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2 , 4 ? 6 9 2 6 9
2 Sheets-Sheet
1
I I S
AGENT
f e m
m aw-MM* Wu9476925@
R .
B . BLACKMAN
MECHANICAL
DIFFERENTIATOR FOR
SMOOTHING
T A R G E T
TRACKING DAT A
F i l e d
A l l g .
2 0 , 1 9 4 5
ammi ;
. F u ñ y i 9 , 1 9 4 9 .
_
/M/E/VTOR
@ i B . BLACK/WIV
V ,
8/11/2019 Us 2476269
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2 9 4 7 7 6 , 2 6 @
â@MC/WAN
R . B .
BLACKMAN
MECHANICAL DIFFERENTIATOR FOR SMOOTHING
TARGET TRACKING DATA
, 1945
J u l y
ï g ,
i l e d A u g . 2 O
w
S
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P a t e n t e d J u l y
1 9 , 1 9 4 9
2 , 4 7 6 , 2 6 9
UNITED STATES
PATENT
OFFICE
2 , 4 7 6 , 2 6 9
MECHANICAL
DIFFERENTIATOR
FOR
SMOOTHIN
G
TARGET
TRACKING
DATA
Ralph B .
Blackman,
C r a n f o r d , N . J . , a s s i g n e r t o
B e l l
Telephone L a b o r a t o r i e s , I n c o r p o r a t e d , New
York, N. Y . ,
a
corporation
o f New o r k
A p p l i c a t i o n
A u g u s t 2 0 ,
1 9 4 5 , S e r i a l N o . 6 1 1 , 6 3 9
( C l .
2 3 S - 6 1 . 5 )
Claims.
1
This
i n v e n t i o n
r e l a t e s t o
a n
i mpr ove me nt
i n
m e c h a n i c a l d i f f e r e n t i a t o r s ,
p a r t i c u l a r l y u s e f u l
i n
a mechanical system f o r
i n d i c a t i n g
a n angular
v e l o c i t y .
The
g e n e r a l
o b j e c t
o f
t h e
i n v e n t i o n
i s t o p r o
v i d e improved
means
f o r i n d i c a t i n g t h e a n g u l a r
v e l o c i t y
o f
a
s h a f t o f
which t h e v a r y i n g angular
p o s i t i o n a n d t h e angular
v e l o c i t y
r e p r e s e n t
r e
s p e c t i v e l y
t h e varying value o f an observed q u a n
t i t y and t h e time
r a t e
o f
change t h e r e o f .
The o b s e r v e d
q u a n t i t y
m a y be t h e h o r i z o n t a l
displacement
o f
a n
a i r p l a n e
i n
i i i g h t
o f
which
t h e p o s i t i o n i s c o n t i n u o u s l y r e c o r d e d
by
an o b
s e r v e r o n
the
groun d. T h e o b s e r v e r ’ s
instruments
may
themselves
be i i a w l e s s but h i s use o f t h e m
i s
u s u a l l y
a f f e c t e d b y r a n d o m e r r o r s o f
overrun
n i n g or u nd er r u nn i ng
a n d
when a shaft
i s
ro
t a t e d t o f o l l o w t h e v a l u e o f t h e o b s e r v e d q u a n t i t y ,
t h e a n g u l a r p o s i t i o n o f
t h i s
s h a f t d o e s n o t change
unif ormly with time even
f
t h e o b s e r v e d q u a n t i t y
i s
s o
c h a n g i n g .
I t
thus
becomes n e c e s s a r y
t o
p r o v i d e
m e a n s
f o r
measuring
t h e s h a f t
angular
v e l o c i t y
and smoothing
o u t
t h e
r a n d o m
v a r i a t i o n s
t h e r e i n .
A u r t h e r
o b j e c t
o f
t h e i n v e n t i o n i s t h e r e f o r e
t o
provide i m p r oved m e a n s
f o r
obtaining
a
smoothed
average o f t h e
angular v e l o c i t y
o f the
r o t a t i n g
s h a f t by e l i m i n a t i o n o f
r a n d o m e r r o r s
o f
o b s e r v a t i o n .
I t may be shown b y mathematical a n a l y s i s
t h a t
i f
a
s e r i e s
o f o b s e r v a t i o n s
o f
instantaneous
an gular v e l o c i t y are averaged over a
convenient
t i m e
i n t e r v a l ,
t h e a n g u l a r v e l o c i t y
b e i n g
found
constant
f p e r f e c t l y o b s e r v e d ,
t h i s
average should
be
obtained
by
p a r a b o l i c weighting
o f
the
s u c c e s
s i v e a n g u l a r v e l o c i t i e s ; t h a t
i s , t h e l e a s t
w e i g h t
should be
g i v e n
t o
the
v e l o c i t i e s
observed
a t
the
b e g i n n i n g a n d a t
t h e
e n d , and
t h e
maximum
weight
t o
t h o s e
a t
the c e n t e r ,
o f
the i n t e r v a l .
T h e
average v e l o c i t y
s o
obtained w i l l be i d e n t i c a l
with
that d e r i v e d
f r o m
the s l o p e o f
a
s t r a i g h t
l i n e
ñtted by a l e a s t squares adjustment
t o
the
s u c c e s s i v e a n g u l a r s h a f t p o s i t i on s p l o t t e d a g a i n s t
time
a n d
the r a n d o m e r r o r s a l l u d e d t o
w i l l
be
f i l t e r e d o u t .
A c c o r d i n g l y ,
i t
i s
another o b j e c t
o f
t h e
inven
t i o n t o
p r o v i d e means
f o r
o b t a i n i n g with a p p r o x i
mately p a r a b o l i c
weighting over
a
convenient
time
i n t e r v a l
the
average value over
that
i n t e r v a l
o f t h e angular v e l o c i t y o f a
r o t a t i n g
s h a f t .
While
t h e
apparatus o f t h e
i n v e n t i o n
may be
m a d e
s u f û c i e n t l y
complex
t o
approach
a s
c l o s e l y
a s d e s i r ed t h e i d e a l
p a r a b o l i c
Weighting
o f i n s t a n
t a n e o u s a n g u l a r v e l o c i t i e s , t h e
i n v e n t i o n
w i l l b e
s e t f o r t h with r e f e r e n c e t o two embodiments
which approximate t h e
i d e a l
a n d
c o n s t i t u t e
i m
provements
o v e r the mecha n isms k n o w n
t o
the
p r i o r
a r t .
The e l e c t r i c a l a n a l o g u e o f t h e mechanical
p r o b l e m
i s f o u n d
where t h e v a r y i n g o b s e r v e d
10
1 5
20
25
30
35
40
45
50
6 0
2
q u a n t i t y
i s r e p r e s e n t e d by a v a r y i n g
v o l t a g e
which i s d i f f e r e n t i a t e d with r e s p e c t t o time
a s ,
f o r
e x a m p l e ,
by t h e d i f f e r e n t i a t i n g a m p l i f i e r d i s
c l o s e d b y E . L .
N o rt o n
i n
United
S t a t e s
Patent
2 , 3 2 4 , 7 9 7 , J u l y 2 0 , 1 9 4 3 . I t i s k n o w n t h a t a n am
p l i ñ e r
having a feedback
path i n c l u d i n g an
i n t e
g r a t i n g c i r c u i t
p r o v i d e s an
o u t p u t
v o l t a g e
which
i s t h e t i m e d e r i v a t i v e o f t h e i n p u t
v o l t a g e .
The
p r e s e n t i n v e n t i o n a p p l i e s t h i s p r i n c i p l e t o
me ch
a n i c a l d i f f e r e n t i a t o r s , s o
t h a t
another o b j e c t o f
t h e i n v e n t i o n
i s
t o p r o v i d e an
improved
me chani
c a l t r a n s m i s s i o n
system
o f t h e t y p e
having be
tween i n p u t a n d output a
mechanical feedback
path c o m p r i s i n g mechanical i n t e g r a t i n g means.
The i n v e n t i o n w i l l
be
understood f r o m
t h e
f o l
lowing d e s c r i p t i o n read with r e f e r e n c e t o
t h e a c
companying
d r a w i n g s
i n
w h i c h :
F i g .
1 p r e s e n t s
c u r v e s
e x h i b i t i n g c e r t a i n
weighting f u n c t i o n s , i d e a l a s
w e l l a s p r a c t i c a b l e ;
F i g .
2 shows a simple mechanical system
ac
c o r d i n g t o t h e p r i o r
a r t f o r i n d i c a t i n g
t h e angu
l a r v e l o c i t y o f
a
r o t a t i n g s h a f t ;
F i g .
3 shows
s c h e m a t i c a l l y
one
embod i me nt
o f
t h e
p r e s e n t
i n v e n t i o n ;
and
F i g .
4 s i m i l a r l y
shows a n o t h e r embodiment o f
t h e
i n v e n t i o n .
In a l l f i g u r e s , l i k e numerals
and
l e t t e r s d e n o t e
l i k e elements.
I t
w i l l
be
convenient
t o
use the n o t a t i o n
o f
t h e o p e r a t i o n a l
c a l c u l u s t o
d e s i g n a t e t h e
v a r i o u s
s h a f t
r o t a t i o n s i n v o l v e d
i n t h e apparatus shown
i n
F i g s .
2 t o 4 ,
i n c l u s i v e .
In t h i s
n o t a t i o n
p f
( t ) i n d i c a t e s t h e
t i m e d e r i v a t i v e ,
w h i l e
1
i f
i )
i n d i c a t e s t h e t i m e i n t e g r a l o f t h e f u n c t i o n f ( t ) .
No
o r e than the r e s u l t s o f mathematical analy
s i s w i l l be s t a t e d h e r e , f o r the reason that
a math
ematical
d i s c u s s i o n i s
unnecessary
t o a n u nd er
s t a n d i n g
o f t h e i n v e n t i o n .
The
a n g u l a r p o s i t i o n
o f a
s h a f t w i l l
be
d e s i g n a t e d by 0 , t h e angular
v e l o c i t y by
0 w i t h s u b s c r i p t s where
a p p r o p r i a t e .
Th e
mechanical
t r a n s m i s s i o n c i r c u i t
beyond
t h e
r o t a t i n g s h a f t
o f
which
t h e a n g u l a r v e l o c i t y
i s t o
be i n d i c a t e d ,
i s analogous
t o
a n e l e c t r i c a l
t r a n s m i s s i o n c i r c u i t i n which t h e output c u r r e n t
e q u a l s
i n p u t
v o l t a g e m u l t i p l i e d b y
t h e s t e a d y
s t a t e t r a n s f e r a d m i t t a n c e ,
which
may e chosen
b y c i r c u i t
d e s i g n
t o r e s u l t i n
an output c u r r e n t
p r o p o r t i o n a l
t o
t h e
t i m e
d e r i v a t i v e o f
t h e i n p u t
v o l t a g e . The i n d i c i a l admittance o f
t h e
c i r c u i t
i s
t h e
w e i g h t i n g
f u n c t i o n
a c c o r d i n g t o
which
i s
a v e r a g e d
t h e
o u t p u t c u r r e n t
t o r e p r e s e n t t h e
b e s t
t i m e d e r i v a t i v e o f t h e i n p u t
v o l t a g e ,
which
may
e varying
a t a u ni fo r m r a t e p l u s the
super
p o s i t i o n o f r a n d o m i r r e g u l a r i t i e s .
T o s o l v e
t h e
problem o f mechanical d i i î e r e n t i a
t i o n ,
one
s p e c i e s
t h e d e s i r e d
mechanical
i n d i c i a l
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2 , 4 7 6 , 2 6 9
3
a d m i t t a n c e , t h a t
i s ,
a mechanical w e i g h t i n g func
t i o n ; d e r i v e s
f r o m
t h i s t h e mechanical t r a n s f e r
a d m i t t a n c e ; and f i n a l l y
d e s i g n s
a
mechanical
system p o s s e s s i n g
a p p r o x i m a t e l y t h e
t r a n s f e r
admittance d e s i r e d . In both the e l e c t r i c a l a n d
the
mechanical
c a s e ,
the
i d e a l
s o l u t i o n
i s
f o r e
g o ne f o r p r a c t i c a l reasons.
R e f e r r i n g
n ow
t o
F i g . 1 , c u r v e s
A ,
B , C a n d D
a r e
w e i g h t i n g
f u n c t i o n s
p l o t t e d
with weight
f a c
t o r a s o r d i n a t e a g a i n s t time a s a b s c i s s a , the
u n i t
o f time b e i n g
p r o p o r t i o n a l
t o
t h e time c o n s t a n t
o f t h e
averaging mechanical network. This
time
c o n s t a n t i s
d e t e r m i n e d ,
a s l a t e r e x p l a i n e d , b y
the
g e a r r a t i o s
and
m otor s p e e d s i n F i g s . 2 , 3
a n d
.
In F i g .
1 , c u r v e A
s
t h e e x p o n e n t i a l weighting
f u n c t i o n g i v e n by t h e s i m p l e d i f f e r e n t i a t o r o f F i g .
2 . Curve
B
s t h e i d e a l p a r a b o l i c W e i g h t i n g which
i s zero a t time z e r o a n d u n i t y . Curve C s o ne
a p p r o x i m a t i o n t o
c u r v e B ,
p r a c t i c a l l y
r e a l i z e d
by
t h e p r e s e n t i n v e n t i o n i n t h e embod i me nt shown
i n
F i g . 3
a n d
curve
D
s
a
b e t t e r
approximation
than curve
C which
i s
r e a l i z e d
by the
system
shown i n F i g .
4 .
The
improvements
p r o v i d e d
by t h e p r e s e n t i n
vention a r e b e s t d i s c u s s e d a f t e r a d e s c r i p t i o n o f
F i g . 2 , which shows
a s i m p l e system
o f apparatus
whereby t h e a n g u l a r v e l o c i t y
o f
a r o t a t i n g s h a f t
may
e measured. Shaft I 0 ,
t u r n i n g
i n
the
s e n s e
i n d i c a t e d
by the a r r o w ,
o c c u p i e s
momentarily
an
angular
p o s i t i o n
0 1 which v a r i e s with time a t
the
r a t e 0 1
which
i s
t o be determined.
Thr ough
d i f f e r e n t i a l gear I I , s h a f t I 0 d r i v e s s h a f t I 2 o n
which i s c a r r i e d p o i n t e r I 3 , t h e a n g u l a r
p o s i t i o n
o f which i s
read
o n
d i a l I 4 .
From s h a f t I 2
through b e v e l
g e a r s
I 5
i s
d r i v e n s h a f t I 6 c a r r y
i n g p i n i o n
I ‘ I
which moves
rack
I 8
t o
t h e
r i g h t ,
when
s h a f t I 6 turns i n the i n d i c a t e d
d i r e c t i o n .
A onstant speed mot o r
CSMI,
o f any
k n o w n
d e s i g n ,
d r i v e s a s i n d i c a t e d d i s c 2 0 ,
which
through
c o n t a c t i n g s p h e r i c a l b a l l s
2 | t u r n s r o l l e r 2 2 about
a n a x i s
a t r i g h t
a n g l e s t o the
a x i s
o f m o t o r
CSMI a t a
r o t a t i o n a l speed
determined b y
the
r a d i a l l o c a t i o n o f b a l l s 2 | o n d i s c 2 D .
The
x i s
o f r o l l e r 2 2
i s
prolonged
a s
s h a f t 2 3 ,
terminated i n
spur gear 2 4 meshing
with
r i n g gear 2 5 o f
d i f
f e r e n t i a l I I . B a l l s 2 | , which may be o f any de
s i r e d
even
number, two
b e i n g shown
i n
F i g .
2 ,
are b y a n y s u i t a b l e
m e a n s constrained b y
the
motion
o f rack
I 8
t o m ove
r a d i a l l y
with
r e s p e c t
t o d i s c 2 0 which r e s u l t s i n a n angular
speed
o f
r o l l e r
2 2 p r o p o r t i o n a l t o
t h e
a n g u l a r
p o s i t i o n
o f s h a f t
I 6 .
Th e d i s c
a nd
r o l l e r system j u s t de
scribed may
be such a s
s h ow n
i n United
States
Patent
1 . 3 1 7 . 9 1 5 ,
October
7 , 1 9 1 9
t o
H. C . Ford o r
i n United S t a t e s
Patent
2 , 0 0 2 , 5 8 5 , May 8 , 1 9 3 5
t o J . J .
Rothwell e t a l . I t w i l l
a t
o n c e
b e
recog
n i z e d t h a t t h e angular p o s i t i o n
o f
s h a f t
2 3
changes i n a n y
time
i n t e r v a l
b y an a m o u n t pro
p o r t i o n a l t o t h a t i n t e r v a l m u l t i p l i e d by
t h e
r a d i a l
s h i f t o f
b a l l s
2 | f r o m the c e n t e r
o f d i s c 2 0 ;
that
i s ,
t o
t h e
r o t a t i o n o f
s h a f t
I 5 ,
which
i s
t h e
s a m e
as
that
o f shaft
I 2 i f gears
I 5
are
o f
unity
r a t i o . When
s h a f t s
I 2 and I 6 through p i n i o n
I 1
a n d rack I 8
a r e
s e t t o
c e n t e r
b a l l s 2 l i o n d i s c
2 0 , p o i n t e r
I 3
i s
a d j u s t e d o n
s h a f t I 2 t o
read
zero
o n
s c a l e
I 4 .
Now, i f
t h e
angular p o s i t i o n 9 2 o f s h a f t I 2
r e p r e s e n t s
an angular v e l o c i t y , t h e r o t a t i o n o f
s h a f t 2 3 d u r i n g any time i n t e r v a l i s p r o p o r t i o n a l
t o
the
time i n t e g r a l o f 6 2 over
that
i n t e r v a l . In
t e r m s
o f
t h e o p e r a t i o n a l c a l c u l u s , t h e a n g u l a r
p o s i t i o n
0 3
o f
s h a f t 2 3 i s
1
-0
p
1 5
25
3 0
35
4 0
60
7 0
By s u i t a b l e c h o i c e o f t h e g e a r r a t i o between
g e a r s
2 4 a n d 2 5 a f r a c t i o n
o f t h i s i n t e g r a l
may
b e impressed
a s
a
r o t a t i o n
o f
r i n g
g e a r
2 5 j u s t
s u f f i c i e n t
t o
o f f s e t t h e r o t a
t i o n o f
s h a f t
I 0 ,
whereupon s h a f t
I comes t o
r e s t
a t a n angular departure 0 2
f r o m
the zero
s e t t i n g above d e f i n e d . When h i s
c o r n e s
about
n o further r o t a t i o n o f
shaft
I 2 takes p l a c e .
0 2
read
o n s c a l e I 4 i s
then
the measu r e o f the a n g u
l a r v e l o c i t y o f
s h a f t I 0 : 01=p0i=6a
The elements f r o m
g e a r s
I 5 through r i n g
gear
2 5 c o n s t i t ut e a n i n t e g r a t i n g mechanical feedback
path
between
o u t p u t
s h a f t I 2 and i n p u t s h a f t I 0 .
The
r e g u l a t e d
power
s u p p l y 3 0 , o f
any
k n o w n
f o r m ,
s u p p l i e s
power
t o d r i v e
mot or I 9 , t h e s p e e d
o f
which m a y
b e
a d j u s t e d
by v a r y i n g r e s i s t o r
3 | . The i n t e g r a t o r above d e s c r i b e d i s g e n e r a l l y
d e s i g n a t e d
a s 9 0
i n c l u d e d
i n
dashed
r e c t a n g l e
I ,
F i e . 2 .
Whenever
a sudden change
i s
brought i n
the
angular
v e l o c i t y
o f
s h a f t I 0 a c e r t a i n
time i n
t e r v a l must
e l a p s e b e f o r e s h a f t I 2
t u r n s
t o
the
corresponding
new
steady reading
o n s c a l e I
4 .
The readjustment
o f s h a f t I 2
i s a t f i r s t r a p i d a n d
then
m o r e
s l o w .
A s may b e
shown
b y a n a n
a l y s i s h e r e o m i t t e d , t h i s
r e a d j u s t m ‘ e n t o b e y s
t h e
law o f c u r v e A f F i g .
1 ,
t h e
e x p o n e n t i a l
weighting
f u n c t i o n
which
a t t a c h e s g r e a t e s t w e i g h t t o
t h e
e a r l i e s t
i n f o r m a t i o n .
F i g ,
2
shows a l s o how
the
angular
v e l o c i t y
02=p01
may
e shown
l e c t r i c a l l y
as w e l l a s me
c h a n i c a l l y . Shaft
I 2
i s p r o l o n g e d
t o
c a r r y brush
3 2
t r a v e r s i n g
l i n e a r
p o t e n t i o m e t e r
3 3
s u p p l i e d
w i t h v o l t a g e f rom b a t t e r y 3 4 , which
may
e i n
cluded i n power
supply 3 0 . Variable
r e s i s t a n c e
3 6 may be a d j u s t e d t o c o n t r o l
t h e
s c a l e
f a c t o r
a t
which
v o l t r n e t e r 3 5 , connected between b rush
3 2 a n d t h e
grounded
end o f potentiometer
3 3 ,
i n
d i c a t e s
a
v o l t a g e p r o p o r t i o n a l t o 0 2 .
A change i n v e l o c i t y o f s h a f t
I 0 o c c u r s
when
t h a t
s h a f t i s f i r s t conn ected with
t h e
apparatus
with which a n observer
i s
tracking a n a i r p l a n e ,
f o r
example,
a n d o t h e r v e l o c i t y changes o c c u r
when
shaft I l l
i s advanced
o r
retarded b y the
observer in correcting for overrun o r
u n d e r r u n
i n h i s o b s e r v a t i o n s .
In
such t r a c k i n g , t h e e a r l i e r
c o r r e c t i o n s a r e
u s u a l l y
l a r g e r
than
t h e l a t e r ,
a n d
the
e a r l i e r o f
t h e
v e l o c i t y
v a r i a t i o n s
av
eraged b y t h e system o f F i g . 1
a r e
g i v e n undue
w e i g h t by
e x p o n e n t i a l
w e i g h t i n g . I t i s
t h e r e
f o r e d e s i r a b l e t o p r o v i d e
a
weighting f u n c t i o n
approximating
the
i d e a l
curve
B f F i g . 1 .
This
i s
done by a n
e l a b o r a t i o n
o f
the
simple
s y s t e m , i n
which
again a r e used the elements
i n c l u d e d
i n dashed
r e c t a n g l e
I o f F i g . 2 .
To
d e r i v e
a
p h y s i c a l l y r e a l i z a b l e
appr o x i ma
t i o n
t o
t h e
p a r a b o l a
o f F i g . 1 ,
c o n s i d e r
t h e i d e a l
i n d i c i a l
admittance
A o < t > and
t h e
correspond
t r a n s f e r
admittance
Y o m ) , where
p i s
t h e d i f
f e r e n t i a l
o p e r a t o r
d
d t
a n d
p“
s
t h e
nth
time
d e r i v a t i v e
ï
d i
I t
may e shown t h a t
d e s i r a b l y
A o ( t ) =6t(1t) f o r t between 0 a n d 1
=0 o r t
<0
or>
1 ,
( 1 )
I 5
where t h e t h e o r e t i c a l r e s p o n s e time o f t h e
me
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2 , 4 7 6 , 2 6 9
c h a n i c a l
c i r c u i t
i s u n i t y . A o ( t ) i s d r awn a s curve
B f F i g .
1 .
The c o r r e s p o n d i n g t r a n s f e r admittance m a y
b e
shown t o b e
g i v e n
by
T he
s p e c i ñ c
e mb o d i me nts shown i n F i g s . 3 a n d
4 c o n s t i t u t e
a p p r o x i m a t i o n s
i n v o l v i n g
t h e
r i g h t
h a n d
m e m b e r o f Equation 2 t o t h e second a n d
t o the fourth power o f p , r e s p e c t i v e l y .
Y 1 ( 1 U ) :ggü 1
P
3 2 2 2 +
1 0
- l - 1 0
which
may
e
written
( 3 )
2 9 .
Y1(P)=
_3 _ _
( 4 )
` 1
-
l
p < p + 5 + â v 5 ) ( p + 5 1 2 J
5 )
where
z ` \ / 1
The c o r r e s p o n d i n g i n d i c i a l a d m i t t a n c e
A 1 ( t )
may
e shown
t o be
s a
40 2-
.
N/ Et
: J n / E e sm ’ à
T h i s i s t h e w e i g h t i n g
f u n c t i o n shown
i n
F i g 1
as c u r ve C.
As another
a p p r o x i m a t i o n ,
l e t
then
1
18 3
_
l
G1=ìña b
_£1 ¿Ddo
t h a t
Y u p )
: i 1 2
p+70
( 6 )
p
4 1 3 + 4 _ 5 _ 0
2 + 2 1 6 0
4 2 0 0
p 4 1 p
41
p 4 1
which may e w r i t t e n
( 7 )
Y2 7 1 ) =
P
4 0 p + 7 0
4 1 ( p 4 - 4 . 2 6 ) @ +3.36 + 1 3 5 7 ) ( p + 3 . 3 c ~ i 3 . 5 7 )
l e a d i n g t o t h e i n d i c i a l a d m i t t a n c e
A z ( t ) ,
p l o t t e d
i n F i g . l as curve
D:
S t a t e d
i n
i t s
most
g e n e r a l f o r m , t h e
r e l a t i o n
s h i p o f
t h e
a n g u l a r d i s p l a c e m e n t 0 2 o f o u t p u t
s h a f t
I 2
t o
0 1 , t h e a n g u l a r d i s p l a c e m e n t o f s h a f t
l l l ,
F i g .
2 , i s 02=Y(p) 0 1 and t h i s i s
a n a l o g o u s
t o
t h e
e l e c t r i c a l c i r c u i t formula I = Y ( p) E , i n which
I i s the
output
current o f
a n
e l e c t r i c a l
network
o f t r a n s f e r admittance Y(p)
a nd
E s the e l e c
tromotive f o r c e impressed a c r o s s the network
i n p u t . By
s u i t a b l e
c h o i c e o f
Y W ) ,
t h e
o u t p u t
1 0
1 5
20
25
30
3 5
40
45
50
5 5
6 0
65
7 0
7 5
6
c u r r e n t may e
m a d e
p r o p o r t i o n a l t o e i t h e r t h e
time
i n t e g r a l o r t h e
time
d e r i v a t i v e o f
t h e
i n
put v o l t a g e ,
a n d
the s a m e
may
be c l o n e i n a
mechanical s y s t e m .
T he
p r e s e n t i n v e n t i o n con
t e m p l a t e s
t h e l a t t e r
n a m e d
r e l a t i o n s h i p between
i n p u t
and
o u t p u t
s h a f t
a n g u l a r
d i s p l a c e m e n t s .
In
t h e s i m p l e d i i f e r e n t i a t o r shown
i n F i g . 2 ,
a n d
the
angular displacement
o f
s h a f t l 2 r e p
r e s e n t s
the
angular v e l o c i t y o f s h a f t
I 0 , ex
p o n e n t i a l l y ave r a g e d .
In
any
c a s e , where
0 2 ( t ) = Y ( p ) . 0 ( t ) , i t may
be
shown t h a t t h e r e s p o n s e
0 2 ( t ) a t time
t i s
g i v e n
b y
t h e e qu a t i o n
z .
c e )
= f _ œ
A c - n 1 o ) d n < 9 1
Where
) 1
i s
time counted
f r o m
the
p a s t
f r o m
the
same
p o i n t
o f r e f e r e n c e
a s t ,
a n d
0100 i s
the
a n g u l a r
v e l o c i t y
(measured c o n t i n u o u s l y a t s u c
c e s s i v e v a l u e s
o f
A )
o f the
s h a f t having t h e a n g u
l a r displacement mt). The age
a t
time t
o f
the me as u re me nt made
a t
time
A
i s written
a s
1 = t > `
a n d
z
.
f _ œ A c - m a m d r
b e c o m e s
L 1 ( 1 ) @ c - f w f ,
where
A ( f ) i s
t h e
w e i g h t f a c t o r
a p p l i e d
t o t h e
data o f age r .
I f
such a
weighting function
as
Ah)
c a n
b e
p r o v i d e d ,
then
0 2 ( t ) = 1
where
_
ó i
i s t h e Weighted average o f
@ . 1 ( Ä )
i s
t h e t r a n s f e r admittance d e t e r m i n i n g t h e f i n a l
v a l u e
o f
6 2 .
Y<p>
i s
t o
be
mechanized.
I t c a n
be
f u r t h e r shown t h a t
t o
be
p r a c t i c a l l y
mechanized
Y(p)
must
be
o f t h e
f o r m
where M(p) a nd
N(p)
a r e
polynomials
i n p
with
c o n s t a n t
r e a l c o e f f i c i e n t s . We h a l l c o n s i d e r
t h e
mechanization o f the c a s e s where N MO)
i s
e i t h e r
one
o r two d e g r e e s higher i n p
than
Mw).
To
p u t
t h e o p e r a t i o n a l e q u a t i o n
i n t o
a
f o r m
s u i t a b l e f o r
mechanization,
i t i s
car
r i e d t h r o u g h t h e f o l l o w i n g t r a n s f o r m a t i o n s , i n
s t e p s a s
f o l l o w s :
w h e r e a=0
i f
N ( p ) l i s o n l y o n e f d e g r e e h i g h e r
i n
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» 7
p
than
Mo».
' r ï f m i s a t most o f
t h e
same de
gree a s Mm). Then
N 0 1 )
P M Q J )
i s expanded i n t o
p a r t i a l
f r a c t i o n s o f which one
i s o f
the
f o r m
N o w ,
l
P
a n d
the
o t h e r s a r e each o f
the f o r m
1
1 1 + @
P
out
i n
common
o a l l t h e s e
t e r m s ,
we have
( 1 0 )
1 1
0 2 : . » 1 1 1 7 - 1 -
1 0 1 - g l a i -
Y »
( p ) l Y . . ( p ) + e t e 1 o 2 ]
I n Equation
1 0 t h e
Y ( p ) ’ s
a r e
each
o f
t h e
f o r m
The
terms
Ym(p),
Y u m ) ,
e t c . , a r e
a l l
o f
the
f o r m
PM@
p )
a n d
s o introduce n o
new roblems
i n the design
now o be
proposed.
When
i = 0
a nd B 1 = 1 a n d t h e
terms i n Ym(p),
e t c . , a r e o m i t t e d , Equation
1 0
r e d u c e s t o t h e
f o r m
@ F m - § 0 2
( 1 0 )
which
i s t h e c a s e o f
the
system
o f F i g . 2 .
The
system
o f
F i g . 3 c o r r e s p o n d s
t o v a l u e s
o f A1 a n d
B1 both
g r e a t e r than
z e r o , s t i l l o m i t t i n g
Ym(p),
e t c . Adding Ym(p) l e a d s t o t h e system
o f
F i g . 4 .
E a c h o f
the
systems o f F i g s . 3 a n d 4 e s t a b l i s h e s
a weighting
function approximating
the i d e a l
p a r a b o l a , c u r v e
B
o f F i g . 1 , and o b v i o u s l y b y
p r o g r e s s i v e l y
i n c r e a s i n g t h e
c o m p l e x i t y
o f
t h e
m e c h a n i s m
the
a p p r o x i m a t i o n
c a n
b e
carried as
far as d e s i r e d .
Mechanization
o f such
a
factor as
P - I - b
o b v i o u s l y i n v o l v e s
the g e n e r a t i o n
o f
0 2 a s the
i n
t e g r a l
o f
6 1 4 - 1 2 0 2 ,
t h a t
i s ,
and
i n
t h e
s y s t e m o f
F i g . 3 s h a f t I 2 , i n s t e a d o f
b e i n g
d i r e c t l y t h e o u t p u t s h a f t o f
d i f f e r e n t i a l
I I
i s t h e r e t o connected
through
a n i n t e r v e n i n g me
c h a n i c a l
i n t e g r a t o r
o f
t h e
g e n e r a l
fo r m i n c l u d e d
i n dashed r e c t a n g l e I o f
F i g .
2 .
10
1 5
20
25
30
35
40
45
5 0
55
6 0
6 5
70
7 5
R e f e r r i n g
now t o
F i g .
3 ,
i n p u t s h a f t
I 0 and
output s h a f t
I 2 c o n t i n u e
t o be
connected by t h e
f e e d b a c k p a t h
( d a s h e d
r e c t a n g l e I ) e n t e r i n g d i f
f e r e n t i a l gear I I . The
d i r e c t
connection f r o m
d i f f e r e n t i a l
gear
I l
t o
output
s h a f t I 2 i s
here i n
t e r r u p t e d t o i n c l u d e, i n dashed
r e c t a n g l e
2 ,
t h e
i n t e r v e n i n g
i n t e g r a t o r
mentioned
i n
t h e
p r e c e d
i n g p a r a g r a p h . O p p o s i t e s h a f t
I l l ,
o u t p u t s h a f t
4 0 l e a d s
t o d i f f e r e n t i a l
gear
4 I
a n d
therethrough
t o s h a f t 4 2
terminating
i n b e v e l g e a r s 4 3 .
Through
g e a r s 4 3 ,
s h a f t 4 2
d r i v e s
s h a f t 4 4
c a r r y
i n g
p i n i o n 4 5
engaged by r a c k 4 6 .
Rack 4 6
c on
t r o l s ,
a s d o e s
rack I 8 ,
an i n t e g r a t i n g
element
g e n e r a l l y
d e s i g n a t e d
a s 5 0
a n d i d e n t i c a l l y
l i k e
elements
CSMI
o 2 2 o f F i g . 2 . Output s h a f t 5 I
o f
i n t e g r a t o r
5 0 d r i v e s , through b e v e l
g e a r s
5 2
and
5 3 , ñnal
o u t p u t s h a f t
I 2 . The last-named
s h a f t
i s provided with
b e v e l g e a r s
I 5 a n d c a r r i e s
p o i n t e r I 3
a s
i n F i g . 2 . The feedback
path
b e
tween
s h a f t s I 2 a nd I 0
i s
i d e n t i c a l
with that i n
F i g .
2 .
On
h a f t
I 2 ,
a t
t h e
end
o p p o s i t e p o i n t e r
I 3 ,
i s
c a r r i e d
spur gear 5 4 meshing with r i n g - gear
5 5 o f
d i f f e r e n t i a l
gear 4 I .
The angular d i s p l a c e
me nt 0 2 o f
s h a f t I 2
i s here
r e l a t e d
t o
t h e
angular
d i s p l a c e m e n t 6 4
o f
s h a f t 4 0 by t h e
r e l a t i o n
1
( 9 a - m 0 4
S i n c e 0 4 i s , a s i n
F i g .
2 f o r 6 2 , e q u a l t o
t h e f i n a l d i s p l a c e m e n t o f
s h a f t
I 2 i n
F i g .
3 i s
1
a
9 2 _ p + b 0 ‘ - P 0 2 )
Exami nat i o n o f the d i ag r am o f F i g . 3 shows that
while the
i n i t i a l
e f f e c t o f the r o t a t i o n 0 4 i s t o
b r i n g about
a
p r o p o r t i o n a l
angular
v e l o c i t y o f
s h a f t 5 I ,
t h e i n c r e a s i n - g displacement H z o f s h a f t
I 2 p r o g r e s s i v e l y c a n c e l s
t h i s
e f f e c t s o that
i n t e
g r a t o r
5 U c e a s e s
t o
o p e r a t e s i m u l t a n e o u s l y with
t h e
co mi ng
t o r e s t o f
s h a f t
I 2 ,
p r o v i d e d
t h e
a n g u
l a r
v e l o c i t y 0 1 i s
s t r i c t l y c o n s t a n t .
When h a f t
I 2
i n
F i g .
3 c omes t o r e s t , i t
may
be shown
t h a t
i t s angular p o s i t i o n 0 2 i s propor
t i o n a l
t o
t h e
angular v e l o c i t y 0 1 o f s h a f t I 0
weighted s u b s t a n t i a l l y i n accordance with c u r v e
C , F i g .
1 . I t
w i l l
be o b s e r v e d t h a t angular p o s i
t i o n
feedback has been introduced
f r o m
shaft
I 2 t o r i n g gear 5 5 ,
i n
a d d i t i o n t o t h e feedback
me
c h a n i c a l
i n t e g r a t i n g
path
f r o m
s h a f t I 2 t o r i n g
gear 2 5 .
The
added p a t h ,
i n c l o s e d i n dashed
o u t l i n e 2 , i s
a n
improvement
p r o v i d e d by t h e
p r e s
ent i n v e n t i o n ; a n a d d i t i o n a l
i m p r oveme nt
i s
shown i n F i g .
4 .
Without d e t a i l i n g t h e n e c e s s a r y
mathematical
a n a l y s i s , i t may be s t a t e d t h a t the appr o x i ma
t i o n
t o the p a r a b o l i c Weighting f u n c t i o n , curve
B f F i g .
l , may e
p r o g r e s s i v e l y improved
b y
a d d i ng
a n y n u m b e r
o f
admittance paths i n par
a l l e l with
the
path between
g e a r s I 5 a n d
i n t e
g r a t o r 9 0 o f F i g . 2 . E a c h o f t h e s e added ad
mittance paths
r e q u i r e s
the
i n t r o d u c t i o n
o f a
d i f f e r e n t i a l gear t o e n a b l e i t s output t o j o i n that
f r o m
g e a r s
I 5
t o
be operated
o n
b y
i n t e g r a t o r
9 0 .
I t w i l l s u i i i c e here t o
i l l u s t r a t e
the
a d d i t i o n
o f
o ne
such admittance.
Referring
now o F i g . 4 , a system providing a
w e i g h t i n g f u n c t i o n s u b s t a n t i a l l y t h a t shown by
c u r v e D , F i g . 1 , the system o f F i g . 3
i s
e l a b o r a t e d
b y adding
a
t h i r d i n t e g r a t o r
i n c l u d e d
i n dashed
r e c t a n g l e
3 . Bevel
g e a r s
6 0 transmit t h e mot i o n
o f s h a f t
I 2
t o a u x i l i a r y
s h a f t
6
I ,
from which
b e v e l
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ö t i i t i i i i ‘ i
N U U W É
2 , 4 2 8 , 2 6 6
g e a r s 6 2 r e d i r e c t t h e motion t o e n t e r d i f f e r e n t i a l
g e a r
6 3 .
The output
s h a f t
6 4
o f gear 6 3
c a r r i e s
b e v e l
g e a r s
6 5 whereby i s d r i v e n
rack
6 8 c o n t r o l
l i n g
t h e i n t e g r a t o r
g e n e r a l l y
d e s i g n a t e d
a s
1 0 .
o f
l i k e fo r m
t o
t h e p r e v i o u s l y d e s c r i b e d i n t e g r a
t o r s
i n
F i g s .
2
and
.
Thr ough
b e v e l g e a r s
‘ I 2
a n d
1 3 , and r i n g g e a r I 4 t h e o u t p u t
o f
i n t e g r a t o r I 0
i n t r o d u c e s i n t o d i f f e r e n t i a l
6 3
a m ot i on propor
t i o n a l
t o
t h e
time i n t e g r a l o f
t h e motion
o f
s h a f t
G 4 a n d i n a
sense adapted t o check
the
m o t i o n
o f
t h e
l a s t
n a m e d s h a f t .
T o ad d the mot i o n
o f
s h a f t 6 4 t o that o f s h a f t
I 6 , d i f f e r e n t i a l 1 5 i s i n t r o d u c e d
between
g e a r s I 5
and p i n i o n
I l
a n d
rack I 8 i s m o v e d f r o m a b o v e ,
a s i n
F i g . 2 ,
t o
below
p i n i o n
I I . Shaft
6 4
i s pro
l o n g e d t o
d r i v e
through b e v e l
g e a r s
1 6 ,
r i n g
g e a r
I l
o f
d i f f e r e n t i a l I 5 i n
t h e
s e n s e
t o
add t h e
m ot i on o f s h a f t 6 4
t o that
o f s h a f t I 6 ,
the
l a t t e r
d r i v e n through
d i f f e r e n t i a l I 5 by s h a f t I 6 .
The
c om b ined m otion o f
s h a f t s 6 4
a n d
I 6 i s then
i n t e g r a t e d
by
i n t e g r a t o r
9 D ,
a s p r e v i o u s l y
d e
s c r i b e d i n
connection with F i g . 2 ,
t o c a n c e l
pro
g r e s s i v e l y t h e motion o f t h e output s h a f t o f d i f
f e r e n t i a l I l .
In
F i g s .
2 , 3 a n d 4 , f u l l l i n e arrows
i n d i c a t e
t h e
ñnal
d i r e c t i o n s
o f
movement
o f
t h e
r a c k s i n
i n
t e g r a t o r s
9 0 ,
5 0
and l 0 , when
s h a f t
I 2 i s moving
f r o m z e r o t o i t s
f i n a l
r e s t
p o s i t i o n ,
a s indicated
b y the
dashed arrows.
The
r a c k s
o f i n t e g r a t o r s 5 0
a n d I 0 i n i t i a l l y
m o v e a s
shown b y the
dashed arrows a n d t h e n ,
a s
s h a f t
I 2
approaches i t s
ñnal p o s i t i o n , r e t u r n
( f u l l
l i n e
a r r o w s )
t o
c e n t e r t h e t r a n s m i t t i n g b a l l s
o n
t h e i r d r i v i n g d i s c s
i f b 1 i s
c o n s t a n t .
The rack
o f i n t e g r a t o r
S 0
moves o n l y a s
shown b y
the f u l l
arrow,
c o m i n g
t o
a
f i n a l p o s i t i o n a s
shaft
I 2
does
s o .
I t w i l l
be noted that the d i r e c t i o n s o f r o t a
t i o n
o f t h e d i s c s d r i v e n by c o n s t a n t speed motors
in
a l l
three integrators
are
the
same.
I t i s t o
b e
un derstood that
t h i s
i s only i l l u s t r a t i v e , a n d ` » t h a t
the mot o r
r o t a t i o n s
may
e
conveniently chosen
i f
regard
i s h a d t o
preserve
the
sense o f
the
shaft
motions a s i n d i c a t e d . Further, a
l i t t l e
consid
e r a t i o n o f
F i g .
4 w i l l show that a s
f o r
i n t e g r a t o r
5 0 i n
F i g .
3 ,
t h e co mi ng
t o r e s t o f
s h a f t I 2 w i l l
b e accompanied by
t h e
c e s s a t i o n o f i n t e g r a t i n g
o p e r a t i o n by b o t h
i n t e g r a t o r s
5 0
and I I I
i f
t h e
m ot i on
0 1 o f s h a f t
I U i s
s t r i c t l y un i f or m with t i m e .
Only i n t e g r a t o r
9 0
w i l l i n t h a t e v e n t c o n t i n u e t o
o p e r a t e
t o m a k e 0 2 = p ü i = 0 1 . S i n c e t h e c o n s t a n t
s p e e d
motors r un
c o n t i n u o u s l y ,
a l l
t r a n s m i t t i n g
b a l l s
c o m e t o c e n t e r when s h a f t
I 0
i s a t r e s t .
The
time
c o n s t a n t o f t h e system i s determined
b y
t h e v a r i o u s g e a r r a t i o s a n d
i n t e g r a t o r
d i me n
s i o n s ,
t o g e t h e r w i t h t h e
s p e e d s
o f t h e c o n s t a n t
s p e e d motors CSMI, CSM2
and
CSM3, a n d
may
b e c h o s e n a t p l e a s u r e
by a d j u s t i n g t h e s e
s p e e d s .
I t i s : t o be understood
t h a t
a l l
t h e c o n s t a n t
s p e e d
motors m a y
b e
s u p p l i e d ,
by means shown
o n l y
f o r
CSMI, f r o m power
s u p p l y
3 0 ,
F i g . 2 .
S i n c e
t h e t i m e c o n s t a n t m a y b e t h u s s i m p l y c o n t r o l l e d ,
i t i s deemed unnecessary herein t o p r e s c r i b e gear
r a t i o s
a n d dimensions
o f p a r t s ; t h e s e may be
chosen a s
seems
convenient t o
the
d e s i g n e r .
A d j a c e n t t h e important
s h a f t s
i n F i g s . 2 , 3 and
4 a r e
i l l u s t r a t e d
t h e i r
r e s p e c t i v e
angular
d i s p l a c e
ments
a s
0 i ,
0 2 ,
e t c . I t may
e p r o f i t a b l e t o
tabu
l a t e
t h e
r e l a t i o n s
o f
t h e s e d i s p l a c e m e n t s
i n t h e
s e v e r a l f i g u r e s ,
s t a t i n g
t h e
c o r r e s p o n d i n g
W e i g h t
i n g f u n c t i o n s .
In F i g .
2 :
a
_
P
.
0 2 - 9 1 - 5 - 9 2 _m 1
w e i g h t i n g
f u n c t i o n
e x p o n e n t i a l ,
c u r v e A
f F i g . 1 .
i 6
I n F i g . 3 2
1
9 = _ _ _ _ . . , 9
’
n + 1 »
‘
:___-___P 0
p2+pb+a ‘
l o w e i g h t i n g
f u n c t i o n
a p p r o x i m a t e l y p a r a b o l i c ,
Equation , c u r v e
C
f F i g . 1 .
In
F i g . 4 :
l
@ g m t
a l
20
2 5 ‘ 0 1 1
w e i g h t i n g f u n c t i o n
a p p r o x i m a t e l y
p a r a b o l i c ,
Equation , curve
D f
F i g .
1 .
In t h e
a b o v e
e x p r e s s i o n s
f o r 0 2 , t h e c o n s t a n t s
a , b
a n d c
r e f e r o f course t o the gear r a t i o s c o n
cerned
i n d r i v i n g t h e r i n g
g e a r s .
O b v i o u s m o d i f i c a t i o n s
i n
t h e g r a d u a t i o n
o f
s c a l e
I 4
and
i n
t h e b a t t e r y c o n n e c t i o n
t o
p o t e n t i o m e t e r
3 3 can be m a d e t o e n a b l e the
system
t o
i n d i c a t e
angular v e l o c i t i e s o f
s h a f t
I I ) i n
t h e
o p p o s i t e
sense to that shown n the
drawin gs .
C a l i b r a t i o n o f
t h e system i s
m a d e b y
i m p o s i n g ,
f r o m
a n y s u i t a b l e source
a
known
constant
a n g u l a r
v e l o c i t y
on
s h a f t
I 0 , t h e t r a n s m i t t i n g
b a l l s
o f
t h e
s e v e r a l
i n t e g r a t o r s
9 0 , 5 D a n d I 0 b e i n g
5 c e n t e r e d o n t h e i r r e s p e c t i v e d r i v i n g d i s c s which
a r e i n r o t a t i o n a t constant
s p e e d .
T he
f i n a l
p o s i
t i o n o f p o i n t e r I 3 ,
a n d
t h e time taken t o reach
t h a t
p o s i t i o n , a r e n o t e d . T he d i s c
speeds
may
e
changed i f t h i s
time
i s t o o
l o n g
o r t o o s h o r t ,
a n d
p r o v i s i o n , not shown, may e m a d e t o gear u p o r
d ow n
the
m o v e me nt o f
p o i n t e r I 3 .
I t
i s
obvious
fr o m
a
c o n s i d e r a t i o n
o f
F i g .
2 ,
f o r
e x a m p l e , t h a t
t h e
h i g h e r
t h e
s p e e d o f d i s c 2 0 ,
t h e
l e s s
t h e
d i s
p l a c e m e n t o f
s h a f t
I
2
f o r a , g i v e n a n g u l a r v e l o c i t y
5 o f
s h a f t I 0 . I f the response time s t o be shortened
a n d
the s c a l e f a c t o r o n s c a l e I 4 i s t o be kept the
same, p o i n t e r I 3 must be geared u p i n the s a m e
r a t i o
a s
t h e d i s c speed i s i n c r e a s e d .
The c h o i c e a m o n g t h e s y s t e m s o f F i g s . 2 , 3
a n d
4
60 i s
t o
be
based o n the
character
o f
the
m ot i on
0 1
o f
s h a f t
I 0 . I f t h i s m ot i on i s uni for m with t i m e ,
t h e
simple
system o f
F i g . 2 w i l l
s e r v e .
I f 0 1
i s
a
m ot i on un i f or m with time
p l u s
r a n d o m i n c r e a s e s
a n d
d e c r e a s e s
i n
v e l o c i t y , t h e system
o f
F i g . 4
5 5 i s p r e f e r r e d
t o
t h a t
o f F i g .
3
u n l e s s
t h e a d d i t i o n a l
me ch a n i s m i s unwelcome. T he apparatus o f F i g .
4 ,
r e a l i z i n g
c u r v e
D
f
F i g .
1 ,
m o r e
c l o s e l y
f o l l o w s
the
parabola B, a n d thus provides a m o r e a c c u
r a t e
r e s u l t
than
d o e s t h e apparatus
o f
F i g .
3
70
which
c o r r e s p o n d s t o c u r v e C .
Moreover,
s i n c e
curve D eaches zero sooner than curve
C ,
the
error due t o the curve
area
b e y o n d
t = 1 i s
l e s s .
I t
w i l l
be u n d e r s t o o d
t h a t
t h e s p e c i f i c i n t e g r a t
i n g
e l e m e n t s shown i n i n t e g r a t o r s 9 0 , 5 0 and 1 0
7 5 a r e i l l u s t r a t i v e o n l y , t h e r e b e i n g numerous me~
30
35
4 0
8/11/2019 Us 2476269
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2 , 4 % , 2 6 9
c h a n i c a l s p e e d changing s y s t e m s
which m a y
b e
u s e d , i n p l a c e o f t h o s e
shown,
t o produce
t h e same
r e s u l t .
In F i g .
2 ,
f o r
e x a m p l e ,
a l l
t h a t i s r e q u i r e d
i s
a means o r
conferring
o n
shaft 23 a n a ngula r
v e l o c i t y p r o p o r t i o n a l
t o
t h e
a n g u l a r
d i s p l a c e m e n t
o f
shaft
I 2 f r o m
,
zero
p o s i t i o n ,
a n d
a n y
means
o r
s o
doing may
e p l a c e
t h a t
shown without
d e p a r t
i n g f r o m the p r e s e n t i n v e n t i o n .
For a
s h a f t
I l l turning
with
a g r a d u a l l y
varying
angular v e l o c i t y , with
o r
without r a n d o m i r r e g u
l a r i t i e s , t h e i n v e n t i o n p r o v i d e s ,
i n
t h e embodi
ments
shown
i n F i g s .
3
a n d
4 , an
angular v e l o c i t y
a v e r a g e d
w i t h s u b s t a n t i a l l y p a r a b o l i c w e i g h t i n g
over a
time
i n t e r v a l o f
s e l e c t a b l e
l e n g t h .
The
s p e e d o f t h e
t i m i n g
d i s c s
i n
t h e i n t e g r a t o r s s h o u l d
be s e t
f o r
a response time
s e v e r a l
times the period
o f
t h e p r i n c i p a l i r r e g u l a r i t i e s . The system
o f
t h e
i n v e n t i o n
then p r o v i d e s
a
run n i n g average
a n g u l a r v e l o c i t y
o f t h e
i n p u t s h a f t ,
smoothing o u t
r a n d o m
f l u c t u a t i o n s .
I
am ware
that
m e c h a n i c a l
d i f f e r e n t i a t i n g
a n d
s m o o t h i n g
n e t w o r k s ,
c o m b i n i n g
d i f f e r e n t i a l
g e a r s
a n d mechanical
i n t e g r a t o r s ,
are k n ow n . I - I o w
e v e r , the d e s i g n herein d i s c l o s e d a n d based u p o n
the
derivation o f E qua t i o n
10 i s
believed t o i n - ~
c l u d e advantages not heretofore r e a l i z e d i n such
mechanisms. These advantages a r e :
1 . The
d e s i g n
i s independent o f t h e n u m b e r o f
r e a l o r conjugate, o r b o th r e a l
a n d conjugate,
complex p a i r s o f e x p o n e n t i a l
f u n c t i o n s
o f t i m e
which
are c o m b i n e d
t o
obtain a
s a t i s f a c t o r y
w e i g h t i n g f u n c t i o n .
2 .
T he n u m b e r
o f p r e c i s i o n
p a r t s
i s
a l s o i n d i .
pendent o f
t h e n u m b e r
o f
e x p o n e n t i a l
f u n c t i o n s .
Since i f t h e angular v e l o c i t y o f s h a f t I 0
i s
ab
s o l u t e l y
c o n s t a n t
a l l
i n t e g r a t o r s
e x c e p t t h a t
g e n e r a l l y
designated
a s 9 0
e v e n t u a l l y
return t o
a
n e u t r a l p o s i t i o n , o n l y i n t e g r a t o r 9 0
needs
t o
b e
o f
high
p r e c i s i o n .
In a d d i t i o n , a l l g e a r s may e o f
low
p r e c i s i o n ,
e x c e p t ,
a s i n F i g . 4 , g e a r s I 5 ,
d i f f e r e n t i a l 1 5 , p i n i o n
I 1
and
r a c k
I 8 , and
p r e c i s e
s p e e d r e g u l a t i o n i s r e q u i r e d o n l y
f o r
motor
CSMI.
What s claimed
s :
1 .
Mechanis m
f o r i n d i c a t i n g t h e
angular
v e
l o c i t y
o f
a f i r s t
r o t a t i n g
s h a f t comprising a second
s h a f t , m e a n s
including
a f i r s t d i f f e r e n t i a l gearing
f o r
d r i v i n g t h e second s h a f t
f r o m
t h e
f i r s t
s h a f t
a n d i n the o p p o s i t e sense o f
r o t a t i o n ,
a
t h i r d s h a f t ,
m e a n s including a sec on d
d i f f e r e n t i a l
gearing
f o r
driving the t h i r d shaft f r o m the
second
shaft
i n
the
sense
o f
rotation
o f
the
f i r s t
s h a f t ,
a fourth
s h a f t ,
me a ns i n c l u d i n g a
mecha ni ca l
i n t e g r a t o r
f o r d r i v i n g
t h e f o u r t h
s h a f t f r o m t h e t h i r d s h a f t
i n the sense
o f
rotation o f
the second
shaft a t a n
a n g u l a r v e l o c i t y
p r o p o r t i o n a l
t o t h e a n g u l a r d i s
p l a c e m e n t
of the
third
shaft,
means for intro
ducing
f r o m the fourth s h a f t t o the t h i r d s h a f t
a n g u l a r
d i s p l a c e m e n t
f e e d b a c k
p r o p o r t i o n a l
t o
a n d i n the s e n s e
o f
the angular di splacement
o f
the fourth s h a f t , m e a n s including a m e c h a n i c a l
i n t e g r a t o r connected between
t h e
fourth s h a f t
a nd t h e ñ r s t d i l f e r e n t i a l g e a r i n g f o r adding t o t h e
angular
v e l o c i t y o f
the second
s h a f t
a n o p p o s i t e
a n g u l a r v e l o c i t y
p r o p o r t i o n a l
t o
t h e
a n g u l a r d i s
placement o f
the
fourth s h a f t , a n d
m e a n s
f o r i n
d i c a t i n g t h e last-named a n g u l a r
d i s p l a c e m e n t .
2 . A
mechanical system
c o n t r o l l e d
b y
the
ro
tation o f
a f i r s t
shaft c o m p r i s i n g a
sec on d
shaft
d r i v e n
through d i f f e r e n t i a l
g e a r i n g
f r o m the
ñ r s t
s h a f t ,
a t h i r d s h a f t driven through
d i f f e r e n t i a l
gearing f r o m the second ` s h a f t , a fourth s h a f t , a
mechanical path i n c l u d i n g i n t e g r a t i n g
means b e
I I )
1 A
2 0
65
N
r
12
tween
t h e t h i r d s h a f t a n d t h e f o u r t h s h a f t , means
f o r i n t r o d u c i n g angular p o s i t i o n f e e d b a c k
f r o m
the fou rth s h a f t
t o
t h e se co nd- name d
d i f f e r e n t i a l
gearing a n d a
mecha ni ca l
feedback
path
including
i n t e g r a t i n g m e a n s
between
the
fou rth shaft a n d
t h e
first-named
d i f f e r e n t i a l
g e a r i n g ,
whereby
r o
t a t i o n o f the f i r s t shaft occasions a n an gular d i s
placement o f
the fou rth
s h a f t
p r o p o r t i o n a l
t o the
angular v e l o c i t y
o f
t h e
f i r s t
s h a f t .
3 . Me c h a n i s m
f o r
i n d i c a t i n g the angular
ve
l o c i t y
o f a
f i r s t
r o t a t i n g
shaft comprising
a
second
s h a f t , me a ns including
a
ñ r s t d i f f e r e n t i a l
gearing
f o r d r i v i n g t h e
second
s h a f t f r o m the f i r s t s h a f t
a n d i n the o p p o s i t e
s e n s e
o f r o t a t i o n , a t h i r d s h a f t ,
m e a n s including
a
second d i f f e r e n t i a l gearing
f o r
d r i v i n g
t h e t h i r d s h a f t f r o m t h e second
s h a f t
i n
the sense o f
r o t a t i o n
o f the
f i r s t
s h a f t , a fourth
s h a f t , me a ns i n c l u d i n g
a mechanical
i n t e g r a t o r
f o r d r i v i n g the
fourth
s h a f t f r o m
the t h i r d
s h a f t
i n
the sense o f rotation o f the sec on d shaft a t
a n
angular
v e l o c i t y
p r o p o r t i o n a l
t o
t h e
angular
d i s
placement o f
the
t h i r d s h a f t , m e a n s f o r introduc
i n g f r o m the
fourth shaft
t o the
t h i r d shaft
a n g u
l a r displacement feedback
p r o p o r t i o n a l
t o
a n d i n
t h e
s e n s e o f the
angular displacement
o f the
fourth
s h a f t , a f i f t h
s h a f t , m e a n s
including
a
t h i r d d i f f e r e n t i a l g e a r i n g f o r d r i v i n g t h e ñfth
s h a f t
f r o m the
fourth
s h a f t
i n the o p p o s i t e
s e n s e
o f
r o t a t i o n , means including a
mechanical
i n
t e g r a t o r
connected
between the f i f t h s h a f t a n d
t h e t h i r d d i f f e r e n t i a l gearing f o r adding
t o
the
m o ti o n
o f the f i f t h
shaft
a n angular
v e l o c i t y
p r o p o r t i o n a l a n d opposed
t o
t h e
a n g u l a r d i s p l a c e
m e n t
o f
the f i f t h s h a f t , a s i x t h s h a f t , m e a n s
i n
c l u d i n g a fourth
d i f f e r e n t i a l
gearing f o r impart
ing
t o
the
s i x t h
shaft
a n
angular displacement
p r o p o r t i o n a l
t o
t h e
s u m o f
the
angular d i s p l a c e
ments o f
the
fourth
a n d f i f t h s h a f t s , m e a n s
i n
cluding
a
mechanical
i n t e g r a t o r connected
be
tween
the sixth shaft
and
the f i r s t
d i f f e r e n t i a l
g e a r i n g f o r adding
t o
the
angular v e l o c i t y o f
t h e
second s h a f t a n o p p o s i t e angular v e l o c i t y
pro
p o r t i o n a l t o
t h e
angular displacement o f
t h e
s i x t h s h a f t , a n d me a ns
f o r i n d i c a t i n g t h e
angular
displacement
o f t h e f o u r t h
s h a f t .
4 .
A echanical system a s i n c laim 2 i n c l u d i n g ,
i n
a d d i t i o n ,
a
f i f t h s h a f t d r i v e n
through
d i f f e r e n
t i a l
gearing
f r o m
the fourth
s h a f t , a mechanical
feedback path
i n c l u d i n g i n t e g r a t i n g
means
b e
tween the
f i f t h
s h a f t a n d the last-named d i f f e r e n
t i a l gearing
a n d m e a n s
f o r a d d i n g
the m o t i o n
o f
the
f i f t h
shaft t o
that
o f
the fourth s h a f t i n the
feedback path between
the fourth
shaft a n d
the
f i r s t - n a m e d d i f f e r e n t i a l
g e a r i n g .
RALPH
B.
BLACKMAN.
REFERENCES CITED
The
following references are
o f record i n
the
f i l e o f t h i s p a t e n t :
UNITED
STATES PATENTS
N u m b e r
Name Date
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28,
19 3 7
2,089,878
Corbin ___________
_
Aug. 1 0 ,
1 9 3 7
2 , 136 , 213 Hodgman
________
_ Nov. ,
1938
2 , 206 ,875
Chaffee ___________
_
Ju ly 9 , 19 4 0
2 , 2 48, 072 Fry _______________
__ Jul y
8 , 1 9 4 1
2,377,898 Myers
___________
_
June 1 2 , 1 9 4 5
2 , 4 2 6 , 584 Baker ____________ __ SeptA 2 , 19 4 7
2 , 4 3 3 , 0 0 6 Weiss ____________
_ Dec .
23,
19 4 7
2 , 4 4 2 , 792
White
____________
_
June ,
1948