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11. 发明申请

US20170260961A1 PUMPED-STORAGE POWER GENERATION CONTROL DEVICE AND PUMPED-STORAGE POWER GENERATION CONTROL METHOD 审中-公开
公开(公告)号：US20170260961A1
公开(公告)日：2017-09-14
申请号：US15153022
申请日：2016-05-12
申请人： KABUSHIKI KAISHA TOSHIBA
发明人： Junji MORI , Toshiaki SUZUKI , Kiyoshi KUSUNOKI , Toru KUBO , Shoji llDA , Takahisa KAGEYAMA
IPC分类号： F03B13/06 , F01D17/00 , F01D15/10 , G05B15/02 , H02K7/18
CPC分类号： F03B13/06 , F01D15/10 , F01D17/00 , F03B15/00 , F05B2270/00 , G05B15/02 , H02J15/003 , H02K7/1823 , Y02E10/22 , Y02E10/226 , Y02E60/17 , Y02P90/50
摘要： According to one embodiment, a pumped-storage power generation control device includes a control section that controls at least one of the pumping input of the pumped-storage power generation facility in the pumping operation and the power output of the pumped-storage power generation facility in the power generating operation such that a value, which is obtained by a predetermined calculation using the measurement value relating to the pumping input of the pumped-storage power generation facility in the pumping operation and the measurement value relating to the power output of the pumped-storage power generation facility in the power generating operation, becomes a set target value.

12. 发明授权

US09388706B2 Method and system for tuning a turbine using secondary injection nozzles in nozzle ring 有权
标题翻译：用于使用喷嘴环中的二次注射喷嘴调节涡轮机的方法和系统
公开(公告)号：US09388706B2
公开(公告)日：2016-07-12
申请号：US13757034
申请日：2013-02-01
申请人： Fluid Equipment Development Company
发明人： Ryan Kitzmiller , Jason B. Hunt
IPC分类号： F04D29/46 , F03B1/04 , F01D17/00 , B01D61/06 , F03B3/02 , F03B3/18 , F03B11/00 , F03B15/04
CPC分类号： F01D17/00 , B01D61/06 , F03B3/02 , F03B3/18 , F03B3/183 , F03B11/004 , F03B15/04 , F05B2220/40 , F05B2220/62 , Y02E10/223
摘要： A turbine and method of operating the same includes a housing having a volute and an outlet and an impeller rotatable coupled to the housing. The turbine includes a nozzle ring having a plurality of primary nozzles and a plurality of secondary nozzles. The plurality of primary nozzles and the plurality of secondary nozzles direct fluid toward the impeller. An auxiliary valve assembly selectively communicates fluid from the volute to the plurality of secondary nozzles. An actuator is coupled to the valve auxiliary assembly moving the auxiliary valve assembly from a first position communicating fluid from the volute into the secondary nozzles to a second position blocking flow of fluid to the secondary nozzles.
摘要翻译：涡轮机及其操作方法包括具有蜗壳和出口的壳体和可旋转地联接到壳体的叶轮。涡轮机包括具有多个主喷嘴和多个次喷嘴的喷嘴环。多个主喷嘴和多个次喷嘴将流体引向叶轮。辅助阀组件选择性地将流体从蜗壳传送到多个次喷嘴。致动器联接到阀辅助组件，其将辅助阀组件从第一位置移动，第一位置将流体从蜗壳连通到次喷嘴到阻止第二喷嘴流体流动的第二位置。

13. 发明申请

US20150337675A1 ACTIVE CLEARANCE CONTROL FOR GAS TURBINE ENGINE 审中-公开
标题翻译：气动涡轮发动机主动间隙控制
公开(公告)号：US20150337675A1
公开(公告)日：2015-11-26
申请号：US14672561
申请日：2015-03-30
申请人： United Technologies Corporation
发明人： Gabriel L. Suciu , Jesse M. Chandler , Nathan Snape
IPC分类号： F01D11/14 , F02C7/25 , F01D17/00 , F02C5/12 , F01D25/24 , F01D25/14
CPC分类号： F01D11/14 , F01D11/24 , F01D17/00 , F01D25/145 , F01D25/24 , F02C5/12 , F02C7/25 , F05D2220/32 , F05D2260/231
摘要： A gas turbine engine includes a fluid intake. A turbine section includes a turbine case. A firewall is located upstream of the turbine section. A conduit is configured to direct a fluid from the fluid intake to the turbine case. A valve is located on a first side of the firewall opposite from the turbine section and is configured to regulate a flow of the fluid through the conduit.
摘要翻译：燃气涡轮发动机包括流体入口。涡轮机部分包括涡轮机壳体。防火墙位于涡轮机部分的上游。导管构造成将流体从流体入口引导到涡轮壳体。阀门位于与涡轮机部分相对的防火墙的第一侧上，并且构造成调节通过导管的流体的流动。

14. 发明授权

US09169779B2 Systems and methods for altering inlet airflow of gas turbine engines 有权
标题翻译：改变燃气涡轮发动机入口气流的系统和方法
公开(公告)号：US09169779B2
公开(公告)日：2015-10-27
申请号：US11869040
申请日：2007-10-09
申请人： Michael Winter
发明人： Michael Winter
IPC分类号： F01D17/00 , F02C7/042 , F02C7/047 , F02K3/06
CPC分类号： F02C7/042 , F02C7/047 , F02K3/06
摘要： Systems and methods for altering airflow to gas turbine engines are provided. In this regard, a representative system includes a gas turbine engine inlet having a slat, the slat being movable between a retracted position and an extended position. In the extended position, the slat increases an effective diameter of the inlet compared to the diameter of the inlet when in the retracted position.
摘要翻译：提供了改变燃气轮机发动机气流的系统和方法。在这方面，代表性系统包括具有板条的燃气涡轮发动机入口，所述板条可在缩回位置和伸出位置之间移动。在延伸位置，当处于缩回位置时，板条增加入口的有效直径与入口的直径相比。

15. 发明授权

US09151167B2 Turbine assembly 有权
标题翻译：涡轮总成
公开(公告)号：US09151167B2
公开(公告)日：2015-10-06
申请号：US13370949
申请日：2012-02-10
申请人： William Scott Zemitis , Christopher Michael Penny
发明人： William Scott Zemitis , Christopher Michael Penny
IPC分类号： F01D17/00 , F01D5/30 , F01D5/26
CPC分类号： F01D5/3007 , F01D5/26
摘要： According to one aspect of the invention, a turbine assembly includes an airfoil extending from a blade and a dovetail located on a lower portion of the blade, wherein the dovetail has a dovetail contact surface. The turbine assembly also includes a member with a slot configured to couple to the airfoil via the dovetail, the slot having a slot contact surface to contact the dovetail contact surface, wherein the dovetail contact surface is reduced by a relief to alter a fundamental frequency of an assembly of the blade and member.
摘要翻译：根据本发明的一个方面，涡轮组件包括从叶片延伸的翼型件和位于叶片下部的燕尾榫，其中燕尾榫具有燕尾接触表面。涡轮机组件还包括具有狭槽的构件，槽被配置成经由燕尾形件连接到翼型件，该槽具有接触燕尾接触表面的槽接触表面，其中燕尾接触表面被减压以改变基部频率叶片和构件的组件。

16. 发明授权

US09043118B2 Methods and systems for model-based control of gas turbines 有权
标题翻译：燃气轮机模型控制方法与系统
公开(公告)号：US09043118B2
公开(公告)日：2015-05-26
申请号：US12054651
申请日：2008-03-25
申请人： Timothy Andrew Healy
发明人： Timothy Andrew Healy
IPC分类号： F02C9/00 , F01D17/00 , F02C9/22 , F02C9/26 , F02C9/28 , G05B13/04
CPC分类号： F02C9/00 , F01D17/00 , F02C9/22 , F02C9/26 , F02C9/28 , F05D2270/3011 , F05D2270/3013 , F05D2270/303 , F05D2270/31 , F05D2270/44 , F05D2270/54 , F05D2270/71 , G05B13/041
摘要： Embodiments of systems and methods for tuning a turbine are provided. In one embodiment, a method may include receiving at least one of a measured operating parameter or a modeled operating parameter of a turbine during operation; and tuning the turbine during operation. The turbine may be tuned during operation by applying the measured operating parameter or modeled operating parameter or parameters to at least one operational boundary model, applying the measured operating parameter or modeled operating parameter or parameters to at least one scheduling algorithm, comparing the output of the operational boundary model or models to the output of the scheduling algorithm or algorithms to determine at least one error term, and closing loop on the one error term or terms by adjusting at least one turbine control effector during operation of the turbine.
摘要翻译：提供了用于调节涡轮机的系统和方法的实施例。在一个实施例中，一种方法可以包括在运行期间接收涡轮机的测量操作参数或建模操作参数中的至少一个; 并在运行期间调整涡轮。可以在操作期间通过将测量的操作参数或建模的操作参数或参数应用于至少一个操作边界模型来在运行期间进行调节，将测量的操作参数或建模的操作参数或参数应用于至少一个调度算法，操作边界模型或模型到调度算法或算法的输出以确定至少一个误差项，以及通过在涡轮机的运行期间调节至少一个涡轮机控制效应器来关闭一个误差项或术语上的闭环。

17. 发明授权

US08926265B2 Inlet bleed heat system 有权
标题翻译：入口放气系统
公开(公告)号：US08926265B2
公开(公告)日：2015-01-06
申请号：US13291208
申请日：2011-11-08
申请人： Valery Ivanovich Ponyavin , Hua Zhang
发明人： Valery Ivanovich Ponyavin , Hua Zhang
IPC分类号： F01D25/10 , F01D17/00 , F02C7/045 , F02C7/047 , F02C7/057
CPC分类号： F01D17/00 , F02C7/045 , F02C7/047 , F02C7/057 , F02C9/18 , F05D2250/313 , F05D2270/101
摘要： An embodiment of the present invention takes the form of an IBH system that has a single conduit, which is positioned close to a downstream end of a silencer section. This arrangement may reduce the overall pressure drop associated with the inlet system. This arrangement may also promote a substantially uniform mixing between the cooler ambient air and the warmer heated air.
摘要翻译：本发明的一个实施例采用IBH系统的形式，该IBH系统具有靠近消音器部分的下游端的单个导管。这种布置可以减少与入口系统相关联的整体压降。这种布置还可以促进较冷的环境空气和较热的加热空气之间的基本上均匀的混合。

18. 发明授权

US08870530B2 Gas turbine engine 有权
标题翻译：燃气轮机
公开(公告)号：US08870530B2
公开(公告)日：2014-10-28
申请号：US13087870
申请日：2011-04-15
申请人： Romuald Morvant , Kevin M. Britchford
发明人： Romuald Morvant , Kevin M. Britchford
IPC分类号： F01D17/00 , F01D25/16 , F02K3/06 , F02K1/34 , F01D25/28 , F02C7/20
CPC分类号： F01D25/162 , B64D33/06 , F01D25/28 , F02C7/20 , F02K3/06 , F05D2240/14
摘要： A gas turbine engine has an annular bypass duct defined between a fan nacelle and a core fairing through which fan air is discharged. One or more bifurcator members are positioned inside the exit of the bypass duct to bifurcate the air flow in the bypass duct around the bifurcator members prior to exiting the bypass duct. The bifurcator members modify the flow field of the air in the bypass duct radially and/or tangentially with respect to the axis of the annular bypass duct.
摘要翻译：燃气涡轮发动机具有环形旁通管道，其限定在风扇机舱和风扇空气排出的整流罩之间。一个或多个分支器构件位于旁路管道的出口内部，以在离开旁路管道之前将分流器构件周围的旁路管道中的空气流分叉。分支器构件相对于环形旁通管的轴线径向地和/或切向地改变旁路管道中的空气的流场。

19. 发明授权

US08789369B2 Supercharging apparatus for vehicle 有权
标题翻译：车辆增压装置
公开(公告)号：US08789369B2
公开(公告)日：2014-07-29
申请号：US13546045
申请日：2012-07-11
申请人： Osamu Sato
发明人： Osamu Sato
IPC分类号： F02D23/00 , F01N3/00 , F01N3/027 , F01B25/00 , F01D17/00 , F01D19/00 , F01D21/00
CPC分类号： F02B37/20 , F02B37/025 , F02B37/183 , Y02T10/144
摘要： A turbocharger of a supercharging apparatus includes a turbine impeller, which is rotatable by exhaust gas discharged from an internal combustion engine of a vehicle. An electric heater is placed in an exhaust passage, which extends from an exhaust outlet of the internal combustion engine to the turbine impeller. The electric heater generates a heat when the electric heater is energized.
摘要翻译：增压装置的涡轮增压器包括涡轮叶轮，其可以通过从车辆的内燃机排出的废气旋转。电加热器放置在从内燃机的排气出口延伸到涡轮机叶轮的排气通道中。当电加热器通电时，电加热器产生热量。

20. 发明授权

US08523511B2 Adaptive variable geometry turbocharger strategy 有权
标题翻译：自适应变量几何涡轮增压器策略
公开(公告)号：US08523511B2
公开(公告)日：2013-09-03
申请号：US11938999
申请日：2007-11-13
申请人： Andrew C. Love , Gary Agnew , Baptiste Szczyrba
发明人： Andrew C. Love , Gary Agnew , Baptiste Szczyrba
IPC分类号： F01D17/00 , F01D17/16
CPC分类号： F01D17/165 , F02B29/0406 , F02B37/013 , F02B37/24 , F02D23/00 , F02D41/0007 , F02D41/2432 , F02D41/2438 , F02D41/2464 , F02D2250/16 , F05D2220/40 , F05D2270/62 , Y02T10/144
摘要： A variable geometry turbocharger employs multiple vanes in the turbine inlet with a unison ring and integral cast wall in the turbine housing forming the nozzle walls. An actuator rotates the unison ring through a rack and pinion driven crank shaft to move the vanes through a range of vane positions that extends between a hard-stop closed position and a hard-stop open position, and that includes a reference position corresponding to a desired flow condition. A variable geometry turbine controller uses a sensor indicating the actuation position of the actuator to guide the operation of the vanes to the reference position. The controller intermittently directs the actuator to force the vanes to the hard-stop closed and hard-stop open positions, and uses sensor information from those positions to reestablish the reference-position information that the actuator uses to guide the actuation of the vanes.
摘要翻译：可变几何涡轮增压器在涡轮机入口中使用多个叶片，其具有共振环和在涡轮机壳体中形成喷嘴壁的整体浇铸壁。致动器通过齿条和小齿轮驱动的曲轴使协调环旋转，以使叶片移动通过在硬停止关闭位置和硬停止打开位置之间延伸的一系列叶片位置，并且其包括对应于所需流量条件。可变几何涡轮机控制器使用传感器来表示致动器的致动位置，以将叶片的操作引导到参考位置。控制器间歇地引导致动器以迫使叶片进入硬停闭和硬停止位置，并且使用那些位置的传感器信息来重新建立致动器用于引导叶片致动的参考位置信息。

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