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波箔型径向气体箔片轴承-转子系统升降速动态特性试验

徐方程 刘占生 马瑞贤 黄飞淋

徐方程, 刘占生, 马瑞贤, 黄飞淋. 波箔型径向气体箔片轴承-转子系统升降速动态特性试验[J]. 航空动力学报, 2014, 29(1): 216-224. doi: 10.13224/j.cnki.jasp.2014.01.028
引用本文: 徐方程, 刘占生, 马瑞贤, 黄飞淋. 波箔型径向气体箔片轴承-转子系统升降速动态特性试验[J]. 航空动力学报, 2014, 29(1): 216-224. doi: 10.13224/j.cnki.jasp.2014.01.028
XU Fang-cheng, LIU Zhan-sheng, MA Rui-xian, HUANG Fei-lin. Dynamic performance tests of bump-type gas foil journal bearing-rotor system in start-up and shut-down procedures[J]. Journal of Aerospace Power, 2014, 29(1): 216-224. doi: 10.13224/j.cnki.jasp.2014.01.028
Citation: XU Fang-cheng, LIU Zhan-sheng, MA Rui-xian, HUANG Fei-lin. Dynamic performance tests of bump-type gas foil journal bearing-rotor system in start-up and shut-down procedures[J]. Journal of Aerospace Power, 2014, 29(1): 216-224. doi: 10.13224/j.cnki.jasp.2014.01.028

波箔型径向气体箔片轴承-转子系统升降速动态特性试验

doi: 10.13224/j.cnki.jasp.2014.01.028
基金项目: 国家自然科学基金(11176010);航空科学基金(20110377005)

Dynamic performance tests of bump-type gas foil journal bearing-rotor system in start-up and shut-down procedures

  • 摘要: 为了研究以波箔型径向气体箔片轴承为支承的轴承-转子系统动力学特性,专门设计了波箔型径向气体箔片轴承试验台,质量为0.458kg的转子在该试验台上实现了超过80000r/min的运转速度.径向轴承为波箔型径向气体箔片轴承,止推轴承为多叶箔片轴承.试验结果表明:波箔型径向气体箔片轴承能够实现转子高速运行,在转子起飞后具有良好的运行稳定性,其轴承支承处振动位移幅值一直维持在20μm之内.由于驱动涡轮受到不平衡气流力的作用,转轴升速时的起飞转速要高于降速时的起飞转速.

     

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出版历程
  • 收稿日期:  2012-12-07
  • 刊出日期:  2014-01-28

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