Stress area: 693.55 mm² · Proof load: 156,049 N · Clamp load (75%): 117,037 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 772.4 | 569.7 | 6836.3 | 7876.3 |
| Oiled | 0.15 | 579.3 | 427.3 | 5127.2 | 5907.2 |
| Zinc Plated | 0.18 | 695.2 | 512.8 | 6153.0 | 7089.1 |
| Waxed | 0.1 | 386.2 | 284.8 | 3418.2 | 3938.2 |
| MoS₂ | 0.12 | 463.5 | 341.9 | 4102.3 | 4726.4 |
| Galvanized | 0.25 | 965.6 | 712.2 | 8546.3 | 9846.4 |
Stress area: 760.85 mm² · Proof load: 171,191 N · Clamp load (75%): 128,393 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 847.4 | 625.0 | 7500.1 | 8641.1 |
| Oiled | 0.15 | 635.5 | 468.7 | 5624.7 | 6480.3 |
| Zinc Plated | 0.18 | 762.7 | 562.5 | 6750.5 | 7777.4 |
| Waxed | 0.1 | 423.7 | 312.5 | 3750.1 | 4320.6 |
| MoS₂ | 0.12 | 508.4 | 375.0 | 4499.7 | 5184.3 |
| Galvanized | 0.25 | 1059.2 | 781.2 | 9374.7 | 10800.9 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 225 MPa × 693.55 mm² = 117,037 N
Step 2 — Torque (dry): T = 0.20 × 0.0330 m × 117,037 N = 772.4 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