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1.发明授权Method and apparatus for cooling combustor liner and transition piece of a gas turbine 有权一种用于冷却燃气轮机的燃烧器衬套和过渡件的方法和装置公开(公告)号：US07493767B2
公开(公告)日：2009-02-24
申请号：US10907866
申请日：2005-04-19
申请人： Ronald Scott Bunker , Jeremy Clyde Bailey , Stanley Kevin Widener , Thomas Edward Johnson , John C Intile
发明人： Ronald Scott Bunker , Jeremy Clyde Bailey , Stanley Kevin Widener , Thomas Edward Johnson , John C Intile
CPC分类号： F23R3/002 , F23R3/06 , F23R2900/03042 , F23R2900/03044
摘要： A method and apparatus for cooling a combustor liner and transitions piece of a gas turbine include a combustor liner with a plurality of turbulators arranged in an array axially along a length defining a length of the combustor liner and located on an outer surface thereof; a first flow sleeve surrounding the combustor liner with a first flow annulus therebetween, the first flow sleeve having a plurality of rows of cooling holes formed about a circumference of the first flow sleeve for directing cooling air from the compressor discharge into the first flow annulus; a transition piece connected to the combustor liner and adapted to carry hot combustion gases to a stage of the turbine; a second flow sleeve surrounding the transition piece a second plurality of rows of cooling apertures for directing cooling air into a second flow annulus between the second flow sleeve and the transition piece; wherein the first plurality of cooling holes and second plurality of cooling apertures are each configured with an effective area to distribute less than 50% of compressor discharge air to the first flow sleeve and mix with cooling air from the second flow annulus.
摘要翻译： 一种用于冷却燃烧器衬套和燃气轮机的过渡件的方法和设备包括具有多个湍流器的燃烧器衬套，该多个湍流器沿着限定燃烧器衬套的长度并位于其外表面上的长度轴向排列; 围绕所述燃烧器衬套的第一流动套筒，其间具有第一流动环空，所述第一流动套筒具有围绕所述第一流动套筒的圆周形成的多排冷却孔，用于将冷却空气从所述压缩机排出口引导到所述第一流动环空中; 连接到所述燃烧器衬套并适于将热燃烧气体运送到所述涡轮机的级的过渡件; 围绕所述过渡件的第二流动套筒，用于将冷却空气引导到所述第二流动套筒和所述过渡件之间的第二流动环空中的第二多排冷却孔; 其中所述第一多个冷却孔和第二多个冷却孔分别配置有有效区域以将小于50％的压缩机排出空气分配到所述第一流动套筒并与来自所述第二流动环的冷却空气混合。
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公开(公告)号：US07373778B2
公开(公告)日：2008-05-20
申请号：US10711131
申请日：2004-08-26
IPC分类号： F02C1/00
CPC分类号： F02C7/12 , F01D25/12 , F01D25/14 , F02C7/18 , F05D2240/35 , F05D2260/202 , F05D2260/2212 , F05D2260/22141 , F23R3/005
摘要： A combustor liner for a gas turbine includes a body having a plurality of angled strips on an outside surface of the combustor liner. The plurality of angled strips are arranged in an array about the outside surface. A space is disposed between each of said plurality of angled strips so as to create vortices in a cooling air flowing in a longitudinal direction across said outside surface of said combustor liner. A method of fabricating a combustor liner includes forming a plurality of angled strips on an outside surface of the combustor liner and arranged in an array about the outside surface, each of the angled strips is disposed so as to be spaced apart to create vortices in a cooling air flowing across the outside surface of the combustor liner.
摘要翻译： 用于燃气轮机的燃烧器衬套包括在燃烧器衬套的外表面上具有多个成角度的条带的主体。 多个成角度的条带围绕外表面布置成阵列。 在所述多个成角度的条带中的每一个之间设置一个空间，以便在穿过所述燃烧器衬套的所述外表面沿纵向方向流动的冷却空气中产生涡流。 一种制造燃烧器衬套的方法包括在燃烧器衬套的外表面上形成多个成角度的带，并围绕外表面排列成阵列，每个成角度的带被设置为间隔开以形成涡流 流过燃烧器衬套的外表面的冷却空气。
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公开(公告)号：US06984102B2
公开(公告)日：2006-01-10
申请号：US10718003
申请日：2003-11-19
IPC分类号： F01D5/18
CPC分类号： F01D5/20 , F01D5/187 , F05D2260/2212 , F05D2260/22141 , Y02T50/67 , Y02T50/671 , Y02T50/676
摘要： A component includes at least one wall having an inner portion and an outer portion. A number of pins extend between the inner and outer portions of the wall. The pins define a mesh cooling arrangement having a number of flow channels. A number of turbulators are disposed on at least one of the inner and outer portions of the wall.
摘要翻译： 一个部件包括至少一个具有内部部分和外部部分的壁。 多个销在壁的内部和外部之间延伸。 销钉限定具有多个流动通道的网状冷却装置。 多个扰流器设置在壁的内部和外部的至少一个上。
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公开(公告)号：US06350102B1
公开(公告)日：2002-02-26
申请号：US09575704
申请日：2000-07-19
IPC分类号： F01D520
摘要： A turbine assembly includes a plurality of rotor blades comprising a root portion, an airfoil having a pressure sidewall and a suction sidewall, and a top portion having a cap. An outer shroud is concentrically disposed about said rotor blades, said shroud in combination with said tip portions defining a clearance gap. At least one circumferential shroud leakage discourager is disposed within the shroud. The leakage discourager(s) increase the flow resistance and thus reduce the flow of hot gas flow leakage for a given pressure differential across the clearance gap to improve overall turbine efficiency.
摘要翻译： 涡轮组件包括多个转子叶片，其包括根部部分，具有压力侧壁的翼型件和抽吸侧壁以及具有盖的顶部部分。 围绕所述转子叶片同心地设置外护罩，所述护罩与所述末端部分组合形成间隙。 至少一个周向护罩泄漏disc is器设置在护罩内。 泄漏劝阻者增加流动阻力，从而减少跨越间隙的给定压差的热气流泄漏流，以提高总体涡轮机效率。
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5.发明授权Method for improving the cooling effectiveness of a gaseous coolant stream, and related articles of manufacture 有权用于改善气态冷却剂流的冷却效果的方法以及相关的制品公开(公告)号：US06234755B1
公开(公告)日：2001-05-22
申请号：US09411206
申请日：1999-10-04
IPC分类号： F01D518
CPC分类号： F01D5/20 , F01D5/186 , F01D5/288 , F01D25/12 , F05D2230/90 , F05D2260/202 , F05D2260/221 , F05D2300/611 , Y02T50/67 , Y02T50/676
摘要： A method is described for improving the cooling effectiveness of a fluid which flows through a row of passage holes in a substrate (e.g., a turbine component), out to a high-temperature surface of the substrate. The method involves forming a slot over the holes, within the high temperature surface of the substrate. The slot can be formed within protective coatings applied over the substrate. Alternatively, it can be formed partially within the substrate, and partially within the protective coatings. Movement of a film coolant through the substrate and into the slot results in greater cooling effectiveness. Related articles are also described.
摘要翻译： 描述了一种用于改善流过基板（例如，涡轮机部件）中的一排通道孔的流体到基板的高温表面的冷却效率的方法。 该方法包括在衬底的高温表面内在孔上形成槽。 槽可以形成在施加在基板上的保护涂层内。 或者，其可以部分地形成在基底内，部分地形成在保护性涂层内。 薄膜冷却剂通过基底并进入槽中的运动导致更大的冷却效果。 还描述了相关文章。
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公开(公告)号：US07186084B2
公开(公告)日：2007-03-06
申请号：US10720045
申请日：2003-11-19
IPC分类号： F01D5/18
CPC分类号： F28F13/12 , F01D5/187 , F05D2230/90 , F05D2250/28 , F05D2260/2212 , F05D2260/2214 , F05D2260/22141 , F28F3/022 , F28F3/044 , Y02T50/67 , Y02T50/671 , Y02T50/676 , Y10T29/4932
摘要： A component includes at least one wall having an inner portion and an outer portion. A number of pins extend between the inner and outer portions of the wall. The pins define a mesh cooling arrangement having a number of flow channels. A number of dimples are located in at least one of the inner and outer portions of the wall. The component may also include a number of turbulators disposed on at least one of the inner and outer portions of the wall.
摘要翻译： 一个部件包括至少一个具有内部部分和外部部分的壁。 多个销在壁的内部和外部之间延伸。 销钉限定具有多个流动通道的网状冷却装置。 多个凹坑位于壁的内部和外部的至少一个中。 该部件还可以包括设置在壁的内部和外部部分中的至少一个上的多个紊流器。
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公开(公告)号：US09435208B2
公开(公告)日：2016-09-06
申请号：US13448469
申请日：2012-04-17
申请人： Ronald Scott Bunker
发明人： Ronald Scott Bunker
CPC分类号： F01D5/147 , B23P15/04 , F01D5/186 , F01D5/189 , F05D2230/30 , F05D2230/90 , F05D2260/204 , Y02T50/672 , Y02T50/673 , Y02T50/676 , Y10T29/49229
摘要： A component includes a substrate having outer and inner surfaces, where the inner surface defines at least one hollow, interior space. The outer surface defines pressure side and suction side walls, which are joined together at leading and trailing edges of the component. The outer surface defines one or more grooves that extend at least partially along the pressure or suction side walls in a vicinity of the trailing edge. Each groove is in fluid communication with a respective hollow, interior space. The component further includes a coating disposed over at least a portion of the outer substrate surface. The coating comprises at least a structural coating that extends over the groove(s), such that the groove(s) and the structural coating together define one or more channels for cooling the trailing edge. A method of forming cooling channels in the vicinity of the trailing edge is also provided.
摘要翻译： 组件包括具有外表面和内表面的基底，其中内表面限定至少一个中空的内部空间。 外表面限定压力侧和吸力侧壁，其在部件的前缘和后缘处连接在一起。 外表面限定一个或多个凹槽，其至少部分地沿着后缘附近的压力或吸力侧壁延伸。 每个槽与相应的中空的内部空间流体连通。 该部件还包括设置在外部基板表面的至少一部分上的涂层。 该涂层包括至少一个在凹槽上延伸的结构涂层，使得凹槽和结构涂层一起限定一个或多个通道以冷却后缘。 还提供了在后缘附近形成冷却通道的方法。
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公开(公告)号：US09327384B2
公开(公告)日：2016-05-03
申请号：US13168117
申请日：2011-06-24
申请人： Ronald Scott Bunker
发明人： Ronald Scott Bunker
CPC分类号： B24C1/045 , C23C4/04 , C23C4/073 , F01D5/186 , F01D5/187 , F01D5/288 , F05D2230/90 , Y02T50/672 , Y02T50/676
摘要： A manufacturing method includes forming one or more grooves in a component that comprises a substrate with an outer surface. The substrate has at least one interior space, and each groove extends at least partially along the substrate and has a base. The manufacturing method further includes forming one or more access holes through the base of a respective groove, to connect the groove in fluid communication with the respective hollow interior space. The manufacturing method further includes forming at least one connecting groove in the component, such that each connecting groove intersects at least a subset of the one or more grooves. The manufacturing method further includes disposing a coating over at least a portion of the outer surface of the substrate, such that the groove(s) and the coating together define one or more channels for cooling the component. The coating does not completely bridge the connecting groove, such that the connecting groove at least partially defines an exit region for the respective cooling channel(s).
摘要翻译： 一种制造方法包括在包括具有外表面的基板的部件中形成一个或多个凹槽。 衬底具有至少一个内部空间，并且每个凹槽至少部分地沿衬底延伸并且具有基底。 制造方法还包括通过相应凹槽的底部形成一个或多个入口孔，以将凹槽与相应的中空内部空间流体连通。 制造方法还包括在部件中形成至少一个连接槽，使得每个连接槽与一个或多个槽的至少一个子集相交。 该制造方法还包括在衬底的外表面的至少一部分上设置涂层，使得凹槽和涂层一起限定一个或多个通道以冷却部件。 涂层不能完全桥接连接槽，使得连接槽至少部分地限定用于各个冷却通道的出口区域。
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9.发明授权Components with microchannel cooled platforms and fillets and methods of manufacture 有权具有微通道冷却平台和圆角的部件和制造方法公开(公告)号：US09243503B2
公开(公告)日：2016-01-26
申请号：US13478517
申请日：2012-05-23
申请人： Ronald Scott Bunker
发明人： Ronald Scott Bunker
CPC分类号： F01D5/187 , F01D5/288 , F05D2240/81 , F05D2260/204 , Y02T50/672 , Y02T50/673 , Y02T50/676
摘要： A component includes a substrate that has outer and inner surfaces. The inner surface defines at least one hollow, interior space. The outer surface defines pressure and suction sidewalls that are joined together at leading and trailing edges of the component and together form an airfoil portion of the component. The outer substrate surface further defines at least one platform and at least one fillet that extends between and integrally connects the airfoil to the respective platform. The outer surface defines one or more grooves that extend at least partially along a respective fillet. Each groove is in fluid communication with a respective hollow, interior space. The component further includes a coating disposed over at least a portion of the outer substrate surface and including at least a structural coating that extends over the groove(s). The groove(s) and the structural coating together define channel(s) for cooling the respective fillet.
摘要翻译： 组件包括具有外表面和内表面的基底。 内表面限定至少一个中空的内部空间。 外表面限定压力和抽吸侧壁，其在部件的前缘和后缘处连接在一起并且一起形成部件的翼型部分。 外基材表面进一步限定至少一个平台和至少一个在所述翼型件之间延伸并且将翼片整体连接到相应的平台的圆角。 外表面限定了至少部分地沿着相应的圆角延伸的一个或多个凹槽。 每个槽与相应的中空的内部空间流体连通。 该部件还包括设置在外部基底表面的至少一部分上的涂层，并且至少包括在凹槽上延伸的结构涂层。 沟槽和结构涂层一起限定用于冷却相应圆角的通道。
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公开(公告)号：US09216491B2
公开(公告)日：2015-12-22
申请号：US13168144
申请日：2011-06-24
申请人： Ronald Scott Bunker
发明人： Ronald Scott Bunker
CPC分类号： B24C1/045 , B23K26/364 , B23K26/389 , B23K2101/001 , F01D5/186 , F05D2230/14 , F05D2230/90 , Y02T50/672 , Y02T50/676
摘要： A manufacturing method is provided. The manufacturing method includes forming one or more grooves in a component comprising a substrate. Each groove extends at least partially along the substrate and has a base, a top and at least one discharge end. The manufacturing method further includes forming a crater, such that the crater is in fluid connection with the respective discharge end for each groove, and disposing a coating over at least a portion of an outer surface of the substrate. The groove(s) and the coating together define one or more channels for cooling the component. The coating does not completely bridge each of the one or more craters, such that each crater defines a film exit. A component with cratered film exits is also provided.
摘要翻译： 提供了一种制造方法。 制造方法包括在包括基板的部件中形成一个或多个凹槽。 每个凹槽至少部分地沿着衬底延伸并且具有底座，顶部和至少一个排出端。 制造方法还包括形成火山口，使得所述火山口与每个槽的相应排出端流体连接，并且在所述基板的外表面的至少一部分上设置涂层。 凹槽和涂层一起限定一个或多个通道用于冷却部件。 涂层不完全桥接一个或多个凹坑中的每一个，使得每个凹坑限定薄膜出口。 还提供了带有起重胶卷出口的部件。
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