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公开(公告)号：US07168708B2
公开(公告)日：2007-01-30
申请号：US11225625
申请日：2005-09-13
IPC分类号： F01D11/02
CPC分类号： F01D11/001 , F01D11/02 , F05D2240/56 , F16J15/164 , F16J15/3288 , F16J15/442
摘要： A seal segment for a turbine is provided having labyrinth teeth and a brush seal disposed along the labyrinth teeth. A plurality of the segments for a seal ring. The segments are separable from each other so that the seal can retract. Each segment has two ends, each of which abuts another segment, with those ends lying along a radius (when looking down the shaft of the turbine). The brush disposed in each segment has ends that do not lie along a radius, but fit together in a tongue and groove configuration when the seal segments come together to form a seal.
摘要翻译： 涡轮机的密封段设有迷宫齿和沿着迷宫齿布置的刷密封件。 用于密封环的多个段。 这些片段可彼此分离，以便密封件可以缩回。 每个段具有两个端部，每个端部邻接另一个段，其中端部沿着半径（当向下俯视涡轮机的轴时）。 设置在每个区段中的刷子具有不沿着半径放置的端部，但是当密封段一起形成密封件时，它们以榫舌和凹槽的形状配合在一起。
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公开(公告)号：US07032903B1
公开(公告)日：2006-04-25
申请号：US09543951
申请日：2000-04-06
IPC分类号： F01D11/02
CPC分类号： F01D11/001 , F01D11/02 , F05D2240/56 , F16J15/164 , F16J15/3288 , F16J15/442
摘要： A seal segment for a turbine is provided having labyrinth teeth and a brush seal disposed along the labyrinth teeth. A plurality of the segments for a seal ring. The segments are separable from each other so that the seal can retract. Each segment has two ends, each of which abuts another segment, with those ends lying along along a radius (when looking down the shaft of the turbine). The brush disposed in each segment has ends that do not lie along a radius, but fit together in a tongue and groove configuration when the seal segments come together to form a seal.
摘要翻译： 涡轮机的密封段设有迷宫齿和沿着迷宫齿布置的刷密封件。 用于密封环的多个段。 这些片段可彼此分离，以便密封件可以缩回。 每个段具有两个端部，每个端部邻接另一个段，其中这些端部沿着半径（当向下俯视涡轮机的轴时）。 设置在每个区段中的刷子具有不沿着半径放置的端部，但是当密封段一起形成密封件时，它们以榫舌和凹槽的形状配合在一起。
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3.发明授权System and method for accommodating changing resource conditions for a steam turbine 有权用于适应汽轮机变化的资源条件的系统和方法公开(公告)号：US08313292B2
公开(公告)日：2012-11-20
申请号：US12564082
申请日：2009-09-22
IPC分类号： F01D25/24
CPC分类号： F01D9/041 , F01D5/14 , F05D2220/31 , F05D2230/60 , F05D2250/70
摘要： A system and method for configuring a steam turbine to accommodate changing resource conditions, such as may be encountered with geothermal wells. A plurality of sets of nozzle/blade assemblies are provided for installation in a diaphragm structure and on a rotor, respectively. As the condition of steam provided to the turbine changes, a different set of nozzle/blade assemblies may be installed to maintain a preferred thermodynamic efficiency for the turbine.
摘要翻译： 一种用于配置蒸汽轮机以适应变化的资源状况的系统和方法，例如可能遇到地热井。 多组喷嘴/叶片组件分别设置在隔膜结构和转子上。 随着提供给涡轮机的蒸汽状况发生变化，可以安装不同组的喷嘴/叶片组件，以维持涡轮机的优选热力学效率。
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4.发明申请System and Method for Accommodating Changing Resource Conditions for a Steam Turbine 有权适应汽轮机变化资源条件的系统和方法公开(公告)号：US20110070064A1
公开(公告)日：2011-03-24
申请号：US12564082
申请日：2009-09-22
CPC分类号： F01D9/041 , F01D5/14 , F05D2220/31 , F05D2230/60 , F05D2250/70
摘要： A system and method for configuring a steam turbine to accommodate changing resource conditions, such as may be encountered with geothermal wells. A plurality of sets of nozzle/blade assemblies are provided for installation in a diaphragm structure and on a rotor, respectively. As the condition of steam provided to the turbine changes, a different set of nozzle/blade assemblies may be installed to maintain a preferred thermodynamic efficiency for the turbine.
摘要翻译： 一种用于配置蒸汽轮机以适应变化的资源状况的系统和方法，例如可能遇到地热井。 多组喷嘴/叶片组件分别设置在隔膜结构和转子上。 随着提供给涡轮机的蒸汽状况发生变化，可以安装不同组的喷嘴/叶片组件，以维持涡轮机的优选热力学效率。
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5.发明授权Apparatus and methods for minimizing vibrational stresses in axial flow turbines 失效轴流式涡轮机振动应力最小化的装置及方法
公开(公告)号：US5116200A
公开(公告)日：1992-05-26
申请号：US544956
申请日：1990-06-28
摘要： The axial flow turbine has an asymmetrical flow input, for example, at the first nozzle plate and which flow is attenuated towards an axi-symmetric flow by a baffle plate located between the first nozzle plate and the second stage. The baffle plate directs the flow towards a more symmetrical flow pattern before permitting the flow to pass through the second stage. Consequently, the long turbine blades in the later stages of the turbine respond to an attenuated asymmetrical flow rather than a larger asymmetrical flow which might induce vibrations or vibrations at the natural resonant frequency of the turbine blading which could break the turbine blades.
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