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1.发明授权Process for treating a coated gas turbine part, and coated gas turbine part 有权用于处理涂覆的燃气轮机部件和涂覆的燃气轮机部件的方法公开(公告)号：US06773753B2
公开(公告)日：2004-08-10
申请号：US10211352
申请日：2002-08-05
申请人： Gordon Anderson , Reinhard Fried , Michael Loetzerich , Markus Oehl , Stefan Schlechtriem , Joerg Stengele
发明人： Gordon Anderson , Reinhard Fried , Michael Loetzerich , Markus Oehl , Stefan Schlechtriem , Joerg Stengele
IPC分类号： B32B1500
CPC分类号： F01D5/288 , F01D5/145 , F01D5/286 , F05D2230/10 , F05D2230/90 , F05D2250/60 , F05D2250/62 , F05D2250/621 , F05D2260/221 , F05D2260/2214 , F05D2300/2118 , F05D2300/611 , Y10T428/12451 , Y10T428/24355 , Y10T428/24942 , Y10T428/31
摘要： The invention discloses a process for treating a ceramic protective layer (3) which is applied to the surface (2) of a gas turbine part (1). The roughness of the ceramic protective layer (3) is reduced at at least one first location (5), and the original roughness is retained at at least one second location (6). The roughness is advantageously retained at locations (6) on a turbine blade or vane (1) which are at risk of detachment, while the roughness of the remaining surface (2) is reduced in order to reduce the heat transfer to the surrounding hot-gas flow.
摘要翻译： 本发明公开了一种处理燃气轮机部件（1）的表面（2）的陶瓷保护层（3）的处理方法。 陶瓷保护层（3）的粗糙度在至少一个第一位置（5）处减小，并且原始粗糙度保持在至少一个第二位置（6）。 有利地，粗糙度保持在涡轮叶片或叶片（1）上的位于有分离风险的位置（6）处，同时减少了剩余表面（2）的粗糙度，以便减少向周围热交换器 气流。
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公开(公告)号：US07311741B2
公开(公告)日：2007-12-25
申请号：US10495227
申请日：2002-11-08
IPC分类号： B01D45/12
CPC分类号： B01D45/16 , B01D50/002
摘要： The invention describes a device for separating dust and dirt out of flowing media. A curved flow path (1) is imposed on the flow (21), and heavy foreign bodies are separated out of the main flow by centrifugal force. The partial stream required to carry away the foreign bodies is aftertreated in a filter (11) and returned in purified form. Unlike with conventional filters, which have to process the entire flow of media, pressure losses during the separation of dust are minimized, and on the other hand no medium is lost for removing the dust load.
摘要翻译： 本发明描述了一种用于从流动介质中分离灰尘和污垢的装置。 在流动（21）上施加弯曲的流动路径（1），并且通过离心力将重的异物分离出主流体。 携带异物所需的部分流在过滤器（11）中进行后处理，并以纯化的形式返回。 与必须处理整个介质流的常规过滤器不同，在分离灰尘期间的压力损失最小化，另一方面不会丢失用于去除灰尘负载的介质。
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公开(公告)号：US20050076622A1
公开(公告)日：2005-04-14
申请号：US10495227
申请日：2002-11-08
CPC分类号： B01D45/16 , B01D50/002
摘要： The invention describes a device for separating dust and dirt out of flowing media. A curved flow path (1) is imposed on the flow (21), and heavy foreign bodies are separated out of the main flow by centrifugal force. The partial stream required to carry away the foreign bodies is aftertreated in a filter (11) and returned in purified form. Unlike with conventional filters, which have to process the entire flow of media, pressure losses during the separation of dust are minimized, and on the other hand no medium is lost for removing the dust load.
摘要翻译： 本发明描述了一种用于从流动介质中分离灰尘和污垢的装置。 在流动（21）上施加弯曲的流动路径（1），并且通过离心力将重的异物分离出主流体。 携带异物所需的部分流在过滤器（11）中进行后处理，并以纯化的形式返回。 与必须处理整个介质流的常规过滤器不同，在分离灰尘期间的压力损失最小化，另一方面不会丢失用于去除灰尘负载的介质。
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公开(公告)号：US07264445B2
公开(公告)日：2007-09-04
申请号：US11330268
申请日：2006-01-12
申请人： Shailandra Naik , Sacha Parneix , Ulrich Rathmann , Helene Saxer-Felici , Stefan Schlechtriem , Beat Von Arx
发明人： Shailandra Naik , Sacha Parneix , Ulrich Rathmann , Helene Saxer-Felici , Stefan Schlechtriem , Beat Von Arx
IPC分类号： F01D5/18
CPC分类号： F01D5/187 , F01D25/12 , F05D2250/185 , F05D2260/211
摘要： A cooled blade or vane for a gas turbine has a main blade or vane part which starts from a blade or vane root and a blade or vane shank and has a leading edge and a trailing edge, as well as, inside the main blade or vane part, a plurality of cooling ducts, which extend in the radial direction, are connected in series in terms of flow and of which a first cooling duct has a main stream of a cooling medium flowing through it along the leading edge. A second cooling duct has a main stream of a cooling medium flowing through it along the trailing edge, from the blade or vane root to the tip of the main blade or vane part. The outlet of the first cooling duct is in communication, via a first diverting region, a third cooling duct arranged between the first and second cooling ducts, and a second diverting region, with the inlet of the second cooling duct.
摘要翻译： 用于燃气轮机的冷却的叶片或叶片具有从叶片或叶片根部以及叶片或叶片柄开始并具有前缘和后缘以及主叶片或叶片内的主叶片或叶片部分 部分，沿径向方向延伸的多个冷却管道以流动方式串联连接，并且第一冷却管道具有沿着前缘流过其中的冷却介质的主流。 第二冷却管道具有沿着后缘从叶片或叶片根部流到主叶片或叶片部分的尖端的冷却介质的主流。 第一冷却管道的出口经由第一转向区域与布置在第一和第二冷却管道之间的第三冷却管道与第二冷却管道的入口与第二转向区域连通。
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公开(公告)号：US20060292006A1
公开(公告)日：2006-12-28
申请号：US11483091
申请日：2006-07-10
申请人： Shailandra Naik , Sacha Parneix , Ulrich Rathmann , Helene Saxer-Felici , Stefan Schlechtriem , Beat Von Arx
发明人： Shailandra Naik , Sacha Parneix , Ulrich Rathmann , Helene Saxer-Felici , Stefan Schlechtriem , Beat Von Arx
IPC分类号： F01D5/18
CPC分类号： F01D5/187 , F01D5/081 , F05D2250/50 , F05D2260/205 , F05D2260/221
摘要： A cooled blade for a gas turbine has a blade airfoil, which emerges from a blade root and a blade shank and has a leading edge and a trailing edge and, within the blade airfoil, a plurality of sequential coolant ducts, in terms of flow, extending in a radial direction. A first coolant duct along the leading edge, and a second coolant duct along the trailing edge, have a main flow of a coolant flowing through them from the blade root to the tip of the blade airfoil. An inlet of the first coolant duct is in connection with a main coolant inlet, and an outlet of the first coolant duct is in connection with the inlet to the second coolant duct via a first deflection region. A third coolant duct is arranged between the first and the second coolant duct and a second deflection region. An additional flow of cooler coolant provided from outside is added from the third coolant duct into the heated main flow of the coolant flowing into the second coolant duct. An orifice can, for example, extend from the main coolant inlet to the second deflection region.
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公开(公告)号：US07520724B2
公开(公告)日：2009-04-21
申请号：US11483091
申请日：2006-07-10
申请人： Shailandra Naik , Sacha Parneix , Ulrich Rathmann , Helene Saxer-Felici , Stefan Schlechtriem , Beat Von Arx
发明人： Shailandra Naik , Sacha Parneix , Ulrich Rathmann , Helene Saxer-Felici , Stefan Schlechtriem , Beat Von Arx
IPC分类号： F01D5/18
CPC分类号： F01D5/187 , F01D5/081 , F05D2250/50 , F05D2260/205 , F05D2260/221
摘要： A cooled blade for a gas turbine has a blade airfoil, which emerges from a blade root and a blade shank and has a leading edge and a trailing edge and, within the blade airfoil, a plurality of sequential coolant ducts, in terms of flow, extending in a radial direction. A first coolant duct along the leading edge, and a second coolant duct along the trailing edge, have a main flow of a coolant flowing through them from the blade root to the tip of the blade airfoil. An inlet of the first coolant duct is in connection with a main coolant inlet, and an outlet of the first coolant duct is in connection with the inlet to the second coolant duct via a first deflection region. A third coolant duct is arranged between the first and the second coolant duct and a second deflection region. An additional flow of cooler coolant provided from outside is added from the third coolant duct into the heated main flow of the coolant flowing into the second coolant duct. An orifice can, for example, extend from the main coolant inlet to the second deflection region.
摘要翻译： 用于燃气涡轮机的冷却叶片具有叶片翼型件，叶片翼型件从叶片根部和叶片柄部突出并且具有前缘和后缘，并且在叶片翼型件内，在流动方面，多个顺序的冷却剂管道， 沿径向延伸。 沿着前缘的第一冷却剂管道和沿着后缘的第二冷却剂管道具有从叶片根部到叶片翼型的尖端流过它们的冷却剂的主流。 第一冷却剂管道的入口与主冷却剂入口连接，并且第一冷却剂管道的出口经由第一偏转区域与第二冷却剂管道的入口连接。 第三冷却剂管道布置在第一和第二冷却剂管道和第二偏转区域之间。 从外部提供的另外冷却剂冷却流从第三冷却剂管道加入流入第二冷却剂管道的冷却剂的加热主流。 孔可以例如从主冷却剂入口延伸到第二偏转区域。
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公开(公告)号：US09435213B2
公开(公告)日：2016-09-06
申请号：US12701852
申请日：2010-02-08
CPC分类号： F01D5/3007 , F01D11/005 , F05D2240/55 , F05D2250/13 , F05D2250/182 , Y10T29/49316
摘要： A method is described for improving the sealing between rotor and a plurality of blades. The rotor has a plurality of generally axially extending profiled recesses into which a ring of blades, which have corresponding blade root profiles, are inserted in a form-fitting and/or frictionally locking manner into these recesses in a generally axial insertion direction. Between the recesses the rotor has tangential surface sections or circumferential surface sections which extend in the axial direction and circumferential direction and are generally indirectly covered by lower shrouds of circumferentially adjacently arranged blades in the radial direction. At least one of the tangential surface or circumferential surface sections is provided with a step in the radial direction, and a corresponding recess, which adjoins as flush as possible, is provided in the underside of the shroud of the blade which is arranged above it. Corresponding rotors or blades are also described.
摘要翻译： 描述了一种用于改善转子和多个叶片之间的密封的方法。 转子具有多个大致轴向延伸的成型凹槽，具有对应的叶片根部轮廓的叶片环以大致轴向的插入方向以形状配合和/或摩擦锁定的方式插入到该凹槽中。 在凹部之间，转子具有在轴向和圆周方向上延伸的切向表面部分或圆周表面部分，并且在径向方向上通常间接地被周向相邻布置的叶片的下部护罩覆盖。 切向表面或周向表面部分中的至少一个在径向方向上设置有台阶，并且在其上方布置有叶片的护罩的下侧设置相应的凹陷，该凹槽邻近齐平。 还描述了相应的转子或叶片。
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公开(公告)号：US20060177310A1
公开(公告)日：2006-08-10
申请号：US11330268
申请日：2006-01-12
申请人： Shailendra Naik , Sacha Parneix , Ulrich Rathmann , Helene Saxer-Felici , Stefan Schlechtriem , Beat Von Arx
发明人： Shailendra Naik , Sacha Parneix , Ulrich Rathmann , Helene Saxer-Felici , Stefan Schlechtriem , Beat Von Arx
IPC分类号： F01D5/18
CPC分类号： F01D5/187 , F01D25/12 , F05D2250/185 , F05D2260/211
摘要： A cooled blade or vane for a gas turbine has a main blade or vane part which starts from a blade or vane root and a blade or vane shank and has a leading edge and a trailing edge, as well as, inside the main blade or vane part, a plurality of cooling ducts, which extend in the radial direction, are connected in series in terms of flow and of which a first cooling duct has a main stream of a cooling medium flowing through it along the leading edge. A second cooling duct has a main stream of a cooling medium flowing through it along the trailing edge, from the blade or vane root to the tip of the main blade or vane part. The outlet of the first cooling duct is in communication, via a first diverting region, a third cooling duct arranged between the first and second cooling ducts, and a second diverting region, with the inlet of the second cooling duct.
摘要翻译： 用于燃气轮机的冷却的叶片或叶片具有从叶片或叶片根部以及叶片或叶片柄开始并具有前缘和后缘以及主叶片或叶片内的主叶片或叶片部分 部分，沿径向方向延伸的多个冷却管道以流动方式串联连接，并且第一冷却管道具有沿着前缘流过其中的冷却介质的主流。 第二冷却管道具有沿着后缘从叶片或叶片根部流到主叶片或叶片部分的尖端的冷却介质的主流。 第一冷却管道的出口经由第一转向区域与布置在第一和第二冷却管道之间的第三冷却管道与第二冷却管道的入口与第二转向区域连通。
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公开(公告)号：US06358003B2
公开(公告)日：2002-03-19
申请号：US09424481
申请日：2000-03-03
申请人： Stefan Schlechtriem
发明人： Stefan Schlechtriem
IPC分类号： F01D514
CPC分类号： F01D5/141 , F04D29/324 , F05D2250/713 , Y02T50/673
摘要： A rotor blade airfoil of an axial-flow turbomachine, for a fan or a compressor high-pressure stage of a gas turbine system, configured in the tip area to improve supersonic performance. The blade afflux edge has a forward-back sweep. The tip region of the blade efflux edge can be designed essentially similar to the blade afflux edge, with the tip region extending across the outer 15% to 25% of the blade span.
摘要翻译： 轴流式涡轮机的转子叶片翼型，用于燃气轮机系统的风扇或压缩机高压级，配置在尖端区域以改善超音速性能。 叶片的边缘具有前后扫描。 叶片排出边缘的尖端区域可以被设计成基本上类似于叶片边缘边缘，其中尖端区域延伸跨越叶片跨度的外部15％至25％。
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