Stress area: 1120.9 mm² · Proof load: 252,203 N · Clamp load (75%): 189,152 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 1588.9 | 1171.9 | 14063.0 | 16202.3 |
| Oiled | 0.15 | 1191.7 | 879.0 | 10547.4 | 12152.0 |
| Zinc Plated | 0.18 | 1430.0 | 1054.7 | 12656.6 | 14582.0 |
| Waxed | 0.1 | 794.4 | 585.9 | 7031.0 | 8100.7 |
| MoS₂ | 0.12 | 953.3 | 703.1 | 8437.4 | 9721.0 |
| Galvanized | 0.25 | 1986.1 | 1464.9 | 17578.5 | 20252.7 |
Stress area: 1205.7 mm² · Proof load: 271,282 N · Clamp load (75%): 203,462 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 1709.1 | 1260.6 | 15126.8 | 17428.0 |
| Oiled | 0.15 | 1281.8 | 945.4 | 11344.9 | 13070.8 |
| Zinc Plated | 0.18 | 1538.2 | 1134.5 | 13614.2 | 15685.3 |
| Waxed | 0.1 | 854.5 | 630.2 | 7563.0 | 8713.5 |
| MoS₂ | 0.12 | 1025.4 | 756.3 | 9075.6 | 10456.2 |
| Galvanized | 0.25 | 2136.3 | 1575.7 | 18907.9 | 21784.3 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 225 MPa × 1120.9 mm² = 189,152 N
Step 2 — Torque (dry): T = 0.20 × 0.0420 m × 189,152 N = 1588.9 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