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钝头弹撞击不同材质蜂窝夹芯板的损伤特性研究 被引量:2

Study on Damage Characteristics of Honeycomb Sandwich Plates with Different Material Impacted by Blunt-Nosed Projectiles
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摘要 利用一级气炮系统发射钝头弹进行铝蜂窝夹芯板与纸蜂窝夹芯板的撞击实验,分析靶板材质对弹道极限、夹芯板失效模式和比能量吸收的影响规律及机理。结果表明:钝头弹撞击铝蜂窝夹芯板的弹道极限高于纸蜂窝夹芯板。与纸蜂窝夹芯板相比,铝蜂窝夹芯板受钝头弹撞击前面板产生明显的凹坑变形与纤维分层现象;芯体由撞击撕裂破坏转变为褶皱折叠变形与压溃失效;后面板由纤维拉伸断裂与菱形鼓包变形转变为纤维拉伸失效下大面积的菱形分层破坏,纤维条撕裂的形状由片状转变为带状;前面板与芯体生成的撞击碎屑转变为规则的圆形冲塞。铝蜂窝夹芯板的比能量吸收明显高于纸蜂窝夹芯板。 The aluminum honeycomb sandwich plates and paper honeycomb sandwich plates were impacted by the blunt-nosed projectiles launched by a one-stage gas gun,and the influence of material of targets on the ballistic limits,failure modes and specific energy absorption(SEA)were analyzed.The results show that the ballistic limit of aluminum honeycomb sandwich plates impacted by blunt-nosed projectiles are higher than paper honeycomb sandwich plates.Compared with the paper honeycomb sandwich plates,the aluminum honeycomb sandwich plates generate obvious pit deformation and fiber stratification on the front panel after impact by blunt-nosed projectiles,the failure mode of core changes from impact tear damage to fold collapse deformation and collapse failure,rear panel is transformed by the fiber tensile fracture and rhombic bulge deformation into large area of rhombic delamination under fibers tension failure,the shape of torn fiber strip changes from sheet to strip,the impact debris generated by the front panel and the core transforms into a regular circular plug.The specific energy absorption of aluminum honeycomb sandwich plates is significantly higher than paper honeycomb sandwich plates.
作者 彭捷 路明建 邓云飞 PENG Jie;LU Ming-jian;DENG Yun-fei(College of Aeronautical Engineering,Civil Aviation University of China,Tianjin 300300,China)
出处 《机械设计与制造》 北大核心 2018年第A02期126-129,共4页 Machinery Design & Manufacture
基金 国家自然科学青年基金项目(11702317) 中央高校基本科研业务费项目(3122017035)
关键词 不同材质 蜂窝夹芯板 弹道极限 失效模式 比能量吸收 Different Material Honeycomb Sandwich Plates Ballistic Limit Failure Mode Specific Energy Absorption
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  • 1高玉华.铝合金LC4和LY12CZ在高应交率拉伸和压缩下的本构关系[J].材料科学与工艺,1994,2(2):24-29. 被引量:22
  • 2梁森,陈花玲,陈天宁,梁天锡.蜂窝夹芯结构面内等效弹性参数的分析研究[J].航空材料学报,2004,24(3):26-31. 被引量:38
  • 3陆赵情,张美云,王志杰,吴养育,代攀.芳纶纸基复合材料研究进展及关键技术[J].宇航材料工艺,2006,36(6):5-8. 被引量:13
  • 4劳动部教材办公室.车工工艺学[M].北京:中国劳动出版社.2000.
  • 5Andrews E W, Gioux G, Onck P R, et al. Size effects in ductile cel- lular solids. Part If:experimental results. Int J Mech Sci,2001 ,43: 701-713.
  • 6Bastawros A F, Bart-Smith H, Evans A G. Experimental analysis ofdeformation mechanisms in a closed-cell aluminum alloy foam. J Mech Phys Solids ,2000 ,48:301-322.
  • 7Jeon I, Asahina T. The effect of structural defects on the compressive behavior of closed-cell A1 foam. Acta Mater,2005 ,53:3415-3423.
  • 8Teklu C,Gibson L J,Pardoen T, et al. Size effects in foams: Ex- periments and Modeling Prog Mater Sci,2011 ,56:109-138.
  • 9Chen C, Fleck N A. Size effects in the constrained deformation of metallic foams. J Mech Phys Solids ,2002 ,50:955-977.
  • 10Sun D Q, Zhang W H. Mean in-plane plateau stresses of hexagonal honeycomb cores under impact loadings. Compos Struct, 2009,91: 168-185.

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