薄面板复合材料蜂窝夹层结构冲击试验

Test of composite honeycomb sandwich structure with thin facesheets subject to impact load

  • 摘要: 为研究薄面板复合材料蜂窝夹层结构在冲击载荷下的接触力响应和损伤情况,用两种不同质量的冲头对不同面板厚度的复合材料夹层结构进行了多种能量的落锤式冲击试验,并对冲击后的试验件进行了损伤测量。结果表明:冲击能量相对较低时,最大接触力较小,随着冲击能量的增加,最大接触力在增大过程中会出现门槛值,即达到某一值后不再上升。低能量下,冲击损伤表现为面板凹坑和冲击点周围的少量分层,随着冲击能量变大,面板逐渐出现纤维断裂进而被穿透。面板未穿透时,冲头会反弹,接触力-时间曲线的下降段没有台阶,分层区域直径约为冲头直径的1.2倍;面板穿透时,冲头不反弹,接触力-时间曲线下降段出现台阶,分层区域直径约为冲头直径的1.8倍。当最大接触力达到门槛值后,相同冲击能量下,冲头质量越大,冲击持续时间越长,凹坑越深。

     

    Abstract: To study the dynamic response of contact force and damage condition of composite sandwich structures with thin facesheets subject to impact load, specimens of different facesheet thicknesses were tested via dropping weight method at various levels of impact energy using two impactors of different mass. The damage of specimen after impact was measured. The results reveal that when the impact energy is relatively low, the maximum contact force is low and increases with the increase of impact energy, and it will be constant after it reaches the threshold value. The dent in the facesheet and slight delamination around the impact center are the major failure modes at low impact energy, and fiber fracture and penetration will emerge as the impact energy increases. The diameter of delamination area is about 1.2 times of the impactor when the facesheet is un-penetrated with impactor rebound, and in this case there is no plateau on the declining stage of contact force-time curve. While in the penetrated cases, the impactor does not rebound and the diameter of delamination area is about 1.8 times of the impactor, in this case, there is plateau on the declining stage of contact force-time curve. Besides, the bigger mass impactor will lead to longer contact duration and bigger dent depth under the same impact energy after the maximum contact force reaches the threshold value.

     

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