Stress area: 192.47 mm² · Proof load: 43,306 N · Clamp load (75%): 32,479 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 116.9 | 86.2 | 1034.7 | 1192.1 |
| Oiled | 0.15 | 87.7 | 64.7 | 776.2 | 894.3 |
| Zinc Plated | 0.18 | 105.2 | 77.6 | 931.1 | 1072.7 |
| Waxed | 0.1 | 58.5 | 43.1 | 517.8 | 596.5 |
| MoS₂ | 0.12 | 70.2 | 51.8 | 621.3 | 715.8 |
| Galvanized | 0.25 | 146.2 | 107.8 | 1294.0 | 1490.8 |
Stress area: 216.23 mm² · Proof load: 48,652 N · Clamp load (75%): 36,489 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 131.4 | 96.9 | 1163.0 | 1339.9 |
| Oiled | 0.15 | 98.5 | 72.6 | 871.8 | 1004.4 |
| Zinc Plated | 0.18 | 118.2 | 87.2 | 1046.2 | 1205.3 |
| Waxed | 0.1 | 65.7 | 48.5 | 581.5 | 670.0 |
| MoS₂ | 0.12 | 78.8 | 58.1 | 697.4 | 803.5 |
| Galvanized | 0.25 | 164.2 | 121.1 | 1453.3 | 1674.4 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 225 MPa × 192.47 mm² = 32,479 N
Step 2 — Torque (dry): T = 0.20 × 0.0180 m × 32,479 N = 116.9 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