ACTIVE CONTROL OF WIND TURBINE ROTOR TORSIONAL VIBRATION Warren N. White Zhichao Yu Mechanical and...
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Transcript of ACTIVE CONTROL OF WIND TURBINE ROTOR TORSIONAL VIBRATION Warren N. White Zhichao Yu Mechanical and...
ACTIVE CONTROL OF WIND TURBINE ROTOR TORSIONAL VIBRATION
Warren N. WhiteZhichao Yu
Mechanical and Nuclear EngineeringKansas State UniversityManhattan, KS 66506
[email protected]@ksu.edu
Ruth Douglas MillerDavid Ochs
Electrical and Computer EngineeringKansas State UniversityManhattan, KS 66506
[email protected]@gmail.com
Kansas State University 2013 DSCC 10-21-13
AgendaIntroduction
Torsion Measurement Scheme
Generator Model and Controller
The Vibration Isolator
Results
Conclusions
* Especially appreciate ePEP’s generosity for supporting the research
Kansas State University 2013 DSCC 10-21-13
IntroductionReduction of rotor shaft torsional vibrations
Active control of generator torque
Measurement of the rotor shaft torsion
NREL FAST simulation with PMSG for different conditions
Kansas State University 2013 DSCC 10-21-13
Torsion Measurement Scheme
opticalfiber
centerline
gratings
opticalfiber
graded indexlenses
Kansas State University 2013 DSCC 10-21-13
Generator Model and Controller qqdqde iLLiip
2
3
dt
diLiLpRiv ddqqrdd
dt
diLiLpRiv qqddrqq
(2)
(3)
Direct and Quadrature voltage:
Linearization and decoupling:
Feedback linearization, let:
dqrsd vipLv dt
diLRiv qsqq
(6)
(7)
qrdrsq vpipLv
dt
diLRiv dsdd
(5)
(4)
Generator torque:
PMSGGenerator
(1)0
Kansas State University 2013 DSCC 10-21-13
Generator Model and Controller Cont.
dt
diLRiv qsqq
(6)
(7)
dt
diLRiv dsdd
RsLsV
sI
sq
q
1(8)
sIsIsE qqd (9)
Define the error signal:
Define the transfer function between E(s) and sVq :
cs
RsL
sE
sVsq
(10)
(8)
(10)
cssE
sIq 1 (11)
1
1
cssI
sI
dq
qCLTF:
PMSGGenerator
(12)
Kansas State University 2013 DSCC 10-21-13
Generator Simulink Model
rotorangularvelocity
DQ - PM Generator Model
2
iq
1
id
1s
quadrature axis current
1/Ls
q 1/Ls
p*psi
p*psi
[Lspwriq]
iq-NL source
[Lspwriq]
iq- NL
[Lspwrid]
id-NL source
[Lspwrid]
id-NL
1s
direct axis current
1/Ls
d 1/Ls
R
R - q axis
R
R - d axis
Ls*p*wr*iq
Ls*p*wr*id
Ls*p
Ls*p
3
vq
2
wr
1
vd
PMSGGenerator
Kansas State University 2013 DSCC 10-21-13
2
tau eactual
1
id
2/(3*p*psi)
torque to iq
p*psi
p*psi
[Lspwriq]
iq-NL source
[Lspwriq]
iq- NL
(3*p*psi)/2
iq to torque
[Lspwrid]
id-NL source
[Lspwrid]
id-NL
0
id - desired
v d
wr
v q
id
iq
PMSGGenerator
PI(s)
PI Controller1
PI(s)
PI Controller
Ls*p*wr*iq
Ls*p*wr*id
Ls*p
Ls*p q
Ls*p
Ls*p d
2
tau edesired
1
wr
Generator Torque Controller
Kansas State University 2013 DSCC 10-21-13
The vibration Isolator
Drive Train Two Mass Model
Vibration Isolator Derivation
Speed, Torque, and Vibration Control
Kansas State University 2013 DSCC 10-21-13
Drive Train Two Mass Model
Rotor
generator inertiareflected through
gearboxN2JG
rotor inertiaJ
aero
1
Torsional stiffness Ks
Torsional damper D
Ne
N2
Kansas State University 2013 DSCC 10-21-13
Vibration Isolator Derivation
scss
sKss
s
sKs aerord
PIe
1
1
10
101
Generator torque:
Speed Control High pass filter
Low pass filter
BPF
1000HZ10HZ
(13)
Kansas State University 2013 DSCC 10-21-13
Speed, Torque, and Vibration Control
1
FAST tau e
-10000(s+1)
s
Speed Controller
wr
tau e desired
tau e actual
PMSG Subsys
0.1s
0.1s+1
High PassFilter
-100
FilterGain
3
tau r
2
wd
1
wr
Rotor Speed
DesiredRotor Speed
Rotor Torque
Kansas State University 2013 DSCC 10-21-13
ResultsNREL 5 MW Turbine
Blade Pitches = 12.5 ̊
Rotor Speed Control, ωd = 11 RPM
Steady, Time-varying, Turbulent wind, vmean= 15 m/s
Kansas State University 2013 DSCC 10-21-13
STEADY WIND
0 100 200 300 400 500 600 700-1000
-500
0
500
1000
1500
2000
2500
3000
3500
4000
Time(sec)
Roto
r T
orq
ue(k
N-m
)
Steady Wind
without Isolator
Isolator gain=10Isolator gain=100
0 5 10 15 20 25 30 35 40-700
-600
-500
-400
-300
-200
-100
0
100
200
300
Time(sec)
Roto
r T
orq
ue(k
N-m
)
Steady Wind
without Isolator
Isolator gain=10Isolator gain=100
Kansas State University 2013 DSCC 10-21-13
Time Varying Wind
0 100 200 300 400 500 600 700-1000
0
1000
2000
3000
4000
5000
Time(sec)
Rot
or T
orqu
e(kN
-m)
Time Varying Wind
without Isolator
Isolator gain=10Isolator gain=100
500 502 504 506 508 510 512 514 516 518 5203500
3600
3700
3800
3900
4000
4100
4200
Time(sec)
Roto
r T
orq
ue(k
N-m
)
Time Varying Wind
without Isolator
Isolator gain=10Isolator gain=100
Kansas State University 2013 DSCC 10-21-13
Turbulent Wind
0 100 200 300 400 500 600 700-2000
-1000
0
1000
2000
3000
4000
5000
6000
Time(sec)
Rot
or T
orqu
e(kN
-m)
Turbulent Wind
without Isolator
Isolator gain=10Isolator gain=100
390 392 394 396 398 400 402 404 406 408 4103800
3900
4000
4100
4200
4300
4400
4500
4600
Time(sec)
Rot
or T
orqu
e(kN
-m)
Turbulent Wind
without Isolator
Isolator gain=10Isolator gain=100
Kansas State University 2013 DSCC 10-21-13
500 502 504 506 508 510 512 514 516 518 52035
36
37
38
39
40
41
42
43
44
45
Time(sec)
Gen
erat
or T
orqu
e(kN
-m)
Time Varying Wind
without Isolator
Isolator gain=100
390 392 394 396 398 400 402 404 406 408 4104100
4150
4200
4250
Time(sec)
Rot
or T
orqu
e an
d N
et B
endi
ng M
omen
t(kN
-m)
Turbulent Wind
Isolator gain = 90
Isolator gain = 100
GENERATOR TORQUE FOR TWO DIFFERENT ISOLATOR GAINS ROBUSTNESS TEST FOR ISOLATOR
Kansas State University 2013 DSCC 10-21-13
0 100 200 300 400 500 600 700-1000
0
1000
2000
3000
4000
5000
Time(sec)
Rot
or T
orqu
e an
d N
et B
endi
ng M
omen
t(kN
-m)
Turbulent Wind (K = 100)
Rotor Torque
Blade Base In-plane Bending Moment Sum
0 100 200 300 400 500 600 700-2
-1
0
1
2
3
4
5
6x 10
6
Time(sec)
Pow
er (
wat
ts)
Time Varying Wind
without Isolator
Isolator gain=100
ROBUSTNESS TEST FOR ISOLATOR – IN-PLANE BLADE BASE BENDING MOMENT SUM USED FOR FEEDBACK
GENERATOR POWER FOR TWO ISOLATOR GAINS
Kansas State University 2013 DSCC 10-21-13
Conclusions
Rotor vibrations were eliminated or substantially reduced
Application of rotor torque measurement scheme
Including generator electrical system in analysis
Kansas State University 2013 DSCC 10-21-13
Future WorkBand pass filter
Including gearbox model in the analysis
Including doubly fed induction generator(DFIG)
Assessing life extension by reduction of torsion
Kansas State University 2013 DSCC 10-21-13
I Appreciate Your Attention
The End
Questions?Warren N. White
Zhichao [email protected]
Ruth Douglas MillerDavid Ochs
[email protected]@gmail.com