Experimental and numerical study on the dynamic and lubrication characteristics of the rotor-bearing-frame system in a variable-speed scroll compressor

Che Wang, Hua Zhong, Shuai Zhang, Junming Cheng, Jianhua Wu
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Abstract

The variable-speed scroll compressors can adapt to the various demands of heating and cooling capacity, and the rotational speeds significantly influence the rotor dynamic and bearings lubrication, which might cause performance and reliability issues. In this paper, numerical models for the rotor-bearing-frame system are developed by coupling the Reynolds equation, rotor dynamic equation, and the flexibility equation of the frame. The experimental apparatus is also established to directly measure the journal displacement response in the hermetic high-pressure shell of the compressor. The predicted journal center trajectories are compared with the experimental results and they show good agreement. Results show that the whirl radius decreases with the increase of rotational speed at the measuring point, while the opposite tendency can be observed at the bottom of the main bearing. Transient dynamic analysis of the rotor shows that the tilting and deformation of the rotor vary with respect to different rotational speeds. The displacement of the crank part could lead to the separating tendency between orbiting and fixed scrolls through the coupled orbiting bearing, especially at the lower rotational speed, due to the pull of main balance weight. The numerical results also reveal that the distribution of oil film pressure is dominated by the squeeze effect due to the relatively stable magnitude but the variable direction of loads on the shaft. The influence of the deformation of the cantilevered bearing frame on the oil film thickness is significant but the maximum deformation moves downward at the higher rotational speed.
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变速涡旋式压缩机转子-轴承-框架系统动态和润滑特性的实验和数值研究
变速涡旋压缩机可适应各种制热和制冷能力需求,而转速对转子动态和轴承润滑有显著影响,可能导致性能和可靠性问题。本文通过耦合雷诺方程、转子动态方程和机架柔性方程,建立了转子-轴承-机架系统的数值模型。同时还建立了实验装置,以直接测量压缩机密封高压壳体中的轴颈位移响应。将预测的轴颈中心轨迹与实验结果进行比较,两者显示出良好的一致性。结果表明,在测量点处,旋涡半径随着转速的增加而减小,而在主轴承底部则观察到相反的趋势。转子的瞬态动态分析显示,转子的倾斜和变形随不同的转速而变化。曲柄部分的位移可通过耦合轨道轴承导致轨道涡旋和固定涡旋之间的分离趋势,特别是在较低转速时,由于主平衡重的拉力。数值结果还显示,由于轴上载荷的大小相对稳定但方向多变,油膜压力的分布主要受挤压效应的影响。悬臂轴承架的变形对油膜厚度的影响很大,但在转速较高时,最大变形向下移动。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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