Stress area: 2030.0 mm² · Proof load: 456,750 N · Clamp load (75%): 342,562 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 3836.7 | 2829.8 | 33957.7 | 39123.6 |
| Oiled | 0.15 | 2877.5 | 2122.3 | 25468.0 | 29342.4 |
| Zinc Plated | 0.18 | 3453.0 | 2546.8 | 30561.6 | 35210.9 |
| Waxed | 0.1 | 1918.4 | 1414.9 | 16979.3 | 19562.3 |
| MoS₂ | 0.12 | 2302.0 | 1697.9 | 20374.4 | 23474.0 |
| Galvanized | 0.25 | 4795.9 | 3537.3 | 42447.3 | 48904.8 |
Stress area: 2120.0 mm² · Proof load: 477,000 N · Clamp load (75%): 357,750 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 4006.8 | 2955.3 | 35463.2 | 40858.1 |
| Oiled | 0.15 | 3005.1 | 2216.4 | 26597.4 | 30643.6 |
| Zinc Plated | 0.18 | 3606.1 | 2659.7 | 31916.7 | 36772.1 |
| Waxed | 0.1 | 2003.4 | 1477.6 | 17731.6 | 20429.1 |
| MoS₂ | 0.12 | 2404.1 | 1773.2 | 21278.1 | 24515.1 |
| Galvanized | 0.25 | 5008.5 | 3694.1 | 44329.0 | 51072.7 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 225 MPa × 2030.0 mm² = 342,562 N
Step 2 — Torque (dry): T = 0.20 × 0.0560 m × 342,562 N = 3836.7 N·m
Proof stress per ISO 898-1:2013 Table 4. Stress area per ISO 898-1 Annex A. K-factor per VDI 2230.
Non-critical assemblies, light-duty applications, general-purpose hardware where high strength is not required