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20.2 Wind Turbines

443

wind park, then the number of generators ngen > 1. The capacity of each generator is about [0.5, 5] MVA (being 1 and 2 MVA the most common capacities), thus ngen [0.2Sn, 2Sn]. An inconsistent value of ngen can lead to an inadequate initialization of the wind speed.

2.Machine impedances and inertiæ are equivalent weighted pu values of the machines that compose the aggregate wind park.

20.2.2Wind Turbine Initialization

Wind turbines are initialized after power flow analysis and a static generator is needed to impose the desired voltage and active power at the wind turbine bus. Once the power flow solution is available, v0, θ0, p0 and q0 at the generation bus are used for initializing the state and input variables, the latter being the wind speed vw0, which is used as the average wind speed vwa for the wind speed models. Due to the nonlinearity of generator, converter and turbine models, the initialization requires the implementation of a Newton’s method. For the interested reader, further insights on wind turbine initialization are given in [285] and [133].

The following subsections are organized taking into account implementation issues. The models that are common to all wind turbine are described first. These are the turbine model and the shaft model. Then, each specific wind generator type is described. With this aim, electrical machine and VSC converter models are described together.

20.2.3Turbine Model

The mechanical model of the wind turbine is independent from the generator configuration. Thus, the mechanical equations of the turbine can be implemented as a separate class and then imported in the wind generator model.

Following items describe two models, namely fixed-blade and variable pitch angle position blade turbines. Table 20.4 defines all parameters used below.

Table 20.4 Turbine mechanical parameters

Variable

Description

Unit

 

 

 

 

 

 

Kp

Pitch control gain

rad/pu

nblade

Number of blades

int

ngen

Number of machines that compose the wind park

int

npole

Number of poles

int

Sn

Power rating

MVA

R

Rotor radius

m

Tp

Pitch control time constant

s

ηGB

Gear box ratio

-

ρ

Air density

kg/m3

444

20 Wind Power Devices

Fixed-Blade Turbine Model

This model assumes fixed turbine blades and is adequate for wind generators without speed regulation. The mechanical power pw extracted from the wind is a function of the wind speed vw and the turbine rotor speed ωt and can be approximated as follows:

p

w

=

ngenρ

c

(λ)A v3

(20.12)

 

 

 

 

p

r w

 

 

 

 

2Sn

 

 

where cp is the performance coe cient or power coe cient, λ the tip speed ratio and Ar = πR2 the area swept by the rotor. The speed tip ratio λ is the ratio between the blade tip speed vbt and the wind upstream the rotor vw :

λ =

vbt

= ηGB

2t

(20.13)

 

npolevw

 

vw

 

Finally, the cp(λ) curve is approximated as follows:

cp = 0.44

125

6.94

e

16.5

(20.14)

 

 

 

λi

 

λi

with

 

 

 

1

 

 

 

 

λi

=

 

 

 

 

(20.15)

 

 

 

 

1

+ 0.002

 

 

 

 

 

 

λ

 

 

 

 

 

Turbine Model with Pitch Angle Control

In this model, turbine blades can rotate in order to reduce the rotor speed in case of super-synchronous conditions. The angular position θp of the blades is called pitch angle. This turbine model is adequate for wind generators with speed control.

The mechanical power pw extracted from the wind is a function of the wind speed vw , the rotor speed ωm and the pitch angle θp. The mechanical power pw can be approximated as:

pw =

ngenρ

cp(λ, θp)Ar v3

(20.16)

 

 

 

w

 

 

2Sn

 

where parameters and variables are the same as in (20.12) and the speed tip ratio λ is defined in (20.13). The cp(λ, θp) curve is approximated as follows [126]:

cp = 0.22 λi

0.4θp

5 eλi

(20.17)

 

 

 

116

 

 

12.5

 

with

 

 

 

1

 

0.035

 

 

1

=

 

 

 

(20.18)

 

λi

λ + 0.08θp

 

θp3 + 1

 

20.2Wind Turbines

Alternative equations are given in [284], as follows:

cp = 0.73 λi

0.58θp 0.002θ2.14 13.2 e

151

 

 

 

 

 

 

 

with

1

 

1

 

0.003

 

 

=

 

 

 

 

 

 

 

 

 

λi

λ − 0.02θp

θp3 + 1

18.4

λi

445

(20.19)

(20.20)

As discussed above, the pitch angle θp is controlled to avoid super-synchro- nous speeds. The control diagram is shown in Figure 20.6 and described by the di erential equation:

˙

ref

) − θp)/Tp

(20.21)

θp = (Kpφ(ωm − ω

 

where φ is a function which allows varying the pitch angle set point only when the di erence (ωm − ωref) exceeds a predefined value ±Δω. Since the pitch control works only for super-synchronous speeds, an anti-windup limiter locks the pitch angle to θp = 0 for sub-synchronous speeds.

ωm

+

θp

 

 

Kp

 

 

1 + Tps

 

 

 

 

ωref

 

 

0

Fig. 20.6 Pitch angle control diagram

The speed control is aimed to maximize the power production of the wind turbine. Figure 20.7 shows the dependence of the mechanical power pw produced by the wind turbine on the wind speed vw and the turbine rotor speed ωt. The solid line is the maximum mechanical power locus for each wind and rotor speeds. This curve is used for defining, for each value of the rotor speed, the optimal mechanical power pw that the turbine has to produce. Figure 20.8 shows a possible implementation of the (pw , ωt) characteristic. For super-synchronous speeds, the reference power is fixed to 1 pu to avoid overloading the generator. For ωt < 0.5 pu, the reference mechanical power is set to zero.

The detailed (pw , ωt) characteristic is:

p (ω ) =

p

(ω ) that satisfies dpw (ωt , vw , θp)

= 0 if

0.5 ω 1

w t

0

if

ωt < 0.5

 

t

w

t

 

t

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

1

if

ωm > 1

 

 

 

 

 

 

 

 

 

(20.22)

446

 

 

 

 

20 Wind Power Devices

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Fig. 20.7 Speed-power characteristic of the wind turbine. The pitch angle is assumed θp = 0 to plot the pw(ωt, vw , θp ) curve

The simplified (pw, ωt) characteristic is:

pw(ωt) =

2ωt

if

1

t if 0.5 ωt

 

1

(20.23)

 

 

0

ω

< 0.5

 

 

 

 

 

 

ωt > 1

 

 

 

1

if

 

 

 

 

 

 

 

 

 

 

 

 

 

 

20.2.4Dynamic Shaft

The shaft of wind generators can be modelled as two masses connected by a spring. The masses represent the turbine shaft and the generator shaft, while the spring models the shaft sti ness. The resulting model is similar to the one described in Section 15.1.10 of Chapter 15.

Mechanical di erential equations are:

ω˙ t = (τt − Ksδtm)/(2Ht)

(20.24)

ω˙ m = (Ksδtm − τe)/(2Hm)

˙

δtm = Ωb(ωt ωm)

where Ωb is the system rated frequency in rad/s, ωt is the wind turbine angular speed, ωm is the generator rotor speed, δtm is the relative angle

20.2 Wind Turbines

447

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Fig. 20.8 Optimal and implemented control speed-power characteristics

displacement of the two shafts, τe is the electrical torque and τt is the mechanical torque:

τt =

pw

(20.25)

ωt

 

 

and all other parameters are defined in Table 20.5.

A periodic torque pulsation can be added to τt to simulate the tower shadow e ect. The shadow-e ect frequency depends on the rotor speed ωt, the gear box ratio ηGB , and the number of blades nblade, as follows:

Ωbωt

 

τ˜t = τt 1 + αs sin ηGB nblade t

(20.26)

where the torque pulsation amplitude can be fixed equal to αs = 0.025 [7]. The expression (20.26) substitutes the mechanical torque in the first equation of (20.24).

Shaft oscillations cannot be removed in the squirrel-cage induction generator type. For other wind turbine types that include VSC devices, the converter controls can e ectively damp shadow e ect modes and shaft oscillations [187]. If the control is e cient enough, the shaft can be considered rigid, i.e., ωt = ωm. Hence:

ω˙ t = (τt − τe)/(2Ht + 2Hm)

(20.27)

448

 

 

20 Wind Power Devices

 

Table 20.5 Wind turbine shaft parameters

 

 

 

 

 

 

 

Variable

Description

Unit

 

 

 

 

 

 

 

Hm

Machine rotor inertia constant

MWs/MVA

 

 

 

Ht

Wind turbine inertia constant

MWs/MVA

 

 

 

Ks

Shaft sti ness

pu

 

 

αs

Shadow e ect factor

-

 

 

20.2.5Non-Controlled Speed Wind Turbine

The simplified electrical circuit used for the squirrel-cage induction generator is the same as the one for the single-cage induction motor, shown in Figure 15.14 of Chapter 15. The only di erence with respect to the induction motor is that the currents are positive if injected into the network. The equations are formulated in terms of the real (d-) and imaginary (q-) axes, with respect to the network reference angle. Table 20.6 summarizes and defines all parameters of the squirrel-cage induction machine.

Table 20.6 Squirrel-cage induction machine parameters

Variable

Description

Unit

 

 

 

rr

Rotor resistance

pu

rs

Stator resistance

pu

xr

Rotor reactance

pu

xs

Stator reactance

pu

xμ

Magnetizing reactance

pu

Network Interface

In a synchronously rotating reference frame, the link between the network and the stator machine voltages is:

vd = −vh sin θh

(20.28)

vq = vh cos θh

 

and the active and reactive power productions are:

 

ph = vdid + vq iq

(20.29)

qh = vq id − vdiq + bc(vd2 + vq2)

 

where bc is the fixed capacitor conductance which is determined at the initialization step to impose the required bus voltage level.

20.2 Wind Turbines

449

Machine Electro-Magnetic Equations

The di erential equations in terms of the voltage behind the stator resistance rS are:

ed − vd = rsid − x iq

(20.30)

eq − vq = rsiq + x id

 

whereas the link between voltages, currents and state variables is as follows:

e˙d

=

Ωb(1 − ωm)eq (ed (x0 − x )iq )/T0

(20.31)

e˙

 

=

Ω (1

ω

m

)e

(e

+ (x

0

x )i

)/T

 

q

 

b

 

d

q

 

d

 

0

where ωm is the rotor angular speed, and x0, x and T0 can be obtained from generator parameters:

x0

= xs + xμ

(20.32)

x

= xs +

xr xμ

 

xr + xμ

 

T

=

xr + xμ

 

 

0

 

ΩbrR

 

 

 

 

Turbine and Machine Mechanical Equations

The mechanical DAE system is (20.12) and (20.24)-(20.26), where the electrical torque τe is defined as:

τe = edid + eq iq

(20.33)

20.2.6Doubly-Fed Asynchronous Generator

The model of the doubly-fed asynchronous generator is assumed steady-state, as the stator and rotor flux dynamics are fast with respect to grid dynamics. As a result of these assumptions, one has the DAE system described below. Table 20.7 summarizes and defines all parameters required by wind turbine with doubly-fed asynchronous generator.

Network Interface

 

Stator voltages depends on the bus voltage v¯h:

 

vs,d = −vh sin θh

(20.34)

vs,q = vh cos θh

 

450

 

 

20 Wind Power Devices

Table 20.7 Doubly-fed asynchronous generator parameters

 

 

 

 

 

 

Variable

Description

Unit

 

 

 

 

 

 

 

KV

Voltage control gain

pu/pu/s

 

 

pmax

Maximum active power

pu

 

 

pmin

Minimum active power

pu

 

 

qmax

Maximum reactive power

pu

 

 

qmin

Minimum reactive power

pu

 

 

rr

Rotor resistance

pu

 

 

rs

Stator resistance

pu

 

 

T

Power control time constant

s

 

 

xr

Rotor reactance

pu

 

 

xs

Stator reactance

pu

 

 

xμ

Magnetizing reactance

pu

 

The generator active and reactive power productions depend on the stator and converter currents is,d + jis,q and ic,d + jic,q, respectively, and stator and converter voltages vs,d + jvs,q and vc,d + jvc,q, respectively, as follows:

ph = vs,dis,d + vs,q is,q + vc,dic,d + vc,qic,q

(20.35)

qh = vs,q is,d − vs,dis,q + vc,q ic,d − vc,dic,q

 

The expressions above can be rewritten as a function of stator and rotor currents is,d + jis,q and ir,d + jir,q, respectively, and stator and rotor voltages vs,d + jvs,q and vr,d + jvr,q , respectively. In fact, the converter powers on the grid side are:

pc = vc,dic,d + vc,q ic,q qc = vc,qic,d − vc,dic,q

whereas, on the rotor side:

pr = vr,dir,d + vr,q ir,q qr = vr,q ir,d − vr,dir,q

(20.36)

(20.37)

Assuming a loss-less converter model, the active power of the converter coincides with the rotor active power, thus pc = pr. The reactive power injected into the grid can be approximated neglecting stator resistance and assuming that the d-axis coincides with the maximum of the stator flux. Therefore, the powers injected in the grid are:

ph = vs,dis,d + vs,q is,q + vr,dir,d + vr,q ir,q

(20.38)

qh =

xμvhir,d

 

v2

 

 

h

 

xs + xμ

xμ

 

 

20.2 Wind Turbines

451

Machine Electro-Magnetic Equations

The machine stator and rotor voltages are a function of stator and rotor currents and the rotor speed ωm:

vs,d = −rsis,d + ((xs + xμ)is,q + xμir,q )

(20.39)

vs,q = −rsis,q ((xs + xμ)is,d + xμir,d)

 

vr,d = −rr ir,d + (1 − ωm)((xs + xμ)ir,q + xμis,q )

 

vr,q = −rr ir,q (1 − ωm)((xs + xμ)ir,d + xμis,d)

 

whereas the links between stator fluxes and generator currents are:

 

ψs,d = ((xs + xμ)is,d + xμir,d)

(20.40)

ψs,q = ((xs + xμ)is,q + xμir,q )

 

Turbine and Machine Mechanical Equations

The generator motion equation is modeled as a single shaft, i.e., (20.27), as it is assumed that the converter controls are able to filter shaft dynamics. For the same reason, no tower shadow e ect is considered in this model. In (20.27), the electrical torque is:

τe = ψs,dis,q − ψs,q is,d

(20.41)

Substituting the stator flux equations (20.40) in (20.41) leads to:

τe = xμ(ir,q is,d − ir,dis,q )

(20.42)

In [286], the following approximation of the electrical torque τe is proposed:

τe ≈ −

xμvhir,q

(20.43)

Ωb(xs + xμ)

where Ωb is the system rated frequency in rad/s.

Mechanical equations are completed by the mechanical torque τt equation (20.25) and the turbine model (20.16) and (20.17)-(20.18) or (20.19)-(20.20) and the pitch angle control (20.21).

VSC Regulators

Since VSC dynamics are quite fast with respect to the electro-mechanical transients, the converter can be modeled as an ideal current source, where ir,q and ir,d are state variables and are used for controlling the rotor speed and the bus voltage, respectively. VSC control diagrams are depicted in Figures 20.9 and 20.10. The DAE system of the converter currents is:

452 20 Wind Power Devices

 

+ x

μ

 

 

1

 

i˙r,q =

xs

pw

(ωm)m − ir,q

 

(20.44)

xμv

 

T

˙

(vh − v

ref

)

− vh/xμ − ir,d

 

ir,d = KV

 

 

 

where vref is the reference voltage computed at the initialization step and pw(ωm) is the power-speed characteristic (20.22) or (20.23).

 

 

 

 

ir,qmax

 

ωm

pw

pw

τm

(xs + xμ)

ir,q

 

 

 

 

 

 

ωm

 

xμv(1 + sT )

 

 

 

 

 

 

 

 

 

 

ir,qmin

 

Fig. 20.9 Rotor speed control diagram

imaxr,d

vref

+

1

ir,d

KV

1 + s

+

+

iminr,d

1

xμ

vh

Fig. 20.10 Voltage control diagram of the doubly-fed asynchronous generator

Hard Limits

Both the speed and voltage controls undergo anti-windup limiters to avoid converter over-currents. Rotor current limits are computed based on active and reactive limits, and assuming bus voltage vh 1 one has:

ir,qmax ≈ −

xs + xμ

pmin

 

(20.45)

xμ

 

min

≈ −

xs + xμ

p

max

 

 

 

 

 

ir,q

 

 

 

 

 

 

 

xμ

 

 

 

 

 

 

max

≈ −

xs + xμ

 

min

xs + xμ

ir,d

 

q

 

 

 

 

 

xμ

 

 

x2

 

 

 

 

 

 

 

μ

min

≈ −

xs + xμ

 

max

 

xs + xμ

ir,d

 

q

 

 

 

 

x

 

 

x2

 

 

μ

 

 

 

 

μ