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基于有限元法的极化磁系统等效磁路模型的研究
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摘要
航天电磁继电器是国防电子系统中主要的电子元器件之一。极化磁系统以其灵敏度高、功耗低、体积小、动作快和电寿命长等一系列优点,被广泛应用于航天电磁继电器产品中。含永磁磁系统吸力特性分析是进行继电器磁系统参数化设计的基础,对于永磁的恰当处理和计算是准确分析吸力特性的前提。
     由于永磁内部磁通分布不均匀,极化磁系统中各段永磁工作在不同的回复线上,为了对各段永磁进行等效,首先需要求出各段永磁的起始工作点。根据永磁的不同装配方式,分别对永磁“开路”情况和完全装配情况进行三维磁场仿真分析,计算永磁各截面的磁通,获得永磁各段中心截面的平均磁感应强度,将其作为各段永磁的起始工作点对应的磁感应强度值。研制永磁截面磁通测量装置,对三维磁场仿真分析结果进行验证。
     为了提高等效磁路模型的精度,需要得到计算精度较高的永磁漏磁导。利用有限元软件获得条形永磁开路及装配情况下磁场分布情况,“开路”情况下永磁在空气中的漏磁通管为新月形截面,并将计算出的漏磁导与磁场仿真结果及实验计算结果进行比较;完全装配情况下永磁漏磁通包括经过空气闭合及经过轭铁闭合两种情况,经过空气闭合的漏磁通管为新月形截面,经过轭铁闭合的漏磁通管可分为柱形截面、部分圆环形截面、不同心圆环形截面三种,将计算出的漏磁导与磁场仿真结果进行比较;给出永磁漏磁通经不同介质闭合的分界面确定方法。
     利用三维有限元方法获得不同装配情况下永磁的磁场分布情况,并按照磁场分布对永磁进行合理分段,利用磁场仿真结果计算出各段永磁的工作回复线,给出各段永磁等效磁势与等效磁阻的计算方法。在此基础上建立永磁分段后的等效磁路模型。利用该模型建立方法为现有产品及实验模型建立等效磁路模型,计算出吸力特性,并与实验结果、有限元方法及未分段等效磁路方法计算结果进行比较。
Electromagnetic relay in aerospace is one of main electronic components in national defense weapon equipment system. Polarized magnetic system is widely used in electromagnetic relay in aerospace as it has a series of features, such as high-sensitivity, low power consumption, small volume, quick movement, long electrical life and so on. The analysis of electromagnetic attractive force characteristic of magnetic system with permanent magnet is a foundation for the parameter design in relay’s magnetic system, whether the permanent magnet is treated and calculated appropriately or not is the precondition to analyze the electromagnetic attractive force characteristic accurately.
     The different parts of PM don’t work on the same recoil line because of the uneven PM’s internal magnetic field distribution. Initial work points of each section of PM are calculated to conduct equivalent magnetic models. According to different ways of permanent magnet assembly, analyses of 3d magnetic field simulation are used to simulate PM in air and PM in whole magnetic system. Magnetic flux density distribution of PM’s sections is obtained by post processing simulation result and can be used to obtain the characteristic of the magnetic flux density distribution curve. The value of B corresponding to initial work point for each part is assigned the average magnetic flux density of this part. Internal magnet flux measurement device is developed to verify 3d magnetic field simulation results.
     Calculation accuracy of equivalent magnetic circuit method could be effectively improved with exact calculation of PM leakage permeance. Magnetic field distributions of PM in air and PM in whole magnetic system can be obtained by FEM software. Cross-sections of leakage magnetic flux tubes of PM in air are close to crescent, leakage permeance calculated are compared with results calculated by simulation and measuring results; paths of leakage magnetic flux of PM in whole magnetic system are closed through the air or through the yoke. Cross-sections of leakage magnetic flux through the yoke can be divided into cylindrical section, partial circular annular cross-section and non-circular cross-section, leakage permeance calculated are compared with results calculated by simulation. Method of determining interface of PM leakage flux is provided.
     Magnetic field distributions of PM in air and PM in whole magnetic system can be obtained by FEM software, and PM is divided into parts based on magnetic field distributions. Recoil lines of each section are calculated with simulation results. Calculation methods of equivalent magnetic potential and equivalent reluctance of PM subsection are provided. Equivalent magnetic circuit is established to calculate attractive force characteristics of existing product and experimental model, which are compared with simulation results, measuring results and traditional magnetic circuit model results.
引文
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