meltedEng
Mechanical
- Aug 24, 2017
- 47
Hello,
For reference this question is related to ASME BPVC VIII Div 1, appendix A. This is where we started.
I'm trying to justify the allowable load and the joint design on an expanded only enhanced TTS joint (type i per Table A-2). Normally we only work in welded only using A-2 with A-3 testing, but currently we are working with some unweldable alloys for corrosion.
We created some QW-193 style mock-ups and push-out tests per A-1(e)(3)(-d). We could apply A-2 (with fr from A-3) to get L(max) as we normally do for welded, which gives an acceptable allowable load of 2000 lbs for at operating temperature push-out. Our application only requires 400 lbs.
A-1(e)(3)(-d) requires A-5 to be satisfied, which by inspection requires an fr of 1. This would give us an allowable load of 5000 lbs. We only need an fr of ~0.2 for this application. Rolling this material to reach an fr of 1 is ill advised.
Essentially we don't need to handle the loads that appendix A seems to be designing for. We are considering disregarding A-5 as it appears to be wanting us to highly over engineer. Our push-out at temp gave us the 2000 lbs allowable, and we're comfortable with that.
Is there another industry standard or reference for determining the allowable load on this joint type at operating temperature? If anyone has some insight or reference into the justification of A-5, that would be appreciated.
For reference this question is related to ASME BPVC VIII Div 1, appendix A. This is where we started.
I'm trying to justify the allowable load and the joint design on an expanded only enhanced TTS joint (type i per Table A-2). Normally we only work in welded only using A-2 with A-3 testing, but currently we are working with some unweldable alloys for corrosion.
We created some QW-193 style mock-ups and push-out tests per A-1(e)(3)(-d). We could apply A-2 (with fr from A-3) to get L(max) as we normally do for welded, which gives an acceptable allowable load of 2000 lbs for at operating temperature push-out. Our application only requires 400 lbs.
A-1(e)(3)(-d) requires A-5 to be satisfied, which by inspection requires an fr of 1. This would give us an allowable load of 5000 lbs. We only need an fr of ~0.2 for this application. Rolling this material to reach an fr of 1 is ill advised.
Essentially we don't need to handle the loads that appendix A seems to be designing for. We are considering disregarding A-5 as it appears to be wanting us to highly over engineer. Our push-out at temp gave us the 2000 lbs allowable, and we're comfortable with that.
Is there another industry standard or reference for determining the allowable load on this joint type at operating temperature? If anyone has some insight or reference into the justification of A-5, that would be appreciated.