Stress area: 1757.73 mm² · Proof load: 395,489 N · Clamp load (75%): 296,617 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 3084.8 | 2275.2 | 27302.8 | 31456.3 |
| Oiled | 0.15 | 2313.6 | 1706.4 | 20477.1 | 23592.2 |
| Zinc Plated | 0.18 | 2776.3 | 2047.7 | 24572.3 | 28310.5 |
| Waxed | 0.1 | 1542.4 | 1137.6 | 13651.4 | 15728.2 |
| MoS₂ | 0.12 | 1850.9 | 1365.2 | 16381.9 | 18874.0 |
| Galvanized | 0.25 | 3856.0 | 2844.0 | 34128.5 | 39320.4 |
Stress area: 1828.6 mm² · Proof load: 411,435 N · Clamp load (75%): 308,576 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 3209.2 | 2367.0 | 28403.8 | 32724.9 |
| Oiled | 0.15 | 2406.9 | 1775.2 | 21302.9 | 24543.6 |
| Zinc Plated | 0.18 | 2888.3 | 2130.3 | 25563.6 | 29452.6 |
| Waxed | 0.1 | 1604.6 | 1183.5 | 14201.9 | 16362.4 |
| MoS₂ | 0.12 | 1925.5 | 1420.2 | 17042.1 | 19634.7 |
| Galvanized | 0.25 | 4011.5 | 2958.7 | 35504.8 | 40906.1 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 225 MPa × 1757.73 mm² = 296,617 N
Step 2 — Torque (dry): T = 0.20 × 0.0520 m × 296,617 N = 3084.8 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