Valve control apparatus
    1.
    发明授权
    Valve control apparatus 失效
    阀门控制装置

    公开(公告)号:US5152309A

    公开(公告)日:1992-10-06

    申请号:US706912

    申请日:1991-05-29

    CPC classification number: G05D7/0635 Y10T137/0357 Y10T137/7759 Y10T137/7761

    Abstract: The present invention provides a valve control apparatus which can be programmed to deliver a desired flow of gas. A valve 22 is connected to a stepper motor 28 which is controlled by a computer 32 to open or close the valve in steps within a gas flow line 24 to deliver a desired rate of flow. A flowmeter 30 is provided along the gas flow line 24 for measuring the flow and inputting this flow to the computer 32. The computer 32 calculates rate of flow information obtained from the flowmeter 30 and controls the stepper motor 28 to open or close the valve 22 as necessary in accordance with the received rate of flow information and a desired rate of flow preprogrammed into the computer 32. As a result, a precise desired rate of flow can be obtained. Also, position indicators 34 may be added to the valve 22 to indicate when the valve 22 is completely open or completely closed. The valve 22 may be provided with a return spring 36 to automatically close the valve 22 in the event of a power loss. The computer 32 may be programmed to detect a significant increase in the rate of gas flow being closing the valve 22 accordingly. Additionally, a pressure switch 38 may be provided along the gas flow line 24 to cause the valve 22 to close upon a pressure change. Finally, temperature 40 and pressure 42 sensors may be added along the gas flow line so that the computer 32 can calculate and maintain a specific mass flow of gas.

    Abstract translation: 本发明提供了一种阀控制装置,其可编程为输送期望的气体流。 阀门22连接到步进马达28,步进马达28由计算机32控制,以在气体流动管线24内逐步打开或关闭阀门,以输送所需的流量。 沿着气体流路24设置流量计30,用于测量流量并将该流量输入到计算机32.计算机32计算从流量计30获得的流量信息,并控制步进马达28打开或关闭阀22 根据所接收的流量信息和预编程到计算机32中的期望流量,根据需要,可以获得精确的期望流量。 此外,位置指示器34可以被添加到阀22以指示阀22何时完全打开或完全关闭。 阀22可以设置有复位弹簧36,以在功率损失的情况下自动关闭阀22。 计算机32可以被编程为检测相应地关闭阀门22的气体流量的显着增加。 另外,压力开关38可以沿着气体流动管线24设置,以使得阀22在压力变化时闭合。 最后,温度40和压力42传感器可以沿着气体流动管线被添加,使得计算机32可以计算和维持气体的特定质量流量。

    Method of matching sensors in a multi-probe turbine blade vibration monitor
    3.
    发明授权
    Method of matching sensors in a multi-probe turbine blade vibration monitor 有权
    在多探头涡轮叶片振动监测器中匹配传感器的方法

    公开(公告)号:US08683866B2

    公开(公告)日:2014-04-01

    申请号:US13191711

    申请日:2011-07-27

    CPC classification number: G01H1/003 G01H1/08

    Abstract: A method of matching sensors in a multi-probe blade vibration monitor for a turbine. The method includes providing at least two probes mounted in a casing of the turbine adjacent to a rotating blade structure of the turbine. Targets are provided on radially outer portions of the blade structure. Each of the probes includes a sensor generating signals corresponding to target passing events, and a set of synchronous harmonics of the rotational speed of the rotor are produced for each sensor. The position of the sensors is adjusted such that the sets of harmonics of the sensors are substantially matched, indicating that the positions of the sensors are matched.

    Abstract translation: 一种用于涡轮机的多探针叶片振动监测器中匹配传感器的方法。 该方法包括提供安装在涡轮机壳体中的至少两个探针,其与涡轮机的旋转叶片结构相邻。 靶设置在叶片结构的径向外部。 每个探头包括产生对应于目标通过事件的信号的传感器,并且为每个传感器产生一组转子的转速的同步谐波。 调整传感器的位置,使得传感器的谐波组合基本匹配,表明传感器的位置匹配。

    Method for monitoring the condition of a vibration sensor
    4.
    发明授权
    Method for monitoring the condition of a vibration sensor 有权
    监测振动传感器状况的方法

    公开(公告)号:US08645101B2

    公开(公告)日:2014-02-04

    申请号:US13024496

    申请日:2011-02-10

    CPC classification number: G01H13/00

    Abstract: A system and method for monitoring the condition of a vibration sensor in a system. Vibrations are received in the system at one or more vibration sensors. Sensor data is output by the vibration sensor(s). The sensor data includes data representative of the vibrations in the system and data representative of a natural frequency of the corresponding vibration sensor. The sensor data output from the vibration sensor(s) is monitored, and upon a change in the data representative of the natural frequency of a vibration sensor, that vibration sensor is flagged.

    Abstract translation: 一种用于监测系统中的振动传感器的状态的系统和方法。 在一个或多个振动传感器的系统中接收振动。 传感器数据由振动传感器输出。 传感器数据包括表示系统中的振动的数据和表示相应的振动传感器的固有频率的数据。 监测从振动传感器输出的传感器数据,并且在代表振动传感器的固有频率的数据改变时,该振动传感器被标记。

    METHOD AND APPARATUS FOR DISTRIBUTED CLEFT AND LIBERATED TILE DETECTION ACHIEVING FULL COVERAGE OF THE TURBINE COMBUSTION CHAMBER
    5.
    发明申请
    METHOD AND APPARATUS FOR DISTRIBUTED CLEFT AND LIBERATED TILE DETECTION ACHIEVING FULL COVERAGE OF THE TURBINE COMBUSTION CHAMBER 审中-公开
    方法和装置,用于实现涡轮机燃烧室的全面覆盖的分布式和自动检测

    公开(公告)号:US20130008180A1

    公开(公告)日:2013-01-10

    申请号:US13177717

    申请日:2011-07-07

    Abstract: A component sensing system for monitoring the condition of ceramic tiles in a combustion chamber of a gas turbine engine. The sensing system includes an optical fiber that is mounted to the component being monitored, for example, the ceramic tiles in the gas turbine combustion chamber. The optical fiber can be formed in any suitable orientation or configuration, such as a meandering or serpentine orientation. The fiber is optically coupled to a Brillouin signal analyzer that provides an optical pulse to the sensing section of the fiber and detects Brillouin backscattering from the fiber as the pulse travels along the fiber. The frequency of the Brillouin backscattering signal is monitored relative to the distance along the sensing section of the fiber. A rise in temperature at a location of the fiber shows up in the analyzer as an increase in frequency of the backscattered signal.

    Abstract translation: 一种用于监测燃气涡轮发动机的燃烧室中的瓷砖状态的部件感测系统。 感测系统包括安装到被监测的部件的光纤,例如燃气轮机燃烧室中的陶瓷瓦。 光纤可以以任何合适的取向或构型形成,例如曲折或蛇形取向。 光纤光耦合到布里渊信号分析仪,其向光纤的感测部分提供光脉冲,并且随着脉冲沿着光纤行进,从光纤检测布里渊后向散射。 布里渊后向散射信号的频率相对于沿着光纤的感测部分的距离被监测。 随着反向散射信号频率的增加,光纤位置的温度上升在分析仪中出现。

    Method of measuring in situ differential emissivity and temperature
    6.
    发明授权
    Method of measuring in situ differential emissivity and temperature 有权
    测量原位差分发射率和温度的方法

    公开(公告)号:US08192077B2

    公开(公告)日:2012-06-05

    申请号:US12574096

    申请日:2009-10-06

    CPC classification number: G01J5/0003 G01J5/524 G01J5/602 G01J2005/0074

    Abstract: A method for measuring the differential emissivity between two sites on the surface of a body and the temperature of the two sites. The method includes a plurality of measurements of the infrared radiation arising from each of the two sites under a number of different conditions. Some of the measurements include irradiation by external infrared radiation at a known wavelength and intensity. The infrared radiation arising from each of the sites may include emitted radiation, reflected ambient radiation, and reflected external radiation. Additionally, the temperature determined using the method described can be used to calibrate infrared imaging devices used to inspect the entire body.

    Abstract translation: 一种用于测量身体表面两个位置与两个部位的温度之间的差异发射率的方法。 该方法包括在多个不同条件下从两个位置中的每一个产生的红外辐射的多个测量。 一些测量包括以已知波长和强度的外部红外辐射照射。 从每个地点产生的红外辐射可能包括发射的辐射,反射的环境辐射和反射的外部辐射。 另外,使用所述方法确定的温度可用于校准用于检查整个身体的红外成像装置。

    METHOD OF MATCHING SENSORS IN A MULTI-PROBE TURBINE BLADE VIBRATION MONITOR
    7.
    发明申请
    METHOD OF MATCHING SENSORS IN A MULTI-PROBE TURBINE BLADE VIBRATION MONITOR 有权
    在多个涡轮叶片振动监测器中匹配传感器的方法

    公开(公告)号:US20110277535A1

    公开(公告)日:2011-11-17

    申请号:US13191711

    申请日:2011-07-27

    CPC classification number: G01H1/003 G01H1/08

    Abstract: A method of matching sensors in a multi-probe blade vibration monitor for a turbine. The method includes providing at least two probes mounted in a casing of the turbine adjacent to a rotating blade structure of the turbine. Targets are provided on radially outer portions of the blade structure. Each of the probes includes a sensor generating signals corresponding to target passing events, and a set of synchronous harmonics of the rotational speed of the rotor are produced for each sensor. The position of the sensors is adjusted such that the sets of harmonics of the sensors are substantially matched, indicating that the positions of the sensors are matched.

    Abstract translation: 一种用于涡轮机的多探针叶片振动监测器中匹配传感器的方法。 该方法包括提供安装在涡轮机壳体中的至少两个探针,其与涡轮机的旋转叶片结构相邻。 靶设置在叶片结构的径向外部。 每个探头包括产生对应于目标通过事件的信号的传感器,并且为每个传感器产生一组转子的转速的同步谐波。 调整传感器的位置,使得传感器的谐波组合基本匹配,表明传感器的位置匹配。

    Method of on-line turbine blade slope and sensor position verification
    8.
    发明授权
    Method of on-line turbine blade slope and sensor position verification 有权
    在线涡轮叶片斜率和传感器位置验证方法

    公开(公告)号:US07775114B2

    公开(公告)日:2010-08-17

    申请号:US11861532

    申请日:2007-09-26

    CPC classification number: G01H1/003

    Abstract: A method of monitoring vibrations in a blade structure of a turbine including generating signals from a sensor located adjacent to a radial outer edge of the blade structure to sense passage of targets located on the blade structure. The sensor is mounted eccentrically and the signals are obtained with the sensor located at different angular positions. In a first aspect of the invention, the signals from the sensor are used to determine a target slope angle of a target on a first turbine blade during operation of the turbine. In a second aspect of the invention, the signals from the sensor are used to position the sensor in response to a sensed variation in the axial position of the target on the first turbine blade.

    Abstract translation: 一种监测涡轮机叶片结构中的振动的方法,包括从位于叶片结构的径向外边缘附近的传感器产生信号,以感测位于叶片结构上的目标的通过。 传感器偏心安装,传感器位于不同角度位置时获得信号。 在本发明的第一方面,来自传感器的信号用于在涡轮机运行期间确定目标在第一涡轮叶片上的目标倾斜角。 在本发明的第二方面,来自传感器的信号用于响应于目标在第一涡轮叶片上的轴向位置的感测变化来定位传感器。

    Non-synchronous vibrational excitation of turbine blades using a rotating excitation structure
    9.
    发明授权
    Non-synchronous vibrational excitation of turbine blades using a rotating excitation structure 有权
    使用旋转激励结构的涡轮叶片的非同步振动激励

    公开(公告)号:US07654145B2

    公开(公告)日:2010-02-02

    申请号:US11862752

    申请日:2007-09-27

    CPC classification number: G01H1/06 G01H1/003

    Abstract: A method of measuring vibration in a bladed rotor structure with a vibration monitor. The vibration monitor includes a sensor for sensing passage of the sensor targets on radially outer portions of the blade structure, and the sensor generates signals corresponding to target passing events. An excitation structure is provided including at least one air jet for providing an excitation force to the blade structure. The blade structure is rotated about an axis of rotation and the air jet is driven in a circular path about the axis of rotation at a different rotational speed to apply a non-synchronous excitation force to the blade structure.

    Abstract translation: 用振动监测器测量叶片转子结构中的振动的方法。 振动监测器包括用于感测传感器目标在叶片结构的径向外部上的通过的传感器,并且传感器产生对应于目标通过事件的信号。 提供了一种激励结构,其包括用于向叶片结构提供激励力的至少一个空气喷射。 叶片结构围绕旋转轴线旋转,并且空气射流以不同旋转速度的旋转轴线以圆形路径驱动,以将不同步的激励力施加到叶片结构。

    METHOD OF MEASURING IN SITU DIFFERENTIAL EMISSIVITY AND TEMPERATURE
    10.
    发明申请
    METHOD OF MEASURING IN SITU DIFFERENTIAL EMISSIVITY AND TEMPERATURE 有权
    测量差异发生和温度的方法

    公开(公告)号:US20100014555A1

    公开(公告)日:2010-01-21

    申请号:US12574096

    申请日:2009-10-06

    CPC classification number: G01J5/0003 G01J5/524 G01J5/602 G01J2005/0074

    Abstract: A method for measuring the differential emissivity between two sites on the surface of a body and the temperature of the two sites. The method includes a plurality of measurements of the infrared radiation arising from each of the two sites under a number of different conditions. Some of the measurements include irradiation by external infrared radiation at a known wavelength and intensity. The infrared radiation arising from each of the sites may include emitted radiation, reflected ambient radiation, and reflected external radiation. Additionally, the temperature determined using the method described can be used to calibrate infrared imaging devices used to inspect the entire body.

    Abstract translation: 一种用于测量身体表面两个位置与两个部位的温度之间的差异发射率的方法。 该方法包括在多个不同条件下从两个位置中的每一个产生的红外辐射的多个测量。 一些测量包括以已知波长和强度的外部红外辐射照射。 从每个地点产生的红外辐射可能包括发射的辐射,反射的环境辐射和反射的外部辐射。 另外,使用所述方法确定的温度可用于校准用于检查整个身体的红外成像装置。

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