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[James_H._Harlow]_Electric_Power_Transformer_Engin(BookSee.org)

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L ijo = N i N j ijo (3.10.31)<br />

1.4<br />

where ijo is the average flux cutting each conductor in section i due to the current I j , and where N is the<br />

number of turns in each section, then the inductance (L ij , H) as a function of frequency is:<br />

1.3<br />

L<br />

ij<br />

Lijo<br />

b<br />

tanh( 1<br />

j)<br />

b<br />

( 1<br />

j)<br />

a<br />

a<br />

(3.10.32)<br />

The impedance (Z prox,ij , ) is obtained by multiplying the inductance by the complex variable s. Using<br />

the same notation as in Equation 3.10.29, the impedance of the conductor due to the proximity effect<br />

is given as<br />

H<br />

PER UNIT CAPACITANCE<br />

1.2<br />

1.1<br />

1<br />

BEFORE AGING<br />

AFTER AGING<br />

Z s L ijo<br />

prox<br />

tanh <br />

(3.10.33)<br />

ij<br />

<br />

3.10.7.2 Core Losses<br />

The effect of eddy currents in the core have been represented in various works [26,48,49] by the welltested<br />

formula:<br />

where<br />

(3.10.34)<br />

x= d j <br />

(3.10.35)<br />

2<br />

and where<br />

l = length of the core limb (axial direction), m<br />

d = thickness of the lamination, m<br />

= permeability of the material, H/m<br />

N = number of turns in the coil<br />

A = total cross-sectional area of all laminations<br />

= frequency, rad/sec<br />

This formula represents the equivalent impedance of a coil wound around a laminated iron core limb.<br />

The expression was derived [49] by solving Maxwell’s equations assuming the electromagnetic field<br />

distribution is identical in all laminations and an axial component of the magnetic flux.<br />

The total hysteresis loss in core volume, V, in which the flux density is everywhere uniform and varying<br />

cyclically at a frequency of , can be expressed as:<br />

where<br />

N A<br />

Z 4 2<br />

x x<br />

ld<br />

2 tanh<br />

P h = total hysteresis loss in core<br />

= constant, a function of material<br />

V = core volume<br />

= flux density<br />

n = exponent, dependent upon material, 1.6 to 2.0<br />

= frequency, rad/sec<br />

P h = 2 V n max (3.10.36)<br />

PER UNIT CONDUCTANCE, LOG(G)<br />

0.9<br />

0.8<br />

10 2 10 3 10 4 10 5 10 6 10 7<br />

FREQUENCY, LOG(F)<br />

10 4<br />

10 3<br />

10 2<br />

10 1<br />

10 0<br />

AFTER AGING<br />

10 2 10 3 10 4 10 5 10 6 10 7<br />

FREQUENCY, LOG(F)<br />

FIGURE 3.10.7 Top) Oil-soaked paper capacitance as a function of frequency; bottom) Oil-soaked paper conductance<br />

as a function of frequency.<br />

3.10.7.3 Dielectric Losses<br />

The capacitive structure of a transformer has associated with it parallel losses. At low frequency, the effect<br />

of capacitance on the internal voltage distribution can be ignored. As such, the effect of the losses in the<br />

dielectric structure can be ignored. However, at higher frequencies the losses in the dielectric system can<br />

have a significant effect on the transient response. Batruni et al. [50] explore the effect of dielectric losses<br />

on the impedance-vs.-frequency characteristic of the materials in power transformers. These losses are<br />

frequency dependent and are shown in Figure 3.10.7.<br />

3.10.8 Winding Construction Strategies<br />

BEFORE AGING<br />

3.10.8.1 Design<br />

The successful design of a commercial transformer requires the selection of a simple structure so that<br />

the core and coils are easy to manufacture. At the same time, the structure should be as compact as<br />

possible to reduce required materials, shipping concerns, and footprint. The form of construction should<br />

© 2004 by CRC Press LLC<br />

© 2004 by CRC Press LLC

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