FreddieH
Nuclear
- Apr 15, 2013
- 5
Hi,
After searching around for awhile with no luck I have decided to write a post.
I am sizing and assessing a cylindrical nozzle positioned in the centre of a torispherical head. I have completed evaluations of intersecting cylinders, however I cannot find a WRC Bulletin or any other material that provides formulae to calculate membrane stress and surface stress intensity on nozzles or vessels in spherical shells with a cylindrical nozzle. I can only find area reinforcement rules for radial nozzles on spherical shells, however I am required to assess the nozzle against stress criteria.
I need to calculate stress due to internal pressure, I have used WRC Bulletin 537 to find the stress due to external loading. Although, when using WRC 537, the attachment parameters Gamma and rho lay outside of the data range so I had to make up a much weaker thinner nozzle with no reinforcement to get the parameters to lie within the usable range. (Is that normal, because using area reinforcement rules I had to INCREASE the size of the tapered reinforcement), but then to analyse the stresses I had to REDUCE the taper to return to a straight thin cylinder attached to the torispherical head. This caused an issue as now with a reduced vessel and nozzle wall section when calculating the stress from the dimensionless membrane force, it becomes very very large unless I then revert back to using the actual vessel wall thickness. Which may be a problem as it is a different vessel wall thickness to that which was used to calculate the dimensionless membrane force.
The stresses in radial nozzles on spherical shells due to internal pressure seems to be lacking, In the mean time I have calculated the force the internal pressure exerts inside the nozzle (circular area inside nozzle * pressure) and then summed that with the external loading and calculated the stress assuming all loading is in the form of external loads. I read here [URL unfurl="true"]http://www.carmagen.com/news/engineering_articles/news30.htm[/url] that this is a conservative method.
Does anyone have any understanding of this type of problem?
Thank you in advance.
After searching around for awhile with no luck I have decided to write a post.
I am sizing and assessing a cylindrical nozzle positioned in the centre of a torispherical head. I have completed evaluations of intersecting cylinders, however I cannot find a WRC Bulletin or any other material that provides formulae to calculate membrane stress and surface stress intensity on nozzles or vessels in spherical shells with a cylindrical nozzle. I can only find area reinforcement rules for radial nozzles on spherical shells, however I am required to assess the nozzle against stress criteria.
I need to calculate stress due to internal pressure, I have used WRC Bulletin 537 to find the stress due to external loading. Although, when using WRC 537, the attachment parameters Gamma and rho lay outside of the data range so I had to make up a much weaker thinner nozzle with no reinforcement to get the parameters to lie within the usable range. (Is that normal, because using area reinforcement rules I had to INCREASE the size of the tapered reinforcement), but then to analyse the stresses I had to REDUCE the taper to return to a straight thin cylinder attached to the torispherical head. This caused an issue as now with a reduced vessel and nozzle wall section when calculating the stress from the dimensionless membrane force, it becomes very very large unless I then revert back to using the actual vessel wall thickness. Which may be a problem as it is a different vessel wall thickness to that which was used to calculate the dimensionless membrane force.
The stresses in radial nozzles on spherical shells due to internal pressure seems to be lacking, In the mean time I have calculated the force the internal pressure exerts inside the nozzle (circular area inside nozzle * pressure) and then summed that with the external loading and calculated the stress assuming all loading is in the form of external loads. I read here [URL unfurl="true"]http://www.carmagen.com/news/engineering_articles/news30.htm[/url] that this is a conservative method.
Does anyone have any understanding of this type of problem?
Thank you in advance.