aeroUB
Aerospace
- Jun 23, 2003
- 31
I'm making a pressure vessel header out of a sch. 80 8" pipe and for the nozzle coming out of the pipe I would like to use a butt welded 8" Tee.
There are required loads that the "nozzle" needs to be able to support. But I'm not sure how I can demonstrate if it can support them or not. There are calcs. for nozzle loads and resulting max stresses but these all seem to refer to a pipe nozzle being welded into a much larger dome (not one of the same dia.). Also just the geometry of the tee is different...not the sharp 90* joint that would occur if you just welded a pipe into a much larger dome. Per ASME, the max allowable stress in this material is 17,100psi.
Is there a way (other than FEA) to find what the MAX stress in the tee would be, based on the given moments (3) and loads (3)? Are there any calcs/formulas for finding the resulting max stresses for butt welded tees?
Thanks for any input!
There are required loads that the "nozzle" needs to be able to support. But I'm not sure how I can demonstrate if it can support them or not. There are calcs. for nozzle loads and resulting max stresses but these all seem to refer to a pipe nozzle being welded into a much larger dome (not one of the same dia.). Also just the geometry of the tee is different...not the sharp 90* joint that would occur if you just welded a pipe into a much larger dome. Per ASME, the max allowable stress in this material is 17,100psi.
Is there a way (other than FEA) to find what the MAX stress in the tee would be, based on the given moments (3) and loads (3)? Are there any calcs/formulas for finding the resulting max stresses for butt welded tees?
Thanks for any input!