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Analytical Modeling of the Magnetic Field in Axial Field Flux-Switching
Permanent Magnet Machines at No-Load
Mouheb Dhifli*, Habiba Bali**, Yanis Laoubi*, Georges Barakat*, Yacine Amara*
*GROUPE DE RECHERCHE EN ELECTROTECHNIQUE ET AUTOMATIQUE DU
HAVRE. 75, rue bellot 76058
Le Havre, France
Tel.: +33 / (0) – 2.32.85.99.53
E-Mail: [email protected]
** UNIVERSITE DE JIJEL, FACULTE DES SCIENCES ET DE LA TECHNOLOGIE,
DEPARTEMENT DE GENIE ELECTRIQUE. ALGERIE
BP 98, Ouled Aissa 18000
Jijel Algeria
Keywords
« axial field flux-switching machines », « permanent magnets », « analytical solution », « axial flux-
switching », « finite element analysis », « electromagnetic analysis ».
Abstract
In this paper an analytical model for prediction of the no-load magnetic field in axial field flux
switching permanent magnet machines (FSPM) is presented. The proposed method is based on an
exact 2D analytical solution of Maxwell‟s equations in low permeability regions (stator/rotor slots,
air gap, permanent magnets (PMs) and surrounding air regions), using the separation of variables
technique. For each region, the magnetic vector potential solution is expressed as a sum of Fourier
series. Combining obtained solutions in each region and boundary conditions leads to a set of linear
equations which allows calculation of the coefficients of the Fourier series in the different regions. The
developed model is validated by comparing magnetic field components for a machine modeled with
this analytical model and the finite element method (FEM).
I. Introduction
In the automotive industry , demand for electromechanical machines which have a high torque density
and a high and variable speed capability is increasing [3]. The flux switching permanent magnet
(FSPM) machine is a good candidate since it combines the advantages of a switched reluctance
machine (high speed and robust rotor structure) and a brushless permanent magnet machine as shown
in Fig. 1 (high torque density) [1][2].
Fig. 1 The advantages of the SRM (a) and the PMSM (b) are embodied in a FSPM (c).
In the literature, this machine is often modeled by FEM or with the magnetic equivalent circuit (MEC)
model due to the nonlinear behavior and the doubly salient topology [1][3][4][5]. A hybrid model
which combines the MEC and the Fourier analysis exist too [3][4][6].
In fact MEC model allows the prediction of the electromagnetic performance of a AFSPM machine
but it suffers from coarse discretization of the resulting field solution, whereas the FEM has the
disadvantage of a long computational time [3].
In this paper, analytical modeling of AFSPM machine is presented as a solution to solve the
disadvantages of the MEC model and to reduce computation time compared to FEM. This technique
is based on an exact 2D solution of Maxwell equations using the separation variables method and
Fourier analysis. The 2D configuration is set by unrolling the curved surface obtained by using a
cylindrical cutting plane at the main flux region of the studied machine [7]-[9]. The topology of the
machine is given together with a brief definition of the working principle in section II.
The magnetic field distribution is calculated accurately in the different regions of the AFSPM machine
(stator/rotor, slots, air gap, PMs and the surrounding air regions) with a reasonable computation time.
Results issued from the proposed model, for both local and global quantities, are compared and
validated with those stemming from a 2D FEM. Furthermore, this model could be an effective tool to
explore a set of solutions in the early stages of the AFSPM machine design procedure.
II. AFSPM MACHINE
A. Topology
The geometry of the studied AFSPM machine 12/10-pole is presented in Fig. 2, which is a double-
sided structure [1][10]. The stator includes armature coils and twelve permanent inductor magnets, the
rotor is completely passive which allows to operate at very high speed. This three-phase machine
comprises four magnets and four concentrated coils per phase, while the rotor contains ten teeth
(Nr = 10). For a better understanding of the FSPM, it is mandatory to understand the underlying
physical phenomena inside the machine.
Fig. 2: Topology of the 12/10 AFSPM machine Fig. 3: Working principle of the AFSPM machine
B. Flux switching principle
The stator part of the FSPM machine consists of 12 modular U-shaped laminated segments between
which are placed permanent magnets (PMs). The magnetization is reversed in polarity from one
magnet to the next [10][11]. The principle of flux-switching has been shown in Fig.3. According to the
position of the mobile part, the magnetic flux-linkage in the armature winding switches direction and
can be counted as either positive or negative, and is then alternative. The working principle is similar
to the conventional radial field FSPM [3][4][12][13].
III. COMPUTATION OF THE EXACT 2D ANALYTICAL MAGNETIC
FIELD DISTRIBUTION
A. Assumptions
Stator 1
Stator 2
Windings
PMs
Stator and rotor
configuration
Stator 1
Direction of movement
Stator 2
Rotor tooth
Knowing the 3D nature of axial flux machine, the first geometrical assumption is to reduce the 3D
problem to a 2D one. The 2D analytical model is less time consuming and allows to take into account
the 3D intrinsic nature of the magnetic field in the axial flux machine by the multi-slice technique. The
main assumption of the analytical model is that the permeability of the soft-magnetic material is
considered infinite. The permeability of PMs is assumed to be equal to that of air and their resistivity
is infinite. Also, eddy current effects are neglected [7][8]. This goal is achieved by the use of a
cylindrical cutting plane at the mean radius and then the derived plane is unrolled to obtain the surface.
According to the AFSPM topology, half of the machine needs to be modeled [3][12].
In this approach the magnetic vector potential has only a radial component which depends on the axial
and circumferential coordinates. Therefore, in cylindrical coordinates the magnetic quantities can be
considered as follows:
rezAA , (1) zz ezBezBB ,, (2)
The second part is to model the machine in a Cartesian plane (x, y) as shown in Fig. 4, without unduly
compromising accuracy [6]. The studied machine is symmetrical over a period noted per and have a
period length given by (4), where moyR is the average radius:
sper Np,gcd2 (3) permoyper RL (4)
Fig. 4: FSPM machine model in Cartesian coordinates.
The magnetic quantities are then expressed as follows:
and (5)
B. Exact 2D analytical magnetic field solution
The FSPM machine model in Cartesian coordinates has different field regions (rotor slots (I), air gap
(II), PMs (III), stator slots (IV) and surrounding air (V)). The governing field equations, in terms of
the Coulomb Gauge, , is given by:
(6)
Therefore, equation (6) is reduced to a scalar formulation and can be written in the following form:
x
B
y
B
y
A
x
A yRxR
2
2
2
2
(7)
The vector potential solution for every region can be written by using the separation of variables
technique [9][14] as:
xx e
y
AB
yy e
x
AB
0 A
IIIregioninBA
VandIVIIIregionsinA
R2
2 ,,0
wes wa
wer hdr
hes
ha
e
(0,0) x
y
I
II
III
IV
V
0,3,3
,3,3,3
0,3
0,3
sinhsincos
coshsincos1,
kl
kl
k
lk
lklll
kykxFkxD
kykxEkxC
kyDayxA (8)
0
0 sincossinhcosh1
,
n
ni
nni
nni
nni
nn
ii xkFxkEykDykCk
ayxA (9)
note that i represents the regions I, II, IV and V. The potential vector is the derived to find field
expressions.
To facilitate post processing of the machine performance (local and global quantities), the following
change of variable is made: *rx and zy , note that 𝑟 = moyR is the average radius.
Therefore, equation (7) can be written in the scalar form in cylindrical coordinates as follows:
RB
rz
AA
r
112
2
2
2
2 (10)
The rotor coordinate system that refers to stator coordinate system is considered and defined by
relation (11), where 𝑟 = moyR is the average radius and d is the relative displacement of the rotor:
ezzR and dR (11)
Therefore, the vector potential solution for each region can be written as:
0,3,3
,3,3,3
0,3
0,3
sin
cos,
ml
ml
m
lm
lmlll
mprmpzshFrmpzchE
mprmpzshDrmpzchC
mp
rzDazA
(12)
0
0sin
cos,
ni
ni
n
in
inii
nprnpzshFrnpzchE
nprnpzshDrnpzchC
np
razA
(13)
where i represents the regions I, II, IV and V.
Magnetic field vector components are deduced from the magnetic vector potential zA i , as
shown:
A
rBz
1and
z
AB
(14)
Field components expressions will be derived for each region in the following subsections.
C. Region I (rotor slots regions)
Boundary conditions to be satisfied by the magnetic field components in region I in slot „i‟, are:
erdlld
derdl
Rl
zw
NlwforzB
1,
,122
0, (15)
(16)
Where 1,,0 dNl , pNNN srd ,gcd , and p is the pole pair number.
The general expressions of the magnetic field components in region I are given by:
ehzforzB drRl 0,,1
0
,1,1
0
,1,1
sin,
cos,
m
dlR
erdr
er
er
drR
lmRR
lz
m
dlR
erdr
er
er
drR
lmRR
l
w
m
hwr
mch
wr
hzmch
zB
w
m
hwr
mch
wr
hzmsh
zB
(17)
D. Region II (air gap region)
In this region, the general solution of the magnetic field is:
npr
npzshF
r
npzchEnp
r
npzshD
r
npzchCzB
npr
npzchF
r
npzshEnp
r
npzchD
r
npzshCzB
nn
n
nnz
nn
n
nn
cossin,
sincos,
22
0
222
22
0
222
(18)
E. Region III (permanent magnet region)
The boundary condition for this region is given by, where and :
(19)
The general solution for the magnetic field components in this region is:
0
,3,3,3
0
,3,3,30
,3
sin,
cos,
m
alaa
lm
a
lm
lz
m
alaa
lm
a
lm
ll
w
mz
rw
mshDz
rw
mchCzB
w
mz
rw
mchDz
rw
mshCDzB
(20)
F. Region IV (stator slots regions)
Regions IV are composed of Nm regions (which correspond to half of stator slots). Boundary
conditions to be satisfied by the magnetic field components are listed in (21), where and
:
esl hzforzB 0,,4 (21)
General expressions of magnetic field components can be written by taking into account these
boundary conditions:
1,,0 mNl pNNN ssm ,gcd
adlla
maallz
w
NlwforzB
1,
,322
0,
1,,0 mNl
esdsas www 2
eselle
sdsa
ellz
w
lww
forzB
1,
,420,
0
,4,4
0
,4,4
sin,
cos,
m
el
es
es
es
es
es
lm
lz
m
el
es
es
es
es
es
lm
l
w
m
hwr
mch
wr
hzmch
GzB
w
m
hwr
mch
wr
hzmsh
GzB
(22)
G. Region V (surrounding air)
The boundary condition for this region can be expressed by setting the magnetic field components to
zero at z . These magnetic field components can be written as:
0
555
0
555
cossinexp,
sincosexp,
n
nnz
n
nn
npnFnpEzr
npzB
npFnpEzr
npzB
(23)
H. Boundary condition between areas
In order to compute the Fourier series coefficients of the magnetic field, boundary conditions between
regions (interface conditions) are required. In the studied machine, the magnetic field strength in iron
is zero since the permeability of stator and rotor core is assumed to be infinite. Also, it is assumed that
the stator and the rotor iron as well as PMs are not conductive materials. So, the surface current
density is equal to zero everywhere. Then, the boundary conditions between region I (rotor slots
regions) and region II (air gap region) are:
1,,0,0,
,0, 1,
2,1
2,1
d
ldddl
zdl
z
dl
Nlfor
eBB
eHH
(24)
12 0, dlddlforeH (25)
The use of the last boundary conditions yields to a system of equations made up of relations between
Fourier coefficients of the magnetic field in the air gap region. The next boundary conditions that will
be exploited between regions II, III (stator slots regions) and IV (PMs regions), can be expressed as
follows:
1,,00,0,
0,0, 1,
,32
,32
m
laal
lzz
l
Nlfor
BB
HH
(26)
1,,00,0,
0,0, 1,
,42
,42
m
leel
lzz
l
Nlfor
BB
HH
(27)
11,
1,2 00,alle
ellaforH
(28)
This step helps establish relations between coefficients of region II with those of region III and region
IV. Final step consists in the exploitation of the interface conditions between regions III and V and can
be written as follows:
1,,0,,
,, 1,
,35
,35
m
laal
al
zaz
al
a
Nlfor
hBhB
hHhH
(29)
11,5 0, allaa forhH (30)
The treatment of the aforementioned boundary conditions leads to a set of unknown variables for the
magnetic field expressions. However, to evaluate the unknown coefficients additional boundary
conditions are necessary . These can be obtained by using the continuity of the magnetic vector
potential property firstly between region II and region III, then between region III and region V [9].
This approach can be obtained by setting one of the arbitrary coefficients found in Eq. 9 to zero.
Consequently, system of linear equations is obtained and the unknowns are coefficients of the
magnetic field in regions II and V. Solving this linear equation and using interface conditions give
coefficients of magnetic vector potential in other regions.
IV. GLOBAL QUANTITIES COMPUTATION
Computation of the cogging torque, flux linkage, EMF allows the evaluation of the machine's
performance. In the next subsections global quantities will be evaluated.
A. Electromotive force calculation
The EMF is computed using Faraday‟s law based on the time variation of magnetic flux as given by
[14]-[16]:
t
cjje
(31)
The cj is the PM flux linking a coil “j” with tn turns in series and can be expressed in the
cylindrical coordinates by:
2
0
222
,2
dBFRR
ndsBn dzDjio
t
s
tcj (32)
where S is the surface of the coil, d is the angular position of the rotor with respect to the stator
frame and is the angular position in the stator frame.
DjF designates the distribution function of a coil “j”. It can be expressed using Fourier series as
follows [16]:
0
0 coscosn
jDn
jDn
jDDj npFnpEEF (33)
B. Cogging torque computation
The cogging torque is calculated by applying Maxwell stress tensor method and can be expressed as
follows:
ia0
2
0
222
0
,,1
o
i
R
R
zC ddreBeBrT (34)
Where 2
zB and 2
B are respectively the normal and tangential magnetic field components in region II
Ri and Ro are respectively the outer and the inner radius.
After integration, the cogging torque can be given by:
(35)
In the next section, the electromagnetic performance of the 12/10-pole FSPM machine will be
predicted by using the foregoing model and 2D FEA.
V. Results and discussion
The magnetic field distribution is calculated for a disc type axial flux switching permanent magnet
machine which main parameters are given in Table I and verified with 2D FEA. This analysis has been
done with a relative permeability of 1∗ 𝑒5 for ferromagnetic cores.
Therefore the derived analytical expressions of the field distribution have been validated by finite-
element calculations of the tangential and normal magnetic field components in various regions of the
machine.
The solution in the centre of the air gap for a given position of the rotor relatively to the stator is
shown in Fig.5 where excellent agreement is obtained. The magnetic field components are also
compared for both methods in the external air region as shown in Fig. 6. For the rotor slots and the
stator slots a comparison between analytical model and FEM results shows small differences as
presented in Fig. 7 and Fig.8. This can be explained by meshing irregularities and poor accuracy of
the model inside slots. Despite these differences, it can be seen that the analytical prediction agrees
well with the finite-element solution in the slot opening, air gap and external air regions. the
comparison between the analytically predicted and finite-element calculated magnetic field
components in PMs region is presented in Fig.9. As seen, fairly good agreement is again achieved.
0
2222
0
22
3n
nnnnio
C EDFCRR
T
Fig.5: Comparison of the magnetic field components in
the air gap region (z = - e/2) (region II)
TABLE I – Machine Parameters
Parameter Value
Pole pair number 10
Slot number 12
Air gap e (mm) 1
Relative permeability of PMs
r 1.045
Remanent flux density BR (T) 1.16
Active length Lpp (mm) 60
hdr, hes, ha (mm)
20, 10 and
21
wa, wer and wes (mm) 6, 15 and 4
VI. Conclusion
A general analytical model of a disc type switching flux permanent magnet machine is discussed,
where the periodic geometry is divided into regions. The proposed model is based on an exact 2D
solution of the magnetic field. The mathematical approach leading to the exact solution of the
Maxwell‟s equations using the separation of variables method in the different regions was briefly
exposed. Then, the global quantities expressions were derived from the 2D solution of the magnetic
field. Finally, the analytical results for the magnetic field were compared with those obtained by FEA,
and good agreement was obtained. The developed model can then be used in the early stage of the
design process of such type of electrical machines.
Fig. 6: Comparison of the magnetic field components
in the external air region (z = ha + 1/2) (region V)
(region II)
Fig. 7: Comparison of the magnetic field components in
the rotor slot region (z = hes /2) (region VI)
(region II)
Fig. 9: Comparison of the magnetic field components
in the permanent magnet region (z = ha /2) (region III)
Fig. 8: Comparison of the magnetic field components
in the stator slot region (z = -hdr /2) (region I)
(region II)
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