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Determination of calibration function for fatigue crack propagation by measurment surface deformation

机译:通过测量表面变形确定疲劳裂纹扩展的校准函数

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Components and structures exposed to elastic dynamic loading respond with elastic strains on the surface of the material. Mechanical response could be monitored by deformations on the surface. The measurements and monitoring of these parameters could be performed with electronic devices for on-line measurements, controlled by computerized systems. In the case of fatigue crack initiation and propagation the cyclic strain amplitude deviated from initial strain response (mean value and amplitude). Implementation of appropriate monitoring system supported by computerized programs for evaluation, analyses and activation represent important means to safe service component or construction. To evaluate flaw depth growth, the strain gauge measuring sensors could be used. These sensors measure surface deformation relaxation due to flaw depth growth. The monitoring of the material under cyclic loading could be performed with experimentally determined calibration curve, representing deformation on the surface and depth of the semi-elliptical crack growth on the surface or cross section of the material. The goal of this paper is describe electronic device and experimental procedure in order to determine calibration function.
机译:承受弹性动态载荷的组件和结构通过材料表面的弹性应变来响应。机械响应可以通过表面变形来监测。这些参数的测量和监视可以通过计算机系统控制的电子设备进行在线测量。在疲劳裂纹萌生和扩展的情况下,循环应变振幅会偏离初始应变响应(均值和振幅)。实施适当的监测系统,在计算机化程序的支持下进行评估,分析和激活,是确保服务组件或建设安全的重要手段。为了评估缺陷深度的增长,可以使用应变仪测量传感器。这些传感器测量由于缺陷深度增加而引起的表面变形松弛。可以通过实验确定的校准曲线对材料进行循环载荷监测,该校准曲线表示材料表面或截面上半椭圆形裂纹扩展的深度和深度。本文的目的是描述电子设备和实验程序,以确定校准功能。

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