Stress area: 2030.0 mm² · Proof load: 1,177,400 N · Clamp load (75%): 883,050 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 9890.2 | 7294.6 | 87535.7 | 100852.3 |
| Oiled | 0.15 | 7417.6 | 5470.9 | 65651.3 | 75638.8 |
| Zinc Plated | 0.18 | 8901.1 | 6565.1 | 78781.4 | 90766.3 |
| Waxed | 0.1 | 4945.1 | 3647.3 | 43767.8 | 50426.2 |
| MoS₂ | 0.12 | 5934.1 | 4376.8 | 52521.2 | 60511.2 |
| Galvanized | 0.25 | 12362.7 | 9118.3 | 109419.2 | 126064.9 |
Stress area: 2120.0 mm² · Proof load: 1,229,600 N · Clamp load (75%): 922,200 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 10328.6 | 7618.0 | 91415.9 | 105322.8 |
| Oiled | 0.15 | 7746.5 | 5713.5 | 68562.3 | 78992.6 |
| Zinc Plated | 0.18 | 9295.8 | 6856.2 | 82274.8 | 94791.1 |
| Waxed | 0.1 | 5164.3 | 3809.0 | 45707.9 | 52661.4 |
| MoS₂ | 0.12 | 6197.2 | 4570.8 | 54849.9 | 63194.1 |
| Galvanized | 0.25 | 12910.8 | 9522.5 | 114270.3 | 131654.0 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 580 MPa × 2030.0 mm² = 883,050 N
Step 2 — Torque (dry): T = 0.20 × 0.0560 m × 883,050 N = 9890.2 N·m
Proof stress per ISO 898-1:2013 Table 4. Stress area per ISO 898-1 Annex A. K-factor per VDI 2230.
Automotive engines, structural connections, high-strength machinery, flanged joints — the most common high-strength grade