材料工程与机械制造

复合材料螺接性能的影响因素研究

  • 张岐良 ,
  • 曹增强
展开
  • 西北工业大学 机电学院,陕西 西安 710072

收稿日期: 2011-07-26

  修回日期: 2011-10-13

  网络出版日期: 2012-04-20

Study on Factors Influencing the Performance of Composite Bolted Connections

  • ZHANG Qiliang ,
  • CAO Zengqiang
Expand
  • School of Mechanical Engineering, Northwestern Polytechnical University, Xi’an 710072, China

Received date: 2011-07-26

  Revised date: 2011-10-13

  Online published: 2012-04-20

摘要

利用有限元软件ANSYS建立了单钉双剪复合材料单拉接头的1/2模型,研究了钉孔配合、螺栓预紧力和接触面间摩擦对接头的强度等性能的影响。设计了若干实验,证明有限元模型是有效的,其计算误差控制在10%以内。有限元计算结果表明:小干涉量的过盈配合能极大地提高接头的强度,与3%间隙量相比,最优干涉量下接头强度可提高36.5%;适当的螺栓拧紧力矩也可提高接头的强度;接头中被连接板间的摩擦对接头强度也是有利的,但在一定接头尺寸条件下,摩擦力的增大有可能会改变接头的破坏模式。以上研究成果为复合材料多钉连接钉载分配均匀化的参数化分析提供了一个突破口,这也是本文后续研究的一个内容。

本文引用格式

张岐良 , 曹增强 . 复合材料螺接性能的影响因素研究[J]. 航空学报, 2012 , (4) : 755 -762 . DOI: CNKI:11-1929/V.20111202.1031.002

Abstract

A double-lap single-bolt composite joint is designed as a model using the ANSYS finite element (FE) package. The joint is subjected to longitudinal tensile loads and half of the model is numerically analyzed. Three key factors influencing the performance of the connection are studied, including the bolt-hole fit, bolt pretightening force and the friction between the contacting plates. The model is then validated by several experiments, with computational errors of less than 10%. Analytical results show that a small magnitude of interference substantially improves the strength of the joints. With optimum interference, there is an increase of joint strength up to 36.5% as compared with the 3% clearance fit scenario. An adequate tightening torque also enhances the joint strength. The friction between the connecting laminates is also beneficial to increasing the strength. The failure mode varies with the friction coefficients between the plates for specific connection sizes. These findings signifies a beginning for the parametric analysis on load distribution uniformization in multi-bolted composite joints, which will be explored in subsequent studies.

参考文献

[1] Chen S J. Composite technology and large aircraft. Acta Aeronautica et Astronautica Sinica, 2008, 29(3): 605-610.(in Chinese) 陈绍杰. 复合材料技术与大型飞机. 航空学报,2008, 29(3): 605-610.
[2] McCarthy M A, McCarthy C T, Lawlor V P, et al. Three-dimensional finite element analysis of single-bolt, single-lap composite bolted joints:Part I—model development and validation. Composite Structures, 2005, 71(2): 140-158.
[3] Ireman T. Three-dimensional stress analysis of bolted single-lap composite joints. Composite Structures, 1998, 43(3): 195-216.
[4] Thoppul S D, Finegan J, Gibson R F. Mechanics of mechanically fastened joints in polymer-matrix composite structures—a review. Composites Science and Technology, 2009, 69(3-4): 301-329.
[5] Hühne C, Zerbst A K, Kuhlmann G, et al. Progressive damage analysis of composite bolted joints with liquid shim layers using constant and continuous degradation models. Composite Structures, 2010, 92(2): 189-200.
[6] Park H J. Effects of stacking sequence and clamping force on the bearing strengths of mechanically fastened joints in composite laminates. Composite Structures, 2001, 53(2): 213-221.
[7] Park H J. Bearing failure analysis of mechanically fastened joints in composite laminates. Composite Structures, 2001, 53(2): 199-211.
[8] Kiral B G. Effect of the clearance and interference-fit on failure of the pin-loaded composites. Materials & Design, 2010, 31(1): 85-93.
[9] Chakherlou T N, Mirzajanzadeh M, Abazadeh B, et al. An investigation about interference fit effect on improving fatigue life of a holed single plate in joints. European Journal of Mechanics, 2010, 29(4): 675-682.
[10] Pradhan B, Ramesh B P. Assessment of beneficial effects of interference-fit in pin-loaded FRP composites. Journal of Reinforced Plastics and Composites, 2007, 26(8): 771-89.
[11] Pakdil M. Failure analysis of composite single bolted-joints subjected to bolt pretension. Indian Journal of Engineering & Materials Sciences, 2009, 16(2): 79-85.
[12] Li H X, Hu Y C, Zhang J Z. Study on simulating bolt pretension by using ANSYS. Journal of Shandong University of Science and Technology: Natural Science, 2006, 25(1): 57-59.(in Chinese) 李会勋, 胡迎春, 张建中. 利用ANSYS模拟螺栓预紧力的研究. 山东科技大学学报: 自然科学版, 2006, 25(1): 57-59.
[13] Oh J H, Kim Y G, Lee G D. Optimum bolted joints for hybrid composite materials. Composite Structures, 1997, 38(1-4): 329-341.
[14] Xiao Y, Ishikawa T. Bearing strength and failure behavior of bolted composite joints. Part I: experimental investigation. Composites Science and Technology, 2005, 65(7-8): 1022-1031.
[15] Sen F, Pakdil M, Sayman O, et al. Experimental failure analysis of mechanically fastened joints with clearance in composite laminates under preload. Materials & Design, 2008, 29(6): 1159-1169.
[16] Waszczak J P, Cruse T A. Failure mode and strength predictions of anisotropic bolt bearing specimens. Journal of Composite Materials, 1971, 5(3): 421-425.
[17] ASTM standard D5961/D5961M-10. Standard test method for bearing response of polymer-matrix composite laminates. West Conshohocken,PA: ASTM International, 2010.
[18] Geoffrey L K, John W F, John H S. Guide to design criteria for bolted and riveted joints. 2nd ed. Chicago: AISC, 1987: 111.
[19] Kelly G, Hallström S. Bearing strength of carbon fibre/epoxy laminates: effects of bolt-hole clearance. Composi-tes Part B, 2004, 35(4): 331-343.
[20] Adams D O, Bell S J. Compression strength reductions in composite laminates due to multiple-layer waviness. Composites Science and Technology, 1995, 53(2): 207-212.
[21] Caprino G, Giorleo G, Nele L, et al. Pin-bearing strength of glass mat reinforced plastics. Composites Part A, 2002, 33(6): 779-785.
文章导航

/