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21. 发明申请

US20100296912A1 Active Rotor Alignment Control System And Method 审中-公开
标题翻译：主动转子对准控制系统及方法
公开(公告)号：US20100296912A1
公开(公告)日：2010-11-25
申请号：US12470952
申请日：2009-05-22
申请人： Martel Alexander McCallum , Parvangada Ganapathy Bojappa , David August Snider
发明人： Martel Alexander McCallum , Parvangada Ganapathy Bojappa , David August Snider
IPC分类号： F01D11/22
CPC分类号： F01D25/162 , F01D11/22 , F01D21/045
摘要： A rotating machine, such as a gas turbine, includes an active rotor alignment clearance control system wherein a plurality of actuators are circumferentially spaced around at least one rotor shaft bearing. The actuators are configured to eccentrically displace the bearing, and thus the rotor shaft, relative to stationary outer casing structure. A plurality of sensors are circumferentially spaced around a component of the casing structure, such as an inner shroud, and measure a parameter indicative of an eccentricity, such as blade tip clearance between the rotor blades and the structure, as the rotor rotates within the structure. A control system in communication with the sensors and actuators is configured to control the actuators to eccentrically displace the rotor by moving the shaft bearing to compensate for eccentricities detected between the rotor and casing structure.
摘要翻译：诸如燃气轮机的旋转机器包括主动转子对准间隙控制系统，其中多个致动器围绕至少一个转子轴轴承周向隔开。致动器构造成相对于静止的外壳结构偏心地使轴承和转子轴偏移。多个传感器围绕诸如内护罩的壳体结构的部件周向间隔开，并且当转子在结构内旋转时，测量指示偏心的参数，例如转子叶片和结构之间的叶片顶端间隙。与传感器和致动器连通的控制系统被配置为通过移动轴承来补偿致动器偏心地移动转子，以补偿在转子和壳体结构之间检测到的偏心。

22. 发明申请

US20100257837A1 SYSTEMS INVOLVING HYBRID POWER PLANTS 审中-公开
标题翻译：涉及混合动力装置的系统
公开(公告)号：US20100257837A1
公开(公告)日：2010-10-14
申请号：US12423415
申请日：2009-04-14
申请人： Mark Stewart Schroder , Michael Joseph Alexander , Scott Francis Johnson , David August Snider
发明人： Mark Stewart Schroder , Michael Joseph Alexander , Scott Francis Johnson , David August Snider
IPC分类号： F02C6/00 , F02C7/10
CPC分类号： F02C7/10 , F01K13/02 , F01K23/10 , F02C6/00 , Y02E20/16
摘要： A system comprises, a first heat recovery steam generator (HRSG) having an upstream intake duct portion, a first gas turbine engine connected to a first exhaust duct operative to output exhaust from the first gas turbine engine to the upstream intake duct portion of the first HRSG, and a second gas turbine engine connected to a second exhaust duct operative to output exhaust from the second gas turbine engine to the upstream intake duct portion of the first HRSG.
摘要翻译：一种系统包括具有上游进气管道部分的第一热回收蒸汽发生器（HRSG），连接到第一排气管道的第一燃气涡轮发动机，该第一排气管道可操作以将第一燃气涡轮发动机的排气输送到第一燃气涡轮发动机的上游进气管道部分 HRSG和连接到第二排气管道的第二燃气涡轮发动机，其可操作以将排气从第二燃气涡轮发动机输出到第一HRSG的上游进气管道部分。

23. 发明授权

US08955334B2 Systems and methods for controlling the startup of a gas turbine 有权
标题翻译：用于控制燃气轮机启动的系统和方法
公开(公告)号：US08955334B2
公开(公告)日：2015-02-17
申请号：US12841726
申请日：2010-07-22
申请人： Brian Patrick Hansen , Christopher Edward LaMaster , Timothy Edward DeJoris , David August Snider
发明人： Brian Patrick Hansen , Christopher Edward LaMaster , Timothy Edward DeJoris , David August Snider
IPC分类号： F02C7/22 , F02C7/26 , F02C9/00 , F01D19/00
CPC分类号： F02C7/26 , F01D19/00 , F02C9/00 , F05D2260/85
摘要： Systems and methods for controlling the startup of a gas turbine are described. A gas discharge component may be configured to discharge gas from a compressor component associated with the gas turbine. A fuel control component may be configured to control a fuel flow provided to a combustor component associated with the gas turbine. A drive component may be configured to supply a rotational force to a shaft associated with the gas turbine. At least one control device may be configured to (i) direct the gas discharge component to discharge gas from the compressor component, (ii) direct the fuel control component to adjust the fuel flow, and (iii) direct the drive component to rotate the shaft.
摘要翻译：描述了用于控制燃气轮机启动的系统和方法。气体放电部件可以构造成从与燃气轮机相关联的压缩机部件排出气体。燃料控制部件可以被配置为控制提供给与燃气轮机相关联的燃烧器部件的燃料流。驱动部件可以被配置为向与燃气轮机相关联的轴提供旋转力。至少一个控制装置可以被配置为（i）引导气体放电部件从压缩机部件排放气体，（ii）引导燃料控制部件来调节燃料流量，以及（iii）引导驱动部件旋转轴。

24. 发明授权

US08844295B2 Method for meeting a purge flow requirement for a power plant and a power plant having a purge control system 有权
标题翻译：满足发电厂和具有清洗控制系统的发电厂的净化流量要求的方法
公开(公告)号：US08844295B2
公开(公告)日：2014-09-30
申请号：US13342559
申请日：2012-01-03
申请人： David August Snider , Christopher John Morawski
发明人： David August Snider , Christopher John Morawski
IPC分类号： F02C7/26 , F01D19/00
CPC分类号： F02C7/26 , F01D19/00 , F23N2027/04 , F23N2027/06 , F23N2041/20
摘要： A method of delivering a purge flow through a gas turbomachine includes generating a purge flow, guiding the purge flow through at least one of a combustor assembly and a turbine portion of the gas turbomachine, determining a cumulative purge volume passing through the one of the combustor assembly and the turbine portion of the gas turbomachine to determine a predetermined purge volume, and discontinuing the purge flow once the predetermined purge volume has passed through the one of the combustor assembly and the turbine portion of the gas turbomachine.
摘要翻译：将吹扫流输送通过气体涡轮机的方法包括产生吹扫流，引导吹扫流通过气体涡轮机的燃烧器组件和涡轮部分中的至少一个，确定通过燃烧器中的一个的累积吹扫体积组件和气体涡轮机的涡轮机部分，以确定预定的净化容积，并且一旦预定的净化容积已经通过燃气组件和气体涡轮机的涡轮部分，就停止吹扫流。

25. 发明授权

US08510013B2 Gas turbine shutdown 有权
标题翻译：燃气轮机停机
公开(公告)号：US08510013B2
公开(公告)日：2013-08-13
申请号：US12434755
申请日：2009-05-04
申请人： Harold Lamar Jordan, Jr. , David August Snider
发明人： Harold Lamar Jordan, Jr. , David August Snider
IPC分类号： F02C9/00 , F02C9/26 , F02C9/48 , F02C7/057
CPC分类号： F02C9/48 , F01D21/00 , F05D2270/304 , Y02T50/671
摘要： A gas turbine includes a rotor, and a controller for controlling a shutdown of the gas turbine based on a target fuel-to-air ratio profile and/or controlling a rotor speed according to a target speed schedule to attain a specified duration for the shutdown. The controller controls the rotor speed by engaging the starting system to turn the rotor.
摘要翻译：燃气轮机包括转子和控制器，用于根据目标速度调度来控制燃气轮机的目标燃料空气比分布和/或控制转子速度以达到停机的指定持续时间。控制器通过接合启动系统来转动转子来控制转子速度。

26. 发明申请

US20130167550A1 METHOD FOR MEETING A PURGE FLOW REQUIREMENT FOR A POWER PLANT AND A POWER PLANT HAVING A PURGE CONTROL SYSTEM 有权
标题翻译：用于发电厂的电流流量要求的方法和具有电压控制系统的发电厂
公开(公告)号：US20130167550A1
公开(公告)日：2013-07-04
申请号：US13342559
申请日：2012-01-03
申请人： David August Snider , Christopher John Morawski
发明人： David August Snider , Christopher John Morawski
IPC分类号： F02C7/26
CPC分类号： F02C7/26 , F01D19/00 , F23N2027/04 , F23N2027/06 , F23N2041/20
摘要： A method of delivering a purge flow through a gas turbomachine includes generating a purge flow, guiding the purge flow through at least one of a combustor assembly and a turbine portion of the gas turbomachine, determining a cumulative purge volume passing through the one of the combustor assembly and the turbine portion of the gas turbomachine to determine a predetermined purge volume, and discontinuing the purge flow once the predetermined purge volume has passed through the one of the combustor assembly and the turbine portion of the gas turbomachine.
摘要翻译：将吹扫流输送通过气体涡轮机的方法包括产生吹扫流，引导吹扫流通过气体涡轮机的燃烧器组件和涡轮部分中的至少一个，确定通过燃烧器中的一个的累积吹扫体积组件和气体涡轮机的涡轮机部分，以确定预定的净化容积，并且一旦预定的净化容积已经通过燃气组件和气体涡轮机的涡轮部分，就停止吹扫流。

27. 发明申请

US20130103323A1 TURBINE RADIAL SENSOR MEASUREMENT 审中-公开
标题翻译：涡轮径向传感器测量
公开(公告)号：US20130103323A1
公开(公告)日：2013-04-25
申请号：US13280565
申请日：2011-10-25
申请人： David August Snider , Harold Lamar Jordan, JR. , Christopher Ryan Holsonback
发明人： David August Snider , Harold Lamar Jordan, JR. , Christopher Ryan Holsonback
IPC分类号： G06F19/00 , G01L7/00 , G06F17/18
CPC分类号： F01D17/08 , F01D21/003 , F05D2200/00
摘要： A method of measuring parameters of a gas turbine flow path is described. The method includes installing along one or more existing struts in the gas turbine flow path a first plurality of sensors for measuring a first parameter at one or more radial positions along the one or more struts and a second plurality of sensors for measuring a second parameter at one or more radial positions along the one or more struts. The method further includes producing an actual profile of the gas turbine flow path first parameter and second parameter.
摘要翻译：描述了一种测量燃气轮机流路参数的方法。该方法包括沿燃气涡轮机流路中的一个或多个现有支柱安装第一多个传感器，用于测量沿着一个或多个支柱的一个或多个径向位置处的第一参数和用于测量第二参数的第二多个传感器沿着一个或多个支柱的一个或多个径向位置。该方法还包括产生燃气轮机流路第一参数和第二参数的实际轮廓。

28. 发明授权

US08322145B2 Systems and methods for providing surge protection to a turbine component 有权
标题翻译：为涡轮机部件提供喘振保护的系统和方法
公开(公告)号：US08322145B2
公开(公告)日：2012-12-04
申请号：US12428769
申请日：2009-04-23
申请人： David August Snider , Harold Lamar Jordan, Jr. , Timothy Andrew Healy , John David Stampfli
发明人： David August Snider , Harold Lamar Jordan, Jr. , Timothy Andrew Healy , John David Stampfli
IPC分类号： F02C7/00
CPC分类号： F02C9/00 , F05D2260/80 , F05D2270/101
摘要： Systems and methods for providing surge protection to turbine components are provided. A surge protection limit may be determined for the turbine component. One or more measurements associated with operation of the turbine component may be received and provided to a cycle model executed to predict an operating condition of the turbine component. The predicted operating condition of the turbine component may be adjusted based at least in part on the received one or more measurements. The surge protection limit may be adjusted based on the adjusted predicted operating condition of the turbine component.
摘要翻译：提供了用于向涡轮机部件提供喘振保护的系统和方法。可以为涡轮机部件确定浪涌保护极限。可以接收与涡轮机部件的操作相关联的一个或多个测量，并且将其提供给执行以预测涡轮机部件的操作状态的循环模型。可以至少部分地基于所接收的一个或多个测量来调整涡轮机部件的预测操作状态。浪涌保护极限可以根据调整后的涡轮机部件的运行状况进行调整。

29. 发明申请

US20120240591A1 METHOD FOR SHUTTING DOWN A GENERATOR TO PREPARE THE GENERATOR FOR RESTART 审中-公开
标题翻译：用于切断发电机以准备发电机以重新启动的方法
公开(公告)号：US20120240591A1
公开(公告)日：2012-09-27
申请号：US13490091
申请日：2012-06-06
申请人： David August Snider , Michael Joseph Alexander , Robert Lester Brooks , Elsie Angelly Carantini , Michael James Dutka , Christopher John Morawski , Eugene Armstead Post
发明人： David August Snider , Michael Joseph Alexander , Robert Lester Brooks , Elsie Angelly Carantini , Michael James Dutka , Christopher John Morawski , Eugene Armstead Post
IPC分类号： F02C7/22
CPC分类号： F01K23/101 , Y02E20/16
摘要： A method and apparatus for shutting down a generator to prepare the generator for restart is disclosed. A power down sequence of a gas turbine of the generator is initiated from an operating state. A purge gas is forced into the gas turbine to extinguish a combustion flame in the gas turbine. The purge gas is swept through the gas turbine to displace the fuel from the gas turbine using a coast down airflow through the gas turbine during the power down sequence to prepare the generator for restart.
摘要翻译：公开了一种用于关闭发电机以准备用于重启的发电机的方法和装置。从运行状态开始发电机的燃气轮机的断电顺序。吹扫气体被迫进入燃气轮机以熄灭燃气轮机中的燃烧火焰。吹扫气体被扫过燃气轮机，以在断电序列期间使用通过燃气轮机的自由下降的气流从燃气涡轮机移动燃料，以准备用于再起动的发电机。

30. 发明申请

US20100280733A1 GAS TURBINE SHUTDOWN 有权
标题翻译：燃气轮机关闭
公开(公告)号：US20100280733A1
公开(公告)日：2010-11-04
申请号：US12434755
申请日：2009-05-04
申请人： Harold Lamar Jordan, JR. , David August Snider
发明人： Harold Lamar Jordan, JR. , David August Snider
IPC分类号： F02C9/00
CPC分类号： F02C9/48 , F01D21/00 , F05D2270/304 , Y02T50/671
摘要： A gas turbine includes a rotor, and a controller for controlling a shutdown of the gas turbine based on a target fuel-to-air ratio profile and/or controlling a rotor speed according to a target speed schedule to attain a specified duration for the shutdown. The controller controls the rotor speed by engaging the starting system to turn the rotor.
摘要翻译：燃气轮机包括转子和控制器，用于根据目标速度调度控制燃气轮机的目标燃料空气比分布和/或控制转子速度，以达到关闭的指定持续时间。控制器通过接合启动系统来转动转子来控制转子速度。

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