华驰动能(北京)科技有限公司,北京 101111
彭龙(1984—),男,硕士研究生,高级工程师,研究方向:主要从事飞轮储能系统整机与转子结构设计开发,E-mail:penglong1984@126.com;
苏森,高级工程师,研究方向:主要研究方向为磁悬浮轴承控制技术,飞轮储能结构设计及系统开发,E-mail:susen@huachidongneng.com。
收稿:2026-08-24,
修回:2026-10-16,
网络首发:2026-10-19,
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彭龙, 苏森, 韩坤, 等. 双转子磁悬浮飞轮储能系统动力学特性研究[J]. 储能科学与技术, XXXX, XX(XX): 1-11.
Peng Long, Su Sen, Han Kun, et al. Study on Dynamic Characteristics of Dual‑Rotor Magnetically Levitated Flywheel Energy Storage System[J]. Energy Storage Science and Technology, XXXX, XX(XX): 1-11.
彭龙, 苏森, 韩坤, 等. 双转子磁悬浮飞轮储能系统动力学特性研究[J]. 储能科学与技术, XXXX, XX(XX): 1-11. DOI: 10.19799/j.cnki.2095-4239.2026.0732.
Peng Long, Su Sen, Han Kun, et al. Study on Dynamic Characteristics of Dual‑Rotor Magnetically Levitated Flywheel Energy Storage System[J]. Energy Storage Science and Technology, XXXX, XX(XX): 1-11. DOI: 10.19799/j.cnki.2095-4239.2026.0732.
针对大功率飞轮储能系统真空工况下电机散热受限的技术难题,本文提出一种电机-飞轮转子分离布置的新型结构,该结构将飞轮转子置于真空腔内、电机转子布置于腔外常压环境,通过筒式磁联轴器实现非接触转矩传递。本文基于牛顿-欧拉方程,建立综合考虑陀螺力矩、磁轴承刚度阻尼及联轴器径向耦合刚度的双转子动力学模型。电磁场仿真结果表明,磁联轴器极限转矩为11.26 kN·m,在0~10 kN·m工作转矩区间内,等效径向刚度为-416.40~-445.58 N/mm。动力学分析显示,系统前7阶刚体模态临界转速为371.21~1988.10 r/min,一阶弯曲临界转速13707 r/min,工作转速区间内安全裕度充足;不平衡激励会使飞轮、电机两侧产生同频共振,最大振动位移分别为65.19 μm和30.23 μm。参数敏感性结果表明,磁轴承刚度决定系统低阶临界转速,阻尼可使共振振幅降幅超70%,而联轴器刚度对系统动力学性能影响微弱。本文搭建1.2 MW-125 kWh样机开展全转速振动测试实验,测试与仿真结果规律吻合,为该类双转子飞轮储能系统设计提供理论参考。
Aiming at the technical challenge of limited motor heat dissipation under vacuum conditions in high-power flywheel energy storage systems
this paper proposes a novel structure with separated motor and flywheel rotors. In this configuration
the flywheel rotor is placed inside the vacuum chamber while the motor rotor is arranged in an atmospheric environment outside the chamber
and contactless torque transmission is realized via a tubular magnetic coupling. Based on the Newton-Euler equations
a dual-rotor dynamic model is established
which comprehensively considers the gyroscopic moment
stiffness and damping of magnetic bearings
as well as the radial coupling stiffness of the magnetic coupling. Electromagnetic field simulations show that the ultimate torque of the magnetic coupling is 11.26 kN·m
and its equivalent radial stiffness ranges from -416.40 to -445.58 N/mm within the operating torque range of 0~10 kN·m. Dynamic analyses reveal that the critical speeds of the first seven rigid-body modes of the system are 371.21~1988.10 r/min
and the first bending critical speed is 13707 r/min
indicating sufficient safety margin within the operating speed range. Unbalance excitation induces synchronous resonance on both the flywheel and motor sides
with maximum vibration displacements of 65.19 μm and 30.23 μm
respectively. Parameter sensitivity results demonstrate that the magnetic bearing stiffness dominates the low-order critical speeds of the system
damping can reduce the resonance amplitude by more than 70%
whereas the coupling stiffness has a minor effect on the system dynamic performance. A 1.2 MW-125 kWh prototype is constructed and full-speed vibration tests are carried out. The experimental results agree well with the simulation trends
providing a theoretical reference for the design of such dual-rotor flywheel energy storage systems.
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