Turbine blade core cooling apparatus and method of fabrication
    22.
    发明授权
    Turbine blade core cooling apparatus and method of fabrication 有权
    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

    IPC分类号: F01D518

    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。

    Method for quantifying film hole flow rates for film-cooled parts
    23.
    发明授权
    Method for quantifying film hole flow rates for film-cooled parts 有权
    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

    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。

    System and method for monitoring in real time, a gap between portions in a machine
    24.
    发明授权
    System and method for monitoring in real time, a gap between portions in a machine 有权
    用于实时监控的系统和方法,机器中部分之间的间隙

    公开(公告)号:US09488467B2

    公开(公告)日:2016-11-08

    申请号:US12913886

    申请日:2010-10-28

    IPC分类号: H04N7/18 G01B11/14

    CPC分类号: G01B11/14

    摘要: A monitoring system for monitoring, in real time, a gap between a rotating portion and a stationary portion of a machine. The monitoring system includes an imaging device for forming a reference image of the gap and one or more next images of the gap, the imaging device including a portion disposed within the machine and a portion external to the machine. The system also includes an image processor coupled to the imaging device configured to monitor whether the gap is increasing or decreasing by comparing the reference image to the one or more next images.

    摘要翻译: 一种用于实时监测机器的旋转部分和静止部分之间的间隙的监视系统。 监测系统包括用于形成间隙的参考图像和间隙的一个或多个下一图像的成像装置,成像装置包括设置在机器内的部分和机器外部的部分。 该系统还包括耦合到成像装置的图像处理器,该图像处理器被配置为通过将参考图像与一个或多个下一个图像进行比较来监视间隙是增加还是减小。

    Method, sensor and system for measuring a lower heating value and a Wobbe Index of a gaseous fuel
    25.
    发明授权
    Method, sensor and system for measuring a lower heating value and a Wobbe Index of a gaseous fuel 有权
    用于测量气体燃料的较低热值和沃泊指数的方法,传感器和系统

    公开(公告)号:US08486710B2

    公开(公告)日:2013-07-16

    申请号:US11299588

    申请日:2005-12-12

    IPC分类号: G01N33/00

    CPC分类号: G01N25/22 Y10T436/218

    摘要: A method for measuring a lower heating value of a gaseous fuel. The method includes mixing a gaseous fuel with air to provide a combustible air-fuel mixture. The air-fuel mixture is directed to flow across a flow surface of a first micro-hotplate maintained at a constant temperature. A change in power required to maintain a constant temperature of the first micro-hotplate flow surface due to a convective and conductive heat transfer from the first micro-hotplate flow surface to the air-fuel mixture is measured. The air-fuel mixture is directed to flow across a flow surface of a second micro-hotplate maintained at a constant temperature. The air-fuel mixture is combusted as the air-fuel mixture flows across the second micro-hotplate flow surface. A change in power required to maintain a constant temperature of the second micro-hotplate flow surface due to the combustion of the air-fuel mixture is measured.

    摘要翻译: 一种用于测量气体燃料的较低热值的方法。 该方法包括将气态燃料与空气混合以提供可燃空气 - 燃料混合物。 空气 - 燃料混合物被引导流过维持在恒定温度的第一微电热板的流动表面。 测量由于从第一微型加热板流动表面到空气 - 燃料混合物的对流和导电的热传递来维持第一微型电热板流动表面的恒定温度所需的功率变化。 空气 - 燃料混合物被引导流过维持在恒定温度的第二微电热板的流动表面。 空气燃料混合物随着空气 - 燃料混合物流过第二微电镀板流动表面而燃烧。 测量由于空气 - 燃料混合物的燃烧而保持第二微型加热板流动表面的恒定温度所需的功率变化。

    Thermal inspection system and method
    26.
    发明授权
    Thermal inspection system and method 失效
    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

    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。

    THERMAL INSPECTION SYSTEM AND METHOD
    27.
    发明申请
    THERMAL INSPECTION SYSTEM AND METHOD 失效
    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

    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。

    Systems, methods, and apparatus for detecting failure in gas turbine hardware
    29.
    发明授权
    Systems, methods, and apparatus for detecting failure in gas turbine hardware 有权
    用于检测燃气轮机硬件故障的系统,方法和装置

    公开(公告)号:US08818684B2

    公开(公告)日:2014-08-26

    申请号:US12761029

    申请日:2010-04-15

    IPC分类号: G06F19/00

    摘要: Certain embodiments of the invention may include systems, methods, and apparatus for detecting failure in gas turbine hardware. According to an example embodiment of the invention, a method for detecting a failure in a gas turbine is provided. The method can include monitoring a parameter associated with the turbine, wherein the monitored parameter comprises at least one turbine bucket temperature, detecting an event associated with operation of the turbine, wherein the event is based at least in part on the monitored parameter, and initiating shutdown of the turbine upon detection of the event wherein the monitored parameter is above a predetermined value for at least a predetermined time duration.

    摘要翻译: 本发明的某些实施例可以包括用于检测燃气轮机硬件故障的系统,方法和装置。 根据本发明的示例性实施例,提供了一种用于检测燃气轮机故障的方法。 该方法可以包括监测与涡轮相关联的参数,其中所监测的参数包括至少一个涡轮机桶温度,检测与涡轮机的运行相关联的事件,其中该事件至少部分地基于所监测的参数,并且启动 在检测到所监视的参数高于预定值至少预定持续时间的事件的情况下关闭涡轮机。