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61. 发明授权

US08959769B2 Method and apparatus for heat recovery within a syngas cooler 有权
标题翻译：在合成气冷却器内热回收的方法和装置
公开(公告)号：US08959769B2
公开(公告)日：2015-02-24
申请号：US11828785
申请日：2007-07-26
申请人： Robert Henri Gauthier , James Michael Storey , Yasir Hafeez Abbasi
发明人： Robert Henri Gauthier , James Michael Storey , Yasir Hafeez Abbasi
IPC分类号： F28F9/22 , F28D7/16 , F28D7/00 , C10J3/86 , F01K23/06 , F28F9/02 , F28D21/00
CPC分类号： F28D7/0041 , C10J3/86 , C10J2300/0959 , C10J2300/0973 , C10J2300/0996 , C10J2300/165 , C10J2300/1671 , C10J2300/1675 , C10J2300/1678 , C10J2300/1838 , C10J2300/1884 , F01K23/068 , F28D2021/0075 , F28F9/02 , Y02E20/18 , Y02P20/124 , Y10T29/4935 , Y10T29/49364
摘要： A method of assembling a syngas cooler is provided. The method includes coupling a supply line within a cooler shell, coupling a heat transfer panel within the cooler shell, and coupling a heat transfer enclosure within the cooler shell such that the heat transfer enclosure substantially isolates the heat transfer panel from the cooler shell. A manifold is coupled in flow communication with the supply line, the heat transfer enclosure, and the heat transfer panel.
摘要翻译：提供了组合合成气冷却器的方法。该方法包括将冷却器壳体内的供应管线联接在一起，将冷却器壳体内的传热面板联接在一起，并将冷却器壳体内的传热外壳联接在一起，使得传热外壳将传热面板与冷却器壳体基本隔离。歧管与供应管线，传热外壳和传热板流体连通地联接。

62. 发明授权

US08834584B2 Method of assembly and apparatus for cooling syngas 有权
标题翻译：装配方法和冷却合成气的装置
公开(公告)号：US08834584B2
公开(公告)日：2014-09-16
申请号：US12568275
申请日：2009-09-28
申请人： Lien-Yan Chen , James Michael Storey , Yasir H. Abbasi , George Dodan
发明人： Lien-Yan Chen , James Michael Storey , Yasir H. Abbasi , George Dodan
IPC分类号： B01J7/00 , C10J3/86 , F02C3/28 , F28D7/00 , F28D7/16 , F28D21/00
CPC分类号： F02C3/28 , C10J3/86 , C10J2300/1653 , C10J2300/1678 , F28D7/0041 , F28D7/1669 , F28D2021/0075 , Y02E20/18 , Y10T29/49826
摘要： A syngas cooler for use in a gasification system is described that includes a head portion including a plurality of conduit headers. The syngas cooler also includes an annular shell portion including a plurality of conduits, the plurality of conduits configured to be coupled in flow communication with the plurality of conduit headers. The syngas cooler also includes a quench portion configured to remove particulates entrained in a flow of syngas flowing through the syngas cooler. The head portion and the shell portion are configured to be coupled together with a circumferential seam weld.
摘要翻译：描述了用于气化系统的合成气冷却器，其包括包括多个导管集管的头部。合成气冷却器还包括包括多个管道的环形壳体部分，多个导管被构造成与多个管道集管流动连通地联接。合成气冷却器还包括骤冷部分，其构造成去除夹带在流过合成气冷却器的合成气流中的微粒。头部和外壳部分构造成与圆周缝合焊接在一起。

63. 发明授权

US08357215B2 Method and apparatus of particulate removal from gasifier components 有权
标题翻译：从气化器部件中除去微粒的方法和装置
公开(公告)号：US08357215B2
公开(公告)日：2013-01-22
申请号：US12397658
申请日：2009-03-04
申请人： Steven Craig Russell , James Michael Storey , Robert Henri Gauthier
发明人： Steven Craig Russell , James Michael Storey , Robert Henri Gauthier
IPC分类号： C10J3/82 , F28G7/00
CPC分类号： C10J3/72 , C10J3/526 , C10J3/74 , C10J3/86 , C10J2200/36 , F22B1/1846 , F28D7/0041 , F28G7/00 , F28G9/00 , F28G15/02
摘要： Disclosed is a method of removing a particulate layer from a gasification system component including locating a shedding apparatus in operable communication with the gasification system component. A force is transmitted from the shedding apparatus into the gasification system component and the particulate layer is shed from the gasification system component as a result of the force. Further disclosed is a syngas cooler for a gasification system including a vessel and a plurality of thermal energy transfer platens located in the vessel. A shedding apparatus is in operable communication with the plurality of platens and is capable of shedding a particulate layer from the plurality of platens by transmitting a force to the plurality of platens. The apparatus includes a manifold disposed between the shedding apparatus and the plurality of platens and connected to the plurality of platens via one or more struts capable of distributing the force to the plurality of platens.
摘要翻译：公开了一种从气化系统部件除去颗粒层的方法，包括定位与气化系统部件可操作地连通的脱开装置。力从脱落装置传递到气化系统部件中，并且由于力而使颗粒层从气化系统部件脱落。还公开了一种用于气化系统的合成气冷却器，其包括容器和位于容器中的多个热能转移压板。脱落装置与多个压板可操作地连通，并且能够通过将力传递到多个压板而从多个压板中脱落颗粒层。该设备包括设置在脱落装置和多个压板之间的歧管，并经由能够将力分配给多个压板的一个或多个支柱连接到多个压板。

64. 发明授权

US08287815B2 Methods and systems for controlling temperature in a vessel 有权
标题翻译：用于控制容器温度的方法和系统
公开(公告)号：US08287815B2
公开(公告)日：2012-10-16
申请号：US12114545
申请日：2008-05-02
申请人： Steven Craig Russell , James Michael Storey , Robert Henri Gauthier
发明人： Steven Craig Russell , James Michael Storey , Robert Henri Gauthier
IPC分类号： B01J19/00 , F28D7/00 , F28D21/00 , F25D17/06 , F02B43/00
CPC分类号： F28D7/0066 , F02C3/24 , F02C3/28 , F02C6/18 , F05D2220/72 , F05D2260/61 , F28D7/0041 , F28D2021/0075 , F28F2265/10 , Y02E20/18
摘要： A method and system for preheating a vessel that includes an area of excess heat and a flow of purge fluid that is channeled to an area to be purged wherein the purge fluid is deficient of heat are provided. The system includes a cooling tube assembly positioned between the area of excess heat and the area to be purged and a first heat exchanger coupled in flow communication to the cooling tube assembly, the first heat exchanger configured to transfer heat between a flow of cooling fluid through the cooling tube assembly and the flow of purge fluid wherein the flow of cooling fluid through the cooling tube assembly is maintained sub-cooled and the flow of purge fluid is heated to facilitate reducing a thermal stress in the area purged.
摘要翻译：提供一种用于预热容器的方法和系统，该容器包括过热区域和被吹送到待清洗区域的清洗流体流，其中清洗流体不足热。该系统包括一个位于过热区域和待净化区域之间的冷却管组件，以及与冷却管组件流动连通地连接的第一热交换器，第一热交换器构造成在冷却流体流通过之间传递热量冷却管组件和吹扫流体的流动，其中通过冷却管组件的冷却流体的流动被维持过冷却，并且净化流体的流动被加热以便于减少清洗的区域中的热应力。

65. 发明授权

US08024930B2 Heat integration in coal gasification and methanation reaction process 有权
标题翻译：煤气化和甲烷化反应过程中的热集成
公开(公告)号：US08024930B2
公开(公告)日：2011-09-27
申请号：US12349127
申请日：2009-01-06
申请人： Sampath Kumar Bommareddy , Karthik Subramanyan , James Michael Storey , Jerrold Samuel Kassman , Kurt Richard Imai
发明人： Sampath Kumar Bommareddy , Karthik Subramanyan , James Michael Storey , Jerrold Samuel Kassman , Kurt Richard Imai
IPC分类号： F01K7/34
CPC分类号： F02C6/18 , C10J3/466 , C10J3/86 , C10J2300/1662 , C10J2300/1675 , C10J2300/1807 , C10K1/101 , C10K3/04 , C10L3/08 , F01K3/185 , F01K3/188 , F01K7/18 , F22B1/1838 , Y02P20/123 , Y02P20/124
摘要： A combined Gasification, methanation and power island steam turbine system. The system includes a gasification portion, the methanation portion and a steam turbine portion. The Gasification portion includes the new heat recovery design and associated controls for obtaining a desired steam to dry gas ration of 1.1-2.2. The methanation portion includes first, second and third methanation reactors and associated heat recovery integrated with a high-pressure, low-pressure superheater, and HP economizers. The power Island steam turbine includes a High pressure, Intermediate pressure, low-pressure steam turbine having an input coupled to an output of the superheaters in Methanation process.
摘要翻译：组合气化，甲烷化和动力岛蒸汽轮机系统。该系统包括气化部分，甲烷化部分和汽轮机部分。气化部分包括新的热回收设计和相关控制，用于获得所需的蒸汽至干燥气体比为1.1-2.2。甲烷化部分包括与高压，低压过热器和HP节能器集成的第一，第二和第三甲烷化反应器和相关联的热回收。 Power Island蒸汽轮机包括一个高压，中压，低压蒸汽轮机，其具有在甲烷化过程中耦合到过热器的输出的输入。

66. 发明授权

US08006983B2 Sealing assembly for use with a pressurized vessel and methods of assembling the same 有权
标题翻译：用于加压容器的密封组件及其组装方法
公开(公告)号：US08006983B2
公开(公告)日：2011-08-30
申请号：US11965079
申请日：2007-12-27
申请人： Steven Craig Russell , Nicholas Simon Graham , Kelsey Elizabeth Beach , James Michael Storey
发明人： Steven Craig Russell , Nicholas Simon Graham , Kelsey Elizabeth Beach , James Michael Storey
IPC分类号： F16L21/02 , F16J15/02
CPC分类号： C10J3/485 , C10J3/74 , C10J3/845 , C10J2200/09 , C10K1/04 , C10K1/08 , C10K1/101 , F01K23/067 , F28D2021/0075 , F28F2230/00 , Y02E20/18
摘要： A method for assembling a seal assembly is provided. The method includes coupling a first ring within a vessel, coupling a second ring within the vessel, and coupling a first seal layer between the first ring and the second ring such that the first seal layer contacts at least the first ring.
摘要翻译：提供了组装密封组件的方法。该方法包括在容器内连接第一环，将容器内的第二环联接，并且在第一环和第二环之间联接第一密封层，使得第一密封层至少接触第一环。

67. 发明申请

US20100170217A1 SYSTEMS AND METHODS FOR DETECTING A FLAME IN A FUEL NOZZLE OF A GAS TURBINE 有权
标题翻译：用于检测气体燃料燃料喷射器中的火焰的系统和方法
公开(公告)号：US20100170217A1
公开(公告)日：2010-07-08
申请号：US12350626
申请日：2009-01-08
申请人： Gilbert Otto Kraemer , James Michael Storey , John Lipinski , Julio Enrique Mestroni , David Lee Williamson , Jason Randolph Marshall , Anthony Krull
发明人： Gilbert Otto Kraemer , James Michael Storey , John Lipinski , Julio Enrique Mestroni , David Lee Williamson , Jason Randolph Marshall , Anthony Krull
IPC分类号： F02C9/46 , G01L11/00
CPC分类号： F23N5/184 , F23N5/242 , F23N2025/04 , F23N2031/28
摘要： A system may detect a flame about a fuel nozzle of a gas turbine. The gas turbine may have a compressor and a combustor. The system may include a first pressure sensor, a second pressure sensor, and a transducer. The first pressure sensor may detect a first pressure upstream of the fuel nozzle. The second pressure sensor may detect a second pressure downstream of the fuel nozzle. The transducer may be operable to detect a pressure difference between the first pressure sensor and the second pressure sensor.
摘要翻译：系统可以检测燃气轮机的燃料喷嘴周围的火焰。燃气轮机可以具有压缩机和燃烧器。该系统可以包括第一压力传感器，第二压力传感器和换能器。第一压力传感器可以检测燃料喷嘴上游的第一压力。第二压力传感器可以检测燃料喷嘴下游的第二压力。传感器可操作以检测第一压力传感器和第二压力传感器之间的压力差。

68. 发明授权

US07003958B2 Multi-sided diffuser for a venturi in a fuel injector for a gas turbine 失效
标题翻译：用于燃气轮机的燃料喷射器中的文丘里管的多面扩散器
公开(公告)号：US07003958B2
公开(公告)日：2006-02-28
申请号：US10879102
申请日：2004-06-30
申请人： Constantin Alexandru Dinu , Iris Ziqin Hu , James Michael Storey
发明人： Constantin Alexandru Dinu , Iris Ziqin Hu , James Michael Storey
IPC分类号： F02C1/00 , F02G3/00
CPC分类号： F23R3/34 , F23R3/286 , F23R3/40
摘要： A combustor for a gas turbine includes a main fuel injector for receiving compressor discharge air and mixing the air with fuel for flow to a downstream catalytic section. The main fuel injector includes an array of venturis each having an inlet, a throat and a diffuser. A main fuel supply plenum between forward and aft plates supplies fuel to secondary annular plenums having openings for supplying fuel into the inlets of the venturis upstream of the throats. Each diffuser transitions from a circular cross-section at the throat to multiple discrete angularly related side walls at the diffuser exit. Gaps between circumferentially and radially spaced diffusers at their exits are eliminated. With this arrangement, uniform flow distribution of the fuel/air, velocity and temperature is provided at the catalyst inlet.
摘要翻译：用于燃气轮机的燃烧器包括主燃料喷射器，用于接收压缩机排放空气并将空气与用于流动的燃料混合到下游催化部分。主燃料喷射器包括每个具有入口，喉部和扩散器的孔的阵列。前后板之间的主要燃料供应气室将燃料供给到具有用于将燃料供应到喉部上游的通风口的入口的开口的次级环形增压室。每个扩散器从喉部的圆形横截面到扩散器出口处的多个离散的角度相关的侧壁。在其出口处的周向和径向间隔的扩散器之间的间隙被消除。通过这种布置，在催化剂入口处提供了燃料/空气，速度和温度的均匀流量分布。

69. 发明授权

US06568188B2 Bypass air injection method and apparatus for gas turbines 有权
公开(公告)号：US06568188B2
公开(公告)日：2003-05-27
申请号：US10205228
申请日：2002-07-26
申请人： Kevin Michael Kolman , James Michael Storey
发明人： Kevin Michael Kolman , James Michael Storey
IPC分类号： F02C100
CPC分类号： F23C13/00 , F23R3/40
摘要： A bypass air injection scheme for a combustor of a gas turbine. Combustor includes a body with an inner liner and a casing enclosing the body with a passageway defined therebetween. A predetermined amount of the compressor discharge air passing through the passageway is extracted through a manifold. A conduit feeds the extracted air into an injection manifold having a plurality of injection tubes for injecting the extracted air into the combustor bypassing the reactor. The injection tubes and the injection manifold are disposed in a substantially common axial plane.

70. 发明授权

US06449956B1 Bypass air injection method and apparatus for gas turbines 有权
公开(公告)号：US06449956B1
公开(公告)日：2002-09-17
申请号：US09828471
申请日：2001-04-09
申请人： Kevin Michael Kolman , James Michael Storey
发明人： Kevin Michael Kolman , James Michael Storey
IPC分类号： F02C100
CPC分类号： F23C13/00 , F23R3/40
摘要： A bypass air injection scheme for a combustor of a gas turbine. Combustor includes a body with an inner liner and a casing enclosing the body with a passageway defined therebetween. A predetermined amount of the compressor discharge air passing through the passageway is extracted through a manifold. A conduit feeds the extracted air into an injection manifold having a plurality of injection tubes for injecting the extracted air into the combustor bypassing the reactor. The injection tubes and the injection manifold are disposed in a substantially common axial plane.

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