Vectors and determining plate thickness

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SUMMARY

The discussion centers on the calculation of plate thickness for lifting lugs in a concrete tunnel, specifically using a 5-tonne RUD lug for load testing as per AS4991 standards. The user, Harvez, calculated the load in the direction of pull to be 455kN and derived a required plate thickness greater than 82mm based on the formula t > √[(4xM*x10^6)/(øxfyxb)]. However, the accuracy of the method and the appropriateness of designing for a 5-tonne load while only testing to 3 tonnes were questioned. The importance of matching lug geometry to shackle design to avoid bending stress was also emphasized.

PREREQUISITES
  • Understanding of AS4991 load testing standards
  • Knowledge of structural engineering principles, specifically regarding load calculations
  • Familiarity with lifting lug and shackle design
  • Proficiency in using formulas for calculating plate thickness and load distribution
NEXT STEPS
  • Review AS4991 standards for load testing requirements
  • Study the principles of load distribution in lifting applications
  • Learn about the geometry of lifting lugs and shackles to prevent bending stress
  • Investigate advanced methods for calculating plate thickness in structural applications
USEFUL FOR

Structural engineers, lifting equipment designers, and safety compliance professionals involved in load testing and lifting operations will benefit from this discussion.

harvez_007
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Hi,

I have two 1.5 lifting lugs supported in the roof of a concrete tunnel 3.5m apart at a height of 7m.

The lugs require load testing and as per AS4991 require load testing to double the W.L.L therefore 3 tonne.

My work has a 5 tonne RUD lug readily available therefore was thinking of using that, however the plate to mount the lug on is required.

I have designed the plate for the 5 tonne - 5 x 1.5 (strength) x 1.5 (dynamic) x 9.81 = 111kN

The angle the 5 tonne lug will be at is 75.9 degrees.

Therefore the load in the direction of pull will be 111kN / cos75.9 = 455kN ? I am not sure if this is correct.

M* = N* x l (I have assumed a plate 400mm x 400mm - therefore lever arm = 0.2m)
= 455kN x 0.2
= 91kN.m


øMs = øfy x [b(t^2)]/4

Let M* = øMs

t > √[(4xM*x10^6)/(øxfyxb)]

∴t > 82mm

Due to the large thickness I am getting I am not sure if the process I am using is correct. I do understand I am only load testing to 3 tonne however designing for 5 tonne - is this OK? I am happy to increase the size of the plate however could someone please ensure I am using the correct method for calculating this.

Any help is appreciated in advance.

Regards,
Harvez
 

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Designing lifting lugs is a little more complicated than scribbling a few formulas down on a piece of paper and plugging numbers into them.

The geometry of the lug must match the design of the shackles being used, in order to put the shackle pins in bearing stress only and not bending stress. You also have no overall sketch showing the load to be lifted, its weight and center of gravity, the location of the lugs, a calculation showing the expected forces in the shackles, etc.

My advice: Start over and proceed in a more systematic fashion.
 

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