Stress area: 1120.9 mm² · Proof load: 347,479 N · Clamp load (75%): 260,609 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 2189.1 | 1614.6 | 19375.2 | 22322.7 |
| Oiled | 0.15 | 1641.8 | 1210.9 | 14531.2 | 16741.8 |
| Zinc Plated | 0.18 | 1970.2 | 1453.1 | 17437.7 | 20090.5 |
| Waxed | 0.1 | 1094.6 | 807.3 | 9688.0 | 11161.9 |
| MoS₂ | 0.12 | 1313.5 | 968.8 | 11625.5 | 13394.0 |
| Galvanized | 0.25 | 2736.4 | 2018.3 | 24219.2 | 27903.6 |
Stress area: 1205.7 mm² · Proof load: 373,767 N · Clamp load (75%): 280,325 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 2354.7 | 1736.7 | 20840.9 | 24011.3 |
| Oiled | 0.15 | 1766.0 | 1302.5 | 15630.4 | 18008.3 |
| Zinc Plated | 0.18 | 2119.3 | 1563.1 | 18757.4 | 21610.9 |
| Waxed | 0.1 | 1177.4 | 868.4 | 10420.9 | 12006.2 |
| MoS₂ | 0.12 | 1412.8 | 1042.0 | 12504.3 | 14406.6 |
| Galvanized | 0.25 | 2943.4 | 2170.9 | 26051.3 | 30014.4 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 310 MPa × 1120.9 mm² = 260,609 N
Step 2 — Torque (dry): T = 0.20 × 0.0420 m × 260,609 N = 2189.1 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