gvc99
Mechanical
- Nov 3, 2002
- 16
I'm re-evaluating two pressure vessels with swing bolt closures (pairs of parallel lugs welded equally spaced around the circumference of the vessel flange and closure head flange, hinge pins through the vessel lugs capturing swing bolts which swing up between the corresponding closure head lugs and are capped by washers and hexnuts bearing on the top surfaces of the upper lugs). The vessels are designed to Section VIII Division 1 of the B&PVC.
The vessels have been fabricated by a subsidiary, who neglected to calculate the bending stresses in the hinge pins due to the swing bolt loads. The vessels have been tested, stamped, and delivered to the customer.
I have used our company's evaluation method for hinge pin bending, which assumes that the pins are simply supported beams with a span equal to the width of the distance between the inside faces of the lugs, and loaded with a uniformly distributed load over the width of the swing bolt head -
|.|.|.|.|.|.|
....VVVVVVVV....
===========
^--------------^
Using this approach, the bending stress in the pin, 63000 psi, is over the allowable stress for the pin material, 25000 psi(SA193B7).
I've looked at two alternative loadings - point loading at the edges of the swing bolt head
|............|
V...........V
==========
^--------------^
and a "v-shaped distributed load" over the width of the bolt head -
......|..........|
......||.......||
......|||....|||
......VVVVVV
==========
^..................^
Using the company's evaluation method as a reference,
the alternative methods give bending stresses that are 55%
and 24% of the reference stress, respectively.
Only the point load case stress, 15000 psi, will meet code requirements.
The actual loading on pin probably falls somewhere between the extremes of the cases that I've evaluated. I recognize that using the point load case less conservative, but is it non-conservative? I don't believe there is a cut and dried answer.
Also, since the pins are made of a material normally used for bolting, should the more conservative factors of safety that form the basis for the allowable stress be used, or could a argument be made for using a higher allowable?
My recollection is that the design basis for the higher factors of safety on bolting materials is that they are heat treated to achieve their properties, and thus have yield and ultimate strengths fairly close together, which indicates that they may not be as ductile as materials used for shell and head construction.
I greatly appreciate any insights into this problem that forum members may have.
George Chapek, PE.
The vessels have been fabricated by a subsidiary, who neglected to calculate the bending stresses in the hinge pins due to the swing bolt loads. The vessels have been tested, stamped, and delivered to the customer.
I have used our company's evaluation method for hinge pin bending, which assumes that the pins are simply supported beams with a span equal to the width of the distance between the inside faces of the lugs, and loaded with a uniformly distributed load over the width of the swing bolt head -
|.|.|.|.|.|.|
....VVVVVVVV....
===========
^--------------^
Using this approach, the bending stress in the pin, 63000 psi, is over the allowable stress for the pin material, 25000 psi(SA193B7).
I've looked at two alternative loadings - point loading at the edges of the swing bolt head
|............|
V...........V
==========
^--------------^
and a "v-shaped distributed load" over the width of the bolt head -
......|..........|
......||.......||
......|||....|||
......VVVVVV
==========
^..................^
Using the company's evaluation method as a reference,
the alternative methods give bending stresses that are 55%
and 24% of the reference stress, respectively.
Only the point load case stress, 15000 psi, will meet code requirements.
The actual loading on pin probably falls somewhere between the extremes of the cases that I've evaluated. I recognize that using the point load case less conservative, but is it non-conservative? I don't believe there is a cut and dried answer.
Also, since the pins are made of a material normally used for bolting, should the more conservative factors of safety that form the basis for the allowable stress be used, or could a argument be made for using a higher allowable?
My recollection is that the design basis for the higher factors of safety on bolting materials is that they are heat treated to achieve their properties, and thus have yield and ultimate strengths fairly close together, which indicates that they may not be as ductile as materials used for shell and head construction.
I greatly appreciate any insights into this problem that forum members may have.
George Chapek, PE.