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• Convert Matrix to Metric Information
Part No.
Thru Bore
|
D |
L |
E |
F |
G |
Clamp
|
Set |
Inch
+.000
-.010 |
Inch
±.015 |
Inch
±.005
Note
2 |
Inch
±.015 |
Inch
±.005 |
(screw) Inch
(torque) LB.IN.
Note
4 |
| FTOOO075 |
.745 |
1.00 |
.190 |
.550 |
.230 |
(18)
|
2-56
18 |
FTOOO100
FTSOO100 |
.995
.995 |
1.25
1.10 |
.230
.230 |
.550
.500 |
.230
.230 |
(18)
|
6-32
34 |
FTOOO125
FTSOO125 |
1.240
1.240 |
1.25
1.10 |
.290
.290 |
.550
.500 |
.230
.230 |
(18)
|
6-32
34 |
| FTOOO150 |
1.485 |
1.25 |
.375 |
.500 |
.230 |
(41)
|
8-32
59 |
Part No.
Thru Bore
|
A Shaft |
B Bore |
Static Torque |
Torsional Stiffness |
Inertia |
Mass |
Misalignment
(see definitions) |
MM
+.025
-.000
Notes
1,2,3 |
Inch
+.001
-.000
Notes
1,2,3 |
MM
+.025
-.000
Notes
1,2,3 |
Inch
+.001
-.000
Notes
1,2,3 |
LB.IN
Note
6 |
MIN /
LB.IN
Note
7 |
10-3
Ib.in.2
Note
9 |
Ib.
Note
9 |
Angular
Offset Degrees |
Parallel
Off Set
Inch
|
Axial
Motion
Inch |
| FTOOO075 |
5 |
0.187 |
5 |
0.187 |
|
|
|
|
5° |
0.015 |
±.015 |
| 6 |
0.250 |
6 |
0.250 |
|
|
|
|
| 8 |
0.312 |
8 |
0.312 |
28 |
8.5 |
2.179 |
0.025 |
FTOOO100
FTSOO100 |
5 |
0.187 |
5 |
0.187 |
|
|
|
|
5° |
0.025
0.020 |
±.020
±.020 |
| 6 |
0.250 |
6 |
0.250 |
|
|
|
|
| 8 |
0.312 |
8 |
0.312 |
42 |
6.8 |
9.927 |
0.066 |
| 10 |
0.375 |
10 |
0.375 |
|
|
|
|
| 12 |
0.437 |
12 |
0.437 |
|
|
|
|
FTOOO125
FTSOO125 |
6 |
0.250 |
6 |
0.250 |
|
|
|
|
5° |
0.030
0.025 |
±.025
±.025 |
| 8 |
0.312 |
8 |
0.312 |
|
|
|
|
| 10 |
0.375 |
10 |
0.375 |
63 |
3.00 |
24.26 |
0.102 |
| 12 |
0.437 |
12 |
0.437 |
|
|
|
|
| 14 |
0.500 |
14 |
0.500 |
|
|
|
|
| FTOOO150 |
8 |
0.312 |
8 |
0.312 |
|
|
|
|
5° |
0.030 |
±.030 |
| 10 |
0.375 |
10 |
0.375 |
|
|
|
|
| 12 |
0.437 |
12 |
0.437 |
70 |
1.33 |
50.08 |
0.142 |
| 14 |
0.500 |
14 |
0.500 |
|
|
|
|
| 16 |
0.625 |
16 |
0.625 |
|
|
|
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|
• Convert Matrix to Imperial Measurement
Part No.
Thru Bore
|
D |
L |
E |
F |
Clamp
|
Set |
MM
+.00
-.025 |
MM
±..38 |
MM
±.13
Note
2 |
MM
±.38 |
(screw) MM
(torque) Nm
Note
4 |
| FTOOM075 |
19.00 |
25.40 |
4.80 |
8.90 |
M2X.4
2.1
|
(3.84) |
FTOOM100
FTSOM100 |
25.00
25.00 |
31.75
27.90 |
5.80
5.50 |
8.90 8.90
|
M3X.5
2.1
|
(3.84) |
FTOOM125
FTSOM125 |
31.50
31.50 |
31.75
27.90 |
7.36
7.36 |
8.90 8.90 |
M3X.5
2.1
|
(3.84) |
| FTOOM150 |
37.60 |
31.75 |
9.50 |
8.90 |
M4X.7
4.6
|
(6.60) |
Part No.
Thru Bore
|
A Shaft |
B Bore |
Static Torque |
Torsional Stiffness |
Inertia |
Mass |
Misalignment
(see definitions) |
Inch
+.001
-.000
Notes
1,2,3 |
MM
+.025
-.000
Notes
1,2,3 |
Inch
+.001
-.000
Notes
1,2,3 |
MM
+.025
-.000
Notes
1,2,3 |
Nm
Note
6 |
MIN /
Nm
Note
7 |
10-3
kgm2
Note
9 |
kg
Note
9 |
Angular
Offset Degrees |
Parallel
Off Set
MM
|
Axial
Motion
MM |
| FTOOM075 |
0.187 |
5 |
0.187 |
5 |
|
|
|
|
5° |
0.38 |
±.38 |
| 0.250 |
6 |
0.250 |
6 |
|
|
|
|
| 0.312 |
8 |
0.312 |
8 |
3.16 |
0.96 |
0.0006 |
0.012 |
FTOOM100
FTSOM100 |
0.187 |
5 |
0.187 |
5 |
|
|
|
|
5° |
0.63
0.51 |
±.51
±.51 |
| 0.250 |
6 |
0.250 |
6 |
|
|
|
|
| 0.312 |
8 |
0.312 |
8 |
4.75 |
0.77 |
0.0029 |
0.030 |
| 0.375 |
10 |
0.375 |
10 |
|
|
|
|
| 0.437 |
12 |
0.437 |
12 |
|
|
|
|
FTOOM125
FTSOM125 |
0.250 |
6 |
0.250 |
6 |
|
|
|
|
5° |
0.76
0.63 |
±.63
±.63 |
| 0.312 |
8 |
0.312 |
8 |
|
|
|
|
| 0.375 |
10 |
0.375 |
10 |
7.12 |
0.34 |
0.0071 |
0.046 |
| 0.437 |
12 |
0.437 |
12 |
|
|
|
|
| 0.500 |
14 |
0.500 |
14 |
|
|
|
|
| FTOOM150 |
0.312 |
8 |
0.312 |
8 |
|
|
|
|
5° |
0.76 |
±.76 |
| 0.375 |
10 |
0.375 |
10 |
|
|
|
|
| 0.437 |
12 |
0.437 |
12 |
7.90 |
0.15 |
0.0147 |
0.065 |
| 0.500 |
14 |
0.500 |
14 |
|
|
|
|
| 0.625 |
16 |
0.625 |
16 |
|
|
|
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- All E and F couplings have an inside relief so the shafts will not touch the beams at the maximum misalignment ratings.
- Clamps are an integral part of the coupling and cannot be removed.
- All screws are hex socket, steel with black oxide finish. For stainless steel screws.
- Screw torques are the screw manufacturer’s maximum ratings.
- Coupling material is 2024-T3.51. QQA225/6 aluminum with MIL-A8625 Type II black anodize.
- Static torque is the maximum coupling torque rating.
- Torque and torsional stiffness rating are at a maximum misalignment, not in a straight line.
- The expanding shaft torque holding force is dependent on the pilot hole finish and the expander screw’s tightness.
- Mass and inertia are calculated without the G10 insert.
- E & F have thru bores only.
- TEST BEFORE YOU BUY. Rocom will furnish samples at no charge for all new OEM designs or for comparative evaluation.
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