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翼型悬浮抛光液动压流场的数值模拟

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分析了盘式翼型悬浮抛光(ASP)的液动压分布规律,推导了工件盘和抛光盘不同心角速度反向等速条件下的液动压数学模型.对盘式翼型悬浮抛光流场进行了数值模拟,揭示了抛光盘和工件盘的运动关系以及抛光盘不同翼型曲线和迎角对流体动压力的大小和均匀性的影响规律.研究表明,当抛光盘和工件盘反向旋转时的流体动压力均匀性明显优于同向旋转,且当转速比为-1 时流体动压力分布的数值模拟效果最佳;当选用NACA 16018 翼型曲线、迎角为0°时,液动压带的面积数值效果最优.
Numerical simulation of hydrodynamic pressure field during airfoil suspension polishing process
Distribution of hydrodynamic pressure during airfoil suspension polishing(ASP)process are analyzed,by using hydrodynamic pressure mathematical models deduced when considering eccentric,constant angular velocity and reverse rotation between workpiece plate and polishing plate.Flow field of airfoil suspension polishing is nu-merically simulated,and motion relationship between disc polishing and workpiece disc,as well as effect of airfoil curves and attack angles of polish plate on magnitude and uniformity of hydrodynamic pressure,is declared.Re-sults suggest that uniformity of hydrodynamic pressure when using co-rotating mode is better than that of eccentric rotating between workpiece plate and polishing plate.Best uniformity of hydrodynamic pressure distribution is gotten when rotational speed ratio is-1.Best hydrodynamic pressure band distribution is found when using NACA 16018 airfoil curve with 0° attack angle.

airfoil suspension polishing(ASP)hydrodynamic pressureratio of speedkinematic analysis

卢凯锋、孔凡志、文东辉

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特种装备制造与先进加工技术教育部/浙江省重点实验室 杭州 310023

浙江工业大学机械工程学院 杭州 310023

翼型悬浮抛光(ASP) 液动压力 转速比 运动分析

国家自然科学基金浙江省自然科学基金重点项目

51775509LZ17E050003

2024

高技术通讯
中国科学技术信息研究所

高技术通讯

CSTPCD北大核心
影响因子:0.19
ISSN:1002-0470
年,卷(期):2024.34(1)
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