



liveforphysics wrote:Up the tubing diameter by a 1/4".
Problem will be solved.

psycholist wrote:Look up hydrogen embrittlement. Brazing is the most desirable method for welding chrome-moly.




John in CR wrote:Sounds like bogus 4130 to me, and/or you got 4140, which does require heat treatment. Get real stuff from an aircraft supply and use that larger diameter and double the wall thickness and be done with it.
If you already have the tubing, then shape the joint differently and/or use a reinforcing sleeve cut at an angle or V to spread the stress and heat related weakness along the axis of the boom instead of perpendicular to it.






John in CR wrote:Sounds like bogus 4130 to me, and/or you got 4140, which does require heat treatment. Get real stuff from an aircraft supply and use that larger diameter and double the wall thickness and be done with it.
If you already have the tubing, then shape the joint differently and/or use a reinforcing sleeve cut at an angle or V to spread the stress and heat related weakness along the axis of the boom instead of perpendicular to it.



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