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Hydrodynamic Lubrication Performance Analysis of the Self-Cooled Bearing Structure in Aero-Gear Pump Considering the Cavitation Effect

机译:考虑空化效应的空气齿轮泵中自冷轴承结构的流体动力润滑性能分析

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In this paper, a load coupling numerical method is developed to analyze the performance of the journal bearing considering the internal flow simulation inside aero-engine gear pump. First, three-dimensional flow analysis is conducted. Then based on the JFO theory, an improved hybrid scheme including switch function is used to solve Reynolds equation while the external load given by the simulation result of the gear pump. The robust, convergence and validation of algorithm is tested compared with the experiment result where the pressure maximum error less than 2%. Finally, parametric study on different groove structure and working conditions of an aero-gear pump bearing has been presented to assess the performance features of the bearing hydrodynamic lubrication problem. The result shows that the effect of external load on bearing was dependent on eccentricity. In addition, the pressure distribution in bearing was markedly affected by the oil groove structure where relative pressure difference at 5% and inlet pressure is proportional to maximum pressure.
机译:在本文中,开发了一种负载耦合数值方法,以分析期刊轴承的性能考虑到航空发动机齿轮泵内部的内部流模拟。首先,进行三维流动分析。然后基于JFO理论,一种改进的混合方案,包括开关功能,用于解决雷诺等式,而齿轮泵的仿真结果给出的外部负载。与实验结果相比,测试了算法的稳健,收敛和验证,其中压力最大误差小于2 %。最后,已经提出了对不同凹槽结构的参数研究和航空齿轮泵轴承的工作条件,以评估轴承流体动力润滑问题的性能特征。结果表明,外部负荷对轴承的影响取决于偏心率。另外,轴承的压力分布显着受油槽结构的影响,其中5℃的相对压力和入口压力与最大压力成比例。

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