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公开(公告)号：US08021118B2
公开(公告)日：2011-09-20
申请号：US11974895
申请日：2007-10-16
申请人： Katharina Bergander , Georg Bostanjoglo , Tobias Buchal , Winfried Eβer , Dirk Goldschmidt , Torsten Koch , Rudolf Küperkoch , Thorsten Mattheis , Jan Münzer , Ralf Müsgen , Matthias Oechsner , Ursula Pickert , Volker Vosberg
发明人： Katharina Bergander , Georg Bostanjoglo , Tobias Buchal , Winfried Eβer , Dirk Goldschmidt , Torsten Koch , Rudolf Küperkoch , Thorsten Mattheis , Jan Münzer , Ralf Müsgen , Matthias Oechsner , Ursula Pickert , Volker Vosberg
IPC分类号： F01D5/14
CPC分类号： F01D25/12 , F01D5/18 , F05D2230/10 , F05D2230/21 , F05D2230/232 , F05D2230/238 , F05D2240/81 , F05D2260/36
摘要： A turbine blade for a turbine of a thermal power plant, with a platform for partial delimiting of a flow passage in the turbine, wherein the platform has at least one cooling medium passage, which extends inside the platform, for guiding a cooling medium, is characterized according to the invention in that the at least one cooling medium passage emerges from the platform at at least two connecting openings, and the turbine blade has at least one supplementary component which can be fastened on the platform, with a communicating passage, which is designed for interconnecting the connecting openings in a fluid-guiding manner.
摘要翻译： 一种用于火力发电厂的涡轮机的涡轮机叶片，具有用于部分限定涡轮机中的流动通道的平台，其中平台具有至少一个在平台内延伸以用于引导冷却介质的冷却介质通道，是 根据本发明的特征在于，至少一个冷却介质通道在至少两个连接开口处从平台排出，并且涡轮叶片具有可以紧固在平台上的至少一个辅助部件，连通通道 设计用于以流体引导方式互连连接开口。
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公开(公告)号：US08257032B2
公开(公告)日：2012-09-04
申请号：US12009314
申请日：2008-01-17
申请人： Alexander R. Beeck , Katharina Bergander , Georg Bostanjoglo , Tobias Buchal , Winfried Eβer , Dirk Goldschmidt , Torsten Koch , Rudolf Küperkoch , Thorsten Mattheis , Jan Münzer , Ralf Müsgen , Matthias Oechsner , Ursula Pickert , Volker Vosberg
发明人： Alexander R. Beeck , Katharina Bergander , Georg Bostanjoglo , Tobias Buchal , Winfried Eβer , Dirk Goldschmidt , Torsten Koch , Rudolf Küperkoch , Thorsten Mattheis , Jan Münzer , Ralf Müsgen , Matthias Oechsner , Ursula Pickert , Volker Vosberg
IPC分类号： F04D29/54
CPC分类号： F01D9/00 , F01D5/146 , F05D2240/301 , Y02T50/673
摘要： A guide vane for a gas turbine with a vane base body which is of single-piece design and comprises a profiled vane blade extending between a vane root and a cover plate and also the vane root formed integrally with the vane blade and the cover plate formed integrally with the vane blade, is intended, in a relatively simple way to be able to be matched to the individual conditions of use with especially little outlay on apparatus and logistics. For this purpose, according to the invention, a flow-routing body with an advance guide blade that is connected upstream of the vane blade as seen in the direction of flow of the working medium of the gas turbine is joined to the vane base body.
摘要翻译： 一种具有叶片基体的燃气轮机的导向叶片，其具有单件式设计，并且包括在叶片根部和盖板之间延伸的异型叶片叶片，以及与叶片和盖板一体形成的叶片根部 与叶片一体地，以相对简单的方式旨在能够与单独的使用条件匹配，特别是在设备和物流方面的特别少的费用。 为此，根据本发明，在叶片叶片的工作介质的流动方向上观察到连接在叶片叶片的上游的具有前进导向叶片的流动路线体与叶片基体接合。
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3.发明授权Stator blade segment of a thermal turbomachine, associated production method and also thermal turbomachine 失效热涡轮机的定子叶片段，相关的生产方法和热涡轮机公开(公告)号：US08128357B2
公开(公告)日：2012-03-06
申请号：US12225933
申请日：2007-02-21
申请人： Katharina Bergander , Georg Bostanjoglo , Tobias Buchal , Winfried Eβer , Dirk Goldschmidt , Torsten Koch , Rudolf Küperkoch , Thorsten Mattheis , Jan Münzer , Ralf Müsgen , Matthias Oechsner , Ursula Pickert , Volker Vosberg
发明人： Katharina Bergander , Georg Bostanjoglo , Tobias Buchal , Winfried Eβer , Dirk Goldschmidt , Torsten Koch , Rudolf Küperkoch , Thorsten Mattheis , Jan Münzer , Ralf Müsgen , Matthias Oechsner , Ursula Pickert , Volker Vosberg
IPC分类号： F04D29/44
CPC分类号： F01D9/042 , F01D25/246 , F05D2230/23 , F05D2230/238 , F05D2240/10 , F05D2240/80 , F05D2260/30 , Y10T29/49323
摘要： The invention relates to a guide blade segment of a thermal turbomachine, in particular a gas turbine, comprising a number of profiled blades which are arranged on a platform. A plurality of securing elements for securing the guide blade segment to an associated guide blade support are arranged on the side of the platform which is oriented away from the blade. The aim of the invention is to provide a guide blade segment which can be produced in a simple and economical manner avoiding casting problem areas enabling the guide blade segment to be attached in a particularly reliable and secure manner to the associated guide blade support. According to the invention, at least one section of at least one of the securing elements is a separately produced component which is rigidly connected to the platform or to an additional section of the securing element.
摘要翻译： 本发明涉及一种热涡轮机的导向叶片段，特别是燃气涡轮机，其包括布置在平台上的多个异型叶片。 用于将引导片段固定到相关联的引导叶片支撑件上的多个固定元件布置在平台的远离叶片的侧面上。 本发明的目的是提供一种可以以简单和经济的方式制造的导向叶片段，避免了铸造问题区域，使得导向叶片段以特别可靠和可靠的方式附接到相关联的导向叶片支撑件。 根据本发明，至少一个固定元件的至少一个部分是单独制造的部件，其刚性地连接到平台或固定元件的附加部分。
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公开(公告)号：US07832988B2
公开(公告)日：2010-11-16
申请号：US11807387
申请日：2007-05-29
申请人： Katharina Bergander , Georg Bostanjoglo , Tobias Buchal , Winfried Eβer , Dirk Goldschmidt , Torsten Koch , Rudolf Küperkoch , Thorsten Mattheis , Jan Münzer , Ralf Müsgen , Matthias Oechsner , Ursula Pickert , Volker Vosberg
发明人： Katharina Bergander , Georg Bostanjoglo , Tobias Buchal , Winfried Eβer , Dirk Goldschmidt , Torsten Koch , Rudolf Küperkoch , Thorsten Mattheis , Jan Münzer , Ralf Müsgen , Matthias Oechsner , Ursula Pickert , Volker Vosberg
IPC分类号： F01D5/18
CPC分类号： F01D5/20 , F01D5/147 , F05D2230/232
摘要： A turbine blade with an aerodynamically profiled blade leaf which is produced from two assembled shell elements is provided. The shell elements forming the suction-side and the pressure-side blade leaf wall have been assembled by a high-temperature and high-pressure bonding process. In the region of the blade leaf tip, a cramp is provided which hooks the two blade walls together with one another with a form fit.
摘要翻译： 提供了由两个组装的壳单元制成的具有空气动力学异型叶片叶片的涡轮叶片。 形成吸入侧和压力侧叶片叶片的壳单元已经通过高温高压粘合工艺组装。 在叶片叶尖的区域中，提供了将两个叶片壁彼此钩合在一起的抽筋。
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5.发明申请STATOR BLADE SEGMENT OF A THERMAL TURBOMACHINE, ASSOCIATED PRODUCTION METHOD AND ALSO THERMAL TURBOMACHINE 失效热涡轮机的定子叶片分段，相关的生产方法和热涡轮机公开(公告)号：US20090304503A1
公开(公告)日：2009-12-10
申请号：US12225933
申请日：2007-02-21
申请人： Katharina Bergander , Georg Bostanjoglo , Tobias Buchal , Winfried Esser , Dirk Goldschmidt , Torsten Koch , Rudolf Küperkoch , Thorsten Mattheis , Jan Münzer , Ralf Müsgen , Matthias Oechsner , Ursula Pickert , Volker Vosberg
发明人： Katharina Bergander , Georg Bostanjoglo , Tobias Buchal , Winfried Esser , Dirk Goldschmidt , Torsten Koch , Rudolf Küperkoch , Thorsten Mattheis , Jan Münzer , Ralf Müsgen , Matthias Oechsner , Ursula Pickert , Volker Vosberg
CPC分类号： F01D9/042 , F01D25/246 , F05D2230/23 , F05D2230/238 , F05D2240/10 , F05D2240/80 , F05D2260/30 , Y10T29/49323
摘要： The invention relates to a guide blade segment of a thermal turbomachine, in particular a gas turbine, comprising a number of profiled blades which are arranged on a platform. A plurality of securing elements for securing the guide blade segment to an associated guide blade support are arranged on the side of the platform which is oriented away from the blade. The aim of the invention is to provide a guide blade segment which can be produced in a simple and economical manner avoiding casting problem areas enabling the guide blade segment to be attached in a particularly reliable and secure manner to the associated guide blade support. According to the invention, at least one section of at least one of the securing elements is a separately produced component which is rigidly connected to the platform or to an additional section of the securing element.
摘要翻译： 本发明涉及一种热涡轮机的导向叶片段，特别是燃气涡轮机，其包括布置在平台上的多个异型叶片。 用于将引导片段固定到相关联的引导叶片支撑件上的多个固定元件布置在平台的远离叶片的侧面上。 本发明的目的是提供一种可以以简单和经济的方式制造的导向叶片段，避免了铸造问题区域，使得导向叶片段以特别可靠和可靠的方式附接到相关联的导向叶片支撑件。 根据本发明，至少一个固定元件的至少一个部分是单独制造的部件，其刚性地连接到平台或固定元件的附加部分。
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公开(公告)号：US20080267771A1
公开(公告)日：2008-10-30
申请号：US12009314
申请日：2008-01-17
申请人： Alexander R. Beeck , Katharina Bergander , Georg Bostanjoglo , Tobias Buchal , Winfried Esser , Dirk Goldschmidt , Torsten Koch , Rudolf Kuperkoch , Thorsten Mattheis , Jan Munzer , Ralf Musgen , Matthias Oechsner , Ursula Pickert , Volker Vosberg
发明人： Alexander R. Beeck , Katharina Bergander , Georg Bostanjoglo , Tobias Buchal , Winfried Esser , Dirk Goldschmidt , Torsten Koch , Rudolf Kuperkoch , Thorsten Mattheis , Jan Munzer , Ralf Musgen , Matthias Oechsner , Ursula Pickert , Volker Vosberg
IPC分类号： F01D1/02
CPC分类号： F01D9/00 , F01D5/146 , F05D2240/301 , Y02T50/673
摘要： A guide vane for a gas turbine with a vane base body which is of single-piece design and comprises a profiled vane blade extending between a vane root and a cover plate and also the vane root formed integrally with the vane blade and the cover plate formed integrally with the vane blade, is intended, in a relatively simple way to be able to be matched to the individual conditions of use with especially little outlay on apparatus and logistics. For this purpose, according to the invention, a flow-routing body with an advance guide blade that is connected upstream of the vane blade as seen in the direction of flow of the working medium of the gas turbine is joined to the vane base body.
摘要翻译： 一种具有叶片基体的燃气轮机的导向叶片，其具有单件式设计，并且包括在叶片根部和盖板之间延伸的异型叶片叶片，以及与叶片和盖板一体形成的叶片根部 与叶片一体地，以相对简单的方式旨在能够与单独的使用条件匹配，特别是在设备和物流方面的特别少的费用。 为此，根据本发明，在叶片叶片的工作介质的流动方向上观察到连接在叶片叶片的上游的具有前进导向叶片的流动路线体与叶片基体接合。
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公开(公告)号：US20100014980A1
公开(公告)日：2010-01-21
申请号：US11807387
申请日：2007-05-29
申请人： Katharina Bergander , Georg Bostanjoglo , Tobias Buchal , Winfried Esser , Dirk Goldschmidt , Torsten Koch , Rudolf Kuperkoch , Thorsten Mattheis , Jan Munzer , Ralf Musgen , Matthias Oechsner , Ursula Pickert , Volker Vosberg
发明人： Katharina Bergander , Georg Bostanjoglo , Tobias Buchal , Winfried Esser , Dirk Goldschmidt , Torsten Koch , Rudolf Kuperkoch , Thorsten Mattheis , Jan Munzer , Ralf Musgen , Matthias Oechsner , Ursula Pickert , Volker Vosberg
IPC分类号： F01D5/18
CPC分类号： F01D5/20 , F01D5/147 , F05D2230/232
摘要： There is described a turbine blade with an aerodynamically profiled blade leaf which is produced from two assembled shell elements. The shell elements forming the suction-side and the pressure-side blade leaf wall have been assembled by means of a high-temperature high-pressure bonding process and, under certain circumstances, may come apart at the blade tip. In order to prevent this, in the region of the blade leaf tip, a cramp is provided which hooks the two blade walls together with one another with a form fit.
摘要翻译： 描述了具有由两个组装的壳元件制成的具有空气动力学异型叶片叶片的涡轮机叶片。 形成吸入侧和压力侧叶片叶壁的壳单元已经通过高温高压接合工艺组装，并且在某些情况下可能在叶片尖端处分离。 为了防止这种情况，在叶片叶尖的区域中，设置有将两个叶片壁彼此钩合在一起的抽筋。
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公开(公告)号：US20080240927A1
公开(公告)日：2008-10-02
申请号：US11974895
申请日：2007-10-16
申请人： Katharina Bergander , Georg Bostanjoglo , Tobias Buchal , Winfried Esser , Dirk Goldschmidt , Torsten Koch , Rudolf Kuperkoch , Thorsten Mattheis , Jan Munzer , Ralf Musgen , Matthias Oechsner , Ursula Pickert , Volker Vosberg
发明人： Katharina Bergander , Georg Bostanjoglo , Tobias Buchal , Winfried Esser , Dirk Goldschmidt , Torsten Koch , Rudolf Kuperkoch , Thorsten Mattheis , Jan Munzer , Ralf Musgen , Matthias Oechsner , Ursula Pickert , Volker Vosberg
CPC分类号： F01D25/12 , F01D5/18 , F05D2230/10 , F05D2230/21 , F05D2230/232 , F05D2230/238 , F05D2240/81 , F05D2260/36
摘要： A turbine blade for a turbine of a thermal power plant, with a platform for partial delimiting of a flow passage in the turbine, wherein the platform has at least one cooling medium passage, which extends inside the platform, for guiding a cooling medium, is characterized according to the invention in that the at least one cooling medium passage emerges from the platform at at least two connecting openings, and the turbine blade has at least one supplementary component which can be fastened on the platform, with a communicating passage, which is designed for interconnecting the connecting openings in a fluid-guiding manner.
摘要翻译： 一种用于火力发电厂的涡轮机的涡轮机叶片，具有用于部分限定涡轮机中的流动通道的平台，其中平台具有至少一个在平台内延伸以用于引导冷却介质的冷却介质通道，是 根据本发明的特征在于，至少一个冷却介质通道在至少两个连接开口处从平台排出，并且涡轮叶片具有可以紧固在平台上的至少一个辅助部件，连通通道 设计用于以流体引导方式互连连接开口。
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公开(公告)号：US08437010B2
公开(公告)日：2013-05-07
申请号：US13502787
申请日：2010-10-13
IPC分类号： G01B11/24
CPC分类号： G01B11/24 , F01D5/005 , F01D5/186 , F23R2900/00019 , Y02T50/67 , Y02T50/676
摘要： A process for determining the position of closed holes in a component is provided. By carrying out laser triangulation measurements on an uncoated component and a coated component with holes, the exact position of the holes to be reopened may be detected following the coating. A device used to carry out this process is also provided.
摘要翻译： 提供了用于确定部件中的闭孔的位置的方法。 通过对未涂覆的部件和带有孔的涂层部件进行激光三角测量，可以在涂层之后检测要重新打开的孔的确切位置。 还提供了用于执行该过程的装置。
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公开(公告)号：US08186056B2
公开(公告)日：2012-05-29
申请号：US11823767
申请日：2007-06-28
申请人： Robert S. Willis , Scott P. Irwin , Stacy Fang , Thomas H. Milidantri, Jr. , Adam J. Taetsch , Martin C. Gosling , Georg Bostanjoglo , Dan Shipman , Orville Morgan , Gerry Milidantri
发明人： Robert S. Willis , Scott P. Irwin , Stacy Fang , Thomas H. Milidantri, Jr. , Adam J. Taetsch , Martin C. Gosling , Georg Bostanjoglo , Dan Shipman , Orville Morgan , Gerry Milidantri
IPC分类号： B23P6/00
CPC分类号： B23P6/002 , F01D5/005 , F05D2230/80 , Y10T29/49318 , Y10T29/4975
摘要： A system and method for reconfiguring a turbine vane. In at least one embodiment, the system may be used to straighten an airfoil of a turbine vane segment to remove lean, twist, or racking, or any combination thereof. The airfoil may be straightened by fixing portions of the forward and aft hooks of the inner and outer shrouds of the turbine vane, restricting other portions of the forward and aft hooks of the inner and outer shrouds of the turbine vane to only move rotationally about a centerline of the inner or outer shrouds, and applying a load to various portions of the inner and outer shrouds and the airfoil to return the turbine vane to be within predetermined specifications.
摘要翻译： 一种用于重新配置涡轮叶片的系统和方法。 在至少一个实施例中，该系统可以用于矫直涡轮叶片段的翼型件以去除倾斜，扭转或翻倒，或其任何组合。 翼片可以通过固定涡轮叶片的内护罩和外护罩的前钩和后钩的部分而被拉直，限制涡轮叶片的内护罩和外护罩的前钩和后钩的其它部分仅仅围绕涡轮叶片旋转移动 内部或外部护罩的中心线，并且将负载施加到内部和外部护罩和翼型件的各个部分以将涡轮叶片返回到预定规格内。
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