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气动式冲击响应谱试验台仿真研究与试验验证

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基于设计-测试-优化的气动式冲击响应谱试验台研制方式存在试验周期长和可靠性不足时改进成本高的问题,有限元分析可以在设计阶段模拟系统撞击过程从而缩短研发周期.为了满足上升斜率 9 dB/Oct、拐点频率 1 000 Hz和试验量级 4 000 g的冲击响应谱试验规范,文章设计了一种气动式冲击响应谱试验系统.本文首先建立气动式冲击响应谱试验台有限元模型,然后对比仿真与实测加速度曲线的时域特征和频域特征,最终表明:仿真与实测加速度曲线均呈现复杂的衰减振荡型;仿真与实测上升斜率均接近 9 dB/Oct;仿真拐点频率 1 080 Hz左右,实测拐点频率1 130 Hz左右,该冲击响应谱试验台可以满足上述冲击响应谱试验规范,并且验证了仿真结果的准确性.
Simulation Study and Experimental Verification of Pneumatic Impact Response Spectrum Test Bench
The development method of pneumatic impact response spectrum test bench based on design test optimization has the problems of long test cycle and high improvement cost due to insufficient reliability.Finite element analysis can simulate the system impact process in the design stage to shorten the development cycle.In order to meet the shock response spectrum test specifications of a rising slope of 9 dB/Oct,a turning point frequency of 1 000 Hz,and a test magnitude of 4 000 g,a pneumatic shock response spectrum test system was designed in this article.This article first establishes a finite element model of the pneumatic impact response spectrum test bench,and then compares the time-domain and frequency-domain characteristics of the simulated and measured acceleration curves.Finally,it shows that both the simulated and measured acceleration curves exhibit complex attenuation oscillations;The simulated and measured rising slopes are both close to 9 dB/Oct;The simulated inflection point frequency is around 1 080 Hz,and the measured inflection point frequency is around 1 130 Hz.This shock response spectrum test bench can meet the above shock response spectrum test specifications and verify the accuracy of the simulation results.

shock response spectrumrising slopeinflection point frequencyfinite element method

杨鹏、朱江峰、李二攀、马爱军

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苏州苏试试验集团股份有限公司,苏州 215019

冲击响应谱 上升斜率 拐点频率 有限元法

2024

环境技术
广州电器科学研究院有限公司

环境技术

CSTPCD
影响因子:0.995
ISSN:1004-7204
年,卷(期):2024.42(12)