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1. 发明授权

US09038394B2 Convolution seal for transition duct in turbine system 有权
标题翻译：涡轮机系统中过渡管道的卷积密封
公开(公告)号：US09038394B2
公开(公告)日：2015-05-26
申请号：US13459533
申请日：2012-04-30
申请人： James Scott Flanagan , Jeffrey Scott LeBegue , Kevin Weston McMahan , Daniel Jackson Dillard , Ronnie Ray Pentecost
发明人： James Scott Flanagan , Jeffrey Scott LeBegue , Kevin Weston McMahan , Daniel Jackson Dillard , Ronnie Ray Pentecost
IPC分类号： F02C1/00 , F02C3/04 , F01D9/02 , F23R3/00 , F01D11/00
CPC分类号： F01D9/023 , F01D11/005 , F05D2240/55 , F05D2250/183 , F05D2300/10 , F05D2300/501 , F23R3/002
摘要： A turbine system is disclosed. In one embodiment, the turbine system includes a transition duct. The transition duct includes an inlet, an outlet, and a passage extending between the inlet and the outlet and defining a longitudinal axis, a radial axis, and a tangential axis. The outlet of the transition duct is offset from the inlet along the longitudinal axis and the tangential axis. The transition duct further includes an interface feature for interfacing with an adjacent transition duct. The turbine system further includes a convolution seal contacting the interface feature to provide a seal between the interface feature and the adjacent transition duct.
摘要翻译：公开了一种涡轮机系统。在一个实施例中，涡轮机系统包括过渡管道。过渡管道包括入口，出口和在入口和出口之间延伸并且限定纵向轴线，径向轴线和切线轴线的通道。过渡管道的出口沿着纵向轴线和切线轴线从入口偏移。过渡管道还包括用于与相邻过渡管道相连接的界面特征。涡轮机系统还包括接触接口特征的卷积密封件，以在接口特征和相邻的过渡管道之间提供密封。

2. 发明授权

US08650852B2 Support assembly for transition duct in turbine system 有权
标题翻译：涡轮机系统过渡管支撑组件
公开(公告)号：US08650852B2
公开(公告)日：2014-02-18
申请号：US13176183
申请日：2011-07-05
申请人： Jeffrey Scott LeBegue , Kevin Weston McMahan , Ronnie Ray Pentecost , James Scott Flanagan
发明人： Jeffrey Scott LeBegue , Kevin Weston McMahan , Ronnie Ray Pentecost , James Scott Flanagan
IPC分类号： F02C3/00
CPC分类号： F02C3/14 , F01D9/023 , F05D2250/25
摘要： A support assembly for a turbine system is disclosed. The support assembly includes a transition duct extending between a fuel nozzle and a turbine section. The transition duct has an inlet, an outlet, and a passage extending between the inlet and the outlet and defining a longitudinal axis, a radial axis, and a tangential axis. The outlet of the transition duct is offset from the inlet along the longitudinal axis. The support assembly further includes an annular contact member extending from the transition duct. The contact member is configured to allow movement of the transition duct about at least one axis.
摘要翻译：公开了一种用于涡轮机系统的支撑组件。支撑组件包括在燃料喷嘴和涡轮部分之间延伸的过渡管道。过渡管道具有入口，出口和在入口和出口之间延伸并且限定纵向轴线，径向轴线和切线轴线的通道。过渡管道的出口沿着纵向轴线从进口偏移。支撑组件还包括从过渡管道延伸的环形接触构件。接触构件构造成允许过渡管道围绕至少一个轴线移动。

3. 发明申请

US20130283817A1 FLEXIBLE SEAL FOR TRANSITION DUCT IN TURBINE SYSTEM 审中-公开
标题翻译：涡轮机系统中过渡管的柔性密封
公开(公告)号：US20130283817A1
公开(公告)日：2013-10-31
申请号：US13459501
申请日：2012-04-30
申请人： James Scott Flanagan , Jeffrey Scott LeBegue , Kevin Weston McMahan , Daniel Jackson Dillard , Ronnie Ray Pentecost
发明人： James Scott Flanagan , Jeffrey Scott LeBegue , Kevin Weston McMahan , Daniel Jackson Dillard , Ronnie Ray Pentecost
IPC分类号： F02C7/28
CPC分类号： F01D9/023 , F01D11/005 , F05D2240/55 , F05D2300/10 , F05D2300/501 , F05D2300/6012
摘要： A turbine system is disclosed. In one embodiment, the turbine system includes a transition duct. The transition duct includes an inlet, an outlet, and a passage extending between the inlet and the outlet and defining a longitudinal axis, a radial axis, and a tangential axis. The outlet of the transition duct is offset from the inlet along the longitudinal axis and the tangential axis. The transition duct further includes an interface feature for interfacing with an adjacent transition duct. The turbine system further includes a flexible seal contacting the interface feature to provide a seal between the interface feature and the adjacent transition duct. The flexible seal includes a sheet having a first surface, an opposing second surface, and a peripheral edge therebetween.
摘要翻译：公开了一种涡轮机系统。在一个实施例中，涡轮机系统包括过渡管道。过渡管道包括入口，出口和在入口和出口之间延伸并且限定纵向轴线，径向轴线和切线轴线的通道。过渡管道的出口沿着纵向轴线和切线轴线从入口偏移。过渡管道还包括用于与相邻过渡管道相连接的界面特征。涡轮机系统还包括接触接口特征的柔性密封件，以在接口特征和相邻的过渡管道之间提供密封。柔性密封件包括具有第一表面，相对的第二表面和它们之间的周边边缘的片材。

4. 发明申请

US20130283804A1 TRANSITION DUCT WITH LATE INJECTION IN TURBINE SYSTEM 有权
标题翻译：在涡轮机系统中具有最初注入的过渡管
公开(公告)号：US20130283804A1
公开(公告)日：2013-10-31
申请号：US13459516
申请日：2012-04-30
申请人： Jeffrey Scott LeBegue , Ronnie Ray Pentecost , James Scott Flanagan , Won-Wook Kim , Kevin Weston McMahan
发明人： Jeffrey Scott LeBegue , Ronnie Ray Pentecost , James Scott Flanagan , Won-Wook Kim , Kevin Weston McMahan
IPC分类号： F02C7/232
CPC分类号： F01D9/023 , F23R3/06 , F23R3/286 , F23R3/346 , F23R3/46 , F23R2900/03044
摘要： A system for supplying an injection fluid to a combustor is disclosed. The system includes a transition duct comprising an inlet, an outlet, and a passage extending between the inlet and the outlet and defining a longitudinal axis, a radial axis, and a tangential axis. The outlet of the transition duct is offset from the inlet along the longitudinal axis and the tangential axis. The passage defines a combustion chamber. The system further includes a tube providing fluid communication for the injection fluid to flow through the transition duct and into the combustion chamber.
摘要翻译：公开了一种用于向燃烧器供应喷射流体的系统。该系统包括过渡管道，其包括入口，出口和在入口和出口之间延伸并且限定纵向轴线，径向轴线和切线轴线的通道。过渡管道的出口沿着纵向轴线和切线轴线从入口偏移。通道限定燃烧室。该系统还包括提供流体连通的管，用于使注射流体流过过渡管并进入燃烧室。

5. 发明授权

US08459041B2 Leaf seal for transition duct in turbine system 有权
标题翻译：涡轮机系统过渡管叶片密封
公开(公告)号：US08459041B2
公开(公告)日：2013-06-11
申请号：US13292366
申请日：2011-11-09
申请人： James Scott Flanagan , Jeffrey Scott LeBegue , Kevin Weston McMahan , Daniel Jackson Dillard , Ronnie Ray Pentecost
发明人： James Scott Flanagan , Jeffrey Scott LeBegue , Kevin Weston McMahan , Daniel Jackson Dillard , Ronnie Ray Pentecost
IPC分类号： F23R3/60 , F01D9/023
CPC分类号： F01D9/023 , F01D11/005 , F05D2240/57
摘要： A turbine system is disclosed. In one embodiment, the turbine system includes a transition duct. The transition duct includes an inlet, an outlet, and a passage extending between the inlet and the outlet and defining a longitudinal axis, a radial axis, and a tangential axis. The outlet of the transition duct is offset from the inlet along the longitudinal axis and the tangential axis. The transition duct further includes an interface member for interfacing with a turbine section. The turbine system further includes a leaf seal contacting the interface member to provide a seal between the interface member and the turbine section.
摘要翻译：公开了一种涡轮机系统。在一个实施例中，涡轮机系统包括过渡管道。过渡管道包括入口，出口和在入口和出口之间延伸并且限定纵向轴线，径向轴线和切线轴线的通道。过渡管道的出口沿着纵向轴线和切线轴线从入口偏移。过渡管道还包括用于与涡轮部分相接合的接口部件。涡轮机系统还包括接触接口构件的叶片密封件，以在接口构件和涡轮机部分之间提供密封。

6. 发明申请

US20130008177A1 SUPPORT ASSEMBLY FOR TRANSITION DUCT IN TURBINE SYSTEM 有权
标题翻译：用于涡轮机系统过渡管的支撑组件
公开(公告)号：US20130008177A1
公开(公告)日：2013-01-10
申请号：US13176166
申请日：2011-07-05
申请人： Jeffrey Scott LeBegue , Kevin Weston McMahan , Ronnie Ray Pentecost , James Scott Flanagan
发明人： Jeffrey Scott LeBegue , Kevin Weston McMahan , Ronnie Ray Pentecost , James Scott Flanagan
IPC分类号： F02C7/20
CPC分类号： F01D9/023 , F02C3/14 , F05D2250/40
摘要： A support assembly for a turbine system is disclosed. The support assembly includes a transition duct extending between a fuel nozzle and a turbine section. The transition duct has an inlet, an outlet, and a passage extending between the inlet and the outlet and defining a longitudinal axis, a radial axis, and a tangential axis. The outlet of the transition duct is offset from the inlet along the longitudinal axis. The support assembly further includes a plurality of protrusions extending from the transition duct. The plurality of protrusions are configured to allow movement of the transition duct about at least one axis.
摘要翻译：公开了一种用于涡轮机系统的支撑组件。支撑组件包括在燃料喷嘴和涡轮部分之间延伸的过渡管道。过渡管道具有入口，出口和在入口和出口之间延伸并且限定纵向轴线，径向轴线和切线轴线的通道。过渡管道的出口沿着纵向轴线从进口偏移。支撑组件还包括从过渡管道延伸的多个突起。多个突起构造成允许过渡管道围绕至少一个轴线移动。

7. 发明申请

US20070129568A1 Ionic liquids 审中-公开
标题翻译：离子液体
公开(公告)号：US20070129568A1
公开(公告)日：2007-06-07
申请号：US11607138
申请日：2006-12-01
申请人： Scott Flanagan , Andrew Hunt
发明人： Scott Flanagan , Andrew Hunt
IPC分类号： C07C51/41 , C07C51/16 , C07F5/00 , C07F9/22 , C07F7/00 , C07F15/00
CPC分类号： C07F9/54 , B01F1/00 , C07C53/128 , C07C63/26 , C10N2220/04 , C25D3/66 , H01M8/1018 , H01M8/1072 , H01M2300/0045 , Y02P70/56
摘要： Low melting point organic liquid compounds with high boiling points are prepared by a preferred process having the J+xQy(R—COO−)x-y where x is 1 to 8, preferably 1-3, y is 0 to x−1, where R—COO− is an anion selected from the group consisting of 2-ethyl hexanoate, pivalate, neodecanoate, and mixtures thereof, Q is another anion or mixture of other anions, and J+x is a cation selected from cations of Groups IA, IIA, IB, IIB, IIIB, IVB, VB, VIB, VIIB, VIII and lanthanide metals, cations selected from cations of B, Si, Ge, As, Sb, Te and Po metalloids, an ammonium cation derived from ammonia or an organic amine, an organic phosphonium cation, and mixtures thereof the organic liquid compounds being substantially free of volatile organic compounds. These compounds, as liquids, are useful as low volatile organic solvents, e.g., solvents in which a variety of chemical reactions may be carried out.
摘要翻译：具有高沸点的低熔点有机液体化合物通过优选的方法制备，所述优选方法具有J + + Q'（R-COO）其中x为1至8，优选1-3，y为0至x-1，其中R-COO - 为选自下组的阴离子：2 - 己酸乙酯，新戊酸酯，和它们的混合物，Q是另一阴离子或其它阴离子的混合物，J + +是选自IA，IIA，IB，IIB，IIIB族的阳离子的阳离子，IVB，VB，VIB，VIIB，VIII和镧系元素金属，选自B，Si，Ge，As，Sb，Te和Po准金属离子的阳离子，衍生自氨或有机胺的铵阳离子，有机鏻阳离子，及其混合物，基本上不含挥发性有机化合物的有机液体化合物。这些化合物作为液体可用作低挥发性有机溶剂，例如可以进行各种化学反应的溶剂。

8. 发明授权

US07145412B2 Electronic and optical devices and methods of forming these devices 有权
公开(公告)号：US07145412B2
公开(公告)日：2006-12-05
申请号：US10362435
申请日：2001-08-24
申请人： Andrew T. Hunt , Mark G. Allen , David Kiesling , Robert E. Schwerzel , Yongdong Jiang , Fe Alma Gladden , John Wegman , Zhiyong Zhao , Matthew Scott Vinson , J. Eric McEntyre , Scott Flanagan , Todd Polley , J. Stevenson Kenney
发明人： Andrew T. Hunt , Mark G. Allen , David Kiesling , Robert E. Schwerzel , Yongdong Jiang , Fe Alma Gladden , John Wegman , Zhiyong Zhao , Matthew Scott Vinson , J. Eric McEntyre , Scott Flanagan , Todd Polley , J. Stevenson Kenney
IPC分类号： H01P5/04
CPC分类号： H01P1/181 , G02B6/12004 , G02B6/12007 , G02B6/29361 , G02B6/29395 , G02F1/0316 , G02F1/035 , G02F1/0508 , G02F1/0553 , G02F1/292 , H01G4/008 , H01G4/1227 , H01G4/33 , H01G7/06 , H01L21/31691 , H01L27/016
摘要： Electronic and optical (or photonic) devices with variable or switchable properties and methods used to form these devices, are disclosed. More specifically, the present invention involves forming layers of conductive material and dielectric material or materials with varying conductivity and indexes of refraction to form various electronic and optical devices. One such layer of adjustable material is formed by depositing epitaxial or reduced grain boundary barium strontium titanate on the C-plane of sapphire.

9. 发明授权

US4895583A Apparatus and method for separating air 失效
标题翻译：用于分离空气的装置和方法
公开(公告)号：US4895583A
公开(公告)日：1990-01-23
申请号：US296543
申请日：1989-01-12
申请人： Scott Flanagan , Robert A. Mostello , Anne P. Ko
发明人： Scott Flanagan , Robert A. Mostello , Anne P. Ko
IPC分类号： F25J3/04
CPC分类号： F25J3/04169 , F25J3/04206 , F25J3/04303 , F25J3/04309 , F25J3/04418 , F25J2200/54 , F25J2205/62 , F25J2250/40 , F25J2250/50
摘要： Method and Apparatus for separating a gaseous mixture into component gases wherein a portion of a compressed cooled stream of the gaseous mixture is substantially liquefied and respective portions sent to high and low pressure columns and either one of the gaseous components or a portion of the gaseous mixture is utilized for refrigeration from expansion with a portion of the work utilized for compression of the gaseous mixture.

10. 发明授权

US09133722B2 Transition duct with late injection in turbine system 有权
标题翻译：涡轮机系统后期喷射过渡管
公开(公告)号：US09133722B2
公开(公告)日：2015-09-15
申请号：US13459516
申请日：2012-04-30
申请人： Jeffrey Scott LeBegue , Ronnie Ray Pentecost , James Scott Flanagan , Won-Wook Kim , Kevin Weston McMahan
发明人： Jeffrey Scott LeBegue , Ronnie Ray Pentecost , James Scott Flanagan , Won-Wook Kim , Kevin Weston McMahan
IPC分类号： F23R3/34 , F01D9/02 , F23R3/06 , F23R3/28 , F23R3/46
CPC分类号： F01D9/023 , F23R3/06 , F23R3/286 , F23R3/346 , F23R3/46 , F23R2900/03044
摘要： A system for supplying an injection fluid to a combustor is disclosed. The system includes a transition duct comprising an inlet, an outlet, and a passage extending between the inlet and the outlet and defining a longitudinal axis, a radial axis, and a tangential axis. The outlet of the transition duct is offset from the inlet along the longitudinal axis and the tangential axis. The passage defines a combustion chamber. The system further includes a tube providing fluid communication for the injection fluid to flow through the transition duct and into the combustion chamber.
摘要翻译：公开了一种用于向燃烧器供应喷射流体的系统。该系统包括过渡管道，其包括入口，出口和在入口和出口之间延伸并且限定纵向轴线，径向轴线和切线轴线的通道。过渡管道的出口沿着纵向轴线和切线轴线从入口偏移。通道限定燃烧室。该系统还包括提供流体连通的管，用于使注射流体流过过渡管并进入燃烧室。

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