaberg , Mark Disch
发明人： Jonathan Carl Thatcher , Scott Schaberg , Mark Disch
IPC分类号： F02C9/00
CPC分类号： F02C9/20 , F05D2270/44 , F05D2270/707 , F05D2270/708
摘要： A method for controlling and modeling a turbine is provided. The method may include modeling the turbine by a primary adaptive turbine model that includes at least one primary operating parameter and modeling the turbine by an alternate adaptive turbine model that includes at least one alternate operating parameter. The method may also include determining a first output value from the primary adaptive turbine model that corresponds at least in part to the operation of the turbine based on a primary control strategy and adjusting the alternate operating parameter or parameters based on an alternate control strategy and based at least in part on the first output value. The method may further include determining comparison data based at least in part on a comparison between the primary control strategy and the alternate control strategy.
摘要翻译：提供了一种用于控制和建模涡轮机的方法。该方法可以包括通过包括至少一个主要操作参数的主要自适应涡轮机模型来建模涡轮机，并且通过包括至少一个替代操作参数的备选自适应涡轮机模型对涡轮机进行建模。该方法还可以包括从主要自适应涡轮机模型确定第一输出值，该第一输出值至少部分地基于主控制策略对涡轮机的运行进行对应，并且基于替代控制策略并且基于至少部分地基于第一输出值。该方法还可以包括至少部分地基于主控制策略和替代控制策略之间的比较来确定比较数据。

4. 发明授权

US07822512B2 Methods and systems for providing real-time comparison with an alternate control strategy for a turbine 有权
标题翻译：用于与涡轮机的替代控制策略实时比较的方法和系统
公开(公告)号：US07822512B2
公开(公告)日：2010-10-26
申请号：US11971007
申请日：2008-01-08
申请人： Jonathan Carl Thatcher , Scott Schaberg , Mark Disch
发明人： Jonathan Carl Thatcher , Scott Schaberg , Mark Disch
IPC分类号： G05B13/02
CPC分类号： F02C9/20 , F05D2270/44 , F05D2270/707 , F05D2270/708
摘要： A method for controlling and modeling a turbine is provided. The method may include modeling the turbine by a primary adaptive turbine model that includes at least one primary operating parameter and modeling the turbine by an alternate adaptive turbine model that includes at least one alternate operating parameter. The method may also include determining a first output value from the primary adaptive turbine model that corresponds at least in part to the operation of the turbine based on a primary control strategy and adjusting the alternate operating parameter or parameters based on an alternate control strategy and based at least in part on the first output value. The method may further include determining comparison data based at least in part on a comparison between the primary control strategy and the alternate control strategy.
摘要翻译：提供了一种用于控制和建模涡轮机的方法。该方法可以包括通过包括至少一个主要操作参数的主要自适应涡轮机模型来建模涡轮机，并且通过包括至少一个替代操作参数的备选自适应涡轮机模型对涡轮机进行建模。该方法还可以包括从主要自适应涡轮机模型确定第一输出值，该第一输出值至少部分地基于主控制策略对涡轮机的运行进行对应，并且基于替代控制策略并且基于至少部分地基于第一输出值。该方法还可以包括至少部分地基于主控制策略和替代控制策略之间的比较来确定比较数据。

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