Comparative design analysis of Permanent Magnet rotor topologies for an aircraft starter-generator
Author:
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/6868672/6874158/06874194.pdf?arnumber=6874194
Cited by 10 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. Permanent Magnet Assisted Synchronous Reluctance Machine Design for Light Traction Applications;IEEE Transactions on Industry Applications;2024-07
2. A flexible flux adjustable variable flux leakage starter‐generator for helicopters;IET Electric Power Applications;2024-06-17
3. Influence of Modification of Dual V-Shaped IPMSM Rotor Permanent Magnet Structure on Motor Performance;2023 IEEE Vehicle Power and Propulsion Conference (VPPC);2023-10-24
4. First Step to Optimum Rotor Design for E-Motors with High Power Density for Aircraft Propulsion;2022 25th International Conference on Electrical Machines and Systems (ICEMS);2022-11-29
5. Associated Fault Diagnosis of Power Supply Systems Based on Graph Matching: A Knowledge and Data Fusion Approach;Mathematics;2022-11-17
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