期刊文献+

轴压铆接加筋板局部屈曲弹性支持分析方法

Local Buckling Analysis Method of Elastically Restrained Riveted Stiffened Panels Under Uniaxial Compression
下载PDF
导出
摘要 考虑铆钉连接对筋条扭转弹性支持作用的影响,利用三角函数构造筋条在铆钉连接情况下的扭转支持刚度,采用里兹能量法建立轴压铆接加筋平板蒙皮局部屈曲问题的弹性支持理论分析模型及分析方法。分别采用试验方法、有限元方法、工程简化分析方法和本文分析方法对典型轴压金属Z形铆接加筋平板的蒙皮局部屈曲临界应力进行算例分析,验证了本文分析方法的合理性。在此基础上进一步研究了不同的铆钉间距和铆钉连接方式对加筋板蒙皮局部屈曲临界应力的影响。结果表明:在Z形加筋板结构形式、尺寸、铆钉间距皆为工程常用范围的前提之下,若铆钉连接方式不变,改变铆钉间距对屈曲临界应力影响不足1%;若铆钉间距不变,单排连接改为双排或者交错排可以提高屈曲临界应力约11%。 Given the influence of riveted joints on elastically rotational restraint of stiffeners,the trigonometric function was used to simulate rotational restraining rigidity of stiffener,and Ritz method was used to establish an analytical model for local skin buckling problem of riveted stiffened panels under uniaxial compression.Critical local skin buckling stresses of typical metal riveted stiffened panels with Z-shaped stiffeners were calculated and analyzed by the experimental method,the finite element method(FEM),the engineering simplified analytical method and the proposed analytical method. The reasonableness of the proposed analytical method was verified. Furthermore,the influences of rivet spacing and rivet attachment form on critical local skin buckling stresses were studied. Results showed that the variation of rivet spacing had less than 1% effects on critical local skin buckling stresses,while rivet attachment form stayed unchanged;and that double-row and interleaving-row rivet attachments could increase critical local skin buckling stresses about 11% compared with single-row rivet attachment,while rivet spacing stayed unchanged on conditions that configurations,dimensions and rivet spacing of Z-shaped stiffened panels were in common range of aerospace engineering use.
作者 陈金睿 孔斌 陈普会 杨军 甘学东 CHEN Jinrui;KONG Bin;CHEN Puhui;YANG Jun;GAN Xuedong(AVIC Chengdu Aircraft Design&Research Institute,Chengdu,610091,China;State Key Laboratory of Mechanics and Control of Mechanical Structures,Nanjing University of Aeronautics&Astronautics,Nanjing,210016,China)
出处 《南京航空航天大学学报》 EI CAS CSCD 北大核心 2020年第6期989-996,共8页 Journal of Nanjing University of Aeronautics & Astronautics
基金 民机科研(MJ-2015-F-038)资助项目。
关键词 铆钉连接 加筋壁板 弹性支持 局部屈曲 里兹法 riveting stiffened panels elastical restraint local buckling Ritz method
  • 相关文献

参考文献4

二级参考文献21

  • 1陈桂娟,矫桂琼,熊伟,王忠平.复合材料层合板非线性后屈曲特性的研究[J].武汉科技大学学报,2005,28(1):103-107. 被引量:4
  • 2程文渊,崔德刚,顾志芬,崔德渝,王进.复合材料多墙结构承载能力分析[J].复合材料学报,2006,23(4):119-123. 被引量:6
  • 3朱菊芬,杨海平,汪海,余守旗.复合材料加筋板壳结构的后屈曲强度及破坏分析程序系统[J].计算结构力学及其应用,1996,13(4):489-493. 被引量:11
  • 4Pietropaoli E,Riccio A.Finite element analysis of the stability(buckling and post-buckling) of composite laminated structures:well established procedures and challenges[J].Appl Compos Master.2012,19(1):79-96.
  • 5Jaunky N,Knight N F.Formulation of an improved smeared theory for buckling analysis of grid-stiffened composite panels[J].Composite PartB,1996,27B(5):519-526.
  • 6Chen N Z,Guedes Soares C.Reliability assessment of post-buckling compressive strength of laminated composite plates and stiffened panels under axial compression[J].Solids and Structure.2007,44(22/23):7167-7182.
  • 7Bisagni C,Lanzi L.Post-buckling optimization of composite stiffened panels using neural networks[J].Composite Structures.2002,58(2):237-247.
  • 8崔德渝,顾志芬.复合材料层板损伤起止问题研究 //中国科协2001年学术年会.长春:中国科协,2001.
  • 9中国航空研究院.飞机设计手册(第九册)[M].北京:航空工业出版社,2001.
  • 10A.C. Orifici,S.A. Shah,I. Herszberg,A. Kotler,T. Weller.Failure analysis in postbuckled composite T-sections[J].Composite Structures.2008(1)

共引文献40

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部