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1.发明授权Multi-frequency image processing for inspecting parts having complex geometric shapes 失效用于检查具有复杂几何形状的零件的多频图像处理公开(公告)号：US07817845B2
公开(公告)日：2010-10-19
申请号：US11617859
申请日：2006-12-29
申请人： Ui Won Suh , Gigi Olive Gambrell , William Stewart McKnight , Preeti Pisupati , Peyush Kumar Mishra , Sandeep Kumar Dewangan , Changting Wang
发明人： Ui Won Suh , Gigi Olive Gambrell , William Stewart McKnight , Preeti Pisupati , Peyush Kumar Mishra , Sandeep Kumar Dewangan , Changting Wang
CPC分类号： G01N27/9046 , G01N27/902 , G06K9/4604
摘要： A method for detecting small cracks and other anomalies on parts having complex geometries is disclosed. The method includes eddy current inspection incorporating collection of data from multi-frequency eddy current signals. Phase analysis is used to combine the multi-frequency data to enhance the signal to noise ratio of the raw inspection image. The image is then reprocessed using a spatiotemporal filter to correlate with the frequency components of the eddy current flaw signal to separate signals associated with cracks and other flaws at edges that would ordinarily be hidden by edge effect signals.
摘要翻译： 公开了一种用于检测具有复杂几何形状的部件上的小裂纹和其他异常的方法。 该方法包括涡流检测，包括从多频涡流信号中收集的数据。 相位分析用于组合多频数据，增强原始检查图像的信噪比。 然后使用时空滤波器对图像进行再处理，以与涡流缺陷信号的频率分量相关联，以分离与通常由边缘效应信号隐藏的边缘处的裂纹和其他缺陷相关的信号。
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公开(公告)号：US20120143908A1
公开(公告)日：2012-06-07
申请号：US13369706
申请日：2012-02-09
申请人： Veera Venkata Ravi Kumar Geddam , Sambasiva Rao Maddali , Devaraja Holla Vaderahobli , Narendhar Rao Soma , Rajesh Balakrishnan , Venugopal Subbarao , Sandeep Kumar Dewangan
发明人： Veera Venkata Ravi Kumar Geddam , Sambasiva Rao Maddali , Devaraja Holla Vaderahobli , Narendhar Rao Soma , Rajesh Balakrishnan , Venugopal Subbarao , Sandeep Kumar Dewangan
IPC分类号： G06F17/30
摘要： A framework for supporting one or more repair processes of one or more aircraft. The repair processes are based on repair information or repair solution corresponding to the damages to one or more structural components of the aircraft. The framework includes a knowledge engine, and a deployment engine. The knowledge engine automatically generates one or more knowledge interpretation systems based on the user inputs. The knowledge interpretation systems provide the repair information corresponding to the various structural components of the aircraft based on the user inputs. The deployment engine fulfils the deployment requirements corresponding to the one or more knowledge interpretation systems.
摘要翻译： 用于支持一个或多个飞机的一个或多个维修过程的框架。 修理过程基于与飞机的一个或多个结构部件的损坏相对应的修理信息或修理解决方案。 框架包括知识引擎和部署引擎。 知识引擎基于用户输入自动生成一个或多个知识解释系统。 知识解释系统基于用户输入提供对应于飞行器的各种结构部件的修复信息。 部署引擎满足与一个或多个知识解释系统相对应的部署要求。
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公开(公告)号：US20100318396A1
公开(公告)日：2010-12-16
申请号：US12511211
申请日：2009-07-29
申请人： Veera Venkata Ravi Kumar Geddam , Sambasiva Rao Maddali , Devaraja Holla Vaderahobli , Narendhar Rao Soma , Rajesh Balakrishnan , Venugopal Subbarao , Sandeep Kumar Dewangan
发明人： Veera Venkata Ravi Kumar Geddam , Sambasiva Rao Maddali , Devaraja Holla Vaderahobli , Narendhar Rao Soma , Rajesh Balakrishnan , Venugopal Subbarao , Sandeep Kumar Dewangan
摘要： A framework for supporting one or more repair processes of one or more aircraft. The repair processes are based on repair information or repair solution corresponding to the damages to one or more structural components of the aircraft. The framework includes a knowledge engine, and a deployment engine. The knowledge engine automatically generates one or more knowledge interpretation systems based on the user inputs. The knowledge interpretation systems provide the repair information corresponding to the various structural components of the aircraft based on the user inputs. The deployment engine fulfils the deployment requirements corresponding to the one or more knowledge interpretation systems.
摘要翻译： 用于支持一个或多个飞机的一个或多个维修过程的框架。 修理过程基于与飞机的一个或多个结构部件的损坏相对应的修理信息或修理解决方案。 框架包括知识引擎和部署引擎。 知识引擎基于用户输入自动生成一个或多个知识解释系统。 知识解释系统基于用户输入提供对应于飞行器的各种结构部件的修复信息。 部署引擎满足与一个或多个知识解释系统相对应的部署要求。
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公开(公告)号：US07299697B2
公开(公告)日：2007-11-27
申请号：US11094909
申请日：2005-03-31
IPC分类号： G01N29/11
CPC分类号： G01N29/07 , G01N29/0645 , G01N29/069 , G01N29/11 , G01N29/343 , G01N29/4463 , G01N2291/0258 , G01N2291/0289 , G01N2291/0422 , G01N2291/044 , G01N2291/105 , G01N2291/2636
摘要： A method and apparatus for estimating a depth of a crack from ultrasound scan data are provided. The method includes mapping multiple amplitude responses from the ultrasound scan data, each mapped amplitude response being representative of a signal from one of the sensors. The method further includes locating multiple linear responses among the mapped amplitude responses, each linear response being an indicator of a reflected signal from the crack. One or more sensor that corresponds to the linear responses from a given crack is identified. The depth of the crack is estimated using data from the identified sensors.
摘要翻译： 提供了一种用于从超声扫描数据估计裂纹深度的方法和装置。 该方法包括从超声扫描数据映射多个幅度响应，每个映射幅度响应代表来自传感器之一的信号。 该方法还包括在映射的幅度响应之间定位多个线性响应，每个线性响应是来自裂纹的反射信号的指示符。 识别与给定裂纹的线性响应对应的一个或多个传感器。 使用来自识别的传感器的数据来估计裂纹的深度。
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5.发明授权System and method for calculating a comprehensive pipeline integrity business risk score 有权用于计算综合管道完整性业务风险评分的系统和方法公开(公告)号：US08510147B2
公开(公告)日：2013-08-13
申请号：US12699384
申请日：2010-02-03
申请人： Dipayan Mitra , Sandeep Kumar Dewangan , Larry Joesph Rubenacker , Manish Verma , Prakash Dhake , Paras Sachdeva
发明人： Dipayan Mitra , Sandeep Kumar Dewangan , Larry Joesph Rubenacker , Manish Verma , Prakash Dhake , Paras Sachdeva
IPC分类号： G06Q10/00
CPC分类号： G06Q40/08 , G06Q10/0635 , G06Q10/067 , G06Q10/08 , G06Q30/018
摘要： A method and system for calculating pipeline integrity business risk score for a pipeline network is provided. The method includes a step of first calculating a structural risk score, an operational risk score and a commercial risk score for each pipeline segment in a pipeline network. The method further includes calculating pipeline integrity business risk score for each pipeline segment. The structural risk score, operational risk score, commercial risk score and pipeline integrity business risk score for each pipeline segment is rolled-up to calculate the respective risk scores of a pipeline network. The rolled-up risk scores are calculated by computing weight factors for each pipeline segment, relative risk scores weight of each pipeline segment and relative risk scores contribution of each pipeline segment. The system of the invention comprises executable files, dynamic linked libraries and risk score computing modules configured to display the risk scores using a dashboard.
摘要翻译： 提供了一种用于计算管道网络管道完整性业务风险评分的方法和系统。 该方法包括首先计算管道网络中每个管道段的结构风险评分，操作风险评分和商业风险评分的步骤。 该方法还包括计算每个管道段的管道完整性业务风险评分。 汇总每个管道段的结构风险评分，操作风险评分，商业风险评分和管道完整性业务风险评分，以计算管道网络各自的风险评分。 卷积风险评分通过计算每个管道段的权重因子，每个管道段的相对风险分数权重和每个管道段的相对风险分数贡献来计算。 本发明的系统包括被配置为使用仪表板显示风险分数的可执行文件，动态链接库和风险评分计算模块。
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6.发明授权公开(公告)号：US07305885B2
公开(公告)日：2007-12-11
申请号：US10955804
申请日：2004-09-30
IPC分类号： G01N29/06 , G01N29/265
CPC分类号： G01N29/043 , B61K9/10 , G01N29/262 , G01N2291/02854 , G01N2291/0422 , G01N2291/0428 , G01N2291/044 , G01N2291/106 , G01N2291/2623
摘要： In accordance with one embodiment, the present technique provides a testing apparatus for testing material integrity of an object. The exemplary testing apparatus includes a phased array transducer, which is disposed external to the object. The phased array transducer is configured to transmit a first set of ultrasonic signals and to receive a second set of ultrasonic signals. The testing apparatus further includes logic circuitry coupled to the phased array transducer. The logic circuitry is configured to dynamically control apertures for transmitting the first set of ultrasonic signals and receiving the second set of ultrasonic signals based on a region of interest and a testing speed.
摘要翻译： 根据一个实施例，本技术提供了一种用于测试物体的材料完整性的测试装置。 示例性测试装置包括位于物体外部的相控阵转换器。 相控阵转换器被配置为传送第一组超声信号并接收第二组超声波信号。 测试装置还包括耦合到相控阵转换器的逻辑电路。 逻辑电路被配置为动态地控制用于发送第一组超声波信号的孔径，并且基于感兴趣的区域和测试速度接收第二组超声波信号。
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公开(公告)号：US06911826B2
公开(公告)日：2005-06-28
申请号：US10727401
申请日：2003-12-03
申请人： Yuri Alexeyevich Plotnikov , Thomas James Batzinger , Shridhar Champaknath Nath , Sandeep Kumar Dewangan , Carl Stephen Lester , Kenneth Gordon Herd , Curtis Wayne Rose
发明人： Yuri Alexeyevich Plotnikov , Thomas James Batzinger , Shridhar Champaknath Nath , Sandeep Kumar Dewangan , Carl Stephen Lester , Kenneth Gordon Herd , Curtis Wayne Rose
CPC分类号： G01N27/904
摘要： A pulsed eddy current sensor probe includes a sensor array board. A number of sensors are arranged on the sensor array board and are operable to sense and generate output signals from the transient electromagnetic flux in a part being inspected. Each of the sensors has a differential output with a positive and a negative output. At least one drive coil is disposed adjacent to the sensors and is operable to transmit transient electromagnetic flux into the part. A first and a second multiplexer are arranged on the sensor array board and are operable to switch between the sensors. The first and second multiplexers are connected to the positive and negative outputs of the sensors, respectively.
摘要翻译： 脉冲涡流传感器探头包括传感器阵列板。 多个传感器布置在传感器阵列板上，并且可操作以在被检查的部件中感测并产生来自瞬态电磁通量的输出信号。 每个传感器都具有带正和负输出的差分输出。 至少一个驱动线圈被布置成与传感器相邻，并且可操作以将瞬态电磁通量传输到该部件中。 第一和第二多路复用器布置在传感器阵列板上并可操作以在传感器之间切换。 第一和第二多路复用器分别连接到传感器的正和负输出。
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公开(公告)号：US08670893B2
公开(公告)日：2014-03-11
申请号：US13369706
申请日：2012-02-09
申请人： Veera Venkata Ravi Kumar Geddam , Sambasiva Rao Maddali , Devaraja Holla Vaderahobli , Narendhar Rao Soma , Rajesh Balakrishnan , Venugopal Subbarao , Sandeep Kumar Dewangan
发明人： Veera Venkata Ravi Kumar Geddam , Sambasiva Rao Maddali , Devaraja Holla Vaderahobli , Narendhar Rao Soma , Rajesh Balakrishnan , Venugopal Subbarao , Sandeep Kumar Dewangan
摘要： A framework for supporting one or more repair processes of one or more aircraft. The repair processes are based on repair information or repair solution corresponding to the damages to one or more structural components of the aircraft. The framework includes a knowledge engine, and a deployment engine. The knowledge engine automatically generates one or more knowledge interpretation systems based on the user inputs. The knowledge interpretation systems provide the repair information corresponding to the various structural components of the aircraft based on the user inputs. The deployment engine fulfills the deployment requirements corresponding to the one or more knowledge interpretation systems.
摘要翻译： 用于支持一个或多个飞机的一个或多个维修过程的框架。 修理过程基于与飞机的一个或多个结构部件的损坏相对应的修理信息或修理解决方案。 框架包括知识引擎和部署引擎。 知识引擎基于用户输入自动生成一个或多个知识解释系统。 知识解释系统基于用户输入提供对应于飞行器的各种结构部件的修复信息。 部署引擎满足与一个或多个知识解释系统相对应的部署要求。
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公开(公告)号：US07234355B2
公开(公告)日：2007-06-26
申请号：US11022726
申请日：2004-12-27
CPC分类号： G01N29/11 , G01N2291/044 , G01N2291/105 , G01N2291/2675
摘要： A method and system for detecting weld signatures from an ultrasound scan data obtained from scanning a pipeline is provided. The method includes a step for mapping multiple amplitude responses from the ultrasound scan data, each amplitude response being representative of a respective sensor signal. Continuous amplitude responses are located from the amplitude responses and corresponding signatures are identified for the continuous amplitude responses. The method also includes a step for tagging the corresponding signatures as weld signatures.
摘要翻译： 提供了一种从扫描管道获得的超声波扫描数据中检测焊接特征的方法和系统。 该方法包括用于映射来自超声扫描数据的多个幅度响应的步骤，每个振幅响应代表相应的传感器信号。 连续振幅响应来自振幅响应，并且针对连续振幅响应识别相应的特征。 该方法还包括将对应的签名标记为焊接签名的步骤。
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