Stress area: 1473.19 mm² · Proof load: 854,450 N · Clamp load (75%): 640,838 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 6152.0 | 4537.5 | 54449.8 | 62733.2 |
| Oiled | 0.15 | 4614.0 | 3403.1 | 40837.4 | 47049.9 |
| Zinc Plated | 0.18 | 5536.8 | 4083.7 | 49004.8 | 56459.9 |
| Waxed | 0.1 | 3076.0 | 2268.7 | 27224.9 | 31366.6 |
| MoS₂ | 0.12 | 3691.2 | 2722.5 | 32669.9 | 37639.9 |
| Galvanized | 0.25 | 7690.1 | 5671.9 | 68063.2 | 78417.5 |
Stress area: 1602.9 mm² · Proof load: 929,682 N · Clamp load (75%): 697,262 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 6693.7 | 4937.0 | 59244.3 | 68257.0 |
| Oiled | 0.15 | 5020.3 | 3702.8 | 44433.4 | 51193.0 |
| Zinc Plated | 0.18 | 6024.3 | 4443.3 | 53319.6 | 61431.0 |
| Waxed | 0.1 | 3346.9 | 2468.5 | 29622.6 | 34129.0 |
| MoS₂ | 0.12 | 4016.2 | 2962.2 | 35546.4 | 40954.0 |
| Galvanized | 0.25 | 8367.1 | 6171.3 | 74055.1 | 85321.0 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 580 MPa × 1473.19 mm² = 640,838 N
Step 2 — Torque (dry): T = 0.20 × 0.0480 m × 640,838 N = 6152.0 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