Home / Examples / Coupled Analysis / Transient Magnetic-Thermal Analysis [Luvens/Watt] / Example 1: Thermal Analysis of IPM Motor

Example 1: Thermal Analysis of IPM Motor


General

Analysis Conditions

Item

Settings

Solver

Magnetic Analysis [Luvens]

Thermal Analysis [Watt]

Analysis Type

Magnetic Analysis: Transient Analysis

Thermal Analysis: Steady-state Analysis

Unit

mm

Options

Select External Circuit Coupling.

Select Rotating Machinery.

 

[Conversion]

Model Thickness: 30×10-3 [m]

Select Partial Model.

Division Number: 4

[Conversion of external circuit I/O values]

Select Convert

Number of Series: 2

Number of Parallels: 2

Select Convert results to full model for output

 

The Rotating Machinery tab is set as follows.

Tab

Setting Item

Settings

Rotating Machinery

Rotational Move

Select Constant Velocity.

Number of Rotations: 1800 [r/min]

Rotor’s Initial Rotation Position: 0 [deg]

Number of Sliding Mesh Divisions

Circumferential Division Angle: 1.0 [deg]

Rotational Quantity per Step: 1 [mesh]

Number of Sliding Mesh Layers: 3

 

External circuit is as follows.

3-phase AC voltage of 60 [Hz] is applied.

 

Set the Mesh Tab as follows.

Tab

Setting Item

Settings

Mesh

Meshing Setup

Set the general mesh size automatically : Deselect

General Mesh Size: 4 [mm]

Ambient Air Creation

Select Create ambient air automatically.

Ambient Air Scale: 1.2

 

The Transient Analysis tab is set up as follows.

With the settings as below, number of calculation steps is 450, circumferential division angle is 1.0[deg], and rotational quantity per step is 1 [mesh], the rotation up to 450 degrees (=450*1.0*1) is analyzed.

The steps are set until the magnetic field reaches the steady state.

Tab

Setting Item

Settings

Transient Analysis

Timestep

Automatic

Table

Number

Calculation Steps

Output Interval

1

450

1

 

 

Fast stabilizer is set up as follows to make the magnetic field reach the steady state in short calculation time.

Tab

Setting Item

Settings

Fast Stabilizer

Correction Method

Simplified 3-Phase AC TP-EEC Method

Coil Name on the External Circuit

U Coil: Circuit_Coil1

V Coil: Circuit_Coil2

W Coil: Circuit_Coil3

Graphical Objects

A rotor core and magnet are placed in the center. A stator and coils are placed around them.

This is a 3D analysis of a symmetric quarter model.

Half period rotation boundary (symmetry) is set.

[Create ambient air automatically] is selected.

Adiabatic boundary condition is set on the shaft and the gap between stator and rotor.

Body Attributes and Materials

Body Number/Type

Body Attribute Name

Material Name

28/Solid

coil_1

Cu

34/Solid

coil_2

Cu

35/Solid

coil_3

Cu

36/Solid

coil_4

Cu

37/Solid

coil_5

Cu

38/Solid

coil_6

Cu

55/Solid

mag

mag

45/Solid

stator_core

core

47/Solid

rotor_core

core

 

The body attribute is set up as follows.

For the core, the homogenizing method is selected to simulate the layered steel plates.

Body Attribute Name

Tab

Settings

coil_1

Current

Waveform: External Circuit Coupling

Coil Name on the Circuit: Circuit_Coil1

Turns: 35 [Turns]

Direction: Specify Inflow/Outflow Faces

Stator/Rotor/Air

Stator

coil_2

Current

Waveform: External Circuit Coupling

Coil Name on the Circuit: Circuit_Coil1

Turns: 35 [Turns]

Direction: Specify Inflow/Outflow faces

Stator/Rotor/Air

Stator

coil_3

Current

Waveform: External Circuit Coupling

Coil Name on the Circuit: Circuit_Coil2

Turns: 35 [Turns]

Direction: Specify Inflow/Outflow faces

Stator/Rotor/Air

Stator

coil_4

Current

Waveform: External Circuit Coupling

Coil Name on the Circuit: Circuit_Coil2

Turns: 35 [Turns]

Direction: Specify Inflow/Outflow faces

Stator/Rotor/Air

Stator

coil_l5

Current

Waveform: External Circuit Coupling

Coil Name on the Circuit: Circuit_Coil3

Turns: 35 [Turns]

Direction: Specify Inflow/Outflow faces

Stator/Rotor/Air

Stator

coil_6

Current

Waveform: External Circuit Coupling

Coil Name on the Circuit: Circuit_Coil3

Turns: 35 [Turns]

Direction: Specify Inflow/Outflow faces

Stator/Rotor/Air

Stator

mag

Direction

Vector: X=1, Y=1, Z=0

Stator/Rotor/Air

Rotor

rotor_core

Layer

Select Take into account layer

Space Factor: 97 [%]

Layer Vector: X=0, Y=0, Z=1

Stator/Rotor/Air

Rotor

stator_core

Layer

Select Take layer into account

Space Factor: 97 [%]

Layer Vector: X=0, Y=0, Z=1

Stator/Rotor/Air

Stator

 

The material properties are set as follows.

Material Name

Tab

Properties

Cu

Conductivity

Conductivity Type: Conductor

Conductivity: 5.977x107 [S/m]

Thermal Conductivity

Thermal Conductivity: 398 [W/m/deg]

mag

Relative permeability

Material Type: Permanent Magnet

Magnet

Magnetization Characteristic Type: Linear

Magnetization Strength: 1.25

Relative Permeability: 1.05

Thermal Conductivity

Thermal Conductivity: 1 [W/m/deg]

core

Electric Conductivity

Conductivity Type: Conductor

Conductivity: 1.7 x106 [S/m]

Permeability

Magnetization Characteristic Type: Select B-H curve

  

B-H Curve Table

Magnetic Field [A/m]

Magnetic Flux Density [T]

0 0
58 0.42
90 0.8
180 1.19
380 1.37
1100 1.48
2000 1.55
3000 1.608
11000 1.81
20000 1.91

Thermal Conductivity

Thermal Conductivity: 10 [W/m/deg]

Boundary Conditions

[Natural convection (automatic coefficient calculation)] is set for the outer boundary condition (given to the surroundings of the motor in the case of the thermal analysis).

Half period symmetric boundary is set.

Adiabatic boundary condition is set on the shaft and the gap between stator and rotor.

Boundary Condition Name/Topology

Tab

Boundary Condition Type

Settings

Outer Boundary Condition *

Thermal

Heat transfer: Convection

Natural Convection (Automatic Coefficient Calculation)

Ambient Temperature: 25 [deg]

shaft

Thermal

Adiabatic

 

rotor

Thermal

Adiabatic

 

stator

Thermal

Adiabatic

 

Symmetry

Symmetry/Continuity

Periodic

Rotation Period (Half Period)

 

To set Outer Boundary Condition, go to the [Model] tab
 


 

and click [Outer Boundary Condition] .

Results

The distribution of the magnetic flux density at 450 calculation steps.

 

The diagram below shows time-torque characteristics.

Transient state becomes stable at around 20 [ms].

About 0.5[N*m] of torque is obtained.

 

The diagram below shows the temperature distribution of the stator.

In the steady state, it is around 100 [deg].