1. 北京航空航天大学 能源与动力工程学院,北京,100191
2. 先进航空发动机协同创新中心,北京,100191
3. 中国航空工业集团公司 哈尔滨轴承有限公司 研发中心,哈尔滨,150000
Published:2017
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马艳红, 王永锋, 公平, 洪杰. 航空发动机主轴承接触应力精确仿真计算方法[J]. 航空动力学报, 2017, 32(8): 2000-2008.
doi: 10.13224/j.cnki.jasp.2017.08.025
马艳红, 王永锋, 公平, 洪杰. 航空发动机主轴承接触应力精确仿真计算方法[J]. 航空动力学报, 2017, 32(8): 2000-2008. DOI: 10.13224/j.cnki.jasp.2017.08.025.
doi: 10.13224/j.cnki.jasp.2017.08.025 DOI:
采用稳态热分析与动态接触力学分析相结合的方法以提高计算精度
考虑轴承摩擦生热及瞬态冲击效应的影响
得到经热应力修正的轴承应力分布及变化特征。研究表明:最大动态接触应力位于钢球表面
外圈滚道次之
内圈滚道最小;轴承接触应力具有明显动态冲击响应特性
分布及大小具有随机变化性;接触应力由主应力与剪切应力共同构成
随转速及轴向载荷增大而增大。
The combination of steady state thermal analysis and dynamic contact mechanics analysis was used to improve the calculation accuracy
and the stress distribution was corrected by thermal analysis
meanwhile the variation characteristics of the bearing were obtained. The research shows that
the maximum dynamic contact stress is located on the bearing ball surface
while the stress of the inner is the minimum. The contact stress of bearing has obvious dynamic response characteristics
while its distribution has a random variation. The contact stress
which increases with the rotational speed and the axial load
is composed of the principal stress and the shear stress.
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