首页|基于电磁加载的冲击测试方法及应用

基于电磁加载的冲击测试方法及应用

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针对国防军工和航空航天对材料、结构或产品进行冲击试验的广泛需求,以及现有冲击测试技术在加载速度、加载力、安全隐患及模式单一等方面存在的问题,提出了基于电磁加载的冲击测试方法,开发了电磁加载的冲击测试系统.电磁力驱动的冲击测试方法可针对不同的试验对象和不同试验要求,通过调整电源控制参数(主要是电容值和充电电压值)实现加载脉宽、载荷幅值及加载速度的精确调整和控制;通过改变电磁加载头方向便可实现拉伸 压缩试验的快速转换.此外,针对结构受复杂冲击加载的动态测试需求,基于电磁驱动的多轴多向加载可通过控制程序精准控制多驱动头同时放电,从而实现多轴多向同步加载,保证了作用于试件材料上的各向冲击载荷的同步性.因此,基于电磁加载的测试技术具有可控性好、重复性高、测试精度和试验效率高等优势,基于电磁加载的冲击测试解决了传统测试方法加载速度范围小、测试应变率范围有限、大加载力冲击测试难等难题,实现了冲击测试试验安全、稳定、可靠及更加精确的控制和测量.
Investigation and Application of Impact Testing Technologies Based on Electromagnetic Loading
Impact testing techniques based on electromagnetic loading were proposed to solve the problems of loading speed,loading force,safety problems and single mode of the existing impact testing technology.The accurate control of pulse width,amplitude and loading speed of pulse electromagnetic force can be realized by adjusting the power control parameters(mainly is capacitance and charging voltage)of electromagnetic driving impulse testing technology.The fast conversion of tension-compression test can be realized by changing the direction of electromagnetic loading head.In addition,as more and more attention has been paid to the testing of dynamic mechanical properties of materials under compound impact loads,multi-axis testing based on electromagnetic drive can accurately control the simultaneous discharge of multiple groups of capacitors through the control program,so as to ensure the synchronization of the isotropic impact load acting on the specimen material.Therefore,the testing technology based on electromagnetic loading has the advantages of good controllability,high repeatability,high synchronization of compound loading,high testing accuracy and experimental efficiency.The problems of traditional testing methods,such as small loading speed range,limited strain rate range and difficult impact testing with large loading force,are solved,and the safe,stable,reliable and more accurate control and measurement of impact testing experiment are realized.

Electromagnetic loadingDynamic impactElectromagnetic-Hopkinson barLow-velocity impactStrain rate

王晓荷、曹增强、郭映江、郭程翔、王玥浩轩

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西北工业大学,西安 710072

陕西大工旭航有限公司,西安 710072

电磁加载 动态冲击 电磁霍普金森杆 低速冲击 应变率

陕西省重点研发计划

S2022-YG-GXZD-0020

2024

航空制造技术
北京航空制造工程研究所

航空制造技术

CSTPCD北大核心
影响因子:0.403
ISSN:1671-833X
年,卷(期):2024.67(7)
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