公开(公告)号：US5822853A

公开(公告)日：1998-10-20

申请号：US669069

申请日：1996-06-24

申请人： Ann Melinda Ritter ,  John Raymond Hughes ,  Melvin Robert Jackson ,  Francis Lawrence Kirkpatrick ,  Francisco Jose Tenreiro Cunha ,  Nesim Abuaf ,  Ronald Scott Bunker

发明人： Ann Melinda Ritter ,  John Raymond Hughes ,  Melvin Robert Jackson ,  Francis Lawrence Kirkpatrick ,  Francisco Jose Tenreiro Cunha ,  Nesim Abuaf ,  Ronald Scott Bunker

IPC分类号： F02C7/00 ,  B22F5/10 ,  B23K20/00 ,  B23P15/00 ,  F23R3/00 ,  F23R3/42

CPC分类号： F23R3/005 ,  B22F5/10 ,  B23P15/00 ,  B22F2005/103 ,  B23P2700/13 ,  F05B2250/231 ,  Y02T50/675 ,  Y10T29/49346 ,  Y10T29/49353

摘要： Methods of making cylindrical structures with cooling channels, such as, for example, combustor/transition pieces for gas turbines having a double wall with a plurality of cooling channels, both axially and, in some cases, circumferential cross-flow passages positioned between the structure's inner member and the outer member to provide cooling air thereto, are disclosed. The cooling channels are formed in the area between the inner member of the structure and the outer member thereof. The passages preferably extend both axially and circumferentially with respect to the direction of flow through the structure. The axial passages extend completely from one end to the other and the circumferential passages extend around the circumference of the structure.

摘要翻译： 制造具有冷却通道的圆柱形结构的方法，例如用于燃气轮机的燃烧器/过渡件，其具有带有多个冷却通道的双壁，轴向和在一些情况下位于结构的 内部构件和外部构件以提供冷却空气。 冷却通道形成在结构的内部构件和其外部构件之间的区域中。 通道优选地相对于通过结构的流动方向轴向地和周向地延伸。 轴向通道从一端到另一端完全延伸，周向通道围绕结构的圆周延伸。

公开(公告)号：US06183197B2

公开(公告)日：2001-02-06

申请号：US09253367

申请日：1999-02-22

申请人： Ronald Scott Bunker ,  Nesim Abuaf

发明人： Ronald Scott Bunker ,  Nesim Abuaf

IPC分类号： F01D508

CPC分类号： F01D5/141 ,  F05D2260/231 ,  Y02T50/67 ,  Y02T50/673 ,  Y02T50/675 ,  Y10S415/914

摘要： An airfoil with a reduced heat load for use in either a turbine or a compressor of a gas turbine engine comprises having at least one heat reducing dimple on the body of the airfoil or on the associated endwall of the airfoil. The body of the airfoil is comprised of a leading edge, a trailing edge, a pressure side and a suction side. The length of the heat reducing dimple in the expected direction of hot gas stream flow is at least equal to or greater than the width transverse to such direction. The heat reducing dimple is located on the airfoil or endwall so as to reduce the heat load as the hot gas stream flow passes from the leading edge to the trailing edge.

摘要翻译： 具有用于燃气涡轮发动机的涡轮或压缩机中的具有降低的热负荷的翼型件包括在翼型体的主体或翼型的相关端壁上具有至少一个减热凹坑。 机翼的主体由前缘，后缘，压力侧和吸力侧构成。 热气流期望方向上的减热凹坑的长度至少等于或大于横向于该方向的宽度。 减热凹坑位于翼型件或端壁上，以便随着热气流从前缘到后缘流动而减少热负荷。

公开(公告)号：US5660525A

公开(公告)日：1997-08-26

申请号：US94998

申请日：1993-07-23

申请人： Ching-Pang Lee ,  Ronald Scott Bunker ,  Nesim Abuaf ,  Steven Joseph Brzozowski

发明人： Ching-Pang Lee ,  Ronald Scott Bunker ,  Nesim Abuaf ,  Steven Joseph Brzozowski

IPC分类号： F01D5/18

CPC分类号： F01D5/186 ,  F05D2250/12 ,  F05D2250/121 ,  F05D2260/202

摘要： A wall adapted for use in a gas turbine engine between a first and a hotter second fluid includes a first side over which is flowable the first fluid, and an opposite second side over which is flowable the second fluid. An elongate slot extends inwardly from the second side and is disposed in flow communication with a plurality of longitudinally spaced apart holes extending inwardly from the first side. The holes are disposed at a compound angle relative to the second side for discharging the first fluid obliquely into the slot and at a shallow discharge angle from the slot along the second side. The holes are also disposed in converging pairs to impinge together in the slot the first fluid channeled therethrough. In a preferred embodiment, the slot has an aft surface including a plurality of longitudinally spaced apart grooves extending from the holes to the wall second side.

摘要翻译： 适于在第一和第二热液体之间的燃气涡轮发动机中使用的壁包括可流过第一流体的第一侧和可流动第二流体的相对的第二侧。 细长狭槽从第二侧向内延伸，并且设置成与从第一侧向内延伸的多个纵向间隔开的孔流动连通。 孔以相对于第二侧的复合角度设置，用于将第一流体倾斜地排放到槽中，并且沿着沿着第二侧的槽沿浅放电角排放。 这些孔也以会聚对设置，以将槽中的第一流体冲入其中。 在优选实施例中，槽具有包括从孔延伸到壁第二侧的多个纵向间隔开的槽的后表面。

公开(公告)号：US5933699A

公开(公告)日：1999-08-03

申请号：US669070

申请日：1996-06-24

申请人： Ann Melinda Ritter ,  Melvin Robert Jackson ,  Nesim Abuaf ,  Robert Patrick Campbell ,  Ronald Scott Bunker

发明人： Ann Melinda Ritter ,  Melvin Robert Jackson ,  Nesim Abuaf ,  Robert Patrick Campbell ,  Ronald Scott Bunker

IPC分类号： F02C7/00 ,  B21D51/12 ,  B21D53/84 ,  B21H1/06 ,  B23P15/00 ,  F01D9/02 ,  F23R3/00 ,  F23R3/42 ,  B22F7/02 ,  B22F7/06

CPC分类号： F01D9/023 ,  B23P15/00 ,  F23R3/002 ,  B21H1/06 ,  B23P2700/13 ,  Y02T50/67 ,  Y02T50/672 ,  Y02T50/675

摘要： Methods of making gas turbine structures with cooling channels, such as, for example, combustor/transition pieces for gas turbines having a double wall with a plurality of cooling channels, having axially and/or circumferential cross-flow passages positioned between the structure's inner member and the outer member to provide cooling air thereto, are disclosed. A representative method of producing such annular structures having a hot and a cold wall, and joining ribs, for the inner and the outer components of an annulus, such as for jet engine turbine combustors, to net shape as an annular pre-form includes: forming a pre-form assembly including materials for the hot wall, cold wall, and ribs and sacrificial segments for maintaining cooling channels during forming of the pre-assembly and later processing; rolling the pre-form to a required thickness and length as a flat pre-form; hoop-rolling the preform to a required thickness and a required length; welding the assembly; ring rolling to the pre-form to a desired inner diameter; ring-rolling or metal spinning the pre-form to produce the proper wall contour and removing the sacrificial material to open the cooling channels.

摘要翻译： 制造具有冷却通道的燃气轮机结构的方法，例如具有带有多个冷却通道的双壁的燃气涡轮机的燃烧器/过渡件，具有位于结构的内部构件之间的轴向和/或周向的横向流动通道 和外部构件以提供冷却空气。 用于制造具有热壁和冷壁的环形结构的代表性方法，以及用于环形的内部和外部部件（例如用于喷气式发动机涡轮机燃烧器）的连接肋，作为环形预成型体的净形状包括： 形成预成型组件，其包括用于热壁，冷壁和肋的材料以及用于在形成预组件和稍后处理期间保持冷却通道的牺牲段; 将预制件滚压成所需的厚度和长度作为平面预制件; 将预制棒环绕到所需的厚度和所需长度; 焊接组件; 环状轧制成预制件至期望的内径; 环形轧制或金属纺丝预成型件以产生适当的壁轮廓并去除牺牲材料以打开冷却通道。

公开(公告)号：US06234755B1

公开(公告)日：2001-05-22

申请号：US09411206

申请日：1999-10-04

申请人： Ronald Scott Bunker ,  Jeremy Clyde Bailey ,  Ching-Pang Lee ,  Nesim Abuaf

发明人： Ronald Scott Bunker ,  Jeremy Clyde Bailey ,  Ching-Pang Lee ,  Nesim Abuaf

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。

公开(公告)号：US5651662A

公开(公告)日：1997-07-29

申请号：US968544

申请日：1992-10-29

申请人： Ching-Pang Lee ,  Ronald Scott Bunker ,  Nesim Abuaf

发明人： Ching-Pang Lee ,  Ronald Scott Bunker ,  Nesim Abuaf

IPC分类号： F01D5/18

CPC分类号： F01D5/186 ,  F05D2250/12 ,  F05D2250/121 ,  F05D2260/202

摘要： A wall adapted for use in a gas turbine engine between a first and a hotter second fluid includes a first side over which is flowable the first fluid, and an opposite second side over which is flowable the second fluid. An elongate slot extends inwardly from the second side and is disposed in flow communication with a plurality of longitudinally spaced apart holes extending inwardly from the first side. The holes are disposed at a compound angle relative to the second side for discharging the first fluid obliquely into the slot and at a shallow discharge angle from the slot along the second side. In a preferred embodiment, the slot has an aft surface including a plurality of longitudinally spaced apart grooves extending from the holes to the wall second side.

摘要翻译： 适于在第一和第二热液体之间的燃气涡轮发动机中使用的壁包括可流过第一流体的第一侧和可流动第二流体的相对的第二侧。 细长狭槽从第二侧向内延伸，并且设置成与从第一侧向内延伸的多个纵向间隔开的孔流动连通。 孔以相对于第二侧的复合角度设置，用于将第一流体倾斜地排放到槽中，并且沿着沿着第二侧的槽沿浅放电角排放。 在优选实施例中，槽具有包括从孔延伸到壁第二侧的多个纵向间隔开的槽的后表面。

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

IPC分类号： F01D5/18 ,  F01D5/14 ,  B23P15/04

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。

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

IPC分类号： F01D5/18 ,  B24C1/04 ,  C23C4/04 ,  F01D5/28

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。

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

IPC分类号： F01D5/18 ,  F01D5/28

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。

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

IPC分类号： F01D5/18 ,  B24C1/04 ,  B23K26/36 ,  B23K26/38

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。