NDUCTION inotor designers must
account for the saturation of the vari-
ous components of magnetic reactances
to make accurate predictions of the
motor's performance. To predict the
saturated value of these component re-
actances is difficult because the superpo-
sition principle can no longer be applied
wxith accuracy. When saturation is pres-
ent, to be rigorous, the net field must be
studied not the component fields.
To determine the net field under satu-
rated conditions, it should first be dealt
with as though there were no saturation.
To find the net field with no saturation,
it is valid to find the field of each com-
ponent of reactance and superimpose
them in the various areas of interest.
In studying a particular motor, the
author found it convenient to separate
fluxes, having a portion of their path in
the iron, into three components: the
slot leakage flux, the air-gap space har-
monic leakage flux, and the air-gap
space fundamental flux. It is this latter
flux with which this paper is concerned.
Designers have long recognized that
the space fundamental air-gap flux varies
with axial position because of skewing
the rotor slots with respect to the stator
slots, but to the author's knowledge
nothing has been published giving quan-
titative data showing how much this
flux may vary. It is important that
designers have a knowledge of this effect
because it not only affects the degree of
saturation but also affects iron losses and
noise.
Nomenclature
2a =magnitude of major axis of ellipse
2b =tmagnitude of minor axis of ellipse
B =magnetic induction
I1 = stator current
I,=rotor current
Paper 55-270, recommended by the AIEE Rotating
Machinery Committee and approved by the AIEE
Committee on Technical Operations for presenta-
tion at the AIEE Middle Eastern District Meeting,
Columbus, Ohio, May 4-6, 1955. Manuscript
submitted January 31, 1955; made available for
printing March 16, 1955.
C. E. LINsKOUS is with the General Electric Com-
pany, Fort Wayne, Ind.
The author wishes to express his gratitude to M. L.
Schmidt and F. W. Suhr, General Electric Com-
pany, for the many helpful ideas and suggestions
contributed to this study.
I,[=magnetizing current
L =length of stack
N =-amplitude of backward xvave of mag-
netic induction
P= amplitude of forward ixave of magnetic
induction
R2=-forwxard rotor resistance
R2=backward rotor resistance
s - slip
t=time
x =axial distance of a plane from the end of
the stack which has the leading end
of the rotor bars
X2= rotor leakage reactance
Xm= magnetizing reactance
a= the skexv, electrical degrees
6=electrical angle away from center of the
reference winding pole in the direc-
tion of rotation
N =electrical angle axvay from major axis of
ellipse in the direction of rotation
f= electrical angle by which the forward
magnetizing current, referred to the
reference windings, leads the voltage
applied to the reference winding
7b=electrical angle by which the backward
magnetizing current, referred to the
reference wxinding, leads the applied
voltage
-=electrical angle by which the major axis
of the ellipse is located from the
reference winding. Measure in the
direction of rotation
c =angular velocity of applied voltage
NL=no load
FL= full load
-lI,T =maximum torque
SS= standstill or locked rotor
axial plane = a plane perpendicular to the
axis or, in other words, a plane paral-
lel to the plane of the laminations
reference mmf =the peak value of a space
sine wave of magnetomotive force
(mmf) which would produce the flux
required to balance the line voltage
for a balanced polyphase motor with
no skexv or, in other words, the mmf
that would produce the design flux
density
maximum mmf =the actual maximum mmf
divided by the reference mmf de-
fined in the foregoing
VARIATION OF NET ROTATING FIELD IN
UNBALANCED POLYPHASE AND SINGLE-
PHASE MOTORS AT A PARTICULAR
AXIAL LOCATION
Techniques have been established for
many years for resolving an unbalanced
polyphase or a single-phase motor into
forward and backward rotating sinusoidal
fields of constant amplitude and angular
velocity.'-6 Let it be assumed that the
fundamental flux density waves at a
particular axial location have been found
by these techniques-to be
Bf=P cos (cot-0+rf)
Bb = N cos (cot +9+ TO)
(1)
(2)
wxhere
Bf=magnetic induction of the forward field
at the angular location 0
Bb = magnetic induction of the backward
field at the angular location 0
P = peak value of the forward magnetic
induction wave, positive sequence
N -=peak value of the backward magnetic
induction wave, negative sequence
c =electrical angular velocity
t =time
0=angular location of a point on the stator
measured from the center of a refer-
ence wxinding pole, positive in the
direction of rotation
f= a phase angle for the forward wave for a
voltage applied to the reference
winding of Vm cos ct
-rb=a phase angle for the backward wave
for a voltage applied to the reference
winding of V,m cos cwt
These waves are represented by rotat-
ing vectors in Fig. 1. At any instant,
these two vectors may be added to get a
resultant vector representing the net
field. The projection of the resultant
vector along the line labeled major axis
in Fig. 1 is
(P+-N) cos (27r-ct_f±+b)2
The projection of the resultant vector
along the line labeled minor axis in Fig. 1
is
(P-N) sin (27rf-wt_r)+Tb2
These are the same form as the well-
known expression for an ellipse in para-
metric form and, therefore, the tip of
the resultant vector traces out an ellip-
tical locus. The expression for the an-
gular velocity of the resultant vector is
MAJOR AXIS\
-REFERENCE
MAIN POLE
Fig. 1. Vectors representing the forward and
backward rotating fields
Linkous-Effect of Ske-w on Induction Motor Magnetic Fields
Errect of Skew on Induction Motor
Magnetic Fields
C. E. LINKOUS
ASSOCIATE MEMBER AIEE
760 AUGUST 1955
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(F + B)
'i- DENSITY AT
INSTANT OF 0p
Fig. 3. Normalized curves for determining
the maximum magnetic induction
0
I (B)
Fig. 2. Locus of rotating vector representing
the resultant field
very interesting. It is developed in
Appendix II.
The locus is shown in Fig. 2(A).
The angle of tilt of the major axis of
the ellipse away from the reference pole
is
TfTrb (3)
2
Thus the ellipse shown in Fig. 2(A)
gives the amplitude of the wave of mag-
netic induction as the peak of the wave
crosses any particular angular position.
However, this is not in general the maxi-
mum magnetic induction which that loca-
tion experiences. This can be seen from
Fig. 2(B).
The plot of a sine function in polar
co-ordinates is a circle. The construc-
tion of Fig. 2(B) shows that the mag-
netic induction at the angle \\ the angular posil
of its occurrence
the load is vai
from no load
standstill
\WITlKI,.L'AD)~KCD Fig. 15 (rig
Locus of resul
vector
A. Substituting this value of yp i
equation 8 w ill then give the expression
Bmax
Taking the partial derivative of equat
8 wi-ith respect to yp and equating it to z
gives
/b
Tp=tan - tan X
a
This is the value of j p which makes J
maximum at the angle X. Substitut
equation 9 into equation 8 gives
Brnax a (b)(b)
4 cos2 [tan 1 tan x)]
co,s [-tan-' (- tan (
a2
Substituting into equation 10 that
a =P+-N
(9) 6=tan- X
(P sin (at+-rf) -N sin (at+rb) (15)
B a VP cos (at +Art) +AN cos (ct A+Tb)J
:ing Differentiating this with respect to time
gives
(p2 IN2 (
a=P2A+N2+2PNcos(2wt+Trf±+rb) (w)
(16)
At the time
1
aot =-(w
--rf- rb)2
(11)
the vector has its maximum angular velocity
of
b =P-N
X = 0- = 0
Tf-Tb
2 (13)
gives
Brnax
p2-2PXY l -2
'7
'cos' tan - L<+- )X
tan (0-Tff T)]b X
C T f
Tb
-X
cs 2
Substituting equation 17 into equation 15
showxs that
7T 7f- 7~b0= +
2 2
when the angular velocity is maximum.
Note that this is the angle at which the
amplitude of the resultant wvave is mini-
mum.
Similarly, at the time
ct= - (rf+rb)2
P -N \2
.f \b(6) [tan(> (14)
LP N 2
(7)
the angular velocity has its minimum value
of
The equation for the magnetic induction
at the instant the peak of the sine axve
passes point P is
B =
-.,a2 cos2 ypA+b2 sin2 yPX
cos [X-tan-I(- tan yP)] (8)
The problem is to find the value of yp
which will make B a maximum at the angle
Appendix II. Development of
the Angular Velocity of the
Vector Representing the
Resultant Field
It follows from Fig. 1 that the location of
the resultant vector at any time t is
rin =(PN) (a) (21)
Substituting equation 21 into equation 15
shows that
Tf-Tb
2 (22)
when the angular velocity is minimum.
Note that this is the angle at which the
Linkous-Effect of Skew on Induction Motor Magnetic Fields
(17)
(18)
y =a cos
-y
x= -b sin
-y
(19)
(20)
(12) omax .- P+N (w)
P-N
764 AUGUST 1955
Authorized licensed use limited to: Zhejiang University. Downloaded on July 31,2010 at 12:55:40 UTC from IEEE Xplore. Restrictions apply.
amplitude of the resultant wave is maxi-
mum.
References
1. THE REVOLVING FIELD THEORY OF THE
CAPACITOR MOTOR, Wayne J. Morrill. AIEE
Discussion
P. L. Alger (General Electric Company,
Schenectady, N. Y.): Designers have long
realized that spiralling, or skewing, the slots
of an induction motor increases the react-
ance and affects the performance in many
w-as, besides reducing the magnetic noise
and locking tendency. Despite its import-
ance, no one until now has made any thor-
ough analysis of this subject. This paper is
therefore of great interest and importance
to all motor designers. Mr. Linkous has
brought out very
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