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8/9/2019 ORNL Induction Probe
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3 4 4 5 6 0 0 2 3 8 2 2
2
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This report was prepared as an account
of
work sponsored by t h s Uni ted
Stares Government. Neither the United
S t a r e s
nor the United States Atomic
Energy Commission, nor any of their elnployees, nor any of their contractors,
subcontractors, or their employees, makes any warranty, express nr implied, or
assumes any legal liability
or
responsibility for t h e accuracy, completeness or
usefulness of any inforrnation, apparatus, product or process disclosed, or
represents that i t s use would tnot infringe privately owned r jghts.
.
. _
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OR NL-TM -l t175
Contract
N O . W-71-0;1
-eug
-26
M E T A L S
AND CERAMICS
DIVISION
DESIGN
OF ' INDUCTION PROBES
FOR F E A S U K E m N T
OF
T,EVEL
OF
LIQUID
m'rAu
C .
V .
Dodd C.
C .
Cheng
C . W. N e s t o r ,
J r .
R . B .
H o c s t r n
M A Y
1973
OAK
R I D G E N A TI O N A L LA R O R 4TO R Y
O a k
R i d g e ,
Tennessee 37830
ope
r a t e d by
UNION C A R B I D E COKPORATION
f o r t h e
3 4 4 5 5
0 0 2 3 8 2 2 2
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iii
CONTENT
S
ABSTRACT . . . . . . . . . . . . . . . . . . . . . . . . . . .
.
1
.
I N T R O D U C T I O N
. . . . . . . . . . . . . . . . . . . . . . . . .
2 . THEORETICAL ANALYSIS
. . . . . . . . . . . . . . . . . . . . .
3 -
COMPUTER CALCULATIONS
FOR
11 PROBE INSIDE BISMUTH- . . . . . .
11 . MEASUREMENTS ON LIQUID LEVEL SYSTEM . . . . . . . . . . . . .
5
SUMMARY A N D CONCLUSIONS . . . . . . . . . . . . . . . . . . .
6 A CKNOWLE DGMENTS . . . . . . . . . . . . . . . . . . . . . . .
APPENDIX
A
omputer Programs f o r a L iquid Lev el Pro be
I n s i d e
C o a x i a l C o n d u c t o r s
. . . . . . . . . . . . . . . . . . . . . .
I
. I n t r o d u c t i o n . . . . . . . . . . . . . . . . . . . . . . .
II
D e s c r i p t i o n of INNMUL . . . . . . . . . . . . . . . . . .
A .
D R I V E R
Program . . . . . . . . . . . . . . . . . . . .
B . INhMUI. Subroutine . . . . . . . . . . . . . . . . . .
1
. X J S N T
F u n c t i o n . . . . . . . . . . . . . . . . . .
2 XILNT Function
5
. GAMCAL S u b r o u t i n e . . . . . . . . . . . . . . . .
a
.
GCA1. C S u b r o u t i n e . . . . . . . . . . . . . . .
b
.
MODBES S u b r o u t i n e . . . . . . . . . . . . . .
c
.
CND
KF:
S
S
u
b
r
ou t
i
ne
. . . . . . . . . . . . . .
i . COMKB
S u b r o u t i n e . . . . . . . . . . . . .
ii . C M I S u b r o u t i n e
. . . . . . . . . . . . . .
IC11. Execut ion oP INNMUL
. . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . .
A
.
TELINC.Fh Program
. . . . . . . . . . . . . . . . . .
B
. D a t a D e s c r i p t i o n . . . . . . . . . . . . . . . . . . .
I V . ATTEN Program . . . . . . . . . . . . . . . . . . . . . .
C . S ample Dat a and Re su l t s . . . . . . . . . . . . . . .
Page
_
1
1
c
d
24
33
5’f
38
35
93
99
1O?
108
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I
D E S I G N OF I N D U C T I O N
PROBES FOR MEASTJESPfENT
-
OF
LEVEL
OF LIQUID IIETALS
C . V. Dodd C . C . Chengl
C .
W.
N e s t o r ,
J r . 2
E.
B.
H o f s t r a 2
ABSTRACT
This r e p o r t g i v e s g e n e r a l a n a l y s es
of
e d d y - c u r r e n t p r o b e s
f o r m ea s ur i ng t h e
l e v e l
o f l i q u i d m eta l s . T h e C ~ S P f a c o i l
e n c i r c l i n g a l e v e l c ha mb er a nd t h e
case
of a co-il i n s i d e
a
l e v e l chamber h a v e b e e n solved t h e o r e t i c , d l y , a n d c o m p u t e r
programs
a r e
inclridrAd i n t h e A p p e nd i x f o r t h e l a t t e r case .
A ; a s p e c i f i c e x am p le , w e h a v e d e s l g n e d a p r o be en c l os e d i n
molybdenum (a
good
c o n d u c t o r ) t o measure t h e level
of
m o l t e n
b i s mu th
( i t
p o o r c o n d u c to r ) . Ry u s in g a c om p ut er a n a l y s i s , t h e
q e n s i t i v i t y of
t h e
p r o b e
t o
l e v e l c h an g es i s maximized
w h i l e
t h e s e n s i t i v i t y t o u n de s i r a b l e v a r i a b l e s , s uc h
as
t e m p e r a t u r e
c h a n g e s
i s
min iini z e d . E x p e r im e n ta l me a s ure me nts d e mo n s t ra t e d
t h a t
the
l e v e l c o u l d
be
m ea su re d t o w i t h i n 4 0.089 iu. o v e r a
l e v e l
rangci
f rom
o
t o 13 i n . w i t h i n a t e m p e r a t u r e range of
600"
t o 6 5 0 ° C .
The
h i g h d e g r e e of buccess a ch i ev e d i n t h e
p r o b e d e s i g n and mcasurements f o r t h i s u n f a v o r a b l e c o m b i na t io n
o f c o n du c t or s i n d i c a t e t h a t h i g h l y a c c u r a t e ed dy -c ur r en t meas-
u re me n ts c a n
be
made w i t h a l m o s t
any
c o m b i n a t i o n
of
c o n d u c t o r s .
1.
INTLWDUCTION
T h e a b i l i t y t o m ea su re
t h e
level of B m o l t e n meta l i s very i .mportan t
i n
a
number
of
i n d u s t r i a l a nd c h em i c a l p r o c e s s e s .
W e
h a v e a n a l y z e d t h e
g e n e r a l p r o b l e m
of
m e a s u r i n g t h e 1 . ev e l
of
a c o n d u c t iv e f l u i d b y a n i nd u c-
t i o n , o r e d d y - c u r r e n t p r o c e s s . T he e d d y - c u r r e n t
p r o b e
c o n s i s t s
of
a
l on g b i f i l a r
c o i l ,
which c an e i t h e r e n c i r c l e a c h a m b e r c o n t a i n i n g t h e
l i q u i d m e t a l o r be i n s i d e a t u b e mo un te d i n t h e c ha mb er c o n t a i n i n g t h e
l i q u i d l e v e l . W e o b ta i n ed i n t e g r a l s o l . u t i o n s wh ic h were
v a l i d
f o r
the
c ha mb er e i t h e r e m pt y o r f u l l , a n d , be c au s e of
t h e
p r o b e l e n g t h ,
we
a s s u m e d t h a t
t h e
r e s p o n s e
of
t h e p r o b e
t o
l e v e l s b e t we en t h e s e t wo
ex t r eme wa
s
app
r
oxlmat e l y 1 n e a
r .
showed thLs
t o
b e a n e x c e l l e n t a s s um p ti o n.
A
r e l a x a t i o n s o l u t i o n
c o u l d
L a
t
e r experimen a1
measiir e m e m t
s
lConsu l t an t f ro m t h e U n i v e r s i t y o f T e n n es s e e.
2Ma
themat i c s
D i v i s i o n .
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be us ed t o c a l c u l a t e t h e p ro be r es p on s e s t o v a r i o u s l e v e l s of l i q u i d
m e t a l , b u t w as j u dg e d t o b e
too
e x p e n s iv e t o r u n f o r t h e a d d i t i o n a l
i n fo i -m a t io n g a i n e d . W hi le t h e t e c h n i q u e i s v e r y g e n e r a l a nd c a n b e
a p pl i- e d t o a l m o st an y c o n d u c t i v e f l u i d ,
w e
a n al - yz e d a s y s t e m t h a t c o n -
s i - s t e d
of
a c o i l e n c a s e d i n mo ly bd en um ( a go od c o n d u c t o r ) u se d t o me a su r e
t h e l e v e l
of
mol t en b i smuth ( a
p o o r
c o n d u c t o r ) . T he h i g h d e g r e e o f
s u c c e s s a c h i ev e d i n t h e p ro b e dt . ; i l ; i I and measurements f o r t h i s u n fa v or a bl e
c o m b i n a t i o n of c on du ct :o rs l e a d s u s t o c o n c lu d e t h a t h i g h l y a c c u r a t e e dd y -
c u r r e n t t e c h n i q u e s c a n be d e s i gn e d a n d a p p l i e d f o r l e v e l m ea su re me nt s w i t h
a l m o s t a ny c o m b i n a t i o n o f c o n d u c t o r s .
2. THEORETICAT. ANALYSCS
The g e n e r a l c o n f i g u r a t i o n t o be c o n s id e r e d i s a n a x i a l l y s ym me tr ic
d r i v i n g c o i l l o c a t e d c o n c e n t r i c a l l y w i t h a n a r b i t r a r y riurrlber o f c y l i n -
d
r i c a 1 c o n d u c to r s w i t h a r b i t r a r y t h i c k n e s s , p erm ea b
i
1 t
y ,
p e r m i t t i v i t y ,
a n d c o n d u c t i v i t y . F o r s i m p l i c i t y , we a ss um e Lh dt a l l me dia a r e l i n e a r ,
i s o t r o p i c , a n d h om og en po us , a nd t l ie d r i v i n g c u r r e n t
i s
t ime-ha rmonic w i t h
f r e q u e n c y ,
w .
Th en , t h e c u r r e n t d e n s i t y J and v e c t o r p o t e n t i a l A w i l l
have on ly az i i nu tha l componen t s i n c y l i n d r i c a l c o o rd i n a te s
:
-3
-3
.
p
J ( x )
=
J ( r , z )
^c
6'
and
+ ..)
8
A ( x ) = A ( r , z ) ^e
( 2 )
where e . i s a n a z i m u th a l u n i t v e c t o r . The v e ct -o r p o t e n t i a l a t ( r , ~ ) ,
produ ced by a d r i v i n g c o i l w i t h a c u r r e n t d e n s i t y J ( r ' , z ' ) a t ( r l , z ' ) ,
c a n b e e x p r e s s e d a s
c;
A ( r , z ) =
G ( r , z ; r ' , z ' ) J ( r ' , z '
)
d r ' d z '
D r i v i n g
Coi 1.
where G ( r , z ; r ' , z ' ) i s t h e G r e e n 's
f u n c t i o n f o r a u n i t b - f u n c t io n c u r r e n t
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.+..
a t
( r ' ,
2 ' ).
fiiiic t i o n
s
n t i s i e
In a l i n e a r , i s o t ro p i c , homogeneous medium, t h e
Green's
3
where
1.1, E, 3 i - d n a r e t h e p e r m ea b i l i t y , p e r m i t t i v i t y ,
a n d
c o n d u c t i v i t y
oE the medium.
t h e p r o p e r b ou nd ar y c o n d i t i o n s .
Tlic
s o l u t i o n
o f
E q .
( )
for
e a c h mcadiurn
rlirrst a l s o s a t i s f y
We s h a l l f i r s t
c o n s i d e r a ? ) - fu n c t io n c o i l c o a x i a l
w i t l i
k a k f - ?
c y l i n d r i c a l cu n d u ct o r s; k-1
of
the m i n s i d e
t h e
c o i l
arid
k ' - 1
o f
t l i c n i
o u t s i de th e c o i l , a s
shown
i n F i g . 1. Tlicl g e n e r a l s o l u t i o n o f E q . ( 1 1 )
i n
any
r e g i o n ,
t i ,
may
be
o b t a i n c d
b y
s e p a r a t i o n
of v a r i a b l e s .
S e t t i n g
a n d d i - v i d i n g E q .
1 1 )
by
R ( r ) Z z )
g i v e s :
T h e s
ul,
s
c r
i
p t
s
n 011 the
p
c r m e a b i. 1 i t
y , p e r m i t
t
i
v
j.t
y,
a nd
c
ond
i.ic t i v i : y
d e n o t e t h e
values
of
t h e s e
p a r a m e t e r s i.n t h e r e g i o n n .
We
s h a l l
choose
the
s e p a r a t i o n " c o n s ta n t " , (X'.., o be n e g a t i v e
a n d
de f i -ne
'C. V.
Dodd
and
W.
E . Deeds, J .
A p p l .
Phys ,
2 829-2838 (1968).
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C X FI L-
CWG
7 2 - 3 0 7
2
F i g .
1.
Mul t ip l e Concen t r i - c Conduc to r s
i n
t h e P r e s e n c e o f a Delta
F u n c t i o n C o i l .
Then
we
c a n
w r i t e f o r Ehe z
drpendence
S o l v i n g his d i f f e r e n t i a l e q ua t io n g i v e s :
L ( Z )
A
sin L - ( z - z 0 ) i B cos i e - z 0 ) .
We c a n
d r o p
t h e s i n e t e r m
d u e t o
t h e symmetry a b o u t
z l .
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5
The
r a d i a l t e r m h a s t fi e f o l l o w i n g d e pe n de n ce :
.
T h i s
d i f € e r e n t i a l e q u a t i on
has
t h e
f o l l u w i
ng
s o l u t i . o n :
where
I tY r )
and
K (Q r ) a r e
m o d i f i e d
Ressel
f u n c t i o n s
of
f i r s t o r d e r .
The c om p le te s o l u t i o n t o
t h e
Green's f u n c t i o n i n e a c h r e g i o n i s a n
1 n I n
i n t e g r a l o v e r t h e s e p a r a t i o n c o n s t a n t
0:
f o r
n
L 1,2,
. . .
k ;
l l , ? ' ,
.
. . k'. T h e unknown cons i an t s
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4
ORNL-DWG 72-3046
/-
F i g .
2.
T o p
V i e w
of a Typ ic al Boundary Between
Two
Regions .
U s i n g
t he
G r e e n ' s f u n c t i o n s f r o m
E q .
( 1 0 )
i n
E q .
( 1 2 )
w e
o b t a i n :
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We c a n r e v e r s e t li e o r d e r
o f
i n t e g r a t i o n of t h e i n t e g r a l s c o n t a i n i ng
: - s s e l
f u n c t i o n s an d u s e t h e F o u r i e r i n t e g r a l t he or em ,
F:quation
(16)
t h e n b e c o me s :
A
s i m i l a r o p e r a t i o n
on
E q . ( 1 1
)
g i v e s :
E q u a t i o n s (1
)
and ( 1 - ) r e p r e s e n t
t h e
r e l a t i o n s b e tw ee n t h e c o n s t a n t s
f o r
a n y
two r e g i o n s i n s i d e t h e c o i l . We
s h a l l
now so lve f o r a l l t h e
unkoowyii c o n s t a n t s i n t h e f o l l o w i n g m a n n er . S i n c e t h e i n n e r m o s t r e g i o n
h a s only one unknown cons tan t :
C I , w e
s h a l l s o l v e f o r t h e unknown co n -
s t a n t s i n t h e s e co nd r e g i o n
i n
t e r m s of i t . N ext we s h a l l s o l v e f o r
t h e
u n k n o wn c o n s ta n t s i n t h e t h i r d r e g io n i i i t e rms o f C t h e n t h e f o u rt l l ,
u n t i l we r e ac h t h e r e g i o n c o n t a i n i n g t h e c o i l , k . We s h a l l d o t h e s a m e
k h i n g
f o r t h e r e g io n s outside t h e c o i l , s t - a i t i n g w i t h t h e o u t e r m o s t a n d
w o rk i ng i nw a rd s, s o l v i n g f o r e a ch r e g i o n i n t e rms o f D', u n t i l
we
r e a c h
t l ie r e g i on k ' . We s h a l l t h e n u s e E q . ( 1 0 and E q .
( l e )
f o r t h e c o i l
r e g i o n s k a n d k'. T h i s w i l l g i v e t w o e q u a t i o n s f o r t h e t wo un kn ow ns ,
C
and
D
a nd we c a n s o lv e f o r th em.
h i s
w i l l t h e n a l l o w u s t o
- > ] r i t e
h e e x p r e s s i o n f o r t h e u nknown c o n s t a n t s i n a ny r e g i oi i .
1'
1
1
1 ' '
S o l v i n g E q s .
( 1 0
and
(16)
o r t h e u nknown c o n s t a n t s i n
a n y
r e g i o n ,
n + l ,
i n terms
o f
t h e unknown c o n s t a n t s i n r e g i o n n . w h e r e t h e c o i l i s
n o t b e twe e n
l l i ~
e g i o n s , g i v e s :
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10
T h i s t r a n s f o r m a t i o n
m a t r i x
g i v e s t h e r e l a t i o i l b et wPen t h e c o n s ta n t s i n
a n y two re g i o n s n o t c o n t a i n i n g
t h e
c o i l b e t w ee n t h em . I t
i s
t h e s a me
f o r r e g i o n s i n s i d e
and
o u t s i d e t h e c o i l , w i t h t h e e x c ep t i o n t h a t n s h ou l d
b e r e p l a c p d b y n f o r r e g i on s o u t s i d e t h e c o i l t o c or re sp on d t o o ur
n o t a t i o n .
S t a r t i n g f ro m t h e i n n e rm o s t r e g i o n (n:
1)
an d g o i n g t o t h e s ec on d
g i v e s :
The
c on st ar it s i n t h e t h i r d r e g i o n ca n
b e
o b t a i n e d
b y :
a n d t h e c o n s t a n t s i n t h e f o u r t h r e g i o n b y :
The g e n e r a l e x p r e s s i o n f o r t h e n t h r e g i o n
i s
(26)
To
make o u r e x p r e s s i o n s s h o r t e r ,
we
s h a l l
define:
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v ( n ) T
. . . T
-3,2 T
q1 '
-n, n
-
1
-11
- 1., 1
-
a n d when 11 := lr, w e sha1.1 d r o p t h e a r g u m e n t. T hu s w e h a v e
We h a v e
v e r y
s imi la r e q u a t i -0 1 1 s
f o r
the>
r e g i o n s o u t s i d e
t h e
c o i l
:
where w e
h a v e rriade
a s i m i l a r d e f i n i t i o n :
and we h a v c d r o p p e d t h e a rg u me n t w h e n 11' k' T l ~ u s , we c a n
noTo
w r i t e
t h e c o n s t a n t s
i n
a n y L e qi o n i n
terms
o f t h e co n s t a n t i n
t h e
innerrrlos t
region,
a ~
[ o r
t h e
ouLerrnost region,
a [2,] b y means
o f t h e
t r a n s f o i n i a t i o n m a t r i c e s , V(n) and
U ( n ) . We
s h a l l w r i t
e
E q s . ( 1 ' 0
and
(18) f o r t h e
r e g i o n s
on
e i t h e r
s i d e of
t h e c o i l ,
k
a n d
k .
h a v e r :: L ,
s o
t l i a t
7 ( r -r'
) = 1 . A l s o = 2
=
Cr a nd 13 - H
- ; io, s o
t h a t the
e q u a t i o n s becorric:
-1 -1 '
v
Y
Herr w e
II 11
k
I<
0
k
-
k '
and
ck~,(uor'
4 D K
(Der')
z
c lC ,1
(a r ' )
+
D ~ ,(i-y
r ' )
.
(36)
k 1 1 0
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U si ng o u r m a t r i x n 3 t a t i o n ,
we
c a n w r i t e
2
Dk =
V , C
cl 1
-- LT D ,
'k' 16 1 '
and
We now have
two
equa t i ons and on ly two unknowns .
S o l vi n g t h e s e g i v e s
and
( 4 4 )
whe r e t h e d e n o m in a to r h a s a g a i n b ee n s i m p l i f i e d
by
u s e of t h e Wronsk ian ,
and t h e f a c t t h a t P o
=
2
.
Now
w e
c a n s u b s t i t u t e t h e v a l u es of t h e
0
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c o n s ta n t s i n E y s . k 3 ) a n d (41 i ) i n t o
E q s .
(51
)
and (53) t o g i v e t h e
c o n s t a n t s i n a n y r e g i o n .
Wc'
c a n w r i t e
t h e
G r e e n ' s f u n c t i o n
f o r a n y
r eg io ti i n s i d e t h e c o i l a s
The
G r ee n 's f u n c t i o n f o r a ny r e g i on o u t s i d e t h e c o i l i s
Once
we
h a v e t h e G r e e n ' s f u a c t i o n ,
we
c a n
g e t t h e
v e c t o r p o t e n t i a l
b y u s i n g
E q . ( 3 ) .
c r o s s s e c t i o n , a s shown
in
F i g .
3 .
We
a dd ed a n o t h e r r e g i o n , t h a t c o n -
t a i n s t h e c o i l , and d e si g n at e d
i t
r e g i o n c . For a
dense1.y
a n d u n i f o r m l y
wound c o i l ,
t h e
c u r r e n t d e n s i t y
J ( r ' ,
z '
) i s
a p p r o x i m a t e l y :
The most common type of c o i l is on(: of r e c t a n g u l a r
wherc
n
i s t h e
number
of
t u r n s
p e r
u n i t a r e a , an d
I i s
t h e c u r r e n t p e r
t u r n . S u b s t i t u t i n g
E q s . ( ) + ( )
and
(4))
i n t o
E q .
(3) g i v e s t h e v e c t o r
p o t e n t i a l f o r any r e g i o n i n s i d e t he c o i l a s
C
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14
F i g .
3 .
C o i l w i t h R e c t a n g u l a r Cross S e c t i . o n C o n c e n t r i c w i t h C y l i n -
d r i c a l C o n d u c t o r s .
R e v e r s i n g the o r d e r of i n t e g r a t i o n a n d i n t e g r a t i n g o v e r t h e d i me n si o ns
of
t h e c o i l g i.ve s
a(z-R ) -
sin
( n ) I a
r )
f
V (n)Kl(anr)]
._
..-..
... . ..
.-
1
A (n)(r,
z ) =
1
7T
2
0
(u22v11
-
u 1 2 v 2 1 )
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15
where v w
have
d e f i n e d t h e f u n c t i o n r ;
and
where r and r a r e now taken
a s
t h e c o i l i n n e r and o u t e r r a d i i , and
s h o u l d n o t
b e
c on fu se d w i t h t h e o u t e r r a d i i
of
t h e f i r s t t v 7 0 r e g i o n s .
The v e c t o r p o t e n t i a l f o r a ny r e g ion o u t s i de t h e c o i l i s
1 2
T h e r e g i o n of t h e c o i l r e q u i r e s s p e c i a l t r e a t m e n t .
To
f i n d t h e v e c t o r
p o t e n t i a l a t
a
p o in t i n the c o i l r e g i o n , r , v7e must add
t h e
s o l u t i o n of
A ( > ( r , z ) f o r
a
c o i l g o in g f ro m
r
t o r t o t h e s o l u t i o n
of
2
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7
a
a
a
c
h
-
n
i
-
kt
0
W
7
0
W
.
0
d
0
d
W
d
N
H
u
n
kd
0
W
n
L
d
%
0
t
rhr
H
&
L
0
u
d
’
p
r
L
a
w
d
W
0
2
W
d4
8
0
-
h
d
0
M
G
0
M
i
-
n
L
s
o
u
t
G
4
H
n
L
0
4
n
r
.
0
u(
d
d
0
L
0
d
v
0
7
W
I
d4
4
H
4
0
h
k
r
L
X
-
X
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1 7
We s h a l l
u s e t h e d e f i n i t i o n s g iv en i n E q s . (50)
and
(51)
f o r
1(r2>rl)
and K ( r r ) , and we s h a l l use t he r e l a t i o n s
2 '
1
a n d
E q u a t i o n (53)
t he n
becomes
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18
We
h a v e s ho wn i n a n
c a r l l e r
paper ’ t h a t t h e i n t e g r a l
o f
t h e e x p r e s si o n
i n t h e l a r g e s qu a re b r a ck e t s i s
rn
- e da
(55)
( r , r ) J ( a r )
0 2
2 2 2 1
1
0
where
1
( r ,r
)
5
2 2
1.
c1
Making t h i s s u b s t i t u t i o n g i v e s
:
) - s i n a(z-R
___
’IT
0
We
h av e now d et e r m i ne d t h e v e c t o r p o t e n t i a l f o r a n y re g i o n . Onc e
t h e v e c t o r p o t e n t i a l h a s b ee n d et e rm i ne d ,
we
c a n c a l c u l a t e a ny p h y s i c a l l y
o b s e r v a b l e e l e c t r o m a g n e t i c i n d u c t i o n p h en om en on f r om i t . The p a r t i c u l a r
p a r a m et e r s t h a t w e w is h t o c a l c u l a t e a r e t h e m u t u a l i m pe da nc e a nd t h e
s e l f - i m p e d a n c e of two i d e n t i c a l b i f i l a r c o i l s .
The
mutua l impedance
be tween two c o i l s , 1 and 2 , i s
t h e
v o l t a g e i n du c ed i n one c o i l
by
a u n i t
c u r r e n t i n t h e o t h e r :
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1 9
S i n ce b o t h c o i l s a r e i d e n t i c a l and o ccup y t h e samc r e e f o n , we can
expand
E q . ( 5 7 ) and perforiii the i n t - ’ g r a t i o n o v e r t h e s ec on d c o i l t o o b t a i n
Th e c o i l i m p ed a nc e
i s
and s i n c e t h e c o i l s a r e i d e n t i c a l and i n
the
same r e g i o n , M =
I f
w e t a k e t h e s p e c i a l case
where
t h e r e
are
110 c o n d u c t o r s o u t s i d e the
c o i l
w e
h a v e
E q .
(59)
becomes
1 2
=
l
t h e u n i t m a t r i x . Th en
U22
=
1
and
U I 2
=
0
so
t h a t
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20
A
c o mp u te r p ro g ra m, ENCMTJL, t o e v al u a
s i o n w i l l b e gi v en i n a
l a t e r
r e p o r t .
t h e c o i l ,
we h a v e
x
= 1,,
and
E q .
(5 9 )
r
A
c o mp u te r p ro g ra m, ENCMTJL, t o e v a l ua t - e t h e i n t e g r a l p a r t
o f
t h i s e xp re s- -
s i o n w i l l b e gi v en i n a
l a t e r
r e p o r t .
O r , if we
h av e no c o n d u c t o r s i n s i d e
t h e c o i l ,
we h a v e
x
= 1,, and E q .
(59) becomes
2
2n p
2
0
-
( '2- ' J-> (r2-r1)
%2
-
t e
t h e i n t e g r a l p a r t
o f
t h i s
O r , if we h a v e n o c o n d u c to
becomes
.pres--
i n s i d e
A compute r p rogram, Il???bIuL, t o e v a l u a t e
t h e
i n t e g r a l p a r t o f t h i s
e x F r e s s i o n i s i n t h e a pp en di x.
T h u s ,
by u s e o f t h e s e p r o g ra m s w e c a n c a l c u l a t e t h e m u tu al i n d u ct a n ce
and c o i l imrledance of c o i l s i n a l i q u i d l e v e l p r ob e,
c o n s i s t i n g of m u l t i p l e
c o nd u ct o rs i n s i d e o r o u t s i d e the c o i l s .
We
s h a l l now c o n s i d er t h e e f f e c t s
of t h e c x t e r n a l e l e c t r i c a l c i r c u i t .
The e q u i v a l en t c i r c u i t
o f
a l i q u i d l e v e l p r ob e i s show n i n F i g .
4 .
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21
ORNL-DWG
72-6710
F i g
P r o b e .
Vo DRIVING VOLTAGE
Ro
Cg
Z ,
SERIES RESISTANCE IN THE DRIVING CIRCUIT
S HUNT CA P A CI T A NCE OF THE DRIVING CIRCUIT
R6
M MUTUAL IMPEDANCE BETWEEN THE DRIVER AND PICK-UP COIL
Zpu IMPEDANCE
O F
THE PICK-UP COIL
R,
C,
D.C. RESISTANCE O F THE DRIVER COIL
I M P E DA NCE
OF
THE DRIVER
C OI L
D.C. RESISTANCE OF THE P ICK-UP COIL
S HUNT CA P A CI T A NCE
OF
TH E P ICK-UP CIRCUIT
R g A M P L I F I E R I N P U T I M PE D AN C E
I LOOP CURRENT
, 4 .
Simplified C i r c u i t D ia gr am f o r a n E dd y C u r r e n t L i q u i d L e v e l
W e c a n
w r i t e
t h e f o l l o w i n g s e t of e q u a t i o n s f o r t h e v o l t a g e d r o p s a r ou n d
e a c h
of
t h e
l o o p s
i n t h e c i r c u i t :
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We c an use determinants and solve f or the currelit in the f i n a l loop,
I,,,
produced by an applied voltage V
.
c;’
c:
I ,
\J
0
We
shall solve
€or
the current,
I,,
multiply it
by
t i le
resistance
R
to
dptermine the input voltage to the amplifier, and then multiply by
t h e
amplifier gain G to determine the output voltage:
9
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23
R e a r r a n g i n g terms so t h a t E q . (68) c l e a r l y r e ma in s f i n i t e when t h e
c a p a c i t a n c e go es t o z e r o , we f i n d t h a t
From E q .
( 6 9 )
we c an c a l c u l a t e t h e p h as e s h i f t b etw ee n t h e v o l t a g e
d r i v i n g t h e e d d y - c u r r e n t p r o b e an d t h e a m p. li fi ed v o l t a g e r e c e i v e d b y t h e
p ha se s h i f t d e t e c t o r . S in c e t h e d r i v e r c o i l and pi ck up c o i l a r e i n t h e
same
r e g i o n a nd
a r e
i d e n t i c a l ,
w e
h a v e
where
M
w i l l b e g i ve n by e i t h e r E q . (61) o r E q .
( 6 2 ) .
T o e v a l u a t e E q .
( 6 9 ) , t h e r e i s a compute r p rogram, ATTEN,which c a l c u l a t e s t h e magn i tude
an d p h a se o f t h e o u tp u t v o l t a g e f o r v a r i o u s v a l u e s o f t h e t e r m s i n
E q .
( 6 9 )
The c i r c u i t p a r a m et e r s , Ro, C 6 , R
and C a r e v a l u e s t h a t may b e
9 ’ 7
v a r i e d ( w i th i n c e r t a i n l i m i t s ) w i t h a n e x t e r n a l p l ug -i n a t t e n u a t o r .
Th e a t t e n u a t o r , when p r o p e r l y c h o s en , h a s t h e f o l l o w i n g e f f e c t s :
(1)
The
p h a s e
s h i f t d ue t o t e mp er at ur e d r i f t s c a us i ng
v a r i a t i o n s i n t h e dc r e s i s t a n c e v a l u es of
E:
and
R
c an b e e s s e n t i a l l y e l im i n a te d .
6
7
(2) The
L-C
n et wo rk i n t h e d r i v i n g and p ic ku p c i r c u i t s
i n F ig . 4 a n d t h e m u t u a l c o u p l i n g b e t w ee n t h e c i r -
c u i t s com bin e t o a c t as a b an d- pa ss f i l t e r t h a t
r e d u ce s t h e n o i s e i n t h e i n s t r u m e n ta t i o n .
3 ) A r e d u c t i o n i n s e n s i t i v i t y o c c u rs and t h e p h a se
s h i f t s d u e t o v a r i a t i o n s i n t h e o t h e r parameters
i n c r e a s e . H ow ev er , t h e s e e f f e c t s ca n b e made
n e g l i g i b l e i f t h e a t t e n u a t o r
i s
p r o p e r l y d e s i g n e d .
The a t t e n u a t o r d e s i g n w i l l b e c o ns id e re d i n g r e a t e r d e t a i l i n t h e n e xt
c h a p t e r .
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24
3 . COMPUTER CALCULATIONS
F O R
A
PRO BE I N SI D E
BISMUTH
The t y pe o f l i q u i d l e v e l p r ob e an a ly z ed i n t h i s r e p o r t
i s
shown in
F i g . 5 . I t c o n s i s t s o f a l o n g b i f i l a r c o i l i n s i d e a molybdenum c o n-
t a i n e r . Th e d ra w in g
i s
s ym ni et ri c a b o u t t h e c o i l a x i s , s o o n ly h a l f
of
t h e p r o b e i s shown ( i n c r o s s s e c t i o n ) . 'The p r o b e
i s
p l a c e d i n s i d e a
m oly bd en um c a v i t y , a nd t h e l e v e l of t h e m o l te n b is m ut h i n
t h e
c a v i t y
c a n b e m e a s u r e d .
A
c u r r e n t f l ow i ng i n t h e d r i v i n g c o i l p ro du ce s a n
e l ec t ro m a gn e t i c f i e l d t h a t
i s
m o d i f i e d b y t h e p r e s e n c e of t h e c o n d u c t o r s .
The p ic ku p c o i l d e t e c t s t h i s f i e l d . I n t h e de s ig n
of
t h i s p r o b e , w e
used t h e f o l l o w i n g p r o c e d u r e . We f i r s t maximized t h e s e n s i t i v i t y of
t h e p r ob e t o c ha ng es i n l i q u i d l e v e l , t h e n m in im iz ed t h e e f f e c t s
of
t h e
u n d e s i r a b l e v a r i a b l e s s u c h a s t e m p e ra t u r e d r i f t , and f i n a l l y maximized
t h e s e n s i t i v i t y t o e r r o r r a t i o .
ORNL -DW G
71
9737
I
L i q u i d L e v e l
P r o b e
F i g . 5 .
L i q u i d
L e v e l P ro be I n s i d e C o n d u c t o rs .
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26
w i t h a w a l l t h i c k n e s s o f a p p r o xi m a t el y 1' m i l s , t h e r e i s n o c h a n ge i n
p h as e a s t h e 1 iq ui .d l e v e l
i s
v a r i - e d . A s t h e w a l l t h i- c kn e s s
i s
i n c r e a s e d
f u r t h e r , t h e c u r v e s o f p h a se w i t h a n d wi .t h ou t b i s m u th b ecome q u i t e Ear
a p a r t i n d i c a t i n g t h a t t h e r e
wil l
b e a l a r g e ph as e s h i f t a s t h e l i q u i d
l e v e l
i s
v a r i e d . T he p h a s e d i f f e r e n c e a p p r o a c h e s a maximum a t a p p r o x i -
m a t e l y 4-(m i l s and t h e n d e c r e a s e s a g a i n t o z e r o a s t h e c u r ve s c ro s s a t
14? m i l s , appro ach an o t he r maxi-mui., s ep a ra t i -on , and t he n c ro s s ag a i n .
The b e h a v i o r
o f
t h e m ag n it ud e c u r v e s o f t h e v o l t a g e i s v e r y s i m i l a r ,
w i t 1 1
t h e c u rv es c r o s s in g and approach i -ng a maximum
a n d
t h e n c r o s s i n g
agai .n. The f i - r s t maximum, w hich i s n o t shown i n F i g .
6,
i s t h e l a r g e s t
an d o c c u r s a t z e r o w a l l t h i c k n e s s f o r b o t h t h e m ag n it ud e c h an ge a nd
t h e p has e s h i f t . S in ce t h i s i s i m p r a c t i c a l i n o u r d es i gn , we e l e c t e d
t o
c o n c e n t r a t e o n
t l ie
seco nd maximum. The v a l u e
o f
w a l l t h ic k n e s s a t
which t h i s maximum occ ur s i s a l s o a f u n c t io n
o i
f r e q ue n c y . I n F i g .
r[,
W E h a v e a v e r y s i m i l a r p l o t o f m a g n i tu d e a n d p ha s e o f t i le p i c k u p coi .1
v o l t a g e a s f u n c t i o n s o f t h e c o n t a i n e r w a l l t h i c k n e s s , wi.th an d w i t h ou t
b i sm u t h, a t a f r e q u e n c y of 22 kHz . F igure 6: w h i c h was r u n a t 10 kHz,
i s
v er y s i m i l a r t o F i g .
7,
e x ce p t t h e v a l u e s of w a l l t h i c k n e s s f o r
maximum magni tude and phase change a r e s ma l l e r at-
the
h i g h e r f r e q u e n c y .
A t
20 kHz th e wa l l t h i c kn es se s f o r maximum phase and magni tude change
o cc ur a t 2.7 m i l s and 80 m i l s , r e s p e c t i v e l y , c om pare d t o jk 7 m i l s and
110
m i l s , r e s p e c t i v e l y , a t
10
kHz.
I n g e n e r a l ,
w e
a r e a b l e t o p l o t optimum w a l l t h i c k n e s s
f o r
maximum
s e n s i t i v i t y a g a i n s t f re qu en cy ,
a s
s ho wn i n F i g .
fl
Ln F ig . we have
o p t i m i z e d t h e w a l l t h i c k n e s s f o r t h e iiiaximum p h a s e s h i f t , a nd t li e
amount o f phase s h i f t we ge t a t opt imum
i s
a l s o p lo t t e d a g a i n s t t h e
f r e q u e n c y . B e ca u se t h e c u r v e s a r e r ou nd ed , i t
i s
d i f f i c u l t
t o
e x a c t l y
d e t e rm i n e t h e o ptimum w a l l t h i c k n e s s f o r
a
g i v e n f r e q u e n c y . Th e
s h a p e
o f t h e c u r v e s v a r i e s w i th c o i l s i z e , s o w e made s i m i l a r p l o t s f o r u p t i -
uium w a l l t h i c k n e s s f o r maximum s e n s i t i v i t y t o b o t h m a g n it u d e a nd p h a s e
c ha ng es v s f re q u en c y u s i n g d i f f e r e n t s i z e c o i l s .
A
compos i t e o f t h e s e
p l o t s f o r p hase s h i f t
i s
show n i n F i g . 3. F rom F ig . 'j, we conc luded
t h a t a l i q u i d l e v e l pr ob e w i t h
a
w a l l t h i c k n e s s o f 30 m i l s would have
a d eq u a te s e n s i t i v i t y . Once t h e w a l l t h i c k n e s s h a s b e en f ix e d , t h e n
w e
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PY-
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N
x
I
c
1
(
U
l
4
H
S
3
S
V
'
H
d
f
l
X
k
8
S
N
Y
3
1
V
M
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c a n detemt:i.ne the
o p t i n i i m f r e q u e n c y
f o r
maximum s e n s i t . i v i t y a n d t h e s e n s i -
t i .vf . ty at . t h a t f r eq u en c y f o r a ny s i z e c o i l . I n F i g . 10,
WE ?
h a v e
opt i .mize t l
f o r maximum p h a s e sl-iiEt, and w e have made s i ln i I a r
pl .o ts
f o r mal:i.murn atnp1.i-
t u d e c1-iange, From t h i s pLoL we
d e c i d e d t h a t
w e
would have a d e q u a t e sen.s:i -
t i v i t y i . f the
c o i l
form
01)
was
O.72,Y
i n .
a f requency
of 16 kHz, w e
h a v e 0.1.8 r a d i a n s o r a p p r o x i m a t e l y 10 phase
s h i - f t a s t:he 1 i q u i . d I.e-vel
i.s v d r i e d f r o m f u l l . ' to e m p t y . W l i l t . t h i s i s
not: t l ie most
s e n s i t
i - ~ e onf igura t : io[ j . ,
t h e sen:;-i.ti.vii:y i s riluch
nmre
t h a n
adequigte, and tile compromises
m a d e
t h u s f a r i n s u r e a
good
i nexpens i -ve
m e c h a n i c a l . d e s i g n . W s h a l l . now t u r n o u r
at
With t h i s s i z e coi.1. o p e r a t e d
a t
d r i f t s .
2:
7c
5
0
...
\
-
..
...
O W L - DWG 71.- 7 798
0 . 2 5
R I V L H
c r i i l
31CKUP Colt
L E N G T H O F C O I L - 4 3 i n
TEMPERATIJRF - 700"C
31
RFSiS1
V I l Y=15O$km
Mu R E S I S T I V I T Y - 2 O p C L L m
1AVlTE OD = 7 A
W IRE
D l A h l E T E R z r2 - r , r-45rri Is
W A L L
T H I C K N E S S = A
A = 3 0 m i i s
0.375 0.500 0.625 0.750 0.875 1 0 0 0
LAVITE OD
f i n
1
F i g . 10.
O p t i i r n u m F requency f o r Maximum Phase S h i f t and P h a s e S h i f t
a t Maximum
P l o t t e d
A g a i n s t C o i l Form 01).
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I n t h e c a l c u l a t i o n s t o m in im iz e d r i f t s , w e i n c l u d e d t h e o u t e r m ol yb -
denum con t a ine r a s show n i n F i g .
5.
We assumed t h a t b o t h t h e c o i l s h e a t h
and t l ie o u t e r c o n ta i ne l ' w er e i n f i n i t e l y l o n g ; t h e c o i l was a c t u a l l y
13.625
i n . l o n g.
The m aj or c o n t r i b u t i o n t o d r i f t s i s t h e
w i d e
r a n g e
of
o p e r a t i n g
t e m p e r a t u r e of t h e p r o b e . Th e t e m p e r a t u r e c o n t r i b u t i o n s ca n b e b r o k e n
t h e f o l l o w in g :
'There i s a c ha ng e i n t h e a c f i e l d d u e t o c h an ge s i n t h e
r e s i s t i v i t y
of
t i i t . molybdenum and b i smu th . T h i s ca us es
a
c h an g e i n t h e s e l E - im p e da n c e o f b o t i i t h e d r i v e r a nd
p i c k u p c o i l s an d t h e m u tu a l c o u p l i n g b et w ee n t he m .
T here i s a ch an ge i n t h e d c r e s i s t a n c e o f b o th c o i l s .
T hermal expans ion
oC
t h e c o i l a nd c o n du cl o r s a l s o
c a u s e s a c h a n g e i n t h e i mp e da n ce s a n d m u t u a l c o u p l i n g .
\?e s h a l l c o n s i d e r e a ch of t h e s e f a c t o r s s e p a r a t e l y .
I n F i g .
11
we h a v e p l o t t e d t h e p h a s e o f t l ie v o l t a g e o f t h e p i- ck up
c o i l a g a i n s t fr eq u en cy f o r v a r i o u s t e m p e r a t u re s . We c a n s ee t h a t t h e s e
c ur ve s i n t e r s e c t
a t
a c e r t a i n f r e q u e n c y , w h i ch m ea ns t h a t t h e te m p e r a -
t u r e c o e f f i c i e n t of tlhe phase
i s
e s s e n t i a l l y z e r o air t h a t f r e q u e n c y .
T hese z e r o t e m p e ra t u r e c o e f f i c i e n t p o i n t s o c c u r a t a p p ro x i m a te l y 25
kHz f o r t h e c a s e i n wh ich t h e l i q u i d l e v e l p r ob e i s e mp ty a nd a t a b o u t
.jO kHz f o r t h e p r ob e b e i n g f u l l o f b i sm u t h. More e x a c t c a l c u l a t i o n s
w i t h a n e x t e rn a l c i r c u i t a t ta c h ed
t o
t h e p r ob e f o r an o p e r a t i n g f r e -
quency of
i ' )+.300kHz
a r e s hown i n t h e t a b l e b e l o w.
T a b l e 1 . C a l c u l a t e d P h as e S h i f t V a l u es ( i n D e g r e e s )
w i t 1 1 Bismuth and
A i r
a t S e v e r a l T e m p e ra t ur e s
M a t e r i a l
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W N L - I IWG 71- 9076R
U
u
4
c
I,
1
F i g .
11.
Phase o f t h e Pickup
Coi.1 Vol t
a g e P l o t t e d
A g a i n s t
Frequency
f o r Different T e m p e r a t u r e s .
I n
t h e t e m p e r a t u r e
range
of p a r t i c u l a r i n t e r e s t ,
~ O O
o
f;:;oO(:, we have
c h o s e n our p a r a m e t e r s s o t h a t
we have
e x a c t : l y t h e same p o s i . t : i v e s l o p e
of phase
with te rr ipe ra t :u re
(4-0. $ " / ~ 0 " c )
n
b i s n ~ r t : t ia s t h e
negative
s l o p e
(-'3.06"/50")
i n a i r . T h ese
two e n d
p o i n t s r e p r e s e n t
t h e
worst t,ernpera
-.
t u r e c o e f f i c i e n t ,
and
i t
i s e x pe c te d t o
d e c r e a s e t o z e r o
f o r
t h e c a s e 01
t h e
p r o b e
b e i n g
h a l f
f u l l .
T h i s
worst
c a se
o f t h e c a l c ul . a te t l - t e m p e r a t u r e
c o e f f i c i e n t i s e q u i va l - e nt t o
I-0.0015
n . / " C e r r o r i n t h e l i q u i d
level .
measurement .
S i - m i l a r
c a l c u l a t i o n s
were made
f o r t h e ma g n i tu d e of t h e p i c k u p
c o i l
v o l t a g e , b u t t h e r e
i s no
f r e q u en c y a t w h ic h t h e
magnii-udch
r e ma in s
constant
w i t h t e n i p e r at u r c c h a n ge s .
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we
n e x t c o n s i de r e d t h e v a r i a t i o n i n p ha s e d ue to c h a ng e s i n d c
r e s i s -
t a n ce of t h e c o i l . A s we d i s c us s e d e a r l i e r ,
a
v a l u e o f c a p a c i t a n c e and
r e s i s t a n c e i n t h e d r i v i n g a nd d e t e c t i n g c i r c u i t s c an b e c ho se n ti ia t
w i l l
g i v e e s s e n t i a l l y n o ch an ge i n p ha se a s t h e d c r e s i s t a n c e o f t h e c o i l i s
v a r i e d , a n d will
also
a c t as a f i l t e r t o r ed u c e t h e s ys te ii i n o i s e . How ev er,
when the R - C ne twork
i s
a d j u s t ed t o g i v e e x a c t ly z e r o te mp e ra tu re d r i f t
w i t h t h e b is m ut h p r e s e n t , i t w i l l n o t g i.v e e x a c t l y z e r o d r i f t w i t h t h e
b i s mu t h a b s e n t . T h e r e f o r e , t h e n e tw o rk
i s
a dj us ce d t o g i v e sm al l d r i f t s
of o p p o s i t e s i g n s i n t h e two c a s e s . Bu t t h e more
we
f i . l t e r t o r p du ce
s y s t e m
n o is c , t h e g r e a t e r t h e s e
s m a l l
d r i f t s become. I n a d d i t i o n , t h e
p ha se s h i f t s d ue t o v a r i a t i o n s i n t h e c a p a c i t a n c e and r e s i - s t a n c e v a l u e s
i n t i le c i - r cu i t i n c r e a s e a s
w e
r e d uc e t h e s y st e m n o i s e . T h e r ef o r e ,
w e
m us t co mp ro mi se b e tw e en t h e s y s t e m n o i s e an d d r i f t s . The f o l l o w i n g t a b l e
summar izes t he d r i f t s be tween 60i3'and 6;d) 'c , u s i n g
-*j6.:j
f o r t h e s e r i e s
r e s i s t a n c e of t h e d r i v e r c i r c u i t and t l ie s h u n t r e s i s t a n c e o f t h e p ic k u p
c i r c u i t and 5e.30 pF f o r t h e s h u n t c a p a c i t a n c e .
T a b l e 2. Summary o f P h a se S h i f t s D ue t o V a r i a t i o n s
i n Va r io u s C i r c u i t P a ra m e te r s
P a r a m e t e r V a r i e d
Va r ia t i o n
i n
P aramete r
($)
P h a s e S h i f t
( d e g r e e s
)
D r i v e r C o i l R e s i s t a n c e
P ic k up C o i l R e s i s t a n c e
D r i v e r Sh u nt C a p a c i t a n c e
P i c k u p S hu n t C a p a c i t a n c e
D r i v e r C i r c ui
t
S e r i e s
R e s i s t a n c e
P i c k u p C i r c u i t S h u n t
R e s i s t a n c e
Opera t i ng F requency
1 >
1s
1
1
1
1
1
0.004
0.001
The p h a s e s h i f t s g i v e n
i n
T a b l e 2 a r e t h e a b s o l u t e maximum v a l u e s
t h a t o c c u r a ny wh er e i n t h e t e m p e r a t u r e r a n g e w i t h o r w i t h o u t b i sm u t h .
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53
T h e f i l i a l c o r i t - r i b u t i o n t o d i r f t s t h a t
w e
con s id e re d was t he rm31
e x p a n s i o n o f th e sys tem. In cl ud in g t li er rual. expans i.o i i e f f e c t s , a tempc?ra-
t u r e
v a r i . a t i o n f r o m 600"
t o
6 5 0 ~
aused
a
0.05" d i f f e r e n c e i n t h e p l ~ a s p
change b e t w e e n t h e two t e m p e r a t u r e s , which
can
b e compensated C o r w i t h
a s m a l l f r e q u e n c y c h a n g e .
Additional information o n t h e d e s i g n uf t h i s
probe
is g i v e n i n
I
othe l -
r e p o r t s .
T hr ee d i f f e r e n t
sets of
measurements
h a v e
be en performed on
[:he
l i - q u i d
l eve l .
p r o b e .
T ie f i r s t - s e t o f iiieasuz-cI~metlTs
w a s
p e rf o rm e d a t a
f r e q u e n c y
of
10
kHz
a nd a t room t em per a tu re . T he p r imary purpose o f
t hese measurement s
was
t o
t e s t
tl-ie
linear
.t:y of
t h e
p l - ~ b ~ ,
1- t c1
tile
secc2iitl
p u r p o s e W ~ ~ S
o check t h e a c c u r a c y
o f
t h e c a l c u l a t i o n s
T h e
p r o b e c o n s i s t e d
of
t h e c o i l e n cl os ed i n
a
moI,ybdenuin sheath, I,ut
w i t h -
oii't
any o u te r iiioly1)dennum c o n t a i n e r . The bi.siuu1:11 was
rcpl.aced by 12
r i n g s 01' Snc,onel ,
each machined
t o
1
_ _ 0 . 0 l i j
i n . t h i c k .
The
phase
s h i f t
was
r Q c o r d e d
t:o w L t 1 i i n O.OI." a s t h e
r i n g s
were
added, siim.lI.ating
a n
i n cr e as i -n g l i q u i d l e v e l .
A ] .east-squarc:s
f i t
was
marl
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The measurements
were
made a t a f r eque ncy o f
27.'7
kHz l o r v a r i o u s
l e v e l s o f b i sm u th a nd a t v a r i o u s
t e m p e r a t u r e s b e t w e e n 550°C and 700"C.
T h e r e s u 1 . t ~a r e p l o t t e d i n F i g . 12. T h e p h a s e s h i f t i s a l i n e a r f u n c t i o n
o f l i q u i d l e v e l o v e r a r a ng e f ro m z e r o t o a bo u t 13 i n . The s l o p e o f t h e
c u rv e v a r i e s s l i g h t l y w i t h t em p e ra t ur e , with the minimum temperature
c o e f f i c i - e n t o c c u r r i n g b e t we e n 600" C and 650"
.
The t em p e r at u r e c o e f f i c i e n t o f
t h e
l e v e l r e a d in g was
0.009
n . / " C
I O
f o r t h e chamber e il ip ty and 0.00211 i n . : C f o r t h e c h am be r f u l l o f b i s mu t h.
T he h i g h e r t e m p e r a t u r e c o e f f i c i e n t w i t h t h e c ha mb er e m pt y w as p r o b a b ly
du e t o t h e f e r r o m a gn e t ic o u t e r c a s i n g .
A s e r i e s
of
more a c c u r a t p c a l c u l a t i o n s , c o n s id e r i 'i g m ore d i f f e r e n t
p a r a m e t e r s , sh owed t h a t m o re a c c u r a t e m e a s ur e m en t s c o u l d b e made a t
2)-
kHz f o r t h e t e m p e r a t u r e r a n g e o f 600"~o 650"~. he l e v e l i n t h e p r ob e
14
35
36 37
38
39 40 41
42 43 1 4
45
46
47
PH ASE
SH IFT I deq l
F i g . 12. P ha se S h i f t P l o t t e d A ga i n s t L i q u i d L e v el f o r V a r i o u s
T empera tu res Measured a t a F requency o f 27.7 kHz.
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.55
was s e t a t
t h e maximum, de ter min ed by th e amount of b i sm uth
.i.n
t h e s y s t e m
a t t h e t i m e . The m an om ete r r e a d i n g i n d i c a t e d
10
i n . , b u t l a t e r m ea su re -
m en ts i n d i c a t e t h a t t h e a c t u a l l e v e l was a b ou t 13.5 i n . T ab le 3 shows
b o t h c a l c u l a t e d a nd m e as u re d v a l u e s o f m a g n i t u d e a nd p h a s e . The a c t u a l
c a l c u l . n t i o n s w er e made w i t h t h e p r o be e i t h e r f u l l o r em pt y of b i s m u th ,
and t h e 1 0 - i n . c a l c u l a t i o n s r e p r e s e n t a 1 .i ne ar i n t e r p o l a t i o n b et we e n z e r o
and
13.625
i n . o f b i s m u t h .
The r e s i s t o r v a l u e s a r e t h o s e o f b o t h t h e d r i v e r s e r i e s and t h e p i c ku p
s h u n t r e s i s t a n c e s , an d t h e s e c a n b e v a r i e d t o nc li i- ev e a " f i n e tu n in g " i n
t h e t e m p e r a t u r e c o e f f i c i e n t o f t h e p r o b e . T he p h a s e d if fe rc -. nc :c i
i s
t h e
p h a s e a t t h e l o w er t er np pr at :u re s u b t r a c t e d f ro m t h e p h a se a t t h e u p p e r
t e m p e r a t u r e .
w ou ld h e e q u a l b u t o p p o s i t e i n s i g n w i t h t h e p r o be i u l .1 a nd e mp ty , a s
shown f o r
t he
c a l c u l a t e d v a l u e s u s i - n g
36.3 ~2.
p ha se d i f f e r e n c e was -1.0.1.2 r a t h e r t h an O.06 c a l c u la t e d f o r t h e 1 0 - i n .
l e v e l . By i n c r e a s i n g t h e Val-ue s o f t h e r e s i s t o r s i n t h e a t t e n u a t o r , we
a r e a b l e t o d e c r ea s e bo t h
t h e
c a l c u l a t e d a nd m e as ur ed p h a s e d i f f e r e n , c e s .
The b e s t v a l u e of r e s i s t o r s t o g i v e minimum d r i f t wou1.d p rob abl y b e
s l i g h t l y l a r g e r t ha n
36.3
R. T h e l e v e l was a1 .so v a r i e d u s i n g t h e 75-a
r e s i s t o r s i n . t h e a t t e n u a t o r . The t e m p er a t ur e c o e f f i c i e n t of t h e piinse
v a r i e d f r o m
+O.OO&? / C (-i-O.U352
i n , / °C) w i . t h
t h e
chamber empty t o O.O($ /
" C
w i t h t h e c ham ber f u l l .
Ey
d e c re a s in g t h e v a l u e of t h e r e s i s t o r s , i t
s h ou ld b e p o s s i b l e t o o b t a i n
a
t em p e ra t ur e c o e f f i c i e n t
of
-t-O.OOl.6
i.n./"C
wi t h t h e chamber empty , - 0 . 0016
i n . / " C
w i t h t h e c h am be r f u l l and z e r o
w i t h t h e c ha mb er h a l f f u l
1.
I n t h e i d e a l c a se , t h e p h a se s h i f k s be tw ee n 600°C and
650°C
However , t h e measured
T h e c a l c u l a t e d s l o p e a t 600°C was
0 . 8 ) + j o / i n .
compared
t o
a measured
v a l u e o f 0 . 8 6 6 " / i n .
m a g ne t ic p e r m e a b i l i t y o f t h e o u t e r c o n t a i n e r i s on ly approx ima te ly known.
P a r t o f t h i s e r r o r may b e du e t o t h e f a c t t h a t t h e
W i t l i
t h e i n f o r m a t i
on
g a in c cl i n t h e s e measurements , we
wi l l
b e a b l e
t o c a l i b r a t e t h e p r ob e u se d i n t h e
l o o p
w i t h a n o u t e r c o n t a i n e r
of
molyb-
denum, a s
shown
i n F i g .
3 .
The l o we r c a l i b r a t i o n p o i n t f o r t h e p ro b e
c a n b e o b t a i n e d b e f o r e b i s mu t h
i s
e v e r ad de d t o t h e s y s te m . To g e t t h e
u p pe r c a l i b r a t i o n p o i n t , t h e bi sm u th l e v e l m u s t b e r a i s e d o v e r t h c t o p
o f t h e p ro b e , an d t h e
phase
r e a d i n g r e c o r d e d .
I f
0.110'
i s s u b t r a c t e d
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C
pi
m
U
.
A
r
4
\
D
r
t
c
W
tl
n
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3‘I
f ro m t h i s p h a se re a d in g , t h i s g i v e s the v a l u e of t he pha . se
w h e n
t h e l i q c i d
l e v e l
i s
15 i n . The phase wi l l . be a l i n e a r f u n c t io n
of
t h e b i smuth l e v e l
be tween 0 i n . and
13
i n . W r i n g t h e n i n e ~ ii on .t hso f t e s t i n g o f t h e
probe,
t h e z e r o p o i n t a p p e a r e d t o move, but t h e s l o p e was e s s e n t i a l 1 ~ y o n: ;t am t
( w i t h i n
1 +$).
T h e r e f o r e , b y as s um i ng a c o n s t a n t s l o p e 2 i . t
i s
possLbIe
t o r e c a l i b r a t e t h e p ro b e b y r a i s i n g the b i smuth L eve l o v e r t l i e probe .
T h e r e
w a s
a c o n s i d e r a b l e a m o u n t
of
c o r r o s i o n i . n t h e
l.oc)j) wli.:i.ch
probi~b1.y
accoun ted f o r t l ie s h i f t i n t he z e r o l e v e l p o i n t .
A
p a s s i v e KLC phase
c a l . i . b r a t o r was
c o n s t r u c t e d t o e l i m in a t e i n s t r u -
m e n . t
v a r i a t i o n s
It
g i v e s two measurements of
t h e
i.nst:rurrtt:nt gain. ( s ~ . o p e
and
two
:i.ndependei-it: nei3 sure Inen t s of t h e z e r o p o i n t .
T h e
1.orig-tc1.rm s t a -
b i I - i t y
o f
t h e c a I ih r a t :o r i s a p p r o x i m a t e l y 0 . 0 1 ” .
A d d i t i o n al i n f o r ma t i on on t h e l i n e a r i t y
t e s t s , ‘
t h e i n i t i a l . mcasure-
6
ments
a r e
g iv e n i n
o t h e r
r e p o r t s .
in. t l ie t e s t loop , and t l ie
: f i n a l
measurements‘ i n t h e t e s t l oo p
>
.
SUMMARY ANT) CONCX1ISIONS
The problem
f o r
a c . oi l e i t h e r e n c i r c l. i n g o r enc-.>sed by
a n
a r b i t r a r y
number
of
c o n d u c t o r s h a s bee11 s o l v e d . A c c u r a t e a nd versa : i Je computer
programs have
be t ~ i
w r i t t e n w h ic h n u m e r i c a l l y
eval .uate
t h e s e
s o l . u t i o n s
G o o d a g r e e m e n t h a s
been
o b t a i n e d b e tw e e n t h e c a l c u l a t i . o n s a nd e x p e i r i . m c ? r i t s .
These programs h a v e b ee n. a p p l i e d to d e s i g n very a c c u r a t e l i q u i d l e v e l
p r o b e s even
t hough
w e
a r e l o o k i n g t h r o u g h a
good
conductor (molybdenum)
arid m e as ur in g t h e l e v e l
o f
a p o or c o n d u c t o r ( b i s m u t h ) .
‘Id. E . McNeese e t l . ,-
E n g i n e e r in . g D ev el op me nt S t u d i e s f o r Mol.ten-
S a l t B r ee d er Reactor P r o c e s s in g No. 13, ORNL-TM--3776 ( i n p r e p a r a t i o n >.
I,. E .
McNeesc It
ala,
E nginee r ing Deve lopment Studies f o r
Molten-
S a l t
Breeder R
O I W L - T M - ~ ~
( i n
p r e p a r a t i o n ) .
‘L.
E . McNeese c t
l . ,
E ng inec r ing Deve lopment S t ud i e s F o r r l _ l t c n -
S a l t B r e e d e r R e a ct o r P r o c e s s i n g
N o .
16,
O I W L - T M - I I O ? ~ ( i n
p r e p a r a t i o T -
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6.
ACKNOWLEDGMZNTS
The
a u t h o r s wish
to
acknowledge
t h e
a s s i s t a n c e o f C . C . L u
in
t h e
p r e j
irninary programming, t
r a s s i s t a n r - o f
I 0 . Weeren,
I , .
D.
Chitwood,
a n d
0 . E . Conner i n p e rf o rm i ng
t h e
n e a s u r c m e n t s ,
Id.
E .
Deeds
slid
L . E .
McNeese
f o r e d i
Ling t h e i e p o r t , J a n i c e
Shannon f o r preparing the
f i n a l
manusc r ip t and Jerry R o t l i and L. E . McNeese for providing ovcrall
giii dailce
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APPENDIX A
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APPENDIX A
ComKuL-er.. P ro g ra m s f o r 3 Liq uid J ,evel Probe
I n s i d e
...
C o a x i a l C o n d u c t o r s
I. lNTKODUCTION
T hi s compute r p rogram
i s
u s e d t o ca l c ul a f rv t h e n o r m a l i z e d c o i l i mp ed -
a n ce of b o t h t h e d r i v e r and p i c ku p c o i l s o f an e d d y - c u r re n t p ro be , s u r -
r o un d ed by m u l t i p l e c o a x i a l c y l i n d r i c a l c o n d u c t o r s . T he p ro gr am mi ng
c o n s i s t s of a f u n d a m e n t a l s u b r o u t i n e namcd
I . N M L ,
which i s c a l l e d i n t o
e x e c u t i o n b y a m ai n D R I V E R program. INNMLTL b r a nc h e s t o e i g h t o t h e r new
s u b r o u t i n e s d u r i n g e x e c u t i o n .
Z N N N U T ,
i t s c l
f
i s
a d ap te d f ro m a n e a r l i e r
p rogram i n t h e BASIC l ang uage .
The FORTRAN-IV computer languagc i s u s e d , w i t h
REALYE
a r i t h m e t i c , o n
t h e IBF1/36G c o m p u t e r s .
l a t i o n s w i t h s u f f i c i e n t a c c ur ac y i n t h e c a s e of a " t h i n" r e g i on among
t h e c o n d uc t in g m e di a . I n c o n n e c ti o n w i t h tlij-s, yoine s p e c i a l s u b r o u t i n e s
w er e a l s o d ev el op ed f o r t h e c a l c u l a t j o n o f t h e n e c e s sa r y m od if ie d Re sse l
f u n c t i o n s , w i t h ac cu ra c y of a t l e a s t 15 s i g n i E ic a n t d ec im al d i g i t s f o r
r e a l a rg u m en t s, a nd lu s i g n i f i c a n t d i g i t s f o r c om plex a rg ii me nt s.
New work w a s d on e t o
c a r r y
o u t t h e ne ed ed c a l c u -
An o u t l i f i e of t h e p ro gr am f o l l o w s , w i t h d i s c u s s j o n an d p ro gr am l i s t i n g
o f e ac h s e p n r a t e r o u t i n e . The e i g h t s u b r o u t i n e s r e q u i r r d by I N W L a r e
named
X I I N T , X J J N T ,
GAMCLL, GCALC; MODBES,
CMDKES, COMKB,
and C M I . They
a r e ne ed ed f o r i n t e g r a t i o n s of x3 ( x ) and XI (x ) , f o r c a l c u l a t i o n oE t h e
gamma f a c to r , and f o r i i ie i r l o d i f i e d B e s s e l f u n c t i o n s .
1 1
L a s t a n i n t e r a c t i v e p r og ra m w i l l b e g i v e n f o r g e n e r a t i o n of t h r d a t a
b l o c k F i l e , which I n l i s t b e s u b m i t t e d
w i t h
t h e p r og ra m f o r e x e c u t i o n
011
t h e I B M , / ~ ~ O o m p u t e r .
T l i i s
program, named T E L J N C ,
i s
s t o r e d o n t h e
PDP-10
d is k, and may be used f rom
t h e
t e l e t y p e t o prep '3i-e t h e d a t a i n t h e n e c e s -
s a r y f or ma t f o r t h e D R I V E K . T he d a t a c o u l d , o f c o u r s e , b e s e t up f o r
e x e c u t i o n o f t h e p ro g ra m b y a n y o l -h e r c o n v e n i e n t m e t h o d.
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4 .
11.
DESCRIPTION OF
INNIYIJL
A .
D R I V E R
Program
The D R I V E R
main
p ro gr am r e a d s t h e d a t a f o r
t h e
c a s e s
t o
b e e x e c u t e d
b y
the INNfWL
s u b r o u t i r i e . A f t e r r e c e i vi n g t h e d a t a a n d
making
p r e l i m i n a r y
c a l c u l a t i o n s i f n e c e s sa r y , t h e D R I V E R t h e n b r a n c h ( i s t o INNMLJT,. A f t e r t h e
c a l c u l a t i o n
of
n o r m a l i z e d
c o i l
impedance
i s
comple t ed by INWRTL and
i t s
o t h e r s u b r o u t i ne s , t h e n
Lhe
DRIVER program prepares
a
summary print
o u t ,
showing data and
r e s u l t s .
Data must be g i v e n
t o t h e
DRIVER program f o r t h e
c o i l .
di .mensions, fo r
the a i r n o r m iI . i za t i o ii f a c t o r , an d
f o r
i n f o r m a t i o n a b o u t each r:oriductor
o u t s i d e t:h e c o i l . Th e
inner
r a d i u s , t h e r e I . n t l v e p e r m e a b i l it y ,
2
t h e v a l u e
of
t h e q u a n t i t y (~~p . n i? r e n ee de d f o r
each
c o n d u c t o r .
m
and
b 3 E L '
2
m
he D R I V E R program
i s
w r i t t e n
t o
r e c e i v e t h e q u a n t i t y ,
q J , u F
, i n any
one
of
t h r e e d : i . f f e r e n t
w a y s . F i r s t ,
t l i e v a l u e
of the
q u a n t i t y may b e
g iv e n d i r e c t l y f o r e a c h c o n d u c t o r . S ec on d, t h e f a c t o r
o
may b e g i v en f o r
each c o n d u c t o r . In
t h a t :
case, t he p e r m e a b i l i t y ,
p i i s
IT. x 1.0 x
li .
R A
Then t h e o p e r a t i n g f r e qu e n c y a l s o i s g i v e n i n o r d e r t o o b t a i n 1d
for
t h e
c o i l , and F i n
meters , i s
e i t h e r g i ve n o r c a 1. c ul o te d f o r t h e C L ~ ~ J . ,
- 7
m'
T hi rd , t h e r e s i s t i v i t y ,
p (pil-cm)
may be g iv en a s d a t a
f m ach
c o n -
8
d u c t o r . The r e l a t i o n b e tw ee n
p
and
i~ i s
g i v e n b y :
q u a n t i t y w y a r
i s
c a l c u l a t e d
a s O.. - ,Ogi9 j ?
x f r e q .
x
r
x
ilREL/p. The
c o n s t a n t
i s a
p r o d u c t of c o n v er s io n f a c t o r s
--
( 2 r / - ) ( O . O 2 5 4 ) hi x I . O ) ( l O ) .
T h e re f o re i n this t h i r d case, t h e known d a t a must i n c l u d e t h e d r i v i n g
f r e q u e n c y ( H e r t z ) , a n d
F
( i n . ) , a s
w e l l a s
r e l a t i v e p e r m e a b i l i t y . The
d e t a i l s o f s e t t i n g up t h e d a t a f o r s u b mi s s io n
with
t he compute r p rogram
wi1.L
b e gi v e n i n t h e
l a s t -
s e c t i o n .
o CL 10
p .
Then t h e
2
2
m
F o l l o w i n g
i s
a l i s t o f t l ie program DRIVER.
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A
0
y
i
x
L
03
r
I
4
v
D
C
L
M
P
0
U
F P
-
v
(
T
x
3
m
-
A
-
C
r
I
-
D
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44
9
10
1 I
5
1a Q
185
1 9 0
1 1
2
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45
11
l a ) INNMUL
T he fo rmula which
i s
c a l c u l a t e d by t h e INN?IUL s u b r o u t i n e
i s
t h e
n o r m a l i z e d c o i l i mp ed a nc e ,
of b o th t h e d r i v e r
and
p ic ku p c o i l s i n a b i f i l a r c o i l s ur r ou nd ed by
m u l t i p l e c o a x i a l c o n d u ct o rs .
T h e q u a n t i t y
i s
given by Eq. (50) .
I t
i s c a l c u l a t e d by a b r an c h t o t h e
X I I N T
f u n c t i o n
s u b p r o g r a m . S i m i l a r l y , t h e q u a n t i t y ,
i s
g i v e n by E q .
r a t i o ,
U12/U22,
o r gamma, i s c a l c u l a t e d b y
a
b r a n c h f r o m INNMUL t o t h e
GAMCAL
s u b r o u t i n e .
(56) and i s c a l c u l a t e d b y
the
X J J N T subprogram.
The
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The X I I N T ,
XJJNT,
and GAMCAL s u b r o u t i n e s w i l l
b e
d i s c us s e d s e p a r a t e l y .
The i n t e g r a n d i n t h e n u m er a to r o f t h e i mp ed an ce f o r m u la i n INNMUL
-(XI,
c o n t a i n s a t:errn w i t h t h e f a c t o r ( X -C E
v a l u e s o f
CiL
l e s s
t h a n
0.5,
t h i s f a c t o r i s c a lc u l a t e d by t h e r a t i o n a l
a p p r o x i m a t i o n ,
-
l ) , where I,
=
k - A l . For
2
8
T h i s
i s
d e r i v e d a s a c o n t i n u e d f r a c t i o n a pp ro xi ma nt f ro m t h e P a d e ' t a b l e
a s s o c i a t e d w i t h t h e p ower
s e r i e s ,
-a.
I f CXL
i s
l a r g e r t h an 20, e i s d ro pp e d f ro m t h e c a l c u l a t i o n of
01+
r
--
1 ) . F o r a?, be tween
0.5
and
20,
e
i s
e v a l u a t e d b y L h e e x p o n e n t i a l
f u n c t i o n s ub pr og ra m a v a i l a b l e
i n t h e 1 ~ ~ / 3 6 3ORTRAN l i b r a r y .
-OX A
T h e q u a n t i t y (1
-
cos(ol?,)
w hi ch a p p e a r s i n o n e
t e r m
o f L h e i n t e g r a n d
2 L
2
s o b t a i n e d by t h e h a l f - a n g l e f o rm u la f ro m si n (- ) .
The o v e ra l l i n f i n i t e i n t e g r a l
i s
a p p r o x i m a t e d i n INNMUL
for
a n u p p e r
l i m j t o f 16. T h e a v e r a g e o f t h e i n t e g r a n d
i s
c a l c u l a t e d f o r
100
e q u a l l y -
s p a c e d p o i n t s f r o m
0
t o 1 . F o r e a c h o f t h e r e m a i n i n g 15 i n t e r v a l s oL
u n i t l e n g t h , t h e a v er a ge of t h e i n te g r a n d f o r 20 e q u a l l y s p ac e d p o i n t s
i s u s ed . T h i s h a s be en f ou nd t o g i v e a s u f f i c i e n t l y good a p p r o xi m at i on
t o t h e i n t e g r a l and
i s
named
17
i j I 6 i n t he p rograu i .
A t
t h e same
t i m e
d ur in g t h i s c a l c u l a t i o n i n
'LNNMTJL,
i n t e g r a t i o n
i s
p e rf o rm e d i n d e p e n d e n t l y o n t h e s e c o n d t e r m o f t h e i n t eg r a n d t o o b t a i n
a n e s t i m a t e d a i r v a l u e , named
19.
The a i r va l ue c o n t r i b u t e s t o t h e r e a l
p a r t o f t h e i n t e g r a l , 17, and
i s
b y f a r t h e s l o w e s t p a r t t o co nv er ge .
We
'Als ton
S .
Househo lde r ,
A
G l o s s a r y f o r N u m e r ic a l A n a l ys i s 2
ORNL-2704,
pp 73
-7'4
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c n l c u l a t e t h e air v a l u e i n s c p a r a t e program and givc. t h ~a l u e
a s
p a r t
o f
t h e
d a t a to t h i s p r o g r a m , a s Ag.
The
a i r v a l ue d e p e n d s o t l ly on t h e
o n
t h e c o i l
dimensions
a nd not on
the
c o n d u c t o r , 2 n d
i s
( T h i s term a p p e a r s b o t h i n t h e n u m e r a t o r
and
the denorn ina to r . )
T h e r e f o r e , we c a n o b t a i n
t h e
c o m p l e t e l y c o n v e r g e d
real part
oi t h e i n t e -
g r a l
by
a d d i n g t h e d i f f e r e n c e b et we en A3 and 19. The completely c o n -
v e r g e d r e a l p a r t i s I'( t
(Arj-Iy).
The
normalized impedance is
A listing
of IplNMuL f o l l o w s .
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48
c
C
c
C
C
C
C
C
c
c
C
c
C
C
c
C
C
1
t i l =
I N N E X C U L L
i < A D I U > / MLAN
C D I L t I A D I U S
r
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49
c
G l = O . D O
I;Z =H%
P R I N T 3
3
F ~ K M A T C ~ X ,X ' P
1 4 A 9
'AIR V A L U E U r 5 X ~H E A L
P A t < T ' > G X , ' I M A G
P A R T ' / / / )
C
c b E G I N LMBP DN A L P H A > l l H I C H IS T H E V A K I A L ~ L E NAMED X
c
125 J 7 = 0 * O
J S = O . D O
J ' 9 = O o D O
X = t i * i i 1 * 0 * 5DO
130 W9 = X * L
G I l = )< *X
O = O f * Q 1
Q 6 = 2 * W 1
c
C
C
135
1 4 0
C
c
c
C
c
c
145
KL
C
GAMMA )= ii6 J
I
M
C G A M M A
1=F7
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11.
B e l
and
2 )
X J J N T
and X I I N T
T he se t w o f u n c t i o n s u bp ro gr am s e v a l u a t e t h e e x p r e s s ions,
and
2
x I 1 ( x ) dx ,
xr-l
r e s p e c t i v e l y . These a r e equal. t o t h e va1.i.ies g i v e n f o r
J ( r , > ,
) i n E q .
( $ 6 )
and
I ( r < , r )
i n
E q . (50).
The method
of
i n t e g r a t i o n in l ~ o t i
ases ,
for- a n
u p p e r l i m i t n o t g r e a t e r t h a n
5, i s
t h e summati -on o f a p o w e r
s e r i e s
expre:;-
s i o n
u n t i l t h e
l.nst
i n c l u d e d t e r m i s I.ess t h a n t imes t h e c u r r e n t
s u m .
I f
t h e
upper 1.iinf-t
of the i n t e g r a l
is
g r e a t . e r t h a n 7, a s y m p t o t i . c
formu.--
l a s a r e u s e d
i n
b o t h s u b r o u t i n e s . I n g en .e ra l a p p l i c a t i . o n , we assume
i .a i
t h e s e s u br o u t i n e s t h a t
b o t h
1.imits a r e n o n r i e g a t i v e and
tilie
l o w e r
l i m i t i s
less t h a n O K e q u a l t o t h e u p pe r I .i mi t
on
t h e i n t e g r a l .
r._ 1
2 1
9
An e x p l a n a t i o n f o l l o w s
f o r
the summation method ,
w h i c l t i s uscil i n t h e
c a se
t h a t t h e u pp e r
l i m i t i s l e ss
t h a n o r
e q u a l
t o
5.
For t h e p u r p o s c o f e x p l a i n i n g t h e g e n e r a l mcthod
o f i n t e g r a t i o n , l e t
f x ) b e a ny f u n c t i o n
o f
a
r e a l
v a r i a b l e w it h t h e
Taylor
s e r i e s
expanPion,
Term wise i n t e g r a t i o n y i e l d s
( 771
9W.
A . Si m pson
et GP j omputer Yrogrnins f o r Some Eddy-Curren t
Problems
- 1970, ORNL-TM-3335 p . 259
( J u n e lg'(1
) .
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52
I n t r o d u c e a new sequence,
2 2
2
b-
--
a
-
..
,
and
s o
o n . I n r e l a t i.onnd i t
i .s
s e en t h a t
q
0
=I,
q
1
= = b- . a ,
q 2
t o t h i s s eq ue nc e, o u r i n t e g r a l may be w r i t t e n a s
W
T h i s i s t h e s e r i e s t o b e a p p r o x i m a t e d .
R e c ur r en c e r e l a t i o n s may b e d c r i v e d t o g e t t h e t er m s o f t h e q - se q u en c e
i n t h e f o l l o w i n g w ay. Use t h e a 1g eb ra i. c i d e n t i t y
(‘19)
n
n
-1 n - 1 a b ( b n - 2
-
a n - 2 )
bn -
a
= (cl-tb)(b
- - - a
)
-
11
T h i s g i v e s , w i t h n q
T he n d i v i s i o n by n and s i m p 1 i f i . c a t i o n g i v e s
::: (bn - a ), n qn :: ( a + b ) ( n - l ) q n-1 - a b ( n - 2 )
q
11-2-
n
S i m i l ar l y , one c a n s t a r t w i t h t h e i d e n t i t y
n
2 2 n - 2
n - 2
2 2 11-4 n - 4 )
b n - a = : ( a + b ) ( b - a ) - a b ( b - a
t o o b t a i n a s e co nd u s e f u l r e c u r r e n ce r e l a t i o n ,
(80
( E 2 )
I n t h e f u n ct i on s X J J N T a nd XIINT, t h e s e c on d r e c u r r e n c e r e l a t i o n i s used
f o r n g r e a t e r t h an
3 ,
of xJl(x) and
xT1(x) .
s i nc e a l t e r n a t e
t e rms
a r c z e r o f o r t h e power s e r i e s
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53
I n
o r d er t o a p p l y
t h i s
i n t e g r a t i o n p r oc e du r e,
l ook
f i r s t a t t h e
power se r i e s" f o r
~ ] . ( x ) :
Then
m 2r
+
1
r
( r - i - l )
(86
k )
2k-l
k/2-1 )
(k/2)
(k
)
k
X
X I . x ) =
k=2
( e v e n v a l u e s
o n l y )
I n t h e p r ec e di n g e x p r e s s i o n , (k
)
d en om i na to r, t o c o i n c i d e w i t h t h e
f
k=
0
h a s b e e n m u l t i p l i e d i n t o n u m e r at o r a nd
T a y l o r s e r i e s
k
k k
x .
Then
i t i s
e a s i l y seen t h a t
t h e
c o e f f i c i e n t s f o r an even number
k
a r e :
= 15/8, w i t h
c6
= 1, c4 = y 2 ,
2
k
T he se e ve n- i nd ex ed c o e f f i c i e n t s a r e r e l a t e d by
c
o t h e r
c o e f f i c i e n t s ,
co ,
e l ,
c 7 ,
c5,
. .
a r e z e r o .
c i e n t s h o l d f o r
Jck = ( k + l ) / k .
A l l
k-t,
The same
c o e f f i -
J
'OH. J e f f r e y s a nd 3. S.
Jeffreys,
Methods
of
M a t h e m a t i c a l Phys ic s ,
p .
574,
C am b ri dg e U n i v e r s i t y P r e s s , 1950.
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54
x J l ( x )
x
J
r2lrl
w i t h
t h e
e x c e pt i on t h a t t h e
terms
a r e a l t e r n a t i n g i n s i g n .
The summation m et hod , which j s d e s c r i b e d a b o v e , i s c o m b i n e d w i t h t h e
9
a s y m p t o t i c f or mu la s’ , f o r t h e c a s e t h a t t h e l o we r
l i m i t
i ; l e s s t h a n o r
e qu a l t o 5 , b u t t h e u p p er 1 i i i i i . t
i s
g r e a t p r t h a n
5.
L is t i ngs o f XI INT and X J J N T f o l l o w ,
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c.
i;
f
9 0
1 C 5
c.
c
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56
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.
\
z
L
\
L
C
i
z
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1
5r'
1 r 5
3 C 5
3
0
3 1 1
::
)r
3 1
5
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59
11. B ( 3 )
GAMCAL
uL2/
he GAMCAL s u b r o u t i n e i s used by INNMLJL
t o
compute gamma r a t i o ,
UZ2, w hic h a p p e ar s i n t h e f i r s t t e rm
of
t h e i n t e g ra n d of i n t e r e s t i n
INNMUL
.
I t
i s n e c es s a ry i n t h e c a l c u l a t i o n s o f
GAMCAL t o
h a v e g i v e n t he quan-
~
F 2
named
%, f o r
e a c h c o n d u c t o r .
I n t h i s p ro d uc t i?
i s
t h e
Wlik
k m ’
m
i t y ,
mean
c o i l r a d i u s i n m e t e r s . The a n g u l a r f r e qu e n c y
of
t h e d r i v i n g c u r r e n t
i s
g iven by
w .
The o t h e r v a r i a b l e s I arid
7
a r e t h e p e r m e a b i l i t y a nd
c o n d u c t i v i t y , r e s p e c t i v e l y , of t h e c o n d u c t o r . F o r e a c h c o n d u c t o r ,
k k
where a i s t h e v a r i a b l e of i n t e g r a t i o n
i n
INNMLJL. Then,
The i n n e r r a d i u s and r e l a t i v e p e r m e a b i l i t y m u s t a l s o
be
known f o r
e a c h c o nd u ct o r f o r t h e c a l c u l a t i o n s t o o b ta in gamma. Cau t ion m u s t b e
e x e r c is e d i n t h e c a s e o f a l a r g e p e r m ea b i l i ty t h a t t h e c a l c u l a t i o n s do
n o t l e a d t o c om pu te r o v e r f l o w o r u n d e r f l o w.
The u s e of t h e z e r o - t h and f i r s t o r d e r m o d i li e d B e s s e l f u n c t i o n s
h a s b ee n s ee n i n t h e c h a p t e r d e a l in g w i th t h e o r e t i c a l a n a l y s i s .
s u b r o u t i n e s h a v e b e en w r i t t e n
t o
s e c u r e
more
s i g n i f i c a n t f i g u r e s th a n
p r e v i o u sl y a v a i l a b l e i n t h e c a l c u l a t i o n s o f
GAMCAL.
T h e s e s u b r o u t i n e s ,
names
MODBES,
CMDBES,
COMKB,
and CM I , w i l l b e d e s c r i be d i n d i v i d u a l l y .
New
A d i s t i n c t i o n
i s
made be tween a norma l condu c to r r e g io n and a “ t h in ”
c o n d u c t o r r e g i o n .
A
r e g i o n
i s
c l a s s i f i e d a s t h i n i .f
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t h e o u t e r b o u nd a ry
of
r e g i o n k ,
k-1’
h e e l e m e n t s of t h e T - m a t . r i x a t
r
a r e
T
11 k , k - 1 ) = z K 0 ( z ) I 1
(a
- l r k - l 1
(89)
T 1 2 ( k , k - l ) :::
z K ~ ( z ) K
(a - l r k - l
1
(90
and
T22 k , k - 1 ) = z l O ( z ) K1(a - l r k - l )
(92
(pk/bLk- l ) ak - l rk - l K() (%-l rk- l ) ‘1 (’)
where /. = CI r
(93
k k - l *
For cross ing a normal . ,
o r
“ t h i c k “
reg ion ,
t h e s e m a t r i x e l em e n t s a r e
computed
b y GAMCAL
a c c o rd i n g t o t h c ab ov e r e l a t i o n s h i p s .
H owev er, i f t h e r e g i o n i s “ t h i n ” , a s p e c i a l p r o c e d u r e i s u s e d .
I n
t h a t ca s c, n o t e t h a t a t
t h e
i n n e r
boundai-y, r of
t h e r e g i o n k, t h e
m a t r i x e l e me n ts a r e
k’
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61
To
c r v s s r e g i o n k, t h e
T-rna t r ix
i s
the p r o d u c t T
In t h e
f o l l o w i n g
e q u a t i o n s we
w i l 1
d r o p
t h e ( k i 1 , k - 1 )
f o r convenier icc .
- k + l , k :k,k-l Tki1,k-I.
T h e
matrix
eI.ernents
of the
p r o d u c t
a r c ?
t h e n
T12 = T
1
(k - I - l , k )
T
1 2( k , k - I )
- -
T l f ( k + l , k )
T
2 k , k - 1 ) ,
(100)
TZ1 =;
T,.,
( k + l , k ) T .
(k,k-1) i-
Tpp(k-i-1.,k)
T
( k , k - 1 )
,
(7.01.
)
1
1.1 . ..
21
a n d
(k-i-1,k) T12(k,k-1) 1 T, , , (k t l ,k)
T , > , , ( k , k - l )
(102)
21.
L . L- ..
T,,,,
=
T
:..d
This matrix
rnuI . t i p1 . i ca t i on y i e l d s t h e
following
complcx
e l e m e i ~ t s
of t h e
p r o d u c t m a t r i x :
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n
9
N
W
s
N
W
d
H
Y
/
-
u
-
g
4
,
H
W
-
n
-
d
W
I
N
W
w
d
m
N
H
v
d
-
i
d
W
I
N
v
W
W
d
H
.
N
W
b
i
N
W
s
G
N
U
W
3
r
7
4
v
N
W
r
H
5
N
W
s
o
N
W
-