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空间坐标系中的三维电动机 被引量:17
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作者 万山明 黄声华 +1 位作者 傅光洁 马志云 《中国电机工程学报》 EI CSCD 北大核心 1998年第5期305-309,共5页
提出了空间三维正交坐标系中的广义有功和无功功率的概念,并应用这一方法分析了三维电动机建立在三维空间中的电磁矢量模型及其矢量控制方法。给出了三维电动机伺服系统一种整体仿真的方法。给出了仿真及实验结果。
关键词 三维电动机 矢量控制 电动机 空间坐标系
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正交圆柱结构三维电动机磁系统分析 被引量:1
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作者 崔淑梅 柴风 程树康 《微特电机》 北大核心 1999年第6期26-28,共3页
对正交圆柱结构三维电动机的磁系统进行了分析,分析表明,正交圆柱结构三维电动机,存在磁耦合。求取了最大静转矩计算公式,对样机进行计算和实验结果表明,解析表达式是正确的。
关键词 三维伺服电动机 磁系统 正交圆椎结构 系统分析
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三维电动机位置辩识研究
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作者 蔡炜 黄声华 《船电技术》 2000年第1期22-29,共8页
通过推导出的三维电动机的状态方程表达式,建立了三维电动机中应用扩展卡尔曼滤波的位置辨识算法,利用仿真研究的结果证实了该方案的可行性。
关键词 三维电动机 扩展卡尔曼滤波 位置辩识
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Study on three dimensional electromagnetic model for permanent magnet linear synchronous motor 被引量:2
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作者 汪旭东 王兆安 袁世鹰 《Journal of Coal Science & Engineering(China)》 2002年第1期87-90,共4页
In this paper, with the non-salient pole permanent magnet linear synchronous motor (PMLSM)being cited, by using Fourier transform method and "slot-by-slot", "pole -by-pole" current approach, a 3D e... In this paper, with the non-salient pole permanent magnet linear synchronous motor (PMLSM)being cited, by using Fourier transform method and "slot-by-slot", "pole -by-pole" current approach, a 3D electromagnetic field model of PMLSM is established. Special attention is paid to its structure and the influence of longitudinal and transverse end effect. The distribution of electromagnetic field of PMLSM can be obtained directly and promptly by using FFT algorithm. It can also be used for the analysis of other LSM. 展开更多
关键词 permanent magnet linear synchronous motor quasi-3D electromagnetic field model Fourier transform
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Study on Blade Surface Flow around Wind Turbine by Using LDV Measurements 被引量:4
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作者 Tinnapob Phengpom Yasunari Kamada +3 位作者 Takao Maeda Junsuke Murata Shogo Nishimura Tasuku Matsuno 《Journal of Thermal Science》 SCIE EI CAS CSCD 2015年第2期131-139,共9页
This paper has attempted to study a mechanism of three-dimensional flow around a horizontal axis wind turbine(HAWT) rotor blade. An experimental study of the flow phenomenon in the vicinity of the wind turbine blade i... This paper has attempted to study a mechanism of three-dimensional flow around a horizontal axis wind turbine(HAWT) rotor blade. An experimental study of the flow phenomenon in the vicinity of the wind turbine blade is a challenging endeavor. In this research, the HAWT model with 2.4 m diameter was tested in the large wind tunnel. The flow around the rotating blade surface was measured simultaneously for three velocity components, and two probes were used for the synchronized measurement of three-dimensional flow components. The local velocity was detected for the single seeding particle measured in the point where three pairs of laser beams intersected. Blade sections of interest in this study are composed of radial positions r/R = 0.3, 0.5 and 0.7. Optimum and low tip speed ratio flow characteristics were also compared. The velocity flow vector, skin friction coefficient and bound circulation were calculated from LDV measurements, and the experimental research showed reasonably and clearly the experimental results. 展开更多
关键词 LDV measurement Sectional performance Wind turbine Boundary layer flow Span-wise flow
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Co-simulation and Experimental Study for Wingspan of Flapping Wing Micro Aerial Vehicle 被引量:1
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作者 彭松林 陈文元 张卫平 《Journal of Shanghai Jiaotong university(Science)》 EI 2009年第2期252-256,共5页
The 3D model of flapping wing mechanism and veins is constructed in 3D computer aided design (CAD) software UG.Then the co-simulation model is established by using multibody dynamics software ADAMS and MATLAB.The vali... The 3D model of flapping wing mechanism and veins is constructed in 3D computer aided design (CAD) software UG.Then the co-simulation model is established by using multibody dynamics software ADAMS and MATLAB.The validation of this co-simulation model is verified by comparing the simulation results with final experiments.The simulation results and experiments reveal that the relation between flapping frequency and driving voltage of motor is approximately linear under various wingspans.The variance of flapping frequency among different wingspans augments gradually with increasing voltage.Furthermore,the simulation results suggest that flapping frequency is sensitive to wingspan and decreases with increasing wingspan of veins,and the relation between flapping frequency and moment of inertia of veins is also approximately linear for various voltages. 展开更多
关键词 WINGSPAN micro aerial vehicle (MAV) flapping wing mechanism CO-SIMULATION multibody dynamics software
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