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1. 发明申请

US20140245740A1 COMBUSTOR APPARATUS IN A GAS TURBINE ENGINE 有权
标题翻译：燃气涡轮发动机中的燃烧器装置
公开(公告)号：US20140245740A1
公开(公告)日：2014-09-04
申请号：US13783857
申请日：2013-03-04
申请人： David J. Wiebe , Stephen A. Ramier , Robert H. Bartley , Daniel W. Garan , Erick J. Deane , Mark L. Adamson , Yadollah Naghian
发明人： David J. Wiebe , Stephen A. Ramier , Robert H. Bartley , Daniel W. Garan , Erick J. Deane , Mark L. Adamson , Yadollah Naghian
IPC分类号： F23R3/28
CPC分类号： F23R3/28 , F02C7/22 , F02C7/222 , F05D2300/50211 , F05D2300/50212 , F05D2300/506 , F16L13/007 , F16L15/006 , F16L19/061 , F16L25/0072 , F16L41/084 , F16L41/086 , F23K2301/20 , F23R3/283 , F23R3/286 , F23R3/34 , F23R2900/00005
摘要： A combustor apparatus defines a combustion zone where air and fuel are burned to create high temperature combustion products. The combustor apparatus includes an outer wall, coupling structure on the outer wall adjacent to a fuel inlet opening thereof, a fuel injection system, a fuel feed assembly, and a fitting member. The fuel injection system provides fuel to be burned in the combustion zone. The fuel supply structure includes a threaded inner surface formed from a first material. The fuel feed assembly includes a fuel feed pipe that extends through the fuel inlet opening in the outer wall and has an outlet portion formed from the first material and that is threadedly engaged with the fuel supply structure, and an inlet portion affixed to the outlet portion and formed from a second material. The fitting member secures the fuel feed assembly relative to the outer wall.
摘要翻译：燃烧器装置限定了燃烧区域，其中空气和燃料被燃烧以产生高温燃烧产物。燃烧器装置包括外壁，与其燃料入口相邻的外壁上的联接结构，燃料喷射系统，燃料供给组件和配件构件。燃料喷射系统提供在燃烧区域燃烧的燃料。燃料供给结构包括由第一材料形成的螺纹内表面。所述燃料供给组件包括燃料供给管，所述燃料供给管延伸穿过所述外壁中的所述燃料入口，并且具有由所述第一材料形成并与所述燃料供应结构螺纹接合的出口部分，以及固定到所述出口部分的入口部分并由第二材料形成。装配构件相对于外壁固定燃料供给组件。

2. 发明申请

US20120137691A1 Gas turbine assembly and method therefor 审中-公开
标题翻译：燃气轮机组件及其方法
公开(公告)号：US20120137691A1
公开(公告)日：2012-06-07
申请号：US12957476
申请日：2010-12-01
申请人： Andreas Bõttcher , Timothy A. Fox , Daniel W. Garan , Thomas Grieb , Jens Kleinfeld , Tobias Krieger , Stephen A. Ramier , David M. Ritland , Marcus Zurhorst
发明人： Andreas Bõttcher , Timothy A. Fox , Daniel W. Garan , Thomas Grieb , Jens Kleinfeld , Tobias Krieger , Stephen A. Ramier , David M. Ritland , Marcus Zurhorst
IPC分类号： F02C7/22 , B23P11/00
CPC分类号： F02C7/20 , F05D2260/94 , F05D2260/941 , F23R3/283 , F23R3/286 , F23R2900/00005 , F23R2900/00012 , Y10T29/49229
摘要： An assembly for a gas turbine is presented. The assembly includes a gas supply pipe passing through a bore in a flange of the gas turbine for supplying gas to a combustion chamber of the gas turbine and a sleeve surrounding the gas supply pipe, having a first end and a second end, wherein the first end is sealingly coupled to the gas supply pipe, and wherein the sleeve is adapted to be sealingly coupled to the flange at the second end such that the sleeve extends along a thickness of the flange.
摘要翻译：提出了一种燃气轮机组件。组件包括通过燃气轮机的凸缘中的孔的气体供应管，用于将气体供应到燃气轮机的燃烧室，以及围绕气体供应管的套管，其具有第一端和第二端，其中第一端部密封地联接到气体供应管，并且其中套筒适于在第二端处密封地联接到凸缘，使得套筒沿着凸缘的厚度延伸。

3. 发明申请

US20120047900A1 Burner Assembly 有权
标题翻译：燃烧器装配
公开(公告)号：US20120047900A1
公开(公告)日：2012-03-01
申请号：US13255559
申请日：2010-02-23
申请人： Andreas Böttcher , Tiimothy A. Fox , Thomas Grieb , Birgit Grüger , Tobias Krieger , Stephen A. Ramier , Christin Schlensog , Holger Streb
发明人： Andreas Böttcher , Tiimothy A. Fox , Thomas Grieb , Birgit Grüger , Tobias Krieger , Stephen A. Ramier , Christin Schlensog , Holger Streb
IPC分类号： F23R3/28
CPC分类号： F02C7/222 , F23D2213/00 , F23R3/28 , F23R3/36
摘要： A burner assembly is provided. The burner assembly includes a support housing with a supply manifold, the supply manifold includes a fuel passage system, and fuel nozzles extending from the supply manifold and being supplied with fuel through the fuel passage system of the supply manifold. The supply manifold is sandwiched using at least two subparts.
摘要翻译：提供燃烧器组件。燃烧器组件包括具有供应歧管的支撑壳体，供应歧管包括燃料通道系统，以及从供应歧管延伸并通过供应歧管的燃料通道系统供应燃料的燃料喷嘴。使用至少两个子部件夹持供给歧管。

4. 发明授权

US08955328B2 Burner arrangement 有权
标题翻译：燃烧器安排
公开(公告)号：US08955328B2
公开(公告)日：2015-02-17
申请号：US13029246
申请日：2011-02-17
申请人： Andreas Böttcher , Timothy A. Fox , Thomas Grieb , Tobias Krieger , Stephen A. Ramier
发明人： Andreas Böttcher , Timothy A. Fox , Thomas Grieb , Tobias Krieger , Stephen A. Ramier
IPC分类号： F02C1/00 , F02C7/20 , F23R3/28 , F23D23/00
CPC分类号： F23R3/283 , F23C2900/07021 , F23D23/00 , F23R2900/00018
摘要： A burner arrangement is provided. The burner arrangement includes a support and at least two fuel nozzles attached to the support in the direction of flow, with each fuel nozzle including a support-side section which includes a contact surface on the support side with which it rests on a supporting surface of the support, with at least two fuel nozzle tips embodied in one piece extending out from the support-side section in the direction of flow and the support-side contact surface including at least two extension parts projecting in the direction of the support, with the extension parts each embodying a channel through which fuel is fed in each case to the fuel nozzle tips through passages which are arranged in the support-side contact surface of the support-side section.
摘要翻译：提供燃烧器装置。燃烧器装置包括支撑件和沿流动方向附接到支撑件的至少两个燃料喷嘴，每个燃料喷嘴包括支撑侧部分，该支撑侧部分包括在支撑侧上的接触表面，支撑侧支撑在支撑面的支撑表面上所述支撑件具有至少两个燃料喷嘴尖端，所述至少两个燃料喷嘴尖端沿着流动方向从所述支撑侧部分延伸出一体，并且所述支撑侧接触表面包括至少两个在所述支撑件的方向上突出的延伸部分，延伸部分各自包括通道，通过该通道将燃料在每种情况下通过布置在支撑侧部分的支撑侧接触表面中的通道供应到燃料喷嘴尖端。

5. 发明授权

US08516820B2 Integral flow sleeve and fuel injector assembly 有权
标题翻译：一体式流动套管和燃油喷射器总成
公开(公告)号：US08516820B2
公开(公告)日：2013-08-27
申请号：US12180637
申请日：2008-07-28
申请人： Stephen A. Ramier , William R. Ryan
发明人： Stephen A. Ramier , William R. Ryan
IPC分类号： F02C7/22
CPC分类号： F23R3/286
摘要： A fuel injector assembly for use in a turbine engine having a combustion section and a turbine section downstream from the combustion section. The fuel injector assembly includes a flow sleeve defining a pre-mixing passage of the combustion section and including a sleeve wall having a forward end proximate to a cover plate of the combustion section and an opposed aft end. An annular cavity in fluid communication with a source of fuel is formed in the sleeve wall adjacent the aft end. A fuel dispensing structure is associated with the cavity and includes at least one fuel distribution aperture for distributing fuel from the cavity to the pre-mixing passage.
摘要翻译：一种用于涡轮发动机的燃料喷射器组件，其具有燃烧部分和在燃烧部分下游的涡轮部分。燃料喷射器组件包括流动套筒，其限定燃烧部分的预混合通道，并且包括套管壁，其具有靠近燃烧部分的盖板的前端和相对的后端。在与后端相邻的套筒壁中形成与燃料源流体连通的环形空腔。燃料分配结构与空腔相关联并且包括用于将燃料从腔体分配到预混合通道的至少一个燃料分配孔。

6. 发明授权

US09488105B2 Gas turbine assembly and method therefor 有权
标题翻译：燃气轮机组件及其方法
公开(公告)号：US09488105B2
公开(公告)日：2016-11-08
申请号：US13885710
申请日：2011-11-30
申请人： Andreas Böttcher , Timothy A. Fox , Daniel W. Garan , Thomas Grieb , Jens Kleinfeld , Tobias Krieger , Stephen A. Ramier , David M. Ritland , Marcus Zurhorst
发明人： Andreas Böttcher , Timothy A. Fox , Daniel W. Garan , Thomas Grieb , Jens Kleinfeld , Tobias Krieger , Stephen A. Ramier , David M. Ritland , Marcus Zurhorst
IPC分类号： F02C7/22 , F23R3/28 , F02C7/20
CPC分类号： F02C7/20 , F23R3/283 , F23R3/286 , F23R2900/00005 , F23R2900/00012 , F23R2900/00017 , Y10T29/49229
摘要： An assembly for a gas turbine is presented. The assembly includes a gas supply pipe passing through a bore in a flange of the gas turbine for supplying gas to a combustion chamber of the gas turbine and a sleeve surrounding the gas supply pipe, having a first end and a second end, wherein the first end is sealingly coupled to the gas supply pipe, and wherein the sleeve is adapted to be sealingly coupled to the flange at the second end such that the sleeve extends along a thickness of the flange.
摘要翻译：提出了一种燃气轮机组件。组件包括通过燃气轮机的凸缘中的孔的气体供应管，用于将气体供应到燃气轮机的燃烧室，以及围绕气体供应管的套管，其具有第一端和第二端，其中第一端部密封地联接到气体供应管，并且其中套筒适于在第二端处密封地联接到凸缘，使得套筒沿着凸缘的厚度延伸。

7. 发明授权

US09322558B2 Combustor apparatus in a gas turbine engine 有权
标题翻译：燃气涡轮发动机中的燃烧器装置
公开(公告)号：US09322558B2
公开(公告)日：2016-04-26
申请号：US13928476
申请日：2013-06-27
申请人： Stephen A. Ramier , David J. Wiebe , Lawrence P. Budnick , Mark L. Adamson , Daniel W. Garan , Robert H. Bartley , Yadollah Naghian
发明人： Stephen A. Ramier , David J. Wiebe , Lawrence P. Budnick , Mark L. Adamson , Daniel W. Garan , Robert H. Bartley , Yadollah Naghian
IPC分类号： F23R3/60 , F23R3/28 , F23R3/54 , F16L19/06 , F23R3/34
CPC分类号： F23R3/283 , F16L19/061 , F23R3/286 , F23R3/34 , F23R3/346 , F23R3/54 , F23R3/60
摘要： A combustor apparatus defining a combustion zone where air and fuel are burned to create high temperature combustion products. The combustor apparatus comprises an outer wall including a fuel inlet opening for receiving a fuel feed pipe. A coupling assembly is engaged with the fuel feed pipe at the fuel inlet opening to attach the fuel feed pipe to the outer wall. A fuel injection system is located in the interior volume of the outer wall and comprises fuel supply structure including a fuel feed block having a fuel intake passage aligned with the outlet portion of the fuel feed pipe. A coupling fastener is engaged against an exterior outer face of the fuel feed block to create a sealed coupling for containing fuel passing from the fuel feed pipe into the fuel feed block, and to secure the fuel feed block relative to the coupling assembly.
摘要翻译：一种限定燃烧区域的燃烧器装置，其中燃烧空气和燃料以产生高温燃烧产物。燃烧器装置包括外壁，其包括用于接收燃料供给管的燃料入口。联接组件在燃料入口处与燃料供给管接合以将燃料供给管附接到外壁。燃料喷射系统位于外壁的内部容积中，并且包括燃料供给结构，其包括具有与燃料供给管的出口部分对准的燃料进入通道的燃料供给块。联接紧固件抵靠燃料供给块的外部外表面接合以产生密封联接件，用于容纳从燃料供给管道进入燃料供给块的燃料，并且相对于联接组件固定燃料供给块。

8. 发明申请

US20150159878A1 COMBUSTION SYSTEM FOR A GAS TURBINE ENGINE 审中-公开
标题翻译：燃气涡轮发动机燃烧系统
公开(公告)号：US20150159878A1
公开(公告)日：2015-06-11
申请号：US14102578
申请日：2013-12-11
申请人： Kai-Uwe Schildmacher , Danning You , Ulrich Wörz , Stephen A. Ramier
发明人： Kai-Uwe Schildmacher , Danning You , Ulrich Wörz , Stephen A. Ramier
IPC分类号： F23R3/58
CPC分类号： F23R3/58 , F23R3/06 , F23R3/16 , F23R2900/00014 , F23R2900/03045
摘要： A combustor for a gas turbine engine includes a pilot fuel injector and a plurality of circumferentially located main injectors for injecting fuel and air into a combustion chamber defined by a liner wall of a combustor basket. A combustion zone is located in the combustion chamber where the fuel and air are ignited to produce hot combustion gases. A plurality of vortex generators are located in circumferentially spaced relation on the liner wall and comprise structures extending radially inward into the combustion chamber to create vortices at predetermined circumferential locations downstream from where the fuel and air are ignited to effect a reduction in emissions of the combustion gases.
摘要翻译：用于燃气涡轮发动机的燃烧器包括引燃燃料喷射器和用于将燃料和空气喷射到由燃烧器筐的衬套壁限定的燃烧室中的多个周向定位的主喷射器。燃烧区位于燃烧室中，其中燃料和空气被点燃以产生热燃烧气体。多个涡流发生器位于衬套壁上周向间隔开的关系上，并且包括径向向内延伸进入燃烧室的结构，以在燃料和空气被点燃的燃料和空气的下游的预定圆周位置处产生涡流，以实现燃烧排放的减少气体。

9. 发明申请

US20140130502A1 GAS TURBINE ASSEMBLY AND METHOD THEREFOR 有权
标题翻译：气体涡轮组件及其方法
公开(公告)号：US20140130502A1
公开(公告)日：2014-05-15
申请号：US13885710
申请日：2011-11-30
申请人： Andreas Böttcher , Timothy A. Fox , Daniel W. Garan , Thomas Grieb , Jens Kleinfeld , Tobias Krieger , Stephen A. Ramier , David M. Ritland , Marcus Zurhorst
发明人： Andreas Böttcher , Timothy A. Fox , Daniel W. Garan , Thomas Grieb , Jens Kleinfeld , Tobias Krieger , Stephen A. Ramier , David M. Ritland , Marcus Zurhorst
IPC分类号： F23R3/28 , F02C7/20
CPC分类号： F02C7/20 , F23R3/283 , F23R3/286 , F23R2900/00005 , F23R2900/00012 , F23R2900/00017 , Y10T29/49229
摘要： An assembly for a gas turbine is presented. The assembly includes a gas supply pipe passing through a bore in a flange of the gas turbine for supplying gas to a combustion chamber of the gas turbine and a sleeve surrounding the gas supply pipe, having a first end and a second end, wherein the first end is sealingly coupled to the gas supply pipe, and wherein the sleeve is adapted to be sealingly coupled to the flange at the second end such that the sleeve extends along a thickness of the flange.
摘要翻译：提出了一种燃气轮机组件。组件包括通过燃气轮机的凸缘中的孔的气体供应管，用于将气体供应到燃气轮机的燃烧室，以及围绕气体供应管的套管，其具有第一端和第二端，其中第一端部密封地联接到气体供应管，并且其中套筒适于在第二端处密封地联接到凸缘，使得套筒沿着凸缘的厚度延伸。

10. 发明申请

US20150000283A1 COMBUSTOR APPARATUS IN A GAS TURBINE ENGINE 有权
标题翻译：燃气涡轮发动机中的燃烧器装置
公开(公告)号：US20150000283A1
公开(公告)日：2015-01-01
申请号：US13928476
申请日：2013-06-27
申请人： Stephen A. Ramier , David J. Wiebe , Lawrence P. Budnick , Mark L. Adamson , Daniel W. Garan , Robert H. Bartley , Yadollah Naghian
发明人： Stephen A. Ramier , David J. Wiebe , Lawrence P. Budnick , Mark L. Adamson , Daniel W. Garan , Robert H. Bartley , Yadollah Naghian
IPC分类号： F23R3/28
CPC分类号： F23R3/283 , F16L19/061 , F23R3/286 , F23R3/34 , F23R3/346 , F23R3/54 , F23R3/60
摘要： A combustor apparatus defining a combustion zone where air and fuel are burned to create high temperature combustion products. The combustor apparatus comprises an outer wall including a fuel inlet opening for receiving a fuel feed pipe. A coupling assembly is engaged with the fuel feed pipe at the fuel inlet opening to attach the fuel feed pipe to the outer wall. A fuel injection system is located in the interior volume of the outer wall and comprises fuel supply structure including a fuel feed block having a fuel intake passage aligned with the outlet portion of the fuel feed pipe. A coupling fastener is engaged against an exterior outer face of the fuel feed block to create a sealed coupling for containing fuel passing from the fuel feed pipe into the fuel feed block, and to secure the fuel feed block relative to the coupling assembly.
摘要翻译：一种限定燃烧区域的燃烧器装置，其中燃烧空气和燃料以产生高温燃烧产物。燃烧器装置包括外壁，其包括用于接收燃料供给管的燃料入口。联接组件在燃料入口处与燃料供给管接合以将燃料供给管附接到外壁。燃料喷射系统位于外壁的内部容积中，并且包括燃料供给结构，其包括具有与燃料供给管的出口部分对准的燃料进入通道的燃料供给块。联接紧固件抵靠燃料供给块的外部外表面接合以产生密封联接件，用于容纳从燃料供给管道进入燃料供给块的燃料，并且相对于联接组件固定燃料供给块。

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