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公开(公告)号:US08870526B2
公开(公告)日:2014-10-28
申请号:US13127295
申请日:2009-09-10
申请人: Roderich Bryk , Sascha Dungs , Martin Hartmann , Uwe Kahlstorf , Karl Klein , Oliver Lüsebrink , Mirko Milazar , Nicolas Savilius , Oliver Schneider , Shilun Sheng , Vadim Shevchenko , Gerhard Simon , Norbert Thamm
发明人: Roderich Bryk , Sascha Dungs , Martin Hartmann , Uwe Kahlstorf , Karl Klein , Oliver Lüsebrink , Mirko Milazar , Nicolas Savilius , Oliver Schneider , Shilun Sheng , Vadim Shevchenko , Gerhard Simon , Norbert Thamm
CPC分类号: F01D9/041 , F01D25/246
摘要: A stator blade carrier for a gas turbine is provided. The stator blade carrier includes a plurality of axial segments. At least one axial segment is designed as a tubular lattice structure. This allows a simpler design technically and a more flexible adaptation to the temperature profile present on the stator blade carrier to maintain operational safety.
摘要翻译: 提供了一种用于燃气轮机的定子叶片载体。 定子叶片载体包括多个轴向段。 至少一个轴向段被设计为管状晶格结构。 这允许在技术上更简单的设计和更灵活地适应定子叶片载体上存在的温度分布,以保持操作安全性。
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公开(公告)号:US20110268580A1
公开(公告)日:2011-11-03
申请号:US13127295
申请日:2009-09-10
申请人: Roderich Bryk , Sascha Dungs , Martin Hartmann , Uwe Kahlstorf , Karl Klein , Oliver Lüsebrink , Mirko Milazar , Nicolas Savilius , Oliver Schneider , Shilun Sheng , Vadim Shevchenko , Gerhard Simon , Norbert Thamm
发明人: Roderich Bryk , Sascha Dungs , Martin Hartmann , Uwe Kahlstorf , Karl Klein , Oliver Lüsebrink , Mirko Milazar , Nicolas Savilius , Oliver Schneider , Shilun Sheng , Vadim Shevchenko , Gerhard Simon , Norbert Thamm
IPC分类号: F04D29/00
CPC分类号: F01D9/041 , F01D25/246
摘要: A stator blade carrier for a gas turbine is provided. The stator blade carrier includes a plurality of axial segments. At least one axial segment is designed as a tubular lattice structure. This allows a simpler design technically and a more flexible adaptation to the temperature profile present on the stator blade carrier to maintain operational safety.
摘要翻译: 提供了一种用于燃气轮机的定子叶片载体。 定子叶片载体包括多个轴向段。 至少一个轴向段被设计为管状晶格结构。 这允许在技术上更简单的设计和更灵活地适应定子叶片载体上存在的温度分布,以保持操作安全性。
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公开(公告)号:US20120107136A1
公开(公告)日:2012-05-03
申请号:US13258011
申请日:2010-03-25
申请人: Tobias Buchal , Sascha Dungs , Winfried Esser , Birgit Grüger , Oliver Lüsebrink , Mirko Milazar , Nicolas Savilius , Oliver Schneider , Peter Schröder , Waldemar Socha
发明人: Tobias Buchal , Sascha Dungs , Winfried Esser , Birgit Grüger , Oliver Lüsebrink , Mirko Milazar , Nicolas Savilius , Oliver Schneider , Peter Schröder , Waldemar Socha
IPC分类号: F01D5/08
CPC分类号: F01D5/3015 , F01D11/005 , F05D2230/232
摘要: A rotor blade system, for example, of a gas turbine is provided. The rotor blade system includes a plurality of rotor blades which are arranged annularly on a rotor disk. A plurality of sealing plates are arranged on a side surface of the rotor disk. An individual sealing plate is formed from a plurality of metal sheets, wherein two of the metal sheets are arranged opposite each other a distance apart and parallel to a plane of the sealing plate, forming a gap for guiding of cooling air.
摘要翻译: 提供了例如燃气轮机的转子叶片系统。 转子叶片系统包括环形地设置在转子盘上的多个转子叶片。 多个密封板设置在转子盘的侧面上。 单个密封板由多个金属板形成,其中两个金属板彼此相隔布置并平行于密封板的平面,形成用于引导冷却空气的间隙。
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4.
公开(公告)号:US20120118524A1
公开(公告)日:2012-05-17
申请号:US13275460
申请日:2011-10-18
申请人: Fathi Ahmad , Winfried Esser , Giuseppe Gaio , Waldemar Heckel , Rudolf Küperkoch , Oliver Lüsebrink , Thorsten Mattheis , Mirko Milazar , Artur Mol , Uwe Paul , Oliver Ricken , Oliver Schneider
发明人: Fathi Ahmad , Winfried Esser , Giuseppe Gaio , Waldemar Heckel , Rudolf Küperkoch , Oliver Lüsebrink , Thorsten Mattheis , Mirko Milazar , Artur Mol , Uwe Paul , Oliver Ricken , Oliver Schneider
CPC分类号: B22C7/06 , B22C9/10 , Y10T29/49716
摘要: A core die is provided. The core die includes a first half and a second half where a cavity is formed between the two. Pins are arranged on the halves and the pins are replaceable. By virtue of the modular inner structure of a core die, the core die may be matched to the desired changes of the core, by small changes, more quickly and more easily than would be the case if the core die had only one part or if the pins were a fixed component of the core die halves.
摘要翻译: 提供一个核心模具。 芯模具包括在两者之间形成空腔的第一半和第二半部。 引脚布置在一半上,引脚是可更换的。 由于芯模的模块化内部结构,芯模可以通过小的变化与芯的期望变化相匹配,比如果芯模只有一个部分或如果 销钉是芯半模的固定部件。
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5.
公开(公告)号:US09188015B2
公开(公告)日:2015-11-17
申请号:US12437075
申请日:2009-05-07
申请人: Fathi Ahmad , Stefan Krause , Oliver Lüsebrink
发明人: Fathi Ahmad , Stefan Krause , Oliver Lüsebrink
CPC分类号: F01D5/286 , B22D27/045 , B23P15/02 , C22C19/05 , C22F1/10 , F05D2240/121 , F05D2240/303 , F05D2300/606 , Y02T50/67 , Y10T428/24074
摘要: A component, designed so that the longitudinal grain which experiences the greatest stress has a larger grain width than the other grains, is provided. This longitudinal grain is usually on the edge of the component. The component includes longitudinal grains that are directionally solidified in a rod-crystalline form along the longitudinal axis of the component.
摘要翻译: 提供了一种被设计成使得经受最大应力的纵向颗粒具有比其它颗粒更大的晶粒宽度的部件。 该纵向颗粒通常位于组件的边缘上。 该组件包括纵向晶粒,其沿组件的纵轴以杆状晶体形式定向凝固。
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公开(公告)号:US20110293431A1
公开(公告)日:2011-12-01
申请号:US13145441
申请日:2010-01-08
申请人: Harald Harders , Oliver Lüsebrink
发明人: Harald Harders , Oliver Lüsebrink
CPC分类号: B22D27/045 , C30B29/52 , F01D5/147 , F05D2240/80 , F05D2300/607 , Y02T50/67
摘要: Single-crystalline or stem-shaped turbine blades are difficult to produce. A turbine blade is provided which has varying structures for different areas of the turbine blade, wherein the airfoil region always includes a stem-shaped or single crystalline structure and the other regions may deviate therefrom. A method for producing the turbine blade is also provided.
摘要翻译: 单晶或茎状涡轮叶片难以生产。 提供了一种涡轮机叶片,其具有用于涡轮机叶片的不同区域的变化的结构,其中翼型区域总是包括杆状或单晶结构,并且其它区域可能偏离其。 还提供了一种用于制造涡轮叶片的方法。
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7.
公开(公告)号:US20110159260A1
公开(公告)日:2011-06-30
申请号:US12979483
申请日:2010-12-28
申请人: Alessandro Casu , Oliver Lüsebrink
发明人: Alessandro Casu , Oliver Lüsebrink
CPC分类号: C23C28/00 , F01D5/288 , F05C2201/0463 , F05C2201/0466 , F05D2300/132 , F05D2300/2118 , Y02T50/67 , Y02T50/6765 , Y10T428/24942 , Y10T428/24967 , Y10T428/31678
摘要: A multilayer coating system is provided. The multilayer coating system includes a substrate, a first metallic layer on the substrate, a first ceramic layer on the first metallic layer, a second metallic layer on the first ceramic layer, and an outermost ceramic layer on the second metallic layer. The multilayer coating system achieves a relatively high overall layer thickness since the critical layer thicknesses of the individual layers do not exceed the multilayer coating.
摘要翻译: 提供多层涂布系统。 多层涂布系统包括基板,基板上的第一金属层,第一金属层上的第一陶瓷层,第一陶瓷层上的第二金属层和第二金属层上的最外层陶瓷层。 由于各层的临界层厚度不超过多层涂层,多层涂层系统实现了相对较高的总层厚度。
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8.
公开(公告)号:US20090280291A1
公开(公告)日:2009-11-12
申请号:US12437075
申请日:2009-05-07
申请人: Fathi Ahmad , Stefan Krause , Oliver Lüsebrink
发明人: Fathi Ahmad , Stefan Krause , Oliver Lüsebrink
IPC分类号: B32B5/12
CPC分类号: F01D5/286 , B22D27/045 , B23P15/02 , C22C19/05 , C22F1/10 , F05D2240/121 , F05D2240/303 , F05D2300/606 , Y02T50/67 , Y10T428/24074
摘要: A component, designed so that the longitudinal grain which experiences the greatest stress has a larger grain width than the other grains, is provided. This longitudinal grain is usually on the edge of the component. The component includes longitudinal grains that are directionally solidified in a rod-crystalline form along the longitudinal axis of the component.
摘要翻译: 提供了一种被设计成使得经受最大应力的纵向颗粒具有比其它颗粒更大的晶粒宽度的部件。 该纵向颗粒通常位于组件的边缘上。 该组件包括纵向晶粒,其沿组件的纵轴以杆状晶体形式定向凝固。
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