. .
Dyadic Systems – Mechatronics Cylinder Manual
MF
-005500-EN-5/63
1. Summary
The Mechatronics Cylinder consists of a rotary-linear motion transfer mechanism, a stepper motor, an
encoder, and a servo controller. Manufactured by Dyadic Systems, this product can be a replacement for
pneumatic cylinders. Motion is programmed and controlled using Dyadic’s simple interfaces, allowing for a wide
variety of inputs and inter-operability.
1.1. Features
1.1.1 Overcoming weaknesses of Pneumatic Cylinders
(1)
Simplifying wiring and related equipment.
(2) Multiple positioning: Easy program for up to 16 motions per axis
(3) Programmable Push Force
M
O
D
E L
S C L T 4 - 0 1 5
S C L T 4 - 0 3 0
S C L T 6 - 0 2 5
S C L T 6 - 0 5 0
- X X X A S
- X X X A S
- X X X A B
- X X X A B
A m p l i f i e r
B u i l t - i n t o a c t u a t o r
E x t e r n a l
S t r o k e ( m m )
5 0 / 1 0 0 / 1 5 0 / 2 0 0 / 3 0 0 / 4 0 0 / 5 0 0
5 0 / 1 0 0 / 1 5 0 / 2 0 0 / 3 0 0 / 4 0 0 / 5 0 0 / 6 0 0 / 7 0 0
M a x . T h r u s t ( N ) / ( k g f )
1 5 0 / 1 5
3 0 0 / 3 0
2 5 0 / 2 5
5 0 0 / 5 0
M a x . c a r r i a b l e w t a t p w r O N ( k g )
1 . 5
2 . 5
4
6
P u s h m o d e m a x . T h r u s t ( N ) / ( k g f )
1 0 5 / 1 0 . 5
2 1 0 / 2 1
1 7 5 / 1 7 . 5
3 5 0 / 3 5
B a l l s c r e w l e a d ( m m )
1 2
6
1 2
6
M a x . S p e e d ( m m / s ) * n o t e 1
7 0 0 ( 6 8 0 m m / s f o r
4 0 0 ( 3 4 0 m m / s f o r
6 0 0 ( 5 0 0 m m / s f o r
3 5 0 ( 6 0 0 m m : 3 4 0 m m / s )
5 0 0 m m s t r o k e )
5 0 0 m m s t r o k e )
f o r 7 0 0 m m
s t r o k e )
( 7 0 0 m m : 2 5 0 m m / s )
R e p e a t a b i l i t y ( m m )
±
0 . 0 2
±
0 . 0 2
±
0 . 2
±
0 . 2
B a c k l a s h ( m m )
0 . 1
0 . 1
0 . 1
0 . 1
M a x . H o r L o a d w e i g h t ( k g )
5
1 0
1 6
3 0
M a x . v e r t i c a l l o a d ( k g )
1 . 5
2 . 5
4
6
L o a d m
o m e n t ( N m / k g f - c m
) * 2
M p = 1 2 / 1 2 0 , M y = 1 2 / 1 2 0 , M r = 3 1 / 3 1 0
M p = 2 5 . 7 / 2 5 7 , M y = 2 5 . 7 / 2 5 7 , M r = 5 8 / 5 8 0
P r o g r a m
C a p a c i t y
1 6 P o s i t i o n s
P o w e r S u p p l y
D C 2 4 V
±
1 0 %
( D r i v e P o w e r m
a x . 2 . 0 A m
p s , C o n t r o l p o w e r m a x . 0 . 2 A )
L i f e
3 y e a r s a f t e r d e l i v e r y , o r 1 0 , 0 0 0 k m o p e r a t i o n w h e n u s e d w i t h i n a l l s p e c s .
P a r a l l e l
D C 2 4 V t y p e D i g i t a l I n p u t I n t e r f a c e
I n p u t
N a m e s
P o s i t i o n s e l e c t b i t s ( 4 b i t b i n a r y c o d e d d e c i m a l : P C 1 , P C 2 , P C 4 , P C 8 )
S t a r t ( C S T R ) , M o v e m
e n t I n t e r l o c k ( I L K )
I n p u t c u r r e n t
M a x . 4 m
A / p o r t , P N P S t a n d a r d
M a x . 4 m A / p o r t , P N P S t a n d a r d
I / O
P a r a l l e l
D C 2 4 V t y p e D i g i t a l O u t p u t I n t e r f a c e
O u t p u t
N a m e s
C o m p l e t e d P o s i t i o n N u m
b e r ( 4 b i t b i n a r y : P M 1 , P M 2 , P M 4 , P M 8 ) : ( S C L T 6 O n l y )
H o m e d s i g n a l ( Z F I N ) , Z o n e s i g n a l ( Z O N E ) , A l a r m ( A L M ) , P o s i t i o n c o m p l e t e ( P F I N / I N P )
O u t p u t c u r r e n t
M a x . 1 0 m A / p o r t , P N P S t a n d a r d
M a x . 1 0 m
A / p o r t , P N P S t a n d a r d
S e r i a l S i g n a l
S e r i a l I n t e r f a c e ( C o n n e c t o r S I O )
+ 5 V , 0 V , S + , S - , A S C I I P r o t o c o l F r e e l y A v a i l a b l e
P r o t e c t i o n f u n c t i o n
O v e r s p e e d , M a i n p o w e r o v e r v o l t a g e , a b n o r m a l v o l t a g e ,
O v e r l o a d , S e n s o r a b n o r m
a l , S e r v o a b n o r m a l , E n c o d e r w i r e d i s c o n n e c t e d
A m b i e n c e
O p e r a t e T e m
p e r a t u r e
0 ~ 4 0 ° C
S t o r a g e T e m p e r a t u r e
- 2 0 ~ 6 0 ° C
O p e / S t o r a g e H u m i d i t y
= < 9 0 %
R H , n o n - c o n d e n s i n g
W
e i g h t ( k g s )
1 . 4 2 / 1 . 5 3 / 1 . 6 4 / 1 . 7 4 / 1 . 9 6 / 2 . 1 8 / 2 . 4
2 . 7 / 2 . 9 / 3 . 1 / 3 . 3 / 3 . 7 / 4 . 1 / 4 . 5 / 5 . 0 / 5 . 4
N o t e s : ( * 1 ) T y p i c a l d a t a , ( * 2 ) T h i s i s a l o a d t h a t t h e w t ( m k g ) i s g e n e r a t e d b y t h e o v e r h a n g ( L m ) f r o m t h e a r r i o r s l i d e r .
( T h e c a l c u l a t i o n o f t h e l o a d m o e m e n t ( k g f - c m ) i s : m ( k g ) x L ( c m ) < M p , M y , M r )
T h e a c t u a l m o m e n t w i l l b e c o m b i n a t i o n s o f t h o s e m o m e n t s ( M p , P y , M r ) .
Acceleration
Deceleration
Programmed
Speed
Stop
condition
Speed
Time
Acceleration
Deceleration
Work
Programmed
Speed
Acceleration
Deceleration
Stop
Po
si
tion
Push
Movement
Speed
Stop
condition
Time
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