Stress area: 459.41 mm² · Proof load: 103,367 N · Clamp load (75%): 77,525 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 418.6 | 308.7 | 3704.9 | 4268.5 |
| Oiled | 0.15 | 314.0 | 231.6 | 2779.1 | 3201.9 |
| Zinc Plated | 0.18 | 376.8 | 277.9 | 3335.0 | 3842.3 |
| Waxed | 0.1 | 209.3 | 154.4 | 1852.5 | 2134.3 |
| MoS₂ | 0.12 | 251.2 | 185.3 | 2223.3 | 2561.5 |
| Galvanized | 0.25 | 523.3 | 386.0 | 4631.6 | 5336.2 |
Stress area: 496.18 mm² · Proof load: 111,640 N · Clamp load (75%): 83,730 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 452.1 | 333.5 | 4001.4 | 4610.2 |
| Oiled | 0.15 | 339.1 | 250.1 | 3001.3 | 3457.9 |
| Zinc Plated | 0.18 | 406.9 | 300.1 | 3601.4 | 4149.2 |
| Waxed | 0.1 | 226.1 | 166.8 | 2001.2 | 2305.6 |
| MoS₂ | 0.12 | 271.3 | 200.1 | 2401.2 | 2766.5 |
| Galvanized | 0.25 | 565.2 | 416.9 | 5002.4 | 5763.5 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 225 MPa × 459.41 mm² = 77,525 N
Step 2 — Torque (dry): T = 0.20 × 0.0270 m × 77,525 N = 418.6 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