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公开(公告)号：US20070107710A1
公开(公告)日：2007-05-17
申请号：US11447109
申请日：2006-06-06
IPC分类号： F02B23/08
摘要： An annular combustion chamber comprising axial walls interconnected by a chamber end wall having a coefficient of thermal expansion that is different from that of the axial walls, the chamber end wall being provided with a plurality of inner and outer fastener tabs secured by fastener systems to the end portions of the axial walls. Each fastener system comprises a bolt, a nut tightened onto one of the ends of the bolt, and a slideway bushing disposed around the bolt between the nut and the end portion of the corresponding axial wall, a determined amount of radial clearance being provided between the nut and the end portion of the axial wall so as to enable the chamber end wall to expand radially freely in operation relative to the axial walls.
摘要翻译： 环形燃烧室包括通过腔室端壁互连的轴向壁，其具有与轴向壁的热膨胀系数不同的热膨胀系数，腔室端壁设置有多个通过紧固件系统固定到内部和外部紧固件接头 轴向壁的端部。 每个紧固件系统包括螺栓，紧固在螺栓的一个端部上的螺母，以及设置在螺母和相应的轴向壁的端部之间的螺栓周围的滑道衬套，确定量的径向间隙设置在 螺母和轴向壁的端部，以便使得腔室端壁能够相对于轴向壁在操作中径向自由地膨胀。
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公开(公告)号：US20050028528A1
公开(公告)日：2005-02-10
申请号：US10870051
申请日：2004-06-18
IPC分类号： F02C3/14 , F02C7/18 , F02C7/20 , F02C7/266 , F23R3/00 , F23R3/50 , F23R3/60 , F02C1/00 , F02G3/00
CPC分类号： F02C7/266 , F23R3/007 , F23R3/50 , F23R3/60 , F23R2900/00012 , Y02T50/672
摘要： The invention provides a combustion chamber comprising a chamber wall disposed radially inside a casing, an igniter plug for igniting the air-fuel mixture, the plug being mounted on said casing and comprising a body with a free end that is disposed in an opening formed through said chamber wall with a large amount of clearance to accommodate relative displacement between said casing and said chamber wall, and a sealing device provided between said body and the perimeter of said opening, said sealing device comprising an annular plug-guide through which said body passes, the plug-guide being slidably mounted at the radially-outer end of an annular support whose base is secured to said perimeter, wherein the support is secured to the radially-outer portion of a chimney passing through said opening and presenting at its radially-inner end a collar bearing against the inside face of the chamber wall, and wherein a cooling circuit for said collar is provided.
摘要翻译： 本发明提供了一种燃烧室，其包括径向设置在壳体内的室壁，用于点燃空气 - 燃料混合物的点火器塞，该塞子安装在所述壳体上，并且包括具有自由端的主体，该主体设置在通过 所述室壁具有大量的间隙以适应所述壳体和所述室壁之间的相对位移，以及设置在所述主体和所述开口的周边之间的密封装置，所述密封装置包括环形插塞导向件，所述主体通过所述环形插头导向件 插塞导向件可滑动地安装在其基部固定到所述周边的环形支撑件的径向外端，其中所述支撑件固定到穿过所述开口的烟囱的径向外部， 内端具有抵靠室壁的内表面的轴环，并且其中提供用于所述轴环的冷却回路。
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3.发明授权Mounting a high pressure turbine nozzle in leaktight manner to one end of a combustion chamber in a gas turbine 有权将高压涡轮喷嘴以密封方式安装在燃气轮机中的燃烧室的一端公开(公告)号：US07237387B2
公开(公告)日：2007-07-03
申请号：US11153354
申请日：2005-06-16
申请人： Caroline Aumont , Eric Conete , Mario De Sousa , Didier Hernandez
发明人： Caroline Aumont , Eric Conete , Mario De Sousa , Didier Hernandez
IPC分类号： F23R3/42
CPC分类号： F01D9/042 , F01D9/023 , Y02T50/672 , Y02T50/675
摘要： The downstream end portions of the inner and outer walls of the combustion chamber of the gas turbine are pressed against the inner and outer platforms respectively of the vanes of the high pressure turbine nozzle and they extend thereover substantially to the downstream end of the platforms, and the means for mechanically connecting the turbine nozzle to the downstream end portions of the combustion chamber walls are formed by connection screws implanted in the airfoils of the vanes of the turbine nozzle, passing through holes formed in the end portions of the combustion chamber walls. Thus, the downstream end portions of the combustion chamber walls contribute to preventing leakage from the gas stream at the interface between the chamber and the nozzle, and also along the nozzle.
摘要翻译： 燃气轮机的燃烧室的内壁和外壁的下游端部分别压靠在高压涡轮喷嘴的叶片的内平台和外平台上，并且它们基本延伸到平台的下游端，并且 用于将涡轮喷嘴机械地连接到燃烧室壁的下游端部的装置通过注入在涡轮喷嘴的叶片的翼型中的连接螺钉形成，通过形成在燃烧室壁的端部中的孔。 因此，燃烧室壁的下游端部有助于防止在腔室和喷嘴之间的界面处以及沿着喷嘴的气流的泄漏。
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公开(公告)号：US07101173B2
公开(公告)日：2006-09-05
申请号：US10870051
申请日：2004-06-18
IPC分类号： F23Q7/06
CPC分类号： F02C7/266 , F23R3/007 , F23R3/50 , F23R3/60 , F23R2900/00012 , Y02T50/672
摘要： The invention provides a combustion chamber comprising a chamber wall disposed radially inside a casing, an igniter plug for igniting the air-fuel mixture, the plug being mounted on said casing and comprising a body with a free end that is disposed in an opening formed through said chamber wall with a large amount of clearance to accommodate relative displacement between said casing and said chamber wall, and a sealing device provided between said body and the perimeter of said opening, said sealing device comprising an annular plug-guide through which said body passes, the plug-guide being slidably mounted at the radially-outer end of an annular support whose base is secured to said perimeter, wherein the support is secured to the radially-outer portion of a chimney passing through said opening and presenting at its radially-inner end a collar bearing against the inside face of the chamber wall, and wherein a cooling circuit for said collar is provided.
摘要翻译： 本发明提供了一种燃烧室，其包括径向设置在壳体内的室壁，用于点燃空气 - 燃料混合物的点火器塞，该塞子安装在所述壳体上，并且包括具有自由端的主体，该主体设置在通过 所述室壁具有大量的间隙以适应所述壳体和所述室壁之间的相对位移，以及设置在所述主体和所述开口的周边之间的密封装置，所述密封装置包括环形插塞导向件，所述主体通过所述环形插头导向件 插塞导向件可滑动地安装在其基部固定到所述周边的环形支撑件的径向外端，其中所述支撑件固定到穿过所述开口的烟囱的径向外部， 内端具有抵靠室壁的内表面的轴环，并且其中提供用于所述轴环的冷却回路。
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5.发明申请Assembly comprising a gas turbine combustion chamber integrated with a high pressure turbine nozzle 有权组件包括与高压涡轮喷嘴集成的燃气轮机燃烧室公开(公告)号：US20060032237A1
公开(公告)日：2006-02-16
申请号：US11153356
申请日：2005-06-16
申请人： Caroline Aumont , Eric Conete , Mario De Sousa , Didier Hernandez
发明人： Caroline Aumont , Eric Conete , Mario De Sousa , Didier Hernandez
IPC分类号： F23R3/42
CPC分类号： F01D25/246 , F01D9/023 , F01D9/041 , F05D2230/642 , F23R3/007 , F23R3/60 , Y02T50/672 , Y02T50/675
摘要： The high pressure turbine nozzle is mechanically connected to a downstream end portion of the combustion chamber and inner and outer connection ferrules connect the combustion chamber and turbine nozzle assembly to inner and outer metal shrouds in order to hold said assembly between the shrouds. Locking members are provided to prevent the turbine nozzle from turning about its axis relative to at least one of the metal shrouds so as to prevent the forces that are exerted on the turbine nozzle vanes by the flow of gas coming from the chamber being taken up by the portions of the connection ferrules that extend between the combustion chamber and turbine nozzle assembly and the metal shrouds.
摘要翻译： 高压涡轮喷嘴机械地连接到燃烧室的下游端部分，并且内部和外部连接套管将燃烧室和涡轮喷嘴组件连接到内部和外部金属罩，以将所述组件保持在护罩之间。 提供锁定构件以防止涡轮喷嘴相对于金属罩中的至少一个绕其轴线转动，以便防止通过来自腔室的气体的流动被来自腔室的气体吸收的作用在涡轮喷嘴叶片上的力被 连接套管的在燃烧室和涡轮喷嘴组件之间延伸的部分和金属罩。
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6.发明申请Mounting a high pressure turbine nozzle in leaktight manner to one end of a combustion chamber in a gas turbine 有权将高压涡轮喷嘴以密封方式安装在燃气轮机中的燃烧室的一端公开(公告)号：US20060032236A1
公开(公告)日：2006-02-16
申请号：US11153354
申请日：2005-06-16
申请人： Caroline Aumont , Eric Conete , Mario De Sousa , Didier Hernandez
发明人： Caroline Aumont , Eric Conete , Mario De Sousa , Didier Hernandez
IPC分类号： F23R3/42
CPC分类号： F01D9/042 , F01D9/023 , Y02T50/672 , Y02T50/675
摘要： The downstream end portions of the inner and outer walls of the combustion chamber of the gas turbine are pressed against the inner and outer platforms respectively of the vanes of the high pressure turbine nozzle and they extend thereover substantially to the downstream end of the platforms, and the means for mechanically connecting the turbine nozzle to the downstream end portions of the combustion chamber walls are formed by connection screws implanted in the airfoils of the vanes of the turbine nozzle, passing through holes formed in the end portions of the combustion chamber walls. Thus, the downstream end portions of the combustion chamber walls contribute to preventing leakage from the gas stream at the interface between the chamber and the nozzle, and also along the nozzle.
摘要翻译： 燃气轮机的燃烧室的内壁和外壁的下游端部分别压靠在高压涡轮喷嘴的叶片的内平台和外平台上，并且它们基本延伸到平台的下游端，并且 用于将涡轮喷嘴机械地连接到燃烧室壁的下游端部的装置通过注入在涡轮喷嘴的叶片的翼型中的连接螺钉形成，通过形成在燃烧室壁的端部中的孔。 因此，燃烧室壁的下游端部有助于防止在腔室和喷嘴之间的界面处以及沿着喷嘴的气流的泄漏。
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7.发明申请Gas turbine combustion chamber made of CMC and supported in a metal casing by CMC linking members 有权由CMC制成的燃气轮机燃烧室，通过CMC连接件支撑在金属外壳中公开(公告)号：US20060032235A1
公开(公告)日：2006-02-16
申请号：US11153353
申请日：2005-06-16
申请人： Caroline Aumont , Eric Conete , Mario De Sousa , Didier Hernandez
发明人： Caroline Aumont , Eric Conete , Mario De Sousa , Didier Hernandez
IPC分类号： F23R3/42
CPC分类号： F23R3/60 , F05C2203/08 , F23R3/007
摘要： The annular combustion chamber having ceramic matrix composite material walls is mounted inside a metal casing by linking members fastened to the chamber by brazing. The linking members comprise a plurality of inner linking tabs and a plurality of outer linking tabs connecting the chamber to the inner and outer metal shrouds of the casing, each linking tab has a first portion fastened to the outside surface of a wall of the combustion chamber by brazing, the first portions of the linking tabs being spaced apart from one another circumferentially so that the brazed connections between the chamber and the linking members occupy a set of limited zones that are spaced apart from one another.
摘要翻译： 具有陶瓷基复合材料壁的环形燃烧室通过钎焊连接构件固定在金属外壳内。 连接构件包括多个内连接突片和将腔室连接到壳体的内外金属罩的多个外连接突片，每个连接突片具有固定到燃烧室壁的外表面的第一部分 通过钎焊，连接凸片的第一部分周向地间隔开，使得腔室和连接构件之间的钎焊连接占据彼此间隔开的一组限制区域。
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8.发明申请公开(公告)号：US20050000228A1
公开(公告)日：2005-01-06
申请号：US10845113
申请日：2004-05-14
CPC分类号： F23R3/50 , F05B2230/606 , F23R3/007 , F23R3/60
摘要： The invention relates to an annular combustion chamber for a turbomachine of axis X, in which the chamber end wall is fixed to inner and outer side walls by means of a plurality of radially-inner attachment fittings and by means of a plurality of radially-outer attachment fittings disposed upstream from said chamber end wall by bolting a zone of each of said fittings to said side walls. At least one of said pluralities of attachment fittings is integrated in a ring secured to the chamber end wall and comprises a plurality of pairs of tabs which extend upstream beyond the bolting zones, the two tabs in each pair being disposed circumferentially on either side of a bolting zone and being interconnected at their upstream end to the upstream end of a fixing plate which extends between said two tabs and which presents a bolting zone for being fixed to the adjacent side wall.
摘要翻译： 本发明涉及一种用于轴线X的涡轮机的环形燃烧室，其中腔室端壁借助于多个径向内部的附接配件并且借助于多个径向外部的固定配件固定在内侧壁和外侧壁上 附接配件通过将每个所述配件的区域螺栓连接到所述侧壁而设置在所述室端壁的上游。 所述多个附接配件中的至少一个集成在固定到室端壁上的环中，并且包括多个成对的突出部，其在上游超过螺栓连接区域延伸，每对中的两个突出部沿周向设置在 并且在其上游端连接到在所述两个突片之间延伸的固定板的上游端，并且其具有用于固定到相邻侧壁的螺栓区。
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9.发明申请Mounting a turbine nozzle on a combustion chamber having CMC walls in a gas turbine 有权将涡轮喷嘴安装在燃气轮机中具有CMC壁的燃烧室上公开(公告)号：US20060010879A1
公开(公告)日：2006-01-19
申请号：US11153349
申请日：2005-06-16
IPC分类号： F23R3/42
CPC分类号： F01D9/044 , F01D9/023 , F05D2300/6033 , F23R3/60 , Y02T50/672 , Y02T50/675
摘要： The gas turbine comprises an annular combustion chamber having inner and outer walls made of ceramic matrix composite material, and a high pressure turbine nozzle secured to a downstream end of the combustion chamber and comprising a plurality of stationary airfoils extending between the inner and outer walls of an annular flow path through the nozzle for the gas stream coming from the combustion chamber. The turbine nozzle is made of ceramic matrix composite material and it is connected to the downstream end of the combustion chamber by brazing.
摘要翻译： 燃气轮机包括环形燃烧室，其具有由陶瓷基复合材料制成的内壁和外壁，以及固定到燃烧室下游端的高压涡轮喷嘴，并且包括多个固定翼型件，其在内壁和外壁之间延伸 通过喷嘴的环形流路，用于来自燃烧室的气流。 涡轮喷嘴由陶瓷基复合材料制成，并通过钎焊连接到燃烧室的下游端。
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10.发明授权Mounting a turbine nozzle on a combustion chamber having CMC walls in a gas turbine 有权将涡轮喷嘴安装在燃气轮机中具有CMC壁的燃烧室上公开(公告)号：US07249462B2
公开(公告)日：2007-07-31
申请号：US11153349
申请日：2005-06-16
IPC分类号： F23R3/60
CPC分类号： F01D9/044 , F01D9/023 , F05D2300/6033 , F23R3/60 , Y02T50/672 , Y02T50/675
摘要： The gas turbine comprises an annular combustion chamber having inner and outer walls made of ceramic matrix composite material, and a high pressure turbine nozzle secured to a downstream end of the combustion chamber and comprising a plurality of stationary airfoils extending between the inner and outer walls of an annular flow path through the nozzle for the gas stream coming from the combustion chamber. The turbine nozzle is made of ceramic matrix composite material and it is connected to the downstream end of the combustion chamber by brazing.
摘要翻译： 燃气轮机包括环形燃烧室，其具有由陶瓷基复合材料制成的内壁和外壁，以及固定到燃烧室下游端的高压涡轮喷嘴，并且包括多个固定翼型件，其在内壁和外壁之间延伸 通过喷嘴的环形流路，用于来自燃烧室的气流。 涡轮喷嘴由陶瓷基复合材料制成，并通过钎焊连接到燃烧室的下游端。
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