PDF
Linear Motor in 2D
Introduction
This example shows how to build and analyze a model of a linear motor, a device exerting force in order to produce translational motion. Typical characteristics of linear motors are high precision and quick acceleration. They are used in a wide variety of applications ranging from small actuators to propulsion of transportation systems such as Maglev trains. Here we will consider a flat and slotted topology with a three phase excitation in the stationary part, often called forcer. The other part, often called track, will be the moving part containing permanent magnets which makes out for a brush-less and synchronous design. A 3D representation of the linear motor is illustrated in Figure 1.
Figure 1: A 3D representation of the magnetic parts of the linear motor to be simulated.
A vertical cut along the axis of motion gives a cross section where the currents are perpendicular to the plane and where the major magnetic field gradients vary in-plane, which is in line with 2D magnetic field formulation.
Figure 2: 2D geometry of linear motor with magnetic steel materials in grey, coils in orange and permanent magnets in white.
In principle, a cross section of a linear machine is very similar to a 2D representation of an axial flux machine. A circular surface parallel to the axis of rotation (and in line with the magnetic flux direction), will capture the magnetic field gradients in plane and have perpendicular currents. This linear motor modeling example doubles as a 2D representation of an axial flux machine.
Figure 3: The blue circular surface rolled out can represent a cross section of an axial flux motor in 2D.
For the combined model of a linear and an axial flux motor, consider a fractional slot topology. This means that the number of slots divided by the number of phases and the number of poles is less than one, and that coils do not span around more than one tooth. In terms of a linear motor, the geometry represents a periodic section of the machine. In terms of an axial flux motor, the geometry can represent the entire circular cross section.
For simplicity, consider a low but reasonable number of 12 slots and 10 poles on a periodic and symmetric geometry spanning approximately 150 mm in the direction of linear motion. For an axial flux motor, the modeled surface is preferably centered radially in the magnetic region, which in this case represents a surface diameter of roughly 50 mm.
The simulation comprises two studies, where the first one determines the optimal current angle, and the second one simulates linear motion in time. The resulting air-gap shear stress, total force and torque, energy balance, and harmonics are postprocessed and analyzed.
Modeling in COMSOL Multiphysics
In order to properly account for the interaction between the stationary and moving parts, the geometry is split into two objects called an assembly in COMSOL Multiphysics. In this example, the split is created along a horizontal line centered in the middle of the air gap. The Moving Mesh interface lets you define the motion of the moving part.
The parts are coupled on their adjacent boundaries in the middle of the air gap by the Periodic Pair feature. The Periodic Pair feature performs a transformation of the field crossing the boundaries accounting for the instantaneous velocity. Where the boundaries are not adjacent to each other, the Periodic Pair maps the field back together assuming symmetric geometry. For the external vertical boundaries on each side, a Periodic Condition feature is applied for both stationary and moving parts.
Figure 4: Arrows showing magnetic flux density and direction on boundary in the middle of the air gap. The field protruding from the moving part (red arrows) is mapped onto the stationary part (blue arrows).
In the air gap, a thin domain is added in order to accurately compute the linear force produced. An integral of the magnetic force density in the direction of motion over this domain provides a robust way of calculating the shear force acting on the parts.
The optimal current angle is determined by a stationary simulation keeping the moving part at the initial position, while sweeping the current vector over one electrical period. The initial current angle constant is then updated with an angle corresponding to the maximum force. The motion of the moving part is defined such that it moves in synchronization and in the same direction as the winding magnetic field.
In this example, the motion is prescribed as a constant velocity. It is also possible to add equations governing a dynamic motion — a result of forces, friction, and mass of inertia.
Results and Discussion
Figure 5 shows a plot of the magnetic flux density, giving an impression of the field distribution at a given instant.
Figure 5: Magnetic flux density distribution at the end of first electrical period (the regions without contour lines on each side are postprocessed displacements of the modeled result).
Figure 6 shows the linear force as a function of time for one electrical period. The linear force is on average 56 N and has the 12th harmonic of electrical frequency as the most prominent peak.
Figure 6: Linear force as function of time for one electrical period.
A Fourier transform of the linear force signal reveals that the 12th harmonic is about eight times larger than the 6th harmonic, as shown in Figure 7.
Figure 7: Harmonic content of the linear force with the electrical frequency as basis.
The overall results are evaluated in an Evaluation Group which allows for a tabulated presentation of quantities of different units.
Table 1: Results summary.
Quantity
Value
Airgap shear stress (Pa)
17990
Linear force (N)
56.5
Torque (axial flux motor) (N·m)
1.4
Linear motion power (W)
28.3
Rotational motion power (W)
28.3
Electric input power (W)
38.0
Windings resistive loss (W)
9.7
Magnets induced loss (W)
0.05
Application Library path: ACDC_Module/Devices,_Motors_and_Generators/linear_motor_2d
Modeling Instructions
From the File menu, choose New.
New
In the New window, click  Model Wizard.
Model Wizard
1
In the Model Wizard window, click  2D.
2
In the Select Physics tree, select AC/DC > Electromagnetic Fields > Magnetic Fields (mf).
3
Click Add.
4
Click  Done.
Geometry 1
1
In the Model Builder window, under Component 1 (comp1) click Geometry 1.
2
In the Settings window for Geometry, locate the Units section.
3
From the Length unit list, choose mm.
Global Definitions
Parameters - main
1
In the Model Builder window, under Global Definitions click Parameters 1.
2
In the Settings window for Parameters, type Parameters - main in the Label text field.
3
Locate the Parameters section. In the table, enter the following settings:
Name
Expression
Value
Description
Np
10
10
Nr of poles on moving part/rotor
Ns
12
12
Nr of stator slots
v_lin
0.5[m/s]
0.5 m/s
Linear motion velocity
I_ph
2.5[A]
2.5 A
Phase current rms
Nturn
120
120
Nr of turns per coil
r_inc
25[mm]
0.025 m
Incision/ computational plane radius (axial flux motor)
s_rot
v_lin/(2*pi*r_inc)
3.1831 1/s
Rotational speed (axial flux motor)
f_el
s_rot*Np/2
15.915 1/s
Electrical frequency
ang_el_init
0[deg]
0 rad
Initial current angle (max force/ torque)
L_mag
20[mm]
0.02 m
Length into plane/ radial extent of magnetic materials
t
0[s]
0 s
Time variable alias
Parameters - geometry
1
In the Home toolbar, click  Parameters and choose Add > Parameters.
2
In the Settings window for Parameters, type Parameters - geometry in the Label text field.
3
Locate the Parameters section. In the table, enter the following settings:
Name
Expression
Value
Description
arc_inc
r_inc*2*pi[rad]
0.15708 m
Incision plane arc length
th_air
5[mm]
0.005 m
Air thickness outside
th_rbyoke
5[mm]
0.005 m
Rotor back-yoke thickness
th_mag
3[mm]
0.003 m
Magnet thickness
th_airgap
1[mm]
0.001 m
Airgap thickness
th_stooth
19[mm]
0.019 m
Stator toooth thickness
th_coil
18[mm]
0.018 m
Coil thickness
th_sbyoke
5[mm]
0.005 m
Stator back-yoke thickness
ang_mag
2*pi[rad]/Np*0.8
0.50265 rad
Magnet pitch angle
arc_mag
r_inc*ang_mag
0.012566 m
Magnet arc length
arc_pp
arc_inc/Np
0.015708 m
Pole pitch arc length
w_slot
7.5[mm]
0.0075 m
Slot width
ang_slot
2*asin(w_slot/2/r_inc)
0.30114 rad
Slot pitch angle
arc_slot
r_inc*ang_slot
0.0075284 m
Slot arc length
arc_stooth
arc_inc/Ns-arc_slot
0.0055616 m
Stator tooth arc length
A_wire
th_coil*w_slot/2/Nturn*0.55
3.0938E-7 m²
Wire cross-sectional area including slot fill factor of .55
Variables 1
1
In the Model Builder window, right-click Global Definitions and choose Variables.
2
In the Settings window for Variables, locate the Variables section.
3
In the table, enter the following settings:
Name
Expression
Unit
Description
iA
I_ph*cos(2*pi*f_el*t+ang_el_init)
A
A phase current
iB
I_ph*cos(2*pi*f_el*t+ang_el_init-2*pi/3)
A
B phase current
iC
I_ph*cos(2*pi*f_el*t+ang_el_init-4*pi/3)
A
C phase current
The geometry construction is colored by it being a representation of a 3D axial flux motor. This means that the width and height of a rectangle is treated as ’arc length’ and ’thickness’, respectively.
Geometry 1
Rectangle 1 (r1)
1
In the Geometry toolbar, click  Rectangle.
2
In the Settings window for Rectangle, locate the Size and Shape section.
3
In the Width text field, type arc_mag.
4
In the Height text field, type th_mag.
5
Locate the Position section. In the x text field, type (arc_pp-arc_mag)/2.
6
In the y text field, type -th_mag.
Move 1 (mov1)
1
In the Geometry toolbar, click  Transforms and choose Move.
2
Select the object r1 only.
3
In the Settings window for Move, locate the Displacement section.
4
In the x text field, type arc_pp.
5
Locate the Input section. Select the Keep input objects checkbox.
Magnets up
1
In the Geometry toolbar, click  Transforms and choose Array.
2
In the Settings window for Array, type Magnets up in the Label text field.
3
Select the object r1 only.
4
Locate the Size section. In the x size text field, type Np/2.
5
Locate the Displacement section. In the x text field, type arc_pp*2.
6
Locate the Selections of Resulting Entities section. Select the Resulting objects selection checkbox.
7
From the Show in physics list, choose Off.
Magnets down
1
In the Geometry toolbar, click  Transforms and choose Array.
2
In the Settings window for Array, type Magnets down in the Label text field.
3
Select the object mov1 only.
4
Locate the Size section. In the x size text field, type Np/2.
5
Locate the Displacement section. In the x text field, type arc_pp*2.
6
Locate the Selections of Resulting Entities section. Select the Resulting objects selection checkbox.
7
From the Show in physics list, choose Off.
All magnets
1
In the Geometry toolbar, click  Selections and choose Union Selection.
2
In the Settings window for Union Selection, type All magnets in the Label text field.
3
Locate the Input Entities section. Click  Add.
4
In the Add dialog, in the Selections to add list, choose Magnets up and Magnets down.
5
Click OK.
Rotor back yoke
1
In the Geometry toolbar, click  Rectangle.
2
In the Settings window for Rectangle, type Rotor back yoke in the Label text field.
3
Locate the Size and Shape section. In the Width text field, type arc_inc.
4
In the Height text field, type th_rbyoke.
5
Locate the Position section. In the y text field, type -th_rbyoke-th_mag.
6
Locate the Selections of Resulting Entities section. Select the Resulting objects selection checkbox.
Rotor air
1
In the Geometry toolbar, click  Rectangle.
2
In the Settings window for Rectangle, type Rotor air in the Label text field.
3
Locate the Size and Shape section. In the Width text field, type arc_inc.
4
In the Height text field, type th_mag+th_rbyoke+th_air+th_airgap/2.
5
Locate the Position section. In the y text field, type -th_mag-th_rbyoke-th_air.
6
Locate the Selections of Resulting Entities section. Select the Resulting objects selection checkbox.
Aux torque calc domain
1
In the Geometry toolbar, click  Rectangle.
2
In the Settings window for Rectangle, type Aux torque calc domain in the Label text field.
3
Locate the Size and Shape section. In the Width text field, type arc_inc.
4
In the Height text field, type th_airgap/4.
5
Locate the Position section. In the y text field, type th_airgap/4.
6
Locate the Selections of Resulting Entities section. Select the Resulting objects selection checkbox.
Rotor selection
1
In the Geometry toolbar, click  Selections and choose Union Selection.
2
In the Settings window for Union Selection, type Rotor selection in the Label text field.
3
Locate the Geometric Entity Level section. From the Level list, choose Object.
4
Locate the Input Entities section. Click  Add.
5
In the Add dialog, in the Selections to add list, choose Magnets up, Magnets down, Rotor back yoke, Rotor air, and Aux torque calc domain.
6
Click OK.
Rotor
1
In the Geometry toolbar, click  Booleans and Partitions and choose Union.
2
In the Settings window for Union, type Rotor in the Label text field.
3
Locate the Union section. From the Input objects list, choose Rotor selection.
4
Click the  Zoom Extents button in the Graphics toolbar.
Stator tooth
1
In the Geometry toolbar, click  Rectangle.
2
In the Settings window for Rectangle, type Stator tooth in the Label text field.
3
Locate the Size and Shape section. In the Width text field, type arc_stooth.
4
In the Height text field, type th_stooth.
5
Locate the Position section. In the x text field, type arc_slot/2.
6
In the y text field, type th_airgap.
7
Click  Build Selected.
Stator teeth
1
In the Geometry toolbar, click  Transforms and choose Array.
2
In the Settings window for Array, type Stator teeth in the Label text field.
3
Select the object r5 only.
4
Locate the Size section. In the x size text field, type Ns.
5
Locate the Displacement section. In the x text field, type arc_stooth+arc_slot.
6
Locate the Selections of Resulting Entities section. Select the Resulting objects selection checkbox.
7
From the Show in physics list, choose Off.
Stator back yoke
1
In the Geometry toolbar, click  Rectangle.
2
In the Settings window for Rectangle, type Stator back yoke in the Label text field.
3
Locate the Size and Shape section. In the Width text field, type arc_inc.
4
In the Height text field, type th_sbyoke.
5
Locate the Position section. In the y text field, type th_airgap+th_stooth.
6
Locate the Selections of Resulting Entities section. Select the Resulting objects selection checkbox.
7
From the Show in physics list, choose Off.
Stator yoke selection
1
In the Geometry toolbar, click  Selections and choose Union Selection.
2
In the Settings window for Union Selection, type Stator yoke selection in the Label text field.
3
Locate the Geometric Entity Level section. From the Level list, choose Object.
4
Locate the Input Entities section. Click  Add.
5
In the Add dialog, in the Selections to add list, choose Stator teeth and Stator back yoke.
6
Click OK.
Stator yoke
1
In the Geometry toolbar, click  Booleans and Partitions and choose Union.
2
In the Settings window for Union, type Stator yoke in the Label text field.
3
Locate the Union section. From the Input objects list, choose Stator yoke selection.
4
Clear the Keep interior boundaries checkbox.
Coil leg
1
In the Geometry toolbar, click  Rectangle.
2
In the Settings window for Rectangle, type Coil leg in the Label text field.
3
Locate the Size and Shape section. In the Width text field, type arc_slot/2.
4
In the Height text field, type th_coil.
5
Locate the Position section. In the y text field, type th_airgap+th_stooth-th_coil.
Coil legs left
1
In the Geometry toolbar, click  Transforms and choose Array.
2
In the Settings window for Array, type Coil legs left in the Label text field.
3
Select the object r7 only.
4
Locate the Size section. In the x size text field, type Ns.
5
Locate the Displacement section. In the x text field, type arc_stooth+arc_slot.
6
Locate the Selections of Resulting Entities section. Select the Resulting objects selection checkbox.
7
From the Show in physics list, choose Off.
Coil legs right
1
In the Geometry toolbar, click  Transforms and choose Move.
2
In the Settings window for Move, type Coil legs right in the Label text field.
3
Locate the Input section. From the Input objects list, choose Coil legs left.
4
Select the Keep input objects checkbox.
5
Locate the Displacement section. In the x text field, type arc_slot/2+arc_stooth.
6
Locate the Selections of Resulting Entities section. Select the Resulting objects selection checkbox.
7
From the Show in physics list, choose Off.
Coil domains
1
In the Geometry toolbar, click  Selections and choose Union Selection.
2
In the Settings window for Union Selection, type Coil domains in the Label text field.
3
Locate the Geometric Entity Level section. From the Level list, choose Object.
4
Locate the Input Entities section. Click  Add.
5
In the Add dialog, in the Selections to add list, choose Coil legs left and Coil legs right.
6
Click OK.
7
In the Settings window for Union Selection, locate the Resulting Selection section.
8
From the Show in physics list, choose Domain selection.
Stator air
1
In the Geometry toolbar, click  Rectangle.
2
In the Settings window for Rectangle, type Stator air in the Label text field.
3
Locate the Size and Shape section. In the Width text field, type arc_inc.
4
In the Height text field, type th_airgap/2+th_stooth+th_sbyoke+th_air.
5
Locate the Position section. In the y text field, type th_airgap/2.
6
Locate the Selections of Resulting Entities section. Select the Resulting objects selection checkbox.
7
From the Show in physics list, choose Off.
Stator selection
1
In the Geometry toolbar, click  Selections and choose Union Selection.
2
In the Settings window for Union Selection, type Stator selection in the Label text field.
3
Locate the Geometric Entity Level section. From the Level list, choose Object.
4
Locate the Input Entities section. Click  Add.
5
In the Add dialog, in the Selections to add list, choose Stator yoke selection, Coil legs left, Coil legs right, and Stator air.
6
Click OK.
Stator
1
In the Geometry toolbar, click  Booleans and Partitions and choose Union.
2
In the Settings window for Union, type Stator in the Label text field.
3
Locate the Union section. From the Input objects list, choose Stator selection.
Form Union (fin)
1
In the Model Builder window, under Component 1 (comp1) > Geometry 1 click Form Union (fin).
2
In the Settings window for Form Union/Assembly, locate the Form Union/Assembly section.
3
From the Action list, choose Form an assembly.
4
In the Geometry toolbar, click  Build All.
Geometry 1
In the Model Builder window, collapse the Component 1 (comp1) > Geometry 1 node.
Definitions
Magnetic Steel domains
1
In the Definitions toolbar, click  Union.
2
In the Settings window for Union, type Magnetic Steel domains in the Label text field.
3
Locate the Input Entities section. Under Selections to add, click  Add.
4
In the Add dialog, in the Selections to add list, choose Rotor back yoke and Stator yoke selection.
5
Click OK.
Airgap integration
1
In the Definitions toolbar, click  Nonlocal Couplings and choose Integration.
Next, create an integration operating on the thin domain of the air gap, which will assist in accurate force and torque calculations.
2
In the Settings window for Integration, type Airgap integration in the Label text field.
3
Locate the Source Selection section. From the Selection list, choose Aux torque calc domain.
Variables 2
1
In the Model Builder window, right-click Definitions and choose Variables.
2
In the Settings window for Variables, locate the Variables section.
3
In the table, enter the following settings:
Name
Expression
Unit
Description
F_phi
mf.Bx*mf.By/mu0_const
Pa
Shear stress density
Torque
intop1(F_phi*r_inc)/(th_airgap/4)*L_mag
J
Torque (axial flux motor)
Force
intop1(F_phi)/(th_airgap/4)*L_mag
N
Linear Force (linear motor)
Torque
1
In the Definitions toolbar, click  Probes and choose Global Variable Probe.
Two probes are added to calculate force and torque while solving.
2
In the Settings window for Global Variable Probe, type Torque in the Label text field.
3
Locate the Expression section. In the Expression text field, type Torque.
Shear Force
1
In the Definitions toolbar, click  Probes and choose Global Variable Probe.
2
In the Settings window for Global Variable Probe, type Shear Force in the Label text field.
3
Locate the Expression section. In the Expression text field, type Force.
4
Click to expand the Table and Window Settings section. Click  Add Plot Window.
Definitions
In the Model Builder window, collapse the Component 1 (comp1) > Definitions node.
Add Material
1
In the Materials toolbar, click  Add Material to open the Add Material window.
2
Go to the Add Material window.
3
In the tree, select AC/DC > Soft Iron (Without Losses).
4
Click the Add to Component button in the window toolbar.
5
In the tree, select AC/DC > Hard Magnetic Materials > Sintered NdFeB Grades (Chinese Standard) > N40M (Sintered NdFeB).
6
Click the Add to Component button in the window toolbar.
7
In the tree, select AC/DC > Copper.
8
Click the Add to Component button in the window toolbar.
9
In the Materials toolbar, click  Add Material to close the Add Material window.
Materials
Soft Iron (Without Losses) (mat1)
1
In the Settings window for Material, locate the Geometric Entity Selection section.
2
From the Selection list, choose Magnetic Steel domains.
N40M (Sintered NdFeB) (mat2)
1
In the Model Builder window, click N40M (Sintered NdFeB) (mat2).
2
In the Settings window for Material, locate the Geometric Entity Selection section.
3
From the Selection list, choose All magnets.
Copper (mat3)
1
In the Model Builder window, click Copper (mat3).
2
In the Settings window for Material, locate the Geometric Entity Selection section.
3
From the Selection list, choose Coil domains.
Component 1 (comp1)
1
In the Model Builder window, click Component 1 (comp1).
2
In the Settings window for Component, in the Graphics window toolbar, clicknext to  Colors, then choose Show Material Color and Texture.
3
Click the  Zoom Extents button in the Graphics toolbar.
Moving part/ rotor
1
In the Physics toolbar, click  Moving Mesh and choose Prescribed Deformation.
2
In the Settings window for Prescribed Deformation, type Moving part/ rotor in the Label text field.
3
Locate the Geometric Entity Selection section. From the Selection list, choose Rotor selection.
4
Locate the Prescribed Deformation section. Specify the dx vector as
v_lin*t
X
0
Y
Magnetic Fields (mf)
1
In the Model Builder window, under Component 1 (comp1) click Magnetic Fields (mf).
2
In the Settings window for Magnetic Fields, locate the Thickness section.
3
In the d text field, type L_mag.
In this model, the Out-of-plane thickness setting will affect the resistance and voltage in coil features.
4
Click to expand the Discretization section. From the Magnetic vector potential list, choose Linear.
Periodic Pair 1
1
In the Physics toolbar, click  Pairs and choose Periodic Pair.
Next, add the Periodic Pair feature and configure it to operate on the Identity Boundary Pair which was created in the final step in geometry sequence.
2
In the Settings window for Periodic Pair, locate the Pair Selection section.
3
Click  Add.
4
In the Add dialog, select Identity Boundary Pair 1 (ap1) in the Pairs list.
5
Click OK.
Periodic Condition - stator
1
In the Physics toolbar, click  Boundaries and choose Periodic Condition.
2
In the Settings window for Periodic Condition, type Periodic Condition - stator in the Label text field.
3
Select Boundaries 64, 66, 68, 70, and 190–193 only.
Periodic Condition - moving part/ rotor
1
In the Physics toolbar, click  Boundaries and choose Periodic Condition.
2
In the Settings window for Periodic Condition, type Periodic Condition - moving part/ rotor in the Label text field.
3
Select Boundaries 1, 3, 5, 7, and 60–63 only.
4
Click the  Zoom Extents button in the Graphics toolbar.
Magnetic steel
1
In the Physics toolbar, click  Domains and choose Laminated Core.
2
In the Settings window for Laminated Core, type Magnetic steel in the Label text field.
3
Locate the Domain Selection section. From the Selection list, choose Magnetic Steel domains.
4
Locate the Lamination Model section. From the Lamination model list, choose Out-of-plane lamination.
5
In the s text field, type 1.
A phase winding
1
In the Physics toolbar, click  Domains and choose Coil.
2
In the Settings window for Coil, type A phase winding in the Label text field.
3
Select Domains 16, 19, 28–31, 40, and 41 only.
4
Locate the Coil section. From the Conductor model list, choose Homogenized multiturn.
5
Select the Coil group checkbox.
6
In the Icoil text field, type iA.
7
Locate the Homogenized Conductor section. In the N text field, type Nturn.
8
From the list, choose User defined.
9
Find the High-frequency effective loss subsection. Clear the Include harmonic loss checkbox.
10
In the a text field, type A_wire.
Reversed Current Direction 1
1
In the Physics toolbar, click  Attributes and choose Reversed Current Direction.
2
Select Domains 19, 29, 30, and 40 only.
B phase winding
1
In the Model Builder window, right-click A phase winding and choose Duplicate.
2
In the Settings window for Coil, type B phase winding in the Label text field.
3
Locate the Domain Selection section. Click  Clear Selection.
4
Select Domains 20–23 and 32–35 only.
5
Locate the Coil section. In the Icoil text field, type iB.
Reversed Current Direction 1
1
In the Model Builder window, expand the B phase winding node, then click Reversed Current Direction 1.
2
In the Settings window for Reversed Current Direction, locate the Domain Selection section.
3
Click  Clear Selection.
4
Select Domains 21, 22, 32, and 35 only.
C phase winding
1
In the Model Builder window, right-click B phase winding and choose Duplicate.
2
In the Settings window for Coil, type C phase winding in the Label text field.
3
Locate the Domain Selection section. Click  Clear Selection.
4
Select Domains 24–27 and 36–39 only.
5
Locate the Coil section. In the Icoil text field, type iC.
Reversed Current Direction 1
1
In the Model Builder window, expand the C phase winding node, then click Reversed Current Direction 1.
2
In the Settings window for Reversed Current Direction, locate the Domain Selection section.
3
Click  Clear Selection.
4
Select Domains 24, 27, 37, and 38 only.
In order to ensure zero net current flowing through magnets, Magnet features is added.
Magnet 1
1
In the Physics toolbar, click  Domains and choose Magnet.
2
In the Settings window for Magnet, locate the Domain Selection section.
3
From the Selection list, choose All magnets.
4
Locate the Magnet section. From the Pattern type list, choose Linear pattern (or domain index based).
5
From the Type of periodicity list, choose Alternating.
North 1
1
In the Model Builder window, click North 1.
2
Select Boundary 12 only.
South 1
1
In the Model Builder window, click South 1.
2
Select Boundary 11 only.
3
In the Model Builder window, collapse the Magnetic Fields (mf) node.
The default mesh is slightly refined in order to properly resolve the force harmonics appearing in the air gap.
Mesh 1
In the Model Builder window, under Component 1 (comp1) right-click Mesh 1 and choose Edit Physics-Induced Sequence.
Size 1 - periodic boundaries
1
In the Model Builder window, right-click Free Triangular 1 and choose Size.
2
In the Settings window for Size, type Size 1 - periodic boundaries in the Label text field.
3
Locate the Geometric Entity Selection section. From the Geometric entity level list, choose Boundary.
4
Select Boundaries 3, 5, 7, 64, 66, 68, and 70 only.
5
Locate the Element Size section. Click the Custom button.
6
Locate the Element Size Parameters section.
7
Select the Maximum element size checkbox. In the associated text field, type 2[mm].
Size 2 - magnetic steel
1
Right-click Free Triangular 1 and choose Size.
2
In the Settings window for Size, type Size 2 - magnetic steel in the Label text field.
3
Locate the Geometric Entity Selection section. From the Geometric entity level list, choose Domain.
4
From the Selection list, choose Magnetic Steel domains.
5
Locate the Element Size section. Click the Custom button.
6
Locate the Element Size Parameters section.
7
Select the Maximum element size checkbox. In the associated text field, type 2[mm].
Size 3 - airgap
1
Right-click Free Triangular 1 and choose Size.
2
In the Settings window for Size, type Size 3 - airgap in the Label text field.
3
Locate the Geometric Entity Selection section. From the Geometric entity level list, choose Domain.
4
Select Domain 15 only.
5
Locate the Element Size section. Click the Custom button.
6
Locate the Element Size Parameters section.
7
Select the Maximum element size checkbox. In the associated text field, type 0.5[mm].
8
Click  Build All.
Mesh 1
In the Model Builder window, collapse the Component 1 (comp1) > Mesh 1 node.
Add Study
1
In the Home toolbar, click  Add Study to open the Add Study window.
2
Go to the Add Study window.
3
Find the Studies subsection. In the Select Study tree, select General Studies > Stationary.
4
Click the Add Study button in the window toolbar.
5
In the Home toolbar, click  Add Study to close the Add Study window.
Study 1 - Current angle sweep
In the Settings window for Study, type Study 1 - Current angle sweep in the Label text field.
Step 1: Stationary
1
In the Model Builder window, under Study 1 - Current angle sweep click Step 1: Stationary.
2
In the Settings window for Stationary, click to expand the Study Extensions section.
3
Select the Auxiliary sweep checkbox.
4
Click  Add.
5
In the table, enter the following settings:
Parameter name
Parameter value list
Parameter unit
ang_el_init (Initial current angle (max force/ torque))
range(0,10,360)
deg
Study 1 - Current angle sweep
1
In the Model Builder window, collapse the Study 1 - Current angle sweep node.
2
In the Study toolbar, click  Compute.
Results
Probe Plot Group 1
While solving, click the Probe Plot 1 tab in the graphics window. Note the value of ang_el_init giving the maximum force and update the parameter value.
Global Definitions
Parameters - main
1
In the Model Builder window, under Global Definitions click Parameters - main.
2
In the Settings window for Parameters, locate the Parameters section.
3
In the table, enter the following settings:
Name
Expression
Value
Description
ang_el_init
90[deg]
1.5708 rad
Initial current angle (max force/ torque)
Add Study
1
In the Home toolbar, click  Add Study to open the Add Study window.
2
Go to the Add Study window.
3
Find the Studies subsection. In the Select Study tree, select General Studies > Stationary.
4
Click the Add Study button in the window toolbar.
5
In the Home toolbar, click  Add Study to close the Add Study window.
Study 2 - Transient
In the Settings window for Study, type Study 2 - Transient in the Label text field.
Step 2: Time Dependent
1
In the Study toolbar, click  Study Steps and choose Time Dependent > Time Dependent.
For the transient simulation, modify the default solver settings in order to properly resolve the harmonics to be investigated. In the following steps, let the solver know that 144 time steps per electrical period are needed, which corresponds to 12 steps for the 12th harmonic of the electrical frequency.
2
In the Settings window for Time Dependent, locate the Study Settings section.
3
In the Output times text field, type range(0,1/f_el/144,1/f_el).
Solution 2 (sol2)
1
In the Study toolbar, click  Show Default Solver.
2
In the Model Builder window, expand the Solution 2 (sol2) node.
3
In the Model Builder window, expand the Study 2 - Transient > Solver Configurations > Solution 2 (sol2) > Time-Dependent Solver 1 node, then click Fully Coupled 1.
4
In the Settings window for Fully Coupled, click to expand the Method and Termination section.
5
From the Jacobian update list, choose On every iteration.
Study 2 - Transient
1
In the Model Builder window, collapse the Study 2 - Transient node.
2
In the Study toolbar, click  Compute.
Results
Magnetic Flux Density (mf) 1
In the following part, make two duplicates of the surface plot and displace them to each side in order to reproduce the figure of magnetic flux density in the results section.
Surface 2
1
In the Model Builder window, expand the Magnetic Flux Density (mf) 1 node.
2
Right-click Results > Magnetic Flux Density (mf) 1 > Surface 1 and choose Duplicate.
3
In the Settings window for Surface, click to expand the Title section.
4
From the Title type list, choose None.
5
Locate the Coloring and Style section. From the Color table list, choose PrismDark.
6
Clear the Color legend checkbox.
Transformation 1
1
Right-click Surface 2 and choose Transformation.
2
In the Settings window for Transformation, locate the Transformation section.
3
In the x text field, type -arc_inc.
Surface 3
In the Model Builder window, under Results > Magnetic Flux Density (mf) 1 right-click Surface 2 and choose Duplicate.
Transformation 1
1
In the Model Builder window, expand the Surface 3 node, then click Transformation 1.
2
In the Settings window for Transformation, locate the Transformation section.
3
In the x text field, type arc_inc.
4
In the Magnetic Flux Density (mf) 1 toolbar, click  Plot.
Magnetic Flux Density (mf) 1
Next, create an Evaluation Group, in order to gather the results.
Results summary
1
In the Results toolbar, click  Evaluation Group.
2
In the Settings window for Evaluation Group, type Results summary in the Label text field.
3
Locate the Data section. From the Dataset list, choose Study 2 - Transient/Solution 2 (sol2).
4
Locate the Transformation section. Select the Transpose checkbox.
Surface Average - airgap
1
Right-click Results summary and choose Average > Surface Average.
2
In the Settings window for Surface Average, type Surface Average - airgap in the Label text field.
3
Locate the Selection section. From the Selection list, choose Aux torque calc domain.
4
Locate the Expressions section. In the table, enter the following settings:
Expression
Unit
Description
F_phi
Pa
Airgap shear stress
F_phi*arc_inc*L_mag
N
Linear force
F_phi*arc_inc*L_mag*r_inc
N*m
Torque (axial flux motor)
F_phi*arc_inc*L_mag*v_lin
W
Linear motion power
F_phi*arc_inc*L_mag*r_inc*s_rot*2*pi[rad]
W
Rotational motion power
5
Locate the Data Series Operation section. From the Transformation list, choose Average.
Global Evaluation - windings
1
In the Model Builder window, right-click Results summary and choose Global Evaluation.
2
In the Settings window for Global Evaluation, type Global Evaluation - windings in the Label text field.
Since all coil features differ only by phase offset you can simply multiply the result from a single coil by a factor of three when calculating average values.
3
Locate the Expressions section. In the table, enter the following settings:
Expression
Unit
Description
mf.PCoil_1*3
W
Electrical input power
mf.ICoil_1^2*mf.RCoil_1*3
W
Windings resistive loss
4
Locate the Data Series Operation section. From the Transformation list, choose Average.
Surface Integration - magnets
1
Right-click Results summary and choose Integration > Surface Integration.
2
In the Settings window for Surface Integration, type Surface Integration - magnets in the Label text field.
3
Locate the Selection section. From the Selection list, choose All magnets.
4
Click Replace Expression in the upper-right corner of the Expressions section. From the menu, choose Component 1 (comp1) > Magnetic Fields > Heating and losses > mf.Qrh - Volumetric loss density, electric - W/m³.
5
Locate the Expressions section. In the table, enter the following settings:
Expression
Unit
Description
mf.Qrh*L_mag
W
Magnets induced loss
6
Locate the Data Series Operation section. From the Transformation list, choose Average.
7
In the Results summary toolbar, click  Evaluate.
Linear force
1
In the Results toolbar, click  1D Plot Group.
2
In the Settings window for 1D Plot Group, type Linear force in the Label text field.
3
Locate the Data section. From the Dataset list, choose Study 2 - Transient/Solution 2 (sol2).
Global 1
1
Right-click Linear force and choose Global.
2
In the Settings window for Global, click Replace Expression in the upper-right corner of the y-Axis Data section. From the menu, choose Component 1 (comp1) > Definitions > Variables > Force - Linear Force (linear motor) - N.
3
In the Linear force toolbar, click  Plot.
Torque harmonics
1
In the Results toolbar, click  1D Plot Group.
2
In the Settings window for 1D Plot Group, type Torque harmonics in the Label text field.
3
Locate the Data section. From the Dataset list, choose None.
Table Graph 1
1
Right-click Torque harmonics and choose Table Graph.
When performing the Fourier transform, scale the x-axis to get the results as harmonics of the electrical frequency.
2
In the Settings window for Table Graph, locate the Data section.
3
From the x-axis data list, choose Time (s).
4
From the Plot columns list, choose Manual.
5
In the Columns list, select Torque (axial flux motor) (J).
6
From the Transformation list, choose Discrete Fourier transform.
7
From the Show list, choose Frequency spectrum.
8
Click to expand the Preprocessing section. Find the x-axis column subsection. From the Transformation list, choose Linear.
9
In the Scaling text field, type f_el.
10
Locate the Coloring and Style section. Find the Line style subsection. From the Line list, choose Dashed.
11
Find the Line markers subsection. From the Marker list, choose Square.
12
In the Torque harmonics toolbar, click  Plot.
Torque harmonics
1
In the Model Builder window, click Torque harmonics.
2
In the Settings window for 1D Plot Group, locate the Axis section.
3
Select the Manual axis limits checkbox.
4
In the x minimum text field, type -1.
5
In the x maximum text field, type 25.
6
In the y minimum text field, type -1.
7
In the y maximum text field, type 8.
8
Locate the Grid section. Select the Manual spacing checkbox.
9
In the Torque harmonics toolbar, click  Plot.