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CFRP对称铺层环形法兰连接拉伸刚度计算方法 被引量:1

Calculation Method of Tensile Stiffness of Symmetrically Laminated Annular Flange Connection Made of Carbon Fiber Reinforced Plastics
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摘要 为计算碳纤维增强复合材料(carbon fiber reinforced plastic,CFRP)对称铺层环形法兰连接的拉伸刚度,基于圆板对称弯曲和经典层合板理论提出一种考虑环向支撑、材料各向异性和撬力作用系数的计算方法。在制备过程中,采用预浸料手工铺设和模压成型的方法成型试件,而后开展了3组不同法兰板厚度(2.2,3.0,3.8 mm)连接件轴向拉伸试验。通过对比理论计算值与试验结果,验证了计算方法的正确性,误差均不大于13.61%。通过理论模型分析影响因素,结果表明:拉伸刚度随法兰板厚度、外径和内径的增大而增大,随螺栓所在的半径变大而减小;改变螺栓位置对于拉伸刚度的提升比改变法兰板内外径更显著,当螺栓位置由90 mm调整至85 mm时,拉伸刚度提升59.54%。 To calculate the tensile stiffness of symmetrically laminated annular flange connection made of carbon fiber reinforced plastics(CFRP),a calculation method considering circumferential support,material anisotropy and prying effect factor is proposed based on the symmetrical bending of circular plate and the classical laminated plate theories.By the way of manual laying and molding of prepreg,the forming of the specimen was realized.Then,the axial tensile tests were carried out on three groups of connections with different flange thickness(2.2,3.0,3.8 mm).The theoretical calculation values were compared with the test results,and the correctness of the calculation method was verified,with the maximum error of 13.61%.The influence factors were investigated by the theoretical model.The results show that the tensile stiffness increases with the increase of flange thickness,outer diameter and inner diameter,and decreases with the increase of bolt position radius.The bolt position shifting is more effective for improving the tensile stiffness than changing the inner and outer diameters of the flange plate.When the bolt position is adjusted from 90 mm to 85 mm,the tensile stiffness is increased by 59.54%.
作者 刘建邦 李峰 LIU Jianbang;LI Feng(College of Field Engineering,Army Engineering University of PLA,Nanjing 210007,China)
出处 《陆军工程大学学报》 2023年第3期24-31,共8页 Journal of Army Engineering University of PLA
基金 国家自然科学基金(51778620)。
关键词 CFRP法兰连接 拉伸刚度 对称铺层 预浸料 模压工艺 环形板 位移场 撬力作用系数 CFRP flange connection tensile stiffness symmetrical lamination prepreg molding process annular plate displacement field prying effect factor
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  • 1吴杰,肖正航.碳纤维复合材料残余应力消除方法探讨[J].航天制造技术,2012(4):38-40. 被引量:2
  • 2王建花,钱林方,袁人枢.复合材料身管的热残余应力[J].弹道学报,2007,19(1):82-85. 被引量:7
  • 3徐亮工.缠绕玻璃钢管道的残余热应力[J].玻璃钢/复合材料,1997(1):11-12. 被引量:3
  • 4ZHANG D D,HUANG Y X,ZHAO Q L,et al.Flexural properties of a lightweight hybrid FRP-aluminum modular space truss bridge system[J].Composite Structures,2014,108: 600-615.
  • 5LI F,ZHAO Q L,CHEN L,et al.Experimental and theoretical research on the compression performance of CFRP sheet confined GFRP short pipe[J].The Scientific World Journal,2014,2014: 1-12.
  • 6JEGLEY D C,WU K C,PHELPS J E,et al.Structural efficiency of composite struts for aerospace applications[J].Journal of Spacecraft and Rockets,2012,49(5): 915-924.
  • 7SCHVTZE R.Lightweight carbon fibre rods and truss structures[J].Materials & Design,1997,18(4-6): 231-238.
  • 8钱鹏,叶列平,翁冠群.CFRP杆轴心受力失效模式与变形性能研究[C]//第三届全国FRP学术交流会议论文集.北京: 中国土木工程学会,2004: 349-355.
  • 9WILD P M,VICKERS G W.Analysis of filament-wound cylinderical shells under combined centrifugal pressure and axial loading[J].Composites Part A: Applied Science & Manufacturing,1997,28(1): 47-55.
  • 10JOLICOEUR C,CARDOU A.Analytical solution for bending of coaxial orthotropic cylinders[J].Engineering Mechanics,1994,120(12): 2556-2574.

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