Skip to content
Stan’s Legacy

book

Theory and Calculation of Alternating Current Phenomena (1900) — part 5 of 19

1 January 1900

ratio of potentials, in Curve II., Curve IV., and Curve VI.;

Curves I. and II. refer to a non-inductive receiver circuit ;

RESISTANCE OF TRANSMISSION LINES,

Curves III. and IV. refer to a receiver circuit of

constant susceptance b = .142

Curves V. and VI. refer to a receiver circuit of

constant susceptance b = — .142 ;

Curves VII. and VIII. refer to a non-inductive re- ceiver circuit and non-inductive line.

In Fig. 59, the output is shown as Curve I., and the ratio of potentials as Curve II., for the same line constants, fora constant conductance, ^- = .0592 ohms, and for variable susceptances, b, of the receiver circuit.

OUTPUT P /NO RATIO OF POTENTIAL a t SENDING END OF LINE OF IMPEDANCE. Z0

T RECEIV1 NG^ND =5.5 -3j

AT

CON

TAN

g= . 0592

1 OUTPUT II RATIO OF POTENTIALS —

/

\

/

\

/

\

/

\

/

\

/

\

/

I

/

/

Ns

f

\

1

/

\

\

/

\

/

5

/

\

/

'/

\

\

/

7

/

/

\

\

/

P

\

\

X

-<,

~^_

^

' — -.

SUSCEfA

°T'

iECE

IVE

R C

KCU

IT

-.3 -.2 -.1 0 +.1 +.2 +.3 +.4

Fig. 59. Variation of Potential in Line at Various Loads.

3.) Maximum Efficiency.

  1. The output, for a given conductance, g, of a receiver circuit, is a maximum if b = — b0. This, however, is gen- erally not the condition of maximum efficiency.

94 ALTERNATING-CURRENT PHENOMENA.

The loss of energy in the line is constant if the current is constant ; the output of the generator for a given cur- rent and given generator E.M.F. is a^aximum if the cur- rent is in phase with the E.M.F. at the generator terminals. Hence the condition of maximum output at given loss, or of maximum efficiency, is —

tan £>0 = 0. The current is —

The current I0, is in phase with the E.M.F., E0, if its quadrature component — that is, the imaginary term — dis- appears, or

x + Xo = 0.

This, therefore, is the condition of maximum efficiency,

Hence, the condition of maximum efficiency is, that the reactance of the receiver circuit shall be equal, but of oppo- site sign, to the reactance of the line.

Substituting x = — x0, we have, ratio of E.M.Fs.,

power,

RESISTANCE OF TRANSMISSION LINES.

95

and depending upon the resistance only, and not upon the reactance.

This power is a maximum if g = g0, as shown before; hence, substituting g = g0, r = r0,

E 2

maximum power at maximum efficiency, Pm = —2— ,

at a ratio of potentials, am — — -2— ,

" ro

or the same result as in § 62.

.01 .03 • .03 .01 .05 .06 .07 .08

Fig. 60. Load Characteristic of Transmission Line.

In Fig. 60 are shown, for the constants — E0 = 1,000 volts, Z0 =2.5 — 6/; r0 = 2.5 ohms, x0 = 6 ohms, z0 = 6.5 ohms,

96 ALTERNATING-CURRENT PHENOMENA.

and with the variable conductances, g, of the receiver circuit as abscissae, the —

Output at maximum efficiency, (Curve I.) ;

Volts at receiving end of line, (Curve II.) ;

Efficiency = • , (Curve III.).

r + r0

4.) Control of Receiver Voltage by Shunted Snsceptance.

  1. By varying the susceptance of the receiver circuit, the potential at the receiver terminals is varied greatly. Therefore, since the susceptance of the receiver circuit can be varied at will, it is possible, at a constant generator E.M.F., to adjust the receiver susceptance so as to keep the potential constant at the receiver end of the line, or to vary it in any desired manner, and independently of the generator potential, within certain limits.

The ratio of E.M.Fs. is —

If at constant generator potential E0, the receiver potential E shall be constant,

a — constant ; hence,

#2' or, expanding,

which is the value of the susceptance, b, as a function of the receiver conductance, — that is, of the load, — which is required to yield constant potential, aE0, at the receiver circuit.

For increasing g, that is, for increasing load, a point is reached, where, in the expression —

b = -

RESISTANCE OF TRANSMISSION LINES.

97

the term under the root becomes imaginary, and it thus becomes impossible to maintain a constant potential, aE0. Therefore, the maximum output which can be transmitted at potential aE0, is given by the expression —

hence b = — o0 ,

and g = — g0 --

the susceptance of receiver circuit, the conductance of receiver circuit;

°- —f» the output.

  1. If a = 1, that is, if the voltage at the receiver cir- cuit equals the generator potential —

P=E*(ty00'-g0). If a = 1 when g = 0, b = 0

when g > 0, b < 0 ; if a > 1 when g = 0, or g > 0, b < 0,

that is, condensance; if a < 1 when g = 0, b > 0,

when g = - #, + /f — ^ - <V, ^ = 0 ; when^> -g0 + V/f — ^ - V, * < 0,

or, in other words, if a < 1, the phase difference in the main line must change from lag to lead with increasing load.

  1. The value of a giving the maximum possible output in a receiver circuit, is determined by dP / da = 0 ;

expanding : 2 a (yJL - g\ _ f!f' = 0 ;

\a J a

hence, y0 = 2ag0,

yo 1 Zo

" = = =

98 ALTERNATING-CURRENT PHENOMENA.

the maximum output is determined by —

S == So i = So I

and is, P = —2- .

4 r

From : a = ^ = -^- ,

the line reactance, x0, can be found, which delivers a maximum output into the receiver circuit at the ratio of potentials, a, and z0 = 2 r0 a,

for a == 1,

If, therefore, the line impedance equals 2# times the line resistance, the maximum output, P = E* j ± r0, is trans- mitted into the receiver circuit at the ratio of potentials, a.

If z0 = 2 r0, or x0 = r0 V3, the maximum output, P = £02/4:r0, can be supplied to the receiver circuit, without change of potential at the receiver terminals.

Obviously, in an analogous manner, the law of variation of the susceptance of the receiver circuit can be found which is required to increase the receiver voltage proportionally to the load ; or, still more generally, — to cause any desired variation of the potential at the receiver circuit indepen- dently of any variation of the generator potential, as, for in- stance, to keep the potential of a receiver circuit constant, even if the generator potential fluctuates widely.

  1. In Figs. 61, 62, and 63, are shown, with the output, P = E* g a2, as abscissae, and a constant impressed E.M.F., E0 = 1,000 volts, and a constant line impedance, Z0 = 2.5 — 6/, or, r0 = 2.5 ohms, x0 = 6 ohms, z = 6.5 ohms, the following values :

RATIO'OF RECEIVER VOLTAGE TO SENDER VOLTAGE: d =I.O

LINE IMPEDANCE: Z0= a. 5— 6;

ENERGY CURRENT CONSTANT GENERATOR

TOTAL CURRENT

CURRENT IN NON-INDUCTIVE RECEIVER CIRCUIT WITHOUT COMPENSATION

OUTPUT] IN RECEIVER CIPJCUIT, KILOWJATT 50 60 70 80

Fig. 61. Variation of Voltage Transmission Lines.

• .

RATIO OF RECEIVER VOLTAGE TO SENDER VOLTAGE: LINE MPEDANCE:Z_ = 2.5.— 6J . ENERGY CURRENT CONSTANT GENRATOR POT II. REACTIVE CURRENT III. TOTAL CURRENT IV. POTENTIAL IN NON-INDUCTIVE CIRCUIT WITHOUT C

~|Tt-MJJ MINI

a =.7 :NTIAL E

OMPENS

0= I

~

300

• ' .

DLTS 1000

uoo

too

roo

GOO M) 400 300 200 100 0

""-

:


-^. 

— 

— 

*-•, 

~—  ^. 

* 

V 

nr 

\ 

x 

//' 

"^ 

-^ 

//s 

\ 

\ 

"*x- 

^^ 

\ 

x 

2 

S 

/^ 

A 

1 

, 

s 

^- 

^ 

^T 

) 

^S 

^~ 

^^-* 

•*^=: 

— 

— 

— 

^ 

>^ 

/ 

^ 

^y 

*~^ 

-^. 

•*fc 

x 

f  

-" 

* 

^^ 

•^, 

^> 

-^ 

^ 

—1  — 

—  - 

_____ 

-.  — 

=rrT 

—- 

,  —  • 

01 

r?v 

T   IN 

RE 

iEIV 

x  c 

RC 

IT, 

<ILO 

.VAT 

TS 

30  W  50  CO  70  80 

Fig.  62.     Variation  of  Voltaqe  Transmission  Lines. 

100 

AL  TERNA  TING-CURRENT  PHENOMENA. 

RATIO  OF  RECEIVER  VOLTAGE  TO  SEN  DER  VOLTAGE:  a  =1.3 

INE  IMPEDANCE:  Z0=2.5.— ej" 

CONSTANT  GENERATOR  POTENTIAL  E0=IOOOl 

I.    ENERGY  CURRENT 

II.  "REACTIVE  CURRENT 

III.  TOTAL  CURRENT 

IV.  POTENTIAL  IN  NON-INDUCTIVE  RECEIVER  CIRCUIT  WITHOUT  COMPENSATION 

OUTPUT    N  RECEIVER  C  RCUIT,     KILOWATTS 

30  10  80  60  70  80  90 

Fig.  63.     Variation  of  Voltage  Transn\jssion  Lines. 

Energy  component  of  current,  gE,    (Curve  I.)  ; 

Reactive,  or  wattless  component  of  current,    bE,    (Curve  II.)  ; 
Total  current,  yE,    (Curve  III.)  ; 

for  the  following  conditions  : 

a  =  1.0  (Fig.  61)  ;     a  =    .7  (Fig.  62)  ;     a  =  1.3  (Fig.  63). 

For  the  non-inductive  receiver  circuit  (in  dotted  lines), 
the  curve  of  E.M.F.,  E,  and  of  the  current,  I  =  gE,  are 
added  in  the  three  diagrams  for  comparison,  as  Curves  IV. 
and  V. 

As  shown,  the  output  can  be  increased  greatly,  and  the 
potential  at  the  same  time  maintained  constant,  by  the  judi- 
cious use  of  shunted  reactance,  so  that  a  much  larger  out- 
put can  be  transmitted  over  the  line  at  no  drop,  or  even  at 
a  rise,  of  potential. 

RESISTANCE   OF   TRANSMISSION  LINES. 

101 

5.)    Maximum  Rise  of  Potential  at  Receiver  Circuit. 

70.  Since,  under  certain  circumstances,  the  potential  at 
the  receiver  circuit  may  be  higher  than  at  the  generator, 
it  is  of  interest  to  determine  what  is  the  maximum  value  of 
potential,  E,  that  can  be  produced  at  the  receiver  circuit 
with  a  given  generator  potential,  E0  . 

The  condition  is  that 

a  =  maxmum  or  —  =  mnmum : 
a2 

that  is, 

substituting, 

r0g  + 

(*0g  - 

and  expanding,  we  get, 

dg      =  °;      gss~"£'' 

—  a  value  which  is  impossible,  since  neither  r0  nor  g  can  be 
negative.  The  next  possible  value  is  g  —  0,  —  a  wattless 
circuit. 

Substituting  this  value,  we  get, 

and  by  substituting,  in 

, 

b  +  b0  =  0  ; 

that  is,  the  sum  of  the  susceptances  =  0,  or  the  condition 
of  resonance  is  present. 
Substituting, 

*=-*-£, 
we  have 

102  AL  TERNA  TING-CURRENT  PHENOMENA. 

The  current  in  this  case  is, 

or  the  same  as  if  the  line  resistance  were  short-circuited 
without  any  inductance. 

This  is  the  condition  of  perfect  resonance,  with  current 
and  E.M.F.  in  phase. 

\ 

s 

\ 

\ 

VOLT 

^ 

\ 

\ 

\ 

\ 

1SOO 
1700 
1COO 
1500 
-1400 

\ 

\ 

\\ 

\ 

\ 

CONSTANT  IMPRESSED  E.  M.  F.    Eo^lOOO 
"           LINE  IMPEDANCE  Z0=2.5-  € 
1    MAXIMUM  OUTPUT  BY  COMPENSATION 
II    MAXIMUM  EFFICIENCY  BY  COMPENSATIC 
III    NON-INDUCTiVE  RECEIVER  C  RCU  T 
IV    NON-INDUCTIVE  LINE  AND  NON-INDUCT 
RECEIVER  CIRCUIT 

If 

\ 

IN 

\ 

IVE 

1200 

1100 
1000 

l\ 

> 

s  1 

GOO 
800 
700 
COO 

* 

"-^ 

•^ 

SEC 

JFF 

C1EN_ 

*-. 

-* 

fa 

"N 

^ 

^ 

/^ 

5 

L 

•\ 

// 

tV 

i 

/ 

^ 

\ 

8 

/f 

// 

300 
200 
100 

A 

^ 

'       ., 

/\v 

^ 

tc)P 

^> 

4 

/ 

^  — 

*.ovJS 

^"\ 
PUT 

PUT 

K.W 

0        ' 

i)  i 

it 

Fig.  64.    Efficiency  and  Output  of  Transmission  Line. 

71.  As  summary  to  this  chapter,  in  Fig.  64  are  plotted, 
for  a  constant  generator  E.M.F.,  E0  =  1000  volts,  and  a 
line  impedance,  Z0  =  2.5  —  6/,  or,  r0  =  2.5  ohms,  x0  =  6 
ohms,  z0  =  6.5  ohms  ;  and  with  the  receiver  output  as 

RESISTANCE   OF  TRANSMISSION  LINES.  103 

abscissae   and    the    receiver  voltages    as    ordinates,   curves 
representing  — 

the  condition  of  maximum  output,  (Curve      I.)  ; 

the  condition  of  maximum  efficiency,  (Curve    II.)  ; 

the  condition  b  =  0,  or  a  non-inductive  receiver  cir- 
cuit, (Curve  III.)  ; 

the  condition  b  =  0,   b0  =  0,  or  a  non-inductive  line  and  non- 
inductive  receiver  circuit. 

In  conclusion,  it  may  be  remarked  here  that  of  the 
sources  of  susceptance,  or  reactance, 

a  choking  coil  or  reactive  coil  corresponds  to  an  inductance ; 
a  condenser  corresponds  to  a  condensance  ; 

a  polarization  cell  corresponds  to  a  condensance  ; 

a  synchronizing  alternator  (motor  or  generator)  corresponds  to 

an  inductance  or  a  condensance,  at  will; 
an  induction  motor  or  generator  corresponds  to  an  inductance. 

The  choking  coil  and  the  polarization  cell  are  specially 
suited  for  series  reactance,  and  the  condenser  and  syn- 
chronizer for  shunted  susceptance. 

104  ALTERNATING-CURRENT  PHENOMENA. 

CHAPTER    X. 

EFFECTIVE    RESISTANCE    AND    REACTANCE. 

72.    The  resistance  of  an  electric  circuit  is  determined :  — 

1.)  By  direct  comparison  with  a  known  resistance  (Wheat- 
stone  bridge  method,  etc.). 

This  method  gives  what  may  be  called  the  true  ohmic 
resistance  of  the  circuit. 

2.)    By  the  ratio  : 

Volts  consumed  in  circuit 

Amperes  in  circuit 

In  an  alternating-current  circuit,  this  method  gives,  not 
the  resistance  of  the  circuit,  but  the  impedance, 

3.)    By  the  ratio  : 

r__  Power  consumed  . 

(Current)2 

where,  however,  the  "power"  does  not  include  the  work 
done  by  the  circuit,  and  the  counter  E.M.Fs.  representing 
it,  as,  for  instance,  in  the  case  of  the  counter  E.M.F.  of  a 
motor. 

In  alternating-current  circuits,  this  value  of  resistance  is 
the  energy  coefficient  of  the  E.M.F., 

_  Energy  component  of  E.M.F. 

Total  current 

It  is  called  the  effective  resistance  of  the  circuit,  since  it 
represents  the  effect,  or  power,  expended  by  the  circuit. 
The  energy  coefficient  of  current, 

a._  Energy  component  of  current 

Total  E.M.F. 
is  called  the  effective  conductance  of  the  circuit. 

EFFECTIVE  RESISTANCE  AND   REACTANCE.        105 

In  the  same  way,  the  value, 

_  Wattless  component  of  E.M.F. 

Total  current 
is  the  effective  reactance,  and 

,  _  Wattless  component  of  current 
TotafE.M.F. 

is  the  effective  susceptance  of  the  circuit. 

While  the  true  ohmic  resistance  represents  the  expendi- 
ture of  energy  as  heat  inside  of  the  electric  conductor  by  a 
current  of  uniform  density,  the  effective  resistance  repre- 
sents the  total  expenditure  of  energy. 

Since,  in  an  alternating-current  circuit  in  general,  energy 
is  expended  not  only  in  the  conductor,  but  also  outside  of 
it,  through  hysteresis,  secondary  currents,  etc.,  the  effective 
resistance  frequently  differs  from  the  true  ohmic  resistance 
in  such  way  as  to  represent  a  larger  expenditure  of  energy. 

In  dealing  with  alternating-current  circuits,  it  is  necessary, 
therefore,  to  substitute  everywhere  the  values  "effective  re- 
sistance," "effective  reactance,"  "effective  conductance," 
and  "  effective  susceptance,"  to  make  the  calculation  appli- 
cable to  general  alternating-current  circuits,  such  as  induc- 
tances, containing  iron,  etc. 

While  the  true  ohmic  resistance  is  a  constant  of  the 
circuit,  depending  only  upon  the  temperature,  but  not  upon 
the  E.M.F.,  etc.,  the  effective  resistance  and  effective  re- 
actance are,  in  general,  not  constants,  but  depend  upon 
the  E.M.F.,  current,  etc.  This  dependence  is  the  cause 
of  most  of  the  difficulties  met  in  dealing  analytically  with 
alternating-current  circuits  containing  iron. 

73.  The  foremost  sources  of  energy  loss  in  alternating- 
current  circuits,  outside  of  the  true  ohmic  resistance  loss, 
are  as  follows : 

1.)    Molecular  friction,  as, 

a.)    Magnetic  hysteresis ; 
b.)   Dielectric  hysteresis. 

106  .ALTERNATING-CURRENT  PHENOMENA. 

2.)   Primary  electric  currents,  as, 

a.}   Leakage  or  escape  of  current  through  the  insu- 
lation, brush  discharge  ;  b.)  Eddy  currents  in 
the  conductor  or  unequal  current  distribution. 
3.)  Secondary  or  induced  currents,  as, 

a.)  Eddy  or  Foucault  currents  in  surrounding  mag- 
netic materials  ;  b.}  Eddy  or  Foucault  currents 
in  surrounding  conducting  materials  ;  c.}  Sec- 
ondary currents  of  mutual  inductance  in  neigh- 
boring circuits. 

4.)  Induced  electric  charges,  electrostatic  influence. 
While  all  these  losses  can  be  included  in  the  terms  effec- 
tive resistance,  etc.,  only  the  magnetic  hysteresis  and  the 
eddy  currents  in  the  iron  will  form  the  subject  of  what  fol- 
lows, since  they  are  the  most  frequent  and  important  sources 
of  energy  loss. 

Magnetic  Hysteresis. 

74.  In  an  alternating-current  circuit  surrounded  by  iron 
or  other  magnetic  material,  energy  is  expended  outside  of 
the  conductor  in  the  iron,  by  a  kind  of  molecular  friction, 
which,  when  the  energy  is  supplied  electrically,  appears  as 
magnetic  hysteresis,  and  is  caused  by  the  cyclic  reversals  of 
magnetic  flux  in  the  iron  in  the  alternating  magnetic  field. 

To  examine  this  phenomenon,  first  a  circuit  may  be  con- 
sidered, of  very  high  inductance,  but  negligible  true  ohmic 
resistance ;  that  is,  a  circuit  entirely  surrounded  by  iron,  as, 
for  instance,  the  primary  circuit  of  an  alternating-current 
transformer  with  open  secondary  circuit. 

The  wave  of  current  produces  in  the  iron  an  alternating 
magnetic  flux  which  induces  in  the  electric  circuit  an  E.M.F., 
—  the  counter  E.M.F.  of  self-induction.  If  the  ohmic  re- 
sistance is  negligible,  that  is,  practically  no  E.M.F.  con- 
sumed by  the  resistance,  all  the  impressed  E.M.F.  must  be 
consumed  by  the  counter  E.M.F.  of  self-induction,  that  is, 
the  counter  E.M.F.  equals  the  impressed  E.M.F.  ;  hence,  if 

EFFECTIVE   RESISTANCE   AND   REACTANCE. 

107 

the  impressed  E.M.F.  is  a  sine  wave,  the  counter  E.M.F., 
and,  therefore,  the  magnetic  flux  which  induces  the  counter 
E.M.F.  must  follow  a  sine  wave  also.  The  alternating  wave 
of  current  is  not  a  sine  wave  in  this  case,  but  is  distorted 
by  hysteresis.  It  is  possible,  however,  to  plot  the  current 
wave  in  this  case  from  the  hysteretic  cycle  of  magnetic  flux. 
From  the  number  of  turns,  n,  of  the  electric  circuit, 
the  effective  counter  E.M.F.,  E,  and  the  frequency,  N, 
of  the  current,  the  maximum  magnetic  flux,  <j>,  is  found 
by  the  formula  : 

hence, 

E  108 

A  maximum  flux,  <£,  and  magnetic  cross-section,  S,  give 
the  maximum  magnetic  induction,  (B  =  $  /  6". 

If  the  magnetic  induction  varies  periodically  between 
+  (B  and  —  (B,  the  M.M.F.  varies  between  the  correspond- 
ing values  -f  ff  and  —  JF,  and  describes  a  looped  curve,  the 
cycle  of  hysteresis. 

If  the  ordinates  are  given  in  lines  of  magnetic  force,  the 
abscissae  in  tens  of  ampere-turns,  then  the  area  of  the  loop 
equals  the  energy  consumed  by  hysteresis  in  ergs  per  cycle. 

From  the  hysteretic  loop  the  instantaneous  value  of 
M.M.F.  is  found,  corresponding  to  an  instantaneous  value 
of  magnetic  flux,  that  is,  of  induced  E.M.F.  ;  and  from  the 
M.M.F.,  JF,  in  ampere-turns  per  unit  length  of  magnetic  cir- 
cuit, the  length,  /,  of  the  magnetic  circuit,  and  the  number  of 
turns,  «,  of  the  electric  circuit,  are  found  the  instantaneous 
values  of  current,  i,  corresponding  to  a  M.M.F.,  JF;  that  is, 
magnetic  induction  (B,  and  thus  induced  E.M.F.  e,  as  : 

75.  In  Fig.  65,  four  magnetic  cycles  are  plotted,  with 
maximum  values  of  magnetic  inductions,  (B  =  2,000,  6,000, 
10,000,  and  16,000,  and  corresponding  maximum  M.M.Fs., 

108 

AL  TERNA  TING-CURRENT  PHENOMENA. 

SF  =  1.8,  2.8,  4.3,  20.0.  They  show  the  well-known  hys- 
teretic  loop,  which  becomes  pointed  when  magnetic  satu- 
ration is  approached. 

These  magnetic  cycles  correspond  to  average  good  sheet 
iron  or  sheet  steel,  having  a  hysteretic  coefficient,  77  =  .0033, 
and  are  given  with  ampere-turns  per  cm  as  abscissae,  and 
kilo-lines  of  magnetic  force  as  ordinates. 

a 

M 

«</.  65.    Hysteretic  Cycle  of  Sheet  Iron. 

In  Figs.  66,  67,  68,  and  69,  the  curve  of  magnetic  in- 
duction as  derived  from  the  induced  E.M.F.  is  a  sine  wave. 
For  the  different  values  of  magnetic  induction  of  this  sine 
curve,  the  corresponding  values  of  M.M.F.,  hence  of  current, 
are  taken  from  Fig.  65,  and  plotted,  giving  thus  the  exciting 
current  required  to  produce  the  sine  wave  of  magnetism ; 
that  is,  the  wave  of  current  which  a  sine  wave  of  impressed 
E.M.F.  will  send  through  the  circuit. 

EFFECTIVE  RESISTANCE  AND  REACTANCE.        109 

As  shown  in  Figs.  66,  67,  68,  and  69,  these  waves  of 
alternating  current  are  not  sine  waves,  but  are  distorted  by 
the  superposition  of  higher  harmonics,  and  are  complex 
harmonic  waves.  They  reach  their  maximum  value  at  the 
same  time  with  the  maximum  of  magnetism,  that  is,  90° 

1=2000 

1.6 

N 

^ 

\ 

(Bfeooo 

T2.8 

3  =2.S 

M\ 

\\ 

Figs.  66  and  67.     Distortion  of  Current  Waue  by  Hysteresis. 

ahead  of  the  maximum  induced  E.M.F.,  and  hence  about 
90°  behind  the  maximum  impressed  E.M.F.,  but  pass  the 
zero  line  considerably  ahead  of  the  zero  value  of  magnet- 
ism, or  42°,  52°,  50°,  and  41  °,  respectively. 

The  general  character  of  these  current  waves  is,  that  the 
maximum  point  of  the  wave  coincides  in  time  with  the  max- 

110 

ALTERNA  TING-CURRENT  PHENOMENA. 

imum  point  of  the  sine  wave  of  magnetism  ;  but  the  current 
wave  is  bulged  out  greatly  at  the  rising,  and  hollowed  in  at 
the  decreasing,  side.  With  increasing  magnetization,  the 
maximum  of  the  current  wave  becomes  more  pointed,  as 
shown  by  the  curve  of  Fig.  68,  for  (B  =  10,000  ;  and  at  still 

(B- 

10000 

4. 

& 

NX 

\L 

.  16000 

20 

\ 

G 

13 

\ 

F/SfS.  88  and  69.    Distortion  of  Current  Waue  by  Hysteresis. 

higher  saturation  a  peak  is  formed  at  the  maximum  point, 
as  in  the  curve  of  Fig.  69,  for  (B  =  16,000.  This  is  the  case 
when  the  curve  of  magnetization  reaches  within  the  range  of 
magnetic  saturation,  since  in  the  proximity  of  saturation  the 
current  near  the  maximum  point  of  magnetization  has  to 
rise  abnormally  to  cause  even  a  small  increase  of  magneti- 
zation. The  four  curves,  Figs.  66,  67,  68,  and  69,  are  not 
drawn  to  the  same  scale.  The  maximum  values  of  M.M.F., 

EFFECTIVE  RESISTANCE  A.\D  REACTANCE-     111 

corresponding  to  the  maximum  values  of  magnetic  induction, 
(B  =  2,000,  6,000,  10,000,  and  16,000  lines  of  force  per  cm2, 
'arc  &  =  1.8,  2.8,  4.3,  and  20.0  ampere-turns  per  cm.  In 
the  different  diagrams  these  are  represented  in  the  ratio  of 
8  :  6  :  4  :  1,  in  order  to  bring  the  current  curves  to  approxi- 
mately the  same  height.  The  M.M.F.,  in  C.G.S.  units,  is 
J#r=47r/103r  =  1.257  IF. 

76.  The  distortion  of  the  wave  of  magnetizing  current 
is  as  large  as  shown  here  only  in  an  iron-closed  magnetic 
circuit  expending  energy  by  hysteresis  only,  as  in  an  iron- 
clad transformer  on  Open  secondary  circuit.     As  soon  as  the 
circuit  expends  energy  in  any  other  way,  as  in  resistance,  or 
by  mutual  inductance,  or  if  an  air-gap  is  introduced  in  the 
magnetic  circuit,  the  distortion  of  the  current  wave  rapidly 
decreases  and  practically  disappears,  and  the  current  becomes 
more  sinusoidal.     That  is,  while  the  distorting  component 
remains  the  same,  the  sinusoidal  component  of  the  current 
greatly  increases,  and  obscures  the  distortion.     For  example, 
in  Figs.  70  and  71,  two  waves  are  shown,  corresponding  in 
magnetization  to  ^the  curve  of    Fig.  67,  as  the  one  most 
distorted.     The  curve  in  Fig.  70  is  the  current  wave  of  a 
transformer  at  TV  load.     At  higher  loads  the  distortion  is 
correspondingly  still  less,  except  where  the  magnetic  flux  of 
self-induction,  that  is,  flux  passing  between  primary  and  sec- 
ondary, and  increasing  proportionally  to  the  load,  is  so  large 
as  to  reach  saturation,  in  which  .case  a  distortion  appears 
again  and  increases  with  increasing  load.     The  curve  of  Fig. 
71  is  the  exciting  current  of  a  magnetic  circuit  containing 
an  air-gap  whose  length  equals  ?^  the  length  of  the  magnetic 
circuit.    These  two  curves  are  drawn  to  £  the  size  of  the  curve 
in  Fig.  67.    As  shown,  both  curves  are  practically  sine  waves. 
The  sine  curves  of  magnetic  flux  are  shown  dotted  as  <£. 

77.  The  distorted  wave  of  current  can  be  resolved  into 
two  components  :  A  true  sine  wave  of  equal  effective  intensity 
nnd  equal  power  to  the  distorted  wave,  called  the  equivalent 

112 

ALTERNATING-CURRENT  PHENOMENA. 

sine  wave,  and  a  wattless  JiigJier  harmonic,  consisting  chiefly 
of  a  term  of  triple  frequency. 

In  Figs.  66  to  71  are  shown,  as  /,  the  equivalent  sine' 

\ 

\ 

v 

\ 

Figs.  70  and  71.    Distortion  of  Current  Wave  by  Hysteresis. 

waves  and  as  i,  the  difference  between  the  equivalent  sine 
wave  and  the  real  distorted  wave,  which  consists  of  wattless 
complex  higher  harmonics.  The  equivalent  sine  wave  of 
M.M.F.  or  of  current,  in  Figs.  66  to  69,  leads  the  magnet- 

EFFECTIVE  RESISTANCE  AND  REACTANCE.        113 

ism  by  34°,  44°,  38°,  and  15°. 5,  respectively.  In  Fig.  71 
the  equivalent  sine  wave  almost  coincides  with  the  distorted 
curve,  and  leads  the  magnetism  by  only  9°. 

It  is  interesting  to  note,  that  even  in  the  greatly  dis- 
torted curves  of  Figs.  66  to  68,  the  maximum  value  of  the 
equivalent  sine  wave  is  nearly  the  same  as  the  maximum 
value  of  the  original  distorted  wave  of  M.M.F.,  so  long  as 
magnetic  saturation  is  not  approached,  being  1.8,  2.9,  and 
4.2,  respectively,  against  1.8,  2.8,  and  4.3,  the  maximum 
values  of  the  distorted  curve.  Since,  by  the  definition,  the 
effective  value  of  the  equivalent  sine  wave  is  the  same  as 
that  of  the  distorted  wave,  it  follows,  that  this  distorted 
wave  of  exciting  current  shares  with  the  sine  wave  the 
feature,  that  the  maximum  value  and  the  effective  value 
have  the  ratio  of  V2  -f-  1.  Hence,  below  saturation,  the 
maximum  value  of  the  distorted  curve  can  be  calculated 
from  the  effective  value  —  which  is  given  by  the  reading 
of  an  electro-dynamometer  —  by  using  the  same  ratio  that 
applies  to  a  true  sine  wave,  and  the  magnetic  characteris- 
tic can  thus  be  determined  by  means  of  alternating  cur- 
rents, with  sufficient  exactness,  by  the  electro-dynamometer 
method,  in  the  range  below  saturation. 

78.  In  Fig.  72  is  shown  the  true  magnetic  character- 
istic of  a  sample  of  good  average  sheet  iron,  as  found  by 
the  method  of  slow  reversals  with  the  magnetometer  ;  for 
comparison  there  is  shown  in  dotted  lines  the  same  char- 
acteristic, as  determined  with  alternating  currents  by  the 
electro-dynamometer,  with  ampere-turns  per  cm  as  ordi- 
nates,  and  magnetic  inductions  as  abscissas.  As  repre- 
sented, the  two  curves  practically  coincide  up  to  a  value  of 
&  =  13,000  ;  that  is,  up  to  the  highest  inductions  practicable 
in  alternating-current  apparatus.  For  higher  saturations, 
the  curves  rapidly  diverge,  and  the  electro-dynamometer 
curve  shows  comparatively  small  M.M.Fs.  producing  appar- 
ently very  high  magnetizations. 

114 

AL  TERN  A  TING-CUR  RE  KT  PHENOMENA. 

The  same  Fig.  72  gives  the  curve  of  hysteretic  loss,  in 
ergs  per  cm3  and  cycle,  as  ordinates,  and  magnetic  induc- 
tions as  abscissae. 

TT 

\ 

/ 

/ 

/       / 
/ 

18 

/ 

/ 
/ 

17 

r 

1 
1 

/I 

' 

/ 

/ 

/ 

/ 

/ 

/ 

/ 

' 

/ 

/ 

1 

/ 

/ 

I. 

' 

/ 

// 

/ 

/ 

1 

/ 

I 

/ 

/ 

/ 

/' 

/ 

^ 

^ 

/ 

^" 

^ 

^^ 

^ 

;  j^ 

* 

x 

2=EE 

x^^ 

£=1,000  2,000   3,000  1.0CO  5,000  6,000  7,000  8,000   9,000  10,000  11,000  12,000  13,0<W14,000  15, 
Fig.  72.    Magnetization  and  Hysteresis  Curve. 

woie.ooo  iv.ow 

The  electro-dynamometer  method  of  determining  the 
magnetic  characteristic  is  preferable  for  use  with  alter- 
nating-current apparatus,  since  it  is  not  affected  by  the 
phenomenon  of  magnetic  "creeping,"  which,  especially  at 

EFFECTIVE  RESISTANCE  AND  REACTANCE.         115 

low  densities,  may  in  the  magnetometer  tests  bring  the  mag- 
netism very  much  higher,  or  the  M.M.F.  lower,  than  found 
in  practice  in  alternating-current  apparatus. 

So  far  as  current  strength"  and  energy  consumption  are 
concerned,  the  distorted  wave  can  be  replaced  by  the  equi- 
valent sine  wave,  and  the  higher  harmonics  neglected. 

All  the  measurements  of  alternating  currents,  with  the 
single  exception  of  instantaneous  readings,  yield  the  equiv- 
alent sine  wave  only,  and  suppress  the  higher  harmonic  ; 
since  all  measuring  instruments  give  either  the  mean  square 
of  the  current  wave,  or  the  mean  product  of  instantaneous 
values  of  current  and  E.M.F.,  which,  by  definition,  are  the 
same  in  the  equivalent  sine  wave  as  in  the  distorted  wave. 

Hence,  in  all  practical  applications,  it  is  permissible  to 
neglect  the  higher  harmonic  altogether,  and  replace  the  dis- 
torted wave  by  its  equivalent  sine  wave,  keeping  in  mind, 
however,  the  existence  of  a  higher  harmonic  as  a  possible 
disturbing  factor  which  may  become  noticeable  in  those  cases 
where  the  frequency  of  the  higher  harmonic  is  near  the  fre- 
quency of  resonance  of  the  circuit,  that  is,  in  circuits  con- 
taining capacity  besides  the  inductance. 

79.  The  equivalent  sine  wave  of  exciting  current  leads 
the  sine  wave  of  magnetism  by  an  angle  a,  which  is  called 
the  angle  of  Jiysteretic  advance  of  phase.  Hence  the  cur- 
rent lags  behind  the  E.M.F  by  ^  90°  —  a,  and  the  power 

is  therefore,     p=f£  cog  (9QO  _  a)  =  /E  sin  a 

Thus  the  exciting  current,  7,  consists  of  an  energy  compo- 
nent, /  sin  a,  called  the  Jiysteretic  or  magnetic  energy  current, 
and  a  wattless  component,  /  cos  a,  which  is  called  the  mag- 
netizing current.  Or,  conversely,  the  E.M.F.  consists  of  an 
energy  component,  E  sin  a,  the  Jiysteretic  energy  E.M.F., 
and  a  wattless  component,  E  cos  a,  the  E.M.F.  of  self- 
induction. 

Denoting  the  absolute  value  of  the  impedance  of  the 

116  A  L  TERNA  TING-CURRENT  PHENOMENA  . 

circuit,  E  1  1,  by  s,  —  where  s  is  determined  by  the  mag- 
netic characteristic  of  the  iron,  and  the  shape  of  the 
magnetic  and  electric  circuits,  —  the  impedance  is  repre- 
sented, in  phase  and  intensity,  by  the  symbolic  expression, 

Z  =  r  —  jx  =  z  sin  a  —  jz  cos  a  ; 
and  the  admittance  by, 

Y  =  g  +  j  b  =  -  sin  a  -j-  j  -  cos  a  =  y  sin  a  -f-  jy  cos  a. 

z  z 

The  quantities,  z,  r,  x,  and  y,  g,  b,  are,  however,  not 
constants  as  in  the  case  of  the  circuit  without  iron,  but 
depend  upon  the  intensity  of  magnetization,  (B,  —  that  is, 
upon  the  E.M.F.  This  dependence  complicates  the  investi- 
gation of  circuits  containing  iron. 

In  a  circuit  entirely  inclosed  by  iron,  a  is  quite  consider- 
able, ranging  from  30°  to  50°  for  values  below  saturation. 
Hence,  even  with  negligible  true  ohmic  resistance,  no  great 
lag  can  be  produced  in  ironclad  alternating-current  circuits. 

80.  The  loss  of  energy  by  hysteresis  due  to  molecular 
friction  is,  with  sufficient  exactness,  proportional  to  the 
1.6th  power  of  magnetic  induction  <&.  Hence  it  can  be  ex- 
pressed by  the  formula  : 

where  — 

IV  a  =  loss  of  energy  per  cycle,  in  ergs  or  (C.G.S.)  units  (=  10~7 
Joules)  per  cm8, 

(ft  =  maximum  magnetic  induction,  in  lines  of  force  per  cm2,  and 

77  =  the  coefficient  of  hysteresis. 

This  I  found  to  vary  in  iron  from  .00124  to  .0055.  As  a 
fair  mean,  .0033  *  can  be  accepted  for  good  average  annealed 
sheet  iron  or  sheet  steel.  In  gray  cast  iron,  17  averages 
.013  ;  it  varies  from  .0032  to  .028  in  cast  steel,  according 
to  the  chemical  or  physical  constitution  ;  and  reaches  values 
as  high  as  .08  in  hardened  steel  (tungsten  and  manganese 

*  At  present,  with  the  improvements  in  the  production  and  selection  of  sheet  steel  far 
alternating  apparatus,  .0025  can  be  considered  a  fair  average  in  selected  material  (1899). 

EFFECTIVE  RESISTANCE  AND  REACTANCE.       117 

steel).  Soft  nickel  and  cobalt  have  about  the  same  co- 
efficient of  hysteresis  as  gray  cast  iron ;  in  magnetite  I 
found  rj  =  .023. 

In  the  curves  of  Fig.  62  to  69,  r,  =  .0033. 

At  the  frequency,  N,  the  loss  of  power  in  the  volume,  V, 
is,  by  this  formula,  — 

P=-t]N  F&1-6 10  - '  watts 

where  S  is  the  cross-section  of  the  total  magnetic  flux,  <£. 

The    maximum    magnetic    flux,    <E>,    depends    upon    the 
counter  E.M.F.  of  self-induction, 

E  =  V2  -IT  Nn  4>  10  - 8, 

V2  TT  Nn 

where  n  =  number  of  turns  of  the  electric  circuit. 

Substituting  this    in   the   value  of   the  power,   P,    and 
canceling,  we  get,  — 

E1-'          FIO  5-8  E™     F108 

no5-8        Ka     no3 
»  where  ^  =  ^  o.R  i.«  oi.fi  ..,..  =  58  -n 

T/- 

or,  substituting  •>;  =  .0033,  we  have  ^4  =  191.4  —^ — —  ; 

o    '    /?  * 

or,  substituting  F=  SL,  where  L  =  length  of  magnetic  circuit, 
•n  L  10 5-8  58 » Z 103  Z 

— — 

and  103       191.4  E 

In  Figs.  73,  74,  and  75,  is  shown  a  curve  of  hysteretic 
loss,  with  the  loss  of  power  as  ordinates,  and 

in  curve  73,  with  the  E.M.F.,  E,  as  abscissae,  for  L  =  6, 
S  =  20,  N=  100,  and  n  =  100  ; 

118 

AL  TERNA  TING-CURRENT  PHENOMENA. 

RELATION 

BE 

TW  = 

EN 

EA 

NDP 

F 

OR 

_— 

5,8 

=  20 

N  = 

10 

r5 

=  1 

oo 

/ 

/ 

/ 

K 

/ 

o 

/ 

^/ 

Q. 

x 

^ 

x 

X 

^ 

x 

x 

x 

x 

^ 

X* 

^ 

.  • 

^ 

E.IV 

l.F. 

Fig.  73.    Hysteresis  Loss  as  Function  of  £.  M.  F. 

BETW 
OR  LT6.  S=20,  ^ 

=  100.E= 

SO  100  160  200  250  300 

Fig.  74.    Hysteresis  Loss  as  Function  of  Number  of  Turns. 

EFFECTIVE   RESISTANCE   AND   REACTANCE. 

119 

II    I    I    II    I 

RELATION  BETWEEN   N  AND  P 
FOR  8=20,  L=6, 71  =  100.  E  =  100. 

Fig.  75.     Hysteresis  Loss  as  Function  of  Cycles. 

in  curve  74,  with  the  number  of  turns  as  abscissae,  for 
Z  =  6,  S  =  20,  JV=  100,  and  E  =  100 ; 

in  curve  75,  with  the  frequency,  JV,  or  the  cross-section,  S, 
as  abscissae,  for  L  =  6,  n  =  100,  and  E  =  100. 

As  shown,  the  hysteretic  loss  is  proportional  to  the  1.6th 
power  of  the  E.M.F.,  inversely  proportional  to  the  1.6th 
power  of  the  number  of  turns,  and  inversely  proportional  to 
the  .6th  power  of  frequency,  and  of  cross-section. 

81.  If  g  =  effective  conductance,  the  energy  compo- 
nent of  a  current  is  /  =  Eg,  and  the  energy  consumed  in 
a  conductance,  g,  is  P  =  IE  =  Ezg. 

Since,  however  : 

P  =  A ,  we  have  A =  E2  g ; 

or 

A  58r)L  10s 

191.4 

From  this  we  have  the  following  deduction : 

120 

ALTERNA TING-CURRENT  PHENOMENA. 

The  effective  conductance  due  to  magnetic  hysteresis  is 
proportional  to  the  coefficient  of  hysteresis,  rj,  and  to  the  length 
of  the  magnetic  circuit,  L,  and  inversely  proportional  to  the 
Jj!h  power  of  the  E.M.F.,  to  the  .6th  power  of  the  frequency, 
N,  and  of  the  cross-section  of  tlie  magnetic  circuit,  S,  and  to 
tlie  1.6th  power  of  the  number  of  turns,  n. 

Hence,  the  effective  hysteretic  conductance  increases 
with  decreasing  E.M.F.,  and  decreases  with  increasing 

RELATION 
FOR  L=6, 

BE- 

PWEEN     0AND  E 
00.  S  =  20,?l  =  1O 

V 

\ 

\ 

\ 

^ 

\ 

> 

^. 

.^^ 

__9 

a 

1  -, 

-  —  -. 

—  ^ 

——  . 

. 

•  , 

E 

Ftg.  76.    Hysteresis  Conductance  as  Function  of  E.M.F. 

E.M.F. ;  it  varies,  however,  much  slower  than  the  E.M.F., 
so  that,  if  the  hysteretic  conductance  represents  only  a  part 
of  the  total  energy  consumption,  it  can,  within  a  limited 
range  of  variation  —  as,  for  instance,  in  constant  potential 
transformers  —  be  assumed  as  constant  without  serious 
error. 

In  Figs.  76,  77,  and  78,  the  hysteretic  conductance,  g,  is 
plotted,  for  L  =  6,  E  =  100,  N=  100,  5  =  20  and  n  =  100, 
respectively,  with  the  conductance,  g,  as  ordinates,  and  with 

EFFECTIVE  RESISTANCE  AND   REACTANCE. 

1-21 

RELATION  BETWEEN    Q  AND  N 
FOR  L-6,  E  =  IOO.  S  =  20,  n=IOO 

Fig.  77.     Hysteresis  Conductance  as  Function  of  Cycles, 

• 

R 

LAI 

,0, 

BE 

WE 

EN 

,AS 

D(/ 

FOP 

L= 

6,E 

=  1( 

50, 

00 

,8= 

2a 

\ 

b 

V 

a 

\ 

\ 

s 

\ 

X. 

E 

- 

T 

-NL 

\. 

M~B~ 

:RO 

•  —  , 

F  T 

r= 

200  250  300  350 

Fig.  78.    Hysteresis  Conductance  as  Function  of  Number  of  Turns. 

122  ALTERNATING-CURRENT  PHENOMENA. 

E  as  abscissae  in  Curve  76. 
.A^  as  abscissas  in  Curve  77. 
n  as  abscissas  in  Curve  78. 

As  shown,  a  variation  in  the  E.M.F.  of  50  per  cent 
causes  a  variation  in  g  of  only  14  per  cent,  while  a  varia- 
tion in  N  or  6"  by  50  per  cent  causes  a  variation  in  g  of  21 
per  cent. 

If  (R  =  magnetic  reluctance  of  a  circuit,  £FA  =  maximum 
M.M.F.,  I  —  effective  current,  since  /V2  =  maximum  cur- 
rent, the  magnetic  flux, 

(R  (R

Provenance

Author
Charles Proteus Steinmetz (with Ernst J. Berg)
Rights
Published in 1900, before 1929, and therefore in the public domain in the United States.
Collected By
StanBot reference library