henderrj
Specifier/Regulator
- Oct 13, 2015
- 18
In regards to a simple pipe nozzle in a cylindrical shell:
Reinforcement calculations are done based on a plane that cuts through the center of the nozzle, in line with the longitudinal axis of the cylinder. What about the plane which also runs through the centerline of the nozzle, but is perpendicular to the longitudinal axis of the cylinder?
My question is this: Since the circumferential stress is roughly twice the longitudinal stress in this scenario, shouldn't you be able to have a reinforcing pad that was half the required width at those points? For example, let's say we have a vertical vessel with a 6" nozzle on the shell. The calculations were run, and they called for a 12" diameter pad, total. Speaking about bare minimums, couldn't you use a reinforcing pad that was oblong, with a height of 12" and a width of 9"?
UG-37(b) says this: "Reinforcement shall be provided in amount and distribution such that the area requirements for reinforcement are satisfied for all planes through the center of the opening and normal to the vessel surface. For a circular opening in a cylindrical shell, the plane containing the axis of the shell is the plane of greatest loading due to pressure. Not less than half the required reinforcement shall be on each side of the centerline of single openings.”
The underlined sentence goes along with my point, but it never specifically says one way or the other. For the first sentence, it could be said that the requirements for reinforcement are satisfied, because less reinforcement is required on the perpendicular plane.
I've looked all over and can't find anything covering this, including interpretations. Before anybody gets angry, this is just out of curiosity. I'm not advocating for people to start using oval repads. Thanks!
Reinforcement calculations are done based on a plane that cuts through the center of the nozzle, in line with the longitudinal axis of the cylinder. What about the plane which also runs through the centerline of the nozzle, but is perpendicular to the longitudinal axis of the cylinder?
My question is this: Since the circumferential stress is roughly twice the longitudinal stress in this scenario, shouldn't you be able to have a reinforcing pad that was half the required width at those points? For example, let's say we have a vertical vessel with a 6" nozzle on the shell. The calculations were run, and they called for a 12" diameter pad, total. Speaking about bare minimums, couldn't you use a reinforcing pad that was oblong, with a height of 12" and a width of 9"?
UG-37(b) says this: "Reinforcement shall be provided in amount and distribution such that the area requirements for reinforcement are satisfied for all planes through the center of the opening and normal to the vessel surface. For a circular opening in a cylindrical shell, the plane containing the axis of the shell is the plane of greatest loading due to pressure. Not less than half the required reinforcement shall be on each side of the centerline of single openings.”
The underlined sentence goes along with my point, but it never specifically says one way or the other. For the first sentence, it could be said that the requirements for reinforcement are satisfied, because less reinforcement is required on the perpendicular plane.
I've looked all over and can't find anything covering this, including interpretations. Before anybody gets angry, this is just out of curiosity. I'm not advocating for people to start using oval repads. Thanks!