
Allowable Load of Output Shaft
Radial Load Direction (P) | Thrust Load Directions (A, B) | ||||||||||||||||||||
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| LR/2 |
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| Unit: N (1kgf = 9.8N) | ||||
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Motor |
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| When Assembled | In Operation | ||||||||||||
| Motor Output |
| Radial Load | Thrust Load | Radial Load |
| Thrust Load | ||||||||||||||
Series |
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| Direction A | Direction B | Directions A, B | ||||||||||||||
MUMA |
| 50W, 100W |
| 147 | 88.2 |
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| 117.6 |
| 68.6 |
| 58.8 | |||||||||
| 200W, 400W |
| 392 | 147 |
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| 196 |
| 245 |
| 98 | ||||||||||
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<Remarks>
If a position of load point varies, calculate allowable radial load P (N) from distance L (mm) of a load point from mounting flange face, based on the relational expression, so that the result of calculation will be as follows:
L
P
Motor | Motor Output | Relational Expression | ||||
Series | of Load - Load Point | |||||
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| 1406 |
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| 50W, 100W | P = |
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| L + 7.5 | |||||
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| 2940 |
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MUMA | 200W | P = |
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L – 3 | ||||||
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| 5831 |
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| 400W | P = |
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| L + 8.8 | |||||
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196