d3con
Mechanical
- Jun 14, 2014
- 1
Hello everyone,
I would like to verify a few calculations I was doing to estimate the safety factor with a lifting plate. The plate is essentially 5.5" wide x 0.5" thick x 30" long with a square hole (located 1.25" from the 5.5" wide face) that measures 3" wide, 2" long with 3/8" fillets. This plate is being used to carry 5000 lbs (carried by a 2.25" x 1" pin in the hole, the other end of this plate is part of a piece of equipment) and I would like to estimate the safety factor (60 ksi yield strength steel).
I did a quick simulation in solidworks and the plate appeared to be fine with a maximum stress of 19 ksi. When performing hand calculations, I could not find a stress concentration factor for a square hole and so I treated bottom most portion (5.5" x 1.25") as a beam fixed at both ends with a 5000 lbs distributed load. I then applied the resultant moments and shear force onto the two short vertical side members, if I add the axial stress with the bending stress that the inside face of the hole would experience, then it looks like the member will yield.
What would be the method of analysis (hand calculation wise) you guys would use to check its load capacity? Realistically I would expect this to be primarily a axial load issue, but I am wondering how to take into account the stress concentrations of the corners of the hole.
Thanks,
I would like to verify a few calculations I was doing to estimate the safety factor with a lifting plate. The plate is essentially 5.5" wide x 0.5" thick x 30" long with a square hole (located 1.25" from the 5.5" wide face) that measures 3" wide, 2" long with 3/8" fillets. This plate is being used to carry 5000 lbs (carried by a 2.25" x 1" pin in the hole, the other end of this plate is part of a piece of equipment) and I would like to estimate the safety factor (60 ksi yield strength steel).
I did a quick simulation in solidworks and the plate appeared to be fine with a maximum stress of 19 ksi. When performing hand calculations, I could not find a stress concentration factor for a square hole and so I treated bottom most portion (5.5" x 1.25") as a beam fixed at both ends with a 5000 lbs distributed load. I then applied the resultant moments and shear force onto the two short vertical side members, if I add the axial stress with the bending stress that the inside face of the hole would experience, then it looks like the member will yield.
What would be the method of analysis (hand calculation wise) you guys would use to check its load capacity? Realistically I would expect this to be primarily a axial load issue, but I am wondering how to take into account the stress concentrations of the corners of the hole.
Thanks,