首页> 外文期刊>Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science >Piston ring–cylinder liner lubrication analysis in a CO2 refrigeration reciprocating compressor
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Piston ring–cylinder liner lubrication analysis in a CO2 refrigeration reciprocating compressor

机译:CO 2 制冷往复式压缩机中的活塞环-缸套润滑分析

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A simulation model is developed for the piston ring–cylinder liner lubrication problem in a CO2 refrigeration reciprocating compressor. Patir and Cheng’s modified Reynolds equation including pressure flow factors, shear flow factors, and shear stress factors is used to consider the effect of surface roughness on lubrication. The piston ring is assumed to be fully flooded at the leading edge, and both the cavitation case and fully flooded case are considered at the trailing edge. Modified Reynolds boundary condition is employed. The simulation results show that, the minimum oil film thickness has a maximum magnitude in the middle stroke region for downward stroke and upward stroke. In the vicinity of the dead centres, the magnitude of the friction force is much higher than that in the middle stroke region. The oil film pressure distribution along the piston ring thickness at different specified crank angles is indicated. The effects of ring thickness, crown height on minimum oil film thickness, and friction force are also investigated.
机译:针对CO 2 制冷往复式压缩机的活塞环-缸套润滑问题建立了仿真模型。 Patir和Cheng的修改后的雷诺方程(包括压力流量因子,剪切流量因子和剪切应力因子)用于考虑表面粗糙度对润滑的影响。假定活塞环在前缘处被完全浸没,并且在后缘处同时考虑了气蚀情况和完全浸入情况。采用修正的雷诺边界条件。仿真结果表明,最小油膜厚度在向下行程和向上行程的中间行程区域具有最大量级。在死点附近,摩擦力的大小比中间行程区域大得多。显示了在不同的指定曲柄角下沿活塞环厚度的油膜压力分布。还研究了环厚度,胎冠高度对最小油膜厚度和摩擦力的影响。

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