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361.
362.
针对主动侧杆系统的运行需求,本文设计了一款双三相永磁同步电机,介绍了该种电机的基本结构和优点,分析了极槽配合和裂比两大关键参数的设计方法,研究了在空间限制下电机尺寸设计策略,分析了关键参数对电机性能的影响,对比了参数变化时电机转矩、转矩脉动的变化趋势,研究了电机的优化方向和参数,确定了电机的结构尺寸、绕组分布等参数。通过仿真验证了理论设计的正确性。所设计的电机输出转矩符合设计需求,转距脉动较小,不会为操纵杆手柄带来震荡的问题。电机单余度工作情况下,仍然可以达到额定转距的输出需求,保证了系统的安全性。 相似文献
363.
《中国航空学报》2023,36(2):213-228
Motor drives form an essential part of the electric compressors, pumps, braking and actuation systems in the More-Electric Aircraft (MEA). In this paper, the application of Machine Learning (ML) in motor-drive design and optimization process is investigated. The general idea of using ML is to train surrogate models for the optimization. This training process is based on sample data collected from detailed simulation or experiment of motor drives. However, the Surrogate Role (SR) of ML may vary for different applications. This paper first introduces the principles of ML and then proposes two SRs (direct mapping approach and correction approach) of the ML in a motor-drive optimization process. Two different cases are given for the method comparison and validation of ML SRs. The first case is using the sample data from experiments to train the ML surrogate models. For the second case, the joint-simulation data is utilized for a multi-objective motor-drive optimization problem. It is found that both surrogate roles of ML can provide a good mapping model for the cases and in the second case, three feasible design schemes of ML are proposed and validated for the two SRs. Regarding the time consumption in optimizaiton, the proposed ML models can give one motor-drive design point up to 0.044 s while it takes more than 1.5 mins for the used simulation-based models. 相似文献
364.
《中国航空学报》2023,36(3):285-302
To improve the heat dissipation performance, this paper proposes a novel hybrid cooling method for high-speed high-power Permanent Magnet assisted Synchronous Reluctance Starter/Generator (PMaSynR S/G) in aerospace applications. The hybrid cooling structure with oil circulation in the housing, oil spray at winding ends and rotor end surface is firstly proposed for the PMaSynR S/G. Then the accurate loss calculation of the PMaSynR S/G is proposed, which includes air gap friction loss under oil spray cooling, copper loss, stator and rotor core loss, permanent magnet eddy current loss and bearing loss. The parameter sensitivity analysis of the hybrid cooling structure is proposed, while the equivalent thermal network model of the PMaSynR S/G is established considering the uneven spraying at the winding ends. Finally, the effectiveness of the proposed hybrid cooling method is demonstrated on a 40 kW/24000 r/min PMaSynR S/G experimental platform. 相似文献