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Machines mechanic tr, Schemes and Mind Maps of Nationality law

Machines mechanic transfer oldu

Typology: Schemes and Mind Maps

2017/2018

Uploaded on 04/24/2025

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56
PROBLEM SOLUTIONS: Chapter 5
Problem 5.1
Basic equations are TΦRFfsin δRF. Since the field current is constant, Ff
is constant, Note also that the resultant flux is proptoortional to the terminal
voltage and inversely to the frequency ΦRVt/f.Thuswecanwrite
TVtsin δRF
f
P=ωfTVtsin δRF
part (a): Reduced to 31.1
part (b): Unchanged
part (c): Unchanged
part (d): Increased to 39.6
Problem 5.2
part (a): The windings are orthogonal and hence the mutual inductance is
zero.
part (b): Since the two windings are orthogonal, the phases are uncoupled
and hence the flux linkage under balanced two-phase operation is unchanged by
currents in the other phase. Thus, the equivalent inductance is simply equal to
the phase self-inductance.
Problem 5.3
Lab =1
2(Laa Lal)=2.25 mH
Ls=3
2(Laa Lal)+Lal =7.08 mH
Problem 5.4
part (a):
Laf =2Vll,rms
3ωIf
=79.4mH
part (b): Voltage = (50/60) 15.4 kV = 12.8 kV.
Problem 5.5
part (a): The magnitude of the phase current is equal to
Ia=40 ×103
0.85 ×3 460 =59.1A
and its phase angle is cos10.85 = 31.8.Thus
pf3
pf4
pf5
pf8
pf9
pfa
pfd
pfe
pff

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PROBLEM SOLUTIONS: Chapter 5

Problem 5. Basic equations are T ∝ ΦRFf sin δRF. Since the field current is constant, Ff is constant, Note also that the resultant flux is proptoortional to the terminal voltage and inversely to the frequency ΦR ∝ Vt/f. T hus we can write

T ∝

Vt sin δRF f

P = ωf T ∝ Vt sin δRF part (a): Reduced to 31. 1 ◦ part (b): Unchanged part (c): Unchanged part (d): Increased to 39. 6 ◦

Problem 5. part (a): The windings are orthogonal and hence the mutual inductance is zero. part (b): Since the two windings are orthogonal, the phases are uncoupled and hence the flux linkage under balanced two-phase operation is unchanged by currents in the other phase. Thus, the equivalent inductance is simply equal to the phase self-inductance.

Problem 5.

Lab = −

(Laa − Lal) = − 2. 25 mH

Ls =

(Laa − Lal) + Lal = 7. 08 mH

Problem 5. part (a):

Laf =

2 Vl−l,rms √ 3 ωIf

= 79.4 mH

part (b): Voltage = (50/60) 15.4 kV = 12.8 kV.

Problem 5. part (a): The magnitude of the phase current is equal to

Ia =

40 × 103

0. 85 ×

= 59.1 A

and its phase angle is − cos−^1 0 .85 = − 31. 8 ◦. T hus

Iˆa = 59. 1 e−j^31.^8 ◦

Then

Eˆaf = Va − jXs Iˆa =^460 √ 3

− j 4. 15 × 59. 1 e−j^31.^8

◦ = 136  − 56. 8 ◦^ V

The field current can be calculated from the magnitude of the generator voltage

If =

2 Eaf ωLaf

= 11.3 A

part (b):

Eˆaf = 266  − 38. 1 ◦^ V; If = 15.3 A

part (c):

Eˆaf = 395  − 27. 8 ◦^ V; If = 20.2 A

Problem 5. The solution is similar to that of Problem 5.5 with the exception that the sychronous impedance jXs is replaced by the impedance Zf + jXs. part (a): Eˆaf = 106  − 66. 6 ◦^ V; If = 12.2 A part (b): Eˆaf = 261  − 43. 7 ◦^ V; If = 16.3 A part (c): Eˆaf = 416  − 31. 2 ◦^ V; If = 22.0 A

Problem 5. part (a):

Laf =

2 Vl−l,rms √ 3 ωIf

= 49.8 mH

part (b):

Iˆa =^600 ×^10

3 √ 3 2300

= 151 A

Eˆaf = Va − jXs Iˆa = 1. 77  − 41. 3 ◦^ V

If =

2 Eaf ωLaf

= 160 A

Problem 5. part (a):

SCR =

AFNL

AFSC

part (b): Zbase = 4160^2 /(5000 × 103 ) = 3.46 Ω

Xs =

SCR

= 1.11 pu = 3.86 Ω

part (c):

Xs,u =

AFSC

AFNL, ag

= 0.88 pu = 3.05 Ω

Problem 5. No numerical solution required.

Problem 5. part (a): The total power is equal to S = P /pf = 4200 kW/0.87 = 4828 kVA. The armature current is thus

Iˆa =^4828 ×^10

3 √ 3 4160

 (cos−^1 0 .87) = 670 29. 5 ◦^ A

Defining Zs = Ra + jXs = 0.038 + j 4 .81 Ω

|Eaf | = |Va − ZsIa| = |

− ZsIa| = 4349 V, line − to − neutral

Thus

If = AFNL

= 306 A

part (b): If the machine speed remains constant and the field current is not reduced, the terminal voltage will increase to the value corresponding to 306 A of field current on the open-circuit saturation characteristic. Interpolating the given data shows that this corresponds to a value of around 4850 V line-to-line.

Problem 5.

Problem 5. At rated power, unity power factor, the armature current will be Ia = 5000 kW/(

3 4160 V) = 694 A. The power dissipated in the armature winding will then equal Parm = 3 × 6942 × 0 .011 = 15.9 kW. The field current can be found from

|Eaf | = |Va − ZsIa| = |

− ZsIa| = 3194 V, line-to-neutral

and thus

If = AFNL

= 319 A

At 125◦C, the field-winding resistance will be

Rf = 0. 279

and hence the field-winding power dissipation will be Pfield = If^2 Rf = 21.1 kW. The total loss will then be

Ptot = Pcore + Parm + Pfriction/windage + Pfield = 120 kW

Hence the output power will equal 4880 kW and the efficiency will equal 4880/ = 0.976 = 97.6%.

part (b): Using generator convention for current

part (c):

Eaf =

= 0.357 per-unit

For Va = 1.0 per-unit,

Iˆa = Eaf^ −^ Va jXs

= 1. 08  90 ◦^ per-unit = 1. 36  90 ◦^ kA

using Ibase = 1255 A. part (d): It looks like an inductor. part (e):

Eaf =

= 1.67 per-unit

For Va = 1.0 per-unit,

Iˆa = Eaf^ −^ Va jXs

= 1. 12  − 90 ◦^ per-unit = 1. 41  − 90 ◦^ kA

In this case, it looks like a capacitor.

Problem 5.

Problem 5. part (a): It was underexcited, absorbing reactive power. part (b): It increased. part (c): The answers are the same.

Problem 5. part (a):

Xs =

= 0.268 per-unit

part (b): P = 0.875 and S = P/ 0 .9 = 0.972, both in per unit. The power- factor angle is − cos−^1 0 .9 = − 25. 8 ◦^ and thus Iˆa = 0. 875  − 25. 8 ◦.

Eˆaf = Va + jXs Iˆa = 1. 15  11. 6 ◦^ per-unit

The field current is If = AFNL| Eˆaf | = 958 A. The rotor angle is 11. 6 ◦^ and the reactive power is

Q =

S^2 − P 2 = 4.24 MVA

part (c): Now |Eaf | = 1.0 per unit.

δ = sin−^1

P Xs Va

|Eaf |

and thus Eˆaf = 1. 0  13. 6 ◦.

Iˆa =

Eˆaf − Va jXs

Q = Imag[Va Iˆ∗ a ] = − 0 .104 per-unit = − 1 .04 MVAR

and

Iˆa = Vte

jδt (^) − V∞ jX∞

= 0. 578  3. 93 ◦^ per-unit

Ibase = Pbase/(

3 Vbase) = 15.64 kA and thus Ia = 9.04 kA. (iii) The generator terminal current lags the terminal voltage by δt/2 and thus the power factor is

pf = cos−^1 δt/2 = 0.998 lagging

(iv)

| Eˆaf | = |V∞ + j(X∞ + Xs) Iˆa| = 1.50 per-unit = 36.0 kV,line-to-line

part (b): (i) Same phasor diagram (ii) Iˆa = 0. 928  6. 32 ◦^ per-unit. Ia = 14.5 kA. (iii) pf = 0.994 lagging (iv) Eaf = 2.06 per unit = 49.4 kV, line-to-line.

Problem 5. part (a):

part (b):

part (c):

Problem 5.

part (a): From the solution to Problem 5.15, Xs = 0.964 per unit. Thus, with V∞ = Eaf = 1.0 per unit

Problem 5.

Problem 5.

Problem 5. For Eaf = 0,

Pmax =

V (^) t^2 2

Xq

Xq

This maximum power occurs for δ = 45◦.

Id =

Vt cos δ Xd

= 0.786 per-unit

Iq =

Vt sin δ Xq

= 1.09 per-unit

and thus Ia =

I^2 d + Iq^2 = 1.34 per unit.

S = VtIa = 1.34 per-unit

Hence

Q =

S^2 − P 2 = 1.32 per-unit

Problem 5.

P =

V∞Eaf Xd

sin δ +

V ∞^2

Xq

Xd

sin 2δ

The generator will remain synchronized as long as Pmax > P. An iterative search with MATLAB can easily be used to find the minimum excitation that satisfies this condition for any particular loading. part (a): For P = 0.5, must have Eaf ≥ 0 .327 per unit. part (b): For P = 1.0, must have Eaf ≥ 0 .827 per unit.

Problem 5. part (a):

part (b): We know that P = 0.95 per unit and that

P =

V∞Vt Xbus

sin δt

and that

Iˆa = Vˆt − V∞ jXt

It is necessary to solve these two equations simultaneously for Vˆt = Vt δt so that both the required power is achieved as well as the specified power factor

part (c):

Problem 5.

f = n × poles 120

3000 × 6

= 150 Hz

Problem 5. part (a): Because the load is resistive, we know that

Ia =

P

3 Va

= 13.5 A

part (b): We know that Eaf = 208/

3 = 120 V. Solving

Eaf =

V (^) a^2 + (XsIa)^2

for Xs gives

Xs =

Eaf^2 − V (^) a^2 Ia

part (c): The easiest way to solve this is to use MATLAB to iterate to find the required load resistance. If this is done, the solution is Va = 108 V (line-to-neutral) = 187 V (line-to-line).

Problem 5.

I^ ˆa = Ea Ra + Rb + jωLa

ωKa Ra + Rb + jωLa

Thus

| Iˆa| = ωKa √ (Ra + Rb)^2 + (ωLa) 2

Ka

La

Ra +Rb ωLa

Clearly, Ia will remain constant with speed as long as the speed is sufficient to insure that ω >> (Ra + Rb)/La