欢迎登录材料期刊网

材料期刊网

高级检索

针对制作工艺为连接处预先制孔,粘结和螺栓安装一并完成的复合材料胶-螺混合连接接头,利用其传力机制和胶-螺之间的变形协调条件推导了承载力计算方法。计算了接头中胶连接的破坏荷载,分析了胶连接承受其破坏荷载时胶层剪应变沿搭接长度的分布规律,利用胶-螺之间的变形协调条件计算了此时螺栓连接所承担荷载;胶连接的破坏荷载和此时螺栓连接所承担荷载之和即为接头承载力。利用该公式对一组采用上述工艺制作的试件进行了承载力计算和试验验证,理论值与试验值吻合较好,验证了理论推导的正确性。

The carrying capacity was calculated using the load transfer mechanism and the bonded-bolted deformation harmony condition for the bonded-bolted hybrid composite joints,which make holes,adhere coat and install bolts.The failure load of the bonded connection portion was calculated,and the shearing strain of the adhesive layer along the bonded length was analyzed when the bonded connection portion endured its failure load,and the load of the bolted connection portion was calculated using the bonded-bolted deformation harmony condition.The carrying capacity is the sum of the two loads.The carrying capacity calculated by the method was in good agreement with the experimental data,which validate the method.

参考文献

[1] 沃丁柱.复合材料大全[M].北京:化学工业出版社,2000:660-684.
[2] 中国航空研究院.复合材料连接手册[M].北京:航空工业出版社,1994:11-134.
[3] Hart-Smith L J. Adhesive-bonded double-lap joints, NASA/ CR- 112235 [R]. Virginia: National Aeronautics and Space Administration, 1973: 3-56.
[4] 薛克兴,周瑾.复合材料结构连接件设计与强度[M].北京:航空工业出版社,1988:7-350.
[5] Gomez S, Onoro J, Pecharroman J. A simple mechanical model of a structural hybrid adhesive/riveted single lap joint [J]. International Journal of Adhesion & Adhesives, 2007, 27 (4) : 263-267.
[6] 白瑞祥,郭兆璞,陈浩然,等.复合材料层合板、壳胶-铆混合连接件有限元分析[J].大连理工大学学报,2000,40(3):280-284.
[7] Hart-Smith L J. Bonded - bolted composite joints [ J ]. Journal Aircraft, 1985, 22(11): 993-1000.
[8] 于德昌,陈绍杰,姜从典,等.碳纤维复合材料的连接试验[J].材料工程,1979(3):38-41.
[9] 李煊,党嘉立,郭秉仪.复合材料混合连接接头强度影响因素初探[C]//第十一届全国复合材料学术会议论文集.合肥:中国科学技术大学出版社,2000:475-478.
[10] Kelly G, Load transfer in hybrid (bonded/bolted) composite single-lap joints [J]. Composite Structures, 2005, 69(1): 35-43.
[11] Kelly G. Quasi- static strength and fatigue life of hybrid (bonded/bolted) composite single-lap joints [J]. Composite Struetures, 2006, 72(1); 119-129.
[12] Hoang-Ngoc C T, Paroissien E. Simulation of single- lap bonded and hybrid (bolted/bonded) joints with flexible adhesive [J], International Journal of Adhesion & Adhesives, 2010, 30(3): 117-129.
[13] KweonJH, Jung J W, Kim T H, et al. Failure of earboncomposite- to - aluminum joints with combined mechanical fasteningand adhesive bonding [J]. Composite Structures, 2006, 75(1-4): 192-198.
[14] 沃洛别依 B B,西洛特金 O C.复合材料结构连接技术[M].北京:国防工业出版社,1991:16-18.
[15] 游敏,郑小玲.胶接强度分析及应用[M].武汉:华中科技大学出版社,2009:113-122.
[16] Harris H G, Ojalvo I U, Hooson R E. Stress and deflection analysis of mechanically fastened joints, AFFDL - TR - 70 - 49 [R]. Ohio: Air Force Flight Dynamics Laboratory/Air Force Systems Command, 1970: 27-32.
[17] 张爽,王栋,郦正能,等.复合材料层合板多钉连接结构累积损伤过程可视化仿真模拟[J].复合材料学报,2006.23(3):135-140.
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%