欢迎登录材料期刊网

材料期刊网

高级检索

采用落锤法对复合材料加筋板进行了低速冲击损伤(LVI)试验,根据复合材料加筋板构型,设计了冲击支持支架,研究了支持支架的间距对冲击结果的影响;用相同的冲击能量对复合材料加筋板结构中3处典型位置进行冲击,得到不同位置的损伤形貌;分别对完好件和损伤试验件进行压缩试验,将试验结果进行对比,分析不同位置的冲击损伤对结构压缩性能的影响.试验结果表明:在相同的冲击能量下,支持支架间距越小,所造成的冲击损伤越严重;在50J冲击能量下,筋条区蒙皮处的冲击所造成的损伤不易观察,筋条间蒙皮处的冲击所造成的损伤最为明显,而筋条边缘蒙皮处的冲击可以导致筋条边缘的脱粘;冲击损伤会使加筋板屈曲载荷轻微下降,筋条间蒙皮和筋条区蒙皮冲击损伤对压缩结果影响相对较小,筋条边缘处的冲击会引起损伤处蒙皮的子层屈曲,并影响结构破坏形式,使结构压缩承载能力有较为明显的下降.

参考文献

[1] 陈祥宝.先进树脂基复合材料的发展和应用[J].航空材料学报,2003,23(增刊):198-204.Chen Xiangbao.The development and applications of advanced polymer matrix composites[J].Journal of Aeronautical Materials,2003,23(S1):198-204.
[2] 崔海坡,温卫东,崔海涛.复合材料层合板冲击损伤及剩余强度研究进展[J].材料科学与工程学报,2005,23(3):466-472.Cui Haipo,Wen Weidong,Cui Haitao.Advances of study on low velocity impact damaged and residual strength of composite laminates[J].Journal of Materials Science & Engineering,2005,23(3):466-472.
[3] Choi H Y,Wu H Y,Chang F K.A new approach toward understanding damage mechanisms and mechanics of laminated composites due to low-velocity impact:Part Ⅱ-analysis[J].Journal of Composite Materials,1991,25(8):1012-1038.
[4] Zhou G.The use of experimentally-determined impact force as a damage measure in impact damage resistance and tolerance of composite structures[J].Composite Structures,1998,42(4):375-382.
[5] Tiberkak R,Bachene M,Rechak S,et al.Damage prediction in composite plates subjected to low velocity impact[J].Composite Structures,2008,83(1):73-82.
[6] Gadke M,Geier B,Goetting H C,et al.Damage influence on the buckling load of CFRP stringer-stiffened panels[J].Composite Structures,1996,36(3):249-275.
[7] Kong C,Hong C,Kim C.Postbuckling strength of stiffened composite plates with impact damage[J].AIAA Journal,2000,38(10):1956-1964.
[8] 王 俭,沈 真.复合材料冲击损伤阻抗性能的试验研究[J].航空制造技术,2009(S1):161-164.Wang Jian,Shen Zhen.Experimental study on impact damage resistance property of composites[J].Aeronautical Manufacturing Technology,2009(S1):161-164.
[9] 朱炜垚,许希武.复合材料层合板低速冲击损伤的有限元模拟[J].复合材料学报,2010,27(6):200-206.Zhu Weiyao,Xu Xiwu.Finite element simulation of low velocity impact damage on composite laminates[J].Acta Materiae Compositae Sinica,2010,27(6):200-206.
[10] 古兴瑾,许希武.复合材料整体化加筋壁板高速冲击损伤数值模拟[J].航空学报,2012,33(2):258-272.Gu Xingjin,Xu Xiwu.Numerical simulation of damage in stffened integral composite panels under high velocity impact[J].Acta Aeronautica et Astronautica Sinica,2012,33(2):258-272.
[11] 郑翔,童小燕,程起有,等.复合材料低速冲击及剩余压缩强度实验研究[J].机械科学与技术,2010,29(11):1574-1577.Zheng Xiang,Tong Xiaoyan,Cheng Qiyou,et al.Experimental investigation of low-velocity impact and residual compressive strength of composites[J].Mechanical Science and Technology for Aerospace Engineering,2010,29(11):1574-1577.
[12] 屈天骄,郑锡涛,范献银,等.复合材料层合板低速冲击损伤影响因素分析[J].航空材料学报,2011,31(12):81-86.Qu Tianjiao,Zheng Xitao,Fan Xianyin,et al.Exploration of several influence factors of low-velocity impact damage on composite laminates[J].Journal of Aeronautical Materials,2011,31(12):81-86.
[13] American Society for Testing and Materials.ASTM D7136/D 7136M-12 standard test method for measuring the damage resistance of a fiber-reinforced polymer matrix composite to a drop-weight impact event[S].West Conshohocken,PA:ASTM,2012.
[14] American Society for Testing and Materials.ASTM D7137/D 7137M-12 standard test method for compressive residual strength properties of damaged polymer matrix composite plates[S].West Conshohocken,PA:ASTM,2012.
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%