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针对航天器空间碎片防护材料需求,采用二维编织的TC4纤维作为增强体制备了(2D-Tif)/Al复合材料,并采用二级轻气炮研究了复合材料在高速粒子撞击下的损伤行为及其组织演变规律.结果表明,(2D-Tif)/Al复合材料靶板的破坏以侵彻穿深为主,背面产生了带裂纹的鼓包或发生略微崩落;其抗高速撞击能力优于等厚的LF6基体合金,平均吸能能力比基体合金提高了8.4 J.复合材料内部的基体合金在高速粒子撞击下被严重挤压变形,在远离弹坑部位,基体合金变形减轻,缺陷以微裂纹和微孔洞为主.高强韧Ti纤维的加入起到了承载和吸能作用,有效减缓了基体合金的变形,并抑制了基体合金中绝热剪切带的形成.

参考文献

[1] Donald R L .[J].International Journal of Impact Engineering,2000,24(10):521.
[2] Robinson J H;Nolen A M .[J].International Journal of Impact Engineering,1995,17:685.
[3] Zhou J S et al.[J].Materials Science and Engineering A:Structural Materials Properties Microstructure and Processing,2000,282:177.
[4] Zhu D Z et al.[J].Materials Science and Engineering A:Structural Materials Properties Microstructure and Processing,2008,487:536.
[5] Higashide M et al.[J].International Journal of Impact Engineering,2006,33:335.
[6] Tennyson R.C.;Lamontagne C .Hypervelocity impact damage to composites[J].Composites, Part A. Applied science and manufacturing,2000(8):785-794.
[7] Oka Y I;Nagahashi K;Ishii Y et al.[J].WEAR,2005,258:100.
[8] Piekutowski A J .[J].International Journal of Impact Engineering,1999,23:711.
[9] Tanaka M;Moritaka Y .[J].Advances in Space Research,2004,34:1076.
[10] Murr LE.;Ferreyra E.;Ayala A.;Valerio OL.;Horz F. Bernhard RP.;Quinones SA. .The low-velocity-to-hypervelocity penetration transition for impact craters in metal targets[J].Materials Science & Engineering, A. Structural Materials: Properties, Misrostructure and Processing,1998(1/2):166-182.
[11] Zhen L;Li GA;Zhou JS;Yang DZ .Micro-damage behaviors of Al-6Mg alloy impacted by projectiles with velocities of 1-3.2 km/s[J].Materials Science & Engineering, A. Structural Materials: Properties, Misrostructure and Processing,2005(1/2):354-366.
[12] 谭成文,刘新芹,陈志永,马红磊,王富耻,才鸿年.Ti-6Al-4V合金绝热剪切敏感性与临界破碎速度关系研究[J].稀有金属材料与工程,2008(08):1400-1402.
[13] Meyers M A.Dynamic Behavior of Materials[M].New York:John Wiley and Sons,Inc,1994:228.
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