Tysoo2
Mechanical
- Nov 13, 2023
- 11
Hey all, We are performing Compress code calculations in preparation for a CRN application for an LPG storage vessel in Saskatchewan Canada. The Vessel already has a CRN in Ontario as that is where it was initially constructed and installed. My issue is that it was sold and moved into Saskatchewan prior to the jurisdiction having authority caring about CRN's applicable to their province. Regardless it has come to light that there is not a valid SK CRN for this vessel so we have been contracted to perform the calculations and submit a CRN application package on behalf of the vessel owner.
To get down to the nitty gritty of it, we have issues. Firstly, the vessel was constructed of SA212-B using the 1964 code which I'm not sure of the code implications since that material was replaced by 516-70 in 1964 and SA-212B isn't listed in any code editions after 1962. Secondly the U1A does not state the extent of radiography performed. The data plate has P.X.R. stamped on it under the ASME and U symbols which I understand to mean Partial Radiography. Using this information we can assume at best that we are working with a joint efficiency of 0.85 for spot RT UW-11(b) for the long and circ seams. with a min. thickness of 0.937" and a basic allowable stress of 17,500Psi for SA-212-B @100°F we are left with a MAWP of only 219.8Psi, and we need a MAWP of 250Psi.
From what I can understand is that the engineers originally used a joint efficiency of 1.00 during the original calculations which is what gave them the 250Psi MAWP. However, I believe there was a mistake made either at the time of the design or to the extent that the radiography was performed.
If all my math is correct and my assumptions are correct someone either made a mistake while the vessel was being designed or radiographed, or there was some allowance in the code to use a joint efficiency of 1.00 in some instances I'm unaware of.
Anyways, any insight or suggestions would be greatly appreciated. Otherwise we are looking at performing full radiography of the vessel and performing a modification prior to the CRN submission, but that adds a lot of extra cost, and we would like to avoid that.
I have attached the original U1A for the vessel for reference.
Thanks,
To get down to the nitty gritty of it, we have issues. Firstly, the vessel was constructed of SA212-B using the 1964 code which I'm not sure of the code implications since that material was replaced by 516-70 in 1964 and SA-212B isn't listed in any code editions after 1962. Secondly the U1A does not state the extent of radiography performed. The data plate has P.X.R. stamped on it under the ASME and U symbols which I understand to mean Partial Radiography. Using this information we can assume at best that we are working with a joint efficiency of 0.85 for spot RT UW-11(b) for the long and circ seams. with a min. thickness of 0.937" and a basic allowable stress of 17,500Psi for SA-212-B @100°F we are left with a MAWP of only 219.8Psi, and we need a MAWP of 250Psi.
From what I can understand is that the engineers originally used a joint efficiency of 1.00 during the original calculations which is what gave them the 250Psi MAWP. However, I believe there was a mistake made either at the time of the design or to the extent that the radiography was performed.
If all my math is correct and my assumptions are correct someone either made a mistake while the vessel was being designed or radiographed, or there was some allowance in the code to use a joint efficiency of 1.00 in some instances I'm unaware of.
Anyways, any insight or suggestions would be greatly appreciated. Otherwise we are looking at performing full radiography of the vessel and performing a modification prior to the CRN submission, but that adds a lot of extra cost, and we would like to avoid that.
I have attached the original U1A for the vessel for reference.
Thanks,