Ultrasonic detection method and system
    1.
    发明公开
    Ultrasonic detection method and system 审中-公开
    Ultraschallerfassungsverfahren und System

    公开(公告)号:EP2765417A1

    公开(公告)日:2014-08-13

    申请号:EP14153940.3

    申请日:2014-02-05

    摘要: An ultrasonic detection method and system are disclosed. The ultrasonic detection method includes providing an ultrasonic detection system 100 having a first ultrasonic device arrangement 102 and a second ultrasonic device arrangement 104, positioning the ultrasonic detection system 100 in a peripheral offset position with respect to an object 106 to be measured, and transmitting and receiving an ultrasonic beam between the first ultrasonic device arrangement 102 and the second ultrasonic device arrangement 104, thereby obtaining ultrasonic detection information about the object 106. Additionally or alternatively, the transmitting and receiving of the ultrasonic detection method obtains data on a volume greater than that which is capable of being analyzed by a single probe arrangement. The ultrasonic detection system 100 includes the first ultrasonic device arrangement 102 and the second ultrasonic device arrangement 104 positioned in a peripheral offset position with respect to an object 106 to be measured.

    摘要翻译: 公开了一种超声波检测方法和系统。 超声波检测方法包括提供具有第一超声波装置装置102和第二超声波装置装置104的超声波检测系统100,将超声波检测系统100相对于要测量的对象106定位在外围偏移位置,以及 在第一超声波装置装置102和第二超声波装置装置104之间接收超声波束,从而获得关于对象106的超声波检测信息。另外或替代地,超声波检测方法的发送和接收获得大于 其能够通过单个探针装置进行分析。 超声波检测系统100包括第一超声波装置装置102和第二超声波装置装置104,该第二超声波装置装置相对于被测量物体106定位在周边偏移位置。

    Electrochemical machining method, tool assembly, and monitoring method
    3.
    发明公开
    Electrochemical machining method, tool assembly, and monitoring method 有权
    Werkzeuganordnung zum elektrochemischen Bearbeiten

    公开(公告)号:EP1529588A2

    公开(公告)日:2005-05-11

    申请号:EP04256970.7

    申请日:2004-11-10

    IPC分类号: B23H3/02

    CPC分类号: B23H3/02

    摘要: In an electrochemical machining tool assembly having at least one electrode (26) arranged across a gap (34) from a workpiece (12), the electrode being energized by application of a potential difference ΔV between the electrode and the workpiece, a method of monitoring machining includes exciting at least one ultrasonic sensor (42) to direct an ultrasonic wave toward a surface (102) of the electrode and receiving a reflected ultrasonic wave from the surface of the electrode using the ultrasonic sensor. The reflected ultrasonic wave includes a number of reflected waves from the surface of the electrode and from a surface of the workpiece. The method further includes delaying the excitation of the ultrasonic sensor a dwell time T d after a reduction of the potential difference ΔV across the electrode and the workpiece occurs.

    摘要翻译: 在电化学加工工具组件中,具有跨过工件(12)的间隙(34)布置的至少一个电极(26),通过在电极和工件之间施加电位差DELTA V来激励电极, 监测加工包括激励至少一个超声波传感器(42),以将超声波引向电极的表面(102),并使用超声波传感器从电极的表面接收反射的超声波。 反射的超声波包括从电极的表面和工件的表面的多个反射波。 该方法还包括在跨过电极和工件发生电位差DELTA V的减小之后延迟超声波传感器的激励停留时间Td。

    Turbomachine component monitoring system and method
    6.
    发明公开
    Turbomachine component monitoring system and method 有权
    系统和Verfahren zurÜberwachungeiner Turbomaschinenkomponente

    公开(公告)号:EP2778645A1

    公开(公告)日:2014-09-17

    申请号:EP14158803.8

    申请日:2014-03-11

    IPC分类号: G01M5/00

    摘要: Various embodiments include approaches for monitoring turbomachine components. In various particular embodiments, a system 2 for monitoring a component 6 within a turbomachine 4 includes: a borescope probe 22 sized to pass through an opening 14 in the turbomachine 4, the borescope probe 22 for detecting a symbolic data array 18 on the component 6 within the turbomachine 4; and at least one computing device 24 operably coupled to the borescope probe 22, the at least one computing device 24 configured to: obtain image data 30 about the symbolic data array 18 from the borescope probe 22; evaluate the image data 30 to determine whether the image data is compatible with a symbolic data array analysis program 28; and analyze the image data 30 using the symbolic data array analysis program 28 in response to determining the image data 30 is compatible with the symbolic data array analysis program 28.

    摘要翻译: 各种实施例包括用于监测涡轮机组件的方法。 在各种具体实施例中,用于监测涡轮机4内的部件6的系统2包括:尺寸适于穿过涡轮机4中的开口14的管道探针22,用于检测部件6上的符号数据阵列18的管道镜探头22 在涡轮机4内; 以及可操作地耦合到管道镜探针22的至少一个计算设备24,所述至少一个计算设备24被配置为:从管道镜探针22获得关于符号数据阵列18的图像数据30; 评估图像数据30以确定图像数据是否与符号数据阵列分析程序28兼容; 并且响应于确定图像数据30与符号数据阵列分析程序28兼容,使用符号数据阵列分析程序28分析图像数据30。

    Method And System For Online Creep Monitoring
    8.
    发明公开
    Method And System For Online Creep Monitoring 审中-公开
    Verfahren und System zur Online-Kriechüberwachung

    公开(公告)号:EP2469258A2

    公开(公告)日:2012-06-27

    申请号:EP11193135.8

    申请日:2011-12-13

    IPC分类号: G01M15/05

    CPC分类号: G01M5/0016

    摘要: A creep monitoring system (100) is provided. The system includes a creep sensor assembly (116) formed onto a surface of an object (114) rotatable about an axis, the creep sensor assembly including an image pattern (300), an optical monitoring system with line of sight to the creep sensor assembly, the optical monitoring system configured to collect information from the creep sensor assembly, a processor (110) programmed to receive the information, and determine at least one of an amount of creep (124) of the object.

    摘要翻译: 提供了一种蠕变监测系统(100)。 所述系统包括形成在可围绕轴线旋转的物体(114)的表面上的蠕变传感器组件(116),所述蠕变传感器组件包括图像图案(300),具有到所述蠕变传感器组件的视线的光学监控系统 ,所述光学监视系统被配置为从所述蠕变传感器组件收集信息,被编程为接收所述信息的处理器(110)以及确定所述对象的蠕变量(124)中的至少一个。

    High speed digital radiographic inspection of aircraft fuselages
    10.
    发明公开
    High speed digital radiographic inspection of aircraft fuselages 有权
    飞机机身的数字射线高速监控

    公开(公告)号:EP1130385A3

    公开(公告)日:2003-01-15

    申请号:EP01300075.7

    申请日:2001-01-05

    IPC分类号: G01N23/04

    CPC分类号: G01N23/04

    摘要: A system (10) and method for radiographic inspection of aircraft fuselage (12)s includes a radiation source (28) preferably located inside of the fuselage (12) and a radiation detector (32) preferably located outside of the fuselage (12). A source positioning system (30) is provided for moving the radiation source (28) longitudinally with respect to the fuselage (12), and a detector positioning system (34) is provided for positioning the radiation detector (32) in longitudinal alignment with the radiation source (28). The detector positioning system (34) also moves the radiation detector (32) circumferentially with respect to the fuselage (12). In operation, the radiation detector (32) is moved over the fuselage (12) in a circumferential direction while the radiation source (28) illuminates an adjacent region of the fuselage (12) with radiation.