heddichead
Mechanical
- Feb 5, 2015
- 11
thread404-332009
Hello all,
This might be the unsolved problem in the industry.
Came across the problem of solving the stresses in the winch drum subjected to multi-layers of wire rope. I am using FEA to model the scenario and requires the compression pressure when it is subjected to wire rope tension at different layers.
I have read a lot of materials and forum and the radial pressure on the core is based very simple equation P=2T/Dd. "T" is line tension, "D" is the diameter of the drum and "d" is the wire rope diameter. The equation is layer sensitive; the next successive layer would change the diameter of the drum core by D'=D+2d. In other words, laying a layer of wire rope of diameter "d" on the nude drum core of diameter "D" would increase the second layer pressure to P'=2T/[(D+2d)d]. And so on, the model is therefore iterative in nature.
The textbook Design of Weldment by Omer W Blodgett suggests to consider summation of compression pressure in the outer 2 layers using the formula above.
The stresses is very high in FEA and by hand calculations (thin wall theory). Any one knows any other way to approximate the compression pressure......
Many thnksssssssssssss
Hello all,
This might be the unsolved problem in the industry.
Came across the problem of solving the stresses in the winch drum subjected to multi-layers of wire rope. I am using FEA to model the scenario and requires the compression pressure when it is subjected to wire rope tension at different layers.
I have read a lot of materials and forum and the radial pressure on the core is based very simple equation P=2T/Dd. "T" is line tension, "D" is the diameter of the drum and "d" is the wire rope diameter. The equation is layer sensitive; the next successive layer would change the diameter of the drum core by D'=D+2d. In other words, laying a layer of wire rope of diameter "d" on the nude drum core of diameter "D" would increase the second layer pressure to P'=2T/[(D+2d)d]. And so on, the model is therefore iterative in nature.
The textbook Design of Weldment by Omer W Blodgett suggests to consider summation of compression pressure in the outer 2 layers using the formula above.
The stresses is very high in FEA and by hand calculations (thin wall theory). Any one knows any other way to approximate the compression pressure......
Many thnksssssssssssss