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航发主轴球轴承喷油润滑热场分析及试验研究
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国家自然科学基金青年科学基金项目(52005158)


Thermal Field Analysis and Experimental Study of Oil Lubrication of Aeroengine Spindle Ball Bearing
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    摘要:

    针对航发主轴三点接触球轴承高速运转时容易引起轴承烧伤问题,采用局部法建立轴承生热模型。基于流体两相流理论和耦合传热原理,建立轴承流固耦合模型,分析转速、供油量等对流场以及轴承温度的影响。利用航发球轴承试验机开展轴承温升试验,并对仿真结果进行验证。结果表明:随着供油量的增加,轴承外圈的油量显著增加,轴承温度下降;当供油量达到1.2 L/min时,继续增加供油量冷却效果减弱;随着转速增加,轴承腔内油液减少,轴承内外圈温度均增大且内圈增幅比外圈大;随着轴向载荷增加,轴承内外圈温度均增大。试验结果与仿真计算最大误差为10.27%,验证了模型的合理性。

    Abstract:

    Aiming at the problem that the three-point contact ball bearing of aeroengine spindle is easy to be burned when it runs at high speed,the heat generation model of bearing was established by local method.Based on the theory of fluid two-phase flow and coupled heat transfer principle,a bearing fluid-structure coupling model was established.The influence of rotating speed and oil supply on flow field and bearing temperature was analyzed.The bearing temperature rise test was carried out by using the aeroengine ball bearing testing machine,and the simulation results were verified.The results show that with the increase of oil supply,the oil quantity of the bearing outer ring increases significantly and the bearing temperature decreases.When the oil supply reaches 1.2 L/min and the oil supply continues to increase,the cooling effect is weakened.With the increase of the rotating speed,the oil in the bearing chamber decreases,and the temperature of the inner ring increases and the inner ring increases more than the outer ring.With the increase of axial load,the temperature of the inner and outer rings of the bearing increases.The maximum error between the test results and the simulation calculation is 10.27%,which verifies the rationality of the model.

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刘欢,王健,朱海峰,张占立.航发主轴球轴承喷油润滑热场分析及试验研究[J].机床与液压,2024,52(13):43-49.
LIU Huan, WANG Jian, ZHU Haifeng, ZHANG Zhanli. Thermal Field Analysis and Experimental Study of Oil Lubrication of Aeroengine Spindle Ball Bearing[J]. Machine Tool & Hydraulics,2024,52(13):43-49

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  • 在线发布日期: 2024-07-25
  • 出版日期: 2024-07-15