-
公开(公告)号：US08701383B2
公开(公告)日：2014-04-22
申请号：US12349831
申请日：2009-01-07
申请人： Krishna Kumar Venkataraman , Roy Marshall Washam , Hasan Karim , Jason Charles Terry , Lewis Berkley Davis, Jr.
发明人： Krishna Kumar Venkataraman , Roy Marshall Washam , Hasan Karim , Jason Charles Terry , Lewis Berkley Davis, Jr.
CPC分类号： F02C7/22 , F23N2041/20 , F23R3/34
摘要： A gas turbine engine is provided and includes a late lean injection (LLI) compatible combustor having a first interior in which a first fuel supplied thereto by a fuel circuit is combustible, a turbine, a transition zone, including a second interior in which a second fuel supplied thereto by the fuel circuit and the products of the combustion of the first fuel are combustible, the transition zone being disposed to fluidly couple the combustor and the turbine to one another, and a plurality of fuel injectors, which are structurally supported by the transition zone and coupled to the fuel circuit, and which are configured to supply the second fuel to the second interior in any one of a single axial stage, multiple axial stages, a single axial circumferential stage and multiple axial circumferential stages.
摘要翻译： 提供了一种燃气涡轮发动机，并且包括具有第一内部的后倾稀注射（LLI）兼容的燃烧器，其中由燃料回路供应到其中的第一燃料可燃，涡轮机，过渡区域，其中第二内部 由燃料回路供应的燃料和第一燃料的燃烧产物是可燃的，过渡区设置成使燃烧器和涡轮彼此流体连接，并且多个燃料喷射器在结构上由 过渡区并且连接到燃料回路，并且其构造成在单个轴向级，多个轴向级，单个轴向圆周级和多个轴向圆周级中的任一个中将第二燃料供应到第二内部。
-
公开(公告)号：US20100170216A1
公开(公告)日：2010-07-08
申请号：US12349831
申请日：2009-01-07
申请人： Krishna Kumar Venkataraman , Roy Marshall Washam , Hasan Karim , Jason Charles Terry , Lewis Berkley Davis, JR.
发明人： Krishna Kumar Venkataraman , Roy Marshall Washam , Hasan Karim , Jason Charles Terry , Lewis Berkley Davis, JR.
IPC分类号： F02C7/22
CPC分类号： F02C7/22 , F23N2041/20 , F23R3/34
摘要： A gas turbine engine is provided and includes a late lean injection (LLI) compatible combustor having a first interior in which a first fuel supplied thereto by a fuel circuit is combustible, a turbine, a transition zone, including a second interior in which a second fuel supplied thereto by the fuel circuit and the products of the combustion of the first fuel are combustible, the transition zone being disposed to fluidly couple the combustor and the turbine to one another, and a plurality of fuel injectors, which are structurally supported by the transition zone and coupled to the fuel circuit, and which are configured to supply the second fuel to the second interior in any one of a single axial stage, multiple axial stages, a single axial circumferential stage and multiple axial circumferential stages.
摘要翻译： 提供了一种燃气涡轮发动机，并且包括具有第一内部的后倾稀注射（LLI）兼容的燃烧器，其中由燃料回路供应到其中的第一燃料可燃，涡轮机，过渡区域，其中第二内部 由燃料回路供应的燃料和第一燃料的燃烧产物是可燃的，过渡区设置成使燃烧器和涡轮彼此流体连接，并且多个燃料喷射器在结构上由 过渡区并且连接到燃料回路，并且其构造成在单个轴向级，多个轴向级，单个轴向圆周级和多个轴向圆周级中的任一个中将第二燃料供应到第二内部。
-
公开(公告)号：US08707707B2
公开(公告)日：2014-04-29
申请号：US12349744
申请日：2009-01-07
摘要： A gas turbine engine is provided and includes a combustor having a first interior in which a first fuel supplied thereto is combustible, a turbine, including rotating turbine blades, into which products of at least the combustion of the first fuel are receivable to power a rotation of the turbine blades, a transition zone, including a second interior in which a second fuel supplied thereto and the products of the combustion of the first fuel are combustible, the transition zone being disposed to fluidly couple the combustor and the turbine to one another, and a plurality of fuel injectors, which are supported by the transition zone and coupled to a fuel circuit, and which are configured to supply the second fuel to the second interior in any one or more of a single axial stage, multiple axial stages, a single axial circumferential stage and multiple axial circumferential stages.
摘要翻译： 提供燃气涡轮发动机并且包括具有第一内部的燃烧器，其中供应到其中的第一燃料可燃，包括旋转的涡轮机叶片的涡轮机，至少可燃第一燃料的燃烧的产物可供给其中， 涡轮机叶片的过渡区域，包括第二内部，其中供应到其中的第二燃料和第一燃料的燃烧产物是可燃的，所述过渡区域设置成将燃烧器和涡轮机彼此流体地联接， 以及多个燃料喷射器，其由过渡区域支撑并且联接到燃料回路，并且构造成在单个轴向级，多个轴向级中的任何一个或多个中将第二燃料供应到第二内部， 单轴向圆周阶段和多个轴向周向阶段。
-
公开(公告)号：US20100170254A1
公开(公告)日：2010-07-08
申请号：US12349744
申请日：2009-01-07
IPC分类号： F02C7/22
摘要： A gas turbine engine is provided and includes a combustor having a first interior in which a first fuel supplied thereto is combustible, a turbine, including rotating turbine blades, into which products of at least the combustion of the first fuel are receivable to power a rotation of the turbine blades, a transition zone, including a second interior in which a second fuel supplied thereto and the products of the combustion of the first fuel are combustible, the transition zone being disposed to fluidly couple the combustor and the turbine to one another, and a plurality of fuel injectors, which are supported by the transition zone and coupled to a fuel circuit, and which are configured to supply the second fuel to the second interior in any one or more of a single axial stage, multiple axial stages, a single axial circumferential stage and multiple axial circumferential stages.
摘要翻译： 提供燃气涡轮发动机并且包括具有第一内部的燃烧器，其中供应到其中的第一燃料可燃，包括旋转的涡轮机叶片的涡轮机，至少可燃第一燃料的燃烧的产物可供给其中， 涡轮机叶片的过渡区域，包括第二内部，其中供应到其中的第二燃料和第一燃料的燃烧产物是可燃的，所述过渡区域设置成将燃烧器和涡轮机彼此流体地联接， 以及多个燃料喷射器，其由过渡区域支撑并且联接到燃料回路，并且构造成在单个轴向级，多个轴向级中的任何一个或多个中将第二燃料供应到第二内部， 单轴向圆周阶段和多个轴向周向阶段。
-
5.发明授权公开(公告)号：US08931283B2
公开(公告)日：2015-01-13
申请号：US13010828
申请日：2011-01-21
CPC分类号： F02C3/20 , F02C7/22 , F23C2900/03002 , F23R3/28 , Y02T50/678
摘要： A reformer for use in a gas turbine engine specially configured to treat a supplemental fuel feed to the combustor that includes a reformer core containing a catalyst composition and an inlet flow channel for transporting the reformer fuel mixture, air and steam (either saturated or superheated) into a reformer core. An outlet flow channel transports the resulting reformate stream containing reformed and thermally cracked hydrocarbons and substantial amounts of hydrogen out of the reformer core for later combination with the main combustor feed. Because the catalytic partial oxidation reaction in the reformer is highly exothermic, the additional heat is transferred (and thermally integrated) using one or more heat exchange units for a first and/or second auxiliary gas turbine fuel stream that undergo thermal cracking and vaporization before combining with the reformate. The combined, hydrogen-enriched feed significantly improves combustor performance.
摘要翻译： 一种用于燃气涡轮发动机的改质器，其特别构造为处理燃烧器的补充燃料进料，其包括含有催化剂组合物的重整器芯和用于输送重整器燃料混合物的入口流动通道，空气和蒸汽（饱和或过热） 进入重组核心。 出口流动通道将得到的重整产物流输送到重整器芯中，以便与主燃烧器进料混合。 因为重整器中的催化部分氧化反应是高度放热的，所以使用一个或多个用于在组合之前经受热裂解和蒸发的第一和/或第二辅助燃气轮机燃料流的热交换单元转移（并热集成）附加的热量 与重组。 组合的富氢进料显着提高了燃烧室性能。
-
公开(公告)号：US08683804B2
公开(公告)日：2014-04-01
申请号：US12618636
申请日：2009-11-13
申请人： Gregory Allen Boardman , David Martin Johnson , Ronald James Chila , Nishant Govindbhai Parsania , Hasan Karim , Joseph Citeno
发明人： Gregory Allen Boardman , David Martin Johnson , Ronald James Chila , Nishant Govindbhai Parsania , Hasan Karim , Joseph Citeno
摘要： In one embodiment, a system includes a fuel nozzle that includes a fuel injector that includes a fuel port and a premixer tube. The premixer tube includes a wall disposed about a central passage, multiple air ports extending through the wall into the central passage, and a catalytic region. The catalytic region includes a catalyst, disposed inside the wall along the central passage, configured to increase a reaction of fuel and air.
摘要翻译： 在一个实施例中，系统包括燃料喷嘴，其包括燃料喷射器，燃料喷射器包括燃料口和预混合管。 预混合管包括围绕中心通道设置的壁，多个空气端口延伸穿过壁进入中心通道，以及催化区域。 催化区域包括沿着中心通道设置在壁内的催化剂，构造成增加燃料和空气的反应。
-
公开(公告)号：US08377156B2
公开(公告)日：2013-02-19
申请号：US13566545
申请日：2012-08-03
IPC分类号： C10J3/46
CPC分类号： C01B3/386 , B01J8/0278 , B01J2208/00176 , B01J2208/00221 , B01J2208/00371 , B01J2208/0053 , B01J2208/00849 , C01B2203/0261 , C01B2203/0877 , C01B2203/0883 , C01B2203/84 , C10J3/466 , C10J2200/09 , C10J2300/0959 , C10J2300/0989 , C10J2300/1861 , C10J2300/1884 , F23C2900/03002
摘要： The present subject matter is directed to a method for operating a fuel reformer. The method may generally include directing a fluid stream around a reactor assembly of the fuel reformer to cool the reactor assembly, and mixing a heated reformate stream produced by the reactor assembly with the fluid stream to cool the heated reformate stream.
摘要翻译： 本发明涉及一种操作燃料重整器的方法。 该方法通常可以包括引导燃料重整器的反应器组件周围的流体流以冷却反应器组件，以及将由反应器组件产生的加热的重整产物流与流体流混合以冷却加热的重整产物流。
-
公开(公告)号：US20090301054A1
公开(公告)日：2009-12-10
申请号：US12133065
申请日：2008-06-04
摘要： While the invention has been described in connection with what is presently considered to be the most practical and preferred embodiment, it is to be understood that the invention is not to be limited to the disclosed embodiment, but on the contrary, is intended to cover various modifications and equivalent arrangements included within the spirit and scope of the appended claims.
摘要翻译： 虽然已经结合目前被认为是最实际和优选的实施例描述了本发明，但是应当理解，本发明不限于所公开的实施例，而是相反，旨在覆盖各种 修改和等同布置包括在所附权利要求的精神和范围内。
-
9.发明申请SYSTEMS AND METHODS OF OPERATING A CATALYTIC REFORMING ASSEMBLY FOR USE WITH A GAS TURBINE ENGINE SYSTEM 有权使用燃气涡轮发动机系统使用催化重整装置的系统和方法公开(公告)号：US20110197566A1
公开(公告)日：2011-08-18
申请号：US12704720
申请日：2010-02-12
申请人： Chetan Babu Velkur , Hasan Karim
发明人： Chetan Babu Velkur , Hasan Karim
CPC分类号： F23R3/40 , B01J8/0221 , B01J8/0278 , B01J8/0285 , B01J19/002 , B01J2208/00061 , B01J2208/00548 , B01J2208/00902 , B01J2219/002 , B01J2219/00213 , B01J2219/00236 , B01J2219/00268 , B01J2219/182 , C01B3/386 , C01B2203/0261 , C01B2203/1619 , C01B2203/1676 , C01B2203/84 , F02C3/205 , F23C2900/03002 , F23N5/242 , F23N2037/12
摘要： A method for operating a catalytic reforming assembly. The method includes injecting a quantity of oxidizer gas and a quantity of combustion gas into a reformer to form a mixture. The mixture is channeled across a catalyst bed to form a reformate gas stream. A temperature of the catalyst bed is measured using at least one temperature sensor. A level of the oxidizer gas in the reformate stream is measured using at least one oxidizer gas sensor. A health of the catalyst bed is determined based on at least one of a catalyst bed temperature measurement and an oxidizer gas level.
摘要翻译： 一种操作催化重整组件的方法。 该方法包括将一定数量的氧化剂气体和一定量的燃烧气体注入重整器以形成混合物。 将混合物引导穿过催化剂床以形成重整产品气流。 使用至少一个温度传感器测量催化剂床的温度。 使用至少一种氧化剂气体传感器测量重整产品流中的氧化剂气体的水平。 基于催化剂床温度测量和氧化剂气体水平中的至少一个来确定催化剂床的健康。
-
10.发明申请公开(公告)号：US20060191269A1
公开(公告)日：2006-08-31
申请号：US11361626
申请日：2006-02-24
申请人： Lance Smith , Hasan Karim , Shahrokh Etemad , William Pfefferle
发明人： Lance Smith , Hasan Karim , Shahrokh Etemad , William Pfefferle
IPC分类号： F23R3/30
CPC分类号： F23R3/40 , F23C13/06 , F23D2209/20 , F23R3/343
摘要： A method is provided for expanding a non-swirling gaseous flow exiting a conduit into a larger chamber. The flow conduit exhibits a curved flare exiting into the chamber and a gaseous flow is passed through the conduit along with a separate pilot flow centrally located within the conduit. The pilot flow is expanded by heating thus forcing the gaseous flow outward along the flared exit.
摘要翻译： 提供一种用于将离开管道的非漩涡气流膨胀到较大室中的方法。 流动管道呈现出离开室的弯曲的火炬，气流与导管内中心的单独的先导流一起通过导管。 先导流通过加热膨胀，从而迫使气流沿着扩口出口向外。
-
-
-
-
-
-
-
-
-
搜索结果
35 条记录 (耗时 0.027 秒)