会员体验
专利管家(专利管理)
工作空间(专利管理)
风险监控(情报监控)
数据分析(专利分析)
侵权分析(诉讼无效)
联系我们
交流群
官方交流:
QQ群: 891211   
微信请扫码    >>>
现在联系顾问~
热词
    • 1. 发明申请
    • METHOD AND APPARATUS FOR CALIBRATING A TORQUE MEASUREMENT
    • 用于校准扭矩测量的方法和装置
    • US20120210767A1
    • 2012-08-23
    • US13031770
    • 2011-02-22
    • Peter Ping-Liang SueLawrence Brown Farr, IIDerek Ray Wilson
    • Peter Ping-Liang SueLawrence Brown Farr, IIDerek Ray Wilson
    • G01L25/00
    • G01L25/003G01L3/12Y10T464/20
    • According to one aspect of the invention, a method for calibrating a torque measurement for a rotatable object is disclosed, wherein the method includes coupling the rotatable object to a structure, the structure including a member extending along a length of a surface of the rotatable object, coupling the rotatable object to an adapter and applying a known torque to the rotatable object via the adapter. The method also includes measuring a first rotational displacement via a first sensor coupled to the member at a first axial location of the rotatable object, measuring a second rotational displacement via a second sensor coupled to the member at a second axial location of the rotatable object and determining first and second angular displacements of the rotatable object based on the first and second rotational displacements.
    • 根据本发明的一个方面,公开了一种用于校准可旋转物体的扭矩测量的方法,其中所述方法包括将可旋转物体联接到结构上,所述结构包括沿着所述可旋转物体的表面的长度延伸的构件 将可旋转物体联接到适配器并且通过适配器将已知扭矩施加到可旋转物体上。 该方法还包括通过第一传感器测量第一传感器,第一传感器在可旋转对象的第一轴向位置处耦合到构件,经由第二传感器测量第二旋转位移,第二传感器在可旋转物体的第二轴向位置处联接到构件, 基于第一和第二旋转位移确定可旋转物体的第一和第二角位移。
    • 3. 发明授权
    • Method and apparatus for calibrating a torque measurement
    • 用于校准扭矩测量的方法和装置
    • US08539810B2
    • 2013-09-24
    • US13031770
    • 2011-02-22
    • Peter Ping-Liang SueLawrence Brown Farr, IIDerek Ray Wilson
    • Peter Ping-Liang SueLawrence Brown Farr, IIDerek Ray Wilson
    • G01L25/00
    • G01L25/003G01L3/12Y10T464/20
    • According to one aspect of the invention, a method for calibrating a torque measurement for a rotatable object is disclosed, wherein the method includes coupling the rotatable object to a structure, the structure including a member extending along a length of a surface of the rotatable object, coupling the rotatable object to an adapter and applying a known torque to the rotatable object via the adapter. The method also includes measuring a first rotational displacement via a first sensor coupled to the member at a first axial location of the rotatable object, measuring a second rotational displacement via a second sensor coupled to the member at a second axial location of the rotatable object and determining first and second angular displacements of the rotatable object based on the first and second rotational displacements.
    • 根据本发明的一个方面,公开了一种用于校准可旋转物体的扭矩测量的方法,其中所述方法包括将可旋转物体联接到结构上,所述结构包括沿着所述可旋转物体的表面的长度延伸的构件 将可旋转物体联接到适配器并且通过适配器将已知扭矩施加到可旋转物体上。 该方法还包括通过第一传感器测量第一传感器,第一传感器在可旋转对象的第一轴向位置处耦合到构件,经由第二传感器测量第二旋转位移,第二传感器在可旋转物体的第二轴向位置处联接到构件, 基于第一和第二旋转位移确定可旋转物体的第一和第二角位移。
    • 5. 发明授权
    • High resolution torque measurement on a rotating shaft with movement compensation
    • 在具有运动补偿的旋转轴上进行高分辨率扭矩测量
    • US07415363B2
    • 2008-08-19
    • US11162998
    • 2005-09-30
    • Peter Ping-Liang Sue
    • Peter Ping-Liang Sue
    • G01L3/00
    • G01L3/12
    • An apparatus for determining the torque imposed on a rotatable shaft. The shaft has at least four paired probes, paired horizontal probes and paired vertical probes. The horizontal probes are positioned 90 degrees apart from the vertical probes. If the shaft moves horizontally, the time of arrival detected by the first horizontal probes will be later than a nominal value and the time of arrival for the second horizontal probes will be earlier than a nominal value with the same amount of error. Combining data from the first and second horizontal probes will then automatically cancel out any error from horizontal motion. Similarly, combining data from vertical probes will eliminate the error due to vertical movement. Because any radial movement is a combination of horizontal and vertical movements, the use of the probes removes errors due to movement in any direction.
    • 一种用于确定施加在可旋转轴上的扭矩的装置。 轴具有至少四个成对的探针,成对的水平探针和成对的垂直探针。 水平探头与垂直探头分开定位90度。 如果轴水平移动,则由第一水平探头检测到的到达时间将晚于标称值,并且第二水平探头的到达时间将早于具有相同误差量的标称值。 结合第一和​​第二水平探头的数据将自动消除水平运动中的任何误差。 类似地,组合来自垂直探测器的数据将消除由于垂直移动引起的误差。 因为任何径向运动都是水平和垂直运动的组合,因此使用探头会消除由于任何方向的运动引起的误差。
    • 7. 发明申请
    • SYSTEMS AND METHODS FOR MEASURING TURBINE BLADE VIBRATORY RESPONSE
    • 用于测量涡轮叶片振动响应的系统和方法
    • US20110162457A1
    • 2011-07-07
    • US12652153
    • 2010-01-05
    • Peter Ping-Liang SueHolly DavisMichael Ball
    • Peter Ping-Liang SueHolly DavisMichael Ball
    • G01H1/00
    • G01H1/006G01H9/00G01H9/004G01H9/006
    • Certain embodiments of the invention may include systems and methods for measuring turbine blade vibratory responses. According to an example embodiment of the invention, a method is provided for measuring a vibratory response of a plurality of turbine blades. The method can include mounting an optical probe comprising at least one probe tip optical surface, wherein the at least one probe tip optical surface is substantially parallel to within about +15 or about −15 degrees with respect to a trailing edge surface of at least one of the plurality of turbine blades, directing light towards a trailing edge surface of at least one of the plurality of turbine blades, receiving reflected light from the at least one of the plurality of turbine blades, and determining relative position of the at least one of the plurality of blades based at least in part on the reflected light.
    • 本发明的某些实施例可以包括用于测量涡轮叶片振动响应的系统和方法。 根据本发明的示例性实施例,提供了一种用于测量多个涡轮叶片的振动响应的方法。 该方法可以包括安装包括至少一个探针尖端光学表面的光学探针,其中所述至少一个探针末端光学表面相对于至少一个的后缘表面基本上平行于约+15或约-15度 将多个涡轮机叶片中的至少一个涡轮机叶片的后缘表面引导到多个涡轮机叶片中的至少一个涡轮机叶片的后缘表面,接收来自多个涡轮机叶片中的至少一个的反射光,以及确定至少一个 所述多个叶片至少部分地基于所述反射光。
    • 8. 发明授权
    • System and method for positioning a sensor
    • 用于定位传感器的系统和方法
    • US08573078B2
    • 2013-11-05
    • US12952316
    • 2010-11-23
    • Peter Ping-Liang SueHolly Renae DavisTomasz Ryszard SzmigielPiotr Edward Kobek
    • Peter Ping-Liang SueHolly Renae DavisTomasz Ryszard SzmigielPiotr Edward Kobek
    • G01D21/00
    • F01D21/003F01D17/02F01D25/26G01D11/30
    • A system for positioning a sensor through an inner barrier and an outer barrier includes a first collar configured for engagement with the inner or outer barriers, a collapsible coupling, and a sensor support connected to the collapsible coupling. The collapsible coupling or the sensor support is in sealing engagement with the first collar, and the first collar, collapsible coupling, and sensor support define a passage therethrough. A method for positioning a sensor includes engaging a first collar to at least one of the inner barrier or the outer barrier and inserting a sensor support connected to a collapsible coupling through the outer barrier. The method further includes connecting the sensor support or the collapsible coupling to the first collar and inserting the sensor through the sensor support.
    • 用于通过内屏障和外屏障定位传感器的系统包括构造成用于与内屏障或外挡板接合的第一轴环,可折叠联接器和连接到可折叠联轴器的传感器支架。 可折叠联接器或传感器支撑件与第一套环密封接合,并且第一套环,可折叠联接器和传感器支撑件限定穿过其中的通道。 一种用于定位传感器的方法包括:将第一颈圈接合到所述内屏障或所述外屏障中的至少一个,并且插入通过所述外屏障连接到可折叠联接件的传感器支架。 该方法还包括将传感器支撑件或可折叠联接件连接到第一套环并将传感器插入传感器支撑件。
    • 9. 发明授权
    • Systems and methods for measuring turbine blade vibratory response
    • 用于测量涡轮叶片振动响应的系统和方法
    • US08256297B2
    • 2012-09-04
    • US12652153
    • 2010-01-05
    • Peter Ping-Liang SueHolly DavisMichael Ball
    • Peter Ping-Liang SueHolly DavisMichael Ball
    • G01H9/00G01N29/24G01N29/04
    • G01H1/006G01H9/00G01H9/004G01H9/006
    • Certain embodiments of the invention may include systems and methods for measuring turbine blade vibratory responses. According to an example embodiment of the invention, a method is provided for measuring a vibratory response of a plurality of turbine blades. The method can include mounting an optical probe comprising at least one probe tip optical surface, wherein the at least one probe tip optical surface is substantially parallel to within about +15 or about −15 degrees with respect to a trailing edge surface of at least one of the plurality of turbine blades, directing light towards a trailing edge surface of at least one of the plurality of turbine blades, receiving reflected light from the at least one of the plurality of turbine blades, and determining relative position of the at least one of the plurality of blades based at least in part on the reflected light.
    • 本发明的某些实施例可以包括用于测量涡轮叶片振动响应的系统和方法。 根据本发明的示例性实施例,提供了一种用于测量多个涡轮叶片的振动响应的方法。 该方法可以包括安装包括至少一个探针尖端光学表面的光学探针,其中所述至少一个探针末端光学表面相对于至少一个的后缘表面基本上平行于约+15或约-15度 将多个涡轮机叶片中的至少一个涡轮机叶片的后缘表面引导到多个涡轮机叶片中的至少一个涡轮机叶片的后缘表面,接收来自多个涡轮机叶片中的至少一个的反射光,以及确定至少一个 所述多个叶片至少部分地基于所述反射光。