Stress area: 115.44 mm² · Proof load: 25,974 N · Clamp load (75%): 19,480 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 54.5 | 40.2 | 482.4 | 555.7 |
| Oiled | 0.15 | 40.9 | 30.2 | 362.0 | 417.1 |
| Zinc Plated | 0.18 | 49.1 | 36.2 | 434.6 | 500.7 |
| Waxed | 0.1 | 27.3 | 20.1 | 241.6 | 278.4 |
| MoS₂ | 0.12 | 32.7 | 24.1 | 289.4 | 333.4 |
| Galvanized | 0.25 | 68.2 | 50.3 | 603.6 | 695.4 |
Stress area: 124.55 mm² · Proof load: 28,024 N · Clamp load (75%): 21,018 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 58.8 | 43.4 | 520.4 | 599.6 |
| Oiled | 0.15 | 44.1 | 32.5 | 390.3 | 449.7 |
| Zinc Plated | 0.18 | 53.0 | 39.1 | 469.1 | 540.5 |
| Waxed | 0.1 | 29.4 | 21.7 | 260.2 | 299.8 |
| MoS₂ | 0.12 | 35.3 | 26.0 | 312.4 | 360.0 |
| Galvanized | 0.25 | 73.6 | 54.3 | 651.4 | 750.5 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 225 MPa × 115.44 mm² = 19,480 N
Step 2 — Torque (dry): T = 0.20 × 0.0140 m × 19,480 N = 54.5 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