期刊文献+

汽车空气弹簧橡胶气囊的结构分析方法 被引量:11

Structural Analysis Method of Automotive Air-spring Rubber Air-bag
下载PDF
导出
摘要 为研究一套汽车空气弹簧橡胶气囊的结构分析方法,对橡胶气囊几何模型进行了简化,进而以薄膜理论、网格理论以及层合板理论为理论依据,推导出橡胶气囊薄膜内力、应力、应变、帘线力和变形位移等计算公式。为橡胶气囊的结构分析和强度校核奠定了理论基础。为检验所提出的结构分析方法的精确度和有效性,以一汽车悬架用空气弹簧为实例,计算其变形和帘线力。为了进行比较,还对该空气弹簧结构建立了三维有限元模型,并用非线性有限元软件ABAQUS进行有限元数值分析。这两种方法的计算结果综合比较表明,所提出的结构分析方法不仅预测结果精确,而且大大节省计算量。 To study the structural analysis method of automotive air-spring rubber air-bag, the geometric model of air-spring rubber air-bag is simplified. Then, the equations of internal force, stress, strain, cord force and deformation displacement of the rubber air-bag membrane are derived on the basis of membrane theory, netting theory and laminated plate theory, thus laying a theoretical basis for the structural analysis and strength check of rubber air-bag. To assess the accuracy and validity of the proposed structural analysis method, an air-spring used on a vehicle suspension is taken as an example, its deformation and cord force are calculated. For the purpose of comparison, a 3D finite element model of this air-spring is built, and its numerical analysis is carried out by using nonlinear finite element software ABAQUS. Comprehensive comparison of the calculation results of the two methods shows that the proposed structural analysis method not only predicts accurately, but also saves a great deal of calculation.
出处 《机械工程学报》 EI CAS CSCD 北大核心 2009年第9期221-225,共5页 Journal of Mechanical Engineering
基金 浙江省科技厅重点攻关(2006C11089) 江苏大学研究生创新基金(1291120015) 江苏科技大学青年教师基金(35020802)资助项目
关键词 橡胶气囊 薄膜理论 层合板理论 结构分析 Rubber air-bag Membrane theory Laminated plate theory Structural analysis
  • 相关文献

参考文献10

  • 1WOODROOFFE J.Heavy truck suspension dynamics:Methods for evaluating suspension road friendliness and ride quality[C]//Society of Automotive Engineers.SAE Transactions,February 16-19,1996,Cobo Center,Detroit,Michigan.New York:SAE,1996:337-343.
  • 2杨卫民,陈灿辉,陈亚玲,任燕莎.汽车减震用空气弹簧的有限元分析(英文)[J].北京化工大学学报(自然科学版),2004,31(3):105-109. 被引量:4
  • 3陈燕虹,杨兴龙,王勋龙.大客车空气弹簧动态特性的试验分析[J].汽车技术,2002(10):19-20. 被引量:27
  • 4GRAMOLL K C.Stress analysis of filament wound open-ended composite shells[C]//AIAA/ASME/ASCE/ AHS/ASC.Collection of Technical Papers-AIAA/ASME Structures,Structural Dynamics and MaterialsConfere-nce,April 19-22,1993,La Jolla,California.Washington:AIAA,1993:2 733-2 741.
  • 5俞洪,周锋,丁剑平.充气轮胎性能与结构[M].广州:华南理工大学出版社,1998.
  • 6FUKUNAGA H,CHOU Tsuwei.On laminate configurations for simultaneous failure[J].Journal of Co-mposite Materials,1988,22:271-286.
  • 7GILES G L.Design-oriented analysis of aircraft fuselage structures using equivalent plate methodology[J].Journal of Aircraft,1999,36(11):21-28.
  • 8蔡为仑.复合材料设计[M].北京:科学出版社,1989.
  • 9KULIKOV G M.Computational models for multilayered composite shells with application to tires[J].Tire Science Technology,1996,24(1):11-38.
  • 10张丰发,杜星文,匡震邦.拉伸条件下帘线/橡胶复合材料的失效准则[J].上海交通大学学报,2005,39(5):832-835. 被引量:3

二级参考文献17

  • 1王立公,冯振东,宋传学.Audi100轿车动力总成液力悬置动态特性的实验分析[J].汽车技术,1994(12):14-19. 被引量:4
  • 2Breidenbach R F, Lake G J. Mechanics of fracture in two-ply laminates [J]. Rubber Chemistry and Technology. 1979,52:96-108.
  • 3Lee B L, Liu D S. Cumulative damage of fiber-rubber composites under fatigue loading [J]. J Compos Mater, 1994,28: 1261 - 1286.
  • 4Kawamoto J. Fatigue of rubber composites [D].Cambridge :MIT, 1988.
  • 5Huang Y S, Yeoh O H. Crack initiation and propagation in model cord-rubber composites [J]. Rubber Chemistry and Technology, 1989,62: 709- 725.
  • 6Wu S. A generalized criterion for rubber toughening: the critical matrix ligament thickness[J]. J Appi Polym Sci,1988,35:549-561.
  • 7Palley I. A fracture mechanics approach to interlaminar failure of unidirectional reinforced composites [J]. J Reinf Plast Comp,1990,9:174-181.
  • 8CuiWC, WisnomM R, Jones M. A comparison of failure criteria to predict delamination of unidirectional glass/epoxy specimens waisted through the thickness [J]. Composites, 1992,23:158 - 166.
  • 9Holger T. A review of the biaxial strength of fiberreinforced plastics [J]. Composites, 1998,29A: 869 -886.
  • 10Soden P D,Hinton M J, Kaddour A S. Acomparison of the predictive capabilities of current failure theories for composite laminates[J]. Composites Science and Technology, 1998,58 (7): 1225- 1254.

共引文献43

同被引文献66

引证文献11

二级引证文献28

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