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Credibility of Piping Pressure Transient Measurements Using Strain Gauges

机译:使用应变片测量管道压力瞬态的可靠性

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The use of strain gauge measurements to determine the pressure transient history signature inside the pipe, Szasz [1], needs to be reexamined. Computation of the natural frequencies of the pipe shell vibrations, Leissa [2], including FSI, Ibrahim [3], should precede these measurements. The pressure disturbance signature and its traveling velocity interact dynamically with the pipe shell natural vibration mode shapes and frequencies. The latter have detrimental effects on the measured response magnitude as well as the response signature configuration, Meirovitch [4]. In addition, traveling pressure propagating velocity near or at resonance with the cylindrical shell mode shape distorts and over amplifies the strain gauge transient response. There is no direct technique to back transform the strain response history signature into its original driving pressure history, Leishear [5].In this paper the dynamic response for a simply supported circular cylindrical shell pipe model is formulated. The pressure transient history signatures are simulated as mobile concentrated radial ring force, traveling step pressure shock front, and propagating acoustic harmonic pressure wave. Comparisons between the projected hoop strains obtained based on the equilibrium of the pressure forces [1], and the hoop strains determined from the shell dynamic response are examined.At least two sets of strain gauge bands are needed to confirm the validity of the measured strain data. Limitations on the appropriateness of deploying strain gauge bands as a mean to measure the traveling pressure history inside the pipe are delineated in this paper. Generally, steam transporting pipes are less influenced by these limitations than liquid transporting pipes.
机译:需要重新检查使用应变仪测量来确定管道内部的压力瞬态历史特征(Szasz [1])。在进行这些测量之前,应先计算管壳振动的固有频率Leissa [2],包括FSI,Ibrahim [3]。压力扰动特征及其传播速度与管壳固有振动模式的形状和频率动态相互作用。后者对测得的响应幅度以及响应特征配置Meirovitch有不利影响[4]。另外,接近或共振于圆柱壳模式形状的行进压力传播速度会扭曲并过度放大应变仪的瞬态响应。没有直接的技术可以将应变响应历史签名反变换为原始的驱动压力历史Leishear [5]。 本文提出了一种简单支撑的圆柱壳管模型的动力响应。压力瞬态历史特征被模拟为移动集中径向环力,行进阶跃压力冲击波前和传播的声谐波压力波。检验了基于压力[1]的平衡获得的预计环向应变与根据壳动力响应确定的环向应变之间的比较。 需要至少两组应变仪带来确认测得的应变数据的有效性。本文描述了在部署应变仪带作为测量管道内部行进压力历史记录的方法方面的局限性。通常,与液体输送管相比,蒸汽输送管受这些限制的影响较小。

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