Stress area: 976.0 mm² · Proof load: 219,600 N · Clamp load (75%): 164,700 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 1284.7 | 947.5 | 11370.6 | 13100.3 |
| Oiled | 0.15 | 963.5 | 710.6 | 8527.7 | 9825.0 |
| Zinc Plated | 0.18 | 1156.2 | 852.8 | 10233.2 | 11790.0 |
| Waxed | 0.1 | 642.3 | 473.7 | 5684.8 | 6549.7 |
| MoS₂ | 0.12 | 770.8 | 568.5 | 6822.2 | 7860.0 |
| Galvanized | 0.25 | 1605.8 | 1184.4 | 14212.5 | 16374.7 |
Stress area: 1028.4 mm² · Proof load: 231,390 N · Clamp load (75%): 173,543 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 1353.6 | 998.4 | 11980.4 | 13802.9 |
| Oiled | 0.15 | 1015.2 | 748.8 | 8985.3 | 10352.2 |
| Zinc Plated | 0.18 | 1218.3 | 898.6 | 10782.9 | 12423.2 |
| Waxed | 0.1 | 676.8 | 499.2 | 5990.2 | 6901.5 |
| MoS₂ | 0.12 | 812.2 | 599.0 | 7188.6 | 8282.2 |
| Galvanized | 0.25 | 1692.0 | 1248.0 | 14975.5 | 17253.7 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 225 MPa × 976.0 mm² = 164,700 N
Step 2 — Torque (dry): T = 0.20 × 0.0390 m × 164,700 N = 1284.7 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