RESEARCH ON THE INFLUENCE FACTORS OF THE BEARING CAPACITY FOR BONDED-BOLTED HYBRID JOINTS

Abstract

Abstract: Theoretical and experimental analyses were performed on the effects of the adhesive layer thickness, the bolt location and the bolt rigidity on bearing capacity of bonded-bolted hybrid joints with bonded-bolted deformation harmony. The valid range of the calculation formula for bearing capacity was discussed. It is founded that the varying of the related geometrical and mechanic parameters influence the failure mode and the bearing capacity and the current calculation method is limited.

Key words: composites, bonded-bolted hybrid joint, influence factor, bonded-bolted deformation harmony condition, bearing capacity

CLC Number:

TB332

YUAN Hui, LIU Peng-fei, ZHAO Qi-lin, MA Yu. RESEARCH ON THE INFLUENCE FACTORS OF THE BEARING CAPACITY FOR BONDED-BOLTED HYBRID JOINTS[J]. COMPOSITES SCIENCE AND ENGINEERING, 2013, 0(3): 66-71.

References

[1] 沃丁柱主编. 复合材料大全[M]. 北京: 化学工业出版社,2000.
[2] 朱坤宁,万水. FRP-钢组合结构桥梁建造关键技术研究[J]. 玻璃钢/复合材料,2011,(3).
[3] L. J. Hart-Smith. Bonded-bolted composite joints[J]. Journal of Aircraft,1985,22(11): 993-1000.
[4] L. J. Hart-Smith. Design methodology for bonded-bolted composite joints(Vol. 1 Analysis derivations and illustrative solutions): Technical report AFWAL-TR-81-3154[R]. Wright-Patterson air force base,Ohio: Flight dynamics laboratory/Air force wright aeronautical laboratories/Air force systems command,1981.
[5] 中国航空研究院编. 复合材料连接手册[M]. 北京: 航空工业出版社,1994. 11-134.
[6] 乔海涛,赖士洪,邹贤武. 胶铆连接性能研究[J]. 中国胶粘剂,2001,11(1): 52-53.
[7] Jin-Hwe Kweon,Jae-Woo Jung,Tae-Hwan Kim,et al. Failure of carbon composite-to-aluminum joints with combined mechanical fastening and adhesives bonding[J]. Composite Structures,2006,75: 192-198.
[8] Gordon Kelly. Load transfer in hybrid (bonded/bolted) composite single-lap joints[J]. Composite Structures, 2005,69: 35-43.
[9] Gordon Kelly. Quasi-static strength and fatigue life of hybrid (bonded/bolted) composite single-lap joints[J]. Composite Structures,2006, 72: 119-129.
[10] 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.
[11] Cat-Tan Hoang-Ngoc,Eric Paroissien. Simulation of single-lap bonded and hybrid (bolted/bonded) joints with flexible adhesive[J]. International Journal of Adhesion ＆ Adhesives,2010,30: 117-129.
[12] 马毓. 复合材料胶-螺混合连接接头承载力分析[J]. 复合材料学报,2011,28(4): 225-230.
[13] 晏石林,杨学忠,刘雄亚等编著. 复合材料建筑结构及其应用[M]. 北京: 化学工业出版社,2006.
[14] 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.
[15] 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.
[16] L. J. Hart-Smith. Adhesive-bonded double-lap joints: Techincal report NASA CR-112235[R]. Virginia: National Aeronautics and Space Administration, 1973.
[17] Volkersen O. Die Nietkraftverteilung in Zufbeanspruchten Nietverbindungen mit Konstanten Laschenguerschnitten[J]. Luftfahrtforschung,1938, 15(1/2): 41-47.
[18] Goland M and Reissner E. The stresses in cemented joints[J]. Appl. Mech.,1944,66: 17-27.
[19] 马毓. 纤维增强树脂基复合材料构件连接技术研究[D]. 南京: 解放军理工大学,2011: 92-97.
[20] W. F. Mccombs,J. C. Mcqueen,J. L. Perry. Analytical design methods for aircraft structural joints: Technical report AFFDL-TR-67-184[R]. Wright-Patterson air force base,Ohio: Air force flight dynamics laboratory/Air force systems command,1968.