KEVOS® MAKEOS · Strength
Lifting Lug Design (Plate, Pin and Bearing Checks)
Is this pinned lifting lug strong enough for the sling load: net tension, tear-out, bearing and pin shear?
Check of a plate lifting lug with a pin or shackle: the load per sling leg from the total load, number of legs, sling angle and a dynamic factor, net-section tension across the hole, shear tear-out beyond the hole, bearing of the pin on the plate, double-shear stress in the pin (as the bolt and pin shear tool), utilisation of each against your allowables and the hole clearance.
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How this tool works
Inputs, units and where to find them
| Input | Unit | Typical source |
|---|---|---|
| Total load lifted | kN | Total weight of the load (as force). |
| Sling legs sharing the load | Number of sling legs that share the load (use fewer if the slings may not share evenly). | |
| Sling angle from vertical | ° | Angle of each sling leg from vertical. |
| Dynamic factor | Factor for snatch and acceleration during the lift (your value from the lifting code). | |
| Lug plate thickness | mm | Thickness of the lug plate at the hole. |
| Distance from hole centre to the plate edge (in the load direction) | mm | Distance from the hole centre to the plate edge in the direction of the pull (the edge radius for a round-ended lug). |
| Hole diameter | mm | Diameter of the pin hole. |
| Pin diameter | mm | Diameter of the pin or shackle pin. |
| Allowable tensile stress | MPa | Allowable tensile stress of the plate (your design value). |
| Allowable shear stress (plate) | MPa | Allowable shear stress of the plate. |
| Allowable bearing stress | MPa | Allowable bearing stress between pin and plate. |
| Allowable shear stress (pin) | MPa | Allowable shear stress of the pin. |
| Largest hole clearance | mm | Largest clearance you accept between hole and pin (larger clearance concentrates bearing stress). |
Method and formulas
- Load per lug F = W × dynamic factor ÷ (legs × cos θ).
- Net tension σ = F ÷ [(2R − d_h) t]; tear-out τ = F ÷ [2 t (R − d_h ÷ 2)].
- Bearing σ_b = F ÷ (d_p t); pin in double shear τ_p = F ÷ (2 × π d_p² ÷ 4).
- Example: 200 kN on 2 legs at 30° puts 144.34 kN on each lug; the highest utilisation is 80.188%.
Limitations
- Simplified lug checks; lifting codes add out-of-plane loads, cheek plates and weld checks.
- The lug weld to the structure needs its own check.
- Example values are illustrations. Replace them with values for your actual task.
Typical uses
- Check a lifting lug on a fabricated frame
- Size a padeye for a new lift
- Review a lug when sling angles change
Who it is for
- Structural engineers
- Rigging supervisors
- Fabrication supervisors
What you get
- Design load per lug
- Net tension, tear-out and bearing stresses
- Pin shear and utilisations
Interpreting the result
- Tear-out usually governs short lugs: increase the edge distance before the plate thickness.
References
- Machinery’s Handbook, 29th edition (Industrial Press, 2012), printed pp. 1535, 1720–1735. Topic reference; no source tables or recommended settings are reproduced.
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Open the Lifting Lug Design (Plate, Pin and Bearing Checks) calculator