专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明授权

US09335215B2 Method and system for gas temperature measurement 有权
标题翻译：气体温度测量方法和系统
公开(公告)号：US09335215B2
公开(公告)日：2016-05-10
申请号：US13563024
申请日：2012-07-31
申请人： Guanghua Wang , Nirm Velumylum Nirmalan , Todd Garrett Wetzel , Ronald Scott Bunker , Robert Michael Zacharias , Shawn David Wehe , Robert David Briggs , Jonathan Edward Slepski
发明人： Guanghua Wang , Nirm Velumylum Nirmalan , Todd Garrett Wetzel , Ronald Scott Bunker , Robert Michael Zacharias , Shawn David Wehe , Robert David Briggs , Jonathan Edward Slepski
IPC分类号： G01J5/00 , G01K1/14 , G01K13/00 , G01K3/00 , F01D17/08 , F02C9/28 , G01J5/08 , G01J5/60 , G01J5/10
CPC分类号： G01J5/0014 , F01D17/085 , F02C9/28 , F05D2260/80 , F05D2270/303 , G01J5/0862 , G01J5/0896 , G01J5/602 , G01J2005/106
摘要： A temperature measurement system includes at least one filament configured to emit thermal radiation in a relatively broad and substantially continuous wavelength band that is at least partially representative of a temperature of the at least one filament. The system also includes an optical system configured to receive at least a portion of the thermal radiation emitted from the filament. The optical system includes a wavelength splitting device configured to split the emitted thermal radiation into at least one relatively narrow wavelength band of thermal radiation. The optical system also includes a detector array configured to receive the at least one relatively narrow wavelength band of thermal radiation and to generate electrical signals at least partially representative of the received thermal radiation. The temperature measurement system further includes a controller communicatively coupled to the detector array. The controller is configured to transform the generated electrical signals to a temperature indication using a predetermined conversion module.
摘要翻译：温度测量系统包括至少一根被配置成在相对宽且基本上连续的波长带中发射热辐射的灯丝，其至少部分地代表至少一根灯丝的温度。该系统还包括被配置为接收从灯丝发射的热辐射的至少一部分的光学系统。光学系统包括波长分离装置，其被配置为将发射的热辐射分裂成至少一个相对较窄的热辐射波长带。光学系统还包括被配置为接收至少一个相对较窄的热辐射波段的检测器阵列，并且产生至少部分地表示所接受的热辐射的电信号。温度测量系统还包括通信地耦合到检测器阵列的控制器。控制器被配置为使用预定的转换模块将生成的电信号转换成温度指示。

2. 发明申请

US20140033737A1 METHOD AND SYSTEM FOR GAS TEMPERATURE MEASUREMENT 有权
标题翻译：气温测量方法与系统
公开(公告)号：US20140033737A1
公开(公告)日：2014-02-06
申请号：US13563024
申请日：2012-07-31
申请人： Guanghua Wang , Nirm Velumylum Nirmalan , Todd Garrett Wetzel , Ronald Scott Bunker , Robert Michael Zacharias , Shawn David Wehe , Robert David Briggs , Jonathan Edward Slepski
发明人： Guanghua Wang , Nirm Velumylum Nirmalan , Todd Garrett Wetzel , Ronald Scott Bunker , Robert Michael Zacharias , Shawn David Wehe , Robert David Briggs , Jonathan Edward Slepski
IPC分类号： G01J5/00 , F02C7/00
CPC分类号： G01J5/0014 , F01D17/085 , F02C9/28 , F05D2260/80 , F05D2270/303 , G01J5/0862 , G01J5/0896 , G01J5/602 , G01J2005/106
摘要： A temperature measurement system includes at least one filament configured to emit thermal radiation in a relatively broad and substantially continuous wavelength band that is at least partially representative of a temperature of the at least one filament. The system also includes an optical system configured to receive at least a portion of the thermal radiation emitted from the filament. The optical system includes a wavelength splitting device configured to split the emitted thermal radiation into at least one relatively narrow wavelength band of thermal radiation. The optical system also includes a detector array configured to receive the at least one relatively narrow wavelength band of thermal radiation and to generate electrical signals at least partially representative of the received thermal radiation. The temperature measurement system further includes a controller communicatively coupled to the detector array. The controller is configured to transform the generated electrical signals to a temperature indication using a predetermined conversion module.
摘要翻译：温度测量系统包括至少一根被配置成在相对宽且基本上连续的波长带中发射热辐射的灯丝，其至少部分代表至少一根灯丝的温度。该系统还包括被配置为接收从灯丝发射的热辐射的至少一部分的光学系统。光学系统包括波长分离装置，其被配置为将发射的热辐射分裂成至少一个相对较窄的热辐射波长带。光学系统还包括被配置为接收至少一个相对较窄的热辐射波段的检测器阵列，并且产生至少部分地表示所接受的热辐射的电信号。温度测量系统还包括通信地耦合到检测器阵列的控制器。控制器被配置为使用预定的转换模块将生成的电信号转换成温度指示。

3. 发明授权

US06773231B2 Turbine blade core cooling apparatus and method of fabrication 有权
标题翻译：涡轮叶片芯冷却装置及其制造方法
公开(公告)号：US06773231B2
公开(公告)日：2004-08-10
申请号：US10162755
申请日：2002-06-06
申请人： Ronald Scott Bunker , Frederic Joseph Klug , Shyh-Chin Huang , Susan Marie Hyde , Nirm Velumylum Nirmalan
发明人： Ronald Scott Bunker , Frederic Joseph Klug , Shyh-Chin Huang , Susan Marie Hyde , Nirm Velumylum Nirmalan
IPC分类号： F01D518
CPC分类号： F01D5/225 , B22C9/04 , B22C9/10 , F01D5/187 , F05D2260/22141 , Y02T50/671 , Y02T50/673 , Y02T50/676
摘要： The present invention provides a cooling apparatus for cooling a turbine blade. The cooling apparatus comprises a pressure side plate comprising a plurality of pressure ribs, a suction side plate comprising a plurality of suction ribs, and a plurality of flow redirection areas. The pressure side plate is disposed over the suction side plate, where the pressure ribs are disposed at a first angle with respect to a blade span reference line and the suction ribs are disposed at a second angle with respect to the blade span reference line, to form the flow redirection areas. The present invention provides a method of fabricating the cooling apparatus for the turbine blade comprising aligning the pressure side plate and the suction side plate to form the plurality of flow redirection areas between the pressure side plate and the suction side plate.
摘要翻译：本发明提供一种用于冷却涡轮叶片的冷却装置。冷却装置包括压力侧板，其包括多个加压肋，包括多个吸入肋的吸力侧板和多个流动重定向区域。压力侧板设置在吸力侧板上方，其中压力肋相对于叶片跨度基准线以第一角度设置，并且抽吸肋相对于叶片跨距参考线设置成第二角度，形成流重定向区域。本发明提供一种制造涡轮叶片的冷却装置的方法，包括使压力侧板和吸力侧板对准，以在压力侧板和吸力侧板之间形成多个流动重定向区域。

4. 发明授权

US06732582B2 Method for quantifying film hole flow rates for film-cooled parts 有权
标题翻译：薄膜冷却部件薄膜孔流量的定量方法
公开(公告)号：US06732582B2
公开(公告)日：2004-05-11
申请号：US10064855
申请日：2002-08-23
申请人： Ronald Scott Bunker , Nirm Velumylum Nirmalan
发明人： Ronald Scott Bunker , Nirm Velumylum Nirmalan
IPC分类号： G01K1710
CPC分类号： G01F1/6884 , G01F1/68
摘要： To measure the flow rate of coolant through a cooling hole of a film-cooled part, a transient thermal response of an external surface temperature of the film-cooled part is measured and the transient thermal response is characterized mathematically. From the mathematical characterization, the flow rate through the film hole is determined.
摘要翻译：为了测量通过薄膜冷却部件的冷却孔的冷却剂的流速，测量薄膜冷却部件的外表面温度的瞬时热响应，并且数学地表征瞬态热响应。从数学表征中，确定通过膜孔的流速。

5. 发明授权

US06804622B2 Method and apparatus for non-destructive thermal inspection 有权
标题翻译：非破坏性热检测方法和装置
公开(公告)号：US06804622B2
公开(公告)日：2004-10-12
申请号：US09945990
申请日：2001-09-04
申请人： Ronald Scott Bunker , Nirm Velumylum Nirmalan , Louis Andrew Schick
发明人： Ronald Scott Bunker , Nirm Velumylum Nirmalan , Louis Andrew Schick
IPC分类号： G06F1500
CPC分类号： G01N25/18 , G01K11/30 , G01N25/72
摘要： A method of quantitative non-destructive thermal inspection of an article having at least one internal cavity comprises the steps of inputting physical properties of the article, measuring thermal characteristics of the article, and calculating heat transfer coefficients of the internal cavity.
摘要翻译：具有至少一个内腔的制品的定量非破坏性热检查方法包括输入制品的物理性能，测量制品的热特性以及计算内腔的传热系数的步骤。

6. 发明授权

US07909507B2 Thermal inspection system and method 失效
标题翻译：热检查系统及方法
公开(公告)号：US07909507B2
公开(公告)日：2011-03-22
申请号：US12101285
申请日：2008-04-11
申请人： Ronald Scott Bunker , Nirm Velumylum Nirmalan
发明人： Ronald Scott Bunker , Nirm Velumylum Nirmalan
IPC分类号： G01N25/00 , G01J5/00 , G01K13/00
CPC分类号： G01K17/00 , G01F1/68 , G01K17/20
摘要： A thermal inspection method is provided for a component comprising at least one complex internal passage arrangement defining at least one opening. The thermal inspection method includes flowing a fluid through the at least one complex internal passage arrangement. The fluid has an initial temperature that differs from an initial temperature of the component. The thermal inspection method further includes measuring a thermal response of the component to the fluid flow and analyzing the thermal response to determine a number of heat transfer coefficients {hlmn} corresponding to respective locations {l,m,n} within the complex internal passage arrangement. The thermal inspection method further includes using the heat transfer coefficients {hlmn} to determine at least one of (a) a flow rate through respective ones of the at least one opening, and (b) a cross-sectional area for respective ones of the at least one opening.
摘要翻译：为包括限定至少一个开口的至少一个复杂内部通道装置的部件提供热检查方法。热检查方法包括使流体流过至少一个复合内部通道装置。流体具有不同于组件的初始温度的初始温度。热检测方法还包括测量部件对流体流的热响应并分析热响应以确定与复合内通道装置内的各个位置{1，m，n}对应的多个传热系数{hlmn} 。热检测方法还包括使用传热系数（hlmn）来确定（a）通过至少一个开口中的相应的一个开口的流量中的至少一个，和（b）相应的一个开口的横截面积至少一个开口。

7. 发明申请

US20090255332A1 THERMAL INSPECTION SYSTEM AND METHOD 失效
标题翻译：热检查系统和方法
公开(公告)号：US20090255332A1
公开(公告)日：2009-10-15
申请号：US12101285
申请日：2008-04-11
申请人： Ronald Scott Bunker , Nirm Velumylum Nirmalan
发明人： Ronald Scott Bunker , Nirm Velumylum Nirmalan
IPC分类号： G01F1/68 , G01K13/00
CPC分类号： G01K17/00 , G01F1/68 , G01K17/20
摘要： A thermal inspection method is provided for a component comprising at least one complex internal passage arrangement defining at least one opening. The thermal inspection method includes flowing a fluid through the at least one complex internal passage arrangement. The fluid has an initial temperature that differs from an initial temperature of the component. The thermal inspection method further includes measuring a thermal response of the component to the fluid flow and analyzing the thermal response to determine a number of heat transfer coefficients {hlmn} corresponding to respective locations {l,m,n} within the complex internal passage arrangement. The thermal inspection method further includes using the heat transfer coefficients {hlmn} to determine at least one of (a) a flow rate through respective ones of the at least one opening, and (b) a cross-sectional area for respective ones of the at least one opening.
摘要翻译：为包括限定至少一个开口的至少一个复杂内部通道装置的部件提供热检查方法。热检查方法包括使流体流过至少一个复杂的内部通道装置。流体具有不同于组件的初始温度的初始温度。热检测方法还包括测量部件对流体流的热响应并分析热响应以确定与复合内通道装置内的各个位置{1，m，n}对应的多个传热系数{hlmn} 。热检测方法还包括使用传热系数（hlmn）来确定（a）通过至少一个开口中的相应的一个开口的流量中的至少一个，和（b）相应的一个开口的横截面积至少一个开口。

8. 发明申请

US20120145371A1 COMPONENTS WITH COOLING CHANNELS AND METHODS OF MANUFACTURE 有权
标题翻译：具有冷却通道的组件和制造方法
公开(公告)号：US20120145371A1
公开(公告)日：2012-06-14
申请号：US12965083
申请日：2010-12-10
申请人： Ronald Scott Bunker , Todd Garrett Wetzel
发明人： Ronald Scott Bunker , Todd Garrett Wetzel
IPC分类号： F28F1/00 , B05D3/12 , B05D3/06 , B05D3/14 , C25F3/02 , B23H1/00 , B05D3/00 , B05D3/10
CPC分类号： F01D5/18 , F01D5/147 , F01D5/28 , F01D5/288 , F05D2260/202 , Y02T50/67 , Y02T50/672 , Y02T50/676
摘要： A component is disclosed. The component includes a substrate comprising an outer surface and an inner surface. The inner surface defines at least one hollow, interior space, and the outer surface defines one or more grooves that extend at least partially along the outer substrate surface and have a respective base. One or more access holes are formed through the base of a respective groove, to connect the groove in fluid communication with the respective hollow interior space. The component further includes a coating comprising one or more layers disposed over at least a portion of the outer substrate surface. The groove(s) and the coating together define one or more channels for cooling the component. One or more trenches are formed through one or more coating layers and at least partially define at least one exit region for the cooling channel(s). A method of fabricating a component is also provided.
摘要翻译：公开了一个组件。该组件包括包括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，并且外表面限定一个或多个凹槽，其至少部分地沿着外部衬底表面延伸并且具有相应的底座。通过相应凹槽的基部形成一个或多个通孔，以将凹槽与相应的中空内部空间流体连通。该组件还包括涂层，其包括设置在外基材表面的至少一部分上的一层或多层。凹槽和涂层一起限定一个或多个通道用于冷却部件。一个或多个沟槽通过一个或多个涂层形成，并且至少部分地限定用于冷却通道的至少一个出口区域。还提供了一种制造部件的方法。

9. 发明授权

US08727727B2 Components with cooling channels and methods of manufacture 有权
标题翻译：具有冷却通道和制造方法的部件
公开(公告)号：US08727727B2
公开(公告)日：2014-05-20
申请号：US12965083
申请日：2010-12-10
申请人： Ronald Scott Bunker , Todd Garrett Wetzel
发明人： Ronald Scott Bunker , Todd Garrett Wetzel
IPC分类号： F01D5/18
CPC分类号： F01D5/18 , F01D5/147 , F01D5/28 , F01D5/288 , F05D2260/202 , Y02T50/67 , Y02T50/672 , Y02T50/676
摘要： A component is disclosed. The component includes a substrate comprising an outer surface and an inner surface. The inner surface defines at least one hollow, interior space, and the outer surface defines one or more grooves that extend at least partially along the outer substrate surface and have a respective base. One or more access holes are formed through the base of a respective groove, to connect the groove in fluid communication with the respective hollow interior space. The component further includes a coating comprising one or more layers disposed over at least a portion of the outer substrate surface. The groove(s) and the coating together define one or more channels for cooling the component. One or more trenches are formed through one or more coating layers and at least partially define at least one exit region for the cooling channel(s). A method of fabricating a component is also provided.
摘要翻译：公开了一个组件。该组件包括包括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，并且外表面限定一个或多个凹槽，其至少部分地沿着外部衬底表面延伸并且具有相应的底座。通过相应凹槽的基部形成一个或多个通孔，以将凹槽与相应的中空内部空间流体连通。该组件还包括涂层，其包括设置在外基材表面的至少一部分上的一层或多层。凹槽和涂层一起限定一个或多个通道以冷却部件。一个或多个沟槽通过一个或多个涂层形成，并且至少部分地限定用于冷却通道的至少一个出口区域。还提供了一种制造部件的方法。

10. 发明授权

US06504274B2 Generator stator cooling design with concavity surfaces 有权
公开(公告)号：US06504274B2
公开(公告)日：2003-01-07
申请号：US09754701
申请日：2001-01-04
申请人： Ronald Scott Bunker , Todd Garrett Wetzel , Emil Donald Jarczynski
发明人： Ronald Scott Bunker , Todd Garrett Wetzel , Emil Donald Jarczynski
IPC分类号： H02K900
CPC分类号： H02K1/20
摘要： A stator core assembly comprising adjacent packages of stacked lamination sheets that are separated by a plurality of radially extending spacer blocks, and each adjacent pair of spacer blocks define in cooperation with adjacent axially spaced laminations, a plurality of radial cooling ducts, each duct having a least one lamination surface having plurality of concavities.

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式