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公开(公告)号：US08555648B2
公开(公告)日：2013-10-15
申请号：US12705193
申请日：2010-02-12
IPC分类号： F02C1/00
摘要： A fuel injector nozzle is disclosed. The nozzle includes a nozzle body having a fuel conduit that extends from a fuel inlet through a fuel outlet conduit to a fuel outlet and a fluid conduit that extends from a fluid inlet through a fluid outlet conduit to a fluid outlet. The fuel outlet conduit and fuel outlet configured to produce a liquid fuel jet from the fuel outlet upon introduction of a pressurized liquid fuel into the fuel conduit. The fluid outlet conduit and fluid outlet are configured to produce a liquid fluid jet from the fluid outlet upon introduction of a pressurized liquid fluid into the fluid conduit, wherein the liquid fuel jet and the liquid fluid jet are configured to impact one another and produce a flow stream of atomized fuel.
摘要翻译： 公开了一种燃料喷射器喷嘴。 喷嘴包括具有燃料管道的喷嘴体，燃料导管从燃料入口通过燃料出口导管延伸到燃料出口，以及从流体入口通过流体出口导管延伸到流体出口的流体导管。 燃料出口导管和燃料出口构造成在将加压的液体燃料引入燃料管道中时从燃料出口产生液体燃料射流。 流体出口导管和流体出口构造成在将加压液体流体引入流体导管中时从流体出口产生液体流体射流，其中液体燃料射流和液体流体射流被配置为相互冲击并产生 雾化燃料流。
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公开(公告)号：US20110197588A1
公开(公告)日：2011-08-18
申请号：US12705150
申请日：2010-02-12
摘要： A fuel injector nozzle is disclosed. The nozzle includes a nozzle body for fluid communication of a liquid fuel to produce a liquid fuel jet and a fluid to produce a fluid jet. The nozzle body includes an adapter comprising a fuel conduit and a fluid conduit. The nozzle body also includes a nozzle tip disposed on the adapter comprising a plurality of fuel outlet conduits that are in fluid communication with the fuel conduits and a plurality of fluid outlet conduits that are in fluid communication with the fluid conduits.
摘要翻译： 公开了一种燃料喷射器喷嘴。 喷嘴包括用于液体燃料流体连通以产生液体燃料射流和流体以产生流体射流的喷嘴体。 喷嘴体包括适配器，该适配器包括燃料导管和流体导管。 喷嘴主体还包括设置在适配器上的喷嘴尖端，包括与燃料管道流体连通的多个燃料出口管道和与流体管道流体连通的多个流体出口导管。
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公开(公告)号：US08584467B2
公开(公告)日：2013-11-19
申请号：US12705171
申请日：2010-02-12
IPC分类号： F02C7/22
摘要： A method of controlling a combustor of a gas turbine is disclosed. The method includes operatively disposing a combustor can in a combustor of a gas turbine. The combustor can comprising a plurality of combustor fuel nozzles, each having a fuel injector and configured to selectively provide a liquid fuel, a liquid fluid or liquid fuel and liquid fluid to a fuel injector nozzle that is configured to provide, respectively, a plurality of liquid fuel jets, a plurality of liquid fluid jets or a combination thereof, that are in turn configured to provide an atomized liquid fuel stream, an atomized liquid fluid stream, or an atomized and emulsified liquid fuel-liquid fluid stream, respectively. The method also includes selectively providing an amount of fuel, fluid or a combination thereof to the fuel injector nozzle to produce an atomized fuel stream, atomized fluid stream, or an atomized and emulsified fuel-fluid stream, respectively.
摘要翻译： 公开了一种控制燃气轮机燃烧器的方法。 该方法包括在燃气轮机的燃烧器中可操作地设置燃烧室。 燃烧器可以包括多个燃烧器燃料喷嘴，每个燃料喷嘴具有燃料喷射器并被配置为选择性地向燃料喷射器喷嘴提供液体燃料，液体流体或液体燃料和液体流体，燃料喷射器喷嘴被配置为分别提供多个 液体燃料射流，多个液体流体射流或其组合，其又分别构造成提供雾化液体燃料流，雾化液体流体流或雾化和乳化液体燃料 - 液体流体流。 该方法还包括选择性地将一定量的燃料，流体或其组合提供给燃料喷射器喷嘴，以分别产生雾化燃料流，雾化流体流或雾化和乳化的燃料流体流。
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4.发明申请Systems and Methods for Modified Wobbe Index Control With Constant Fuel Temperature 有权具有恒定燃料温度的改进的沃泊指数控制系统和方法公开(公告)号：US20130008172A1
公开(公告)日：2013-01-10
申请号：US13176017
申请日：2011-07-05
申请人： Dean Matthew Erickson , Brian Gallagher , Mihir Lal , Scott Day
发明人： Dean Matthew Erickson , Brian Gallagher , Mihir Lal , Scott Day
CPC分类号： F02C7/224 , F02C9/26 , F05D2270/08 , F05D2270/303
摘要： The present application provides a gas turbine engine system for combusting a flow of fuel. The gas turbine engine system may include a combustor and a fuel system for providing the flow of fuel to the combustor. The fuel system may include a fuel heat exchanger so as to provide the flow of fuel to the combustor at a substantially constant temperature.
摘要翻译： 本申请提供了一种用于燃烧燃料流的燃气涡轮发动机系统。 燃气涡轮发动机系统可以包括燃烧器和用于向燃烧器提供燃料流的燃料系统。 燃料系统可以包括燃料热交换器，以便在基本恒定的温度下向燃烧器提供燃料流。
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公开(公告)号：US08468834B2
公开(公告)日：2013-06-25
申请号：US12705150
申请日：2010-02-12
IPC分类号： F02C1/00
摘要： A fuel injector nozzle is disclosed. The nozzle includes a nozzle body for fluid communication of a liquid fuel to produce a liquid fuel jet and a fluid to produce a fluid jet. The nozzle body includes an adapter comprising a fuel conduit and a fluid conduit. The nozzle body also includes a nozzle tip disposed on the adapter comprising a plurality of fuel outlet conduits that are in fluid communication with the fuel conduits and a plurality of fluid outlet conduits that are in fluid communication with the fluid conduits.
摘要翻译： 公开了一种燃料喷射器喷嘴。 喷嘴包括用于液体燃料流体连通以产生液体燃料射流和流体以产生流体射流的喷嘴体。 喷嘴体包括适配器，该适配器包括燃料导管和流体导管。 喷嘴主体还包括设置在适配器上的喷嘴尖端，包括与燃料管道流体连通的多个燃料出口管道和与流体管道流体连通的多个流体出口导管。
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6.发明授权Systems and methods for modified wobbe index control with constant fuel temperature 有权具有恒定燃料温度的改进沃泊指数控制的系统和方法公开(公告)号：US08459033B2
公开(公告)日：2013-06-11
申请号：US13176017
申请日：2011-07-05
申请人： Dean Matthew Erickson , Brian Gallagher , Mihir Lal , Scott Day
发明人： Dean Matthew Erickson , Brian Gallagher , Mihir Lal , Scott Day
IPC分类号： F02C7/08
CPC分类号： F02C7/224 , F02C9/26 , F05D2270/08 , F05D2270/303
摘要： The present application provides a gas turbine engine system for combusting a flow of fuel. The gas turbine engine system may include a combustor and a fuel system for providing the flow of fuel to the combustor. The fuel system may include a fuel heat exchanger so as to provide the flow of fuel to the combustor at a substantially constant temperature.
摘要翻译： 本申请提供了一种用于燃烧燃料流的燃气涡轮发动机系统。 燃气涡轮发动机系统可以包括用于向燃烧器提供燃料流的燃烧器和燃料系统。 燃料系统可以包括燃料热交换器，以便在基本恒定的温度下向燃烧器提供燃料流。
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公开(公告)号：US20110197594A1
公开(公告)日：2011-08-18
申请号：US12705171
申请日：2010-02-12
摘要： A method of controlling a combustor of a gas turbine is disclosed. The method includes operatively disposing a combustor can in a combustor of a gas turbine. The combustor can comprising a plurality of combustor fuel nozzles, each having a fuel injector and configured to selectively provide a liquid fuel, a liquid fluid or liquid fuel and liquid fluid to a fuel injector nozzle that is configured to provide, respectively, a plurality of liquid fuel jets, a plurality of liquid fluid jets or a combination thereof, that are in turn configured to provide an atomized liquid fuel stream, an atomized liquid fluid stream, or an atomized and emulsified liquid fuel-liquid fluid stream, respectively. The method also includes selectively providing an amount of fuel, fluid or a combination thereof to the fuel injector nozzle to produce an atomized fuel stream, atomized fluid stream, or an atomized and emulsified fuel-fluid stream, respectively.
摘要翻译： 公开了一种控制燃气轮机燃烧器的方法。 该方法包括在燃气轮机的燃烧器中可操作地设置燃烧室。 燃烧器可以包括多个燃烧器燃料喷嘴，每个燃料喷嘴具有燃料喷射器并被配置为选择性地向燃料喷射器喷嘴提供液体燃料，液体流体或液体燃料和液体流体，燃料喷射器喷嘴被配置为分别提供多个 液体燃料射流，多个液体流体射流或其组合，其又分别构造成提供雾化液体燃料流，雾化液体流体流或雾化和乳化液体燃料 - 液体流体流。 该方法还包括选择性地将一定量的燃料，流体或其组合提供给燃料喷射器喷嘴，以分别产生雾化燃料流，雾化流体流或雾化和乳化的燃料流体流。
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公开(公告)号：US20110197589A1
公开(公告)日：2011-08-18
申请号：US12705193
申请日：2010-02-12
摘要： A fuel injector nozzle is disclosed. The nozzle includes a nozzle body having a fuel conduit that extends from a fuel inlet through a fuel outlet conduit to a fuel outlet and a fluid conduit that extends from a fluid inlet through a fluid outlet conduit to a fluid outlet. The fuel outlet conduit and fuel outlet configured to produce a liquid fuel jet from the fuel outlet upon introduction of a pressurized liquid fuel into the fuel conduit. The fluid outlet conduit and fluid outlet are configured to produce a liquid fluid jet from the fluid outlet upon introduction of a pressurized liquid fluid into the fluid conduit, wherein the liquid fuel jet and the liquid fluid jet are configured to impact one another and produce a flow stream of atomized fuel.
摘要翻译： 公开了一种燃料喷射器喷嘴。 喷嘴包括具有燃料管道的喷嘴体，燃料导管从燃料入口通过燃料出口导管延伸到燃料出口，以及从流体入口通过流体出口导管延伸到流体出口的流体导管。 燃料出口导管和燃料出口构造成在将加压的液体燃料引入燃料管道中时从燃料出口产生液体燃料射流。 流体出口导管和流体出口构造成在将加压液体流体引入流体导管中时从流体出口产生液体流体射流，其中液体燃料射流和液体流体射流被配置为相互冲击并产生 雾化燃料流。
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