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公开(公告)号：US08801370B2
公开(公告)日：2014-08-12
申请号：US11548791
申请日：2006-10-12
Applicant: Dean Matthew Erickson , Hua Zhang , Jason Seale
Inventor： Dean Matthew Erickson , Hua Zhang , Jason Seale
CPC classification number: F01D11/24 , F01D25/14 , F05D2260/201 , Y02T50/676
Abstract: A impingement cooling system for heavy duty turbines that includes a manifold affixed to a casing of the heavy-duty turbine, wherein the manifold includes a plurality of impingement holes in the surface of the manifold and a blower that provides air flow across the plurality of impingement holes of the manifold to cool the casing of the heavy-duty turbine to control the clearance between a tip of a turbine blade and a shroud of the heavy-duty turbine.
Abstract translation: 一种用于重型涡轮机的冲击冷却系统，其包括固定在重载涡轮机的壳体上的歧管，其中歧管包括在歧管表面中的多个冲击孔和提供穿过多个冲击物的气流的鼓风机 歧管的孔以冷却重型涡轮机的壳体，以控制涡轮叶片的尖端和重型涡轮机的护罩之间的间隙。
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2.发明申请Systems and Methods for Modified Wobbe Index Control With Constant Fuel Temperature 有权具有恒定燃料温度的改进的沃泊指数控制系统和方法公开(公告)号：US20130008172A1
公开(公告)日：2013-01-10
申请号：US13176017
申请日：2011-07-05
Applicant: Dean Matthew Erickson , Brian Gallagher , Mihir Lal , Scott Day
Inventor： Dean Matthew Erickson , Brian Gallagher , Mihir Lal , Scott Day
CPC classification number: F02C7/224 , F02C9/26 , F05D2270/08 , F05D2270/303
Abstract: The present application provides a gas turbine engine system for combusting a flow of fuel. The gas turbine engine system may include a combustor and a fuel system for providing the flow of fuel to the combustor. The fuel system may include a fuel heat exchanger so as to provide the flow of fuel to the combustor at a substantially constant temperature.
Abstract translation: 本申请提供了一种用于燃烧燃料流的燃气涡轮发动机系统。 燃气涡轮发动机系统可以包括燃烧器和用于向燃烧器提供燃料流的燃料系统。 燃料系统可以包括燃料热交换器，以便在基本恒定的温度下向燃烧器提供燃料流。
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3.发明授权Externally adjustable impingement cooling manifold mount and thermocouple housing 有权外部可调冲击冷却歧管安装座和热电偶外壳公开(公告)号：US08123406B2
公开(公告)日：2012-02-28
申请号：US12267952
申请日：2008-11-10
Applicant: Dean Matthew Erickson , Mitch Mircea Orza , Michael George Savale , Hua Zhang
Inventor： Dean Matthew Erickson , Mitch Mircea Orza , Michael George Savale , Hua Zhang
CPC classification number: F01D9/04 , F01D9/06 , F01D11/14 , F05B2260/301 , F05D2260/201
Abstract: A mount includes a mounting bolt attached to a casing; an internal bushing that engages the casing at a distal end of the internal bushing; and an external bushing that engages a manifold and engages the internal bushing. The internal bushing is adjustable with respect to the external bushing thereby allowing the manifold to be adjustable with respect to the casing.
Abstract translation: 安装件包括附接到壳体的安装螺栓; 内套管，其在所述内衬套的远端处接合所述壳体; 以及与歧管接合并接合内部衬套的外部衬套。 内部衬套相对于外部衬套可调节，从而允许歧管相对于壳体可调节。
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4.发明申请APPARATUS AND METHOD FOR REDUCING ECCENTRICITY AND OUT-OF-ROUNDNESS IN TURBINES 有权降低涡度偏心度和不合格度的装置和方法公开(公告)号：US20090053035A1
公开(公告)日：2009-02-26
申请号：US11843926
申请日：2007-08-23
Applicant: Hua Zhang , Kenneth Neil Whaling , Jason Allen Seale , Dean Matthew Erickson , Michael Francis Michalski
Inventor： Hua Zhang , Kenneth Neil Whaling , Jason Allen Seale , Dean Matthew Erickson , Michael Francis Michalski
IPC: F01B25/04
CPC classification number: F01D11/24 , F05D2260/201 , Y02T50/676
Abstract: A turbine includes: a plurality of turbine blades arranged within a casing, the arrangement including a clearance between tips of the blades and the casing; a plurality of manifolds disposed proximate to the casing opposite the clearance, wherein each of the manifolds includes a plurality of impingement holes in the surface thereof; a source of clearance information; and a source of cooling air for supplying cooling air through a plurality of flow control devices to selected ones of the manifolds according to the clearance information. A system and a method are also provided.
Abstract translation: 涡轮机包括：布置在壳体内的多个涡轮叶片，该装置包括叶片的尖端和壳体之间的间隙; 多个歧管，其布置成靠近所述壳体与所述间隙相对，其中每个所述歧管在其表面中包括多个冲击孔; 清关信息来源; 以及用于通过多个流量控制装置将冷却空气根据间隙信息提供给所选歧管的冷却空气源。 还提供了一种系统和方法。
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5.发明申请Integrated support/thermocouple housing for impingement cooling manifolds and cooling method 失效用于冲击冷却歧管的集成支撑/热电偶外壳和冷却方法公开(公告)号：US20080193278A1
公开(公告)日：2008-08-14
申请号：US11705496
申请日：2007-02-13
Applicant: Dean Matthew Erickson , Mitch Mircea Orza , Jason Seale , Hua Zhang , Gregory Allan Crum
Inventor： Dean Matthew Erickson , Mitch Mircea Orza , Jason Seale , Hua Zhang , Gregory Allan Crum
IPC: F01D5/08
CPC classification number: F01D25/12 , F01D11/24 , F05D2260/201 , Y02T50/676
Abstract: A impingement cooling system for heavy duty turbines that includes a manifold affixed to a casing of the heavy-duty turbine, wherein the manifold includes a plurality of impingement holes in the surface of the manifold and a blower that provides air flow across the plurality of impingement holes of the manifold to cool the casing of the heavy-duty turbine to control the clearance between a tip of a turbine blade and a shroud of the heavy-duty turbine.
Abstract translation: 一种用于重型涡轮机的冲击冷却系统，其包括固定在重载涡轮机的壳体上的歧管，其中歧管包括在歧管表面中的多个冲击孔和提供穿过多个冲击物的气流的鼓风机 歧管的孔以冷却重型涡轮机的壳体，以控制涡轮叶片的尖端和重型涡轮机的护罩之间的间隙。
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Patent Agency Ranking
公开(公告)号：US09103284B2
公开(公告)日：2015-08-11
申请号：US13484410
申请日：2012-05-31
Applicant: Dean Matthew Erickson , Robert Lester Brooks , Douglas Scott Byrd , Joseph Robert Law
Inventor： Dean Matthew Erickson , Robert Lester Brooks , Douglas Scott Byrd , Joseph Robert Law
Abstract: An approach for utilizing fuel gas to purge a dormant fuel gas circuit is disclosed. In one aspect, there is a fuel gas supply that supplies fuel to fuel gas circuits. Gas control valves, each coupled to one of the fuel gas circuits control the flow of fuel gas thereto from the fuel gas supply. A fuel purge system selectively purges fuel gas circuits from the fuel gas circuits that are dormant with fuel gas from the fuel gas supply.
Abstract translation: 公开了一种利用燃料气体吹扫休眠燃料气体回路的方法。 一方面，存在向燃料气体回路供应燃料的燃料气体供应。 每个与燃料气体回路中的一个连接的气体控制阀控制燃料气体从燃料气体供应的流动。 燃料净化系统选择性地从燃料气体回路中燃烧气体回路，燃料气体回路与来自燃料气体源的燃料气体休眠。
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7.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
Applicant: Kenneth Neil Whaling , Dean Matthew Erickson , Hua Zhang , David Wesley Ball, Jr. , James L. Davis , Michael Savale , Douglas S. Byrd
Inventor： Kenneth Neil Whaling , Dean Matthew Erickson , Hua Zhang , David Wesley Ball, Jr. , James L. Davis , Michael Savale , Douglas S. Byrd
CPC classification number: F04F5/20 , F02C7/222 , F02K9/52 , F04F5/461 , F05D2240/36
Abstract: 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.
Abstract translation: 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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8.发明申请APPARATUS, SYSTEM AND METHOD FOR HEATING FUEL GAS USING GAS TURBINE EXHAUST 有权使用燃气涡轮排气加热燃油的装置，系统和方法公开(公告)号：US20100024429A1
公开(公告)日：2010-02-04
申请号：US12181715
申请日：2008-07-29
Applicant: Hua Zhang , Jatila Ranasinghe , Dean Matthew Erickson
Inventor： Hua Zhang , Jatila Ranasinghe , Dean Matthew Erickson
IPC: F02C7/224
Abstract: An apparatus, a system and a method by which fuel gas to drive a heat source is heated are provided. The apparatus includes a first gas passage by which at least a portion of the fuel gas is transported from an inlet to an outlet, the outlet being fluidly coupled to the heat source, a plurality of heat pipes in thermal communication, at respective first ends thereof, with the portion of the fuel gas transported by the first gas passage, and a heating element, fluidly coupled to the heat source to receive exhaust of the heat source, through which respective second ends of the heat pipes extend to be in position to be heated by the exhaust.
Abstract translation: 提供了一种用于驱动热源的燃料气体被加热的装置，系统和方法。 该装置包括第一气体通道，通过该第一气体通道将至少一部分燃料气体从入口输送到出口，该出口流体地联接到热源，多个热管，其热连通在其相应的第一端 其中由第一气体通道输送的燃料气体的一部分和加热元件流体耦合到热源以接收热源的排气，热管的相应的第二端延伸通过该加热元件的位置为 被排气加热。
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公开(公告)号：US20080089780A1
公开(公告)日：2008-04-17
申请号：US11548791
申请日：2006-10-12
Applicant: Dean Matthew Erickson , Hua Zhang , Jason Seale
Inventor： Dean Matthew Erickson , Hua Zhang , Jason Seale
IPC: F03B11/00
CPC classification number: F01D11/24 , F01D25/14 , F05D2260/201 , Y02T50/676
Abstract: A impingement cooling system for heavy duty turbines that includes a manifold affixed to a casing of the heavy-duty turbine, wherein the manifold includes a plurality of impingement holes in the surface of the manifold and a blower that provides air flow across the plurality of impingement holes of the manifold to cool the casing of the heavy-duty turbine to control the clearance between a tip of a turbine blade and a shroud of the heavy-duty turbine.
Abstract translation: 一种用于重型涡轮机的冲击冷却系统，其包括固定在重载涡轮机的壳体上的歧管，其中歧管包括在歧管表面中的多个冲击孔和提供穿过多个冲击物的气流的鼓风机 歧管的孔以冷却重型涡轮机的壳体，以控制涡轮叶片的尖端和重型涡轮机的护罩之间的间隙。
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10.发明授权Systems and methods for modified wobbe index control with constant fuel temperature 有权具有恒定燃料温度的改进沃泊指数控制的系统和方法公开(公告)号：US08459033B2
公开(公告)日：2013-06-11
申请号：US13176017
申请日：2011-07-05
Applicant: Dean Matthew Erickson , Brian Gallagher , Mihir Lal , Scott Day
Inventor： Dean Matthew Erickson , Brian Gallagher , Mihir Lal , Scott Day
IPC: F02C7/08
CPC classification number: F02C7/224 , F02C9/26 , F05D2270/08 , F05D2270/303
Abstract: The present application provides a gas turbine engine system for combusting a flow of fuel. The gas turbine engine system may include a combustor and a fuel system for providing the flow of fuel to the combustor. The fuel system may include a fuel heat exchanger so as to provide the flow of fuel to the combustor at a substantially constant temperature.
Abstract translation: 本申请提供了一种用于燃烧燃料流的燃气涡轮发动机系统。 燃气涡轮发动机系统可以包括用于向燃烧器提供燃料流的燃烧器和燃料系统。 燃料系统可以包括燃料热交换器，以便在基本恒定的温度下向燃烧器提供燃料流。
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