气动活塞式冲击加速度校准装置研制

doi:10.12060/j.issn.1000-7202.2019.04.07

宇航计测技术

气动活塞式冲击加速度校准装置研制

倪博¹；田芳怡¹；沙江¹；毛志勇¹；翁俊¹；罗晓平¹

1、上海精密计量测试研究所, 上海 201109

出版日期:2019-08-25 发布日期:2019-08-25
作者简介:倪博（1986-），男，博士，工程师，主要研究方向：力学计量与动态测试。

Establishment of Impact Acceleration Calibration Device by Pneumatic Piston

NI Bo¹；TIAN Fang-yi¹；SHA Jiang¹；MAO Zhi-yong¹；WENG Jun¹；LUO Xiao-ping¹

1、Shanghai Precision Metrology &Test Research Institute, Shanghai 201109，China

Online:2019-08-25 Published:2019-08-25

摘要/Abstract

摘要： 基于传感器比较法，开展冲击加速度校准方法研究。采用气动活塞式冲击激励发生技术和PXI总线数据采集分析技术，研制冲击加速度校准装置，运用LabVIEW软件编写了校准软件，并对装置进行测量不确定度评估，该装置可为国防军工产品冲击试验提供冲击加速度参数的量值溯源。

关键词: 冲击加速度传感器, 冲击激励发生装置, PXI总线

Abstract: According to the method of comparison to a reference transducer, the approach for the calibration of impact acceleration is studied. Based on technology of impact excitation by pneumatic piston and technology of data acquisition by PXI bus, impact acceleration calibration device is established. The calibration software is programmed on LabVIEW, and the measurement uncertainty of device is evaluated. The calibration device can be used for national defense products shock test traceability of impact acceleration.

Key words: Impact acceleration transducer, Impact excitation device, PXI bus

倪博；田芳怡；沙江；毛志勇；翁俊；罗晓平. 气动活塞式冲击加速度校准装置研制[J]. 宇航计测技术, doi: 10.12060/j.issn.1000-7202.2019.04.07.

NI Bo；TIAN Fang-yi；SHA Jiang；MAO Zhi-yong；WENG Jun；LUO Xiao-ping. Establishment of Impact Acceleration Calibration Device by Pneumatic Piston[J]. JOURNAL OF ASTRONAUTIC METROLOGY AND MEASUREMENT, doi: 10.12060/j.issn.1000-7202.2019.04.07.

气动活塞式冲击加速度校准装置研制

Establishment of Impact Acceleration Calibration Device by Pneumatic Piston

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