mzamzam
Petroleum
- Feb 26, 2015
- 2
I am a QA/QC engineer in a refinery company but I am not a corrosion specialist. I have a puzzling point about the material used in building some of our towers which were constructed by Chiyoda Corp. The Towers shell and internal rings are made of carbon steel (I can not remember the exact JIS material designation but I think it is equivalent to A285 or A516 Gr.C). The trays, which have a direct contact to the rings, and some internal components are made from SS410 (ASTM A240 410 equivalent).
I searched many times for any codes that can explain the compatibility for the usage of these two different alloys together. In some cases we would prefer to use the austenitic stainless steel series (3xx). I know that the SS316 is more noble than 410 and i think that it will cause/produce a higher galvanic corrosion.
During my searches, I found the two famous codes MIT-STD-889B and NASA-STD-6012. In MIT main chart/table it prohibited both the (ferritic/martensitic & c. steel) coupling and (austenitic & c. steel) one for industrial services. In NASA (ferritic/martenistic & c. steel) is an accepted couple (potential difference between 12%cr and Iron doesn't exceed 0.25V) for space industry (but it does not work in same condition we have in towers "high press. and temp."). I could not find any ASME, ASTM or petroleum related codes that talking about that.
I also read some convincing articles that say that the potential difference, or anodic index difference, is not an enough factor to make a compatible couple. I also saw Wikipedia page where the editor said that the reference is corrosion engineering handbook. I opened the handbook and could not find such anodic index diff. values (0.15, 0.25 & 0.5V) mentioned within!!!
It is very confusing for me. Can I find any NACE, ASME, ASTM, EN, DIN or JIS for?
What are the factors the material selectors and designers use/consider in such case? I think Chiyoda engineers were having a strong reference while making such couple.
Thanks in advance for any help.
I searched many times for any codes that can explain the compatibility for the usage of these two different alloys together. In some cases we would prefer to use the austenitic stainless steel series (3xx). I know that the SS316 is more noble than 410 and i think that it will cause/produce a higher galvanic corrosion.
During my searches, I found the two famous codes MIT-STD-889B and NASA-STD-6012. In MIT main chart/table it prohibited both the (ferritic/martensitic & c. steel) coupling and (austenitic & c. steel) one for industrial services. In NASA (ferritic/martenistic & c. steel) is an accepted couple (potential difference between 12%cr and Iron doesn't exceed 0.25V) for space industry (but it does not work in same condition we have in towers "high press. and temp."). I could not find any ASME, ASTM or petroleum related codes that talking about that.
I also read some convincing articles that say that the potential difference, or anodic index difference, is not an enough factor to make a compatible couple. I also saw Wikipedia page where the editor said that the reference is corrosion engineering handbook. I opened the handbook and could not find such anodic index diff. values (0.15, 0.25 & 0.5V) mentioned within!!!
It is very confusing for me. Can I find any NACE, ASME, ASTM, EN, DIN or JIS for?
What are the factors the material selectors and designers use/consider in such case? I think Chiyoda engineers were having a strong reference while making such couple.
Thanks in advance for any help.