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DEVELOPMENT OF A LINEAR SWEEPING FREQUENCY PRESSURE GENERATOR FOR DYNAMIC PRESSURE CALIBRATION

机译:用于动态压力校准的线性扫描频率发生器的开发

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With the development of aerospace technology, more and more accuracy experiment results are expected to improve the performance of rocket and aerospace crafts. Pressure transducers are widely used in experiments of aerospace technique. Knowing well the characteristics of pressure transducers before used is very important to improve the experiment results of rocket and aerospace crafts. So the need for dynamic pressure calibration has been increasing. Many solutions have been developed to satisfy this demand. Some of them are periodic, and the others are aperiodic. Usually, sinusoidal pressure generator is used to calibrating the amplitude response and phase shift as a function of frequency for transducers. But there are two problems for this generator: one is that the calibrating data are dispersed, it is difficult to get a continuous curve of amplitude response and phase shift as a flinction of frequency for transducers; the other is that the amplitude response and phase shift cannot be obtained near and at the resonant frequency of tested transducer. In order to overcome these disadvantages of sinusoidal pressure generator, we developed a linear sweeping frequency pressure generator. The generator outputs a linear sweeping frequency pressure signal to both of the standard and tested pressure transducers at same time. After processing the outputs of the transducers, the continuous frequency-amplitude and frequency-phase curves of the tested pressure transducer can be obtained directly. The whole performance of the tested transducer in the sweeping frequency range is clear. If the resonant frequency of tested transducer is in the sweeping frequency range, the resonant frequency of tested transducer can be obtained from the frequency-amplitude curve. The sweeping frequency range and working pressure of the generator can be set up before test. In this report, the composition of the generator and the calibration method for tested pressure transducer with it are introduced. The sweeping frequency range of the generator is (0.1~10000)Hz, and the working pressure range is (0.25〜10)MPa.
机译:随着航空航天技术的发展,越来越多的准确性实验结果有望改善火箭和航空航天飞机的性能。压力传感器广泛用于航空航天技术的实验中。熟悉压力传感器在使用前的特性对于改善火箭和航空航天器的实验结果非常重要。因此,对动态压力校准的需求一直在增加。已经开发了许多解决方案来满足该需求。其中一些是周期性的,而其他则是非周期性的。通常,正弦压力发生器用于校准振幅响应和相移,作为传感器频率的函数。但是这种发生器存在两个问题:一个是校准数据分散,很难获得连续的幅度响应和相移曲线,作为换能器的频率波动。另一个是在被测换能器附近和共振频率处不能获得幅度响应和相移。为了克服正弦压力发生器的这些缺点,我们开发了一种线性扫频压力发生器。发生器同时向标准压力传感器和经过测试的压力传感器输出线性扫频压力信号。在处理了传感器的输出之后,可以直接获得被测压力传感器的连续频率振幅和频率相位曲线。在扫频范围内,被测换能器的整体性能是显而易见的。如果被测换能器的谐振频率在扫频范围内,则可以从频率-振幅曲线得到被测换能器的谐振频率。测试前可以设置发生器的扫频范围和工作压力。在此报告中,介绍了发生器的组成以及用于测试压力传感器的校准方法。发电机的扫频范围为(0.1〜10000)Hz,工作压力范围为(0.25〜10)MPa。

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