Stress area: 20.12 mm² · Proof load: 4,527 N · Clamp load (75%): 3,395 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 4.1 | 3.0 | 36.3 | 41.8 |
| Oiled | 0.15 | 3.1 | 2.3 | 27.4 | 31.6 |
| Zinc Plated | 0.18 | 3.7 | 2.7 | 32.7 | 37.7 |
| Waxed | 0.1 | 2.0 | 1.5 | 17.7 | 20.4 |
| MoS₂ | 0.12 | 2.4 | 1.8 | 21.2 | 24.5 |
| Galvanized | 0.25 | 5.1 | 3.8 | 45.1 | 52.0 |
Stress area: 22.03 mm² · Proof load: 4,957 N · Clamp load (75%): 3,718 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 4.5 | 3.3 | 39.8 | 45.9 |
| Oiled | 0.15 | 3.3 | 2.4 | 29.2 | 33.7 |
| Zinc Plated | 0.18 | 4.0 | 3.0 | 35.4 | 40.8 |
| Waxed | 0.1 | 2.2 | 1.6 | 19.5 | 22.4 |
| MoS₂ | 0.12 | 2.7 | 2.0 | 23.9 | 27.5 |
| Galvanized | 0.25 | 5.6 | 4.1 | 49.6 | 57.1 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 225 MPa × 20.12 mm² = 3,395 N
Step 2 — Torque (dry): T = 0.20 × 0.0060 m × 3,395 N = 4.1 N·m
Proof stress per ISO 898-1:2013 Table 4. Stress area per ISO 898-1 Annex A. K-factor per VDI 2230.
Non-critical assemblies, light-duty applications, general-purpose hardware where high strength is not required