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公开(公告)号：US09829200B2
公开(公告)日：2017-11-28
申请号：US14445485
申请日：2014-07-29
Applicant: ALSTOM Technology Ltd
Inventor： Xianfeng Gao , Urs Benz , Andre Theuer , Rohit Kulkarni
CPC classification number: F23R3/42 , F02C3/14 , F05D2220/32 , F05D2240/35 , F05D2260/201 , F05D2260/232 , F23C7/004 , F23D2900/14004 , F23D2900/14021 , F23R3/20 , F23R3/28 , F23R3/286 , F23R3/346 , F23R3/36 , F23R3/46 , F23R2900/00014 , F23R2900/03041 , F23R2900/03043 , F23R2900/03044 , F23R2900/03341
Abstract: The invention relates to a burner arrangement for using in a single combustion chamber or in a can-combustor comprising a center body burner located upstream of a combustion zone, an annular duct with a cross section area, intermediate lobes which are arranged in circumferential direction and in longitudinal direction of the center body. The lobes being actively connected to the cross section area of the annular duct, wherein a cooling air is guided through a number of pipes within the lobes to the center body and cools beforehand at least the front section of the center body based on impingement cooling. Subsequently, the impingement cooling air cools the middle and back face of the center body based on convective and/or effusion cooling. At least the back face of the center body includes on the inside at least one damper.
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公开(公告)号：US20140150435A1
公开(公告)日：2014-06-05
申请号：US14088527
申请日：2013-11-25
Applicant: ALSTOM Technology Ltd
Inventor： Thomas Michael MAURER , Urs Benz , Mirko Ruben Bothien
IPC: F23R3/42
CPC classification number: F23R3/42 , F05D2260/963 , F23M20/005 , F23R3/00 , F23R3/002 , F23R2900/00014
Abstract: The invention relates to a damping device for a gas turbine combustor with significantly reduced cooling air mass flow requirements. The damping device includes a wall with a first inner wall and a second outer wall, arranged in a distance to each other. The inner wall is subjected to high temperatures on a side with a hot gas flow. A plurality of cooling channels extend essentially parallel between the first inner wall and the second outer wall, and at least one damping volume bordered by cooling channels. Furthermore, the damping device includes a first passage for supplying a cooling medium from a cooling channel into the damping volume and a second passage for connecting the damping volume to the combustion chamber. An end plate, fixed to the inner wall, separates the damping volume from the combustion chamber.
Abstract translation: 本发明涉及一种用于燃气轮机燃烧器的阻尼装置，其具有显着降低的冷却空气质量流量要求。 阻尼装置包括具有彼此间隔设置的第一内壁和第二外壁的壁。 内壁在热气流的一侧经受高温。 多个冷却通道基本上平行于第一内壁和第二外壁之间延伸，以及至少一个由冷却通道界定的阻尼体积。 此外，阻尼装置包括用于将冷却介质从冷却通道供应到阻尼容积中的第一通道和用于将阻尼体积连接到燃烧室的第二通道。 固定在内壁上的端板将阻尼体积与燃烧室分开。
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公开(公告)号：US09557062B2
公开(公告)日：2017-01-31
申请号：US14088527
申请日：2013-11-25
Applicant: ALSTOM Technology Ltd
Inventor： Thomas Michael Maurer , Urs Benz , Mirko Ruben Bothien
CPC classification number: F23R3/42 , F05D2260/963 , F23M20/005 , F23R3/00 , F23R3/002 , F23R2900/00014
Abstract: The invention relates to a damping device for a gas turbine combustor with significantly reduced cooling air mass flow requirements. The damping device includes a wall with a first inner wall and a second outer wall, arranged in a distance to each other. The inner wall is subjected to high temperatures on a side with a hot gas flow. A plurality of cooling channels extend essentially parallel between the first inner wall and the second outer wall, and at least one damping volume bordered by cooling channels. Furthermore, the damping device includes a first passage for supplying a cooling medium from a cooling channel into the damping volume and a second passage for connecting the damping volume to the combustion chamber. An end plate, fixed to the inner wall, separates the damping volume from the combustion chamber.
Abstract translation: 本发明涉及一种用于燃气轮机燃烧器的阻尼装置，其具有显着降低的冷却空气质量流量要求。 阻尼装置包括具有彼此间隔设置的第一内壁和第二外壁的壁。 内壁在热气流的一侧经受高温。 多个冷却通道基本上平行于第一内壁和第二外壁之间延伸，以及至少一个由冷却通道界定的阻尼体积。 此外，阻尼装置包括用于将冷却介质从冷却通道供应到阻尼容积中的第一通道和用于将阻尼体积连接到燃烧室的第二通道。 固定在内壁上的端板将阻尼体积与燃烧室分开。
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公开(公告)号：US20140109588A1
公开(公告)日：2014-04-24
申请号：US14060931
申请日：2013-10-23
Applicant: ALSTOM Technology Ltd
Inventor： Andrea Ciani , John Philip Wood , Douglas Anthony Pennell , Ewald Freitag , Urs Benz , Andre Theuer
IPC: F23R3/28
CPC classification number: F23R3/16 , F02C6/003 , F02C9/26 , F02C9/32 , F02C9/34 , F05B2260/222 , F23R3/20 , F23R3/286 , F23R3/34 , F23R3/346 , F23R3/36 , F23R3/46 , F23R2900/03341
Abstract: The present invention relation to a burner for a combustion chamber of a gas turbine with a mixing and injection device. The mixing and injection device includes a limiting wall that defines a gas-flow channel and at least two streamlined bodies, each extending in a first transverse direction into the gas-flow channel. Each streamlined body has two lateral surfaces that are arranged essentially parallel to the main-flow direction, the lateral surfaces being joined to one another at their upstream side to form a leading edge of the body and joined at their downstream side to form a trailing edge of the body. Each streamlined body has a cross-section perpendicular to the first transverse direction that is shaped as a streamlined profile. At least one of the streamlined bodies is provided with a mixing structure and with at least one fuel nozzle located at its trailing edge for introducing at least one fuel essentially parallel to the main-flow direction into the flow channel, wherein at least two of the streamlined bodies have different lengths along the first transverse direction such that they may be used for a can combustor. The invention also relates to a method of using said burner in a gas turbine.
Abstract translation: 本发明涉及一种具有混合和注射装置的燃气轮机燃烧室的燃烧器。 混合和注入装置包括界定气流通道的限制壁和至少两个流线型的主体，每个流体线体在第一横向方向上延伸到气体流动通道中。 每个流线型体具有基本上平行于主流动方向布置的两个侧表面，侧表面在其上游侧彼此连接以形成主体的前缘并在其下游侧接合以形成后缘 的身体。 每个流线型本体具有垂直于第一横向方向的横截面，其形状为流线型轮廓。 流线型主体中的至少一个设置有混合结构，并且具有位于其后缘处的至少一个燃料喷嘴，用于将基本上平行于主流动方向的至少一个燃料引入流动通道中，其中至少两个 流线型主体沿着第一横向方向具有不同的长度，使得它们可以用于罐式燃烧器。 本发明还涉及在燃气轮机中使用所述燃烧器的方法。
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5.发明授权公开(公告)号：US10139112B2
公开(公告)日：2018-11-27
申请号：US14727977
申请日：2015-06-02
Applicant: ALSTOM Technology Ltd
Inventor： Uwe Rüdel , Urs Benz , Christoph Appel , Ivan Lenuzzi
IPC: F02C1/00 , F23R3/50 , F23R3/16 , F02C3/04 , F02C3/14 , F02C7/18 , F23R3/60 , F23R3/00 , F23R3/48 , F01D9/02
Abstract: The invention relates to an annular combustion chamber of a gas turbine having a machine axis. The combustion chamber includes at least two zones. A first zone receives the fuel/air mixture of a plurality of burners. A second zone guides the hot gases being produced by the burners from the first zone to an entrance of a turbine section of said gas turbine. An annular transition liner includes a plurality of liner segments located at the transition between said first zone and second zone. Each of the liner segments includes with respect to the axial hot gas flow a leading edge, a trailing edge, and two sidewalls, and is provided with axial mounting means at the leading and trailing edges, such that the liner segment can be installed in axial direction and is axially fixed by respective segments of the neighboring first zone. Local spacer ribs are provided at the leading edge of the liner segments in order to establish a gap of minimum width between the liner segments and the fixing segments of the neighboring first zone.
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Patent Agency Ranking
6.发明授权Near-wall roughness for damping devices reducing pressure oscillations in combustion systems 有权用于阻尼装置的近壁粗糙度可减少燃烧系统中的压力振荡公开(公告)号：US09261058B2
公开(公告)日：2016-02-16
申请号：US13950805
申请日：2013-07-25
Applicant: ALSTOM Technology Ltd
Inventor： Michael Maurer , Andreas Huber , Lothar Schneider , Urs Benz , Diane Lauffer
CPC classification number: F02M35/1261 , F05B2260/221 , F23M20/005 , F23R3/002 , F23R2900/00014 , F23R2900/03045
Abstract: A damping device for reducing pressure oscillations in a combustion system includes at least a portion provided with a first, outer wall, a second, inner wall, an intermediate plate interposed between the first wall and the second wall. This intermediate plate forms a spacer grid to define at least one chamber between said first wall and said second wall, first passages connecting each of said at least one chamber to the inner of the combustion system, and second passages connecting each of said at least one chamber to the outer of the combustion system. The second passages open at the same side of said chambers as the first passages, the second passages have a portion extending parallel to the inner wall. This parallel portion of said second passages is equipped with heat transfer enhancing means.
Abstract translation: 用于减少燃烧系统中的压力振荡的阻尼装置包括设置有第一外壁，第二内壁，介于第一壁与第二壁之间的中间板的至少一部分。 该中间板形成间隔栅格以在所述第一壁和所述第二壁之间限定至少一个室，将所述至少一个室中的每一个连接到燃烧系统的内部的第一通道，以及将所述至少一个 室到燃烧系统的外部。 所述第二通道在与所述第一通道相同的所述腔室的侧面开口，所述第二通道具有平行于所述内壁延伸的部分。 所述第二通道的该平行部分配备有传热增强装置。
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7.发明申请NEAR-WALL ROUGHNESS FOR DAMPING DEVICES REDUCING PRESSURE OSCILLATIONS IN COMBUSTION SYSTEMS 有权用于阻尼装置的近壁厚度降低燃烧系统中的压力振荡公开(公告)号：US20140053559A1
公开(公告)日：2014-02-27
申请号：US13950805
申请日：2013-07-25
Applicant: ALSTOM Technology Ltd
Inventor： Michael MAURER , Andreas Huber , Lothar Schneider , Urs Benz , Diane Lauffer
IPC: F02M35/12
CPC classification number: F02M35/1261 , F05B2260/221 , F23M20/005 , F23R3/002 , F23R2900/00014 , F23R2900/03045
Abstract: A damping device for reducing pressure oscillations in a combustion system includes at least a portion provided with a first, outer wall, a second, inner wall, an intermediate plate interposed between the first wall and the second wall. This intermediate plate forms a spacer grid to define at least one chamber between said first wall and said second wall, first passages connecting each of said at least one chamber to the inner of the combustion system, and second passages connecting each of said at least one chamber to the outer of the combustion system. The second passages open at the same side of said chambers as the first passages, the second passages have a portion extending parallel to the inner wall. This parallel portion of said second passages is equipped with heat transfer enhancing means.
Abstract translation: 用于减少燃烧系统中的压力振荡的阻尼装置包括设置有第一外壁，第二内壁，介于第一壁与第二壁之间的中间板的至少一部分。 该中间板形成间隔栅格以在所述第一壁和所述第二壁之间限定至少一个室，将所述至少一个室中的每一个连接到燃烧系统的内部的第一通道，以及将所述至少一个 室到燃烧系统的外部。 所述第二通道在与所述第一通道相同的所述腔室的侧面开口，所述第二通道具有平行于所述内壁延伸的部分。 所述第二通道的该平行部分配备有传热增强装置。
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公开(公告)号：US09625154B2
公开(公告)日：2017-04-18
申请号：US14279888
申请日：2014-05-16
Applicant: ALSTOM Technology Ltd
Inventor： Urs Benz , Nicolas Noiray
CPC classification number: F23R3/16 , F23M20/005 , F23M2900/05002 , F23R3/002 , F23R3/60 , F23R2900/00005 , F23R2900/00014
Abstract: The invention relates to a damper for reducing the pulsations in a combustion chamber of a gas turbine. The damper includes a resonator cavity with an inlet and a neck tube in flow communication with the interior of the combustion chamber and resonator cavity, and a compensation assembly pivotably connected with the neck tube. The compensation assembly is inserted between the resonator cavity and the combustion chamber to permit relative rotation between the combustion chamber and the resonator cavity. With the damper according to the present invention, by way of providing the compensation assembly, it is assured the relative rotation between the combustion chamber and the resonator cavity is compensated, hence operation life is elongated.
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公开(公告)号：US20150075168A1
公开(公告)日：2015-03-19
申请号：US14498136
申请日：2014-09-26
Applicant: ALSTOM Technology Ltd.
Inventor： Jeffrey DE JONGE , Andreas Huber , Bruno Schuermans , Urs Benz
CPC classification number: F02C7/24 , B23P19/04 , F23M20/005 , F23R3/002 , F23R2900/00012 , F23R2900/00014 , Y10T29/49323
Abstract: A strip seal arrangement for turbine components employs acoustic damping. A sealing plate having a front face adjacent a combustion chamber and a back face facing away from a combustion chamber configured to have one or more holes of a predefined cross-sectional area. Containers having predefined volumes are attached to the back face of the sealing plate such that the one or more holes are in fluidic communication with the one or more containers thereby creating at least one acoustic damper. The side edges of the sealing plate fit into a slots of burner front panels, creating a seal between the panels.
Abstract translation: 涡轮机部件的带状密封装置采用声阻尼。 密封板，其具有邻近燃烧室的前表面和背离燃烧室的背面，该燃烧室被配置为具有预定横截面积的一个或多个孔。 具有预定体积的容器附接到密封板的背面，使得一个或多个孔与一个或多个容器流体连通，从而形成至少一个声阻尼器。 密封板的侧边缘装配到燃烧器前面板的槽中，在面板之间形成密封。
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公开(公告)号：US20150047364A1
公开(公告)日：2015-02-19
申请号：US14445485
申请日：2014-07-29
Applicant: ALSTOM Technology Ltd
Inventor： Xianfeng Gao , Urs Benz , Andre Theuer , Rohit Kulkarni
CPC classification number: F23R3/42 , F02C3/14 , F05D2220/32 , F05D2240/35 , F05D2260/201 , F05D2260/232 , F23C7/004 , F23D2900/14004 , F23D2900/14021 , F23R3/20 , F23R3/28 , F23R3/286 , F23R3/346 , F23R3/36 , F23R3/46 , F23R2900/00014 , F23R2900/03041 , F23R2900/03043 , F23R2900/03044 , F23R2900/03341
Abstract: The invention relates to a burner arrangement for using in a single combustion chamber or in a can-combustor comprising a center body burner located upstream of a combustion zone, an annular duct with a cross section area, intermediate lobes which are arranged in circumferential direction and in longitudinal direction of the center body. The lobes being actively connected to the cross section area of the annular duct, wherein a cooling air is guided through a number of pipes within the lobes to the center body and cools beforehand at least the front section of the center body based on impingement cooling. Subsequently, the impingement cooling air cools the middle and back face of the center body based on convective and/or effusion cooling. At least the back face of the center body includes on the inside at least one damper.
Abstract translation: 本发明涉及一种在单个燃烧室或罐式燃烧器中使用的燃烧器装置，其包括位于燃烧区上游的中心体燃烧器，具有横截面积的环形管道，沿圆周方向布置的中间叶片， 在中心体的纵向。 叶片主动地连接到环形管道的横截面区域，其中冷却空气被引导穿过叶片内的多个管道到达中心体，并且至少基于冲击冷却来中心体的前部部分预先冷却。 随后，冲击冷却空气基于对流和/或渗流冷却来冷却中心体的中后表面。 至少中心体的背面在内侧至少包括一个阻尼器。
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