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1. 发明公开

EP2390465A3 Gas turbine components which include chevron film cooling holes, and related processes 有权转让
标题翻译：包括人字形薄膜冷却孔的燃气轮机部件及相关工艺
公开(公告)号：EP2390465A3
公开(公告)日：2017-12-20
申请号：EP11159625.0
申请日：2011-03-24
申请人： General Electric Company
发明人： Bunker, Ronald Scott , Lacy, Benjamin Paul
IPC分类号： F01D5/18
CPC分类号： F01D5/186 , F05D2230/10 , Y02T50/67 , Y02T50/672 , Y02T50/676 , Y10T29/49316
摘要： An article is described, including an inner surface (24) which can be exposed to a first fluid; an inlet (30); and an outer surface (26) spaced from the inner surface, which can be exposed to a hotter second fluid. The article further includes at least one row or other pattern of passage holes (28). Each passage hole includes an inlet bore (34) extending through the substrate (20) from the inlet at the inner surface to a passage hole-exit proximate to the outer surface (26), with the inlet bore terminating in a chevron outlet (32) adjacent the hole-exit. The chevron outlet includes a pair of wing troughs (42,44) having a common surface region (46) between them. The common surface region includes a valley (48) which is adjacent the hole-exit; and a plateau (50) adjacent the valley. The article can be an airfoil. Related methods for preparing the passage holes are also described.
摘要翻译：描述了一种物品，其包括可暴露于第一流体的内表面（24）一个入口（30）; 和与内表面间隔开的外表面（26），所述外表面可以暴露于较热的第二流体。该物品还包括至少一排或其他图案的通道孔（28）。每个通道孔包括从内表面处的入口延伸穿过基板（20）到靠近外表面（26）的通道孔出口的入口孔（34），入口孔终止于人字形出口（32 ）与洞出口相邻。人字形出口包括一对翼槽（42,44），它们之间具有共同的表面区域（46）。公共表面区域包括与孔出口相邻的谷（48）和一个靠近山谷的高原（50）。该文章可以是机翼。还描述了用于制备通孔的相关方法。

2. 发明公开

EP2487330A3 Components with cooling channels and methods of manufacture 有权转让
标题翻译：具有冷却通道和制造方法的组件
公开(公告)号：EP2487330A3
公开(公告)日：2017-08-23
申请号：EP12155466.1
申请日：2012-02-14
申请人： General Electric Company
发明人： Bunker, Ronald Scott
IPC分类号： F01D5/14 , F01D5/18
摘要： A method of manufacturing a component (100) is provided. The method includes forming one or more grooves (132) in an outer surface (112) of a substrate (110). Each groove (132) extends at least partially along the surface (112) of the substrate (110) and has a base (134), a top (136) and at least one discharge point (170). The method further includes forming a run-out region (172) adjacent to the discharge point (170) for each groove (132) and disposing a coating (150) over at least a portion of the surface (112) of the substrate (110). The groove(s) (132) and the coating (150) define one or more channels (130) for cooling the component (100). Components (100) with cooling channels (130) are also provided.
摘要翻译：提供了一种制造部件（100）的方法。该方法包括在衬底（110）的外表面（112）中形成一个或多个凹槽（132）。每个凹槽132至少部分地沿着衬底110的表面112延伸并且具有基部134，顶部136和至少一个排放点170。该方法进一步包括为每个凹槽（132）形成与放电点（170）相邻的导出区域（172），并在基板（110）的至少一部分表面（112）上设置涂层）。凹槽（132）和涂层（150）限定用于冷却部件（100）的一个或多个通道（130）。还提供具有冷却通道（130）的部件（100）。

3. 发明公开

EP2381070A3 Hot gas path component cooling system 有权转让
标题翻译：热气路径组件冷却系统
公开(公告)号：EP2381070A3
公开(公告)日：2017-05-31
申请号：EP11155087.7
申请日：2011-02-18
申请人： General Electric Company
发明人： Lacy, Benjamin Paul , Bunker, Ronald Scott , Itzel, Gary Michael
IPC分类号： F01D25/12 , F01D5/18 , F02C7/12
CPC分类号： F01D25/12 , F01D5/186 , F01D5/187 , F02C7/12 , F05D2230/11 , F05D2230/13 , F05D2230/313 , F05D2230/314 , F05D2230/90 , F05D2260/201 , F05D2260/202 , F05D2260/22141
摘要： A cooling system (110) for a hot gas path component (100) is disclosed. The cooling system (110) may include a component layer (120) and a cover layer (125). The component layer (120) may include a first inner surface (122) and a second outer surface (124). The second outer surface (124) may define a plurality of channels (130). The component layer (120) may further define a plurality of passages (140) extending generally between the first inner surface (122) and the second outer surface (124). Each of the plurality of channels (130) may be fluidly connected to at least one of the plurality of passages (140). The cover layer (125) may be situated adjacent the second outer surface (124) of the component layer (120). The plurality of passages (140) may be configured to flow a cooling medium (90) to the plurality of channels (130) and provide impingement cooling to the cover layer (125). The plurality of channels (130) may be configured to flow cooling medium (90) therethrough, cooling the cover layer (125).
摘要翻译：公开了一种用于热气路径部件（100）的冷却系统（110）。冷却系统（110）可以包括组件层（120）和覆盖层（125）。部件层（120）可以包括第一内表面（122）和第二外表面（124）。第二外表面（124）可以限定多个通道（130）。部件层（120）可以进一步限定大致在第一内表面（122）和第二外表面（124）之间延伸的多个通道（140）。多个通道（130）中的每一个可以流体连接至多个通道（140）中的至少一个。覆盖层（125）可以位于组件层（120）的第二外表面（124）附近。多个通道140可构造成使冷却介质90流向多个通道130并向覆盖层125提供冲击冷却。多个通道（130）可以被配置为使冷却介质（90）流过其中，从而冷却覆盖层（125）。

4. 发明授权

EP2466069B1 Thermal inspection and machining method 有权
标题翻译： Wärmeinspektions-和加工方法
公开(公告)号：EP2466069B1
公开(公告)日：2015-11-11
申请号：EP11191460.2
申请日：2011-12-01
申请人： General Electric Company
发明人： Bunker, Ronald Scott , Allen, Jason Randolph , Crosby, Jared
IPC分类号： F01D5/00 , F01D5/18 , G01N25/72 , G06T7/00
CPC分类号： F01D5/005 , B23P2700/06 , F01D5/14 , F01D25/285 , F05D2260/80 , G01N21/951 , G01N25/18 , G01N25/72

5. 发明公开

EP2369236A3 Aerodynamic flame stablizer 审中-公开
标题翻译：气动火焰稳定器
公开(公告)号：EP2369236A3
公开(公告)日：2014-11-12
申请号：EP11157486.9
申请日：2011-03-09
申请人： General Electric Company
发明人： Bunker, Ronald Scott , Evulet, Andrei Tristan
IPC分类号： F23R3/20 , F23R3/34
CPC分类号： F23R3/20 , F23R3/346 , F23R2900/03341
摘要： A flame stabilizer (40) is in fluid communication with a combustor (18) of a gas turbine engine (10). The flame stabilizer (40) has a body (42) with an aerodynamic shape that creates a flow recirculation zone (44) by injection of fluid (48) through a plurality of holes (46) in the body of the flame stabilizer. The aerodynamic shape of the body reduces pressure loss in the combustor (18), particularly when no fuel is being provided to the combustor. In addition, the magnitude of the flow recirculation zone (44) can be modulated by selectively adjusting the flow rate of fluid (48) through the holes (46), or by selectively adjusting the size of the holes (46).

6. 发明授权

EP2537636B1 Component with cooling channels and method of manufacture 有权
标题翻译：具有冷却通道和制造过程组件
公开(公告)号：EP2537636B1
公开(公告)日：2014-04-30
申请号：EP12172824.0
申请日：2012-06-20
申请人： GENERAL ELECTRIC COMPANY
发明人： Bunker, Ronald Scott
IPC分类号： B24C1/04 , B23P15/04 , C23C4/00 , F01D5/18
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 (132) in a component that comprises a substrate (110) with an outer surface (112). The substrate has at least one interior space, and each groove extends at least partially along the substrate and has a base (134). The manufacturing method further includes forming one or more access holes (140) through the base (134) 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 (150) 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 (130) 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 (62) for the respective cooling channel(s).

7. 发明公开

EP2604796A2 Gas turbine components with microchannel cooling 有权转让
标题翻译： Gasturbinen-Komponenten mitMikrokanalkühlung
公开(公告)号：EP2604796A2
公开(公告)日：2013-06-19
申请号：EP12195706.2
申请日：2012-12-05
申请人： General Electric Company
发明人： Bunker, Ronald Scott
IPC分类号： F01D5/18 , F01D5/28 , F01D5/20
摘要： A component includes a substrate (110) having an outer surface (112), an inner surface and a tip (34). The inner surface defines at least one hollow, interior space. The outer surface (112) defines one or more grooves (132), where each groove (132) extends at least partially along the outer surface (112) of the substrate and has a base (134). The component further includes a coating (150) disposed over at least a portion of the outer surface (112) of the substrate (110). The coating (150) includes at least a structural coating (150) that extends over the groove(s) (132), such that the groove(s) (132) and the structural coating (150) together define one or more channels for cooling the component. The tip comprises a tip cap enclosing the hollow, interior space(s), and a tip rim disposed at a radially outer end of the substrate. The tip rim at least partially defines at least one discharge channel in fluid communication with at least one cooling channel (130).
摘要翻译：组件包括具有外表面（112），内表面和尖端（34）的基底（110）。内表面限定至少一个中空的内部空间。外表面（112）限定一个或多个凹槽（132），其中每个凹槽（132）至少部分地沿着基底的外表面（112）延伸并且具有基部（134）。该部件还包括设置在基板（110）的外表面（112）的至少一部分上方的涂层（150）。涂层（150）包括至少一个在凹槽（132）上延伸的结构涂层（150），使得凹槽（132）和结构涂层（150）共同限定一个或多个通道，用于冷却组件。尖端包括封闭中空的内部空间的尖端盖和设置在基板的径向外端处的尖端边缘。尖端边缘至少部分地限定与至少一个冷却通道（130）流体连通的至少一个排放通道。

8. 发明公开

EP2511475A2 Methods of fabricating a coated component using multiple types of fillers 有权转让
标题翻译：一种用于具有若干类型的填料生产涂覆的部件的过程
公开(公告)号：EP2511475A2
公开(公告)日：2012-10-17
申请号：EP12162988.5
申请日：2012-04-03
申请人： General Electric Company
发明人： Rebak, Raul Basilio , Bunker, Ronald Scott , Kool, Lawrence Bernard , Lipkin, Don Mark , McDermott, John Brian , Ritter, Ann Melinda , Rohling, Renee Bushey
IPC分类号： F01D5/18 , F01D5/14
摘要： Methods of fabricating coated components (100) using multiple types of fillers are provided. One method comprises forming one or more grooves (132) in an outer surface (112) of a substrate (110). Each groove has a base (134) and extends at least partially along the outer surface. A sacrificial filler (32) is deposited within the groove(s), a second filler (33) is deposited over the sacrificial filler (32), and a coating (150) is disposed over at least a portion of the outer surface and over the second filler. The method further includes removing the sacrificial filler and at least partially removing the second filler from the groove(s), to define one or more channels (130) for cooling the component.
摘要翻译：提供了使用多种类型的填料的制造涂覆的部件（100）的方法。一种方法包括在形成在基板（110）的外表面（112）一个或更多凹槽（132）。每个凹槽具有基部（134）和沿所述外表面至少部分地延伸。牺牲填料（32）的槽（S），第二填充材料（33）被沉积在牺牲填料（32）和涂层（150）内至少沉积在布置在所述外表面的一部分上以及所述第二填料。该方法包括：去除牺牲此外填料和至少部分地从所述槽（多个）去除第二填料，以用于冷却构件限定一个或多个通道（130）。

9. 发明公开

EP2466069A1 Thermal inspection and machining systems and methods of use 有权
标题翻译： Wärmeinspektions-und Bearbeitungsverfahren
公开(公告)号：EP2466069A1
公开(公告)日：2012-06-20
申请号：EP11191460.2
申请日：2011-12-01
申请人： General Electric Company
发明人： Bunker, Ronald Scott , Allen, Jason Randolph , Crosby, Jared
IPC分类号： F01D5/00 , F01D5/18 , G01N25/72 , G06T7/00
CPC分类号： F01D5/005 , B23P2700/06 , F01D5/14 , F01D25/285 , F05D2260/80 , G01N21/951 , G01N25/18 , G01N25/72
摘要： The present application provides a thermal imaging and machining system (100) for a machine component (130). The thermal imaging and machining system (100) may include a machining subsystem (120) with a machining device (300) for drilling one or more holes (140) in the machine component (130) and a thermal inspection subsystem (110) positioned about the machining subsystem (120). The thermal inspection subsystem (110) may include an imager (160) and one or more fluid supply lines (205) such that a thermal response of the holes (140) in the machine component (130) may be determined.
摘要翻译：本申请提供了用于机器部件（130）的热成像和加工系统（100）。热成像和加工系统（100）可以包括具有用于在机器部件（130）中钻一个或多个孔（140）的加工装置（300）的加工子系统（120）和围绕加工子系统（120）。热检查子系统（110）可以包括成像器（160）和一个或多个流体供应管线（205），使得可以确定机器部件（130）中的孔（140）的热响应。

10. 发明公开

EP2354783A1 Thermal inspection system and method incorporating external flow 有权
标题翻译：戴维斯顿（Durchfluss），维特根斯堡（Värmeinspektionssystemund Verfahren mit externem Durchfluss）
公开(公告)号：EP2354783A1
公开(公告)日：2011-08-10
申请号：EP10196519.2
申请日：2010-12-22
申请人： General Electric Company
发明人： Allen, Jason Randolph , Bunker, Ronald Scott , Crosby, Jared Michael
IPC分类号： G01N25/72
CPC分类号： G01N25/72
摘要： A thermal inspection method is disclosed. The inspection method includes disposing a component in a wind tunnel configured to create a predetermined Mach number distribution for an external surface of the component. A gas is supplied at a known temperature T into the wind tunnel to create an external flow of gas over the external surface of the component in accordance with the predetermined Mach number distribution. The inspection method further includes directly or indirectly measuring one or more external surface temperatures of the component to generate an external surface temperature distribution for the external surface of the component and using the external surface temperature distribution to perform a quality control inspection of the component. A thermal inspection system is also provided.
摘要翻译：公开了一种热检查方法。所述检查方法包括将组件设置在风洞中，所述风洞构造成为所述部件的外表面产生预定的马赫数分布。在已知温度T下将气体供应到风洞中，以根据预定的马赫数分布在部件的外表面上产生气体的外部气流。检查方法还包括直接或间接测量部件的一个或多个外表面温度，以产生组件的外表面的外表面温度分布，并且使用外表面温度分布来执行部件的质量控制检查。还提供热检查系统。

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