首页|期刊导航|航空科学技术|航空用功率电传作动器电机热退磁故障演化规律研究

航空用功率电传作动器电机热退磁故障演化规律研究OA

Study on the Evolution Law of the Thermal Demagnetization Fault in Motors of Aircraft Power-by-Wire Actuators

中文摘要英文摘要

随着多电飞机技术的发展,以电静液作动器和机电作动器等为代表的功率电传作动器成为新一代航空器作动系统的关键部件.然而,在复杂飞行工况下,作为功率电传作动器核心部件的永磁同步电机具有高损耗、高温升、高可靠性要求的特点,其热场特性对退磁故障演化有重要影响.本文针对航空用功率电传作动器电机进行了研究,建立了多场耦合模型,实现对电机温升的求解;分析了永磁体的热退磁行为,探讨了热退磁的演化机理;仿真结果揭示了电机在热累积与交变载荷下的退磁故障特性与热退磁规律.在电机工作过程中,同时出现可逆退磁和渐进的不可逆退磁,而当超过寿命后,可能发生突发性的永磁体失效.为提升功率电传作动器电机的可靠性、优化设计与故障预测提供了理论支持与技术依据.

With the development of more electric aircraft technology,power-by-wire actuators,represented by electro-hydrostatic actuators and electromechanical actuators,have become key components in next-generation aircraft actuation systems.However,under complex flight conditions,the permanent magnet synchronous motor(PMSM),as the core of the power-by-wire actuator,is characterized by high losses,high temperature rise,and strict reliability requirements.Its thermal characteristics significantly affect the evolution of the demagnetization fault.This study investigated PMSMs in aircraft power power-by-wire actuators and established a multi-field coupling model for temperature rise solution.Thermal demagnetization behaviors of permanent magnets were analyzed,and the evolution mechanism of thermal demagnetization was explored.Simulation results reveal the demagnetization fault characteristics and thermal demagnetization patterns under thermal accumulation and alternating loads.During the motor's operation,both reversible demagnetization and progressive irreversible demagnetization occur,with the potential for sudden permanent magnet failure after exceeding its lifespan.It provides theoretical support and technical guidance for improving the reliability,design optimization,and fault prediction of power-by-wire motors.

石存;王维煜;王少萍;刘迪

北京航空航天大学,北京 100191中国空间技术研究院北京控制工程研究所,北京 100094||北京高效能及绿色宇航推进技术工程研究中心,北京 100094北京航空航天大学,北京 100191北京航空航天大学,北京 100191

航空航天

功率电传电静液作动器机电作动器永磁同步电机电机退磁故障演化

power-by-wireelectro-hydrostatic actuatorelectromechanical actuatorpermanent magnet synchronous motormotor demagnetizationfault evolution

《航空科学技术》 2026 (2)

51-60,10

航空科学基金(2023M024051001,2022Z027051001) Aeronautical Science Foundation of China(2023M024051001,2022Z027051001)

10.19452/j.issn1007-5453.2026.02.007

评论