基于二维有限元模型,对复合材料层合板螺栓连接的破坏失效问题利用刚度降低的方法来模拟损伤演化过程.在ABAQUS有限元软件中加入损伤子程序对螺栓连接强度和失效模式进行数值计算.计算结果表明,该方法能够较好地反映和符合实验结果.对计算结果分析发现,对于正交铺层,剪切非线性不明显,非线性和线性分析得到的计算结果差别比较小;而对于角铺层,剪切效应比较显著,非线性和线性分析两种计算结果差别很大,而且非线性分析比较适合于角铺层层合板的计算.配合间隙的大小对挤压强度会产生很大的影响,随着配合间隙的增大,连接强度大大降低.对于不同的配合间隙,出现严重损伤的位置不同.间隙小时,在远离螺栓孔中心线处损伤最大;间隙大时,损伤在靠近螺栓孔中心线位置最为严重;间隙越大,损伤峰值越高.
参考文献
[1] | Hyer M W, Klang E C. The effect of pin elasticity, clearance and friction on the stresses in a pin-load orthotropic plate [J]. J Compos Mater, 1987, 21(3): 190-206. |
[2] | Kelly G, Hallstrom S. Bearing strength of carbon fiber/epoxy laminates: Effects of bolt hole clearance [J]. Composites Part B, 2004, 35(1): 331-343. |
[3] | DiNicola A J, Fantle S L. Bearing strength of clearance fit fastener holes in toughened graphite/epoxy laminates [J].Composite Materials : Testing and Design, 1993, 11 ( 1 ) :220-237. |
[4] | Chen W H, Lee S A, Yeh J T. Three-dimensional contact stress analysis of a composite laminate with bolted joint [J].Composite Structures, 1995, 30 ( 1 ): 287-297. |
[5] | Okutan B. The effects of geometric parameters on the failure strength for pin-loaded multi-directional fiberglass reinforced epoxy laminate [J]. Composites Part B, 2002, 33(2): 567-578. |
[6] | Dano M L, Gendron G, Picard A. Stress and failure analysis of mechanically fastened joints in composites laminates [J]. Composite Structures, 2000, 50(1): 287-296. |
[7] | Tserpes K I, Papanikos P, Kermanidis T H. A three-dimensional progressive damage model for bolted joints in com posite laminates subjected to tensile loading [J]. Composites Part B, 2002, 33(1): 521-529. |
[8] | Marie L D, Gug G, Andre P. Stress and failure analysis of mechanically fastened joints in composite laminates [J].Composite Structures, 2000, 50(1): 287-296. |
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:
-
10%
-
20%
-
30%
-
40%
-
50%