Stress area: 5.03 mm² · Proof load: 1,559 N · Clamp load (75%): 1,169 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 0.7 | 0.5 | 6.2 | 7.1 |
| Oiled | 0.15 | 0.5 | 0.4 | 4.4 | 5.1 |
| Zinc Plated | 0.18 | 0.6 | 0.4 | 5.3 | 6.1 |
| Waxed | 0.1 | 0.4 | 0.3 | 3.5 | 4.1 |
| MoS₂ | 0.12 | 0.4 | 0.3 | 3.5 | 4.1 |
| Galvanized | 0.25 | 0.9 | 0.7 | 8.0 | 9.2 |
Stress area: 5.61 mm² · Proof load: 1,739 N · Clamp load (75%): 1,304 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 0.8 | 0.6 | 7.1 | 8.2 |
| Oiled | 0.15 | 0.6 | 0.4 | 5.3 | 6.1 |
| Zinc Plated | 0.18 | 0.7 | 0.5 | 6.2 | 7.1 |
| Waxed | 0.1 | 0.4 | 0.3 | 3.5 | 4.1 |
| MoS₂ | 0.12 | 0.5 | 0.4 | 4.4 | 5.1 |
| Galvanized | 0.25 | 1.0 | 0.7 | 8.9 | 10.2 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 310 MPa × 5.03 mm² = 1,169 N
Step 2 — Torque (dry): T = 0.20 × 0.0030 m × 1,169 N = 0.7 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