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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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2.发明授权Turbomachine rotor comprising a pretensioning device for pretensioning a rotor blade 失效涡轮机转子包括用于预张紧转子叶片的预张紧装置公开(公告)号：US08512001B2
公开(公告)日：2013-08-20
申请号：US12867567
申请日：2009-01-23
申请人： Francois Benkler , Jörn Bettentrup , Frank Deister , Rudolf Küperkoch , Nicolas Savilius , Oliver Schneider , Dirk Wistuba
发明人： Francois Benkler , Jörn Bettentrup , Frank Deister , Rudolf Küperkoch , Nicolas Savilius , Oliver Schneider , Dirk Wistuba
IPC分类号： F01D25/06
CPC分类号： F01D5/3092 , F01D5/323 , F01D5/326 , Y10T29/49826
摘要： A turbomachine rotor, a rotor blade and a method for assembling a turbomachine rotor are provided. The turbomachine rotor includes a rotor blade with a blade root, a wheel disk with a groove in which the blade root engages such that the rotor blade is maintained in the groove in a positive fit in a radial direction. Further, a pretensioning device is provided, which is supported on the wheel disk as well as on the blade root and which exerts a pretensioning force on the blade root in the radial direction. The pretensioning device is designed such that the pretensioning force can be adjusted when assembling the turbomachine rotor.
摘要翻译： 提供涡轮机转子，转子叶片和组装涡轮机转子的方法。 涡轮机转子包括具有叶片根部的转子叶片，具有槽的轮盘，其中叶片根部接合，使得转子叶片以径向方向以正配合保持在槽中。 此外，提供了预拉伸装置，其被支撑在轮盘上以及叶片根部上，并且在径向方向上对叶根施加预张紧力。 预张紧装置被设计成使得在组装涡轮机转子时可以调节预张紧力。
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3.发明申请Turbomachine Rotor Comprising a Pretensioning Device for Pretensioning a Guide Vane 失效涡轮机转子，包括用于预紧导叶的预张紧装置公开(公告)号：US20110171031A1
公开(公告)日：2011-07-14
申请号：US12867567
申请日：2009-01-23
申请人： Francois Benkler , Jorn Bettentrup , Frank Deister , Rudolf Küperkoch , Nicolas Savilius , Oliver Schneider , Dirk Wistuba
发明人： Francois Benkler , Jorn Bettentrup , Frank Deister , Rudolf Küperkoch , Nicolas Savilius , Oliver Schneider , Dirk Wistuba
CPC分类号： F01D5/3092 , F01D5/323 , F01D5/326 , Y10T29/49826
摘要： A turbomachine rotor, a rotor blade and a method for assembling a turbomachine rotor are provided. The turbomachine rotor includes a rotor blade with a blade root, a wheel disk with a groove in which the blade root engages such that the rotor blade is maintained in the groove in a positive fit in a radial direction. Further, a pretensioning device is provided, which is supported on the wheel disk as well as on the blade root and which exerts a pretensioning force on the blade root in the radial direction. The pretensioning device is designed such that the pretensioning force can be adjusted when assembling the turbomachine rotor.
摘要翻译： 提供涡轮机转子，转子叶片和组装涡轮机转子的方法。 涡轮机转子包括具有叶片根部的转子叶片，具有槽的轮盘，其中叶片根部接合，使得转子叶片以径向方向以正配合保持在槽中。 此外，提供了预拉伸装置，其被支撑在轮盘上以及叶片根部上，并且在径向方向上对叶根施加预张紧力。 预张紧装置被设计成使得在组装涡轮机转子时可以调节预张紧力。
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4.发明申请FASTENING ASSEMBLY FOR BLADES OF TURBOMACHINES HAVING AXIAL FLOW AND METHOD FOR PRODUCING SUCH AN ASSEMBLY 审中-公开具有轴向流动的涡轮机叶片的紧固件组件和用于生产这种组件的方法公开(公告)号：US20130101422A1
公开(公告)日：2013-04-25
申请号：US13696618
申请日：2011-05-11
IPC分类号： F01D5/30
CPC分类号： F01D5/30 , F01D5/3007 , F01D5/3053 , F01D5/323 , F01D9/042 , F04D29/322 , F05B2240/94 , F05D2230/60 , F05D2230/64 , F05D2230/70 , F05D2240/91 , Y10T29/49321
摘要： A fastening assembly for blades of turbomachines through which axial flow can take place, preferably compressors, includes a blade carrier having a lateral face, in which retaining groves are distributed along the circumference, with blades being inserted in the grooves, wherein a resilient tensioning element is provided between each groove base and the underside of the respective blade foot, the underside being located opposite of the groove base. The tensioning element is supported on the respective underside and on the respective groove base in a pretensioning manner, wherein a channel is provided both in the groove base and in the underside, with the tensioning element resting in the channels.
摘要翻译： 一种用于涡轮机叶片的紧固组件，通过其可以发生轴向流动，优选地，压缩机包括具有侧面的叶片载体，其中保持槽沿着圆周分布，其中叶片插入槽中，其中弹性张紧元件 设置在每个凹槽底部和相应的叶片脚的下侧之间，下侧位于凹槽底部的相对侧。 张紧元件以预张紧的方式支撑在相应的下侧和相应的槽底部上，其中在槽底部和下侧都设有通道，张紧元件位于通道中。
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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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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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