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公开(公告)号：US08966903B2
公开(公告)日：2015-03-03
申请号：US13212105
申请日：2011-08-17
CPC分类号： F23R3/002 , F23M20/005 , F23R2900/00014
摘要： Certain embodiments of the present disclosure include a combustor resonator having a non-uniform annulus between a combustor assembly and a resonator shell. The combustor resonator may further include resonator necks or passages having non-uniform lengths and geometries.
摘要翻译： 本公开的某些实施例包括在燃烧器组件和谐振器壳体之间具有不均匀环空的燃烧器谐振器。 燃烧器谐振器还可以包括具有不均匀长度和几何形状的谐振器颈部或通道。
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公开(公告)号：US20130042619A1
公开(公告)日：2013-02-21
申请号：US13212105
申请日：2011-08-17
IPC分类号： F23R3/16
CPC分类号： F23R3/002 , F23M20/005 , F23R2900/00014
摘要： Certain embodiments of the present disclosure include a combustor resonator having a non-uniform annulus between a combustor assembly and a resonator shell. The combustor resonator may further include resonator necks or passages having non-uniform lengths and geometries.
摘要翻译： 本公开的某些实施例包括在燃烧器组件和谐振器壳体之间具有不均匀环空的燃烧器谐振器。 燃烧器谐振器还可以包括具有不均匀长度和几何形状的谐振器颈部或通道。
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公开(公告)号：US20120297785A1
公开(公告)日：2012-11-29
申请号：US13115058
申请日：2011-05-24
摘要： A system includes a gas turbine combustor, which includes a combustion liner disposed about a combustion region, a flow sleeve disposed about the combustion liner, an air passage between the combustion liner and the flow sleeve, and a structure between the combustion liner and the flow sleeve. The structure obstructs an airflow through the air passage. The gas turbine combustor also includes a wake reducer disposed adjacent the structure. The wake reducer directs a flow into a wake region downstream of the structure.
摘要翻译： 一种系统包括燃气轮机燃烧器，其包括围绕燃烧区域设置的燃烧衬套，围绕燃烧衬套设置的流动套筒，在燃烧衬套和流动套筒之间的空气通道，以及燃烧衬套与流体之间的结构 袖。 该结构阻碍通过空气通道的气流。 燃气轮机燃烧器还包括邻近结构布置的尾流减速器。 尾流减速器将流动引导到结构下游的尾流区域。
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公开(公告)号：US08893501B2
公开(公告)日：2014-11-25
申请号：US13072820
申请日：2011-03-28
摘要： The present application and the resultant patent provide a combustor for mixing a flow of air and a flow of fuel. The combustor may include an air path for the flow of air, a number of fuel injectors positioned in the air path for the flow of fuel, and a crossfire tube positioned within the air path upstream of the fuel injectors. The crossfire tube may include a number of purge holes positioned on a downstream side thereof to reduce a wake in the flow of air caused by the crossfire tube in the air path.
摘要翻译： 本申请和所得专利提供了一种用于混合空气流和燃料流的燃烧器。 燃烧器可以包括用于空气流动的空气路径，位于用于燃料流动的空气路径中的多个燃料喷射器，以及位于燃料喷射器上游的空气路径内的交叉火管。 交火管可以包括位于其下游侧的多个吹扫孔，以减少由空气路径中的交火管引起的空气流中的尾流。
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公开(公告)号：US08919127B2
公开(公告)日：2014-12-30
申请号：US13115058
申请日：2011-05-24
摘要： A system includes a gas turbine combustor, which includes a combustion liner disposed about a combustion region, a flow sleeve disposed about the combustion liner, an air passage between the combustion liner and the flow sleeve, and a structure between the combustion liner and the flow sleeve. The structure obstructs an airflow through the air passage. The gas turbine combustor also includes a wake reducer disposed adjacent the structure. The wake reducer directs a flow into a wake region downstream of the structure.
摘要翻译： 一种系统包括燃气轮机燃烧器，其包括围绕燃烧区域设置的燃烧衬套，围绕燃烧衬套设置的流动套筒，在燃烧衬套和流动套筒之间的空气通道，以及燃烧衬套与流体之间的结构 袖。 该结构阻碍通过空气通道的气流。 燃气轮机燃烧器还包括邻近结构布置的尾流减速器。 尾流减速器将流动引导到结构下游的尾流区域。
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公开(公告)号：US20120247118A1
公开(公告)日：2012-10-04
申请号：US13072820
申请日：2011-03-28
摘要： The present application and the resultant patent provide a combustor for mixing a flow of air and a flow of fuel. The combustor may include an air path for the flow of air, a number of fuel injectors positioned in the air path for the flow of fuel, and a crossfire tube positioned within the air path upstream of the fuel injectors. The crossfire tube may include a number of purge holes positioned on a downstream side thereof to reduce a wake in the flow of air caused by the crossfire tube in the air path.
摘要翻译： 本申请和所得专利提供了一种用于混合空气流和燃料流的燃烧器。 燃烧器可以包括用于空气流动的空气路径，位于用于燃料流动的空气路径中的多个燃料喷射器，以及位于燃料喷射器上游的空气路径内的交火火管。 交火管可以包括位于其下游侧的多个吹扫孔，以减少由空气路径中的交火管引起的空气流中的尾流。
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公开(公告)号：US20120279224A1
公开(公告)日：2012-11-08
申请号：US13099938
申请日：2011-05-03
申请人： Donald Mark Bailey , Jonathan Dwight Berry , Luis Manuel Flamand , Kwanwoo Kim , Patrick Benedict Melton , Robert Joseph Rohrssen , John Drake Vanselow
发明人： Donald Mark Bailey , Jonathan Dwight Berry , Luis Manuel Flamand , Kwanwoo Kim , Patrick Benedict Melton , Robert Joseph Rohrssen , John Drake Vanselow
IPC分类号： F23C3/00
CPC分类号： F23R3/283 , F23D2900/00003 , F23R3/286 , F23R3/46 , F23R3/54 , F23R2900/00017 , F23R2900/00018
摘要： A gas turbine engine combustor is provided and includes an array of fuel nozzles, a combustion casing assembly disposed about the array of fuel nozzles and an end cap assembly disposed within the combustion casing assembly to define with the combustion casing assembly an axis-symmetric annulus through which fluid travels into each of the fuel nozzles, at least one of the combustion casing assembly and the end cap assembly being formed with lobed, three-dimensional contouring.
摘要翻译： 提供了一种燃气涡轮发动机燃烧器，其包括燃料喷嘴阵列，围绕燃料喷嘴阵列设置的燃烧壳体组件和设置在燃烧壳体组件内的端盖组件，以便与燃烧壳体组件形成轴对称的环通过 所述流体行进到每个燃料喷嘴中，燃烧壳体组件和端盖组件中的至少一个形成有叶状的三维轮廓。
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8.发明授权公开(公告)号：US08938978B2
公开(公告)日：2015-01-27
申请号：US13099938
申请日：2011-05-03
申请人： Donald Mark Bailey , Jonathan Dwight Berry , Luis Manuel Flamand , Kwanwoo Kim , Patrick Benedict Melton , Robert Joseph Rohrssen , John Drake Vanselow
发明人： Donald Mark Bailey , Jonathan Dwight Berry , Luis Manuel Flamand , Kwanwoo Kim , Patrick Benedict Melton , Robert Joseph Rohrssen , John Drake Vanselow
CPC分类号： F23R3/283 , F23D2900/00003 , F23R3/286 , F23R3/46 , F23R3/54 , F23R2900/00017 , F23R2900/00018
摘要： A gas turbine engine combustor is provided and includes an array of fuel nozzles, a combustion casing assembly disposed about the array of fuel nozzles and an end cap assembly disposed within the combustion casing assembly to define with the combustion casing assembly an axis-symmetric annulus through which fluid travels into each of the fuel nozzles, at least one of the combustion casing assembly and the end cap assembly being formed with lobed, three-dimensional contouring.
摘要翻译： 提供了一种燃气涡轮发动机燃烧器，其包括燃料喷嘴阵列，围绕燃料喷嘴阵列设置的燃烧壳体组件和设置在燃烧壳体组件内的端盖组件，以便与燃烧壳体组件形成轴对称的环通过 所述流体行进到每个燃料喷嘴中，燃烧壳体组件和端盖组件中的至少一个形成有叶状的三维轮廓。
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9.发明授权Gas turbine combustor endcover assembly with integrated flow restrictor and manifold seal 有权具有集成流量限制器和歧管密封件的燃气轮机燃烧器整流器组件公开(公告)号：US08820086B2
公开(公告)日：2014-09-02
申请号：US13008399
申请日：2011-01-18
IPC分类号： F02C1/00
CPC分类号： F23R3/283 , F23K5/14 , F23K2900/05142 , F23R2900/00005 , F23R2900/00012
摘要： An endcover assembly for a turbine combustor adapted to support one or more combustor nozzles includes a substantially flat plate having one side which in use, faces a combustion chamber and an opposite side which, in use, faces away from the combustion chamber. At least one fuel passage extends through the substantially flat plate. A fuel manifold porting block is secured to the opposite side of the flat plate with at least one port aligned with the at least one passage. A fuel restrictor insert formed with multiple flow orifices is located between the flat plate and the fuel manifold porting block in alignment with the at least one fuel passage and the at least one port.
摘要翻译： 适于支撑一个或多个燃烧器喷嘴的用于涡轮机燃烧器的封盖组件包括基本平坦的板，其具有一个侧面，其在使用中面向燃烧室，在使用中相对侧面远离燃烧室。 至少一个燃料通道延伸穿过基本平坦的板。 燃料歧管移动块被固定到平板的相对侧，其中至少一个端口与至少一个通道对准。 形成有多个流动孔的燃料限制器插件位于平板和燃料歧管移动块之间，与至少一个燃料通道和至少一个端口对准。
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公开(公告)号：US20120305677A1
公开(公告)日：2012-12-06
申请号：US13153506
申请日：2011-06-06
IPC分类号： F23D11/38
摘要： A system for conditioning flow through a plurality of nozzles arranged in a combustor includes a shield circumferentially surrounding at least a portion of the plurality of nozzles and a plurality of baffles disposed circumferentially around the shield. Each baffle is circumferentially disposed between adjacent nozzles.
摘要翻译： 用于调节流过布置在燃烧器中的多个喷嘴的流动系统包括周向围绕多个喷嘴的至少一部分的屏蔽件和围绕屏蔽件周向设置的多个挡板。 每个挡板周向地设置在相邻喷嘴之间。
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