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气体止推箔片轴承试验台设计及试验

徐方程 刘占生 张广辉 张雯 孙毅

徐方程, 刘占生, 张广辉, 张雯, 孙毅. 气体止推箔片轴承试验台设计及试验[J]. 航空动力学报, 2016, 31(9): 2298-2304. doi: 10.13224/j.cnki.jasp.2016.09.032
引用本文: 徐方程, 刘占生, 张广辉, 张雯, 孙毅. 气体止推箔片轴承试验台设计及试验[J]. 航空动力学报, 2016, 31(9): 2298-2304. doi: 10.13224/j.cnki.jasp.2016.09.032
XU Fang-cheng, LIU Zhan-sheng, ZHANG Guang-hui, ZHANG Wen, SUN Yi. Test rig design and experiment of gas thrust foil bearing[J]. Journal of Aerospace Power, 2016, 31(9): 2298-2304. doi: 10.13224/j.cnki.jasp.2016.09.032
Citation: XU Fang-cheng, LIU Zhan-sheng, ZHANG Guang-hui, ZHANG Wen, SUN Yi. Test rig design and experiment of gas thrust foil bearing[J]. Journal of Aerospace Power, 2016, 31(9): 2298-2304. doi: 10.13224/j.cnki.jasp.2016.09.032

气体止推箔片轴承试验台设计及试验

doi: 10.13224/j.cnki.jasp.2016.09.032
基金项目: 

国家自然科学基金(11572098)

详细信息
    作者简介:

    徐方程(1985-),男,浙江金华人,副教授,博士后,主要研究方向为气体箔片轴承、挤压油膜阻尼器及转子动力学等.

  • 中图分类号: V229+.2;TH133.37

Test rig design and experiment of gas thrust foil bearing

  • 摘要: 设计并制造了带有箔片密封式活塞加载装置的气体止推箔片轴承试验台,对带有冷却通道和径向辐射分布波纹箔片的止推箔片轴承进行了试验研究,分别在15000,20000,25000r/min转速下采用摩擦力矩法对带有冷却通道的止推箔片轴承进行了承载力测试试验.结果表明:带有箔片密封结构的活塞式加载装置能够很好地实现止推轴承加载功能,验证了试验台设计的成功,该止推箔片轴承在不同转速下分别得到了145,195,260N的推力,并且轴承承载力和气膜间隙成非线性关系.

     

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出版历程
  • 收稿日期:  2015-02-11
  • 刊出日期:  2016-09-28

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