Stress area: 459.41 mm² · Proof load: 142,417 N · Clamp load (75%): 106,813 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 576.8 | 425.4 | 5105.1 | 5881.7 |
| Oiled | 0.15 | 432.6 | 319.1 | 3828.8 | 4411.3 |
| Zinc Plated | 0.18 | 519.1 | 382.9 | 4594.4 | 5293.4 |
| Waxed | 0.1 | 288.4 | 212.7 | 2552.6 | 2940.9 |
| MoS₂ | 0.12 | 346.1 | 255.3 | 3063.2 | 3529.3 |
| Galvanized | 0.25 | 721.0 | 531.8 | 6381.4 | 7352.2 |
Stress area: 496.18 mm² · Proof load: 153,816 N · Clamp load (75%): 115,362 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 623.0 | 459.5 | 5514.0 | 6352.9 |
| Oiled | 0.15 | 467.2 | 344.6 | 4135.1 | 4764.1 |
| Zinc Plated | 0.18 | 560.7 | 413.6 | 4962.6 | 5717.6 |
| Waxed | 0.1 | 311.5 | 229.8 | 2757.0 | 3176.4 |
| MoS₂ | 0.12 | 373.8 | 275.7 | 3308.4 | 3811.7 |
| Galvanized | 0.25 | 778.7 | 574.3 | 6892.1 | 7940.6 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 310 MPa × 459.41 mm² = 106,813 N
Step 2 — Torque (dry): T = 0.20 × 0.0270 m × 106,813 N = 576.8 N·m
Proof stress per ISO 898-1:2013 Table 4. Stress area per ISO 898-1 Annex A. K-factor per VDI 2230.
Light structural connections, furniture assembly, non-load-bearing joints