Magnus减摇装置及其升/阻力特性分析  

Magnus stabilizer and analysis of its lift/drag characteristics

作　　者：梁利华[1] 姜寅令 亢武臣[3] 赵朋 LIANG Lihua;JIANG Yinling;KANG Wuchen;ZHAO Peng(College of Automation, Harbin Engineering University, Harbin 150001, China;School of Electrical Engineering and Information, Northeast Petroleum University, Daqing 163318, China;SINOPEC Research Institute of Petroleum Engineering, Beijing 100101, China;Department of Transportation and Vehicle Engineering, Tangshan University, Tangshan 063000, China)

机构地区：[1]哈尔滨工程大学自动化学院,黑龙江哈尔滨150001 [2]东北石油大学电气信息工程学院,黑龙江大庆163318 [3]中国石化石油工程技术研究院,北京100101 [4]唐山学院交通与车辆工程系,河北唐山063000

出　　处：《哈尔滨工程大学学报》2021年第4期555-560,共6页Journal of Harbin Engineering University

基　　金：中央高校基本业务经费专项资金项目(HEUCFM170404);唐山学院博创基金(1402001).

摘　　要：为了研究基于Magnus效应的船用减摇装置(转子翼)的水动力特性,本文结合美国Quantum公司推出的Maglift型产品,采用ANSYS软件分析了不同航速、转速下转子翼的升/阻特性。建立了转子翼绕流的几何模型,利用ANSYS-CFX对转子翼的升/阻力及升/阻系数进行稳态仿真分析,将得到的升力进行非线性曲面拟合,得到转子翼升力与转速和航速的关系。仿真结果表明:转子翼的升/阻力受航速、转速的影响显著,均随二者的增加而增加;与传统减摇鳍对比,Magnus减摇装置具有更高的升力系数,开展对Magnus减摇装置的水动力分析具有十分重要而深远的意义。The present work explores the hydrodynamic characteristics of an anti-rolling device for ships(rotor wing)based on the Magnus effect.The lift/drag characteristics of the Maglift rotor stabilizer introduced by Quantum of the United States of America at different air and rotational speeds are analyzed using the software ANSYS.The geometric model of the flow around a rotating cylinder(rotating wing)is modeled.The lift/drag and lift/drag coefficients of the rotor wing are then simulated and analyzed on its steady state.Finally,the relationship among the lift,ship speed,and rotary speed is obtained by non-linear surface fitting.The simulation results show that both the lift and drag of the rotor wing increase with an increase in ship speed and rotary speed.Compared with the traditional fin stabilizer,the Magnus stabilizer has a higher lift coefficient.Hence,the research on hydrodynamics analysis of Magnus stabilizer is important and has far-reaching significance.

关 键 词：Magnus减摇装置 Magnus效应 船舶减摇 升/阻力特性 计算流体力学 ANSYS软件 转子翼 曲面拟合 

分 类 号：TP273[自动化与计算机技术—检测技术与自动化装置] U661.32[自动化与计算机技术—控制科学与工程]