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31.发明授权公开(公告)号：US08006983B2
公开(公告)日：2011-08-30
申请号：US11965079
申请日：2007-12-27
Applicant: Steven Craig Russell , Nicholas Simon Graham , Kelsey Elizabeth Beach , James Michael Storey
Inventor： Steven Craig Russell , Nicholas Simon Graham , Kelsey Elizabeth Beach , James Michael Storey
CPC classification number: C10J3/485 , C10J3/74 , C10J3/845 , C10J2200/09 , C10K1/04 , C10K1/08 , C10K1/101 , F01K23/067 , F28D2021/0075 , F28F2230/00 , Y02E20/18
Abstract: 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.
Abstract translation: 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。
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32.发明申请Method and Apparatus for Shielding Cooling Tubes in a Radiant Syngas Cooler 失效用于屏蔽辐射合成气冷却器中的冷却管的方法和装置公开(公告)号：US20100263841A1
公开(公告)日：2010-10-21
申请号：US12425253
申请日：2009-04-16
Applicant: Judeth Brannon Corry , James Michael Storey
Inventor： Judeth Brannon Corry , James Michael Storey
CPC classification number: F28F9/00 , C10J3/86 , C10J2300/165 , C10J2300/1675 , C10J2300/169 , C10K1/003 , C10K1/004 , C10K1/006 , F28D7/1669 , F28D2021/0075 , F28F19/002 , F28F19/02 , Y02E20/16 , Y02E20/18
Abstract: Methods and a system for shielding cooling tubes in a radiant syngas cooler. The heat shields may prevent direct contact between heated syngas and the cooling tubes. The heat shield may be mounted to a header that also attaches to the cooling tubes. The heat shield may also be separated from the cooling tubes or, alternatively, the heat shield may be coated onto the cooling tubes. Furthermore, prolonged exposure to the heated syngas may corrode the heat shield.
Abstract translation: 用于屏蔽辐射式合成气冷却器中的冷却管的方法和系统。 隔热罩可能会阻止加热合成气与冷却管之间的直接接触。 隔热罩可以安装在也连接到冷却管的集管上。 隔热罩也可以与冷却管分开，或者也可以将热屏蔽层涂覆到冷却管上。 此外，长时间暴露于加热的合成气可能会腐蚀隔热罩。
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33.发明申请SYSTEMS FOR REDUCING COOLING WATER AND POWER CONSUMPTION IN GASIFICATION SYSTEMS AND METHODS OF ASSEMBLING SUCH SYSTEMS 有权用于减少排气系统中的冷却水和功率消耗的系统以及组装这些系统的方法公开(公告)号：US20100170285A1
公开(公告)日：2010-07-08
申请号：US12349366
申请日：2009-01-06
Applicant: Paul Steven Wallace , James Michael Storey , Aaron John Avagliano
Inventor： Paul Steven Wallace , James Michael Storey , Aaron John Avagliano
CPC classification number: F02C6/18 , F01K23/068 , F02C3/28 , F05D2220/31 , F25J3/04018 , F25J3/04121 , F25J3/04133 , F25J3/04545 , F25J3/04575 , F25J3/04606 , F25J3/04612 , F25J3/04618 , F25J2230/06 , F25J2240/70 , Y02E20/18 , Y10T29/53
Abstract: An integrated gasification combined cycle system is provided. The integrated gasification combined cycle system includes an air compressor coupled in flow communication to an air separation unit, a condensate heater coupled in flow communication with the air compressor, and a condenser coupled in flow communication with the condensate heater. The condensate heater and the air compressor are coupled such that a portion of compressed air generated by the air compressor is channeled to the condensate heater. A method of assembling an integrated gasification combined cycle system is also provided.
Abstract translation: 提供了一体化气化联合循环系统。 一体化气化联合循环系统包括与空气分离单元流动连通的空气压缩机，与空气压缩机流动连通的冷凝水加热器，以及与冷凝物加热器流体连通的冷凝器。 冷凝水加热器和空气压缩机联接成使得由空气压缩机产生的一部分压缩空气被引导到冷凝物加热器。 还提供了一种组合气化联合循环系统的方法。
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34.发明申请SYSTEMS AND METHODS FOR DETECTING A FLAME IN A FUEL NOZZLE OF A GAS TURBINE 有权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
Applicant: Gilbert Otto Kraemer , James Michael Storey , John Lipinski , Julio Enrique Mestroni , David Lee Williamson , Jason Randolph Marshall , Anthony Krull
Inventor： Gilbert Otto Kraemer , James Michael Storey , John Lipinski , Julio Enrique Mestroni , David Lee Williamson , Jason Randolph Marshall , Anthony Krull
CPC classification number: F23N5/184 , F23N5/242 , F23N2025/04 , F23N2031/28
Abstract: 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.
Abstract translation: 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。
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35.发明申请METHODS FOR FABRICATING SYNGAS COOLER PLATENS AND SYNGAS COOLER PLATENS 审中-公开用于制作合成冷却器板和SYGAS冷却板的方法公开(公告)号：US20090130001A1
公开(公告)日：2009-05-21
申请号：US11941543
申请日：2007-11-16
Applicant: James Michael Storey , Aaron John Avagliano , Fulton Jose Lopez , John Luigi Battaglioli , Scott Parent
Inventor： James Michael Storey , Aaron John Avagliano , Fulton Jose Lopez , John Luigi Battaglioli , Scott Parent
CPC classification number: F28D7/1676 , C10J3/466 , C10J3/86 , C10J2200/09 , C10J2300/1884 , C10J2300/1892 , F01K23/068 , F28D7/0041 , F28D2021/0075 , F28F2009/224 , Y02E20/18 , Y10T29/4935 , Y10T29/49378
Abstract: A method for fabricating a syngas cooler is provided. The method includes coupling a tube cage within the syngas cooler, and coupling a plurality of platens to the tube cage to facilitate steam production in the syngas cooler. At least a first platen has at least one of a length that is larger than a length of a second platen, a non-linear geometry, and an angular position that is oblique with respect to a wall of the syngas cooler.
Abstract translation: 提供一种制造合成气冷却器的方法。 该方法包括在合成气冷却器内连接管笼，并将多个压板耦合到管笼以促进合成气冷却器中的蒸汽产生。 至少第一压板具有大于第二压板的长度，非线性几何形状以及相对于合成气冷却器的壁倾斜的角位置中的至少一个。
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Patent Agency Ranking
公开(公告)号：US20090078397A1
公开(公告)日：2009-03-26
申请号：US11862021
申请日：2007-09-26
Applicant: James Michael Storey , Aaron John Avagliano , Ashley Nicole Gerbode , John Battaglioli
CPC classification number: F28D7/0041 , F01K23/068 , F22B21/02 , F22B21/34 , F22B21/38 , F22B37/145 , F28D7/1669 , F28D2021/0075 , Y02E20/18 , Y10T29/4935
Abstract: A method of assembling a radiant cooler includes providing a vessel shell that defines a gas flow passage therein that extends generally axially through the vessel shell, forming a tube cage from coupling a plurality of cooling tubes together to form a tube cage defined by a plurality of chevron-shaped projections that extend circumferentially about a center axis of the tube cage, each chevron-shaped projection includes a first side and a second side coupled together a tip, circumferentially-adjacent pairs of projections coupled together such that a valley is defined between each pair of circumferentially-spaced projections, each of the projection tips is positioned radially outward from each of the valleys, and orienting the tube cage within the vessel shell such that the tube cage is in flow communication with the flow passage.
Abstract translation: 组装辐射冷却器的方法包括提供容器壳体，其在其中大致轴向延伸通过容器壳体形成气体流动通道，形成管腔，将多个冷却管连接在一起形成由多个 每个人字形突起包括第一侧和第二侧，第一侧和第二侧联接在一起，所述第一侧和第二侧连接在一起，所述第一侧和第二侧与端部相邻地连接在一起，所述第一侧和第二侧周向相邻的一对突起联接在一起，使得在每个 一对周向间隔开的突起，每个突出末端位于每个谷的径向外侧，并将管笼定向在容器壳内，使得管笼与流动通道流动连通。
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37.发明授权公开(公告)号：US07003958B2
公开(公告)日：2006-02-28
申请号：US10879102
申请日：2004-06-30
Applicant: Constantin Alexandru Dinu , Iris Ziqin Hu , James Michael Storey
Inventor： Constantin Alexandru Dinu , Iris Ziqin Hu , James Michael Storey
Abstract: 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.
Abstract translation: 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。
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公开(公告)号：US06568188B2
公开(公告)日：2003-05-27
申请号：US10205228
申请日：2002-07-26
Applicant: Kevin Michael Kolman , James Michael Storey
Inventor： Kevin Michael Kolman , James Michael Storey
IPC: F02C100
Abstract: 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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公开(公告)号：US06449956B1
公开(公告)日：2002-09-17
申请号：US09828471
申请日：2001-04-09
Applicant: Kevin Michael Kolman , James Michael Storey
Inventor： Kevin Michael Kolman , James Michael Storey
IPC: F02C100
Abstract: 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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公开(公告)号：US08986403B2
公开(公告)日：2015-03-24
申请号：US12495439
申请日：2009-06-30
Applicant: Helge B. Klockow , James Michael Storey , Aaron John Avagliano , Guoqing Wang , Gary Dwayne Mandrusiak , Karl Hardcastle , Scott Parent , Prashant Tiwari , Gregory Laskowski , Judeth Brannon Corry , Constantin Dinu
Inventor： Helge B. Klockow , James Michael Storey , Aaron John Avagliano , Guoqing Wang , Gary Dwayne Mandrusiak , Karl Hardcastle , Scott Parent , Prashant Tiwari , Gregory Laskowski , Judeth Brannon Corry , Constantin Dinu
CPC classification number: C10J3/84 , C10J3/845 , C10J2300/1653 , C10J2300/1671 , C10K1/003 , C10K1/004 , C10K1/08 , C10K1/101 , Y02E20/18
Abstract: In one embodiment, a gasification system component, such as a quench unit or scrubber may retain of pool of a cooling fluid for cooling another fluid. The gasification system component includes a flow damping mechanism designed to dampen flow of the cooling fluid, the other fluid, or both, within the gasification system component. The flow damping mechanism may be disposed in an inner chamber formed between a dip tube and a draft tube or disposed in an outer chamber formed between the walls of the gasification system component and the draft tube. The flow damping mechanism also may be disposed between the inner chamber and the outer chamber.
Abstract translation: 在一个实施例中，气化系统部件，例如骤冷单元或洗涤器可以保留用于冷却另一流体的冷却流体池。 气化系统部件包括流动阻尼机构，其设计成在气化系统部件内抑制冷却流体，其它流体或两者的流动。 流动阻尼机构可以设置在形成在汲取管和引流管之间的内室中，或者设置在形成在气化系统部件的壁与引流管之间的外部室中。 流动阻尼机构还可以设置在内室和外室之间。
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