GD_P
Structural
- Apr 6, 2018
- 128
I have been assigned with the task to design the closure (refer attachment) to comply with ASME Sec VIII Div 1. In this closure assembly, compression bolt engaged in split ring tapping along with split ring ensures the required sealing force.
Design conditions are
Material: SS316, temp: 300 deg C, Pressure: 10 MPa, Gasket: Grafoil, service: Non-lethal
Referring closure assembly parts, code doesn’t contain design rules for part other than shell. As per U-1(3) “The Code does not address all aspects of these activities, and those aspects which are not specifically addressed should not be considered prohibited. Engineering judgment must be consistent with the philosophy of this Division, and such judgments must never be used to overrule mandatory requirements or specific prohibitions of this Division.” So with this reference, I am proposing below procedure to comply the closure assembly to div 1 requirements. Please guide me if I am wrong.
Loose flange: As per Mand Appdx 2, 2-1(a) “The rules in Mandatory Appendix 2 apply specifically to the design of bolted flange connections with gaskets that are entirely within the circle enclosed by the bolt holes and with no contact outside this circle, and are to be used in conjunction with the applicable requirements in Subsections A, B, and C of this Division.” Loose flange doesn’t have any hole in this case. So by engineering judgement, considering PCD (pitch circle dia) at average dia of ‘Loose Flange to Split Ring Contact surface’, we can design loose flange as per Mand appdx 2 rules. Design conditions will be same as given in appdx 2 - Gasket seating & operating. (No doubt that operating condition will govern here).
Cover: Here bolt (compression bolt) PCD is different than the companion loose flange. Also bolt PCD is smaller than the gasket mean diameter. So to keep the design simple i.e., to use UG-34 rules, we can use the PCD same as considered for loose flange design. By engineering judgement this will result in conservative design.
Compression bolt: This will be standard bolt based on the load for “Operating condition” obtained in loose flange design. Here the bolt is in compression as against the mand appdx 2 bolts which are always in tension. So in such a scenario, should I use the same allowable stress for bolts (Sec II D, table3)? Or I can increase them upto yield strength?
Split ring: In div 1, there are no rules to design it. So as per U-2(g), ‘Mand Appdx 46 (46-4 DESIGN BY ANALYSIS) and Proof test are 2 available options. Generating 3.5 times design pressure to proof test is not possible for us considering our current capacity. So the only option is FEA. Also I was wondering that how do we fabricate this. This can not be fabricated from plate form, since this may result in tensile stresses in through thickness direction. Any suggestion.....
Regards,
GD_P
Design conditions are
Material: SS316, temp: 300 deg C, Pressure: 10 MPa, Gasket: Grafoil, service: Non-lethal
Referring closure assembly parts, code doesn’t contain design rules for part other than shell. As per U-1(3) “The Code does not address all aspects of these activities, and those aspects which are not specifically addressed should not be considered prohibited. Engineering judgment must be consistent with the philosophy of this Division, and such judgments must never be used to overrule mandatory requirements or specific prohibitions of this Division.” So with this reference, I am proposing below procedure to comply the closure assembly to div 1 requirements. Please guide me if I am wrong.
Loose flange: As per Mand Appdx 2, 2-1(a) “The rules in Mandatory Appendix 2 apply specifically to the design of bolted flange connections with gaskets that are entirely within the circle enclosed by the bolt holes and with no contact outside this circle, and are to be used in conjunction with the applicable requirements in Subsections A, B, and C of this Division.” Loose flange doesn’t have any hole in this case. So by engineering judgement, considering PCD (pitch circle dia) at average dia of ‘Loose Flange to Split Ring Contact surface’, we can design loose flange as per Mand appdx 2 rules. Design conditions will be same as given in appdx 2 - Gasket seating & operating. (No doubt that operating condition will govern here).
Cover: Here bolt (compression bolt) PCD is different than the companion loose flange. Also bolt PCD is smaller than the gasket mean diameter. So to keep the design simple i.e., to use UG-34 rules, we can use the PCD same as considered for loose flange design. By engineering judgement this will result in conservative design.
Compression bolt: This will be standard bolt based on the load for “Operating condition” obtained in loose flange design. Here the bolt is in compression as against the mand appdx 2 bolts which are always in tension. So in such a scenario, should I use the same allowable stress for bolts (Sec II D, table3)? Or I can increase them upto yield strength?
Split ring: In div 1, there are no rules to design it. So as per U-2(g), ‘Mand Appdx 46 (46-4 DESIGN BY ANALYSIS) and Proof test are 2 available options. Generating 3.5 times design pressure to proof test is not possible for us considering our current capacity. So the only option is FEA. Also I was wondering that how do we fabricate this. This can not be fabricated from plate form, since this may result in tensile stresses in through thickness direction. Any suggestion.....
Regards,
GD_P