Stress area: 560.59 mm² · Proof load: 126,133 N · Clamp load (75%): 94,600 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 567.6 | 418.6 | 5023.7 | 5787.9 |
| Oiled | 0.15 | 425.7 | 314.0 | 3767.8 | 4340.9 |
| Zinc Plated | 0.18 | 510.8 | 376.7 | 4521.0 | 5208.7 |
| Waxed | 0.1 | 283.8 | 209.3 | 2511.8 | 2894.0 |
| MoS₂ | 0.12 | 340.6 | 251.2 | 3014.6 | 3473.2 |
| Galvanized | 0.25 | 709.5 | 523.3 | 6279.6 | 7234.9 |
Stress area: 621.2 mm² · Proof load: 139,770 N · Clamp load (75%): 104,828 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 629.0 | 463.9 | 5567.1 | 6414.0 |
| Oiled | 0.15 | 471.7 | 347.9 | 4174.9 | 4810.0 |
| Zinc Plated | 0.18 | 566.1 | 417.5 | 5010.4 | 5772.6 |
| Waxed | 0.1 | 314.5 | 232.0 | 2783.6 | 3207.0 |
| MoS₂ | 0.12 | 377.4 | 278.4 | 3340.3 | 3848.4 |
| Galvanized | 0.25 | 786.2 | 579.9 | 6958.5 | 8017.0 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 225 MPa × 560.59 mm² = 94,600 N
Step 2 — Torque (dry): T = 0.20 × 0.0300 m × 94,600 N = 567.6 N·m
Proof stress per ISO 898-1:2013 Table 4. Stress area per ISO 898-1 Annex A. K-factor per VDI 2230.
Non-critical assemblies, light-duty applications, general-purpose hardware where high strength is not required