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1. 发明授权

US09121613B2 Combustor with brief quench zone with slots 有权
标题翻译：燃烧器与狭缝的短暂淬火区域
公开(公告)号：US09121613B2
公开(公告)日：2015-09-01
申请号：US13488466
申请日：2012-06-05
申请人： William Francis Carnell, Jr. , Gregory Allen Boardman
发明人： William Francis Carnell, Jr. , Gregory Allen Boardman
IPC分类号： F02C3/20 , F23R3/14 , F23R3/42 , F23R3/12 , F23R3/30 , F23R3/58
CPC分类号： F23R3/42 , F23R2900/00015
摘要： The present application provides a combustor for combusting a number of flows of air and a number of flows of fuel. The combustor may include a central swirler for producing a high swirl quench air flow, a number of trapped vortex cavities surrounding the central swirler for producing a flow of combustion gases, a brief severe quench zone downstream of the trapped vortex cavities to quench the flow of combustion gases between an outer quench air flow and the high swirl quench air flow, and an expansion zone downstream of the brief severe quench zone.
摘要翻译：本申请提供了一种用于燃烧多个空气流和多个燃料流的燃烧器。燃烧器可以包括用于产生高漩涡骤冷空气流的中心旋流器，围绕中心旋流器的多个被捕获的涡流腔，用于产生燃烧气体流，在被捕获的涡流腔下游的短暂的严酷淬火区域以淬灭在外部骤冷空气流与高旋涡骤冷空气流之间的燃烧气体以及在短暂的严酷骤冷区下游的膨胀区。

2. 发明申请

US20130318992A1 Combustor with a Brief Severe Quench Zone 有权
标题翻译：燃烧器与一个严重的淬火区域
公开(公告)号：US20130318992A1
公开(公告)日：2013-12-05
申请号：US13488466
申请日：2012-06-05
申请人： William Francis Carnell, JR. , Gregory Allen Boardman
发明人： William Francis Carnell, JR. , Gregory Allen Boardman
IPC分类号： F23R3/36 , F02C7/228 , F02C3/20 , F23R3/14
CPC分类号： F23R3/42 , F23R2900/00015
摘要： The present application provides a combustor for combusting a number of flows of air and a number of flows of fuel. The combustor may include a central swirler for producing a high swirl quench air flow, a number of trapped vortex cavities surrounding the central swirler for producing a flow of combustion gases, a brief severe quench zone downstream of the trapped vortex cavities to quench the flow of combustion gases between an outer quench air flow and the high swirl quench air flow, and an expansion zone downstream of the brief severe quench zone.
摘要翻译：本申请提供了一种用于燃烧多个空气流和多个燃料流的燃烧器。燃烧器可以包括用于产生高漩涡骤冷空气流的中心旋流器，围绕中心旋流器的多个被捕获的涡流腔，用于产生燃烧气体流，在被捕获的涡流腔下游的短暂的严酷淬火区域以淬灭在外部骤冷空气流与高旋涡骤冷空气流之间的燃烧气体以及在短暂的严酷骤冷区下游的膨胀区。

3. 发明授权

US09182123B2 Combustor fuel nozzle and method for supplying fuel to a combustor 有权
标题翻译：燃烧器燃料喷嘴和用于向燃烧器供应燃料的方法
公开(公告)号：US09182123B2
公开(公告)日：2015-11-10
申请号：US13344033
申请日：2012-01-05
申请人： Gregory Allen Boardman , Ronald James Chila , Johnie F. McConnaughhay
发明人： Gregory Allen Boardman , Ronald James Chila , Johnie F. McConnaughhay
IPC分类号： F23R3/14 , F23R3/28
CPC分类号： F23R3/14 , F23R3/286
摘要： A combustor fuel nozzle includes a center body and an inner shroud that circumferentially surrounds at least a portion of the center body. The inner shroud has a downstream surface. The fuel nozzle includes an inner passage between the center body and the inner shroud, an outer passage that circumferentially surrounds at least a portion of the inner shroud and a first plurality of fuel ports extending substantially radially outward through the center body. The first plurality of fuel ports is upstream from the downstream surface of the inner shroud. A method for supplying fuel to a combustor fuel nozzle includes flowing a working fluid through an inner passage between a center body and an inner shroud, injecting a fuel from the center body against the inner shroud, and flowing a portion of the working fluid through an outer passage that surrounds at least a portion of the inner shroud.
摘要翻译：燃烧器燃料喷嘴包括中心体和周向围绕中心体的至少一部分的内护罩。内护罩具有下游表面。燃料喷嘴包括在中心体和内护罩之间的内通道，周向围绕内护罩的至少一部分的外通道和基本上径向向外延伸穿过中心体的第一多个燃料口。第一多个燃料口在内护罩的下游表面上游。向燃烧器燃料喷嘴供给燃料的方法包括使工作流体流过中心体和内护罩之间的内部通道，将燃料从中心体喷射到内护罩上，并使工作流体的一部分流过外通道围绕内护罩的至少一部分。

4. 发明授权

US09157635B2 Fuel distribution manifold 有权
标题翻译：燃油分配歧管
公开(公告)号：US09157635B2
公开(公告)日：2015-10-13
申请号：US13342497
申请日：2012-01-03
申请人： Donald Mark Bailey , Gregory Allen Boardman , William Thomas Ross
发明人： Donald Mark Bailey , Gregory Allen Boardman , William Thomas Ross
IPC分类号： B01F5/00 , F23K5/06 , F02C7/22
CPC分类号： F23K5/06 , F02C7/222 , Y10T137/85938
摘要： A fuel distribution manifold comprises an outer shell having an inner surface. The outer shell defines an inlet for receiving fuel from a parent supply line, a base opposite the inlet, a central manifold axis that intersects the inlet, and a plurality of outlets for delivering fuel to offspring fuel lines, each outlet defining a respective outlet axis. In one exemplary embodiment, a fuel distribution manifold also comprises a center-body having an outer surface and being positioned within the outer shell wherein the outer surface of the center-body and the inner surface of the outer shell define a flow-path through which fluid flows from the inlet to the plurality of outlets. In another exemplary embodiment, at least one of the outlets is positioned adjacent to the base and oriented so that its respective outlet axis is rotated relatively to a radial direction that intersects the central manifold axis.
摘要翻译：燃料分配歧管包括具有内表面的外壳。外壳限定用于从母体供应管线接收燃料的入口，与入口相对的底座，与入口相交的中心歧管轴线以及用于将燃料输送到后代燃料管线的多个出口，每个出口限定相应的出口轴线。在一个示例性实施例中，燃料分配歧管还包括具有外表面并且位于外壳内的中心体，其中中心体的外表面和外壳的内表面限定了流动路径，通过该流路流体从入口流到多个出口。在另一个示例性实施例中，至少一个出口定位成与基座相邻并且定向成使得其相应的出口轴线相对于与中心歧管轴线相交的径向方向旋转。

5. 发明授权

US08991190B2 Fuel nozzle staging with water flowing prior to fuel in a main fuel circuit during start-up 有权
标题翻译：燃油喷嘴在启动期间在主燃料回路中的燃料流动之前进行分级
公开(公告)号：US08991190B2
公开(公告)日：2015-03-31
申请号：US13362059
申请日：2012-01-31
申请人： Hua Zhang , Douglas Frank Beadie , Gregory Allen Boardman , Geoffrey David Myers
发明人： Hua Zhang , Douglas Frank Beadie , Gregory Allen Boardman , Geoffrey David Myers
IPC分类号： F02C7/26
CPC分类号： F02C7/236 , F02C3/30 , F02C9/40 , F23D11/10 , F23D2209/30 , F23D2900/00016 , F23K5/14 , F23K5/18 , F23K2301/20 , F23N2027/02 , F23N2027/04
摘要： A method for transferring fuel includes flowing water to at least one nozzle of a main fuel circuit. Also included is flowing oil to the at least one nozzle of the main fuel circuit. Further included is flowing liquid fuel to the at least one nozzle of the main fuel circuit, wherein flowing water to the at least one nozzle of the main fuel circuit occurs prior to flowing oil to the at least one nozzle of the main fuel circuit and flowing liquid fuel to the at least one nozzle of the main fuel circuit.
摘要翻译：一种用于输送燃料的方法包括将水流向主燃料回路的至少一个喷嘴。还包括流动油到主燃料回路的至少一个喷嘴。还包括流动的液体燃料到主燃料回路的至少一个喷嘴，其中流动的水到主燃料回路的至少一个喷嘴发生在将油流到主燃料回路的至少一个喷嘴并流动液体燃料到主燃料回路的至少一个喷嘴。

6. 发明授权

US08801428B2 Combustor and method for supplying fuel to a combustor 有权
标题翻译：用于向燃烧器供应燃料的燃烧器和方法
公开(公告)号：US08801428B2
公开(公告)日：2014-08-12
申请号：US13252279
申请日：2011-10-04
申请人： Patrick Benedict Melton , Willy Steve Ziminsky , Gregory Allen Boardman
发明人： Patrick Benedict Melton , Willy Steve Ziminsky , Gregory Allen Boardman
IPC分类号： F02C1/00 , F23R3/10 , F23R3/28 , F23R3/46 , F23R3/34 , F23D14/62
CPC分类号： F23R3/343 , F23D14/62 , F23R3/10 , F23R3/286 , F23R3/46 , F23R2900/00001 , F23R2900/03343
摘要： A combustor includes an end cap having upstream and downstream surfaces and a cap shield surrounding the upstream and downstream surfaces. First and second sets of premixer tubes extend from the upstream surface through the downstream surface. A first fuel conduit supplies fuel to the first set of premixer tubes. A casing circumferentially surrounds the cap shield to define an annular passage, and a second fuel conduit supplies fuel through the annular passage to the second set of premixer tubes. A method for supplying fuel to a combustor includes flowing a working fluid through first and second sets of premixer tubes, flowing a first fuel into the first set of premixer tubes, and flowing a second fuel through an annular passage surrounding the end cap and into the second set of premixer tubes.
摘要翻译：燃烧器包括具有上游和下游表面的端盖和围绕上游表面和下游表面的盖罩。第一组和第二组预混合管从上游表面延伸穿过下游表面。第一燃料管道向第一组预混合器管供应燃料。壳体周向地围绕盖罩以限定环形通道，并且第二燃料管道将燃料通过环形通道供应到第二组预混合器管。用于向燃烧器供应燃料的方法包括使工作流体流过第一组和第二组预混合器管，将第一燃料流入第一组预混合器管，并使第二种燃料流过围绕端盖的环形通道并进入第二组预混管。

7. 发明申请

US20130192236A1 Method For Transferring Fuel 有权
标题翻译：燃料转运方法
公开(公告)号：US20130192236A1
公开(公告)日：2013-08-01
申请号：US13362059
申请日：2012-01-31
申请人： Hua Zhang , Douglas Frank Beadie , Gregory Allen Boardman , Geoffrey David Myers
发明人： Hua Zhang , Douglas Frank Beadie , Gregory Allen Boardman , Geoffrey David Myers
IPC分类号： F02M61/16
CPC分类号： F02C7/236 , F02C3/30 , F02C9/40 , F23D11/10 , F23D2209/30 , F23D2900/00016 , F23K5/14 , F23K5/18 , F23K2301/20 , F23N2027/02 , F23N2027/04
摘要： A method for transferring fuel includes flowing water to at least one nozzle of a main fuel circuit. Also included is flowing oil to the at least one nozzle of the main fuel circuit. Further included is flowing liquid fuel to the at least one nozzle of the main fuel circuit, wherein flowing water to the at least one nozzle of the main fuel circuit occurs prior to flowing oil to the at least one nozzle of the main fuel circuit and flowing liquid fuel to the at least one nozzle of the main fuel circuit.
摘要翻译：一种用于输送燃料的方法包括将水流向主燃料回路的至少一个喷嘴。还包括流动油到主燃料回路的至少一个喷嘴。还包括流动的液体燃料到主燃料回路的至少一个喷嘴，其中流动的水到主燃料回路的至少一个喷嘴发生在将油流到主燃料回路的至少一个喷嘴并流动液体燃料到主燃料回路的至少一个喷嘴。

8. 发明申请

US20130186094A1 Axial Flow Fuel Nozzle with a Stepped Center Body 有权
标题翻译：具有阶梯式中心体的轴流式燃油喷嘴
公开(公告)号：US20130186094A1
公开(公告)日：2013-07-25
申请号：US13354897
申请日：2012-01-20
申请人： Nishant Govindbhai Parsania , Geoffrey D. Myers , Gregory Allen Boardman
发明人： Nishant Govindbhai Parsania , Geoffrey D. Myers , Gregory Allen Boardman
IPC分类号： F23R3/14
CPC分类号： F23R3/286 , F23D11/16 , F23L7/002 , F23R3/14
摘要： An axial flow fuel nozzle for a gas turbine includes a plurality of annular passages for delivering materials for combustion. An annular air passage receives compressor discharge air, and a plurality of swirler vane slots are positioned adjacent an axial end of the annular air passage. A first next annular passage is disposed radially inward of the annular air passage and includes first openings positioned adjacent an axial end of the first annular passage and downstream of the swirler vane slots. A second next annular passage is disposed radially inward of the first annular passage and includes second openings positioned adjacent an axial end of the second annular passage and downstream of the first openings.
摘要翻译：用于燃气轮机的轴流式燃料喷嘴包括用于输送用于燃烧的材料的多个环形通道。环形空气通道接收压缩机排放空气，并且多个旋流器叶片槽邻近环形空气通道的轴向端定位。第一个下一个环形通道设置在环形空气通道的径向内侧，并且包括邻近第一环形通道的轴向端部并且位于旋流器叶片槽的下游的第一开口。第二个下一个环形通道设置在第一环形通道的径向内侧，并且包括邻近第二环形通道的轴向端部和第一开口下游定位的第二开口。

9. 发明授权

US08418469B2 Fuel nozzle assembly for gas turbine system 有权
标题翻译：燃气轮机系统燃油喷嘴总成
公开(公告)号：US08418469B2
公开(公告)日：2013-04-16
申请号：US12890903
申请日：2010-09-27
申请人： Geoffrey David Myers , Nishant Govindbhai Parsania , Gregory Allen Boardman
发明人： Geoffrey David Myers , Nishant Govindbhai Parsania , Gregory Allen Boardman
IPC分类号： F02C1/00
CPC分类号： F23R3/14 , F23D11/402 , F23D14/64 , F23D2900/00008 , F23D2900/14701 , F23R3/286 , F23R3/343 , F23R3/36
摘要： A fuel nozzle assembly is disclosed. The fuel nozzle assembly comprises an outer burner tube and an inner burner tube defining a pre-mixing annulus therebetween. The fuel nozzle assembly further comprises a swirler assembly, the swirler assembly comprising a plurality of swirler vanes disposed in an annular array about the inner burner tube and configured to interact with primary air upstream of the pre-mixing annulus. The fuel nozzle assembly further comprises an air injection feature configured to flow secondary air into the pre-mixing annulus downstream of the swirler assembly such that the secondary air flows in a generally linear path longitudinally with respect to the pre-mixing annulus and adjacent at least one of the outer burner tube and the inner burner tube.
摘要翻译：公开了一种燃料喷嘴组件。燃料喷嘴组件包括外部燃烧器管和在其间限定预混合环的内部燃烧器管。所述燃料喷嘴组件还包括旋流器组件，所述旋流器组件包括围绕所述内部燃烧器管设置成环形阵列并被配置为与所述预混合环空上游的一次空气相互作用的多个旋流器叶片。燃料喷嘴组件还包括空气喷射特征，该空气喷射特征构造成将二次空气流入旋流器组件下游的预混合环空，使得二次空气相对于预混气环纵向流动，并且至少相邻外部燃烧器管和内部燃烧器管之一。

10. 发明申请

US20120305086A1 SYSTEM AND METHOD FOR SUPPLYING FUEL 有权
标题翻译：供油系统和方法
公开(公告)号：US20120305086A1
公开(公告)日：2012-12-06
申请号：US13153585
申请日：2011-06-06
申请人： Hua Zhang , Douglas Frank Beadie , Gregory Allen Boardman , Geoffrey David Myers , William Thomas Ross
发明人： Hua Zhang , Douglas Frank Beadie , Gregory Allen Boardman , Geoffrey David Myers , William Thomas Ross
IPC分类号： F17D3/00 , E03B11/16
CPC分类号： F23K5/12 , F02C3/30 , F02C7/222 , F05D2240/126 , F05D2240/127 , Y10T137/0318 , Y10T137/85978
摘要： A system for supplying fuel includes a fuel manifold, a water manifold, and a fluid junction between the fuel manifold and the water manifold. A turbulator downstream from the fluid junction receives a fluid flow from the fluid junction. A method for supplying fuel includes flowing fuel through a fuel manifold, flowing water through a water manifold, and combining a portion of the water from the water manifold with the fuel from the fuel manifold to create emulsion fuel. The method further includes flowing the emulsion fuel through a turbulator.
摘要翻译：用于供应燃料的系统包括燃料歧管，水歧管以及燃料歧管和水歧管之间的流体连接。从流体连接器下游的湍流器接收来自流体结的流体流。用于供应燃料的方法包括使燃料流经燃料歧管，使水流过水歧管，并且将来自水歧管的一部分水与来自燃料歧管的燃料组合以产生乳化燃料。该方法还包括使乳化燃料流过湍流器。

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