Analysis of Orbiting Scroll Overturning for Scroll Compressor

Man Zhao, S. Yu, Chaoyin Li, Yang Yu
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引用次数: 3

Abstract

Studies on leakage and friction have received considerable attention in scroll compressor, especially which between the fitting surface of orbiting scroll and fixed scroll, as they affect the scroll compressor performance. According to the scroll compressor working principle and structure, combined with the force model of the orbiting scroll, the overturning moment on the orbiting scroll was analyzed and verified by a specific example, in which the azimuth angle and of the overturning moment action line were calculated and compared. The results show that the overturning moment will have a significant effect not only on the leak and friction loss at the fitting surface of orbiting and fixed scroll, also on the dynamic characteristics of the orbiting scroll due to the linear change of the azimuth angle and the unstable of the azimuth angle . The result is helpful for the study on leakage, friction, and the dynamics and tribology coupling problem research of scroll compressor.
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涡旋压缩机涡旋翻转分析
涡旋压缩机的泄漏和摩擦问题是影响涡旋压缩机性能的重要因素,尤其是轨道涡旋与固定涡旋配合面之间的泄漏和摩擦问题。根据涡旋压缩机的工作原理和结构,结合轨道涡旋的受力模型,对轨道涡旋上的倾覆力矩进行了分析,并通过具体算例进行了验证,对倾覆力矩作用线的方位角和作用线进行了计算比较。结果表明:由于方位角的线性变化和方位角的不稳定性,倾覆力矩不仅会对轨道涡旋与固定涡旋的拟合面泄漏和摩擦损失产生显著影响,而且会对轨道涡旋的动态特性产生显著影响。研究结果对涡旋压缩机的泄漏、摩擦及动力学与摩擦学耦合问题的研究具有一定的指导意义。
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