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International Journal of Electrical Engineering and Technology (IJEET), ISSN 0976 –
6545(Print), ISSN 0976 – 6553(Online) Volume 3, Issue 2, July- September (2012), © IAEME
457
DESIGN AND SIMULATION ANALYSIS OF OUTER STATOR INNER
ROTOR DFIG BY 2D AND 3D FINITE ELEMENT METHODS
H. Mellah‡
*, K. E. Hemsas*
LAS, Laboratoire d’Automatique de Sétif, Department of Electrical Engineering, Sétif 1university, Sétif,
Algeria.
‡
Corresponding Author;Mellah Hacen ,Department of electrical engineering, Faculty of Technologie University
Ferhat Abbas of Setif, Cité Maabouda, Route de Béjaia / 19000 / Algérie, 213 05 53 03 87 39,
mell_has@yahoo.fr
Abstract
In this paper, a time stepping 2D and 3D FEM is performed for modeling and analysis interior rotor DFIG .The
finite element method currently represents the state-of-the-art in the numerical magnetic field computation
relating to electrical machines. FEM is a numerical method to solve the partial differential equations (PDE) that
expresses the physical quantities of interest, in this case Maxwell’s equations. This will result in a more accurate
result compared to analytical modeling, which can be regarded as a simplification of the PDE. FEM analysis is
used for transient mode, magnetic field calculation, the magnetic flux density and vector potential of machine is
obtained. In this model we including, non linear material characteristics, eddy current effect, torque-speed
characteristics, ambient temperature effect and magnetic analysis are investigated.
Keywords- Modelling, DFIG, FEM, Wind Turbines, Energy.
1. Introduction
There is now general acceptance that the burning of fossil fuels is having a significant
influence on the global climate. Effective mitigation of climate change will require deep
reductions in greenhouse gas emissions, with UK estimates of a 60–80% cut being necessary
by 2050 [1], Still purer with the nuclear power, this last leaves behind dangerous wastes for
thousands of years and risks contamination of land, air, and water[2]; the catastrophe of
Japan is not far. Wind power can contribute to fulfilling several of the national environmental
quality objectives decided by Parliament in 1991. Continued expansion of wind power is
therefore of strategic importance [3], hence, the energy policy decision states that the
objective is to facilitate a change to an ecologically sustainable energy production system [3],
as example the Swedish Parliament adopted new energy guidelines in 1997 following the
trend of moving towards an ecologically sustainable society. The decision also confirmed that
INTERNATIONAL JOURNAL OF ELECTRICAL ENGINEERING &
TECHNOLOGY (IJEET)
ISSN 0976 – 6545(Print)
ISSN 0976 – 6553(Online)
Volume 3, Issue 2, July – September (2012), pp. 457-470
© IAEME: www.iaeme.com/ijeet.html
Journal Impact Factor (2012): 3.2031 (Calculated by GISI)
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IJEET
© I A E M E
International Journal of Electrical Engineering and Technology (IJEET), ISSN 0976 –
6545(Print), ISSN 0976 – 6553(Online) Volume 3, Issue 2, July- September (2012), © IAEME
458
the 1980 and 1991 guidelines still apply, i.e., that the nuclear power production is to be
phased out at a slow rate so that the need for electrical can be met without risking
employment and welfare. The first nuclear reactor of Barseback was shut down 30th of
November 1999. Nuclear power production shall be replaced by improving the efficiency of
electricity use, conversion to renewable forms of energy and other environmentally
acceptable electricity production technologies [3]. On the individual scale in Denmark Poul la
Cour, who was among the first to connect a windmill to a generator [4]. In real wind power
market, three types of wind power system for large wind turbines exit. The first type is fixed-
speed wind power (SCIG), directly connected to the grid. The second one is a variable speed
wind system using a DFIG or SCIG. The third type is also a variable speed wind turbine,
PMSG [5]. One can noticed two problems of PMSG used in wind power. First is the inherent
cogging torque due to magnet materials naturally attractive force. This kind of torque is bad
for operation, especially stopping wind turbine starting and making noise and vibration in
regular operation. The other one is the risk of demagnetization because of fault happening
and overheating of magnets. This risk is very dangerous and the cost for replacing bad
magnets is much higher than the generator itself [5].There are several reasons for using
variable-speed operation of wind turbines; the advantages are reduced mechanical stress and
optimized power capture. Speed variability is possible due to the AC–DC–AC converter in
the rotor circuit required to produce rotor voltage at slip frequency. Using a back-to-back
converter allows bidirectional power flows and hence operation at both sub- and super-
synchronous speeds. Formulating the control algorithm of the converters in a synchronously
rotating frame allows for effective control of the generator speed (or active power) and
terminal voltage [6]. Without forgotten the second major advantage of the DFIG, which has
made it popular, is that the power electronic equipment only has to handle a fraction (20–
30%) of the total system power [3]. This means that the losses in the power electronic
equipment can be reduced in comparison to power electronic equipment that has to handle the
total system power as for a direct-driven synchronous generator, apart from the cost saving of
using a smaller converter.
2. Review of Related Research
The development of modern wind power conversion technology has been going on since
1970s, and the rapid development has been seen from 1990s. Various wind turbine concepts
have been developed and different wind generators have been built [7]. The average annual
growth rate of wind turbine installation is around 30% during last ten years [8].
At the end of 2006, the global wind electricity generating capacity increased to 74223
MW from 59091 MW in 2005. By the end of 2020, it is expected that this will have increased
to well over 1260000 MW, which will be sufficient for 12% of the world’s electricity
consumption [7-8]. Fig. 1 depicts the total wind power installed capacity for some countries
from 1985 to 2006. The countries with the highest total installed capacity are Germany (20
622 MW), Spain (11 615 MW), the USA (11 603 MW), India (6270 MW) and Denmark
(3136 MW) [7-8].
In addition, the Global Wind Energy Council (GWEC) results, Europe continues to lead
the market with 48,545 MW of installed capacity at the end of 2006, representing 65 % of the
global total installation. The European Wind Energy Association (EWEA) has set a target of
satisfying 23% European electricity needs with wind energy by 2030. It is clear that the
global market for the electrical power produced by wind turbines has been increasing
steadily, which directly pushes the wind generation technology into a more competitive area
[8-7].
International Journal of Electrical Engineering and Technology (IJEET), ISSN 0976 –
6545(Print), ISSN 0976 – 6553(Online) Volume 3, Issue 2, July- September (2012), © IAEME
459
The energy production can be increased by 2–6% for a variable-speed wind turbine in
comparison to a fixed-speed wind turbine, while in it is stated that the increase in energy can
be 39% [3]. The gain in energy generation of the variable-speed wind turbine compared to the
most simple fixed-speed wind turbine can vary between 3–28% depending on the site
conditions and design parameters. Efficiency calculations of the DFIG system have been
presented in several papers [3]. A comparison to other electrical systems for wind turbines
are, however, harder to find. One exception presented is in [3], where Datta et al. have made
a comparison of the energy capture for various WT systems. The energy capture can be
significantly increased by using a DFIG. They state an increased energy capture of a DFIG by
over 20% with respect to a variable-speed system using a cage-bar induction machine and by
over 60% in comparison to a fixed-speed system. One of the reasons for the various results is
that the assumptions used vary from investigation to investigation. Factors such as speed
control of variable-speed WTs, blade design, what kind of power that should be used as a
common basis for comparison, selection of maximum speed of the WT, selected blade
profile, missing facts regarding the base assumptions etc, affect the outcome of the
investigations. There is thus a need to clarify what kind of energy capture gain there could be
when using a DFIG WT, both compared to another variable-speed WT and towards a
traditional fixed-speed WT [3].
3. DFIG discription
Doubly-fed induction generators (DFIGs) are widely used in wind power systems. A
DFIG works as a component of a wind power system, as shown below, where the wind
turbine transforms wind energy into mechanical energy, and the DFIG transforms mechanical
energy into electrical energy. For a DFIG, both the stator and the rotor are equipped with
poly-phase AC windings. The stator and rotor windings may, or may not, have the same
number of phases, but they must have the same number of poles p [9].
A DFIG system can deliver power to the grid through the stator and rotor, while the rotor
can also absorb power. This depends on the rotational speed of the generator. If the generator
operates above synchronous speed, power will be delivered from the rotor through the
converters to the network, and if the generator operates below synchronous speed, then the
rotor will absorb power from the network through the converters [1].
Fig. 1. Total cumulative wind power installed capacity for different countries (1980–2006)
International Journal of Electrical Engineering and Technology (IJEET), ISSN 0976 –
6545(Print), ISSN 0976 – 6553(Online) Volume 3, Issue 2, July- September (2012), © IAEME
460
Fig. 2. Typical configuration of a DFIG wind turbine
In order to produce terminal voltages with desired frequency f in the stator winding, the
rotor winding must be excited by balanced poly-phase currents with the slip frequency Sf via
an AC-DC-AC convert. Slip s is defined as [9]:
0
1 (1 )- /s n n=
Where n is the rotor speed, and n0 is the synchronous speed as given below:
0
6 0 ( 2 )/f pn =
When the rotor speed is lower than the synchronous speed, the rotor currents have the
same phase sequence as the stator currents, and the rotor winding gets power from the
converter. However, when the rotor speed is higher than the synchronous speed, the phase
sequence of the rotor currents is different from that of the stator currents, and the rotor
winding outputs power to the converter [1-9].
For a given wind turbine, the power coefficient (the ratio of turbine power to the wind
power), is a function of the tip speed ratio (the ratio of the blade tip speed to the wind speed).
In order to track the maximum power point, the tip speed ratio must keep constant - at its
optimal value. The input mechanical power with Maximum Power Point Tracking (MPPT)
must satisfy [9]:
3
_ e( / ) (3)m ech m ref m r fP P ω ω=
Where Pm_ref is the turbine power with MPPT at a reference speed of ωref based on the
optimal tip speed ratio, and ωm is the rotor speed in rad/s. The rotor mechanical loss is:
3
_ e
(4)( / )f f ref m r f
P P ω ω=
Where Pf_ref is mechanical loss measured at a reference speed of ωref .The electro-
magnetic power in the air gap is:
( ) / (1 ) (5)em m ech f
P P P s= − −
Therefore, the stator output electrical power at rated operation is:
2
1 1 1 1 1 1 1
cos (6)em
P P m I R m V I ϕ= − =
where m1 is the number of phases of the stator winding, R1 is the stator phase resistance,
V1 is the stator rated phase voltage, I1 is the rated stator phase current to be determined, and
cos ߮ is the rated power factor. Solving for I1, one obtains:
1
1
2
1 1 1 1
(7 )
2 /
co s ( co s ) 4 /
em
em
P m
I
V V R P mϕ ϕ
=
+ +
International Journal of Electrical Engineering and Technology (IJEET), ISSN 0976 –
6545(Print), ISSN 0976 – 6553(Online) Volume 3, Issue 2, July- September (2012), © IAEME
461
Then, based on the equivalent circuit shown below, one obtains:
Fig. 3. DFIG equivalent circuit
Now, rotor input electrical power can be computed as:
2
2 2 2 2 ( 8 )e mP s P m I R= +
Where m2 is the number of phases of the rotor winding.
The electromagnetic torque Tem is:
( 9 )/e m e m
T P ω=
Where ω? denotes the synchronous speed in rad/s.
The input mechanical torque on the shaft is:
(1 0 )m e c h e m f
T T T= +
Where Tf denotes the frictional torque.
The total electrical output power is:
1 2
(1 1 )e le c F e
P P P P= − −
Where pFe is the core loss. The efficiency is defined as:
( 1 2 )1 0 0 %e l e c
m e c h
P
P
η =
4. Geometric Dimention And Parameters Design Of Dfig Studie
The operation principle of electric machines is based on the interaction between the
magnetic fields and the currents flowing in the windings of the machine. Rotational Machine
Expert (RMxprt) is an interactive software package used for designing and analyzing
electrical machines, is a module of Ansoft Maxwell 12.1 [10]. The structure of coil
connection is shown in Fig. 4, Fig. 5, and the 3D geometries of the generator are shown in
Fig. 6
Fig. 4. Stator and coil structure of the designed generator
V2S
International Journal of Electrical Engineering and Technology (IJEET), ISSN 0976 –
6545(Print), ISSN 0976 – 6553(Online) Volume 3, Issue 2, July- September (2012), © IAEME
462
Table 1. Stator and rotor slot parameters
Stator Slot Parameter Rotor Slots Parameter
hs0 (mm): 2 hr0 (mm): 2
hs1 (mm): 2 hr1 (mm): 2
hs2 (mm): 10 hr2 (mm): 15
bs0 (mm): 2.5 br0 (mm): 2.5
bs1 (mm): 8.52819 br1 (mm): 9.19419
bs2 (mm): 10.6303 br2 (mm): 5.24462
rs (mm) : 2 rr (mm) : 2
Fig. 5. Slot type
Table 2. SOME RATED VALUES, GEOMETRIC PARAMETERS OF THE DESIGNED MACHINES
Somme Electrical And Dimensional Parameters Value
Rated output power (kW) 0.55
Rated voltage (V) 220
Given rated speed (rpm) 1500
Number of poles 4
Outer diameter of stator (mm) 180
Inner diameter of stator (mm) 121
Number of stator slots 30
Outer diameter of rotor (mm) 120
Inner diameter of rotor (mm) 50
Number of stator slots 24
Length of stator core (rotor) (mm) 65
Stacking factor of stator core 0.97
Stacking factor of iron core 0.97
Frictional loss (W) 12
Operating temperature (0
C) 75
Fig. 6. 3D view of the DFIG inner rotor designed
5. Simulation Results
The finite element model is created. First, the geometric outlines are drawn, which is
similar to the available mechanical engineering packages. Then, material properties are
assigned to the various regions of the model. Next, the current sources and the boundary
conditions are applied to the model. Finally, the finite element mesh is created. In the solver
part, the finite element solution is conducted [10]. The FEA model of electromagnetic field is
built by Maxwel12D; in this case the total number of mesh element is 9336.
International Journal of Electrical Engineering and Technology (IJEET), ISSN 0976 –
6545(Print), ISSN 0976 – 6553(Online) Volume 3, Issue 2, July- September (2012), © IAEME
463
Fig. 7. 2D DFIG inner rotor mesh
A. Efficiency of DFIG at variable environmental thermal condition
The DFIG performance is obtained, by considering a variable ambient temperature, Fig 8.
Show the influences of environmental thermal condition on efficiency, the increase in the
ambient temperature, so the DFIG losses increase, thus the efficiency decreases.
0.00 500.00 1000.00 1500.00 2000.00 2500.00 3000.00
RSpeed [rpm ]
-100.00
-75.00
-50.00
-25.00
0.00
25.00
50.00
75.00
100.00
Y1[fraction]
RMxprtDesign1Percentage ANSOFT
Curve Info
Efficiency
Setup1 : Performance
Efficiency_1
Setup2 : Performance
Efficiency_2
Setup3 : Performance
Efficiency_3
Setup4 : Performance
Efficiency_4
Setup5 : Performance
Efficiency_5
Setup6 : Performance
Efficiency_6
Setup7 : Performance
Efficiency_7
Setup8 : Performance
Efficiency_8
Setup9 : Performance
Efficiency_9
Setup10 : Performance
a.Percentage (efficiency) variation at different thermal condition
1000.00 1500.00 2000.00 2500.00 3000.00
RSpeed [rpm]
62.67
65.00
70.00
75.00
80.00
85.00
88.96
Y1[fraction]
RMxprtDesign1Percentage ANSOFT
Curve Info
Efficiency
Setup1 : Perf ormance
Efficiency_1
Setup2 : Perf ormance
Efficiency_2
Setup3 : Perf ormance
Efficiency_3
Setup4 : Perf ormance
Efficiency_4
Setup5 : Perf ormance
Efficiency_5
Setup6 : Perf ormance
Efficiency_6
Setup7 : Perf ormance
Efficiency_7
Setup8 : Perf ormance
Efficiency_8
Setup9 : Perf ormance
Efficiency_9
Setup10 : Performance
b. ZOOM
Fig. 8. Percentage (efficiency) variation at different thermal condition
B. DFIG modelisation results by 2D finite element method
One considers a DFIG connected an infinite bus, the grid frequency is 50Hz, and turns at
constant speed 1660rpm.
International Journal of Electrical Engineering and Technology (IJEET), ISSN 0976 –
6545(Print), ISSN 0976 – 6553(Online) Volume 3, Issue 2, July- September (2012), © IAEME
464
Fig. 9 show the torque variation, the torque value in steady state is -3.5 Nm.
0.00 100.00 200.00 300.00 400.00 500.00
Time [ms]
-8.00
-7.00
-6.00
-5.00
-4.00
-3.00
-2.00
-1.00
0.00
Moving1.Torque[NewtonMeter]
Maxwell2DDesign1Torque ANSOFT
Curve Info
Moving1.Torque
Setup1 : Transient
Fig. 9. Torque in DFIG inner rotors
Fig. 10 illustrates the stator and rotor flux linkage of DFIG, when in study state the first
one value is 0.6wb and the second is 0.2wb.
0.00 100.00 200.00 300.00 400.00 500.00
Time [ms]
-1.25
-1.00
-0.75
-0.50
-0.25
0.00
0.25
0.50
0.75
1.00
Y1[Wb]
Maxwell2DDesign1Winding_1 ANSOFT
Curve Info
FluxLinkage(PhaseA)
Setup1 : Transient
FluxLinkage(PhaseB)
Setup1 : Transient
FluxLinkage(PhaseC)
Setup1 : Transient
FluxLinkage(PhaseU)
Setup1 : Transient
FluxLinkage(PhaseV)
Setup1 : Transient
FluxLinkage(PhaseW)
Setup1 : Transient
Fig. 10. DFIG stator and rotor flux linkage
The DFIG stator current winding is shown in Fig. 11, the magnitude is 2A and the
frequency is 50Hz, The frequency equal has 50 Hz by what the speed (mechanical) east notes.
0.00 100.00 200.00 300.00 400.00 500.00
Time [ms]
-8.00
-6.00
-4.00
-2.00
0.00
2.00
4.00
6.00
Y1[A]
Maxwell2DDesign1Stator Currents ANSOFT
Curve Info
Current(PhaseA)
Setup1 : Transient
Current(PhaseB)
Setup1 : Transient
Current(PhaseC)
Setup1 : Transient
Fig. 11. DFIG stator current winding
There are two types of stranded loss quantities, StrandedLoss and StrandedLossR [9]:
• StrandedLoss represents the resistive loss in a 2D or 3D volume and is calculated by:
21
=
vol
Solid Loss J
σ
∫ (13)
Where J is the conductivity of the material.
International Journal of Electrical Engineering and Technology (IJEET), ISSN 0976 –
6545(Print), ISSN 0976 – 6553(Online) Volume 3, Issue 2, July- September (2012), © IAEME
465
•StrandedLossR represents the loss based on I2 times the resistance R.
Fig. 12 illustrates the two types of loss, when the value of StrandedLoss in transient state
is 355w and stabilized at 24w in steady-state, but the StrandedLossR is constant at 14.3w.
0.00 100.00 200.00 300.00 400.00 500.00
Time [ms]
0.00
125.00
250.00
355.00
Y1[W]
Maxwell2DDesign1Loss ANSOFT
Curve Info
StrandedLoss
Setup1 : Transient
StrandedLossR
Setup1 : Transient
Fig. 12. DFIG StrandedLoss and StrandedLossR
Fig. 13 shows the DFIG stator and rotor induced voltage, when the value of stator is
185v, but the value of rotor induced voltage is 8v.
0.00 100.00 200.00 300.00 400.00 500.00
Time [ms]
-200.00
-150.00
-100.00
-50.00
0.00
50.00
100.00
150.00
200.00
Y3[V]
Maxwell2DDesign1InducedVoltage ANSOFT
Curve Info
InducedVoltage(PhaseA)
Setup1 : Transient
InducedVoltage(PhaseB)
Setup1 : Transient
InducedVoltage(PhaseC)
Setup1 : Transient
InducedVoltage(PhaseU)
Setup1 : Transient
InducedVoltage(PhaseV)
Setup1 : Transient
InducedVoltage(PhaseW)
Setup1 : Transient
Fig. 13. DFIG stator and rotor induced voltage
Fig.14 show DFIG stator winding current spectrum, one does not find the harmonic by
that the current operate and purely sinusoidal.
0.00 0.01 0.10 1.00 10.00
Freq [kHz]
0.00
0.20
0.40
0.60
0.80
1.00
1.20
mag(Current(PhaseA))[A]
Maxwell2DDesign1XY Plot 1 ANSOFT
Curve Info
mag(Current(PhaseA))
Setup1 : Transient
Fig. 14. DFIG stator winding current spectrum
International Journal of Electrical Engineering and Technology (IJEET), ISSN 0976 –
6545(Print), ISSN 0976 – 6553(Online) Volume 3, Issue 2, July- September (2012), © IAEME
466
0.00 100.00 200.00 300.00 400.00 500.00
Time [ms]
-8.00
-6.00
-4.00
-2.00
0.00
2.00
4.00
6.00
8.00
Y1[A]
-200.00
-150.00
-100.00
-50.00
0.00
50.00
100.00
150.00
200.00
Y3[V]
Maxwell2DDesign1InputCurrent ANSOFT
Curve Info Y Axis
InputCurrent(PhaseU)
Setup1 : Transient
Y1
InputCurrent(PhaseV)
Setup1 : Transient
Y1
InputCurrent(PhaseW)
Setup1 : Transient
Y1
InputVoltage(PhaseA)
Setup1 : Transient
Y3
InputVoltage(PhaseB)
Setup1 : Transient
Y3
InputVoltage(PhaseC)
Setup1 : Transient
Y3
Fig. 15. Rotor current and stator voltage of DFIG
Fig. 15 shows the rotor current and stator voltage of DFIG, the magnitude and the
frequency of the first one is 9.5A is ≈5Hz, and the second one is 180v is 50Hz respectively.
C. Field results in 2D of the elemnt finits model
The FEA model of electromagnetic field is built by Maxwell2D, the flux, flux density,
field intensity.
Fig. 16. Flux distribution of DFIG at 0.5s
The Fig.16 indicates the flux line distribution of the DFIG at 0.5s.
It is important to note that in order to obtain accurate results, the triangular mesh elements
assigned to the airgap should have an aspect ratio close to one. A large aspect ratio between
the sides of a triangular element will result in accurate computation of the flux density and
hence the electromagnetic torque.
Fig 17 shows the DFIG’s flux density distribution at 0.5s, the maximum value of flux
density is 1.47T.
Fig. 17. flux density of DFIG at 0.5s
International Journal of Electrical Engineering and Technology (IJEET), ISSN 0976 –
6545(Print), ISSN 0976 – 6553(Online) Volume 3, Issue 2, July- September (2012), © IAEME
467
Fig.18 indicates the vector diagram and contours diagram of flux density at 0.5s.
Fig. 18. Contours and vector diagrams of flux density in DFIG
According to Fig. 18 and Fig. 16, the flux line and magnetic field are symmetrical in the
whole machine and the distribution regularities of flux line and magnetic field are the same.
The total loss of DFIG is illustrated in fig19, when the winding losses have a great
contribution.
Fig. 19. Total Loss of DFIG
D. Field results in 3D of the finite element model
The 3D FEA model of electromagnetic field is built by Maxwell 3D, this simulation is
obtained by Terra pc (QuadroFX380, i7 CPU, 3.07 GHZ, 8 CPU and 4G RAM). Our model
of DFIG used in Maxwell 3D environment has 98586 number of mesh element. The largest
saving in computation time is made by doing the simulation in 2D instead of 3D. The analyze
will be fairly limited due to the large increase in simulation time, approximately 4 minutes
per time step compared to 5 seconds for a corresponding 2D model. In our application the
simulation rest in execution during some day.
International Journal of Electrical Engineering and Technology (IJEET), ISSN 0976 –
6545(Print), ISSN 0976 – 6553(Online) Volume 3, Issue 2, July- September (2012), © IAEME
468
Fig. 20. 3D DFIG inner rotor mesh
Fig 20 shows the 3D DFIG’s flux density distribution at 0.4s, the maximum value of flux
density is 1.59T. According to Fig. 17 and Fig. 21, the maximum value of flux density
obtained by 3D model is bigger than in 2D,
Fig. 21. 3D flux density of DFIG at 0.4s
Fig. 22. 3D vector diagram of flux density of DFIG at 0.4s
Fig.23 indicates the 3D vector diagram of flux density at 0.4s.
International Journal of Electrical Engineering and Technology (IJEET), ISSN 0976 –
6545(Print), ISSN 0976 – 6553(Online) Volume 3, Issue 2, July- September (2012), © IAEME
469
Fig. 23. 3D current density of DFIG at 0.4s
Fig.24 shows the 3D total loss of DFIG at 0.4s.
Fig. 24. 3D Total loss of DFIG inner rotor
6. Conclusion
Finite element analysis (FEA) is a frequently used method for analysis of
electromechanical converters. As a numerical analysis method, FEA allows for including any
practical material, external excitation (voltage driven or current driven), inclusion of motion,
and nonlinear effects such as magnetic saturation and eddy current effects.
A 2D model of the DFIG inner rotor is given, solved, some simulation result is given and
commented, to return our simulation results finer a 3D model is developed and solved, but
the resolution time is very large, this time is a scale of the days.
This model 2D and 3D obtained by using Ansoft finite element software, this last can be
used as an effective way to design and calculate the DFIG performance. This work is the
necessary preparations for design and development high reliability and high security of DFIG
applications.
References
[1] AL. Olimpo, J. Nick, E. Janaka, C. Phill and H Mike,Wind Energy Generation Modelling and Control, John
Wiley & Sons, Ltd 2009.
[2] Ian woofenden, wind power for dummies, Wiley Publishing, 2009.
[3] A. Petersson, Analysis, Modeling and Control of Doubly-Fed Induction Generators for Wind Turbines, phd
thesis, chalmers university of technology,GÖteborg, Sweden 2005.
[4] Martin O. L. Hansen, Aerodynamics of Wind Turbines, Earthscan in the UK and USA in 2008.
[5] Zongxi Fang ,Permanent magnet machine topologies for wind power generation,university of Sheffield
2010.
International Journal of Electrical Engineering and Technology (IJEET), ISSN 0976 –
6545(Print), ISSN 0976 – 6553(Online) Volume 3, Issue 2, July- September (2012), © IAEME
470
[6] B.C. Pal F. Mei, Modelling adequacy of the doubly fed induction generator for small-signal stability studies
in power systems, IET Renewable Power Generation 2008.
[7] H. Li, Z. Chen, Overview of different wind generator systems and their comparisons, Renewable Power
Generation, IET 2007.
[8] H. Li1, Z. Chen, Henk Polinder, research report on models for numerical evaluation of variable speed
different wind generator systems, Integrating and strengthening the European Research Area, 2002-2006.
[9] Help of Ansoft Maxwell V12®, Ansoft Corporation 2010.
[10] H. Mellah, K.E Hemsas, Dynamic design and simulation analysis of permanent magnet motor in
different scenario of fed alimentation, conference international on automatique and mécatronique, novembre
22 -23, 2011, usto, oran, Algeria.

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Design and Simulation Analysis of Outer Stator Inner Rotor DFIG by 2d and 3d Finite Element Methods

  • 1. International Journal of Electrical Engineering and Technology (IJEET), ISSN 0976 – 6545(Print), ISSN 0976 – 6553(Online) Volume 3, Issue 2, July- September (2012), © IAEME 457 DESIGN AND SIMULATION ANALYSIS OF OUTER STATOR INNER ROTOR DFIG BY 2D AND 3D FINITE ELEMENT METHODS H. Mellah‡ *, K. E. Hemsas* LAS, Laboratoire d’Automatique de Sétif, Department of Electrical Engineering, Sétif 1university, Sétif, Algeria. ‡ Corresponding Author;Mellah Hacen ,Department of electrical engineering, Faculty of Technologie University Ferhat Abbas of Setif, Cité Maabouda, Route de Béjaia / 19000 / Algérie, 213 05 53 03 87 39, mell_has@yahoo.fr Abstract In this paper, a time stepping 2D and 3D FEM is performed for modeling and analysis interior rotor DFIG .The finite element method currently represents the state-of-the-art in the numerical magnetic field computation relating to electrical machines. FEM is a numerical method to solve the partial differential equations (PDE) that expresses the physical quantities of interest, in this case Maxwell’s equations. This will result in a more accurate result compared to analytical modeling, which can be regarded as a simplification of the PDE. FEM analysis is used for transient mode, magnetic field calculation, the magnetic flux density and vector potential of machine is obtained. In this model we including, non linear material characteristics, eddy current effect, torque-speed characteristics, ambient temperature effect and magnetic analysis are investigated. Keywords- Modelling, DFIG, FEM, Wind Turbines, Energy. 1. Introduction There is now general acceptance that the burning of fossil fuels is having a significant influence on the global climate. Effective mitigation of climate change will require deep reductions in greenhouse gas emissions, with UK estimates of a 60–80% cut being necessary by 2050 [1], Still purer with the nuclear power, this last leaves behind dangerous wastes for thousands of years and risks contamination of land, air, and water[2]; the catastrophe of Japan is not far. Wind power can contribute to fulfilling several of the national environmental quality objectives decided by Parliament in 1991. Continued expansion of wind power is therefore of strategic importance [3], hence, the energy policy decision states that the objective is to facilitate a change to an ecologically sustainable energy production system [3], as example the Swedish Parliament adopted new energy guidelines in 1997 following the trend of moving towards an ecologically sustainable society. The decision also confirmed that INTERNATIONAL JOURNAL OF ELECTRICAL ENGINEERING & TECHNOLOGY (IJEET) ISSN 0976 – 6545(Print) ISSN 0976 – 6553(Online) Volume 3, Issue 2, July – September (2012), pp. 457-470 © IAEME: www.iaeme.com/ijeet.html Journal Impact Factor (2012): 3.2031 (Calculated by GISI) www.jifactor.com IJEET © I A E M E
  • 2. International Journal of Electrical Engineering and Technology (IJEET), ISSN 0976 – 6545(Print), ISSN 0976 – 6553(Online) Volume 3, Issue 2, July- September (2012), © IAEME 458 the 1980 and 1991 guidelines still apply, i.e., that the nuclear power production is to be phased out at a slow rate so that the need for electrical can be met without risking employment and welfare. The first nuclear reactor of Barseback was shut down 30th of November 1999. Nuclear power production shall be replaced by improving the efficiency of electricity use, conversion to renewable forms of energy and other environmentally acceptable electricity production technologies [3]. On the individual scale in Denmark Poul la Cour, who was among the first to connect a windmill to a generator [4]. In real wind power market, three types of wind power system for large wind turbines exit. The first type is fixed- speed wind power (SCIG), directly connected to the grid. The second one is a variable speed wind system using a DFIG or SCIG. The third type is also a variable speed wind turbine, PMSG [5]. One can noticed two problems of PMSG used in wind power. First is the inherent cogging torque due to magnet materials naturally attractive force. This kind of torque is bad for operation, especially stopping wind turbine starting and making noise and vibration in regular operation. The other one is the risk of demagnetization because of fault happening and overheating of magnets. This risk is very dangerous and the cost for replacing bad magnets is much higher than the generator itself [5].There are several reasons for using variable-speed operation of wind turbines; the advantages are reduced mechanical stress and optimized power capture. Speed variability is possible due to the AC–DC–AC converter in the rotor circuit required to produce rotor voltage at slip frequency. Using a back-to-back converter allows bidirectional power flows and hence operation at both sub- and super- synchronous speeds. Formulating the control algorithm of the converters in a synchronously rotating frame allows for effective control of the generator speed (or active power) and terminal voltage [6]. Without forgotten the second major advantage of the DFIG, which has made it popular, is that the power electronic equipment only has to handle a fraction (20– 30%) of the total system power [3]. This means that the losses in the power electronic equipment can be reduced in comparison to power electronic equipment that has to handle the total system power as for a direct-driven synchronous generator, apart from the cost saving of using a smaller converter. 2. Review of Related Research The development of modern wind power conversion technology has been going on since 1970s, and the rapid development has been seen from 1990s. Various wind turbine concepts have been developed and different wind generators have been built [7]. The average annual growth rate of wind turbine installation is around 30% during last ten years [8]. At the end of 2006, the global wind electricity generating capacity increased to 74223 MW from 59091 MW in 2005. By the end of 2020, it is expected that this will have increased to well over 1260000 MW, which will be sufficient for 12% of the world’s electricity consumption [7-8]. Fig. 1 depicts the total wind power installed capacity for some countries from 1985 to 2006. The countries with the highest total installed capacity are Germany (20 622 MW), Spain (11 615 MW), the USA (11 603 MW), India (6270 MW) and Denmark (3136 MW) [7-8]. In addition, the Global Wind Energy Council (GWEC) results, Europe continues to lead the market with 48,545 MW of installed capacity at the end of 2006, representing 65 % of the global total installation. The European Wind Energy Association (EWEA) has set a target of satisfying 23% European electricity needs with wind energy by 2030. It is clear that the global market for the electrical power produced by wind turbines has been increasing steadily, which directly pushes the wind generation technology into a more competitive area [8-7].
  • 3. International Journal of Electrical Engineering and Technology (IJEET), ISSN 0976 – 6545(Print), ISSN 0976 – 6553(Online) Volume 3, Issue 2, July- September (2012), © IAEME 459 The energy production can be increased by 2–6% for a variable-speed wind turbine in comparison to a fixed-speed wind turbine, while in it is stated that the increase in energy can be 39% [3]. The gain in energy generation of the variable-speed wind turbine compared to the most simple fixed-speed wind turbine can vary between 3–28% depending on the site conditions and design parameters. Efficiency calculations of the DFIG system have been presented in several papers [3]. A comparison to other electrical systems for wind turbines are, however, harder to find. One exception presented is in [3], where Datta et al. have made a comparison of the energy capture for various WT systems. The energy capture can be significantly increased by using a DFIG. They state an increased energy capture of a DFIG by over 20% with respect to a variable-speed system using a cage-bar induction machine and by over 60% in comparison to a fixed-speed system. One of the reasons for the various results is that the assumptions used vary from investigation to investigation. Factors such as speed control of variable-speed WTs, blade design, what kind of power that should be used as a common basis for comparison, selection of maximum speed of the WT, selected blade profile, missing facts regarding the base assumptions etc, affect the outcome of the investigations. There is thus a need to clarify what kind of energy capture gain there could be when using a DFIG WT, both compared to another variable-speed WT and towards a traditional fixed-speed WT [3]. 3. DFIG discription Doubly-fed induction generators (DFIGs) are widely used in wind power systems. A DFIG works as a component of a wind power system, as shown below, where the wind turbine transforms wind energy into mechanical energy, and the DFIG transforms mechanical energy into electrical energy. For a DFIG, both the stator and the rotor are equipped with poly-phase AC windings. The stator and rotor windings may, or may not, have the same number of phases, but they must have the same number of poles p [9]. A DFIG system can deliver power to the grid through the stator and rotor, while the rotor can also absorb power. This depends on the rotational speed of the generator. If the generator operates above synchronous speed, power will be delivered from the rotor through the converters to the network, and if the generator operates below synchronous speed, then the rotor will absorb power from the network through the converters [1]. Fig. 1. Total cumulative wind power installed capacity for different countries (1980–2006)
  • 4. International Journal of Electrical Engineering and Technology (IJEET), ISSN 0976 – 6545(Print), ISSN 0976 – 6553(Online) Volume 3, Issue 2, July- September (2012), © IAEME 460 Fig. 2. Typical configuration of a DFIG wind turbine In order to produce terminal voltages with desired frequency f in the stator winding, the rotor winding must be excited by balanced poly-phase currents with the slip frequency Sf via an AC-DC-AC convert. Slip s is defined as [9]: 0 1 (1 )- /s n n= Where n is the rotor speed, and n0 is the synchronous speed as given below: 0 6 0 ( 2 )/f pn = When the rotor speed is lower than the synchronous speed, the rotor currents have the same phase sequence as the stator currents, and the rotor winding gets power from the converter. However, when the rotor speed is higher than the synchronous speed, the phase sequence of the rotor currents is different from that of the stator currents, and the rotor winding outputs power to the converter [1-9]. For a given wind turbine, the power coefficient (the ratio of turbine power to the wind power), is a function of the tip speed ratio (the ratio of the blade tip speed to the wind speed). In order to track the maximum power point, the tip speed ratio must keep constant - at its optimal value. The input mechanical power with Maximum Power Point Tracking (MPPT) must satisfy [9]: 3 _ e( / ) (3)m ech m ref m r fP P ω ω= Where Pm_ref is the turbine power with MPPT at a reference speed of ωref based on the optimal tip speed ratio, and ωm is the rotor speed in rad/s. The rotor mechanical loss is: 3 _ e (4)( / )f f ref m r f P P ω ω= Where Pf_ref is mechanical loss measured at a reference speed of ωref .The electro- magnetic power in the air gap is: ( ) / (1 ) (5)em m ech f P P P s= − − Therefore, the stator output electrical power at rated operation is: 2 1 1 1 1 1 1 1 cos (6)em P P m I R m V I ϕ= − = where m1 is the number of phases of the stator winding, R1 is the stator phase resistance, V1 is the stator rated phase voltage, I1 is the rated stator phase current to be determined, and cos ߮ is the rated power factor. Solving for I1, one obtains: 1 1 2 1 1 1 1 (7 ) 2 / co s ( co s ) 4 / em em P m I V V R P mϕ ϕ = + +
  • 5. International Journal of Electrical Engineering and Technology (IJEET), ISSN 0976 – 6545(Print), ISSN 0976 – 6553(Online) Volume 3, Issue 2, July- September (2012), © IAEME 461 Then, based on the equivalent circuit shown below, one obtains: Fig. 3. DFIG equivalent circuit Now, rotor input electrical power can be computed as: 2 2 2 2 2 ( 8 )e mP s P m I R= + Where m2 is the number of phases of the rotor winding. The electromagnetic torque Tem is: ( 9 )/e m e m T P ω= Where ω? denotes the synchronous speed in rad/s. The input mechanical torque on the shaft is: (1 0 )m e c h e m f T T T= + Where Tf denotes the frictional torque. The total electrical output power is: 1 2 (1 1 )e le c F e P P P P= − − Where pFe is the core loss. The efficiency is defined as: ( 1 2 )1 0 0 %e l e c m e c h P P η = 4. Geometric Dimention And Parameters Design Of Dfig Studie The operation principle of electric machines is based on the interaction between the magnetic fields and the currents flowing in the windings of the machine. Rotational Machine Expert (RMxprt) is an interactive software package used for designing and analyzing electrical machines, is a module of Ansoft Maxwell 12.1 [10]. The structure of coil connection is shown in Fig. 4, Fig. 5, and the 3D geometries of the generator are shown in Fig. 6 Fig. 4. Stator and coil structure of the designed generator V2S
  • 6. International Journal of Electrical Engineering and Technology (IJEET), ISSN 0976 – 6545(Print), ISSN 0976 – 6553(Online) Volume 3, Issue 2, July- September (2012), © IAEME 462 Table 1. Stator and rotor slot parameters Stator Slot Parameter Rotor Slots Parameter hs0 (mm): 2 hr0 (mm): 2 hs1 (mm): 2 hr1 (mm): 2 hs2 (mm): 10 hr2 (mm): 15 bs0 (mm): 2.5 br0 (mm): 2.5 bs1 (mm): 8.52819 br1 (mm): 9.19419 bs2 (mm): 10.6303 br2 (mm): 5.24462 rs (mm) : 2 rr (mm) : 2 Fig. 5. Slot type Table 2. SOME RATED VALUES, GEOMETRIC PARAMETERS OF THE DESIGNED MACHINES Somme Electrical And Dimensional Parameters Value Rated output power (kW) 0.55 Rated voltage (V) 220 Given rated speed (rpm) 1500 Number of poles 4 Outer diameter of stator (mm) 180 Inner diameter of stator (mm) 121 Number of stator slots 30 Outer diameter of rotor (mm) 120 Inner diameter of rotor (mm) 50 Number of stator slots 24 Length of stator core (rotor) (mm) 65 Stacking factor of stator core 0.97 Stacking factor of iron core 0.97 Frictional loss (W) 12 Operating temperature (0 C) 75 Fig. 6. 3D view of the DFIG inner rotor designed 5. Simulation Results The finite element model is created. First, the geometric outlines are drawn, which is similar to the available mechanical engineering packages. Then, material properties are assigned to the various regions of the model. Next, the current sources and the boundary conditions are applied to the model. Finally, the finite element mesh is created. In the solver part, the finite element solution is conducted [10]. The FEA model of electromagnetic field is built by Maxwel12D; in this case the total number of mesh element is 9336.
  • 7. International Journal of Electrical Engineering and Technology (IJEET), ISSN 0976 – 6545(Print), ISSN 0976 – 6553(Online) Volume 3, Issue 2, July- September (2012), © IAEME 463 Fig. 7. 2D DFIG inner rotor mesh A. Efficiency of DFIG at variable environmental thermal condition The DFIG performance is obtained, by considering a variable ambient temperature, Fig 8. Show the influences of environmental thermal condition on efficiency, the increase in the ambient temperature, so the DFIG losses increase, thus the efficiency decreases. 0.00 500.00 1000.00 1500.00 2000.00 2500.00 3000.00 RSpeed [rpm ] -100.00 -75.00 -50.00 -25.00 0.00 25.00 50.00 75.00 100.00 Y1[fraction] RMxprtDesign1Percentage ANSOFT Curve Info Efficiency Setup1 : Performance Efficiency_1 Setup2 : Performance Efficiency_2 Setup3 : Performance Efficiency_3 Setup4 : Performance Efficiency_4 Setup5 : Performance Efficiency_5 Setup6 : Performance Efficiency_6 Setup7 : Performance Efficiency_7 Setup8 : Performance Efficiency_8 Setup9 : Performance Efficiency_9 Setup10 : Performance a.Percentage (efficiency) variation at different thermal condition 1000.00 1500.00 2000.00 2500.00 3000.00 RSpeed [rpm] 62.67 65.00 70.00 75.00 80.00 85.00 88.96 Y1[fraction] RMxprtDesign1Percentage ANSOFT Curve Info Efficiency Setup1 : Perf ormance Efficiency_1 Setup2 : Perf ormance Efficiency_2 Setup3 : Perf ormance Efficiency_3 Setup4 : Perf ormance Efficiency_4 Setup5 : Perf ormance Efficiency_5 Setup6 : Perf ormance Efficiency_6 Setup7 : Perf ormance Efficiency_7 Setup8 : Perf ormance Efficiency_8 Setup9 : Perf ormance Efficiency_9 Setup10 : Performance b. ZOOM Fig. 8. Percentage (efficiency) variation at different thermal condition B. DFIG modelisation results by 2D finite element method One considers a DFIG connected an infinite bus, the grid frequency is 50Hz, and turns at constant speed 1660rpm.
  • 8. International Journal of Electrical Engineering and Technology (IJEET), ISSN 0976 – 6545(Print), ISSN 0976 – 6553(Online) Volume 3, Issue 2, July- September (2012), © IAEME 464 Fig. 9 show the torque variation, the torque value in steady state is -3.5 Nm. 0.00 100.00 200.00 300.00 400.00 500.00 Time [ms] -8.00 -7.00 -6.00 -5.00 -4.00 -3.00 -2.00 -1.00 0.00 Moving1.Torque[NewtonMeter] Maxwell2DDesign1Torque ANSOFT Curve Info Moving1.Torque Setup1 : Transient Fig. 9. Torque in DFIG inner rotors Fig. 10 illustrates the stator and rotor flux linkage of DFIG, when in study state the first one value is 0.6wb and the second is 0.2wb. 0.00 100.00 200.00 300.00 400.00 500.00 Time [ms] -1.25 -1.00 -0.75 -0.50 -0.25 0.00 0.25 0.50 0.75 1.00 Y1[Wb] Maxwell2DDesign1Winding_1 ANSOFT Curve Info FluxLinkage(PhaseA) Setup1 : Transient FluxLinkage(PhaseB) Setup1 : Transient FluxLinkage(PhaseC) Setup1 : Transient FluxLinkage(PhaseU) Setup1 : Transient FluxLinkage(PhaseV) Setup1 : Transient FluxLinkage(PhaseW) Setup1 : Transient Fig. 10. DFIG stator and rotor flux linkage The DFIG stator current winding is shown in Fig. 11, the magnitude is 2A and the frequency is 50Hz, The frequency equal has 50 Hz by what the speed (mechanical) east notes. 0.00 100.00 200.00 300.00 400.00 500.00 Time [ms] -8.00 -6.00 -4.00 -2.00 0.00 2.00 4.00 6.00 Y1[A] Maxwell2DDesign1Stator Currents ANSOFT Curve Info Current(PhaseA) Setup1 : Transient Current(PhaseB) Setup1 : Transient Current(PhaseC) Setup1 : Transient Fig. 11. DFIG stator current winding There are two types of stranded loss quantities, StrandedLoss and StrandedLossR [9]: • StrandedLoss represents the resistive loss in a 2D or 3D volume and is calculated by: 21 = vol Solid Loss J σ ∫ (13) Where J is the conductivity of the material.
  • 9. International Journal of Electrical Engineering and Technology (IJEET), ISSN 0976 – 6545(Print), ISSN 0976 – 6553(Online) Volume 3, Issue 2, July- September (2012), © IAEME 465 •StrandedLossR represents the loss based on I2 times the resistance R. Fig. 12 illustrates the two types of loss, when the value of StrandedLoss in transient state is 355w and stabilized at 24w in steady-state, but the StrandedLossR is constant at 14.3w. 0.00 100.00 200.00 300.00 400.00 500.00 Time [ms] 0.00 125.00 250.00 355.00 Y1[W] Maxwell2DDesign1Loss ANSOFT Curve Info StrandedLoss Setup1 : Transient StrandedLossR Setup1 : Transient Fig. 12. DFIG StrandedLoss and StrandedLossR Fig. 13 shows the DFIG stator and rotor induced voltage, when the value of stator is 185v, but the value of rotor induced voltage is 8v. 0.00 100.00 200.00 300.00 400.00 500.00 Time [ms] -200.00 -150.00 -100.00 -50.00 0.00 50.00 100.00 150.00 200.00 Y3[V] Maxwell2DDesign1InducedVoltage ANSOFT Curve Info InducedVoltage(PhaseA) Setup1 : Transient InducedVoltage(PhaseB) Setup1 : Transient InducedVoltage(PhaseC) Setup1 : Transient InducedVoltage(PhaseU) Setup1 : Transient InducedVoltage(PhaseV) Setup1 : Transient InducedVoltage(PhaseW) Setup1 : Transient Fig. 13. DFIG stator and rotor induced voltage Fig.14 show DFIG stator winding current spectrum, one does not find the harmonic by that the current operate and purely sinusoidal. 0.00 0.01 0.10 1.00 10.00 Freq [kHz] 0.00 0.20 0.40 0.60 0.80 1.00 1.20 mag(Current(PhaseA))[A] Maxwell2DDesign1XY Plot 1 ANSOFT Curve Info mag(Current(PhaseA)) Setup1 : Transient Fig. 14. DFIG stator winding current spectrum
  • 10. International Journal of Electrical Engineering and Technology (IJEET), ISSN 0976 – 6545(Print), ISSN 0976 – 6553(Online) Volume 3, Issue 2, July- September (2012), © IAEME 466 0.00 100.00 200.00 300.00 400.00 500.00 Time [ms] -8.00 -6.00 -4.00 -2.00 0.00 2.00 4.00 6.00 8.00 Y1[A] -200.00 -150.00 -100.00 -50.00 0.00 50.00 100.00 150.00 200.00 Y3[V] Maxwell2DDesign1InputCurrent ANSOFT Curve Info Y Axis InputCurrent(PhaseU) Setup1 : Transient Y1 InputCurrent(PhaseV) Setup1 : Transient Y1 InputCurrent(PhaseW) Setup1 : Transient Y1 InputVoltage(PhaseA) Setup1 : Transient Y3 InputVoltage(PhaseB) Setup1 : Transient Y3 InputVoltage(PhaseC) Setup1 : Transient Y3 Fig. 15. Rotor current and stator voltage of DFIG Fig. 15 shows the rotor current and stator voltage of DFIG, the magnitude and the frequency of the first one is 9.5A is ≈5Hz, and the second one is 180v is 50Hz respectively. C. Field results in 2D of the elemnt finits model The FEA model of electromagnetic field is built by Maxwell2D, the flux, flux density, field intensity. Fig. 16. Flux distribution of DFIG at 0.5s The Fig.16 indicates the flux line distribution of the DFIG at 0.5s. It is important to note that in order to obtain accurate results, the triangular mesh elements assigned to the airgap should have an aspect ratio close to one. A large aspect ratio between the sides of a triangular element will result in accurate computation of the flux density and hence the electromagnetic torque. Fig 17 shows the DFIG’s flux density distribution at 0.5s, the maximum value of flux density is 1.47T. Fig. 17. flux density of DFIG at 0.5s
  • 11. International Journal of Electrical Engineering and Technology (IJEET), ISSN 0976 – 6545(Print), ISSN 0976 – 6553(Online) Volume 3, Issue 2, July- September (2012), © IAEME 467 Fig.18 indicates the vector diagram and contours diagram of flux density at 0.5s. Fig. 18. Contours and vector diagrams of flux density in DFIG According to Fig. 18 and Fig. 16, the flux line and magnetic field are symmetrical in the whole machine and the distribution regularities of flux line and magnetic field are the same. The total loss of DFIG is illustrated in fig19, when the winding losses have a great contribution. Fig. 19. Total Loss of DFIG D. Field results in 3D of the finite element model The 3D FEA model of electromagnetic field is built by Maxwell 3D, this simulation is obtained by Terra pc (QuadroFX380, i7 CPU, 3.07 GHZ, 8 CPU and 4G RAM). Our model of DFIG used in Maxwell 3D environment has 98586 number of mesh element. The largest saving in computation time is made by doing the simulation in 2D instead of 3D. The analyze will be fairly limited due to the large increase in simulation time, approximately 4 minutes per time step compared to 5 seconds for a corresponding 2D model. In our application the simulation rest in execution during some day.
  • 12. International Journal of Electrical Engineering and Technology (IJEET), ISSN 0976 – 6545(Print), ISSN 0976 – 6553(Online) Volume 3, Issue 2, July- September (2012), © IAEME 468 Fig. 20. 3D DFIG inner rotor mesh Fig 20 shows the 3D DFIG’s flux density distribution at 0.4s, the maximum value of flux density is 1.59T. According to Fig. 17 and Fig. 21, the maximum value of flux density obtained by 3D model is bigger than in 2D, Fig. 21. 3D flux density of DFIG at 0.4s Fig. 22. 3D vector diagram of flux density of DFIG at 0.4s Fig.23 indicates the 3D vector diagram of flux density at 0.4s.
  • 13. International Journal of Electrical Engineering and Technology (IJEET), ISSN 0976 – 6545(Print), ISSN 0976 – 6553(Online) Volume 3, Issue 2, July- September (2012), © IAEME 469 Fig. 23. 3D current density of DFIG at 0.4s Fig.24 shows the 3D total loss of DFIG at 0.4s. Fig. 24. 3D Total loss of DFIG inner rotor 6. Conclusion Finite element analysis (FEA) is a frequently used method for analysis of electromechanical converters. As a numerical analysis method, FEA allows for including any practical material, external excitation (voltage driven or current driven), inclusion of motion, and nonlinear effects such as magnetic saturation and eddy current effects. A 2D model of the DFIG inner rotor is given, solved, some simulation result is given and commented, to return our simulation results finer a 3D model is developed and solved, but the resolution time is very large, this time is a scale of the days. This model 2D and 3D obtained by using Ansoft finite element software, this last can be used as an effective way to design and calculate the DFIG performance. This work is the necessary preparations for design and development high reliability and high security of DFIG applications. References [1] AL. Olimpo, J. Nick, E. Janaka, C. Phill and H Mike,Wind Energy Generation Modelling and Control, John Wiley & Sons, Ltd 2009. [2] Ian woofenden, wind power for dummies, Wiley Publishing, 2009. [3] A. Petersson, Analysis, Modeling and Control of Doubly-Fed Induction Generators for Wind Turbines, phd thesis, chalmers university of technology,GÖteborg, Sweden 2005. [4] Martin O. L. Hansen, Aerodynamics of Wind Turbines, Earthscan in the UK and USA in 2008. [5] Zongxi Fang ,Permanent magnet machine topologies for wind power generation,university of Sheffield 2010.
  • 14. International Journal of Electrical Engineering and Technology (IJEET), ISSN 0976 – 6545(Print), ISSN 0976 – 6553(Online) Volume 3, Issue 2, July- September (2012), © IAEME 470 [6] B.C. Pal F. Mei, Modelling adequacy of the doubly fed induction generator for small-signal stability studies in power systems, IET Renewable Power Generation 2008. [7] H. Li, Z. Chen, Overview of different wind generator systems and their comparisons, Renewable Power Generation, IET 2007. [8] H. Li1, Z. Chen, Henk Polinder, research report on models for numerical evaluation of variable speed different wind generator systems, Integrating and strengthening the European Research Area, 2002-2006. [9] Help of Ansoft Maxwell V12®, Ansoft Corporation 2010. [10] H. Mellah, K.E Hemsas, Dynamic design and simulation analysis of permanent magnet motor in different scenario of fed alimentation, conference international on automatique and mécatronique, novembre 22 -23, 2011, usto, oran, Algeria.