Strook
Mechanical
- Nov 4, 2020
- 23
G'day guys,
Working with some significant nozzle loads (250 kN axial, 580 kN.m for DN900 into 1800OD vessel) and thinking through various options for strengthening the nozzle.
At this stage, reinforced set-in nozzle construction is yielding shell & comp plate thicknesses around 40mm, a little higher than I'm hoping to get away with.
External gussets are subject to thermal differential, leading to cracking of welds etc. Could this be counteracted simply by insulating the vessel? Vessel operating at ambient to 115degC.
The other suggestion I have is nozzle internal projection providing real estate for an internal gusseting arrangement in lieu of the typical external gusseting. I suspect such an arrangement wouldn't be as likely subject to thermal differential, and would provide direct connection to shell rather than to comp plate. Obviously this wouldn't help the nozzle neck much but conceivably would reduce shell & comp plate thicknesses.
Thoughts on the principle of such a design are welcome, please.
EDIT: The most obscure aspect - existing vessel operating at -8 kPa(g) / +37 kPa(g), 1800 OD and 15m tall with skirt. Extremely low pressure equipment but somehow (?!) piping loads onto this plant are astronomical. I've suggested the piping design is revised to reduce these loads, but in the mean time thinking through worst case options.
Working with some significant nozzle loads (250 kN axial, 580 kN.m for DN900 into 1800OD vessel) and thinking through various options for strengthening the nozzle.
At this stage, reinforced set-in nozzle construction is yielding shell & comp plate thicknesses around 40mm, a little higher than I'm hoping to get away with.
External gussets are subject to thermal differential, leading to cracking of welds etc. Could this be counteracted simply by insulating the vessel? Vessel operating at ambient to 115degC.
The other suggestion I have is nozzle internal projection providing real estate for an internal gusseting arrangement in lieu of the typical external gusseting. I suspect such an arrangement wouldn't be as likely subject to thermal differential, and would provide direct connection to shell rather than to comp plate. Obviously this wouldn't help the nozzle neck much but conceivably would reduce shell & comp plate thicknesses.
Thoughts on the principle of such a design are welcome, please.
EDIT: The most obscure aspect - existing vessel operating at -8 kPa(g) / +37 kPa(g), 1800 OD and 15m tall with skirt. Extremely low pressure equipment but somehow (?!) piping loads onto this plant are astronomical. I've suggested the piping design is revised to reduce these loads, but in the mean time thinking through worst case options.