CBernard
Mechanical
- Sep 12, 2017
- 2
I'm designing a tower 74" ID and 71' 3" S/S. I'm trying to use the rigging analysis "tail lug" attach feature, and using my clients standard tail lug detail. I'm getting failure and the error "The load ratio for the EN13445 calculation exceeds 1.Lift load 122,627 lbf exceeds maximum allowable load 26,701 lbf." for EN as well as WRC 537 "The local stresses in the WRC 537 calculation are excessive."
The lug design calls for the lug to be between the bottom and upper base rings, with continuous welds along the shell, upper base ring, and lower base ring. Based on the diagram in compress, it looks like there is only a continuous weld on the component you are attaching to (in this case the base ring).
My question is there any way to account for the actual strength of this situation in Compress, and not just the worst case localized to the base ring? I can of course run an FEA, but was hoping to keep it in the compress model.
Any help is appreciated.
Thanks,
The lug design calls for the lug to be between the bottom and upper base rings, with continuous welds along the shell, upper base ring, and lower base ring. Based on the diagram in compress, it looks like there is only a continuous weld on the component you are attaching to (in this case the base ring).
My question is there any way to account for the actual strength of this situation in Compress, and not just the worst case localized to the base ring? I can of course run an FEA, but was hoping to keep it in the compress model.
Any help is appreciated.
Thanks,