欢迎登录材料期刊网

材料期刊网

高级检索

Z-pin增强泡沫夹层结构作为一种新兴的复合材料夹层结构形式,能够克服传统蜂窝夹层结构的诸多缺陷.采用预浸碳纤维增强Rohacell夹芯,进行Z-pin角度为15°和25°,夹芯厚度分别为12.7mm和8mm两种Z-pin增强泡沫夹层结构的面内压缩性能试验,并与相同批次和尺寸的未增强件进行对比,考察其对传统泡沫夹层结构的增强作用.试验发现X状Z-pin增强能够大幅度提高夹层结构的压缩强度与刚度.同时,增强材料表现出与传统泡沫夹层结构不同的压缩变形与破坏模式.证实Z-pin的弹性屈曲控制着结构的压缩强度,夹芯厚度和Z-pin角度影响Z-pin屈曲的计算长度,从而成为材料压缩强度的控制因数.在此基础上,考虑面板对Z-pin的有限转动约束,通过引进约束修正系数改进现有的压缩强度预测模型,预测值与试验结果更加接近.

参考文献

[1] KAY B F.RWSTD airframe technology foundation for the 21st centry[A].Washington,2001:911-918.
[2] CARSTENSEN T C;KUNKEL E;MAGEE C.X cor advanced sandwich core material[A].Seattle,2001:452-466.
[3] O′BRIEN K T;PARIS I L.Exploratory investigation of failure mechanisms in transition regions between solid laminates and X cor truss sandwich[J].Computers & Structures,2002(57):189-204.
[4] Denis D. Cartie;Norman A. Fleck .The effect of pin reinforcement upon the through-thickness compressive strength of foam-cored sandwich panels[J].Composites science and technology,2003(16):2401-2409.
[5] VAIDYA U K;NELSON S.Processing and high strain rate impact response of multi functional sandwich composites[J].Computers & Structures,2001(52):429-440.
[6] Rice MC;Fleischer CA;Zupan M .Study on the collapse of pin-reinforced foam sandwich panel cores[J].Experimental Mechanics,2006(2):197-204.
[7] 田旭,肖军,李勇.X-cor夹层结构试制与性能研究[J].飞机设计,2004(01):22-25.
[8] 黄涛,矫桂琼,徐婷婷.Z向增强泡沫夹层结构复合材料[J].纤维复合材料,2005(03):19-23.
[9] TIMOSHENKO S P;GERE J M.Theory of elastic stability[M].New York:McGraw-Hill,1961
上一张 下一张
上一张 下一张
计量
  • 下载量()
  • 访问量()
文章评分
  • 您的评分:
  • 1
    0%
  • 2
    0%
  • 3
    0%
  • 4
    0%
  • 5
    0%