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Identifying the high-frequency response of a piezoelectric pressure measurement system using a shock tube primary method

机译:使用冲击管初级方法识别压电压力测量系统的高频响应

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The pressure transducers employed in dynamic pressure applications are calibrated using static pressure standards due to the lack of metrological traceability for time-varying pressure measurements, which limits the achievable accuracy of time-varying pressure measurements. This paper proposes and evaluates a method for identifying the frequency response function of a pressure measurement system in the high-frequency range using an independent, traceable pressure step signal generated in a shock tube as the reference input signal. The identification of the frequency response function for a piezoelectric pressure measurement system with a developed diaphragmless shock tube was performed using nitrogen at the atmospheric initial driven pressure and at the initial driver gauge pressures from 4 MPa to 10 MPa. The uncertainties of the amplitude and phase frequency characteristics of the piezoelectric pressure measurement system under calibration were determined by considering the uncertainty contributions of the pressure step amplitude generated within the shock tube and the arrival time of the initial shock front at the end-wall of the driven section, respectively, the repeatability and the systematic errors. The uncertainty analysis shows that the proposed method used with the developed diaphragmless shock tube determines the amplitude ratio of the piezoelectric pressure measurement system with a relative expanded uncertainty of less than 5% and a phase lag with an expanded uncertainty of less than 9° in the 10 kHz range for all the observed initial driver pressures.
机译:由于缺乏用于时变压测量的计量性可追溯性,使用静压标准校准动态压力应用中的压力传感器,这限制了时变压测量的可实现的准确度。本文提出了一种使用在冲击管中产生的独立,可追踪的压力步骤信号来评估用于识别高频范围中的压力测量系统的频率响应功能的方法作为参考输入信号。使用氮气在大气初始驱动的压力下和从4MPa至10MPa的初始驱动器规格压力下进行带式膜片减震管的压电压力测量系统的频率响应函数的识别。通过考虑在冲击管内产生的压力步骤幅度的不确定性以及初始震动前沿的末端壁的到达时间来确定压电压力测量系统的幅度和相位频率特性的不确定性。驱动部分分别是重复性和系统错误。不确定性分析表明,所提出的方法与发达的膜片冲击管一起使用的压电压力测量系统的幅度比具有小于5%的相对膨胀不确定度,并且相位滞后的相位滞后具有小于9°的膨胀不确定度所有观察到的初始驱动压力的10 kHz系列。

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