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双蜗壳离心泵的流固耦合分析 被引量:4
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作者 谈明高 吴贤芳 +2 位作者 刘厚林 王凯 董亮 《中国农村水利水电》 北大核心 2012年第12期127-130,共4页
对一比转数为109的双蜗壳离心泵进行了同时考虑叶轮和蜗壳结构场的双向流固耦合分析,分析了流固耦合作用对泵外特性和内流场分布的影响以及不同时刻泵的结构场的结构变形与等效应力的分布。研究发现,考虑流固耦合作用后数值计算得到的... 对一比转数为109的双蜗壳离心泵进行了同时考虑叶轮和蜗壳结构场的双向流固耦合分析,分析了流固耦合作用对泵外特性和内流场分布的影响以及不同时刻泵的结构场的结构变形与等效应力的分布。研究发现,考虑流固耦合作用后数值计算得到的平均扬程预测精度提高了0.7%;流固耦合作用对叶轮的内流场影响小,对蜗壳螺旋段的压力分布和扩散段的速度分布影响较大;不同时刻泵结构场的变形分布有较大差异,但等效应力分布的差异较小;当叶片正对蜗壳隔舌时,结构变形和等效应力都达到了最大值。 展开更多
关键词 双蜗壳 离心泵 流固耦合
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Impact of the thermal effect on the load-carrying capacity of a slipper pair for an aviation axial-piston pump 被引量:8
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作者 Hesheng TANG Yaobao YIN +2 位作者 Yan REN Jiawei XIANG Jun CHEN 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2018年第2期395-409,共15页
A thermal hydraulic model based on the lumped parameter method is presented to analyze the load-carrying capacity of a slipper pair in an aviation axial-piston pump under specified operating conditions. Both theoretic... A thermal hydraulic model based on the lumped parameter method is presented to analyze the load-carrying capacity of a slipper pair in an aviation axial-piston pump under specified operating conditions. Both theoretical and experimental results are presented to demonstrate the validity of the thermal hydraulic model. The results illustrate that the squeezing force and thermal wedge bearing force are the main factors that affect the film thickness and load-carrying capacity.At high oil temperature and high load pressure, the film thickness decreases with increasing clamping force due to a combined action of the squeezing bearing force and the thermal wedge bearing force, but the load-carrying capacity will increase. An increase of the film thickness is proven to be beneficial under high shaft rotational speed but especially dangerous as it strongly increases the ripple amplitude of the film thickness, which leads to decreasing the load-carrying capacity. The structural parameters of the slipper can be optimized to achieve desired performance, such as the slipper radius ratio and orifice length diameter ratio. To satisfy the requirement of the load-carrying capacity, the slipper radius ratio should be selected from 1.4 to 1.8, and the orifice length diameter ratio should be selected from 4 to 5. 展开更多
关键词 Aviation axial piston pumpfluid lubrication Load-carrying capacity Slipper pair Thermal effect
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