YASKAWA SGMCS, Product Manual

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7.2 Specifications and Ratings
7.2.6 Medium-Capacity Servomotors, with Cores: Ratings
7-11
7
Specifications, Ratings, and Exter
nal Dimensions of SGMCS Servomotors
7.2.6 Medium-Capacity Servomotors, with Cores: Ratings
*1.
These values are for operation in combination with a SERVOPACK when the temperature of the armature wind-
ing is 20
°
C. These are typical values.
*2.
The rated torques are the continuous allowable torque values at a surrounding air temperature of 40
°
C with a
steel heat sink of the dimensions given in the table.
*3.
The thrust loads and moment loads that are applied while a Servomotor is operating are roughly classified into
the following patterns. Design the machine so that the thrust loads or moment loads will not exceed the values
given in the table.
Note: For the bearings used in these Servomotors, the loss depends on the bearing temperature. The amount of
heat loss is higher at low temperatures.
Voltage 200 V
Model SGMCS- 45M 80M 1AM 80N 1EN 2ZN
Rated Output
*1
W 707 1260 1730 1260 2360 3140
Rated Torque
*1, *2
N

m 45.0 80.0 110 80.0 150 200
Instantaneous Maximum Torque
*1
N

m 135 240 330 240 450 600
Stall Torque
*1
N

m 45.0 80.0 110 80.0 150 200
Rated Current
*1
Arms 5.8 9.7 13.4 9.4 17.4 18.9
Instantaneous Maximum Current
*1
Arms 17.0 28.0 42.0 28.0 56.0 56.0
Rated Motor Speed
*1
min
-1
150 150
Maximum Motor Speed
*1
min
-1
300 300 250
Torque Constant N

m/Arms 8.39 8.91 8.45 9.08 9.05 11.5
Motor Moment of Inertia
×
10
-4
kg

m
2
388 627 865 1360 2470 3060
Rated Power Rate
*1
kW/s 52.2 102 140 47.1 91.1 131
Rated Angular Acceleration Rate
*1
rad/s
2
1160 1280 1270 588 607 654
Heat Sink Size mm 750
×
750
×
45
Allowable Load Moment of Inertia
(Motor Moment of Inertia Ratio)
3 times
With External Regenerative Resistor and
Dynamic Brake Resistor
3 times
Allowable
Load
*3
A mm 33 37.5
Allowable Thrust Load N 9000 16000
Allowable Moment Load N

m 180 350
F F
L
F
L
Where F is the external force,
Thrust load = F + Load mass
Moment load = 0 Where F is the external force,
Thrust load = F + Load mass
Moment load = F × L Where F is the external force,
Thrust load = Load mass
Moment load = F × (L + A)
A (Refer to the
values in the
table.)