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1. 发明授权

US09719681B2 System and method for supplying fuel 有权
公开(公告)号：US09719681B2
公开(公告)日：2017-08-01
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： F16K11/20 , F23K5/12 , F02C3/30 , F02C7/22
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.

2. 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。

3. 发明申请

US20130098056A1 SYSTEM AND METHOD FOR TURBINE COMBUSTOR FUEL ASSEMBLY 有权
标题翻译：用于涡轮机燃油组件的系统和方法
公开(公告)号：US20130098056A1
公开(公告)日：2013-04-25
申请号：US13280237
申请日：2011-10-24
申请人： Hua Zhang , Douglas Frank Beadie , Geoffrey David Myers , Fabien Thibault Codron , William Thomas Ross
发明人： Hua Zhang , Douglas Frank Beadie , Geoffrey David Myers , Fabien Thibault Codron , William Thomas Ross
IPC分类号： F02C9/26 , F02C3/30
CPC分类号： F02C3/305 , Y02E20/16 , Y02T50/671
摘要： A system includes a turbine fuel supply system. The turbine fuel supply system includes a first turbine fuel mixer configured to mix a first liquid fuel and a first deaerated water to generate a first fuel mixture. The first fuel mixture is configured to combust in a combustor of a gas turbine engine. The turbine fuel supply system also includes a deaerated water flow path configured to route the first deaerated water to the first turbine fuel mixer and a liquid fuel flow path configured to route the first liquid fuel to the first turbine fuel mixer.
摘要翻译：一种系统包括涡轮燃料供应系统。涡轮燃料供应系统包括构造成混合第一液体燃料和第一脱气水以产生第一燃料混合物的第一涡轮燃料混合器。第一燃料混合物构造成在燃气涡轮发动机的燃烧器中燃烧。涡轮燃料供应系统还包括一个脱气水流通道，其配置成将第一除气水路由第一涡轮燃料混合器和将第一液体燃料路由到第一涡轮燃料混合器的液体燃料流路。

4. 发明授权

US09267433B2 System and method for turbine combustor fuel assembly 有权
标题翻译：涡轮燃烧器燃油组件的系统和方法
公开(公告)号：US09267433B2
公开(公告)日：2016-02-23
申请号：US13280237
申请日：2011-10-24
申请人： Hua Zhang , Douglas Frank Beadie , Geoffrey David Myers , Fabien Thibault Codron , William Thomas Ross
发明人： Hua Zhang , Douglas Frank Beadie , Geoffrey David Myers , Fabien Thibault Codron , William Thomas Ross
IPC分类号： F02C3/30
CPC分类号： F02C3/305 , Y02E20/16 , Y02T50/671
摘要： A system includes a turbine fuel supply system. The turbine fuel supply system includes a first turbine fuel mixer configured to mix a first liquid fuel and a first deaerated water to generate a first fuel mixture. The first fuel mixture is configured to combust in a combustor of a gas turbine engine. The turbine fuel supply system also includes a deaerated water flow path configured to route the first deaerated water to the first turbine fuel mixer and a liquid fuel flow path configured to route the first liquid fuel to the first turbine fuel mixer.
摘要翻译：一种系统包括涡轮燃料供应系统。涡轮燃料供应系统包括构造成混合第一液体燃料和第一脱气水以产生第一燃料混合物的第一涡轮燃料混合器。第一燃料混合物构造成在燃气涡轮发动机的燃烧器中燃烧。涡轮燃料供应系统还包括一个脱气水流通道，其配置成将第一除气水路由第一涡轮燃料混合器和将第一液体燃料路由到第一涡轮燃料混合器的液体燃料流路。

5. 发明授权

US09371989B2 Combustor nozzle and method for supplying fuel to a combustor 有权
标题翻译：燃烧器喷嘴和用于向燃烧器供应燃料的方法
公开(公告)号：US09371989B2
公开(公告)日：2016-06-21
申请号：US13110256
申请日：2011-05-18
申请人： Gregory Allen Boardman , Geoffrey David Myers , William Thomas Ross
发明人： Gregory Allen Boardman , Geoffrey David Myers , William Thomas Ross
IPC分类号： F02C7/22 , F23D11/16 , F23L7/00 , F23R3/34
CPC分类号： F23D11/16 , F23C2900/07021 , F23L7/005 , F23L2900/07008 , F23R3/343
摘要： A combustor nozzle includes a first and second liquid fuel passages that terminate at first and second fuel ports. A first diluent passage terminates at a first diluent outlet radially surrounding the second fuel ports. A second diluent passage terminates at a second diluent outlet between the first diluent outlet and the second fuel ports. A third diluent passage surrounds at least a portion of the first and second diluent passages. A method for supplying fuel to a combustor includes flowing a liquid fuel through a first fuel passage and flowing an emulsified liquid fuel through a second fuel passage. The method further includes flowing a first diluent through a shroud surrounding the second fuel passage to a first diluent passage surrounding at least a portion of the second fuel passage and flowing a second diluent through a second diluent passage radially disposed between the first diluent passage and the second fuel passage.
摘要翻译：燃烧器喷嘴包括在第一和第二燃料端口处终止的第一和第二液体燃料通道。第一稀释剂通道终止于径向围绕第二燃料端口的第一稀释剂出口。第二稀释剂通道在第一稀释剂出口和第二燃料端口之间终止于第二稀释剂出口。第三稀释剂通道围绕第一和第二稀释剂通道的至少一部分。用于向燃烧器供应燃料的方法包括使液体燃料流过第一燃料通道并使乳化液体燃料流过第二燃料通道。该方法还包括使第一稀释剂流过围绕第二燃料通道的护罩到围绕第二燃料通道的至少一部分的第一稀释剂通道，并使第二稀释剂流过放射状设置在第一稀释剂通道和第二稀释剂通道第二燃料通道。

6. 发明申请

US20120291447A1 COMBUSTOR NOZZLE AND METHOD FOR SUPPLYING FUEL TO A COMBUSTOR 有权
标题翻译：燃烧器喷嘴和向燃烧器供应燃料的方法
公开(公告)号：US20120291447A1
公开(公告)日：2012-11-22
申请号：US13110256
申请日：2011-05-18
申请人： Gregory Allen Boardman , Geoffrey David Myers , William Thomas Ross
发明人： Gregory Allen Boardman , Geoffrey David Myers , William Thomas Ross
IPC分类号： F02C7/22
CPC分类号： F23D11/16 , F23C2900/07021 , F23L7/005 , F23L2900/07008 , F23R3/343
摘要： A combustor nozzle includes a first and second liquid fuel passages that terminate at first and second fuel ports. A first diluent passage terminates at a first diluent outlet radially surrounding the second fuel ports. A second diluent passage terminates at a second diluent outlet between the first diluent outlet and the second fuel ports. A third diluent passage surrounds at least a portion of the first and second diluent passages. A method for supplying fuel to a combustor includes flowing a liquid fuel through a first fuel passage and flowing an emulsified liquid fuel through a second fuel passage. The method further includes flowing a first diluent through a shroud surrounding the second fuel passage to a first diluent passage surrounding at least a portion of the second fuel passage and flowing a second diluent through a second diluent passage radially disposed between the first diluent passage and the second fuel passage.
摘要翻译：燃烧器喷嘴包括在第一和第二燃料端口处终止的第一和第二液体燃料通道。第一稀释剂通道终止于径向围绕第二燃料端口的第一稀释剂出口。第二稀释剂通道在第一稀释剂出口和第二燃料端口之间终止于第二稀释剂出口。第三稀释剂通道围绕第一和第二稀释剂通道的至少一部分。用于向燃烧器供应燃料的方法包括使液体燃料流过第一燃料通道并使乳化液体燃料流过第二燃料通道。该方法还包括使第一稀释剂流过围绕第二燃料通道的护罩到围绕第二燃料通道的至少一部分的第一稀释剂通道，并使第二稀释剂流过放射状设置在第一稀释剂通道和第二稀释剂通道第二燃料通道。

7. 发明申请

US20130167954A1 FUEL DISTRIBUTION MANIFOLD 有权
标题翻译：燃油分配管理
公开(公告)号：US20130167954A1
公开(公告)日：2013-07-04
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： F16L41/00
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。

8. 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。

9. 发明申请

US20120266604A1 FUEL NOZZLE AND METHOD FOR OPERATING A COMBUSTOR 有权
标题翻译：燃油喷嘴和操作燃烧器的方法
公开(公告)号：US20120266604A1
公开(公告)日：2012-10-25
申请号：US13449695
申请日：2012-04-18
申请人： Predrag Popovic , Gilbert Otto Kraemer , William Thomas Ross , Vladimir Belvaev
发明人： Predrag Popovic , Gilbert Otto Kraemer , William Thomas Ross , Vladimir Belvaev
IPC分类号： F02C7/22 , F23D14/48 , F02C7/264
CPC分类号： F23R3/14 , F02C7/264 , F02C7/266 , F23C7/004 , F23R3/28 , F23R3/286
摘要： A fuel nozzle and a method for operating a combustor are disclosed. The method includes flowing a fuel and an oxidizer through a fuel nozzle, the fuel nozzle comprising an inner tube, an intermediate tube, and an outer tube each configured for flowing one of the fuel or the oxidizer therethrough. At least one of the inner tube, the intermediate tube, or the outer tube includes a plurality of swirler vanes. The method further includes imparting a swirl to the fuel and the oxidizer in the fuel nozzle, and exhausting the fuel and the oxidizer from the fuel nozzle into a combustion zone.
摘要翻译：公开了燃料喷嘴和操作燃烧器的方法。该方法包括使燃料和氧化剂流过燃料喷嘴，燃料喷嘴包括内管，中间管和外管，每个都配置成使燃料或氧化剂之一流过其中。内管，中间管或外管中的至少一个包括多个旋流叶片。该方法还包括向燃料喷嘴中的燃料和氧化剂施加漩涡，并将燃料和氧化剂从燃料喷嘴排出到燃烧区中。

10. 发明授权

US09500369B2 Fuel nozzle and method for operating a combustor 有权
标题翻译：燃料喷嘴和操作燃烧器的方法
公开(公告)号：US09500369B2
公开(公告)日：2016-11-22
申请号：US13449695
申请日：2012-04-18
申请人： Predrag Popovic , Gilbert Otto Kraemer , William Thomas Ross , Vladimir Belvaev
发明人： Predrag Popovic , Gilbert Otto Kraemer , William Thomas Ross , Vladimir Belvaev
IPC分类号： F23R3/14 , F23R3/28 , F02C7/264 , F02C7/266 , F23C7/00
CPC分类号： F23R3/14 , F02C7/264 , F02C7/266 , F23C7/004 , F23R3/28 , F23R3/286
摘要： A fuel nozzle and a method for operating a combustor are disclosed. The method includes flowing a fuel and an oxidizer through a fuel nozzle, the fuel nozzle comprising an inner tube, an intermediate tube, and an outer tube each configured for flowing one of the fuel or the oxidizer therethrough. At least one of the inner tube, the intermediate tube, or the outer tube includes a plurality of swirler vanes. The method further includes imparting a swirl to the fuel and the oxidizer in the fuel nozzle, and exhausting the fuel and the oxidizer from the fuel nozzle into a combustion zone.
摘要翻译：公开了燃料喷嘴和操作燃烧器的方法。该方法包括使燃料和氧化剂流过燃料喷嘴，燃料喷嘴包括内管，中间管和外管，每个都配置成使燃料或氧化剂之一流过其中。内管，中间管或外管中的至少一个包括多个旋流叶片。该方法还包括向燃料喷嘴中的燃料和氧化剂施加漩涡，并将燃料和氧化剂从燃料喷嘴排出到燃烧区中。

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