Oh yes. Zip-Chem recommended by Boeing, the builder of 737-MAX. . There is this; NO-OX-ID A-Special = https://www.amazon.com/gp/product/B00HDF9EXE/ref=ppx_yo_dt_b_asin_title_o04_s00?ie=UTF8&psc=1
I spent many years offshore sailboat racing where stainless fasteners connecting into aluminum spars was a constant concern and safety issue so i agree it needs to be addressed in the design phase.Having spent many years in the Navy Avionics world, then living in Florida, corrosion is an ever present destroyer.
Galvanic corrosion in particular needs to be addressed in the design phase it needs only moisture in the air like humidity to come about.
I am more concerned about tensile strength of stainless holding my aluminum buss bars to the aluminim terminal tops where I want the greatest surface area to conduct heat and electricity. It actually serves my purpose if there is some corrosion that creates friction or even some galling because I do not want the studs to turn when torqueing them to their Nm spec. I wasn't able to find aluminum studs anyway. My pack will be in a cabinet in an enclosed garage whose air has less humidity than the surrounding air. I am confident in my design but do encourage others to follow your suggestions.If you think that "sealing" your battery posts eliminates the opportunity for galvanic corrosion, read about F16 jets falling out of the sky due to the design mating tin pins to gold sockets inside mil spec "sealed" connectors.
You didn't read the article I linked then.I tried but can find no reference to failure of tin pins mated to gold sockets.
Your chart seems to be at odds with everything I found when I was researching ampacity of bus bars. Most resources indicate 1.0A per mm2 of aluminum, and 1.6A per mm2 of copper.I found it to be very cheap and easy and the results were surprisingly good. The below is from 1/2 inch pipe from a hardware store. OD= 12.7mm, ID= 10.88mm, so total copper cross sectional area = 33.7mm. Based on this link, the ampacity of the full cross section is probably somewhere around 180A. I'm also planning to do some with 3/4 inch pipe which will have a 57mm cross sectional area for an ampacity of 250A.
Your chart seems to be at odds with everything I found when I was researching ampacity of bus bars. Most resources indicate 1.0A per mm2 of aluminum, and 1.6A per mm2 of copper.
Im not saying that you can't run 250A through that bus bar, but I'm pretty sure you are going to have a temperature rise that could get dangerous if you have any combustible materials nearby.
I look forward to seeing your test results. Please don't forget to monitor your temperature rise of the bus bars.
I hope anyone who tries to do their own electroplating follows all the safety precautions. The disposal of your waste is also very important. Research the environmental impact of this before you start. This stuff is dangerous.
I used the Blue Sea ampacity table for wire. 4/0 wire has a cross section area of 107 mm^2 and an ampacity of 445A for 105C insulation and 30C, and 378A when in an engine room which means 50C. This is from the ABYC standard used for marine applications. I trust it.Your chart seems to be at odds with everything I found when I was researching ampacity of bus bars. Most resources indicate 1.0A per mm2 of aluminum, and 1.6A per mm2 of copper.
No, aluminum oxidizes faster than copper but is easier for me to work so that is why I use aluminum buss bars. I have accumulated a 30 years supply of NoAlox because I keep misplacing it and buying another tube for the next project. I also use it on my bussbars on my service panels.Is there an all aluminum solution that eliminates the goop need?
I'm using dual rated aluminum mechanical lugs and NoAlox.Dealing with the galvanic corrosion issue, if you nickel plate the copper lugs (easy to do at home) it prevents the corrosion.