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Rotor Strength Optimization of Surface Mount High Speed Permanent Magnet Motor Based on FEM/Kriging Approximate Model and Evolutionary Algorithm |
Li Wei, Wang Zerun, Zhang Fengge |
School of Electrical Engineering Shenyang University of Technology Shenyang 110870 China |
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Abstract Due to the advantages of small size, high power density, high efficiency, can be directly connected with high-speed load, eliminating the traditional mechanical growth device, reduce system noise and other advantages, high-speed permanent magnet motor has been widely used in high-speed load and distributed power generation system, and has broad development prospects. Due to the high requirements on the rotor strength of high-speed permanent magnet motors, it is an urgent problem to find a method to efficiently optimize the rotor strength. However, for the finite element model (FEM) of the complex structure, it often takes dozens or even hundreds of iterative calculations to obtain the optimal solution, which greatly affects the development process of the motor. This paper took the 1.12 MW, 18 000 r/min surface-mounted high-speed permanent magnet motor rotor as the optimization object, and established its structural parameter model and stress field finite element simulation model. The operating temperature, sheath thickness, permanent magnet thickness and interference were set as the optimization parameters, and the optimal design is carried out with the maximum value of normal and tangential stress of permanent magnet and sheath as small as possible, so as to achieve the purpose of improving the rotor strength of high-speed permanent magnet motor. Combined with the currently commonly used optimization methods, two typical technical routes were specifically designed: the technical route 1 adopted the evolutionary algorithm (EA) combined with FEM to optimize and design. The maximum radial and tangential stresses of permanent magnet and sheath under different structural parameters and temperature parameters were taken as the optimization target quantity in the EA, and a various of parameter combinations were taken out and FEM was called for optimization iterative calculation. Technical route 2 selected the optimization parameters through the Latin hypercube sampling method, and used the FEM to find the corresponding the maximum value of the permanent magnet stress and the jacket stress was used as the output parameter to form the sample space. The sample space was fitted to obtain the Kriging approximation model that was used to replace the traditional FEM solver. Based on the approximate model, the subsequent optimization design process combined with the EA was carried out. Through the analysis and comparison of the two optimization methods, the following conclusions were drawn: technical route 1 can obtain the optimal solutions of sheath thickness, permanent magnet thickness, temperature and interference that reduce the maximum radial and tangential stress of the permanent magnet and the maximum radial stress of the sheath. It shows that the optimization method based on FEM combined with EA has a certain optimization effect, but there are also problems of few optimization attempts and long optimization time. Compared with technical route 1, technical route 2 is not limited by the number of samples, the calculation time is shorter, and the calculation efficiency is higher. When there are too many optimization parameters, there may be a fitting precision low lead to optimal design issue such as difference of accuracy, but based on the distribution of sample points in the sample space can intuitively reflect the optimization of the relationship between parameters and the optimization goal, applicable to the initial optimization phase. In addition, the optimal parameters of the calculation results of the optimal design and the optimal target quantities obtained by the two optimization methods are close, indicating that the EA can more accurately obtain the structural parameters that improve the strength of the rotor. The optimization problem in actual engineering should combine two optimization technical routes. In the preliminary optimization stage, the technical route 2 is used to accurately optimize the parameter interval, and then the technical route 1 is used to expand the optimization to obtain the optimal design.
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Received: 30 May 2022
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