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Approach for simultaneous determination of thickness and sound velocity in layered structures based on sound field simulations

机译:基于声场模拟的分层结构厚度和声速的同时确定方法

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摘要

For imaging in NDT or in medical diagnostics, the value of sound velocity is assumed a priori. Interfaces of hidden objects are imaged by the measured time of flight (ToF). The supposed locations and extensions of these objects are incorrect if the actual sound velocity differs from the assumed. For material characterization the thickness of a specimen is determined by mechanical measurements and the sound velocity is determined by ToF-measurements. For multi-layered structures the mechanical determination of the thickness of the different layers is impossible non-destructively. It is necessary to determine both quantities simultaneously to get information about the thickness and the material of the different layers.A variation method is introduced in [1] allowing the simultaneous determination of sound velocity and thickness of up to two layers by focusing with an annular array at a fixed position. It works by varying the focus positions and the assumed sound velocity, which is used to calculate the delay times for each control mode by means of FERMAT’s principle. The amplitude of the echo signals is determined as a function of the control mode. Because the sound field depends on the sound velocity of the medium and the control mode evaluating the amplitude of the echo signals yields additional information besides the time of flight. Alternatively, in [2], a fast and efficient method for a simultaneous determination of sound velocity and thickness of a two- layered structure has been presented. It analyses the different signal parts of an echo reflected from the examined interface. These signal parts correspond to different propagation paths. The difference in time of flight between the signal parts contains the information about thickness and sound velocity of the layer. These time differences are used as an input for an inverse geometric model. Although an accuracy of over 95% had been reached, increasing this accuracy fails, because in both cases the analysis of the signals only uses a geometric model neglecting the wave properties.A half-analytical method based on GREEN’s functions and point sources synthesis is used to calculate the sound field in the multi-layered structures. The echoes of several interfaces are calculated for each element of the used array. Using the same parameter of specimen and the array as in the experiments the evaluation of the simulated signal yields correct time differences based on the wave propagation. They allow assuming effective, corrected source points for the geometric model. With such an optimization of the geometric model an accuracy of 99% can be reached for simulated signals. Measurements are executed on two-layered structures consisting of a first layer of water and a second layer of steel, cupper or aluminum with a thickness of d = 6 mm, 8 mm, 10 mm and 12 mm. For the second layer a deviation for the combined determination of sound velocity and thickness between 3% and 5% is reached with the geometric model for both evaluation methods. With the corrected source point the accuracy can be improved.
机译:对于NDT或医学诊断中的成像,假设声速的值是先验的。隐藏对象的接口由测量的飞行时间(TOF)成像。如果实际声速与假定的实际声速不同,则这些对象的假想的位置和扩展是不正确的。对于材料表征,通过机械测量确定样品的厚度,并且通过TOF测量确定声速。对于多层结构,非损坏的不同层的厚度的机械测定是不可能的。有必要同时确定两个数量以获取有关不同层的厚度和材料的信息。在[1]中引入了变化方法,允许通过聚焦环形来同时确定最多可达两层的声速和厚度。阵列处于固定位置。它通过改变焦点位置和假定的声速来起作用,该声速用于通过Fermat的原理计算每个控制模式的延迟时间。回波信号的幅度被确定为控制模式的函数。因为声场取决于介质的声速和控制模式,评估回波信号的幅度,除了飞行时间之外,还产生附加信息。或者,在[2]中,已经介绍了同时确定两层结构的声速和厚度的快速有效的方法。它分析了从检查界面反射的回声的不同信号部分。这些信号部分对应于不同的传播路径。信号部件之间的飞行时间差包含有关层的厚度和声速的信息。这些时间差异用作逆几何模型的输入。虽然已经达到了超过95%的准确性,但增加了这种精度失败,因为在这两种情况下,信号的分析仅使用忽略波属性的几何模型。基于绿色函数和点源合成的半分析方法计算多层结构中的声场。针对所用阵列的每个元素计算若干接口的回波。使用标本和阵列的相同参数,如在实验中,模拟信号的评估基于波传播产生正确的时间差。它们允许假设几何模型的有效校正的源点。利用这种几何模型的优化,可以达到模拟信号的精度为99%。测量在由第一水层组成的两层结构上执行测量,并且厚度为D = 6mm,8mm,10mm和12mm的厚度的第二层钢,带子或铝。对于第二层,在评估方法的几何模型中达到了用于组合测定声速和厚度的偏差。通过校正的源点,可以提高精度。

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