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公开(公告)号：US08079803B2
公开(公告)日：2011-12-20
申请号：US12164793
申请日：2008-06-30
申请人： Keita Takamura , Shinya Hashimoto , Masanori Yuri
发明人： Keita Takamura , Shinya Hashimoto , Masanori Yuri
摘要： The present invention includes an introducing passage that is provided within a turbine stationary blade fixed within a turbine casing and that communicates an interior of the turbine casing with an exterior thereof; a nozzle that is provided in an inner circumference of the turbine stationary blade in a manner that the nozzle communicates with the introducing passage and that includes an outlet facing the opening of the rotor cavity and a swirler at the outlet; and a pressurizing passage that communicates a cooling passage with a rotor cavity. In this arrangement, the outlet of the nozzle and the connecting opening of the pressurizing passage are arranged so that distances of the outlet and of the connecting opening from the central axis line in the radial direction of the rotor are the same distance r.
摘要翻译： 本发明包括一个引入通道，其设置在固定在涡轮机壳体内的涡轮机固定叶片内，并将涡轮机壳体的内部与其外部连通; 喷嘴，其以所述喷嘴与所述引导通道连通并且包括面向所述转子腔的开口的出口和所述出口处的旋流器的方式设置在所述涡轮静止叶片的内周中; 以及将冷却通路与转子腔连通的加压通路。 在这种布置中，喷嘴的出口和加压通道的连接开口被布置成使得出口和连接开口在转子的径向方向上与中心轴线的距离是相同的距离r。
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公开(公告)号：US20090324388A1
公开(公告)日：2009-12-31
申请号：US12164793
申请日：2008-06-30
申请人： Keita TAKAMURA , Shinya HASHIMOTO , Masanori YURI
发明人： Keita TAKAMURA , Shinya HASHIMOTO , Masanori YURI
摘要： The present invention includes an introducing passage that is provided within a turbine stationary blade fixed within a turbine casing and that communicates an interior of the turbine casing with an exterior thereof; a nozzle that is provided in an inner circumference of the turbine stationary blade in a manner that the nozzle communicates with the introducing passage and that includes an outlet facing the opening of the rotor cavity and a swirler at the outlet; and a pressurizing passage that communicates a cooling passage with a rotor cavity. In this arrangement, the outlet of the nozzle and the connecting opening of the pressurizing passage are arranged so that distances of the outlet and of the connecting opening from the central axis line in the radial direction of the rotor are the same distance r.
摘要翻译： 本发明包括一个引入通道，其设置在固定在涡轮机壳体内的涡轮机固定叶片内，并将涡轮机壳体的内部与其外部连通; 喷嘴，其以所述喷嘴与所述引导通道连通并且包括面向所述转子腔的开口的出口和所述出口处的旋流器的方式设置在所述涡轮静止叶片的内周中; 以及将冷却通路与转子腔连通的加压通路。 在这种布置中，喷嘴的出口和加压通道的连接开口被布置成使得出口和连接开口在转子的径向方向上与中心轴线的距离是相同的距离r。
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公开(公告)号：US07198463B2
公开(公告)日：2007-04-03
申请号：US11020182
申请日：2004-12-27
CPC分类号： F01D5/081 , F01D5/3007 , Y02T50/671 , Y02T50/676 , Y10S416/50
摘要： Such a rotating blade body is supplied as can prevent not only local wear and deformation but also inadvertent vibration and can maintain cooling efficiency. A rotating blade body consists of a rotor disc 2 and rotating blades 1 which are assembled so as to extend from the outer circumference of the rotor disc 2 in a radial pattern, wherein blade root portions 10 of the rotating blades 1 are engaged into blade grooves 20 which are formed along a direction of a rotating shaft on an edge of the outer circumference of the rotor disc 2. Circulation spaces 25 for the cooling air are formed along the direction of a rotating shaft between the bottom-end portions 10a of the blade root portions 10 and the bottom portions 20a of the blade grooves 20. Pushing-up members 3 which push up the rotating blades 1 outward in a radial direction are inserted into the circulation spaces 25, maintaining circulation of the cooling air.
摘要翻译： 供应这样的旋转叶片体不仅可以防止局部磨损和变形，而且可以避免无意的振动，并且可以保持冷却效率。 旋转叶片体由转子盘2和旋转叶片1构成，转子盘2以旋转叶片1的外圆周方向延伸组装，其中旋转叶片1的叶根部10与叶片槽 20是沿转子盘2的外周边缘上的旋转轴的方向形成的。冷却空气的循环空间25沿着旋转轴的方向形成在底部部分10a的底端部分10a之间 叶片根部10和叶片槽20的底部部分20a。 将旋转叶片1向径向推出的推出构件3插入到循环空间25中，保持冷却空气的循环。
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公开(公告)号：US20050207892A1
公开(公告)日：2005-09-22
申请号：US11020182
申请日：2004-12-27
CPC分类号： F01D5/081 , F01D5/3007 , Y02T50/671 , Y02T50/676 , Y10S416/50
摘要： Such a rotating blade body is supplied as can prevent not only local wear and deformation but also inadvertent vibration and can maintain cooling efficiency. A rotating blade body consists of a rotor disc 2 and rotating blades 1 which are assembled so as to extend from the outer circumference of the rotor disc 2 in a radial pattern, wherein blade root portions 10 of the rotating blades 1 are engaged into blade grooves 20 which are formed along a direction of a rotating shaft on an edge of the outer circumference of the rotor disc 2. Circulation spaces 25 for the cooling air are formed along the direction of a rotating shaft between the bottom-end portions 10a of the blade root portions 10 and the bottom portions 20a of the blade grooves 20. Pushing-up members 3 which push up the rotating blades 1 outward in a radial direction are inserted into the circulation spaces 25, maintaining circulation of the cooling air.
摘要翻译： 供应这样的旋转叶片体不仅可以防止局部磨损和变形，而且可以防止无意的振动，并且可以保持冷却效率。 旋转叶片体由转子盘2和旋转叶片1构成，转子盘2以旋转叶片1的外圆周方向延伸组装，其中旋转叶片1的叶根部10与叶片槽 20是沿转子盘2的外周边缘上的旋转轴的方向形成的。冷却空气的循环空间25沿着旋转轴的方向形成在底部部分10a的底端部分10a之间 叶片根部10和叶片槽20的底部部分20a。将旋转叶片1沿径向向外推的推出构件3插入到循环空间25中，保持冷却空气的循环。
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公开(公告)号：US20090324386A1
公开(公告)日：2009-12-31
申请号：US12164786
申请日：2008-06-30
申请人： Keita Takamura , Shinya Hashimoto , Masanori Yuri
发明人： Keita Takamura , Shinya Hashimoto , Masanori Yuri
IPC分类号： F02C7/141
CPC分类号： F02C7/141 , F01D5/085 , F01D5/087 , F05D2240/12 , F05D2240/61 , F05D2260/20
摘要： A gas turbine includes a shaft directional passage provided to a rotating member that rotates along a central axis of a rotor, which is a rotating axis of the rotating member, about the central axis, or a rotating axis of the rotating member, and in which cooling air flows along a direction of the rotating axis of the rotor, a plurality of radial directional passages provided in a circumferential direction of the rotating member, and compressing the cooling air by being provided outwardly from the center of the rotor, in which one end of each of the radial directional passages is communicated with the shaft directional passage and the other end is communicated with exterior of the rotating member.
摘要翻译： 燃气轮机包括轴向通道，其设置在旋转部件上，该旋转部件沿着作为旋转部件的旋转轴线的转子的中心轴线，绕中心轴线或旋转部件的旋转轴线旋转， 冷却空气沿着转子的旋转轴线的方向流动，多个径向通路设置在旋转构件的圆周方向上，并且通过从转子的中心向外设置来压缩冷却空气，其中一端 每个径向通路与轴定向通道连通，另一端与旋转构件的外部连通。
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公开(公告)号：US08079802B2
公开(公告)日：2011-12-20
申请号：US12164786
申请日：2008-06-30
申请人： Keita Takamura , Shinya Hashimoto , Masanori Yuri
发明人： Keita Takamura , Shinya Hashimoto , Masanori Yuri
CPC分类号： F02C7/141 , F01D5/085 , F01D5/087 , F05D2240/12 , F05D2240/61 , F05D2260/20
摘要： A gas turbine includes a shaft directional passage provided to a rotating member that rotates along a central axis of a rotor, which is a rotating axis of the rotating member, about the central axis, or a rotating axis of the rotating member, and in which cooling air flows along a direction of the rotating axis of the rotor, a plurality of radial directional passages provided in a circumferential direction of the rotating member, and compressing the cooling air by being provided outwardly from the center of the rotor, in which one end of each of the radial directional passages is communicated with the shaft directional passage and the other end is communicated with exterior of the rotating member.
摘要翻译： 燃气轮机包括轴向通道，其设置在旋转部件上，该旋转部件沿着作为旋转部件的旋转轴线的转子的中心轴线，绕中心轴线或旋转部件的旋转轴线旋转， 冷却空气沿着转子的旋转轴线的方向流动，多个径向通路设置在旋转构件的圆周方向上，并且通过从转子的中心向外设置来压缩冷却空气，其中一端 每个径向通路与轴定向通道连通，另一端与旋转构件的外部连通。
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