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17.4 Basic RLC Models

 

 

 

383

 

R

 

L

C

 

h

k

h

k

h

k

 

(a)

 

(b)

(c)

 

 

C

 

 

 

 

 

 

 

R

L

 

 

R

 

 

 

 

h

 

k

h

 

k

 

 

 

 

 

(d)

 

(e)

 

 

 

 

 

 

h

 

 

R

L

C

 

 

h

 

 

k

 

 

 

 

 

L

C

R

 

 

 

 

k

 

 

 

(f)

 

(g)

 

 

 

 

 

 

 

 

Fig. 17.2 RLC circuits

 

 

• Inductance (Figure 17.2.b):

 

˙

(17.8)

iL = vdc/L

0 = iL + idc

 

• Capacitance (Figure 17.2.c):

 

v˙C = −idc/C

(17.9)

0 = vC − vdc

 

• RC parallel (Figure 17.2.d):

 

v˙C = (idc + vC /R)/C

(17.10)

0 = vC − vdc

 

• RL series (Figure 17.2.e):

 

˙

(17.11)

iL = (vdc − RiL)/L

0 = iL + idc

384

17

Direct-Current Devices

• RLC series (Figure 17.2.f):

 

 

˙

− RiL − vC )/L

(17.12)

iL = (vdc

v˙C = iL/C

 

0 = iL + idc

 

• RLC parallel (Figure 17.2.g):

 

 

v˙C = (idc + vC /R + iL)/C

(17.13)

˙

 

 

iL = vC /L

 

 

0 = vC − vdc

Along with the Voltage Source Converter (VSC) described in the following Chapter 18, these basic elements can provide a versatile tool for setting up composite devices. For example, a SMES is an inductance connected to an ac network through a VSC. Furthermore, VSC-based FACTS devices are composed of a VSC or two back-to-back VSCs with a capacitance on the dc side. These devices are described in Chapter 19.

17.5Direct-Current Machines

A power system book of XXth century would have dedicated an entire chapter to direct-current machines. Unfortunately, these beautiful (from the modelling viewpoint) machines are not very common in these years, although a renewed interest could come from some distributed energy resource applications. However, I believe that a book on power system devices is not complete if it does not include at least a brief outline of basic dc machine models and configurations.

Rf

Laa

Ra

h

 

h

+

 

+

if

 

ia

vf

ωLaf if

va

Lf f

 

 

 

k

 

k

Fig. 17.3 Basic dc machine equivalent circuit

Figure 17.3 shows the basic equivalent circuit of a direct-current machine. The following notation assumes that the machine is working as a motor. The dc machine DAE system is [160]:

17.5 Direct-Current Machines

385

˙

(17.14)

if = (vf − Rf if )/Lf f

˙

 

ia = (va − Raia − Laf if ω)/Laa

 

ω˙ = (τe − τm − Dω)/2H

0 = Laf if ia − τe

where ia and if are the armature and field currents, respectively, va and vf are the armature and field voltages, respectively, ω is the rotor angular speed, τe is the electrical torque, and all other parameters are defined in Table 17.3. The coe cient D models frictions and windage losses, hence D 1 pu for τe 1 pu.

Table 17.3 Direct-current machine parameters

Variable

Description

Unit

 

 

 

 

 

 

D

Coe cient for frictions and windage losses

pu

H

Machine inertia constant

MWs/MVA

Laa

Armature winding self-inductance

s

Laf

Mutual field-armature inductance

s

† Las

Mutual series field-armature inductance

s

Lf f

Field winding self-inductance

s

† Lf s

Mutual series-shunt field windings inductance

s

† Lss

Series field winding self-inductance

s

Ra

Armature winding resistance

pu

Rf

Field winding resistance

pu

† Rs

Series field winding resistance

pu

τm

Mechanical torque

pu

Parameters required only for the compound-connected dc machine.

The typical configurations of the dc machine described above are: (i) separate winding excitation, (ii) shunt connection, (iii) series connection and (iv) compound connection. The following items provide the interface equations that make each connection type compliant with (17.2).

Separate Winding Connection

The machine is connected to two pairs of dc nodes, i.e. h-k for the armature winding and h -k for the field winding (see Figure 17.3). The voltage and current pairs (vdc, idc) and (vdc, idc) are associated with the nodes h-k and h -k , respectively. Thus, for the armature winding:

vdc = va,

idc = −ia

(17.15)

and for the field winding:

 

 

 

 

 

 

v

= v ,

i

=

i

f

(17.16)

dc

f

dc

 

 

386

17 Direct-Current Devices

 

 

Rs

 

 

(a)

 

 

 

 

 

+

 

 

 

 

 

is

 

 

 

vs

Lf s

Laa

Ra

 

 

 

 

 

 

(b)

 

 

h

 

 

+

 

 

 

 

 

 

Rf

ia

 

 

 

ωLaf if ± ωLasis

va

 

 

 

 

+

 

 

 

 

if

 

k

 

vf

 

 

 

 

 

 

 

 

Lf f

 

 

Fig. 17.4 Compound-connected dc machine equivalent circuit: (a) shunt field connected ahead the series field, and (b) shunt field connected behind the series field

Shunt-Connected DC Machine

The armature and the field windings are connected in parallel (i.e., h ≡ h and k ≡ k ). Hence:

vdc = va = vf , idc = −ia − if

(17.17)

Series-Connected DC Machine

The armature and the field windings are connected in series (i.e., k ≡ h ). Hence:

vdc = va + vf , idc = −ia = −if

(17.18)

Compound-Connected DC Machine

In this case, the machine is equipped with two field windings (see Figure 17.4). The first winding is connected in series, while the second one in parallel with the armature winding. Assuming that vf and if are the voltage and the current, respectively, for the shunt-connected field winding, and vs and is are the voltage and the current, respectively, for the series-connected field winding, the DAE system becomes:

17.6 Other Direct-Current Devices

 

 

 

 

387

 

 

if

Lf f

Lf s

0

 

1

 

(17.19)

 

dt is

= Lf s

±Lss

0

 

 

 

d

ia ±0

 

 

 

 

 

 

 

 

0 Laa

Rs

0

is

 

 

 

vs

0

 

 

 

 

vf

Rf

 

0

0

if

va ωLaf ±ωLas Ra ia

ω˙ = (τe − τm − Dω)/2H

0 = Laf if ia ± Lasisia − τe

where the ± sign indicates either a cumulative or a di erential series connection. Finally, the dc-network interface constraints depend on the field circuit connections, as follows.

(a) Shunt field connected ahead the series field:

 

 

vdc = vs + va = vf ,

idc = −is − if ,

ia = is

(17.20)

(b) Shunt field connected behind the series field:

ia = is − if

 

vdc = vs + va = vs + vf ,

idc = −is,

(17.21)

17.6Other Direct-Current Devices

This section describes three models of nonlinear dc devices, namely the solid oxide fuel cell, the solar photovoltaic cell and the energy battery. These devices are of growing interest for distributed and/or renewable resource generation and energy storage. Furthermore, they have interesting nonlinear DAE models, which is enough for being included in this section.

17.6.1Solid Oxide Fuel Cell

Fuel cells are a promising technology for producing electrical energy. The main issues that complicate the design of e cient and robust fuel cells are related to electrode heating and corrosion. However, fuel cells are expected to play an important role in distributed generation.

A Solid Oxide Fuel Cell (SOFC) model described in this section is based on what was proposed in [124, 159, 226, 273, 362]. Figure 17.5 depicts the

fuel cell scheme, which is based on the following equations:

 

 

 

 

˙

=

1

 

 

 

 

 

 

 

 

 

 

 

4

 

4

 

 

 

 

 

Θ

 

 

(Qe − hcAc(Θ − Θa) − σεAr (Θ

 

− Θa))

 

 

 

(17.22)

 

mg cp

 

 

 

 

p˙H2

= ((qH2 2Kridc)/KH2 − pH2 )/TH2

 

 

 

 

 

 

 

 

p˙H2O = (2Kridc/KH2O − pH2O)/TH2O

 

 

 

 

 

 

 

 

 

 

 

p˙O2

= ((qH2 /rHO − Kridc)/kO2 − pO2 )/TO2

 

 

 

 

 

 

 

 

q˙H2

= (2Kridc/Uopt − qH2 )/Tf

 

 

rΘ

 

 

 

 

 

 

 

 

0

=

 

v

R

 

(Θ)i

 

+

N0

(E

+

ln(p

 

 

/p

 

))

 

 

 

p

 

 

 

 

 

Vdc,n

 

 

 

 

 

dc

 

dc

 

dc

 

0

 

2f

 

 

H2

O2

 

H2O

 

388

 

17 Direct-Current Devices

 

 

Table 17.4 Solid oxide fuel cell parameters

 

 

 

 

 

 

 

 

Variable

Description

Unit

 

 

 

 

 

 

 

Ac

Cell e ective convection area

m2

 

Ar

Cell e ective radiation area

m2

 

 

cp

Average cell specific heat

J/kg/K

 

 

E0

Ideal standard potential

V

 

 

hc

Convection-cooling coe cient

W/K/m2

 

 

KH2

Valve molar constant for hydrogen

-

 

 

KH2O

Valve molar constant for water

-

 

 

KO2

Valve molar constant for oxygen

-

 

 

˜

Mole flow-dc current coe cient

mol/C

 

 

Kr

 

 

mg

Cell mass

kg

 

 

N0

Number of cells in series in the stack

int.

 

 

Qe

Heat generated by the electrochemical reaction

W

 

 

Rdca

Ohmic losses at ambient temperature

pu

 

 

rHO

Ratio of hydrogen to oxygen

-

 

 

Tf

Fuel processor response time

s

 

 

TH2

Response time for hydrogen flow

s

 

 

TH2O

Response time for water flow

s

 

 

TO2

Response time for oxygen flow

s

 

 

Uopt

Optimal fuel utilization

-

 

 

βr

Ohmic loss temperature factor

-

 

 

ε

Emittance

-

 

 

Θa

Ambient temperature

K

 

where σ = 5.670 · 108 W/m2/K4 is the Stefan-Boltzmann’s constant. The first equation defines the thermodynamic energy balance, while second to fifth equations defines the electrochemical reaction dynamics and the last equation defines the fuel cell voltage. In (17.22), pH2 , pO2 and pH2O are the hydrogen, oxygen and water mole fractions, respectively, qH2 , qO2 and qH2O are the hydrogen, oxygen and water flows, respectively, r is the gas constant (r = 8.314 J/mol/K), f is the Faraday constant (f = 96487 C/mol), and the remaining quantities are defined in Table 17.4. The coe cient Kr depends on the number of electrons ne in the reaction, the Faraday f constant and the current rating Idc,n = Sn/Vdc,n, as follows:

˜

neIdc,n

(17.23)

Kr = KrIdc,n =

 

4f

 

 

The ohmic losses modelled through the resistance Rdc are due to the resistance to the flow of ions in the electrolyte and resistance to the flow of electrons through the electrode materials. The resistance depends on the temperature Θ:

R

 

= Ra

eβr (

1

1

)

(17.24)

dc

Θa

Θ

 

dc

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

6.17

 

 

 

 

 

 

 

 

 

 

 

Other

 

 

 

 

 

2Kr

 

 

 

 

Kr

-Direct

5.17.FigSolid

 

 

 

 

 

 

 

 

Rdc

 

 

 

 

_

 

 

 

 

 

DevicesCurrent

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

+

 

 

 

 

 

 

idc

2Kr

1

 

1

 

 

 

 

 

_

 

 

 

 

 

 

 

 

 

fueloxide

Uopt

Tf s + 1

qH2

rHO

qO2

 

 

 

 

+

 

cell

 

 

 

 

1/KH2

 

1/KH2 O

 

 

1/KO2

 

 

 

 

 

TH2 s + 1

 

TH2O s + 1

 

 

TO2 s + 1

 

scheme

 

 

 

 

 

 

 

 

 

 

 

 

pH2

 

pH2O

 

 

pO2

 

 

 

 

 

 

 

 

pH2

pO2

 

_

 

 

 

 

 

 

rΘ

 

 

 

 

 

 

 

 

N0

E0+

ln

 

 

 

 

 

 

 

 

 

 

2f

pH2O

+

vdc

389

390

17 Direct-Current Devices

17.6.2Solar Photovoltaic Cell

Despite their high cost and low e ciency, solar photovoltaic cells are gaining in recent years popularity, thanks to the growing interest in renewable sources and, especially, thanks to public funding. At the moment, the biggest photovoltaic plant capacity is 60 MW,1 but the vast majority of solar plants have a capacity 0.2 MW. However, at least from the modelling viewpoint, photovoltaic plants are quite interesting [174, 177].

The electrical circuit is described by the following equations (see Figure 17.6):

vD

 

idc = iL − iD Rsh

(17.25)

0= vD − vdc − RSeidc

0= is(Θ)(evD /(γvΘ (Θ)) 1) − iD

where iL is the photo-current generated by sunlight, vD and iD are the PN junction voltage and current, respectively, vΘ is the thermal potential, is is the reverse saturation current, and remaining parameters are defined in Table 17.5. The variables vΘ and is can be expressed as:

vΘ (Θ) =

kB Θ

 

(17.26)

qε

 

 

is(Θ) = is0 Θa

3

eϕ(Θ)

 

 

Θ

 

 

where Θ is the cell temperature and the function ϕ(Θ) is:

ϕ(Θ) = γkB

gΘa a

gΘ

 

(17.27)

 

qε

E (Θ )

 

E (Θ)

 

 

and kB = 1.381 · 1023 J/K is the Boltzmann’s constant, , qε = 1.602 · 1019 C is the electron charge, and Eg is the energy band gap, which is a function of the temperature:

Eg (Θ) = Eg0

αg Θ2

(17.28)

βg + Θ

The light-generated current can be linearized around a temperature of 298 K and an irradiance of 1000 W/m2:

0 = (AaρeG + CΘ (Θ − 298.0))

G

Sn

(17.29)

 

 

 

iL

1000

Vdc,n

where G is the solar irradiance or insolation in W/m2.

1This plant was completed in 2008 and is located in Olmedilla de Alarc´on, CastillaLa Mancha, Spain.

17.6 Other Direct-Current Devices

 

 

391

G

+

iD

ish

idc +

iL

 

 

Rse

 

 

 

 

 

vD

 

Rsh

vdc

 

 

 

 

 

 

Fig. 17.6 Equivalent circuit of photovoltaic cells

Finally, the model is completed by an energy-balance di erential equation that regulates the cell heat transfer with the ambient:

Θ˙ =

1

 

S

 

(vdc − vD )2

+ S

 

vD2

+ S i

v

(17.30)

cpmg

 

Rse

n Rsh

 

 

n

 

n

D D

 

+ (1 − ρc − τc − ηc)AaG − hcAc(Θ − Θa) − σεAr (Θ4 − Θa4)

where σ = 5.670 · 108 W/m2/K4 is the Stefan-Boltzmann’s constant and ηc is the cell power conversion e ciency:

ηc =

Snvdcidc

(17.31)

GAa

 

 

The model described above represents a single cell. A panel is composed of a grid of cells connected in series and in parallel. Then a plant is composed of a series of several panels. However, the model above can be also used for representing the entire plant by using proper equivalent parameters. The photovoltaic cell (detailed or equivalent model) has then to be connected to the ac network. This is generally done through a VSC device and proper controllers. An example of controllers are given in Example 18.2 of Chapter 18.

In this model, the solar irradiance G is the input variable since it depends on time t, season, atmospheric conditions, dirtiness of the cell surface, etc. The solar irradiance can be provided as a series of measurements (i.e., (G, t)- value pairs) or approximated using mathematical models [33].

17.6.3Battery Energy System

Storing electrical energy is a hard task. Since capacitors are far from behaving similarly to an ideal capacitance, the only e ective way to store electrical energy is to convert it in another form of energy. For example, batteries are able to store chemical energy, pumping hydro plants store water potential energy, and flywheels store kinetic energy.2

2Example 18.3 of Chapter 18 provides another example of energy storage device based on a superconducting coil (SMES). In this case the electrical energy is converted into magnetic one.

392

 

17 Direct-Current Devices

 

 

Table 17.5 Solar photovoltaic cell parameters

 

 

 

 

 

 

Variable

Description

Unit

 

 

 

 

 

 

 

Aa

Cell active area

m2

 

Ac

Cell e ective convection area

m2

 

 

Ar

Cell e ective radiation area

m2

 

 

CΘ

temperature coe cient of the photo-current iL

A/K

 

 

cp

Average cell specific heat

J/kg/K

 

 

Eg0, αg , βg

Energy band gap function parameters

eV, eV/K, K

 

 

hc

Convection-cooling coe cient

W/K/m2

 

 

is0

Saturation current at Θa

A

 

 

mg

Cell mass

kg

 

 

Rse

Cell body series resistance

pu

 

 

Rsh

Cell body shunt resistance

pu

 

 

γ

Diode ideality factor

-

 

 

ε

Emittance

-

 

 

Θa

Ambient temperature

K

 

 

ρe

Average spectral responsivity

A/W

 

 

ρc

Cell reflection factor

-

 

 

τc

Cell transmission factor

-

 

In recent years, storage devices have gained more and more relevance because they can help systems with stochastic primary energy sources (e.g., wind or solar energy) maintain a smooth power production profile. Among the several existing energy storage devices (e.g., flywheels, electrolyzers, hydrogen storage, etc.), batteries are one of the most promising [235].

A battery is a voltage source that depends on the generated current and on the state of charge (SOC) of the battery itself. There are several battery types, e.g., lead-acid, lithium-ion, lithium-polymer, nickel-cadmium, nickelmetal hydride, zinc-air, etc. A dynamic rechargeable battery model, based on the classical Shepherd’s model, is as follows [278, 314]:

q˙e = idc/3600

(17.32)

˙

im = (idc im)/Tm

0 = voc − vp(qe, im) + vee−βeqe − Riidc − vdc

where qe is the per unit extracted capacity normalized with respect to the maximum battery capacity Qn in Ah, im is the battery current idc passed through a low-pass filter, the polarization voltage vp(qe) depends on the sign of im, as follows:

vp(qe, im) =

Rpim + Kpqe

 

if

 

R i

K

q

(17.33)

 

SOC

 

 

 

 

 

 

 

 

 

 

 

p m

+

 

p e

 

if im < 0 (charge)

 

SOC

qe + 0.1