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公开(公告)号：US08147190B2
公开(公告)日：2012-04-03
申请号：US12884875
申请日：2010-09-17
申请人： Igor Tsypkaykin , Beat Von Arx , Christoph Nagler
发明人： Igor Tsypkaykin , Beat Von Arx , Christoph Nagler
IPC分类号： F04D29/54
CPC分类号： F01D9/042 , F05D2260/30
摘要： A stator vane for a gas turbine includes a vane airfoil which extends in the longitudinal direction of the vane and which is delimited by a leading edge and a trailing edge, and also an outer platform, the inner side of which is exposed to the hot gas which flows through the gas turbine, and on which provision is made for a hook-like fastening element, projecting outwards in the region of the trailing edge, for fastening the stator vane on a casing of the gas turbine, which fastening element, on its side facing the trailing edge, has a locating slot above the trailing edge for the fixing of a heat shield which adjoins the outer platform of the stator vane in the flow direction of the hot gas. Provision is made on the outer platform of the stator vane between the locating slot and the trailing edge of a structure for reducing the thermal and mechanical stresses in the region of the transition between trailing edge and outer platform.
摘要翻译： 一种用于燃气轮机的定子叶片包括沿着叶片的纵向方向延伸并由前缘和后缘限定的叶片翼片，以及外平台，其内侧暴露于热气体 其流过燃气轮机，并且在其上设置用于钩状紧固元件，其在后缘的区域中向外突出，用于将定子叶片紧固在燃气轮机的外壳上，该紧固元件在其上 面向后缘的侧面具有位于后缘上方的定位槽，用于固定与热气体的流动方向相邻的定子叶片的外平台的隔热罩。 在定子叶片的外平台上在定位槽和结构的后缘之间进行设置，以减少后缘和外平台之间的过渡区域内的热应力和机械应力。
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公开(公告)号：US08632309B2
公开(公告)日：2014-01-21
申请号：US13091605
申请日：2011-04-21
IPC分类号： F01D5/14
CPC分类号： F01D5/225 , F05B2240/33
摘要： A blade is disclosed for a gas turbine including an airfoil, which extends along a longitudinal axis from a blade root to a blade tip, and has a shroud segment at the blade tip. The shroud segment abuts with first and second edges against shroud segments of adjacent blades to form a ring-like shroud. The first and second edges are each provided with a respective side rail on the upper side of the shroud segment. Each of the side rails is subdivided into sections of different height and/or width.
摘要翻译： 公开了一种用于燃气涡轮机的叶片，其包括翼型件，该翼型件沿着纵向轴线从叶片根部延伸到叶片尖端，并且在叶片尖端处具有护罩段。 护罩部分与第一和第二边缘邻接抵靠相邻刀片的护罩部分以形成环形护罩。 第一和第二边缘分别在护罩段的上侧设置有相应的侧轨。 每个侧轨分为不同高度和/或宽度的部分。
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3.发明申请METHOD FOR OPTIMIZING THE CONTACT SURFACES OF SHROUD SEGMENTS, WHICH ABUT AGAINST ONE ANOTHER, OF ADJACENT BLADES OF A GAS TURBINE 审中-公开用于优化除了一个另外另外一个气体涡轮机相邻叶片的接头表面的方法公开(公告)号：US20110293428A1
公开(公告)日：2011-12-01
申请号：US13117166
申请日：2011-05-27
申请人： Igor Tsypkaykin , Andre Saxer
发明人： Igor Tsypkaykin , Andre Saxer
CPC分类号： F01D5/225 , F05D2250/183
摘要： A method for optimizing the contact surfaces of abutting shroud segments of adjacent blades of a rotor blade row of a gas turbine includes providing a 3-D model of an individual blade. A geometry of the individual blade is calculated using the 3-D model while considering centrifugal forces, temperature stresses and pressure loads experienced in a loaded state of the blade during operation. The contact surfaces of the abutting shroud segments of adjacent blades are optimized in the loaded state of the blade. The optimization includes the surfaces of functionally serving interlocking surfaces and functionally serving wedge surfaces disposed on each side of the interlocking surfaces. A geometry of the interlocking surfaces and of the wedge surfaces in an unloaded state corresponding to the optimized contact surfaces in the loaded state of the blade is calculated.
摘要翻译： 用于优化燃气轮机的转子叶片排的相邻叶片的邻接的护罩段的接触表面的方法包括提供单个叶片的3-D模型。 使用三维模型计算单个叶片的几何形状，同时考虑在操作期间在叶片的加载状态下遇到的离心力，温度应力和压力负载。 相邻叶片的邻接护罩段的接触表面在叶片的加载状态下被优化。 优化包括设置在互锁表面的每一侧上的功能性联锁表面和功能性服务楔形表面的表面。 计算在与负载状态下的优化的接触表面相对应的处于未加载状态的互锁表面和楔形表面的几何形状。
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公开(公告)号：US20110286849A1
公开(公告)日：2011-11-24
申请号：US13091605
申请日：2011-04-21
IPC分类号： F01D5/14
CPC分类号： F01D5/225 , F05B2240/33
摘要： A blade is disclosed for a gas turbine including an airfoil, which extends along a longitudinal axis from a blade root to a blade tip, and has a shroud segment at the blade tip. The shroud segment abuts with first and second edges against shroud segments of adjacent blades to form a ring-like shroud. The first and second edges are each provided with a respective side rail on the upper side of the shroud segment. Each of the side rails is subdivided into sections of different height and/or width.
摘要翻译： 公开了一种用于燃气涡轮机的叶片，其包括翼型件，该翼型件沿着纵向轴线从叶片根部延伸到叶片尖端，并且在叶片尖端处具有护罩段。 护罩部分与第一和第二边缘邻接抵靠相邻刀片的护罩部分以形成环形护罩。 第一和第二边缘分别在护罩段的上侧设置有相应的侧轨。 每个侧轨分为不同高度和/或宽度的部分。
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公开(公告)号：US20110189002A1
公开(公告)日：2011-08-04
申请号：US13012317
申请日：2011-01-24
IPC分类号： F01D9/04
CPC分类号： F01D9/042 , F01D25/246 , F05D2230/64 , F05D2240/80
摘要： A turbine guide vane (10) has a platform (12) from which at least a guide vane blade (13) extends. The platform (12) has a front rail (18) and a rear rail (20) arranged to be housed in guide vane carrier seats (19, 21). The front and rear rails (18, 20) have projecting pads (23, 24) arranged to rest against the guide vane carrier seats (19, 21). The front and rear rails (18, 20) have at least two pads (23) extending from one side of the front and rear rails (18, 20) and at least two further pads (24) extending from an opposite side of the front and rear rails (18, 20). The pads (23, 24) extend from opposite circumferential portions (26) of the front and rear rails (18, 20). The pads (23, 24) extending from the same circumferential portion (26) of the front and rear rails (18, 20) are at least partly staggered with respect to one another.
摘要翻译： 涡轮引导叶片（10）具有平台（12），至少一个导叶叶片（13）从该平台延伸。 平台（12）具有布置成容纳在导向叶片承载座（19,21）中的前轨（18）和后轨（20）。 前导轨和后导轨（18,20）具有布置成抵靠引导叶片承载座（19,21）的突出垫（23,24）。 前导轨和后导轨（18,20）具有从前后导轨（18,20）的一侧延伸的至少两个焊盘（23）和从前部的相对侧延伸的至少两个另外的焊盘（24） 和后导轨（18,20）。 垫（23,24）从前后导轨（18,20）的相对周向部分（26）延伸。 从前后导轨（18,20）的同一圆周部分（26）延伸的焊盘（23,24）相对于彼此至少部分地交错。
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公开(公告)号：US20110286834A1
公开(公告)日：2011-11-24
申请号：US13116138
申请日：2011-05-26
IPC分类号： F03B11/00
CPC分类号： F01D9/041 , F05D2240/122 , F05D2240/304 , F05D2240/80 , F05D2260/941
摘要： A guide vane is provided for a gas turbine and has an airfoil extending in the radial direction between an inner platform and an outer platform. The airfoil extends transversely to the direction of the hot gas flow between a leading edge and a trailing edge and has a pressure side and a suction side. A cooling slot running parallel to the trailing edge is provided on the pressure side in front of the trailing edge, a cooling medium can exit through the cooling slot from the guide vane over the entire length of the guide vane and can cool the trailing edge of the guide vane. In such a guide vane, the service life is extended by a thermal stress reducing element provided on the inner platform below the trailing edge and the cooling slot.
摘要翻译： 为燃气轮机提供引导叶片，并且具有在内平台和外平台之间沿径向延伸的翼型件。 翼型件在前缘和后缘之间横向于热气流的方向延伸并具有压力侧和吸力侧。 平行于后缘延伸的冷却槽设置在后缘前方的压力侧，冷却介质可以在导叶的整个长度上从导向叶片排出冷却槽， 导叶。 在这种导向叶片中，通过设置在后缘和冷却槽下方的内平台上的热应力减少元件来延长使用寿命。
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公开(公告)号：US20110016875A1
公开(公告)日：2011-01-27
申请号：US12884875
申请日：2010-09-17
申请人： Igor TSYPKAYKIN , Beat Von Arx , Christoph Nagler
发明人： Igor TSYPKAYKIN , Beat Von Arx , Christoph Nagler
CPC分类号： F01D9/042 , F05D2260/30
摘要： A stator vane for a gas turbine includes a vane airfoil which extends in the longitudinal direction of the vane and which is delimited by a leading edge and a trailing edge, and also an outer platform, the inner side of which is exposed to the hot gas which flows through the gas turbine, and on which provision is made for a hook-like fastening element, projecting outwards in the region of the trailing edge, for fastening the stator vane on a casing of the gas turbine, which fastening element, on its side facing the trailing edge, has a locating slot above the trailing edge for the fixing of a heat shield which adjoins the outer platform of the stator vane in the flow direction of the hot gas. With such a stator vane, the service life can be extended by provision being made on the outer platform of the stator vane between the locating slot and the trailing edge of structure for reducing the thermal and mechanical stresses in the region of the transition between trailing edge and outer platform.
摘要翻译： 一种用于燃气轮机的定子叶片包括沿着叶片的纵向方向延伸并由前缘和后缘限定的叶片翼片，以及外平台，其内侧暴露于热气体 其流过燃气轮机，并且在其上设置用于钩状紧固元件，其在后缘的区域中向外突出，用于将定子叶片紧固在燃气轮机的外壳上，该紧固元件在其上 面向后缘的侧面具有位于后缘上方的定位槽，用于固定与热气体的流动方向相邻的定子叶片的外平台的隔热罩。 利用这种定子叶片，通过在定子槽和结构的后缘之间的定子叶片的外平台上进行设置来延长使用寿命，以减少在后缘之间的过渡区域内的热和机械应力 和外部平台。
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