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1. 发明授权

US08590315B2 Extruded fluid manifold for gas turbomachine combustor casing 失效
标题翻译：用于气体涡轮机燃烧器套管的挤出流体歧管
公开(公告)号：US08590315B2
公开(公告)日：2013-11-26
申请号：US12791341
申请日：2010-06-01
申请人： Brandon Taylor Overby , Jason Allen Seale , Ibrahim Ucok
发明人： Brandon Taylor Overby , Jason Allen Seale , Ibrahim Ucok
IPC分类号： F02C1/00
CPC分类号： F23R3/002
摘要： A turbomachine includes a compressor, a turbine, and a combustor operatively coupled to the compressor and the turbine. The combustor includes a combustor casing having a flange, an outer surface and an inner surface that defines an internal passage. The combustor casing includes an extruded fluid manifold mounted to the outer surface. The extruded fluid manifold includes first and second walls integrally formed with a third, connecting, wall. The first wall includes a first mounting element and the second wall includes a second mounting element. The first mounting element extends axially along the combustor casing away from the first wall and the second mounting element extends axially along the combustor casing away from the second wall and the first mounting element. The extruded fluid manifold is joined to the outer surface of the combustor casing through the first and second mounting elements.
摘要翻译：涡轮机包括压缩机，涡轮机和可操作地联接到压缩机和涡轮机的燃烧器。燃烧器包括具有凸缘，外表面和限定内部通道的内表面的燃烧器壳体。燃烧器壳体包括安装到外表面的挤压流体歧管。挤压流体歧管包括与第三连接壁一体形成的第一和第二壁。第一壁包括第一安装元件，第二壁包括第二安装元件。第一安装元件沿着燃烧器壳体轴向延伸远离第一壁并且第二安装元件沿着燃烧器壳体轴向延伸远离第二壁和第一安装元件。挤压流体歧管通过第一和第二安装元件连接到燃烧器壳体的外表面。

2. 发明申请

US20110289926A1 EXTRUDED FLUID MANIFOLD FOR GAS TURBOMACHINE COMBUSTOR CASING 失效
标题翻译：用于气体涡轮搅拌机的挤出流体歧管
公开(公告)号：US20110289926A1
公开(公告)日：2011-12-01
申请号：US12791341
申请日：2010-06-01
申请人： Brandon Taylor Overby , Jason Allen Seale , Ibrahim Ucok
发明人： Brandon Taylor Overby , Jason Allen Seale , Ibrahim Ucok
IPC分类号： F02C7/22 , B21D53/00
CPC分类号： F23R3/002
摘要： A turbomachine includes a compressor, a turbine, and a combustor operatively coupled to the compressor and the turbine. The combustor includes a combustor casing having a flange, an outer surface and an inner surface that defines an internal passage. The combustor casing includes an extruded fluid manifold mounted to the outer surface. The extruded fluid manifold includes first and second walls integrally formed with a third, connecting, wall. The first wall includes a first mounting element and the second wall includes a second mounting element. The first mounting element extends axially along the combustor casing away from the first wall and the second mounting element extends axially along the combustor casing away from the second wall and the first mounting element. The extruded fluid manifold is joined to the outer surface of the combustor casing through the first and second mounting elements.
摘要翻译：涡轮机包括压缩机，涡轮机和可操作地联接到压缩机和涡轮机的燃烧器。燃烧器包括具有凸缘，外表面和限定内部通道的内表面的燃烧器壳体。燃烧器壳体包括安装到外表面的挤压流体歧管。挤压流体歧管包括与第三连接壁一体形成的第一和第二壁。第一壁包括第一安装元件，第二壁包括第二安装元件。第一安装元件沿着燃烧器壳体轴向延伸远离第一壁并且第二安装元件沿着燃烧器壳体轴向延伸远离第二壁和第一安装元件。挤压流体歧管通过第一和第二安装元件连接到燃烧器壳体的外表面。

3. 发明申请

US20130081397A1 FORWARD CASING WITH A CIRCUMFERENTIAL SLOPED SURFACE AND A COMBUSTOR ASSEMBLY INCLUDING SAME 审中-公开
标题翻译：具有圆形斜面的前进外壳和包括相同的组合装置
公开(公告)号：US20130081397A1
公开(公告)日：2013-04-04
申请号：US13252525
申请日：2011-10-04
申请人： Brandon Taylor Overby
发明人： Brandon Taylor Overby
IPC分类号： F23R3/00 , F23R3/28
CPC分类号： F23R3/46 , F23R3/10 , F23R3/286 , F23R2900/00014
摘要： A forward casing used in a combustor assembly for a turbine engine includes a circumferential sloped surface which reduces the total interior volume within the forward casing. The circumferential sloped surface can be flat or concave shaped.
摘要翻译：在用于涡轮发动机的燃烧器组件中使用的前部壳体包括周向倾斜的表面，其减小前部壳体内的总内部体积。圆周倾斜的表面可以是平的或凹形的。

4. 发明申请

US20130067923A1 COMBUSTOR AND METHOD FOR CONDITIONING FLOW THROUGH A COMBUSTOR 审中-公开
标题翻译：用于通过燃烧器调节流量的COMBUSTOR和方法
公开(公告)号：US20130067923A1
公开(公告)日：2013-03-21
申请号：US13237064
申请日：2011-09-20
申请人： Brandon Taylor Overby , Keith C. Belsom , Jason Thurman Stewart , Azardokht Hajiloo , Richard Martin DiCintio , Dereck J. Ouellet
发明人： Brandon Taylor Overby , Keith C. Belsom , Jason Thurman Stewart , Azardokht Hajiloo , Richard Martin DiCintio , Dereck J. Ouellet
IPC分类号： F23R3/26 , F23R3/02
CPC分类号： F23R3/04
摘要： A combustor includes an end cover and a casing adjacent to the end cover, wherein the end cover and casing at least partially define a volume inside the combustor. The combustor further includes an end cap that extends radially across at least a portion of the combustor, at least one nozzle arranged in the end cap to provide fluid communication through the end cap, and means for conditioning flow through the volume. A method for conditioning flow through a combustor includes flowing a working fluid through a volume at least partially defined by an end cover, a casing, and an end cap that extends radially across at least a portion of the combustor and flowing the working fluid across an annular insert adjacent to the end cover.
摘要翻译：燃烧器包括端盖和邻近端盖的壳体，其中端盖和壳体至少部分地限定了燃烧器内部的体积。燃烧器还包括端帽，其径向延伸穿过燃烧器的至少一部分，布置在端盖中的至少一个喷嘴以提供通过端盖的流体连通，以及用于调节通过该体积的流动的装置。用于调节通过燃烧器的流动的方法包括使工作流体流过至少部分地由端盖，壳体和端盖限定的体积，所述容积径向延伸穿过燃烧器的至少一部分并使工作流体流过邻近端盖的环形插件。

5. 发明申请

US20130327011A1 Method And Apparatus For A Fuel Nozzle Assembly For Use With A Combustor 审中-公开
标题翻译：用于燃烧器的燃油喷嘴组件的方法和装置
公开(公告)号：US20130327011A1
公开(公告)日：2013-12-12
申请号：US13492561
申请日：2012-06-08
申请人： Brandon Taylor Overby , Dereck Joseph Ouellet
发明人： Brandon Taylor Overby , Dereck Joseph Ouellet
IPC分类号： F02C7/20 , B23P19/00
CPC分类号： F23R3/28 , F23R2900/00014 , Y10T29/49323
摘要： A fuel nozzle assembly for use with a combustor is provided. The fuel nozzle assembly includes a fuel nozzle including a discharge end. A cap is coupled adjacent to the nozzle discharge end, wherein the cap includes an outer surface. At least one dampener mechanism is coupled to the cap outer surface to facilitate reducing vibrations induced to the fuel nozzle.
摘要翻译：提供了一种用于燃烧器的燃料喷嘴组件。燃料喷嘴组件包括具有排出端的燃料喷嘴。帽与喷嘴排出端相邻地连接，其中盖包括外表面。至少一个阻尼器机构联接到盖外表面，以便减少引起燃料喷嘴的振动。

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