Stress area: 1473.19 mm² · Proof load: 331,468 N · Clamp load (75%): 248,601 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 2386.6 | 1760.3 | 21123.2 | 24336.6 |
| Oiled | 0.15 | 1789.9 | 1320.2 | 15842.0 | 18252.0 |
| Zinc Plated | 0.18 | 2147.9 | 1584.2 | 19010.5 | 21902.6 |
| Waxed | 0.1 | 1193.3 | 880.1 | 10561.6 | 12168.3 |
| MoS₂ | 0.12 | 1431.9 | 1056.1 | 12673.4 | 14601.4 |
| Galvanized | 0.25 | 2983.2 | 2200.3 | 26403.6 | 30420.3 |
Stress area: 1602.9 mm² · Proof load: 360,652 N · Clamp load (75%): 270,489 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 2596.7 | 1915.2 | 22982.7 | 26479.1 |
| Oiled | 0.15 | 1947.5 | 1436.4 | 17236.8 | 19859.0 |
| Zinc Plated | 0.18 | 2337.0 | 1723.7 | 20684.2 | 23830.9 |
| Waxed | 0.1 | 1298.3 | 957.6 | 11490.9 | 13239.0 |
| MoS₂ | 0.12 | 1558.0 | 1149.1 | 13789.5 | 15887.2 |
| Galvanized | 0.25 | 3245.9 | 2394.1 | 28728.6 | 33099.1 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 225 MPa × 1473.19 mm² = 248,601 N
Step 2 — Torque (dry): T = 0.20 × 0.0480 m × 248,601 N = 2386.6 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