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基于Kriging模型的轴承结构参数优化设计方法

冯吉路 孙志礼 李皓川 田越

冯吉路, 孙志礼, 李皓川, 田越. 基于Kriging模型的轴承结构参数优化设计方法[J]. 航空动力学报, 2017, 32(3): 723-729. doi: 10.13224/j.cnki.jasp.2017.03.026
引用本文: 冯吉路, 孙志礼, 李皓川, 田越. 基于Kriging模型的轴承结构参数优化设计方法[J]. 航空动力学报, 2017, 32(3): 723-729. doi: 10.13224/j.cnki.jasp.2017.03.026
Optimization design method of bearing structure parameters based on Kriging model[J]. Journal of Aerospace Power, 2017, 32(3): 723-729. doi: 10.13224/j.cnki.jasp.2017.03.026
Citation: Optimization design method of bearing structure parameters based on Kriging model[J]. Journal of Aerospace Power, 2017, 32(3): 723-729. doi: 10.13224/j.cnki.jasp.2017.03.026

基于Kriging模型的轴承结构参数优化设计方法

doi: 10.13224/j.cnki.jasp.2017.03.026
基金项目: 国家科技重大项目(2013ZX04011-011); 中央高校基本科研业务费专项资金(N140306004)

Optimization design method of bearing structure parameters based on Kriging model

  • 摘要: 轴承的生热率与轴承的使用寿命密切相关,为了减小轴承的生热率,以滚动轴承拟静力学分析和滚道控制理论为基础,求得轴承运转过程中的相关参数,进而得到轴承生热率.将轴承最小生热率为目标函数,通过Kriging模型和粒子群优化算法相结合的方式进行了轴承结构参数优化.对NSK 7016A5轴承的研究结果表明:轴承结构参数优化后,轴承整体和轴承内外圈生热率均变小.Kriging模型和粒子群优化算法相结合的轴承结构参数优化方法取得了良好的设计效果,并且提高了轴承的设计效率.

     

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出版历程
  • 收稿日期:  2015-07-09
  • 刊出日期:  2017-03-28

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