Research Article  Open Access
Zhixian Zhong, Yijian Duan, Zhonghou Cai, Yanying Qi, "Design and Cosimulation of TwelvePole Heteropolar Radial Hybrid Magnetic Bearing", Mathematical Problems in Engineering, vol. 2021, Article ID 8826780, 14 pages, 2021. https://doi.org/10.1155/2021/8826780
Design and Cosimulation of TwelvePole Heteropolar Radial Hybrid Magnetic Bearing
Abstract
This paper presents a twelvepole heteropolar radial hybrid magnetic bearing (HRHMB) structure. Firstly, the structure and equivalent magnetic circuit (EMC) are designed. And the radial electromagnetic force characteristics are calculated by the EMC model. At the same time, the rationality of EMC model is verified by the finiteelement method (FEM) of Magnet software. Then, the 2D model of the twelvepole HRHMB is established in Magnet software. The flux density variations of twelvepole HRHMB and eightpole HRHMB under different currents are compared by using the FEM. Finally, a method of MagnetSimulink cosimulation is proposed to analyze the suspension characteristics of the twelvepole HRHMB and compared with the eightpole HRHMB. Thus, the effective combination of theoretical analysis, FEM analysis, and MagnetSimulink cosimulation analysis is realized in the design of HRHMB. The results of MagnetSimulink cosimulation show that the twelvepole HRHMB has the advantages of low power consumption, small coupling, large construction dynamic stiffness, and better suspension characteristics than the eightpole HRHMB.
1. Introduction
Hybrid magnetic bearing (HMB) combines the characteristics of the active magnetic bearing and the passive magnetic bearing. In the HMB, the permanent magnet is used instead of the electromagnetic coil to generate the required bias flux, while the electromagnetic coil is only responsible for generating the control flux. Therefore, the power loss and volume of the magnetic bearing are greatly reduced [1–5]. Based on the above characteristics, HMB has irreplaceable advantages in the field of small size and low power consumption. Hence, HMB has broad application prospects in many industrial occasions such as flywheel energy storage system (FESS) [6], artificial heart [7], highspeed blower [8], molecular vacuum pump [9], and so on [10].
In domestic and foreign research, the HMB can be roughly divided into two categories, namely, homopolar hybrid magnetic bearing and heteropolar hybrid magnetic bearing [11,12]. Among them, the heteropolar radial hybrid magnetic bearing has the advantages of relatively short axial length, less magnetic flux leakage, and lower power consumption than the homopolar radial hybrid magnetic bearing. Therefore, it also has been widely concerned by many scholars [13, 14] proposing a structure of HRHMB. In this structure, the four control magnetic poles of the stator and the four permanent magnetic poles inlaid with permanent magnets are arranged alternately to form the NSNS magnetic pole arrangement sequence. In [15], the parameter design method of the structure is derived, and the prototype of HRHMB is manufactured by using this method [14]. The simulation and experimental results of the prototype show that the HRHMB structure designed by the parameter design method has excellent suspension performance. In order to reduce power consumption and improve the space utilization of the entire system, a novel eightpole heteropolar radialaxial hybrid magnetic bearing is present in [16]. The parameters of the structure are optimized, and the structure prototype is made. The results of experiment and simulation show that the maximum bearing capacity of HMB in the radial and axial directions is 82.6% and 81% of the theoretical value, respectively. Zhu et al. [17] proposed a novel of HRHMB with low power loss for the FESS, and its structural optimization design was carried out based on the equivalent magnetic circuit model. Then after the 3D FEM, the simulation results show that the maximum control current in the electromagnetic coil can be reduced to 40% of the original structure by optimizing the design. In [18], a 3DOF electromagnetic bearing with annular radial control coil is proposed. This structure reduces the copper loss of the electromagnetic bearing structure by using annular coil, and the weak cross coupling effect of 3DOF electromagnetic bearing is proved by 3D FEM. Sun et al. [19] proposed a new decoupling control scheme for a 4DOF PMBAMB in a directdriven spindle system based on the neural network inverse and 2degreeoffreedom internal model control method. And the experimental results demonstrate the effectiveness of the proposed control scheme. In [20], a threedegreeoffreedom hybrid magnetic bearing is optimized as an example. First, a comprehensive sensitivity analysis is carried out to show the relationship between the parameters and optimization objectives in detail. Second, a crossfactor variance analysis is considered due to the possibility of parameter interaction. And then, a hierarchical multiobjective optimization structure is used with the Kriging model and the nondominated Sorting Genetic Algorithm 2. Finally, the simulation results verify the validity of the proposed method.
Most of the structures of HRHMB are based on the eightpole HRHMB in [14, 21]. In this structure, the block permanent magnet is embedded into the stator yoke. Therefore, the bias flux provided by the permanent magnet is uniformly distributed on the stator surface, which realizes the radial 2DOF suspension of the rotor core. However, when the air gap flux of the right two magnetic poles in the horizontal direction increases, the air gap flux of the left two magnetic poles in the vertical direction also increases. Hence, there is a left bearing capacity in the structure, and it weakens the right bearing capacity. This will increase the power consumption of the magnetic bearing and reduce the suspension performance of the electromagnetic bearing. In order to solve this problem, this paper proposes a structure of twelvepole HRHMB. By increasing the number of 8 control magnetic poles to 12, the coupling between the bias flux and the control magnetic field is reduced, and the suspension performance of the electromagnetic bearing is enhanced.
At present, many scholars generally carry out theoretical research on HRHMB, and an experimental platform is built to monitor the changes in parameters such as rotor displacement and coil current of HRHMB. But the experiment of using the above method is difficult, and the cost is high. Besides, data observation is not flexible enough, and it is difficult to truly observe the influence of the HRHMB structural parameters optimization on the actual control [22–27]. In order to solve this problem, this paper proposes a method of MagnetSimulink cosimulation. First, the HRHMB model is imported into Simulink. Then, through the realtime data exchange between Magnet and MATLAB software, the current, voltage, electromagnetic force, speed, displacement, and other parameters in HRHMB can be monitored in real time. Through this method, theoretical analysis, FEM analysis, and control simulation analysis can be effectively combined into the structural optimization design. Taking the control strategy of the system into consideration can make the structural optimization design of HRHMB more accurate and practical. At the same time, the cost of the experiment is reduced, and the efficiency of the HRHMB structure design is improved. Thus, the suspension characteristics and power consumption of the HRHMB system can be analyzed more intuitively [28].
2. Structure and Model
The structure of the twelvepole HRHMB is shown in Figure 1. The twelvepole HRHMB is composed of radial stator, radial control winding, rotor, and permanent magnet. In order to reduce hysteresis and eddy current loss, the radial stator core and rotor core are made of silicon steel sheets. In the stator, the twelve control magnetic poles with the same number of turns are arranged symmetrically, which forms an alternating arrangement of NS poles. Among them and (n = 1, 2, 3) are the upper and lower magnetic poles in the vertical direction of the stator. and (n = 1, 2, 3) are, respectively, the left and right control magnetic poles in the horizontal. In addition, the four block permanent magnets are uniformly embedded in the stator yoke, which provide a bias flux for the structure.
The flux density distribution of the twelvepole HRHMB is shown in Figure 2. The bias flux generated by the permanent magnet passes through the permanent magnet pole, the air gap, the rotor, the control magnetic pole, and the stator yoke, which forms a closed loop. The control flux generated by the control winding passes through the stator yoke, the control magnetic pole, the air gap, and the rotor, which forms a closed loop. Due to the high magnetoresistance of permanent magnets, the control flux cannot pass through permanent magnetic poles. Therefore, the demagnetization of permanent magnets is avoided.
When the rotor is stably suspended in the equilibrium position, the bias flux flows between two adjacent magnetic poles. Therefore, four equal bias fluxes are formed on the surface of the rotor, and the resultant force received by the rotor is zero. If the rotor is subjected to a vertical downward impact force, it will move downward from the central position. As a result, the air gap between the lower magnetic pole and the rotor in the stator is reduced, and the bias flux density increases in the air gap. At this time, due to the unbalance of the bias flux, the direction of the resultant force is downward, and the position of the rotor drops. In order to restore the rotor to the equilibrium state, a certain amount of current must be applied to the magnetic pole on the upper side of the stator. At this point, the control flux generated by the control magnetic pole flows from the middle N pole of the upper pole to the S pole on both sides. And then the control flux flows back to the N pole from the S pole to form a closed loop so that the rotor is subjected to a vertical upward suction. Under the current regulation of the controller, the rotor is finally suspended in the equilibrium position.
3. Analysis of EMC
In Figure 3(a), is the magnetomotive force provided by the permanent magnet. is the coercivity of the permanent magnet. is the radial thickness of the permanent magnet. Thus, it can be approximated as
(a)
(b)
The magnetoresistance of a permanent magnet can be calculated bywhere is the permanent magnet reluctance, is the permeability of permanent magnetic materials, and is the area of the stator pole.
The bias flux in the branches produced by the permanent magnet is defined as (k = 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12). Therefore, the bias flux of each branch can be calculated by
In Figure 3(b), (k = 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12) is the magnetomotive force generated by the control coil. , , , and are the control flux of each branch in the control magnetic circuit. The control magnetic flux of each branch of the magnetic field can be calculated by
Then the total magnetic flux of the magnetic field in each air gap can be expressed aswhere , , , and are the magnetic flux passing through the air gap along the corresponding direction. In addition, the positive direction of the coordinate axis is defined as the positive direction of the force, and the positive direction of the current is defined as the direction that generates the positive force. According to Maxwell’s equation, and can be calculated bywhere is the resultant force of electromagnetic force in the horizontal direction and is the resultant force of electromagnetic force in the vertical direction. The crosssectional area of the air gap corresponding to a single magnetic pole is .
In order to verify the accuracy of EMC, it was compared with the FEM results. The main parameters of the twelvepole HRHMB are listed in Table 1. Then, the comparison of the FEM and the radial force characteristics predicted by the EMC model is shown in Figures 4(a)–4(d). And the other magnetic pole currents are all 2A, when the current in the corresponding magnetic pole changes.

(a)
(b)
(c)
(d)
It can be seen from Figures 4(a)–4(d) that the radial electromagnetic force of the twelvepole HRHMB is linearly related to the control current. And it is also proved that the ratio coefficient of current to electromagnetic force calculated by the EMC method is close to the FEM. When the control current is 5A, the maximum horizontal radial electromagnetic force is 87.8 N, and the maximum vertical radial electromagnetic force is 36 times of the rotor core weight. Therefore, it is sufficient to complete the control of the twelvepole HRHMB.
4. Comparison of Coupling Characteristics
In order to analyze the coupling of the twelvepole HRHMB, first, the twelvepole HRHMB model is established. Then the change of the flux density on the rotor surface is analyzed on the Magnet software under different currents. Finally, the simulation results of twelvepole HRHMB and eightpole HRHMB are compared.
The eightpole HRHMB structure in literature [13] is shown in Figure 5, which is the common structure of HMB. The eightpole HRHMB is formed by inserting a permanent magnet into the yoke of an eightpole active magnetic bearing. Among them and (k = 1, 2) are the upper and lower magnetic poles in the vertical direction of the stator. and are, respectively, the left and right control magnetic poles in the horizontal. Then, the radial suspension of the rotor core is realized by superimposing the control flux and the bias flux. But it can be seen from Figure 6 that when the air gap flux of the d_{1} and d_{2} poles increases, the air gap flux of the a_{2} and c_{1} poles also increases. Therefore, the unbalanced force is generated, and horizontal ability is weakened. At the same time, the excitation power of magnetic bearing is increased, and the suspension performance of magnetic bearing is reduced.
It can be seen from Figure 77(a) that when the current of and (k = 1, 2) changes from 2 A to 5 A, the total difference of flux density in the air gap below and (k = 1, 2) is 0.1845 T and = 0.08 T, which is about 4.44 times and 1.92 times of and in Figure 7(b).
(a)
(b)
(c)
(d)
As shown in Figures 7(c) and 7(d), the current of the magnetic pole controlling the horizontal movement of the rotor between the twelvepole HRHMB and the eightpole HRHMB changes from 2A to 5 A. = = 0.0415 T in Figure 7(d), which is 0.5 and 0.2 times of and in Figure 7(c), respectively.
In summary, the coupling of the twelvepole HRHMB is smaller than that of the eightpole HRHMB, and the current and flux density increment have a better linearity.
5. Cosimulation
As shown in Figure 8, the twelvepole HRHMB model is established in the Magnet software and imported into Simulink. Then the PID control block diagram of the HRHMB system is established [29]. The current source of HRHMB corresponds to the input and output ports of the MagnetSimulink plugin. Besides, the output ports of the MagnetSimulink plugin add rotor displacement, coil electromagnetic force, rotor speed, and other parameters. The vertical and horizontal loads are 2.4 N (the gravity of the rotor model) and 0 N (the external force on the horizontal direction of the rotor is 0). After parameter tuning, the vertical PID controller parameters of the twelvepole HRHMB are K_{P} = 150800, K_{I} = 0.001, and K_{D} = 200, and the horizontal PID controller parameters of the twelvepole HRHMB are K_{P} = 125000, K_{I} = 0.001, and K_{D} = 100. At the same time, the vertical PID controller parameters of the eightpole HRHMB are K_{P} = 205000, K_{I} = 0.001, and K_{D} = 12, and the horizontal PID controller parameters of the eightpole HRHMB are K_{P} = 60000, K_{I} = 0.001, and K_{D} = 850.
(a)
(b)
5.1. Comparison of Suspension Simulation
The radial displacement response of the twelvepole HRHMB system and the eightpole HRHMB system is shown in Figures 9(a)–9(d). The oscillation time of the twelvepole HRHMB system in both vertical and horizontal directions is between 0 and 0.015 s. In the oscillation stage, the maximum overshoot of the rotor in two directions is about and , respectively. However, when the current is applied to the coil, the unbalanced force weakens the horizontal main bearing capacity and seriously affects the suspension characteristics. Therefore, the fluctuation time of the rotor in the horizontal and vertical directions is between 0–0.1 s and 0–0.2 s, respectively. During the oscillation stage, the maximum overshoot in the horizontal and vertical directions of the rotor is about 16.04 and 33.3 times of the twelvepole HRHMB system, respectively. According to the simulation results, the twelvepole HRHMB system has better dynamic performance and suspension characteristics than the eightpole HRHMB system. The flux density distribution of the stable suspension twelvepole HRHMB system and the stable suspension eightpole HRHMB system are shown in Figures 10(a)and 10(b). Because the total number of turns of the two HRHMB winding coils is the same, there is an unbalanced force in the eightpole HRHMB. So the twelvepole HRHMB flux density is higher than the eightpole HRHMB flux density. At the same time, twelvepole HRHMB is less prone to magnetic saturation than eightpole HRHMB.
(a)
(b)
(c)
(d)
(a)
(b)
5.2. Comparison of Equilibrium Current
The current waveforms of the twelvepole HRHMB system and the eightpole HRHMB system are shown in Figures 11(a)–11(d). In the vertical direction, the maximum current of the twelvepole HRHMB system in the floating state is A. The equilibrium current is A, which is about 1/25 of the eightpole HRHMB system. Meanwhile, the maximum current in the horizontal direction of the twelvepole HRHMB is A, and the balance current is only 1/70 of the eightpole HRHMB system. According to the simulation results, the twelvepole HRHMB structure has lower power consumption than the eightpole HRHMB structure.
(a)
(b)
(c)
(d)
6. Comparison of Structure Dynamic Stiffness in the Cosimulation of HRHMB System
In MagnetSimulink cosimulation, the rotor is stabilized in the equilibrium position under the current regulation of the PID controller. Then external impact force F_{K} is applied to the rotor in the balanced state. The maximum distance the rotor deviates from the equilibrium position is also called the maximum overshoot . In the stage of external force action, the ratio of external interference force to the maximum overshoot is used as the construction dynamic stiffness K of the HRHMB [30,31]. Therefore, the construction dynamic stiffness K can be calculated by
6.1. Comparison of Suspension Characteristics
The results are shown in Figures 12(a) and 12(b). At 0.3 s, a vertical impact force of 5N–25 N is applied to the rotor suspended in the equilibrium position. The maximum overshoot of the twelvepole HRHMB system is m, which is reduced by m compared with the maximum overshoot of the eightpole HRHMB system. In addition, the twelvepole HRHMB system returns to the equilibrium position and remained in stable suspension at 0.22 s after the impact. Besides the adjustment time was only 14.28% of the eightpole HRHMB system.
(a)
(b)
(c)
(d)
The horizontal impact simulation is shown in Figures 12(c) and 12(d). The maximum overshoot and adjustment time of the twelvepole HRHMB system were 52.07% and 4% of the eightpole HRHMB system, respectively. Therefore, the above simulation results show that the suspension characteristics of the twelvepole HRHMB structure are better than that of the eightpole HRHMB system.
6.2. Comparison of Structures Dynamic Stiffness
The comparison of construction dynamic stiffness between the twelvepole HRHMB system and the eightpole HRHMB system is shown in Figures 13(a) and 13(b). Under the same impact force, the construction dynamic stiffness of the twelvepole HRHMB is better than the eightpole HRHMB in both horizontal and vertical directions. Due to the unbalanced force of the eightpole HRHMB, the horizontal bearing capacity is weakened, which seriously affects the dynamic stiffness of the structure in the horizontal direction. The construction dynamic stiffness of the eightpole HRHMB is only 56.5% of the twelvepole HRHMB structure. The simulation results show that the twelvepole HRHMB has better suspension characteristics than the eightpole HRHMB.
(a)
(b)
7. Conclusions
This paper proposes a twelvepole HRHMB structure. By using the EMC method, the FEM and the MagnetSimulink cosimulation method, the maximum bearing capacity, coupling, suspension characteristics, power consumption, and construction dynamic stiffness of the twelvepole HRHMB are analyzed. And some positive conclusions are drawn as follows:(1)The results of EMC method shows that the maximum radial load capacity of the twelvepole HRHMB is 87.8 N under the coil current of 5 A. And the maximum radial bearing capacity is about 36 times the weight of the rotor core. Therefore, it is sufficient to support the stable suspension of the rotor.(2)The results of FEM and MagnetSimulink cosimulation show that the twelvepole HRHMB has the advantages of low power consumption, small coupling, large construction dynamic stiffness, and better suspension characteristics than the eightpole HRHMB.
Data Availability
All data are included in the paper.
Conflicts of Interest
The authors declare that they have no conflicts of interest.
Acknowledgments
This work was sponsored by the National Natural Science Foundation of China (51565009) and the Natural Science Foundation of Guangxi Province (2015GXNSFAA139272).
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Copyright © 2021 Zhixian Zhong et al. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.