CUSTOMER
SHALL MAINTAIN
The perpendicularity of the mounting surface with respect to the shaft
is not to exceed .005" T.I.R. at a diameter equal to the bolt
circle. Initial air gap setting of .005" - .020". Concentricity
between the clutch mounting pilot diameter and the shaft not to exceed
.004" T.I.R. |
|
| Mechanical |
| MODEL
NO. |
STATIC
TORQUE
LB. - IN. |
INERTIA
LB. - IN. |
WEIGHT
OZ. |
| ROTOR |
ARM
& HUB |
| FO08 |
2.5 |
.0019 |
.0011 |
2 |
| FO11 |
6 |
.005 |
.0024 |
3.2 |
| FO15 |
10 |
.0054 |
.026 |
3.8 |
| FO17 |
15 |
.059 |
.031 |
11 |
| FO19 |
25 |
.080 |
.042 |
12 |
| FO22 |
50 |
.210 |
.070 |
20 |
| FO26 |
80 |
.451 |
.320 |
28 |
| FO30 |
125 |
.610 |
.561 |
40 |
| FO42 |
250 |
2.50 |
2.30 |
75 |
| TOP
OF PAGE |
|
| Electrical |
| MODEL
NO. |
90
V.D.C. |
24
V.D.C. |
12
V.D.C |
| AMPS |
OHMS |
AMPS |
OHMS |
AMPS |
OHMS |
| FO08 |
.046 |
1977 |
.117 |
205 |
.246 |
48.8 |
| FO11 |
.047 |
1930 |
.198 |
121 |
.447 |
26.8 |
| FO15 |
.042 |
2150 |
.183 |
132 |
.380 |
31.6 |
| FO17 |
.066 |
1369 |
.289 |
83 |
.561 |
21.4 |
| FO19 |
.074 |
1213 |
.294 |
81.6 |
.574 |
20.9 |
| FO22 |
.079 |
1140 |
.322 |
74.6 |
.628 |
19.1 |
| FO26 |
.092 |
980 |
.374 |
64.2 |
.760 |
15.8 |
| FO30 |
.091 |
988 |
.378 |
65.3 |
.729 |
16.5 |
| FO42 |
.124 |
722 |
.468 |
51.2 |
.934 |
12.84 |
Lead
wire is U.L. recognized style 1213, 1015 or 1430, 22 gage.
Insulation is .050" O.D. on 08, 11, 15 units; .064" or .095"
O.D. on all other units. |
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OF PAGE |
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|
|
|
|
| Dimensions |
MODEL
NO. |
A
MAX. |
B
NOM. |
C
NOM. |
D
NOM. |
E
MAX. |
F
NOM.
|
G
MAX. |
H
± .005 |
I
± .005 |
J
MAX. |
K
± .001 |
L
± .001
|
M
NOM. |
N
MIN. |
O
± .500 |
ROTOR
KEYWAY |
P
NOM.
|
Q
MAX. |
R
MAX. |
| BORE |
NOMINAL
KEYWAY |
| X |
Y |
| FO08 |
.882 |
.693 |
.641 |
.582 |
.905 |
1/8
3/16
1/4 |
.034 |
.020 |
.188 |
.980 |
1.1995 |
N.A. |
1.030 |
.094 |
12.00 |
N.A. |
ONE
ROLL PIN PILOT HOLE |
.070 |
.500 |
.237 |
| FO11 |
1.012 |
.772 |
.691 |
.616 |
1.160 |
3/16
1/4
5/16 |
.048 |
.020 |
.188 |
1.230 |
1.498 |
N.A. |
1.312 |
.123 |
12.00 |
N.A. |
ONE
ROLL PIN PILOT HOLE |
.093 |
.687 |
.307 |
| FO15 |
1.302 |
.972 |
.865 |
.800 |
1.500 |
1/4
5/16
3/8 |
.063 |
.100 |
.130 |
1.567 |
1.999 |
N.A. |
1.750 |
.156 |
12.00 |
N.A. |
ONE
ROLL PIN PILOT HOLE |
.125 |
.965 |
.475 |
| FO17 |
1.348 |
1.051 |
.925 |
.800 |
1.780 |
1/4
5/16
3/8 |
.064 |
.100 |
.130 |
1.943 |
2.436 |
.750 |
2.125 |
.186 |
12.00 |
1/4
5/16
3/8 |
.0625
- .0655
.0625 - .0655
.094 - .097 |
.285
- .290
.347 - .352
.417 - .427 |
.115 |
1.19 |
.45 |
| FO19 |
1.330 |
1.029 |
.901 |
.781 |
2.000 |
5/16
3/8
1/2 |
.062 |
.100 |
.130 |
1.943 |
2.436 |
.750 |
2.125 |
.186 |
12.00 |
5/16
3/8
1/2 |
.0625
- .0655
.094 - .097
ROLL PIN HOLE |
.347
- .352
.417 - .427
ROLL PIN HOLE |
.115 |
1.19 |
.455 |
| FO22 |
1.757 |
1.325 |
1.173 |
1.023 |
2.260 |
3/8
1/2 |
.096 |
.100 |
.188 |
2.322 |
2.873 |
1.001 |
2.500 |
.160 |
18.00 |
3/8
1/2 |
.094
- .097
.125 - .128 |
.417
- .427
.560 - .567 |
.115 |
1.005 |
.510 |
| FO26 |
1.813 |
1.460 |
1.300 |
1.150 |
2.645 |
3/8
1/2
5/8 |
.064 |
.375 |
.172 |
2.630 |
3.499 |
1.062 |
3.125 |
.182 |
18.00 |
3/8
1/2
5/8 |
.094
- .097
.125 - .128
.1885 - .1905 |
.417
- .427
.560 - .567
.709 - .716 |
.150 |
1.44 |
.610 |
| FO30 |
1.900 |
1.580 |
1.310 |
1.160 |
3.268 |
1/2
5/8
3/4 |
.097 |
.147 |
.310 |
3.200 |
4.186 |
1.751 |
3.750 |
.182 |
SCREW
TER-
MINALS |
1/2
5/8
3/4 |
.125
- .128
.1885 - .1905
.1885 - .1905 |
.560
- .567
.709 - .716
.836 - .844 |
.150 |
1.825 |
.680 |
| FO42 |
2.280 |
1.760 |
1.490 |
1.345 |
4.270 |
1/2
5/8
3/4
7/8
1 |
.097 |
.190 |
.250 |
4.255 |
5.624 |
1.875 |
5.000 |
.276 |
SCREW
TER-
MINALS |
1/2
5/8
3/4
7/8
1 |
.125
- .128
.1885 - .1905
.1885 - .1905
.1885 - .1905
.251 - .253 |
.560
- .567
.709 - .716
.836 - .844
.962 - .970
1.113 - 1.121 |
.250 |
2.195 |
.890 |
| TOP
OF PAGE |
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Notes:
- 08,
11 and 15 units have one roll pin pilot hole in rotor no
set screws.
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OF PAGE |
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