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1.发明申请GAS TURBINE COMPONENT HAVING THERMAL BARRIER COATING AND A GAS TURBINE USING THE COMPONENT 审中-公开具有热障涂层的气体涡轮机组件和使用组件的气体涡轮机公开(公告)号：US20120159952A1
公开(公告)日：2012-06-28
申请号：US13332605
申请日：2011-12-21
CPC分类号： C23C28/04 , C23C28/042 , C23C28/046 , C23C28/048 , F01D5/288 , Y02T50/67 , Y02T50/671 , Y02T50/6765
摘要： The present invention provides gas turbine components having durability and reliability for use in a corrosive environment such as a turbine employing a low grade fuel, and also provides a gas turbine equipped with the components. One of the components is a gas turbine bucket/nozzle comprising a substrate made from an alloy containing Ni, Co, or Fe, a bonding layer made from an alloy and disposed over the substrate, and a thermal barrier coating disposed over the bonding layer. The thermal barrier coating includes a thermal barrier layer of porous ceramics, an environmental barrier layer containing silica, and an impregnation layer having a silica-containing material in the pores of the porous ceramics.
摘要翻译： 本发明提供了具有耐久性和可靠性的燃气轮机部件，其用于诸如使用低等级燃料的涡轮机等腐蚀性环境，并且还提供了配备有部件的燃气轮机。 其中一个部件是包括由含有Ni，Co或Fe的合金制成的基体的燃气涡轮机桶/喷嘴，由合金制成并设置在基板上的粘合层，以及设置在接合层上的热障涂层。 隔热涂层包括多孔陶瓷的阻热层，含有二氧化硅的环境阻挡层和在多孔陶瓷的孔中具有含二氧化硅的材料的浸渍层。
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公开(公告)号：US20120084981A1
公开(公告)日：2012-04-12
申请号：US13253164
申请日：2011-10-05
IPC分类号： B23P15/02
CPC分类号： F01D5/288 , C23C4/02 , C23C4/134 , C23C4/18 , C23C28/3215 , C23C28/3455 , F01D5/186 , F05D2230/12 , F05D2230/80 , F05D2230/90 , Y02T50/67 , Y02T50/676 , Y02T50/6765 , Y10T29/49341
摘要： In a method of working a film cooling hole which communicates with an internal cooling passage of a turbine blade from an outer surface, in the turbine blade which has a heat shield coating and the internal cooling passage, there is employed a method of working a cooling hole of a turbine including a step of executing a bond coat on a blade base material a step of piercing a cooling hole in accordance with an electric discharge machining, a step of executing a top coat, and a step of removing the top coat in accordance with a mechanical method with respect to a band-like region including a row of cooling holes, by using an abrasive blasting, a water jet method or the like. Accordingly, an occlusion of the cooling hole, and a damage of the TBC due to the piercing are hardly generated.
摘要翻译： 在从外表面与涡轮叶片的内部冷却通道连通的薄膜冷却孔的工作方法中，在具有隔热涂层和内部冷却通路的涡轮叶片中，采用了一种冷却 包括在叶片基材上执行粘合涂层的步骤，根据放电加工刺穿冷却孔的步骤，执行顶涂层的步骤，以及根据所述顶涂层的去除步骤 通过使用喷砂法，水喷射法等，相对于包括一排冷却孔的带状区域的机械方法。 因此，几乎不产生冷却孔的堵塞和由于穿孔引起的TBC的损坏。
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公开(公告)号：US20110165334A1
公开(公告)日：2011-07-07
申请号：US13048576
申请日：2011-03-15
CPC分类号： C22C38/02 , B22F1/0011 , B22F2998/00 , C22C33/0278 , C22C38/002 , C23C4/04 , C23C30/00 , B22F9/082 , B22F9/04
摘要： A spraying material for coating a metallic member, being inexpensive and having superior corrosion and erosion resistance even in high temperature environments, wherein the material is composed of an Fe—Si based compound and comprises an alloy composed of 10 to 35% by weight of Si and the remainder of Fe and inevitable impurities, and further, up to 5% by weight of B may be added to the material in terms of improvement in hardness and adhesiveness of the coating is provided in order to protect components such as heaters and water walls of coal fired boilers and heat exchanger tubes of fluidized bed boilers, etc., from corrosion and erosion. The spraying material is formed into a coating by, for example, high velocity flame spraying or atmospheric plasma spraying.
摘要翻译： 一种用于涂覆金属构件的喷涂材料，即使在高温环境中也是便宜的且具有优异的耐腐蚀和耐腐蚀性，其中该材料由Fe-Si基化合物组成，并且包含由10至35重量％的Si 并且剩余的Fe和不可避免的杂质，并且还可以在提高硬度方面向材料中添加高达5重量％的B，以提供涂层的粘合性，以便保护诸如加热器和水壁的部件 的燃煤锅炉和流化床锅炉的换热器管等，不受腐蚀和侵蚀。 喷涂材料通过例如高速火焰喷涂或大气等离子喷涂形成涂层。
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公开(公告)号：US20110014035A1
公开(公告)日：2011-01-20
申请号：US12825525
申请日：2010-06-29
申请人： Yoshitaka KOJIMA , Hideyuki Arikawa , Akira Mebata , Hiroyuki Doi , Hajime Toriya , Kenjiro Narita
发明人： Yoshitaka KOJIMA , Hideyuki Arikawa , Akira Mebata , Hiroyuki Doi , Hajime Toriya , Kenjiro Narita
IPC分类号： F01D11/00
CPC分类号： F01D11/02 , C22C19/00 , C22C19/058 , C22C19/07 , C23C4/073 , C23C28/02 , C23C30/00 , F01D11/001 , F01D11/122 , F05D2220/31 , F05D2300/509 , Y10T428/249961 , Y10T428/249974 , Y10T428/249981 , Y10T428/249989
摘要： A metal sealing material used in a sealing device which can reduce a gap between a stator and a rotor of a turbine. The metal sealing material used in a sealing device for a stator and a rotor of a turbine includes a surface layer and a lower layer composed of a porous metal layer, wherein the porosity of the surface layer is smaller than the porosity of the lower layer; the porosity of the surface layer is 60 to 65% and the porosity of the lower layer is 67 to 75% or less; and the porous metal layer has a thickness of 0.3 to 3.0 mm and may include, as a main component, an MCrAlY alloy where M is either one of Ni and Co or both thereof, and h-BN as a solid lubricant.
摘要翻译： 用于密封装置中的金属密封材料，其可以减小定子和涡轮机的转子之间的间隙。 用于定子的密封装置和涡轮机的转子的金属密封材料包括表面层和由多孔金属层构成的下层，其中表面层的孔隙率小于下层的孔隙率; 表面层的孔隙率为60〜65％，下层的孔隙率为67〜75％以下。 多孔金属层的厚度为0.3〜3.0mm，作为主要成分，可以举出M是Ni和Co中的任一种或两者的MCrAlY合金以及作为固体润滑剂的h-BN。
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公开(公告)号：US20100227180A1
公开(公告)日：2010-09-09
申请号：US12398577
申请日：2009-03-05
CPC分类号： C22C38/02 , B22F1/0011 , B22F2998/00 , C22C33/0278 , C22C38/002 , C23C4/04 , C23C30/00 , B22F9/082 , B22F9/04
摘要： A spraying material for coating a metallic member, being inexpensive and having superior corrosion and erosion resistance even in high temperature environments, wherein the material is composed of an Fe—Si based compound and comprises an alloy composed of 10 to 35% by weight of Si and the remainder of Fe and inevitable impurities, and further, up to 5% by weight of B may be added to the material in terms of improvement in hardness and adhesiveness of the coating is provided in order to protect components such as heaters and water walls of coal fired boilers and heat exchanger tubes of fluidized bed boilers, etc., from corrosion and erosion. The spraying material is formed into a coating by, for example, high velocity flame spraying or atmospheric plasma spraying.
摘要翻译： 一种用于涂覆金属构件的喷涂材料，即使在高温环境中也是便宜的且具有优异的耐腐蚀和耐腐蚀性，其中该材料由Fe-Si基化合物组成，并且包含由10至35重量％的Si 并且剩余的Fe和不可避免的杂质，并且还可以在提高硬度方面向材料中添加高达5重量％的B，以提供涂层的粘合性，以便保护诸如加热器和水壁的部件 的燃煤锅炉和流化床锅炉的换热器管等，不受腐蚀和侵蚀。 喷涂材料通过例如高速火焰喷涂或大气等离子喷涂形成涂层。
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公开(公告)号：US07449251B2
公开(公告)日：2008-11-11
申请号：US11006763
申请日：2004-12-08
CPC分类号： C23C28/3215 , C23C4/02 , C23C28/3455 , Y02T50/67 , Y10T428/12611 , Y10T428/12861 , Y10T428/12944 , Y10T428/24997 , Y10T428/26 , Y10T428/263
摘要： A thermal barrier coating comprises a bond coating 12 made of high temperature corrosion resistance superior to a substrate 11 and a thermal barrier coating 13 made of ZrO2 series ceramics formed on the bond coating. The thermal barrier coating has cracks extending in the direction of the thickness of the barrier coat. Substantially all of the tips of the cracks have a distance between the tips and the boundary at the substrate side.
摘要翻译： 热障涂层包括由耐热性高于基材11的粘结涂层12和形成在粘结涂层上的ZrO 2系陶瓷制成的热障涂层13。 隔热涂层具有在阻挡涂层的厚度方向上延伸的裂纹。 基本上所有的裂纹的尖端在顶端和衬底侧的边界之间具有一定距离。
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公开(公告)号：US20080261069A1
公开(公告)日：2008-10-23
申请号：US12105310
申请日：2008-04-18
IPC分类号： B32B15/04
CPC分类号： F01D5/288 , C22C19/05 , C23C4/073 , C23C4/11 , C23C4/18 , C23C28/3215 , C23C28/325 , C23C28/3455 , C23C30/00 , F05C2201/0466 , F05D2300/12 , F05D2300/132 , F05D2300/21 , Y02T50/67 , Y02T50/671 , Y02T50/6765 , Y10T428/12535 , Y10T428/12611
摘要： A ceramic top coat is formed over a heat resistant alloy including Ni as a main component through a bond coat which contains Ni essentially as a main component, Cr, and Al. The alloy for the bond coat can include Si in the range from 0 to 10 wt. %. As a result, in a long time operation, the spalling damage of a ceramic top coat is not easily created and the deterioration of the mechanical properties is small.
摘要翻译： 通过包含Ni基本上作为主要成分Cr和Al的粘合涂层，在包含Ni作为主要成分的耐热合金上形成陶瓷顶涂层。 用于粘结涂层的合金可包括0至10重量％的Si。 ％。 结果，在长时间的操作中，不容易产生陶瓷面漆的剥落损伤，并且机械性能的劣化小。
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公开(公告)号：US20080172267A1
公开(公告)日：2008-07-17
申请号：US11849572
申请日：2007-09-04
IPC分类号： G06Q10/00
CPC分类号： F01D5/005 , F05D2230/80 , G05B2219/32118 , G05B2219/32306 , G06Q10/06 , G06Q10/0631 , G06Q10/06311 , Y02P90/14 , Y02P90/20 , Y02P90/86
摘要： An apparatus or system is used for planning the rotation of part usage between shafts or plants based at least on schedule information relating to operation and inspection-purpose shutdown, attribute information relating to part life, part maintenance periods, and other part attributes, and part information relating to the parts to be used in the rotation.
摘要翻译： 使用装置或系统来至少基于与操作和检查关闭关联的时间表信息来规划轴或工厂之间的部件使用的旋转，与部件寿命有关的属性信息，部件维护周期和其他部件属性，以及部件 与旋转中使用的部件有关的信息。
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公开(公告)号：US07162354B2
公开(公告)日：2007-01-09
申请号：US10896922
申请日：2004-07-23
CPC分类号： F01D25/002 , B08B3/02 , B08B9/00 , F05D2260/80 , F05D2270/07 , F05D2270/3011 , F05D2270/3013 , F05D2270/303
摘要： A gas turbine washing-date determination apparatus of the present invention is equipped with a sum cost calculation means for calculating a sum of loss cost due to not washing a compressor from a compressor efficiency calculated, and determines a gas turbine washing-date with using the sum of the loss cost. Meanwhile, in the gas turbine washing-date determination apparatus the compressor efficiency is calculated from process data of a gas turbine plant, and a compressor washing-date is determined, based on the compressor efficiency.
摘要翻译： 本发明的燃气轮机洗涤日期确定装置装备有和成本计算装置，用于根据计算出的压缩机效率来计算由于不冲压压缩机而引起的损失成本的总和，并且使用 总损失成本。 同时，在燃气轮机洗涤日期确定装置中，基于燃气轮机装置的处理数据计算压缩机效率，并且基于压缩机效率来确定压缩机洗涤日期。
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公开(公告)号：US20050096832A1
公开(公告)日：2005-05-05
申请号：US10896922
申请日：2004-07-23
CPC分类号： F01D25/002 , B08B3/02 , B08B9/00 , F05D2260/80 , F05D2270/07 , F05D2270/3011 , F05D2270/3013 , F05D2270/303
摘要： A gas turbine washing-date determination apparatus of the present invention is equipped with a sum cost calculation means for calculating a sum of loss cost due to not washing a compressor from a compressor efficiency calculated, and determines a gas turbine washing-date with using the sum of the loss cost. Meanwhile, in the gas turbine washing-date determination apparatus the compressor efficiency is calculated from process data of a gas turbine plant, and a compressor washing-date is determined, based on the compressor efficiency.
摘要翻译： 本发明的燃气轮机洗涤日期确定装置装备有和成本计算装置，用于根据计算出的压缩机效率来计算由于不冲压压缩机而引起的损失成本的总和，并且使用 总损失成本。 同时，在燃气轮机洗涤日期确定装置中，基于燃气轮机装置的处理数据计算压缩机效率，并且基于压缩机效率来确定压缩机洗涤日期。
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