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    • 1. 发明申请
    • Fastener and fitting based sensing methods
    • 基于紧固件和拟合的感应方法
    • US20070007955A1
    • 2007-01-11
    • US11473297
    • 2006-06-22
    • Neil GoldfineDavid GrundyAndrew WashabaughYanko SheiretovDarrell Schlicker
    • Neil GoldfineDavid GrundyAndrew WashabaughYanko SheiretovDarrell Schlicker
    • G01N27/82
    • G01N27/82
    • Damage and usage conditions in the vicinity of fasteners in joined structures are nondestructively evaluated using the fasteners themselves. Sensors or sensor conductors are embedded in the fasteners or integrated within the fastener construct, either in the clearance gap between the fastener and the structure material or as an insert inside the shaft or pin of the fastener. The response of the material to an interrogating magnetic or electric field is then measured with drive and sense electrodes both incorporated into the fastener or with either drive or sense electrodes external to the fastener on the material surface. In another configuration, an electric current is applied to one or more fasteners and the electric potential is measured at locations typically between the driven electrodes applying the current. The potential is measured circumferentially around the fastener at locations on the material surface or across pairs of fasteners throughout or along the joint. The voltage or potential measurement electrodes may be collinear with the drive electrodes. State sensitive material layers can be added either to the fastener or the test material layers in order to enhance observability of the test material condition, such as the presence of a crack, mechanical stress, delamination, or disbond.
    • 使用紧固件本身对接合结构中紧固件附近的损坏和使用条件进行非破坏性评估。 传感器或传感器导体嵌入到紧固件中或整合在紧固件结构内,无论是在紧固件和结构材料之间的间隙中,或者作为紧固件的轴或销内的插入件。 然后测量材料对询问磁场或电场的响应,其中驱动和感测电极两者并入到紧固件中,或者与材料表面上的紧固件外部的驱动或感测电极结合。 在另一种配置中,电流被施加到一个或多个紧固件,并且在通常在施加电流的驱动电极之间的位置处测量电位。 在整个或沿着接头的材料表面上或穿过成对的紧固件的位置周围围绕紧固件测量电位。 电压或电位测量电极可与驱动电极共线。 可以将状态敏感材料层添加到紧固件或测试材料层中,以便增强测试材料状况的可观察性,例如存在裂纹,机械应力,分层或脱粘。
    • 4. 发明申请
    • Material characterization with model based sensors
    • US20070069720A1
    • 2007-03-29
    • US11229844
    • 2005-09-19
    • Neil GoldfineMark WindoloskiDavid GrundyYanko SheiretovDarrell SchlickerAndrew Washabaugh
    • Neil GoldfineMark WindoloskiDavid GrundyYanko SheiretovDarrell SchlickerAndrew Washabaugh
    • G01N27/82
    • G01N27/72
    • Nondestructive material condition monitoring and assessment is accomplished by placing, mounting, or scanning magnetic and electric field sensors and sensor arrays over material surfaces. The material condition can be inferred directly from material property estimates, such as the magnetic permeability, dielectric permittivity, electrical property, or thickness, or from a correlation with these properties. Hidden cracks in multiple layer structures in the presence of fasteners are detected by combining multiple frequency magnetic field measurements and comparing the result to characteristic signature responses. The threshold value for indicating a crack is adjusted based on a high frequency measurement that accounts for fastener type. The condition of engine disk slot is determined without removal of the disk from the engine by placing near the disk a fixture that contains a sensor for scanning through the slot and means for recording position within the slot. Inflatable support structures can be placed behind the sensor to improve and a guide can be used to align sensor with the slot and for rotating the disk. The condition of an interface between a conducting substrate and a coating is assessed by placing a magnetic field sensor on the opposite side of the substrate from the coating and monitoring at least one model parameter for the material system, with the model parameter correlated to the interfacial condition. The model parameter is typically a magnetic permeability that reflects the residual stress at the interface. Sensors embedded between material layers are protected from damage by placing shims on the faying surface. After determining the areas to be monitored and the areas likely to cause sensor damage, a shim thickness is determined and is then placed in at least one area not being monitored by a sensor. The condition of a test fluid is assessed through a dielectric sensor containing a contaminant-sensitive material layer. The properties of the layer are monitored with the dielectric sensor and correlated to contaminant level.
    • 5. 发明申请
    • Local feature characterization using quasistatic electromagnetic sensors
    • 使用准静态电磁传感器的局部特征表征
    • US20060097718A1
    • 2006-05-11
    • US11249047
    • 2005-10-11
    • Darrell SchlickerNeil GoldfineAndrew WashabaughYanko SheiretovMark Windoloski
    • Darrell SchlickerNeil GoldfineAndrew WashabaughYanko SheiretovMark Windoloski
    • G01R33/12
    • G01N27/023
    • Local features such as cracks in materials are nondestructively characterized by measuring a response with an electromagnetic sensor and converting this response into a selected property using a database. The database is generated prior to data acquisition by using a model to generate a baseline response or field distribution for the sensor and combining these results with another model, which may be simpler than the first model or provide a local representation of the field perturbations around a feature, which is evaluated multiple times over a range of values of the selected property. In addition, the presence of a feature may be detected by converting the sensor response into a reference parameter, such as a lift-off factor that reflects the sensor position relative to a material edge, and using this parameter to determine a reference response that can be compared to the measured response.
    • 局部特征如材料中的裂纹是非破坏性的,其特征在于通过用电磁传感器测量响应并使用数据库将该响应转换成选定的属性。 在数据采集之前通过使用模型生成数据库以生成传感器的基线响应或场分布,并将这些结果与另一模型相结合,该模型可以比第一模型更简单,或者提供周围的场扰动的局部表示 功能,在所选属性的值范围内多次评估。 此外,可以通过将传感器响应转换为参考参数来检测特征的存在,所述参考参数例如反映相对于材料边缘的传感器位置的剥离因子,并且使用该参数来确定可以 与测量响应进行比较。
    • 6. 发明申请
    • Remaining life prediction for individual components from sparse data
    • 从稀疏数据中对各个组件进行剩余寿命预测
    • US20070239407A1
    • 2007-10-11
    • US11653067
    • 2007-01-12
    • Neil GoldfineVladimir ZilbersteinVolker WeissYanko Sheiretov
    • Neil GoldfineVladimir ZilbersteinVolker WeissYanko Sheiretov
    • G06F17/10
    • G01N27/82F05B2270/109F05B2270/404G01B7/34G06N7/005
    • Predicting the remaining life of individual aircraft, fleets of aircraft, aircraft components and subpopulations of these components. This is accomplished through the use of precomputed databases of response that are generated from a model for the nonlinear system behavior prior to the time that decisions need to be made concerning the disposition of the system. The database is calibrated with a few data points, to account for unmodeled system variables, and then used with an input variable to predict future system behavior. These methods also permit identification of the root causes for observed system behavior. The use of the response databases also permits rapid estimations of uncertainty estimates for the system behavior, such as remaining life estimates, particularly, when subsets of an input variable distribution are passed through the database and scaled appropriately to construct the output distribution. A specific example is the prediction of remaining life for an aircraft component where the model calculates damage evolution, input variables are a crack size and the number of cycles, and the predicted parameters are the actual stress on the component and the remaining life.
    • 预测个别飞机,飞机机队,飞机部件和这些部件的子群体的剩余寿命。 这是通过使用预先计算的响应数据库来实现的,该数据库是在关于系统的配置的决定之前从非线性系统行为的模型生成的。 数据库使用几个数据点进行校准,以解释未建模的系统变量,然后与输入变量一起使用以预测未来的系统行为。 这些方法还允许识别观察到的系统行为的根本原因。 响应数据库的使用还允许对系统行为的不确定性估计的快速估计,例如剩余寿命估计,特别是当输入变量分布的子集通过数据库并适当地缩放以构建输出分布时。 一个具体的例子是对模型计算损伤演化的飞机部件的剩余寿命的预测,输入变量是裂纹尺寸和循环次数,预测参数是组件上的实际应力和剩余寿命。