Influence of Stator/Rotor Torque Ratio on Torque Performance in External-Rotor Dual-Armature Flux-Switching PM Machines

Abstract

External-rotor dual-armature flux-switching PM (ER-DA-FSPM) machines have high torque density and decent fault tolerance, making them promising candidates for in-wheel machine applications in electric vehicles. The torque output and optimal design parameters of ER-DA-FSPM machines are affected by the stator/rotor torque ratio, which is the focus of this paper. Firstly, this paper analyzes airgap flux density harmonics of ER-DA-FSPM to provide a clear insight into the torque-generation mechanism. Then, this paper investigates the influence of torque ratio on average torque under the same copper loss. It is found that the average torque decreases with torque ratio increasing due to the reduction of the positive torque component generated by the sixth airgap field harmonics and the rise in the negative torque component from the eighth harmonics. Moreover, this paper also provides the optimal parameter recommendation to guide the machine design. The split ratio should increase, and the arc of PMs should decrease for a larger torque ratio, whilst the other parameters are hardly influenced. Next, this paper makes a comparison among the ER-DA-FSPM machine, external rotor flux-switching PM (ER-FSPM) machine, and surface-mounted PM (ER-SPM) machines. It shows that the ER-DA-FSPM machine, with the torque ratio being 2, can lead to a much larger total torque. In addition, in the event of rotor winding failure, which is more possible due to the existence of slip rings than stator winding failure, the stator can still provide an average torque larger than that of ER-SPM machine and 92.0% that of the ER-FSPM machine, respectively. Finally, the theoretical analysis is verified by the experiments.

1. Introduction

Electric vehicles have gained significant attention and support from governments worldwide due to their notable advantages, such as high efficiency and low emissions [1,2,3,4]. The in-wheel machine drive is one of the typical driving modes of electric vehicles. In-wheel machines provide a direct drive to the wheels. This driving mode eliminates the need for a traditional transmission system and has high efficiency and a simplified structure [5,6,7]. It also has the characteristics of rapid torque response and accurate control, enabling more effective active vehicle safety control [8,9]. Because in-wheel machine needs to be integrated into the wheel hub, it is limited by the hub’s size and cannot be expanded at will to improve output torque. Therefore, the improvement of torque density for in-wheel machines is a research hotspot [10,11,12]. In addition, since safety is the primary consideration when the vehicle is running, it is essential to ensure high reliability under various working conditions and prevent accidents caused by motor failure. As a result, enhancing the torque density and reliability of in-wheel machines with external rotors has become a prominent area of research.

The flux-switching permanent magnet (FSPM) machine is known for high magnetic density, torque density, and efficiency [13,14,15]. In applications with low speed and high torque, such as electric vehicles, the external rotor structure is particularly advantageous for direct-drive in-wheel machines [10,16,17]. Due to the requirements of higher torque and power to meet the vehicle’s acceleration performance, climbing ability, and high-speed cruise, many methods were proposed to improve torque density. Various FSPM machines have been proposed with different core structures like C-Core, E-Core, and Multi-Teeth design [18,19,20] to improve the torque output. However, these designs have lower space utilization than the traditional U-Core structure, which limits the further improvement of torque density. Using V-shaped magnets [11,21] is another way to improve the torque output. However, this structure has large cogging torque and back electromotive force harmonics [21]. In [22], the design of wedge-shaped stator teeth and magnets was proposed to expand the stator slot area, which greatly increases the torque density. In addition, the external rotor FSPM (ER-FSPM) machine with this design can exhibit negligible torque ripples. However, all of these designs cannot essentially solve the competition of the magnets and slot area.

Improving fault tolerance of the FSPM machine is also a research hotspot. The traditional three-phase winding configuration cannot satisfy the high-reliability requirements. In [23,24], the modular FSPM machine can also increase fault tolerance, but the amount of permanent magnets is half that of the traditional FSPM machine, which limits the torque output. Increasing the number of winding phases can also improve fault tolerance. When the machine fails in one or more phases, it continues to operate through the remaining healthy phases. In addition, machines with more phases have lower mutual inductance. Consequently, the healthy phases are less influenced by the faulty phases, which means such machines have better fault tolerance [25]. However, windings with different phases compete for confined space in the stator slots. Therefore, improving the fault-tolerant capability limits the increase in torque density.

To improve torque density and fault tolerance simultaneously, some research has proposed a double-stator FSPM machine. Because each stator has a set of windings, this machine possesses good fault-tolerant capability and torque density [26,27]. However, this structure is relatively complex, which brings challenges to the production, and the double airgap structure has a larger equivalent airgap length, which limits the increase of torque [28]. To keep the single airgap structure and double-winding configuration, the dual-armature flux-switching permanent magnet (DA-FSPM) machine was proposed, which adds another set of windings on the rotor in the internal-rotor FSPM [29,30]. With two sets of windings, stator and rotor slot areas are specially designed to generate the same average electromagnetic torque, which enables the machine to maintain a certain torque output when one set of windings fails. Moreover, the addition of rotor windings optimizes the use of the machine’s internal space, increasing the electrical loading and thereby significantly enhancing torque density.

The dual-armature structure can also be applied to ER-FSPM machines to improve the torque density and fault-tolerant capability of in-wheel machines, which is rarely found in the previous literature. In conventional ER-FSPM machines, since the armature winding and the PMs are both located on the stator and compete with each other in space, they may cause significant magnetic saturation [17]. Magnetic saturation can impact the performance of the machine, such as the decrease of output torque and the increase of torque ripple and machine temperature [31,32,33]. The double-winding structure also reduces magnetic saturation under the same copper loss. Moreover, with part of the windings moved to the external core, the heat dissipation performance of the FSPM machine can be improved [34]. In addition, PM overheating and irreversible demagnetization can also be suppressed [33].

However, in order to meet the requirements of different operating conditions of electric vehicles, such as frequent acceleration and deceleration, the rotor of the in-wheel machine needs to have small inertia [35], which limits the weight of the rotor’s windings and core. Moreover, slip rings in the rotor can make the failure probability of the rotor winding greater than that of the stator winding. The torque generated by the stator windings should be improved to guarantee relatively large output torque under most fault-tolerant operating conditions. Therefore, the assumption of rotor winding providing the same average torque as the stator winding cannot be applicable to in-wheel ER-FSPM machines for EVs [30]. Research concerning how the ratio of the stator torque to rotor torque influences the machine’s performance is needed. It can guide the design of external-rotor dual-armature flux-switching magnet (ER-DA-FSPM) machines, particularly those requiring high reliabilities.

In this paper, the influence of torque ratio on the electromagnetic performance in ER-DA-FSPM machines is investigated. Firstly, the MMF-permeance model is established for airgap field modulation. Next, this paper investigates the influence of torque ratio on total average torque through the analysis of dominating field harmonics generating torque. The characteristics of optimized dimensional parameters with torque ratio are analyzed subsequently. Then, the comparison is made between ER-FSPM, ER-DA-FSPM, and ER-SPM machines about torque density and fault-tolerant capability. Finally, an experimental validation is conducted.

2. Harmonic Analysis of Airgap Fields

Before the influence of stator/rotor torque ratio on the torque performance of the ER-DA-FSPM machine is investigated, the torque-generation mechanism is analyzed from the point of airgap flux density by the MMF-permeance model.

2.1. Topology of ER-DA-FSPM Machine

Figure 1 shows the topology of the investigated ER-DA-FSPM machine. Figure 2 shows the diagram of key design parameters, and

Table 1. Parameters of ER-DA-FSPM machine.

Parameter	Value
Rotor external radius Rro	45 mm
Rotor inner radius Rri	35.4 mm
Stator external radius Rso	34.9 mm
Stator inner radius Rsi	17 mm
Axis length	45 mm
Magnet arc τm	6.1°
Side stator tooth arc τst	5.6°
Rotor tooth arc τrt	14.7°
Stator yoke thickness hsy	1.9 mm
Rotor yoke thickness hry	3.8 mm
Air gap length	0.5 mm
Stator pole/rotor tooth number	12/10
Stator/rotor phase number	3/5
Rated copper loss	24 W
Number of stator winding turns per phase	72
Number of rotor winding turns per phase	68
Slot fill factor	0.4
Magnet remanence	1.2 T
Magnet relative permeability	1.05
Lamination material	M19_24G
Rated speed	400 rpm

provides the parameter values. Compared with the ER-FSPM machine, the ER-DA-FSPM machine has a much higher torque density due to the utilization of the rotor slot area. In addition, the ER-DA-FSPM machine has the potential for fault-tolerant operation as it has two sets of armature windings. For the investigated ER-DA-FSPM machine, both the stator and rotor use a double-layer winding design for higher torque density [36]. Although single-layer winding configuration can better limit the short-circuit current than double-layer winding to further improve the fault tolerance [37], its resulting torque ripple is higher [38,39]. In addition, it is noteworthy that the investigated machine chooses five phases for the rotor windings to achieve the largest winding factor with a relatively low inverter cost. Additionally, it has been found that a rectangle is not the optimal magnet shape for the ER-FSPM machines [22]. The stator slot area is compressed by PMs near the stator yoke, thus constraining the space for stator armature. Therefore, the ER-DA-FSPM machine in this paper adopts wedge-shaped PMs to further improve torque density.

2.2. Harmonic Analysis of Airgap Flux Density

When the machine has two sets of winding, the airgap magnetic fields are generated by three sources, i.e., PMs, stator windings, and rotor windings, making the fields complicated [40,41]. It has been proven that the MMF-permeance model is effective and concise for qualitative research [42,43] of airgap fields. Although the airgap flux density from PM or stator armature reaction for ER-DA-FSPM is similar to that of the ER-FSPM machine, the rotor-armature reaction has not been analyzed, which is the main focus of this section. In this paper, the MMF-permeance model is developed neglecting the end effect. In addition, the saturation of steel lamination is also not considered. The flux lines are perpendicular to the steel-lamination surface, which keeps the tangential component of the airgap fields at zero [42].

Figure 3 shows the airgap permeance model accounting for stator saliency. When the leakage flux is neglected, the airgap permeance accounting for stator saliency mainly changes with the permeability along the stator surface shape [44,45,46]. In addition, the permeability of air, copper windings, and permanent magnets are close to vacuum permeability, whilst the permeability of the core is assumed to be infinite. Therefore, the airgap permeance is a rectangular wave with an offset. In Figure 3, P₁₀ and P₁ are the DC component and peak–to-peak value of the permeance model. p_s, θ_1, and θ₂ are the PM pole-pair number, the half-arc of PM, and the half-arc of PM plus stator tooth, respectively.

The Fourier series expansion of this model can be expressed as (1), in which M_1n and S₁ are the Fourier coefficients [41,42].

$$\left\{\begin{array}{c}{P}_s{(\theta )=P}_{10}{+S}_1{\displaystyle \sum _{n=1}^{\infty }} \left[M_{1n}\cos \left({2\mathit{np}}_s\theta \right)\right]\\ S_1={\displaystyle \frac{{4P}_1}{\pi }}\\ M_{1n}={\displaystyle \frac{\left[\sin \left({2\mathit{np}}_s{\theta }_2\right)-\sin \left({2\mathit{np}}_s{\theta }_1\right)\right]}{n}}\end{array}\right.$$

(1)

The rotor phase currents can be described as

$$\left\{\begin{array}{c}{i}_a=\sqrt{2}{I}_r\sin \left(p_s{\mathsf{\Omega }}_{r}t\right)\\ \begin{array}{c}\begin{array}{c}{i}_b=\sqrt{2}{I}_r\sin \left(p_s{\mathsf{\Omega }}_{r}t-{\displaystyle \frac{2\pi }{5}}\right)\\ i_c=\sqrt{2}{I}_r\sin \left(p_s{\mathsf{\Omega }}_{r}t-{\displaystyle \frac{4\pi }{5}}\right)\\ i_d=\sqrt{2}{I}_r\sin \left(p_s{\mathsf{\Omega }}_{r}t-{\displaystyle \frac{6\pi }{5}}\right)\\ i_e=\sqrt{2}{I}_r\sin \left(p_s{\mathsf{\Omega }}_{r}t-{\displaystyle \frac{8\pi }{5}}\right)\end{array}\end{array}\end{array}\right.$$

(2)

where I_r is the RMS phase current of rotor windings and Ω_r is the mechanical rotor speed. The airgap MMF of the rotor-armature reaction in the ER-DA-FSPM machine accounting for the rotor saliency is presented in Figure 4. N_r is the number of turns per rotor coil, θ₀ is the initial rotor pole position, and θ₃ is the arc of the rotor tooth. For the rotor phase a, the Fourier series expansion of MMF can be expressed as

$$F_{\mathrm{ra}}={\displaystyle \frac{2t_r}{\pi }}\sum _{m=1}^{\infty } M_{\mathit{rm}}{i}_a\cos \left[2m\left(\theta -{\theta }_0-{\mathsf{\Omega }}_{r}t\right)\right]$$

(3)

where t_r is the rotor tooth number, and

$$M_{\mathit{rm}}={\displaystyle \frac{\sin (m{\theta }_3)}{m}}$$

(4)

According to (2), MMF of rotor phase a can be rewritten as

$$F_{\mathrm{ra}}={\displaystyle \frac{t_r}{\pi }}\sum _{m=1}^{\infty } M_{\mathit{rm}}\left\{sin[2m\theta -2m{\theta }_0+\left(p_s-2m\right){\mathsf{\Omega }}_{r}t]+sin[-2m\theta +2m{\theta }_0+\left(p_s+2m\right){\mathsf{\Omega }}_{r}t]\right\}$$

(5)

It can be found that the MMF of the rotor phase a contains two components with different frequencies. MMF for other rotor windings can be obtained accordingly. Therefore, the total MMF by all rotor windings can be expressed as

$$F_r=F_{\mathrm{ra}}+F_{\mathrm{rb}}+F_{\mathrm{rc}}+F_{\mathrm{rd}}+F_{\mathrm{re}}$$

(6)

When m = 5l, m = 5l − 1, and m = 5l − 4, the MMF components with each frequency from different rotor phases are cancelled out due to the current phase difference of the five rotor phases. When m = 5l − 2, the MMF components with frequency (p_s − 2m)Ω_rt are offset, whilst the components with frequency (p_s + 2m)Ω_rt are in the same phase. Therefore, the total MMF can be obtained as

$$F_r(\theta ,t)={\displaystyle \frac{5S_r}{2}}\sum _{m=5l-2}^{\infty } \left[M_{\mathit{rm}}\sin \left(-2m\theta +2m{\theta }_0+\left(p_s+2m\right){\mathsf{\Omega }}_{r}t\right)\right]$$

(7)

where

$$S_r={\displaystyle \frac{2\sqrt{2}{t}_r{I}_r}{\pi }}$$

(8)

Similarly, when m = 5l − 3, the components with frequency (p_s + 2m)Ω_rt, are offset whilst the components with frequency (p_s − 2m)Ω_rt are in the same phase. Therefore, the total MMF can be expressed as

$$F_r(\theta ,t)={\displaystyle \frac{5S_r}{2}}\sum _{m=5l-2}^{\infty } \left[M_{\mathit{rm}}\sin \left(2m\theta -2m{\theta }_0+\left(p_s-2m\right){\mathsf{\Omega }}_{r}t\right)\right]$$

(9)

Hence, the airgap MMF of rotor armature reaction can be summarized as

$$\left\{\begin{array}{c}{F}_r(\theta ,t)={\displaystyle \frac{5S_r}{2}}{\displaystyle \sum _{m=1}^{\infty }} \left[M_{\mathit{rm}}\sin \left(\xi \right)\right]\\ \xi =\left\{\begin{array}{c}2m\theta -2m{\theta }_0+\left(p_s-2m\right){\mathsf{\Omega }}_{r}t,m=5l-3\\ -2m\theta +2m{\theta }_0+\left(p_s+2m\right){\mathsf{\Omega }}_{r}t,m=5l-2\\ 0,m=else\end{array}\right.\\ \end{array}\right.$$

(10)

Combining the permeance model, when m = 5l − 3, the rotor-armature reaction airgap flux-density distribution B_r can be calculated as

$$\left\{\begin{array}{c}{B}_r\left(\theta ,t\right)=F_r\left(\theta ,t\right)P_s\left(\theta \right)\\ ={\displaystyle \frac{5P_{10}{S}_r}{2}}{\displaystyle \sum _{m=1}^{\infty }}\left\{M_{\mathit{rm}}\cos [2m({\theta }_0-\theta )\right.\left.\left.\begin{array}{c}-\left(p_s-2m\right){\mathsf{\Omega }}_{r}t+{\displaystyle \frac{\pi }{2}}\end{array}\right]\right\}\\ +{\displaystyle \frac{5S_1{S}_r}{2}}{\displaystyle \sum _{m=1}^{\infty }} {\displaystyle \sum _{n=1}^{\infty }}\left[M_{\mathit{rm}}{M}_{1n}\left(\cos {\gamma }_1-\cos {\gamma }_2\right)\right]\\ {\gamma }_1=2\left(n{p}_s-m\right)\left[\theta -{\displaystyle \frac{\left(p_s-2m\right){\mathsf{\Omega }}_{r}t-2m{\theta }_0-\frac{\pi }{2}}{2\left(n{p}_s-m\right)}}\right]\\ {\gamma }_2=2\left(n{p}_s+m\right)\left[\theta -{\displaystyle \frac{-\left(p_s-2m\right){\mathsf{\Omega }}_{r}t+2m{\theta }_0+\frac{\pi }{2}}{2(n{p}_s+m)}}\right]\end{array}\right.$$

(11)

when m = 5l − 2, B_r can also be expressed by (11) with a negative sign applied to m.

Based on the above analysis, the characteristics of spatial harmonics from the rotor armature reaction are listed in

Table 2. Characteristics of rotor-armature flux-density components.

	No.	Pole-Pairs	Rotating Speeding, Ωr
m = 5l − 3	1	2m = 10l − 6 = ltr − ps	(2m − ps)/2m
	2	2|nps − m| = |2nps − 10l + 6| = |(2n + 1)ps − ltr|	(2m − ps)/(2m − 2nps)
	3	2(nps + m) = 2nps + 10l − 6 = [2(n − 1) + 1]ps + ltr	(2m − ps)/(2m + 2nps)
m = 5l − 2	1	2m = 10l − 4=(l − 1)tr + ps	(2m + ps)/2m
	2	2(nps + m) = 2nps + 10l − 4=(2n + 1)ps + (l − 1)tr	(2m + ps)/(2m + 2nps)
	3	2|nps − m| = |2nps − 10l + 4| = |[2(n − 1) + 1]ps − (l − 1)tr|	(2m + ps)/(2m − 2nps)

. The open-circuit and stator armature airgap flux density can be obtained from [42], which are shown in

Table 3. Characteristics of open-circuit flux-density components.

No.	Pole-Pairs	Rotating Speeding, Ωr
1	2(i − 1)ps	0(static)
2	ktr + 2(i − 1)ps	ktr/[ktr + 2(i − 1)ps]
3	|ktr − 2(i − 1)ps|	ktr/[ktr − 2(i − 1)ps]

and

Table 4. Characteristics of stator-armature flux-density components.

	No.	Pole-Pairs	Rotating Speeding, Ωr
q = 3r − 2	1	4q = 12r − 8=tr + [2(r − 1) − 1]ps	tr/4q
	2	|ktr −4q| = |ktr − 12r + 8| = |(k − 1)tr − [2(r − 1) − 1]ps|	(k − 1)tr/(ktr − 4q)
	3	ktr + 4q = ktr + 12r – 8 = (k + 1)tr + [2(r − 1) − 1]ps	(k + 1)tr/(ktr + 4q)
q = 3r − 1	1	4q = 12r − 4= − [tr − [2(r + 1) − 1]ps]	−tr/4q
	2	ktr + 4q = ktr + 12r – 4 = (k − 1)tr + [2(r + 1) − 1]ps	(k − 1)tr/(ktr + 4q)
	3	|ktr − 4q| = |ktr − 12r + 4| = |(k + 1)tr − [2(r + 1) − 1]ps|	(k + 1)tr/(ktr − 4q)

, respectively, where i and k are nonnegative integers, and q and r are positive integers. It can be found that the pole-pair numbers of stator- and rotor-armature reaction airgap magnetic fields are consistent with those |(2i − 1)p_s ± kt_r| of open-circuit airgap magnetic fields.

2.3. FE Validation

In this part, the above analysis is validated by an FE simulation on the investigated ER-DA-FSPM machine shown in Figure 1. The stator and rotor RMS phase currents are 6.43 A and 2.02 A, respectively. Under such conditions, the ratio of stator torque to rotor torque, i.e., T_s/T_r, is 2. The FE-predicted radial airgap flux harmonics of the ER-DA-FSPM machine are presented in Figure 5. It can be found that parts of the dominating rotor-armature reaction airgap field harmonics have pole-pair numbers 4 and 6 [2m, when (l = 1, n = 2, 3)] without the modulation of stator saliency. The other dominating harmonics have pole-pair numbers 28 and 30 [2(np_s + m) when (n = 1, m = 8 and n = 2, m = 3)] due to the modulation of the salient stator to the rotor armature reaction MMF, which matches well with the results by the MMF-permeance model.

3. Influence of Stator/Rotor Torque Ratio

This section investigates the influence of the stator/rotor torque ratio on the torque performance of the ER-DA-FSPM machine, before which the ER-DA-FSPM machine is optimized aimed for maximum average torque under different T_s/T_r.

3.1. Parameter Optimization

In order to make a fair comparison, the key dimensional parameters of the investigated ER-DA-FSPM machine are first optimized. Since this paper focuses on the optimization of dimensional parameters for ER-DA-FSPM machines, the core and PM materials are selected as commonly used ones and kept unchanged, which is shown in Table 1. As for the dimensional parameters, the outer and inner diameters, and the axis length, they are usually constrained by the application space of ER-DA-FSPM machines. In addition, the airgap length is limited by the manufacturing and assembly process. Therefore, these parameters are also fixed in the optimization. Hence, the most influential parameters and their initial values are selected in

Table 5. Initial value of key dimensional parameters of ER-DA-FSPM machine.

Order	Parameter	Value
1	Split ratio, Rg/Rro	0.78
2	Magnet-arc-to-stator-pole-pitch ratio, τm/τspp	0.2
3	Side stator tooth arc-to-pole pitch ratio, τst/τspp	0.17
4	Stator-yoke-thickness-to-tooth-arc ratio, hsy/τst	0.6
5	Rotor-tooth-arc-to-tooth-pitch ratio, τrt/τrtp	0.4
6	Rotor-yoke-thickness-to-tooth-arc ratio, hry/τrt	0.4

, which can determine machine-dimensional characteristics, as well as electromagnetic performance. In addition, during optimization, the total copper loss of stator and rotor windings is fixed at 24 W, considering the temperature limit of winding insulation.

The optimization of the ER-DA-FSPM machine is conducted using a sequential approach, as shown in Figure 6. Firstly, the optimization should identify one fixed value for T_s/T_r. Then, the investigated parameters are optimized one after another. When one optimal parameter is found, it is used as the basis for the optimization of the next parameter. It should be noted that when dimensional parameters vary, the areas of stator and rotor slots also change. Therefore, stator- and rotor-armature currents should be adjusted to keep the fixed copper loss [47]. In addition, according to [30], the parameter-optimization order has little effect on the sequential optimization result. In this article, the order goes in Table 5. After the nth cycle of optimization, the average torque T_n is compared with T_n−1 of the last cycle. If (T_n − T_n−1)/T_n ≤ 1%, the optimization ends and T_n is regarded as the maximum average torque for the current T_s/T_r. The maximum average torque for other T_s/T_r can be obtained by repeating the above steps.

The first cycle of optimization of the six different key dimensional parameters when the T_s/T_r equals 2 is shown in Figure 7, where T is the total torque. For each parameter, the value range around the optimal value is shown for clear visibility. It can be found that, when each parameter increases, a maximum average torque can be achieved due to the mutual constraints between armature and PMs [30]. The maximum average torque increases from 4.80 Nm to 5.15 Nm. For the next cycle, the increase of maximum average torque does not exceed 1%. Thus, 5.15 Nm is the maximum average torque under T_s/T_r = 2. The optimization process under the other T_s/T_r is similar and, thus, neglected. In addition, the sensitivity of average torque to these key parameters can also be observed from Figure 7, which is defined as

$$S={\displaystyle \frac{T_{max}{-T}_{min}}{T_{max}}}\times 100\%$$

(12)

where T_max is the peak average torque when each key parameter is optimized, and T_min is the minimum average torque when each key parameter deviates from the optimal value from −0.05 to 0.05. The sensitivities of average torque to the following six key parameters are 8.97%, 7.34%, 8.06%, 0.08%, 1.77%, and 4.32%, respectively. It can be found that R_g/R_ro has the greatest influence on the average torque, whilst h_sy/τ_st almost has no effect.

3.2. Influence of Stator/Rotor Torque Ratio on Maximum Average Torque

After optimization, the average torque and current under different values of T_s/T_r are shown in Figure 8. It can be found that when T_s/T_r increases, the total average torque decreases with a decline rate. This is because the stator winding of ER-DA-FSPM works as a traditional ER-FSPM machine, whilst the rotor winding works as a spoke-type interior PM (IPM) machine. The former usually leads to smaller torque density. To achieve increasing T_s/T_r, more copper loss should be allocated to the stator windings, i.e., the ER-FSPM machine, which thus makes the total average torque decrease.

The paper also explains this phenomenon from the point of airgap field harmonics. The instantaneous electromagnetic torque T(t) excited by radial and tangential field harmonics can be described as

$$T\left(t\right)=\sum _{n=1}^{\infty } {\displaystyle \frac{\pi R^{2}L}{{\mu }_0}}{B}_{\mathit{rn}}{B}_{\mathit{tn}}\cos \left[{\theta }_{\mathit{rn}}\left(t\right)-{\theta }_{\mathit{tn}}\left(t\right)\right]$$

(13)

where L is the active length, R is the airgap radius, and B_rn and B_tn are the nth harmonic magnitudes of the airgap flux-density radial and tangential components, respectively, and θ_rn and θ_tn are the corresponding phases separately. By (5), the torque contribution from each dominant airgap flux density harmonic can be analyzed. The radial and tangential components of airgap flux density are obtained by the FE method at a specific time when the transient torque equals the average torque. Figure 9 shows the torque component contributed by each field harmonic when T_s/T_r = 0.5, 1, 2, and 4. It can be found that the 6th (p_s), 16th (p_s + t_r), and 18th (3p_s) are the dominating airgap field harmonics contributing to the electromagnetic torque when T_s/T_r = 0.5 and 1. When T_s/T_r = 2 and 4, the 4th (−p_s + t_r), 8th (3p_s − t_r), and 28th (3p_s + t_r) also lead to non-negligible torque components. The reason why the total average torque decreases with the increase of T_s/T_r is the decreasing magnitude of the positive sixth component and the increasing magnitude of the negative eighth component. Moreover, the decline rate of the torque reduction can be attributed to the increasing magnitudes of the positive 4th, 18th, and 28th components.

3.3. Influence of Stator/Rotor Torque Ratio on Parameter Design

The variation of optimized key dimensional parameter values with T_s/T_r is shown in Figure 10. It can be found that τ_st/τ_spp, h_sy/τ_st, τ_rt/τ_rtp, and h_ry/τ_rt almost do not change under different T_s/T_r. However, the optimized value of R_g/R_ro increases, whilst the value of τ_m/τ_spp decreases separately with the increasing T_s/T_r. The larger split ratio is preferred because the increasing space for the stator winding and PMs is needed. The selection of τ_m/τ_spp is also influenced by the split ratio. For larger T_s/T_r, the rising split ratio increases the PM width, which is perpendicular to the magnetization direction, as shown in Figure 11. It improves the open-circuit flux density yet has a low rate. Under such conditions, reducing τ_m/τ_spp to increase the electric load is more effective in improving the torque density.

4. Advantage of ER-DA-FSPM Machine

To effectively illustrate the superior torque density and fault-tolerant capability of the ER-DA-FSPM machine, a comparative analysis is conducted with the ER-FSPM and external-rotor surface-mounted PM (ER-SPM) machines, which are shown in Figure 12.

4.1. Comparison of Average Torque for Different Machines

In order to make a fair comparison, the three types of machines are designed with the fixed parameter values shown in

Table 6. Main design parameters of three machines.

Parameter	ER-DA-FSPM	ER-FSPM	ER-SPM
Rotor external radius	45 mm
Stator inner radius	17 mm	17 mm	15 mm
Axis length	45 mm
Air gap length	0.5 mm
Pole/tooth number	12/10	12/10	10/12
Stator/rotor phase number	3/5	3/0	3/0
Rated copper loss	24 W
Number of stator winding turns per phase	72
Number of rotor winding turns per phase	68
Slot fill factor	0.4
Magnet remanence	1.2 T
Magnet relative permeability	1.05
Lamination material	M19_24G
Rated speed	400 rpm

. Sequential optimization is also applied to maximize the average torque for ER-FSPM and ER-SPM machines. The averages of the three machines are shown in Figure 13. It can be found that when T_s/T_r ranges from 0.5 to 5, the least average torque of ER-DA-FSPM can still reach 4.91Nm. The average torques for ER-SPM and ER-FSPM machines are 3.55 Nm and 4.32 Nm, respectively. Therefore, the ER-DA-FSPM machine shows noticeably better torque capability than the ER-SPM and ER-FSPM machines.

4.2. Comparison of Fault-Tolerant Capability for Different Machines

To guarantee machine reliability, the winding temperature is usually carefully checked within the insulation limit, even continuously operating at full load for a much longer time. Compared to the DA-ER-FSPM machine itself, the fault is more likely to happen in the power electronic devices of the converters. Therefore, in this paper, fault-tolerant capability refers to the output torque capability under the same copper loss when a fault occurs in the stator or rotor converter, and the corresponding winding set is completely unsupplied. In addition, the operation of the remaining winding set does not require complicated fault-tolerant control strategies. The average torque when only the stator or rotor winding operates is shown in Figure 13, which is also obtained under total copper loss 24 W. Considering that the failure possibility of the rotor winding is higher due to the existence of the slip ring, the stator torque should be specially focused. It can be found that, when T_s/T_r is 2, the stator winding can output a torque of 76.5% for the whole ER-DA-FSPM machine, which still exceeds that of the ER-SPM machine, and reaches about 92.0% for the ER-FSPM machine. When T_s/T_r becomes larger, the increasing rate of stator torque decreases due to magnetic saturation. In contrast, in the event of a stator-winding failure, both the ER-FSPM machine and the ER-SPM machine are unable to produce torque. Moreover, when T_s/T_r is 2, if the stator winding of the ER-DA-FSPM machine fails, the rotor winding can still generate an average torque of 74.5% for the whole ER-DA-FSPM machine. It is also larger than that of the ER-SPM machine, reaching 89.7% of the ER-FSPM machine under normal operation. Compared to the condition of T_s/T_r = 3, although the stator’s average torque is slightly smaller under fault-tolerant operations, the rotor’s average torque under fault-tolerant operation leads to more torque, and the total torque under normal operation is also larger. Therefore, T_s/T_r = 2 is recommended for the in-wheel machines to achieve decent torque and fault-tolerant capability.

5. Experimental Validation

5.1. Prototype Machine and Experimental Setup

In this section, experimental validation is performed to verify the FE analysis on a 3-stator-phase/5-rotor-phase and a 12-stator-slot/10-rotor-slot internal-rotor DA-FSPM machine. The prototype DA-FSPM machine is shown in Figure 14, and the parameters are listed in

Table 7. Parameters of prototype machine.

Parameter	Value
Stator outer radius	50 mm
Stator inner radius	35.25 mm
Active axial length	50 mm
Stator tooth arc to pole pitch ratio	0.28
Magnet arc to stator pole pitch ratio	0.24
Stator yoke thickness to tooth arc ratio	0.6
Airgap length	0.5 mm
Rotor inner radius	10 mm
Rotor tooth arc to tooth pitch ratio	0.37
Rotor tooth tip arc to tooth pitch ratio	0.055
Rotor yoke thickness to tooth body arc ratio	0.7
Rotor tooth tip height	0.8 mm
Number of stator winding turns per phase	160
Number of rotor winding turns per phase	144
Stator phase resistance	1.55 Ω
Rotor phase resistance	2 Ω

. Since the internal-rotor DA-FSPM machine has a similar working principle to ER-DA-FSPM machines, the experiments on the prototype machine can still validate the accuracy of FE simulation and theoretical analysis. The rotor windings are connected to the slip ring via the groove on the shaft. The experimental setup is shown in Figure 15. The prototype DA-FSPM machine is driven by a DSP controller, and the load is provided by the dynamometer.

5.2. Torque Experiments and Discussion

Since the DA-FSPM machine operates in the motor mode, the total torque is set as 4 Nm. The current, torque, and speed waveforms under different T_s/T_r are shown in Figure 16. It can be found that sinusoidal currents are input into the stator and rotor windings. Although there is a slight ripple in the torque waveforms, the average total torque is 4 Nm. The torque components generated by the stator and rotor windings change with the torque ratio. The rotor speed is 100 rpm with negligible ripples.

The stator and rotor current amplitude and the total copper loss are summarized in Figure 17. The total copper loss is calculated as

$$P_{\mathit{cu}}=Z_s{I_s}^2{R}_s+Z_r{I_r}^2{R}_r$$

(14)

where Z_s and Z_r, I_s and I_r, and R_s and R_r are the phase number, RMS phase current, and phase resistance of stator and rotor winding, respectively.

When the total torque remains fixed at 4 Nm, and when T_s/T_r increases, the stator-current amplitude increases, whereas the rotor-current amplitude decreases. In addition, the copper loss first decreases and then increases. When T_s/T_r < 1, the rotor’s winding generates a larger average torque. However, the rotor winding has a larger phase resistance and more phases. Thus, the copper loss decreases with the increasing T_s/T_r. When T_s/T_r > 1, the stator windings generate more torque components. However, since stator winding shows weaker torque capability than rotor winding, the increased rate of the stator current is larger than the decreasing rate of the rotor current. Therefore, the total copper increases with T_s/T_r. When the same currents are input in the FE simulation, the stator and rotor torque with T_s/T_r are shown in Figure 18. It can be found the measured torque is slightly smaller than the FE-predicted results due to the end effect. In addition, the variation trends are close to each other. Therefore, the effectiveness of FE simulation is confirmed, thereby validating the preceding theoretical analysis.

5.3. Speed Experiments and Discussion

The current, torque, and speed waveforms under different rotor speeds when T_s/T_r = 2 are shown in Figure 19. Compared to the condition of the rotor speed being 100 rpm, which is shown in Figure 16d, it can be found that torque capability remains unchanged when rotor speed increases at the same total copper loss. Therefore, it can be concluded that the above theoretical results are still applicable when the machine operates at different rotor speeds.

5.4. Fault-Tolerant Experiments and Discussion

The current, torque, and speed waveforms when only stator or rotor winding works are shown in Figure 20. When the total torque remains fixed, the copper losses for only stator- and rotor-fault-tolerant operation are 50.4 W and 58.1 W, respectively, which are much larger than those under normal conditions. In addition, when the current values are input into the FE simulation, the predicted average torques are 4.11 Nm and 4.08 Nm, which are close to the experimental results. Therefore, the accuracy of the FE simulation is again validated.

6. Conclusions

The paper focuses on the influence of stator/rotor torque ratio on torque performance on ER-DA-FSPM machines. Firstly, the MMF-permeance model of the machine is established to analyze the dominant airgap field harmonics. Then, in order to investigate the influence of stator/rotor torque ratio, sequential optimization is used to obtain maximum average torques under different stator/rotor torque ratios. It is found that the optimized average torque decreases with increasing torque ratio. This trend is attributed to the reduction in the positive torque component generated by the sixth airgap field harmonics and the rise in the negative torque component produced by the eighth field harmonics. Additionally, the optimized dimensional values of split ratio and PM arcs should increase and decrease when the stator/rotor torque ratio increases, respectively. Furthermore, the paper conducts a comparison of ER-FSPM, ER-DA-FSPM, and ER-SPM machines. When the stator/rotor torque ratio is 2, the torque output of the ER-DA-FSPM machine can be 20.4% and 45.4% greater than the ER-SPM and ER-FSPM machines. Moreover, under rotor-armature failure, the stator winding can output torque 76.5% of that of the whole ER-DA-FSPM machine, which still exceeds that of the ER-SPM machine and reaches about 92.0% of that of the ER-FSPM machine. When the stator winding of the ER-DA-FSPM machine fails, the rotor winding can still generate an average torque of 74.5% of that of the whole ER-DA-FSPM machine, which is also larger than that of the ER-SPM machine and reaches 89.7% of that of the ER-FSPM machine under normal operation. These results strongly support that the ER-DA-FSPM machine has excellent torque density and fault-tolerant capability for in-wheel machine applications, where the stator winding is designed to produce larger torque output. Finally, the theoretical analysis is validated by experiments of torque, speed, and fault-tolerant capability.