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Purpose

This work introduces an efficient and accurate technique to solve the eddy current problem in laminated iron cores considering vector hysteresis.

Design/methodology/approach

The mixed multiscale finite element method based on the based on the T,Φ-Φ formulation, with the current vector potential T and the magnetic scalar potential Φ allows the laminated core to be modelled as a single homogeneous block. This means that the individual sheets do not have to be resolved, which saves a lot of computing time and reduces the demands on the computer system enormously.

Findings

As a representative numerical example, a single-phase transformer with 4, 20 and 184 sheets is simulated with great success. The eddy current losses of the simulation using the standard finite element method and the simulation using the mixed multiscale finite element method agree very well and the required simulation time is tremendously reduced.

Originality/value

The vector Preisach model is used to account for vector hysteresis and is integrated into the mixed multiscale finite element method for the first time.

The mixed multiscale finite element method (MMSFEM) has already been successfully introduced for linear and nonlinear eddy current problems (ECPs), see for example Hollaus (2019) and Hollaus and Schöbinger (2020). In addition, the method has been applied to scalar hysteresis as it occurs in ferromagnetism (Schöbinger et al., 2019). Most notably, it has been demonstrated that the hysteresis phenomenon cannot be neglected when comparing simulation results to measurement data.

A 2 D/1D approach considering hysteresis with a comparison of simulation results with measurement data can be found in Bottauscio and Chiampi (2002). A b-conform and a h-conform homogenisation techniques for the ECP in laminated cores is presented in Dular (2008). A two-step technique has been proposed in Bíró et al. (2005). In the first step, the laminated medium is assumed to have an anisotropic electric conductivity and in the second step, the eddy currents are computed individually in each sheet.

The aim of this paper is to efficiently simulate eddy currents in laminated iron cores considering vector hysteresis. Thanks to the mixed T-Φ, Φ formulation, with a current vector potential (CVP) T and a magnetic scalar potential (MSP) Φ, the vector Preisach model (VPM) can be used in the forward mode. Using a magnetic vector potential (MVP) A would require an inverse mode of the VPM, which is computationally expensive.

The developed technique is evaluated by a transformer excited by known currents in coils, see also Hollaus (2019). The excitation is considered by the corresponding Biot-Savart field.

First, a brief explanation of the computationally optimised scalar Preisach model (SPM) and the VPM and their integration into the finite element method (FEM) are given in Sec. II. Then, the standard formulation for T-Φ, Φ to solve the nonlinear ECP by the time stepping method with the FEM is presented in Sec. III. Next, the MMSFEM is introduced to substantially reduce the overall computational costs of the considered ECP in Sec. IV. Simulation results in Sec. V demonstrate that the results obtained by the MMSFEM agree very well with the results obtained by the reference solution.

The Preisach model describes a hysteresis phenomenon (Mayergoyz, 1991).

In ferromagnetic materials, hysteresis occurs between the magnetic field strength H and the magnetic flux density B. The original version of the Preisach model considered scalar hysteresis only. The fundamental idea for the SPM consists of describing the hysteresis effect through an infinite number of weighted two-state operators γαβ[H(t)]:  →{0,1}, where α and β denote the upper and lower threshold for switching the current state. The operators are weighted by the Preisach function μ(α,β), which uniquely defines a specific material. The integration of these weighted operators over the Preisach plane determines the magnetic flux density

(1)

The Preisach plane Tmax := T(Hmax, − Hmax) is defined as the triangle

(2)

for a maximal value of the magnetic field strength Hmax, which sets the limits of the Preisach model. Possible larger values must be handled separately in a feasible numerical scheme.The integration over a triangle T(α,β) ⊆ Tmax yields the Everett function

(3)

Using the Everett function in (1) yields an increase in performance. Moreover, the approach of perfect demagnetisation reduces the average computational costs tremendously (Tousignant et al., 2017). For the perfect demagnetisation approach the maximal absolute input value over time of the magnetic field strength

(4)

is stored. Finally, the time-variant magnetic flux density is

(5)

The values Mk and mk denote the essential maxima and minima in the input sequence, respectively.

An additional improvement of the performance can be achieved by storing the subtotals of the sum in (5). This approach avoids recalculation of previously calculated results and is particularly useful when the input varies in a limited range without wiping out previous extrema.

For describing the material, the Lorentzian Preisach function is used (Schöbinger et al., 2019). Its Everett function is given by

(6)

The parameters in Table 1 are obtained by solving an inverse problem using measurement data at a frequency of 50 Hz. The remaining integral in (6) does not have an analytic representation and has to be calculated numerically. A major hysteresis loop along with the initial magnetisation curve obtained by these parameters is shown in Figure 1. The discretisation of the Preisach plane is done in 701 steps along the α- and the β-axis, respectively. A critical aspect of magnetic hysteresis is that the magnetic permeability μ=BH is not defined for the magnetic remanence (H = 0) leading to problems in numerical schemes. However, the differential permeability

(7)

where ΔH describes a sufficiently small local discrete step size, is greater than zero in any case.

Table 1.

Parameters for the Lorentzian Everett function for 50 Hz (M400-50A)

a –8.18773707 · 101 
b 4.13538892 · 101 
K1 2.00442033 · 10– 2 
K2 2.49345353 · 10– 1 
e 1.33306276 · 102 
f 5.57513398 · 10– 3 
a –8.18773707 · 101 
b 4.13538892 · 101 
K1 2.00442033 · 10– 2 
K2 2.49345353 · 10– 1 
e 1.33306276 · 102 
f 5.57513398 · 10– 3 
Figure 1.

Initial magnetisation curve and the hysteresis loop with an Everett function based on the Lorentzian function.

Figure 1.

Initial magnetisation curve and the hysteresis loop with an Everett function based on the Lorentzian function.

Close modal

The VPM is a superposition of an infinite number of SPMs. In the three-dimensional case, the SPMs are distributed on the surface of a unit sphere. Hence, each SPM has a position vector eR which affects the scalar magnetic flux density BR=Γ^[H·eR] of the corresponding SPM. The integration over the full unit sphere surface defines the vectorial magnetic flux density

(8)

To uniformly distribute a finite number of SPMs on the unit sphere, Lebedev coordinates with the direction vectors eR,i and the associated weights wi have been chosen for the numerical integration of (8) as shown in Figure 2 (Lebedev, 1976). Experiments have shown that Lebedev coordinates are well suited for the distribution of SPM on the surface of a unit sphere. The number of SPMs has been selected with N = 73 as a good compromise between accuracy and computation costs. The numerical integration of (8) yields the approximation for the vectorial flux density

(9)
Figure 2.

Lebedev distribution for points on the surface of a unit sphere

Figure 2.

Lebedev distribution for points on the surface of a unit sphere

Close modal

It is worth mentioning that the Everett function (3) of a SPM has to be adapted when it is used in the VPM (Mayergoyz, 1991).

The tensor-valued differential permeability

(10)

is a superposition of the scalar differential permeabilities μR,iΔ in (7) weighted by wi according to the Lebedev coordinates and the outer product of the direction vectors eR,i pointing in the direction of each SPM.

The ECP couples a static magnetic field in an electrically non-conducting domain Ω0 with a quasi-static magnetic field in an electrically conducting domain Ωc. Since the VPM is implemented for the forward mode only, the T,Φ-Φ formulation is used (Bíró, 1991).

Considering Ampere’s law ∇ × H = J + JBS, with an impressed current density JBS, the divergence of the current density

(11)

is identically zero. Therefore, the approach

(12)

with the CVPs T and TBS can be applied. The Biot-Savart field

(13)

is used for JBS, where r and r denote source and field point, respectively. Thus, the magnetic field strength is

(14)

with a MSP Φ. Since no eddy currents occur in Ω0, the CVP T vanishes.

Therefore, the boundary value problem (BVP) with the mixed T,Φ-Φ formulation for the quasi-static magnetic field in Ωc is described by

(15)
(16)
(17)
(18)

Moreover, the static magnetic field in Ω0 is described by

(19)
(20)
(21)

Finally, the interface conditions are

(22)

where Γ0c is the interface between Ω0 and Ωc. The indices E, H or B mean that the tangential components of E or H or the normal component of B are prescribed. The indices 0 or c denote the non-conducting or the conducting domain, respectively.

The nonlinear system is split into a linear and a nonlinear part (Bottauscio and Chiampi, 2002). The fixed-point permeability

(23)

is set to be the mean value of the smallest and largest differential permeability. Further, the nonlinear parts are shifted to the right-hand side, leading to constant matrices on the left-hand side. Since the differential permeability of the VPM μ¯¯Δ is tensor-valued, the fixed-point differential permeability μ¯¯FPΔ has to be tensor-valued as well. Therefore, the fixed-point differential permeability is a 3 × 3 diagonal matrix with each diagonal element being equivalent to μFPΔ of the SPM.

The differential approach

(24)

with HΔ= H(n+1)H(n) has been used in the weak formulation in order to exploit the differential permeability μ¯¯Δ. The full weak formulation for the standard finite element method (SFEM) is shown in App. I.

To avoid the necessity to resolve the individual sheets of the iron core, the mixed multiscale approach

(25)

with the micro-shape function ϕ2, which is shown in Figure 3, is selected. The second order Gauss-Lobatto polynomial

(26)

is chosen as micro-shape function (Hollaus, 2019). The average MSP Φ0 takes into account the solution on the large scale while the CVP T2 along with the periodic micro-shape function ϕ2 considers the oscillating variation on the small scale (Hollaus and Schöbinger, 2020).

Figure 3.

Second order Gauss-Lobatto polynomial as micro-shape function ϕ2 in a sheet with an air gap of width d0

Figure 3.

Second order Gauss-Lobatto polynomial as micro-shape function ϕ2 in a sheet with an air gap of width d0

Close modal

In the mixed-multiscale approach the insulated sheets are considered as bulk material. To obtain the specific material parameters in a global integration point, an additional integration with local integration points is needed, see Figure 4. In each local integration point an independent VPM is set up and is updated in every time instant.

Figure 4.

Global (left) and local (right) integration points in the bulk core

Figure 4.

Global (left) and local (right) integration points in the bulk core

Close modal

The weak formulation for MMSFEM can be found in App. II.

The ECP of the laminated iron core shown in Figures 5 and 6 is investigated. The thickness of an iron sheet is dFe = 0.5 mm and the width of the gap d0 = 0.01 mm, yielding a fill-factor kf=dFedFe+d0=0.9804 and the core is composed of 184 sheets. The electric conductivity of iron is selected with σ = 2 · 106S/m. The excitation of the problem is considered by the Biot-Savart field of four symmetric cylindrical coils with 60 turns each. The frequency is selected with f = 50Hz. The arrangement of the core with the coils exhibits three planes of symmetry. Handmade structured hexahedral finite element meshes have been used. The same discretisation by finite elements in the x, y-plane have been used in the models for the SFEM and MSFEM to ensure a fair comparison. One period of time is discretised in 600 steps. The material of the iron sheets is considered to be demagnetised initially. The simulations have been done by Netgen/NGSolve (Schöberl, 2021).

Figure 5.

One eighth of the laminated iron core (gray) with the coils (red), not drawn to scale

Figure 5.

One eighth of the laminated iron core (gray) with the coils (red), not drawn to scale

Close modal
Figure 6.

Top (left) and front (right) view of the geometry, not drawn to scale, dimensions are in mm, planes of symmetry are x = 0, y = 0 and z = 0

Figure 6.

Top (left) and front (right) view of the geometry, not drawn to scale, dimensions are in mm, planes of symmetry are x = 0, y = 0 and z = 0

Close modal

The reference solution with SFEM has been computed to verify the results obtained by the MMSFEM. Simulations with different impressed currents I0 and different number of iron sheets have been carried out. For every time instant the eddy current losses

(27)

have been calculated. Eddy current losses using the BH-curve (initial magnetisation curve) are shown in Figures 7 and 8 and those considering hysteresis are presented in Figures 9 and 10. The additional peaks in Figures 7 and 8 are due to the convex-concave nature of the BH-curve. The eddy current losses are obtained for simulations with I0 = 1 A and I0 = 3 A and with 184 sheets. For the sake of visibility, only every third data point is shown.

Figure 7.

Eddy current losses for I0 = 1 A peak without hysteresis

Figure 7.

Eddy current losses for I0 = 1 A peak without hysteresis

Close modal
Figure 8.

Eddy current losses for I0 = 3 A peak without hysteresis

Figure 8.

Eddy current losses for I0 = 3 A peak without hysteresis

Close modal
Figure 9.

Eddy current losses for I0 = 1 A peak with hysteresis

Figure 9.

Eddy current losses for I0 = 1 A peak with hysteresis

Close modal
Figure 10.

Eddy current losses for I0 = 3 A peak with hysteresis

Figure 10.

Eddy current losses for I0 = 3 A peak with hysteresis

Close modal

Further, the mean value

(28)

has been calculated in the steady state. With the aid of P the error

(29)

is calculated, which is not very sensitive. For a stricter criterion the error

(30)

using the time instants of the eddy current losses p(t), has been introduced. A comparison of the local solutions are shown in Figures 11 and 12 representing the magnetic flux density B and the current density J in the same layer. Further simulation results without hysteresis are summarised in Table 2 and with hysteresis in Table 3. Compared to the nonlinear simulations, the number of iterations increases slightly for the simulations with hysteresis, see Table 4. The reduction of degrees of freedom NDOF increases with the number of sheets in the laminated iron core for both MMSFEM and SFEM. However, MMSFEM requires essentially less NDOF. The same holds for the number of VPMs NVPM, as well as for the required computation time. The number of needed VPMs for small problems with just a few sheets is relatively high, which results in long simulation times tsim also for MMSFEM.

Figure 11.

Magnetic flux density B for I0 = 3 A peak-to-peak at z ≈ 45.9 mm and t = 25ms, reference solution with SFEM on the left and MMSFEM on the right

Figure 11.

Magnetic flux density B for I0 = 3 A peak-to-peak at z ≈ 45.9 mm and t = 25ms, reference solution with SFEM on the left and MMSFEM on the right

Close modal
Figure 12.

Current Density J for I0 = 3 A peak-to-peak at z ≈ 45.9 mm and t = 50ms, reference solution with SFEM on the left and MMSFEM on the right

Figure 12.

Current Density J for I0 = 3 A peak-to-peak at z ≈ 45.9 mm and t = 50ms, reference solution with SFEM on the left and MMSFEM on the right

Close modal
Table 2.

Numerical data for various simulations without hysteresis

No. Sheets420184184
I0 in A 
P in W SFEM 0.336 1.753 3.956 16.18 
 MMSFEM 0.339 1.771 4.009 16.383 
ε1 in %  0.881 1.034 −1.337 1.25 
ε2 in %  3.51 8.21 1.39 7.28 
N DOF SFEM 58,868 195,940 1,600,928 1,600,928 
 MMSFEM 49,859 74,021 122,345 122,345 
NVPM SFEM 14,336 71,680 659,456 659,456 
 MMSFEM 100,352 200,704 401,408 401,408 
tsim in h SFEM 6.0 22.2 208.5 210.2 
 MMSFEM 7.3 12.9 24.7 23.8 
No. Sheets420184184
I0 in A 
P in W SFEM 0.336 1.753 3.956 16.18 
 MMSFEM 0.339 1.771 4.009 16.383 
ε1 in %  0.881 1.034 −1.337 1.25 
ε2 in %  3.51 8.21 1.39 7.28 
N DOF SFEM 58,868 195,940 1,600,928 1,600,928 
 MMSFEM 49,859 74,021 122,345 122,345 
NVPM SFEM 14,336 71,680 659,456 659,456 
 MMSFEM 100,352 200,704 401,408 401,408 
tsim in h SFEM 6.0 22.2 208.5 210.2 
 MMSFEM 7.3 12.9 24.7 23.8 
Table 3.

Numerical data for various simulations with hysteresis

No. Sheets420184184
I0 in A 
P in W SFEM 0.408 2.086 5.008 19.206 
 MMSFEM 0.407 2.079 5.004 19.216 
ε1 in %  0.22 0.33 0.1 0.05 
ε2 in %  6.37 11.62 1.37 11.72 
N DOF SFEM 58,868 195,940 1,600,928 1,600,928 
 MMSFEM 49,859 74,021 122,345 122,345 
NVPM SFEM 14,336 71,680 659,456 659,456 
 MMSFEM 100,352 200,704 401,408 401,408 
tsim in h SFEM 10.7 34.1 295.5 294.9 
 MMSFEM 12.9 18.3 29.5 30.8 
No. Sheets420184184
I0 in A 
P in W SFEM 0.408 2.086 5.008 19.206 
 MMSFEM 0.407 2.079 5.004 19.216 
ε1 in %  0.22 0.33 0.1 0.05 
ε2 in %  6.37 11.62 1.37 11.72 
N DOF SFEM 58,868 195,940 1,600,928 1,600,928 
 MMSFEM 49,859 74,021 122,345 122,345 
NVPM SFEM 14,336 71,680 659,456 659,456 
 MMSFEM 100,352 200,704 401,408 401,408 
tsim in h SFEM 10.7 34.1 295.5 294.9 
 MMSFEM 12.9 18.3 29.5 30.8 
Table 4.

Number of nonlinear iterations

SFEMMMSFEM
No. SheetsI0meanmax.meanmax.
Nonlinear 
1.71 2.04 
20 1.83 2.07 
184 1.82 2.05 
184 1.86 2.08 
Hysteresis 
1.68 2.05 10 
20 1.77 2.05 10 
184 1.80 2.1 
184 1.81 2.08 
SFEMMMSFEM
No. SheetsI0meanmax.meanmax.
Nonlinear 
1.71 2.04 
20 1.83 2.07 
184 1.82 2.05 
184 1.86 2.08 
Hysteresis 
1.68 2.05 10 
20 1.77 2.05 10 
184 1.80 2.1 
184 1.81 2.08 

The MMSFEM introduced in the frequency domain for a linear ECP (Hollaus and Schöbinger, 2020) has been extended for materials with vector hysteresis in the time domain. Simulation results of SFEM with resolved sheets and MMSFEM with a coarse finite element mesh show a very high agreement. The efficiency of MMSFEM compared to SFEM substantially grows with the number of iron sheets.

This work was supported by the Austrian Science Fund (FWF) under Project P 31926.

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The weak formulation for SFEM reads as:

Find (T(n+1)(n+1)) ∈VD := {T(n+1)(n+1)} :T ∈ u,Φ ∈ v and T(n+1) × n = 0 on Γ0c ∪ ΓHc(n+1) = 0 on ΓHc ∪ ΓH0}, such that

(31)

and

(32a)
(32b)

for all (T’,Φ’) ∈ V0, where u and v are finite element subspaces of H(curl,Ωc) and H1(Ω), respectively (Schöberl and Zaglmayr, 2005). The fixed-point method in the weak formulation requires ΦΔ,(n) and TΔ,(n), cf. (24), of the former time instant.

The weak formulation for MMSFEM reads as:

Find (T2(n+1), Φ0(n+1))VD:={(T2(n+1), Φ0(n+1)):T2(n+1)U, Φ0(n+1)V, T2(n+1)×n=0 on Γ0cΓT2ΓHc, Φ0(n+1)=0 on ΓHcΓH0}, such that

(33)

and

(34a)
(34b)

for all (T2,Φ’0) ∈ V0, where u ⊂ H(curl,Ωc), v ⊂ H1(Ω) and ϕ2Hper1(Ωc) have been selected. The interface ΓT2 is the part of Γ0c which represents the smooth surface of the laminated iron core, see Figure 5. The averaged coefficients are denoted by the bar and are calculated as described in (Hollaus and Schöberl, 2018). The fixed-point method is exploited to solve the nonlinear problem, see Sec. III-B. The VPM is applied to describe the ferromagnetic material, see Sec. II-B. To overcome the singularity of the tensor-valued permeability in the magnetic remanence, a differential approach is chosen, see (7).

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