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1. 发明申请

US20110164653A1 THERMAL INSPECTION SYSTEM AND METHOD INCORPORATING EXTERNAL FLOW 审中-公开
标题翻译：热检查系统和外部流量的方法
公开(公告)号：US20110164653A1
公开(公告)日：2011-07-07
申请号：US12683638
申请日：2010-01-07
申请人： Jason Randolph Allen , Ronald Scott Bunker , Jared Michael Crosby
发明人： Jason Randolph Allen , Ronald Scott Bunker , Jared Michael Crosby
IPC分类号： G01N25/20
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，所述风洞被配置为为所述部件的外表面创建预定的马赫数分布。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地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。

2. 发明申请

US20090297336A1 ONLINE SYSTEMS AND METHODS FOR THERMAL INSPECTION OF PARTS 审中-公开
标题翻译：在线检测零件的系统和方法
公开(公告)号：US20090297336A1
公开(公告)日：2009-12-03
申请号：US11842219
申请日：2007-08-21
申请人： Jason Randolph Allen , Ronald Scott Bunker
发明人： Jason Randolph Allen , Ronald Scott Bunker
IPC分类号： F01D25/00 , G01F1/68
CPC分类号： G01F1/68 , F05B2260/80
摘要： A thermal inspection method is provided. The method includes measuring a transient thermal response of a cooled part installed in a turbine engine, wherein the transient thermal response results from operation of the turbine engine. The method also includes using the transient thermal response to determine one or more of a flow rate of a fluid flowing through one or more film cooling holes in the cooled part during operation of the turbine engine, at least one heat transfer coefficient for one or more internal passages in the cooled part, and a combined thermal response for the cooled part. The method further includes comparing at least one of the flow rate, the at least one heat transfer coefficient, and the combined thermal response of at least a portion of the cooled part to at least one baseline value to determine whether a thermal performance of the cooled part is satisfactory.
摘要翻译：提供了热检测方法。该方法包括测量安装在涡轮发动机中的冷却部件的瞬态热响应，其中瞬态热响应来自涡轮发动机的操作。该方法还包括使用瞬态热响应来确定在涡轮发动机运行期间流过冷却部分中的一个或多个膜冷却孔的流体的流速中的一个或多个，至少一个或多个传热系数冷却部分的内部通道，以及冷却部件的组合热响应。该方法还包括将至少一个热传递系数和至少一部分冷却部件的组合热响应中的至少一个比较至至少一个基准值，以确定冷却的部分令人满意

3. 发明申请

US20090016402A1 SYSTEM AND METHOD FOR THERMAL INSPECTION OF PARTS 有权
标题翻译：用于部件热检查的系统和方法
公开(公告)号：US20090016402A1
公开(公告)日：2009-01-15
申请号：US11775502
申请日：2007-07-10
申请人： Ronald Scott Bunker , Jason Randolph Allen
发明人： Ronald Scott Bunker , Jason Randolph Allen
IPC分类号： G01N25/72
CPC分类号： G01N25/72
摘要： A method of thermal inspection of a part having at least one internal cavity is provided. The method includes flowing a fluid through the at least one internal cavity. The method also includes measuring a temperature at one or more locations on the part over time. The method further includes calculating at least one of a first and a second derivative of the temperature with respect to time. The method also includes comparing at least one of the first or the second derivative to one or more baseline values to determine if the part meets a desired specification.
摘要翻译：提供了具有至少一个内部空腔的部件的热检查方法。该方法包括使流体流过至少一个内腔。该方法还包括随时间测量该部件上的一个或多个位置处的温度。该方法还包括相对于时间计算温度的第一和第二导数中的至少一个。该方法还包括将第一或第二导数中的至少一个与一个或多个基线值进行比较，以确定该部分是否满足期望的规范。

4. 发明申请

US20120154570A1 Thermal Inspection and Machining Systems and Methods of Use 有权
标题翻译：热检查和加工系统及使用方法
公开(公告)号：US20120154570A1
公开(公告)日：2012-06-21
申请号：US12968308
申请日：2010-12-15
申请人： Ronald Scott Bunker , Jason Randolph Allen , Jared Crosby
发明人： Ronald Scott Bunker , Jason Randolph Allen , Jared Crosby
IPC分类号： H04N7/18
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 for a machine component. The thermal imaging and machining system may include a machining subsystem with a machining device for drilling one or more holes in the machine component and a thermal inspection subsystem positioned about the machining subsystem. The thermal inspection subsystem may include an imager and one or more fluid supply lines such that a thermal response of the holes in the machine component may be determined.
摘要翻译：本申请提供了用于机器部件的热成像和加工系统。热成像和加工系统可以包括具有用于在机器部件中钻一个或多个孔的加工装置的加工子系统以及围绕加工子系统定位的热检查子系统。热检查子系统可以包括成像器和一个或多个流体供应管线，使得可以确定机器部件中的孔的热响应。

5. 发明授权

US08810644B2 Thermal inspection and machining systems and methods of use 有权
标题翻译：热检查和加工系统及使用方法
公开(公告)号：US08810644B2
公开(公告)日：2014-08-19
申请号：US12968308
申请日：2010-12-15
申请人： Ronald Scott Bunker , Jason Randolph Allen , Jared Crosby
发明人： Ronald Scott Bunker , Jason Randolph Allen , Jared Crosby
IPC分类号： H04N7/18 , F01D5/00 , G01N25/18 , G01N25/72 , G01N21/95 , F01D5/14
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 for a machine component. The thermal imaging and machining system may include a machining subsystem with a machining device for drilling one or more holes in the machine component and a thermal inspection subsystem positioned about the machining subsystem. The thermal inspection subsystem may include an imager and one or more fluid supply lines such that a thermal response of the holes in the machine component may be determined.
摘要翻译：本申请提供了用于机器部件的热成像和加工系统。热成像和加工系统可以包括具有用于在机器部件中钻一个或多个孔的加工装置的加工子系统以及围绕加工子系统定位的热检查子系统。热检查子系统可以包括成像器和一个或多个流体供应管线，使得可以确定机器部件中的孔的热响应。

6. 发明授权

US07651261B2 System and method for thermal inspection of parts 有权
标题翻译：零件热敏检测系统及方法
公开(公告)号：US07651261B2
公开(公告)日：2010-01-26
申请号：US11775502
申请日：2007-07-10
申请人： Ronald Scott Bunker , Jason Randolph Allen
发明人： Ronald Scott Bunker , Jason Randolph Allen
IPC分类号： G01N25/18
CPC分类号： G01N25/72
摘要： A method of thermal inspection of a part having at least one internal cavity is provided. The method includes flowing a fluid through the at least one internal cavity. The method also includes measuring a temperature at one or more locations on the part over time. The method further includes calculating at least one of a first and a second derivative of the temperature with respect to time. The method also includes comparing at least one of the first or the second derivative to one or more baseline values to determine if the part meets a desired specification.
摘要翻译：提供了具有至少一个内部空腔的部件的热检查方法。该方法包括使流体流过至少一个内腔。该方法还包括随时间测量该部件上的一个或多个位置处的温度。该方法还包括相对于时间计算温度的第一和第二导数中的至少一个。该方法还包括将第一或第二导数中的至少一个与一个或多个基线值进行比较，以确定该部分是否满足期望的规范。

7. 发明授权

US07890274B2 Method for quantifying hole flow rates in film cooled parts 失效
标题翻译：定影薄膜冷却部件孔流速的方法
公开(公告)号：US07890274B2
公开(公告)日：2011-02-15
申请号：US12413756
申请日：2009-03-30
申请人： Ronald Scott Bunker , Jason Randolph Allen , Jared Michael Crosby
发明人： Ronald Scott Bunker , Jason Randolph Allen , Jared Michael Crosby
IPC分类号： G01N25/00 , G06F19/00
CPC分类号： G01F1/6884 , F01D5/186 , F05D2300/5024 , G01N25/72
摘要： A method for measuring a flow rate through a cooling hole of a film cooled part includes the steps of 1) measuring a transient thermal response of an internal surface temperature corresponding solely to an inside portion of a cooling hole for a film cooled part resulting from a flow of fluid through the part, the fluid having an initial temperature that is different from an initial temperature of the film cooled part, 2) mathematically characterizing the transient thermal response, and 3) determining the cooling hole flow rate from the mathematical characterization.
摘要翻译：一种用于测量通过薄膜冷却部件的冷却孔的流量的方法包括以下步骤：1）测量仅对应于由冷却部件产生的薄膜冷却部件的冷却孔的内部部分的内部表面温度的瞬态热响应流体流过该部分，流体具有不同于薄膜冷却部分的初始温度的初始温度，2）数学表征瞬态热响应，以及3）从数学表征确定冷却孔流速。

8. 发明申请

US20100250155A1 METHOD FOR QUANTIFYING HOLE FLOW RATES IN FILM COOLED PARTS 失效
标题翻译：电影冷却部件的孔流量定量方法
公开(公告)号：US20100250155A1
公开(公告)日：2010-09-30
申请号：US12413756
申请日：2009-03-30
申请人： Ronald Scott Bunker , Jason Randolph Allen
发明人： Ronald Scott Bunker , Jason Randolph Allen
IPC分类号： G06F19/00 , G01F25/00
CPC分类号： G01F1/6884 , F01D5/186 , F05D2300/5024 , G01N25/72
摘要： A method for measuring a flow rate through a cooling hole of a film cooled part includes the steps of 1) measuring a transient thermal response of an internal surface temperature corresponding solely to an inside portion of a cooling hole for a film cooled part resulting from a flow of fluid through the part, the fluid having an initial temperature that is different from an initial temperature of the film cooled part, 2) mathematically characterizing the transient thermal response, and 3) determining the cooling hole flow rate from the mathematical characterization.
摘要翻译：一种用于测量通过薄膜冷却部件的冷却孔的流量的方法包括以下步骤：1）测量仅对应于由冷却部件产生的薄膜冷却部件的冷却孔的内部部分的内部表面温度的瞬态热响应流体流过该部分，流体具有不同于薄膜冷却部分的初始温度的初始温度，2）数学表征瞬态热响应，以及3）从数学表征确定冷却孔流速。

9. 发明授权

US09284231B2 Hydrocarbon film protected refractory carbide components and use 有权
$Hydrocarbon film protected refractory carbide components and use$
标题翻译：碳膜保护耐火硬质合金元件和使用
公开(公告)号：US09284231B2
公开(公告)日：2016-03-15
申请号：US13328704
申请日：2011-12-16
申请人： William Paul Minnear , Ronald Scott Bunker , Narendra Digamber Joshi , Andrei Tristan Evulet
发明人： William Paul Minnear , Ronald Scott Bunker , Narendra Digamber Joshi , Andrei Tristan Evulet
IPC分类号： F02C7/08 , C04B41/80 , C04B41/00 , F01D25/12 , F02C7/12
CPC分类号： F02C7/16 , C04B41/0072 , C04B41/009 , C04B41/80 , F01D15/10 , F01D25/12 , F02C7/12 , F05D2260/232 , Y02T50/672 , Y02T50/676 , C04B35/56 , C04B35/565 , C04B35/806 , C04B41/4529
摘要： A turbine power generation system with enhanced stabilization of refractory carbides provided by hydrocarbon from high carbon activity gases is disclosed. The disclosure also includes a method of using high carbon activity gases to stabilize hot gas path components.
摘要翻译：公开了一种具有由高碳活性气体由烃提供的难熔碳化物的稳定化的涡轮发电系统。本公开还包括使用高碳活性气体来稳定热气路径成分的方法。

10. 发明授权

US08905713B2 Articles which include chevron film cooling holes, and related processes 有权
标题翻译：包括人字形薄膜冷却孔的文章及相关工艺
公开(公告)号：US08905713B2
公开(公告)日：2014-12-09
申请号：US12790675
申请日：2010-05-28
申请人： Ronald Scott Bunker , Benjamin Paul Lacy
发明人： Ronald Scott Bunker , Benjamin Paul Lacy
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 which can be exposed to a first fluid; an inlet; and an outer surface 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. Each passage hole includes an inlet bore extending through the substrate from the inlet at the inner surface to a passage hole-exit proximate to the outer surface, with the inlet bore terminating in a chevron outlet adjacent the hole-exit. The chevron outlet includes a pair of wing troughs having a common surface region between them. The common surface region includes a valley which is adjacent the hole-exit; and a plateau adjacent the valley. The article can be an airfoil. Related methods for preparing the passage holes are also described.
摘要翻译：描述了一种制品，包括可暴露于第一流体的内表面; 一个入口以及与内表面间隔开的外表面，其可以暴露于较热的第二流体。该制品还包括至少一行或其它图案的通道孔。每个通孔包括从内表面的入口延伸穿过基底的入口孔，靠近外表面的通道孔出口，入口孔终止于邻近孔出口的人字形出口。人字形出口包括一对翼槽，它们之间具有共同的表面区域。公共表面区域包括与孔出口相邻的谷部; 和毗邻山谷的高原。文章可以是一个翼型。还描述了制备通道孔的相关方法。

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