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层状球面弹性轴承刚度设计、仿真与试验
引用本文:陈高升,杨岩.层状球面弹性轴承刚度设计、仿真与试验[J].航空动力学报,2015,30(6):1512-1519.
作者姓名:陈高升  杨岩
作者单位:1. 中国航空工业集团公司 北京航空材料研究院减振降噪材料及应用技术航空科技重点实验室, 北京 100095;
基金项目:基础科研计划(A052013002)
摘    要:从理论上推导了层状球面弹性轴承各橡胶层的压缩刚度和扭转刚度计算公式,通过具体算例,将层状球面弹性轴承各橡胶层压缩刚度和扭转刚度的理论计算结果与仿真结果进行了对比分析.结果表明:各橡胶层压缩刚度的理论计算结果与仿真结果基本吻合,最大误差为3.98%.各橡胶层扭转刚度的仿真结果与理论计算结果存在一定偏差,从小接头开始的前半部分橡胶层扭转刚度的仿真结果大于理论计算结果,最大误差为33.3%;后半部分橡胶层扭转刚度仿真结果小于理论计算结果,最大误差为32.8%.压缩刚度对压力变化表现的非线性特性不明显,扭转刚度则随扭转角的增大,其非线性特性变得越显著.但通过理论方法、有限元仿真方法得到的层状球面弹性轴承等效压缩刚度和等效扭转刚度与试验结果吻合良好. 

关 键 词:弹性轴承    压缩刚度    扭转刚度    球面    橡胶
收稿时间:2014/11/6 0:00:00

Stiffness design, simulation and test of laminated spherical elastomeric bearing
CHEN Gao-sheng and YANG Yan.Stiffness design, simulation and test of laminated spherical elastomeric bearing[J].Journal of Aerospace Power,2015,30(6):1512-1519.
Authors:CHEN Gao-sheng and YANG Yan
Institution:1. Aviation Key Laboratory of Science and Technology on Materials and Application Research for Vibration and Noise Reduction, Beijing Institute of Aeronautical Materials, Aviation Industry Corporation of China, Beijing 100095, China;2. Military Representative Office in Beijing Region, Army Aviation Department, General Staff Headquters, the Chinese People's Liberation Army, Beijing 100083, China
Abstract:The computational formulations of compression stiffness and torsion stiffness of every rubber layer of laminated spherical elastomeric bearing were deduced in theory, and the theoretical results and simulated results of compression stiffness and torsion stiffness of every rubber layer of laminated spherical elastomeric bearing were compared through examples. The results show that the theoretical result of compression stiffness is basically in accord with the simulated result, the maximum error is 3.98%. There are some differences from simulated result and theoretical result for torsion stiffness in every rubber layer; the simulated result of torsion stiffness is bigger than theoretical result for the first half of all the rubber layers from the little end, the maximum error is 33.3%; the simulated result of torsion stiffness is smaller than theoretical result for the second half of all the rubber layers, the maximum error is 32.8%. The nonlinear characteristic of compression stiffness is not evident for the alterable pressure, and that of torsion stiffness is more evident with the increase of the torsion angle. But the equivalent compression stiffness and equivalent torsion stiffness got from theoretical method and finite element simulation method are in good agreement with the test results.
Keywords:elastomeric bearing  compression stiffness  torsion stiffness  spherical  rubber
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