-
11.发明申请GAS TURBINE COMBUSTION SYSTEM WITH RICH PREMIXED FUEL REFORMING AND METHODS OF USE THEREOF 审中-公开具有优先燃料燃料改造的燃气涡轮机燃烧系统及其使用方法公开(公告)号：US20110296844A1
公开(公告)日：2011-12-08
申请号：US12792037
申请日：2010-06-02
CPC分类号： F02C7/22
摘要： A gas turbine engine system, comprising a compressor, a combustor, and a turbine; a fuel system comprising one or more fuel circuits configured to provide fuel to the combustor; a non-catalytic fuel reformer in fluid communication with the one or more fuel circuits, wherein the non-catalytic fuel reformer is configured to receive an oxidant and a fraction of the fuel in the one or more fuel circuits in a fuel-rich ratio and reform the fraction of the fuel to produce a reformate; and a control system configured to regulate at least one of fuel flow and oxidizer flow to the non-catalytic fuel reformer to control a Modified Wobbe Index of the fuel entering the combustor.
摘要翻译： 一种燃气涡轮发动机系统，包括压缩机，燃烧器和涡轮机; 燃料系统，包括被配置为向燃烧器提供燃料的一个或多个燃料回路; 与所述一个或多个燃料回路流体连通的非催化燃料重整器，其中所述非催化燃料重整器构造成在所述一个或多个燃料回路中以富燃比接收氧化剂和一部分燃料， 改革燃料的分数以产生重整产品; 以及控制系统，其被配置为将至少一个燃料流和氧化剂流调节到非催化燃料重整器以控制进入燃烧器的燃料的改性沃泊指数。
-
公开(公告)号：US07966822B2
公开(公告)日：2011-06-28
申请号：US11160596
申请日：2005-06-30
IPC分类号： F02C1/00
CPC分类号： F02C3/145
摘要： A gas turbine combustion system for burning air and fuel into exhaust gases. The gas turbine combustion system may include a combustor, a turbine nozzle integral with the combustor for providing the air to the combustor, and a fuel injector for providing the fuel to the combustor. The turbine nozzle and the fuel injector are positioned within the combustor such that a mixture of the air and the fuel flows in a first direction and the exhaust gases flow in a second direction.
摘要翻译： 一种用于将空气和燃料燃烧成废气的燃气轮机燃烧系统。 燃气轮机燃烧系统可以包括燃烧器，与燃烧器成一体的涡轮喷嘴，用于向燃烧器提供空气，以及用于将燃料提供给燃烧器的燃料喷射器。 涡轮喷嘴和燃料喷射器定位在燃烧器内，使得空气和燃料的混合物沿第一方向流动并且废气沿第二方向流动。
-
公开(公告)号：US20100239418A1
公开(公告)日：2010-09-23
申请号：US12407525
申请日：2009-03-19
IPC分类号： F01D9/00
CPC分类号： F01D9/04 , F02C3/14 , F04D29/547 , F05D2240/12 , F05D2250/52 , F23R3/60
摘要： A diffuser for a turbine engine, including an annular casing to seal compressor discharge air and struts attached to the casing to delimit an annular array of intra-strut regions, is provided and includes a ring portion, including a ring shaped annular body with a forward face disposed on a forward side thereof, the ring portion being supportable by one or more of the struts, and a splitter portion, including a ring shaped annular body with an aft face disposed on an aft side thereof to mate with the forward face of the ring portion body, the splitter portion further including a lead edge, on a forward side of the splitter portion body, which is extendable into a flow path of the compressor discharge air to split the flow path into secondary flow paths defined radially outside of and inside of the splitter portion body.
摘要翻译： 一种用于涡轮发动机的扩散器，包括用于密封压缩机排出空气的环形壳体和附接到壳体的支柱以限定支柱内区域的环形阵列，并且包括环部分，其包括环形环形体，其具有向前 所述环形部分可由一个或多个所述支柱支撑，所述分隔部分包括环形环形体，所述环形环体具有设置在其后侧上的后表面， 环形部分主体，分离器部分还包括引导边缘，位于分离器部分主体的前侧，其可延伸到压缩机排出空气的流动路径中，以将流动路径分成径向地在外部和内部限定的二次流动路径 的分离器部分主体。
-
公开(公告)号：US20130061598A1
公开(公告)日：2013-03-14
申请号：US13232191
申请日：2011-09-14
CPC分类号： F23R3/34 , F02C3/14 , F05D2270/082 , F23R3/286 , F23R3/42
摘要： A system for conditioning a working fluid in a combustor includes a primary combustion chamber, a liner circumferentially surrounding the primary combustion chamber, and a primary nozzle in fluid communication with the primary combustion chamber. A secondary combustion chamber located outside of the primary combustion chamber includes a shroud that defines a fluid passage, a secondary nozzle, and means for igniting fuel in the secondary combustion chamber. A method for conditioning a working fluid in a combustor includes flowing the working fluid through a primary combustion chamber and flowing at least a portion of the working fluid through a secondary combustion chamber located outside of the primary combustion chamber. The method further includes flowing a fuel through the secondary combustion chamber, combusting the fuel, and flowing the combustion gases from the secondary combustion chamber into the primary combustion chamber.
摘要翻译： 用于调节燃烧器中的工作流体的系统包括主燃烧室，周向围绕主燃烧室的衬套和与主燃烧室流体连通的主喷嘴。 位于主燃烧室外的二次燃烧室包括限定流体通道的护罩，二次喷嘴和用于点燃二次燃烧室中的燃料的装置。 用于调节燃烧器中的工作流体的方法包括使工作流体流过初级燃烧室并使至少一部分工作流体通过位于主燃烧室外部的二级燃烧室。 该方法还包括使燃料流过二次燃烧室，燃烧燃料，并使燃烧气体从二级燃烧室流入主燃烧室。
-
公开(公告)号：US08220246B2
公开(公告)日：2012-07-17
申请号：US12563599
申请日：2009-09-21
IPC分类号： F02C3/00
CPC分类号： F23R3/48 , F23R2900/03044
摘要： A crossfire tube assembly is configured for connecting adjacent combustion cans in a gas turbine, and includes a first tube segment having a first end and an opposite female end. A second tube segment has a first end and an opposite male end fitted concentrically within the female end with an overlap region between the female and male ends. Each of the first ends of the tube segments is configured for securing to a liner of a respective combustion can. Oppositely oriented first and second impingement sleeves extend from the female end of the first tube segment to the respective first ends of the tube segments. Combustion cooling air is directed through metering holes in the impingement sleeves and flows axially along concentric cavities defined between the impingement sleeves and the first and second tube segments. The combustion cooling air vents from the cavities into an axial combustion air flow stream between the respective combustion can liners and sleeves.
摘要翻译： 交火管组件构造成用于连接燃气轮机中的相邻燃烧罐，并且包括具有第一端和相对的母端的第一管段。 第二管段具有第一端和相对的阳端，同心地嵌入阴端内，在阴端和阳端之间具有重叠区域。 管段的每个第一端构造成用于固定到相应燃烧罐的衬套。 相对定向的第一和第二冲击套筒从第一管段的阴端延伸到管段的相应的第一端。 燃烧冷却空气被引导通过冲击套筒中的计量孔，并且沿冲击衬套和第一和第二管段之间限定的同心腔轴向流动。 燃烧的冷却空气从空腔排出到相应的燃烧罐衬套和套筒之间的轴向燃烧空气流。
-
公开(公告)号：US20120087784A1
公开(公告)日：2012-04-12
申请号：US12902699
申请日：2010-10-12
IPC分类号： F01D5/08
CPC分类号： F01D5/085 , F02C6/08 , F02C7/18 , F05D2260/14 , F05D2260/97
摘要： An inducer for a casing of a gas turbine system is disclosed. The inducer includes a plurality of orifices defined in the casing, the plurality of orifices disposed in an annular array about the casing, and a plurality of cartridges, each of the plurality of cartridges configured to mate with one of the plurality of orifices. Each of the plurality of cartridges includes an inlet and an outlet for flowing a cooling medium therethrough. The inducer further includes at least one flow modifier disposed in each of the plurality of cartridges for modifying the flow of the cooling medium through each of the plurality of cartridges. Each of the plurality of cartridges is independently removable from each of the plurality of orifices.
摘要翻译： 公开了一种用于燃气轮机系统壳体的导流器。 导流器包括限定在壳体中的多个孔，围绕壳体设置成环形阵列的多个孔和多个筒，多个筒中的每一个被配置为与多个孔中的一个孔配合。 多个盒中的每一个包括用于使冷却介质流过其的入口和出口。 导流器还包括设置在多个盒中的每一个中的至少一个流动改性剂，用于改变通过多个盒中的每一个的冷却介质的流动。 多个盒中的每一个可独立地从多个孔中的每一个排出。
-
公开(公告)号：US20110271688A1
公开(公告)日：2011-11-10
申请号：US12774822
申请日：2010-05-06
IPC分类号： F02C7/20
摘要： A transition piece support for a turbomachine includes one or more support arms extending across a diffuser flowpath to the transition piece. The one or more support arms include a streamwise surface and a crosswise surface. A streamwise extent of the streamwise surface is greater than a crosswise extent of the crosswise surface to reduce flow anomalies in a flow of fluid across the one or more support arms. A turbomachine includes a combustor, a diffuser, a transition piece operably connected to the combustor and a transition piece support including one or more support arms extending across a flow of fluid to the transition piece. The support arms include a streamwise surface and a crosswise surface. A streamwise extent of the streamwise surface is greater than a crosswise extent of the crosswise surface to reduce flow anomalies in a flow of fluid across the one or more support arms.
摘要翻译： 用于涡轮机的过渡件支撑件包括一个或多个支撑臂，跨越扩散器流动路径延伸到过渡件。 一个或多个支撑臂包括流动表面和横向表面。 流动表面的流动范围大于横向表面的横向范围，以减少穿过一个或多个支撑臂的流体流中的流量异常。 涡轮机包括燃烧器，扩散器，可操作地连接到燃烧器的过渡件和过渡件支撑件，该过渡件支撑件包括跨过流体流延伸到过渡件的一个或多个支撑臂。 支撑臂包括流动表面和横向表面。 流动表面的流动范围大于横向表面的横向范围，以减少穿过一个或多个支撑臂的流体流中的流量异常。
-
18.发明申请公开(公告)号：US20100236249A1
公开(公告)日：2010-09-23
申请号：US12408326
申请日：2009-03-20
IPC分类号： F02C1/00
摘要： A system and method for reintroducing gas turbine combustion bypass flow. The system may include a combustor body, wherein the combustor body includes a reaction zone for primary combustion of fuel and air, and a casing enclosing the combustor body and defining an annular passageway for carrying compressor discharge air into the combustor body at one end. The system further may include a reintroduction manifold for receiving combustor bypass air extracted from the compressor discharge air in the annular passageway, and one or more reintroduction slots in communication with the reintroduction manifold for injecting the combustor bypass air into the combustor body downstream of the reaction zone. The method may include extracting combustor bypass air from the annular passageway, transporting the combustor bypass air to a reintroduction manifold, and reintroducing the combustor bypass air into the combustor body through one or more reintroduction slots in communication with the reintroduction manifold.
摘要翻译： 一种用于重新引入燃气轮机燃烧旁路流的系统和方法。 该系统可以包括燃烧器主体，其中燃烧器主体包括用于燃料和空气的初级燃烧的反应区，以及包围燃烧器主体并且限定一个环形通道的壳体，该环形通道在一端承载压缩机排放空气进入燃烧器主体。 该系统还可以包括用于接收从环形通道中的压缩机排出空气抽出的燃烧器旁路空气的再引入歧管，以及与再引入歧管连通的一个或多个再引入槽，用于将燃烧器旁路空气喷射到反应下游的燃烧器体中 区。 该方法可以包括从环形通道提取燃烧器旁路空气，将燃烧器旁路空气输送到再引入歧管，以及通过与再引入歧管连通的一个或多个再引入槽将燃烧器旁路空气重新引入燃烧器主体。
-
19.发明授权公开(公告)号：US06993916B2
公开(公告)日：2006-02-07
申请号：US10862427
申请日：2004-06-08
CPC分类号： F23R3/14 , F23C2900/07001 , F23R3/286
摘要： A hybrid structure that combines characteristics of the DACRS and Swozzle burners to provide the high mixing ability of an axial flowing counter rotating vane swirler with good dynamic flame stability characteristics of a bluff center body.
摘要翻译： 一种混合结构，结合了DACRS和Swozzle燃烧器的特性，提供了具有良好动态火焰稳定性的非流线型中心体的轴流式逆向旋转叶片旋流器的高混合能力。
-
公开(公告)号：US08529195B2
公开(公告)日：2013-09-10
申请号：US12902699
申请日：2010-10-12
IPC分类号： F01D5/08
CPC分类号： F01D5/085 , F02C6/08 , F02C7/18 , F05D2260/14 , F05D2260/97
摘要： An inducer for a casing of a gas turbine system is disclosed. The inducer includes a plurality of orifices defined in the casing, the plurality of orifices disposed in an annular array about the casing, and a plurality of cartridges, each of the plurality of cartridges configured to mate with one of the plurality of orifices. Each of the plurality of cartridges includes an inlet and an outlet for flowing a cooling medium therethrough. The inducer further includes at least one flow modifier disposed in each of the plurality of cartridges for modifying the flow of the cooling medium through each of the plurality of cartridges. Each of the plurality of cartridges is independently removable from each of the plurality of orifices.
摘要翻译： 公开了一种用于燃气轮机系统壳体的导流器。 导流器包括限定在壳体中的多个孔，围绕壳体设置成环形阵列的多个孔和多个筒，多个筒中的每一个被配置为与多个孔中的一个孔配合。 多个盒中的每一个包括用于使冷却介质流过其的入口和出口。 导流器还包括设置在多个盒中的每一个中的至少一个流动改性剂，用于改变通过多个盒中的每一个的冷却介质的流动。 多个盒中的每一个可独立地从多个孔中的每一个排出。
-
-
-
-
-
-
-
-
-
搜索结果
37 条记录 (耗时 0.022 秒)
