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#1
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Welding techniques for 4130?
I am going to begin an aircraft project this winter and it looks like I have a
LOT of welding ahead of me. I'm curious as to the different methods, ie brazing vs. arc, etc., and what the benefits or drawbacks of each method may be. Is one style better? Stronger? Easier? I will be working with a buddy who owns a machine shop and he has just about all the equipment I could ever ask for. Given that availability of equipment, what would you welders out there recommend or prefer? Thanks. |
#2
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Tig if not then oxy/ac
"Building The Perfect Beast" wrote in message ... I am going to begin an aircraft project this winter and it looks like I have a LOT of welding ahead of me. I'm curious as to the different methods, ie brazing vs. arc, etc., and what the benefits or drawbacks of each method may be. Is one style better? Stronger? Easier? I will be working with a buddy who owns a machine shop and he has just about all the equipment I could ever ask for. Given that availability of equipment, what would you welders out there recommend or prefer? Thanks. |
#3
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Tig if not then oxy/ac
"Building The Perfect Beast" wrote in message ... I am going to begin an aircraft project this winter and it looks like I have a LOT of welding ahead of me. I'm curious as to the different methods, ie brazing vs. arc, etc., and what the benefits or drawbacks of each method may be. Is one style better? Stronger? Easier? I will be working with a buddy who owns a machine shop and he has just about all the equipment I could ever ask for. Given that availability of equipment, what would you welders out there recommend or prefer? Thanks. |
#4
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On 28 Aug 2003 02:00 PM, Building The Perfect Beast posted the following:
I am going to begin an aircraft project this winter and it looks like I have a LOT of welding ahead of me. I'm curious as to the different methods, ie brazing vs. arc, etc., and what the benefits or drawbacks of each method may be. Is one style better? Stronger? Easier? I will be working with a buddy who owns a machine shop and he has just about all the equipment I could ever ask for. Given that availability of equipment, what would you welders out there recommend or prefer? I'm going to assume you will be welding 4130 steel structures exclusively. If you are a relative novice to welding, use oxy-acetylene equipment and mild steel rod. Do a Google search on this newsgroup, paying extra close attention to posts by Bruce Frank and a guy named "Highflier." Also, the EAA puts out an excellent publication on aircraft welding. As for equipment, if I were buying new equipment I would buy one of the standard cutting/welding kits from Victor or Harris (now owned by lincoln electric) mainly to get the regulators and hoses. The torches that come with those kits are on the large side for welding thin material, so buy a smaller torch which will be more maneuverable, especially around fuselage clusters. I've heard good reports about the Meco Midget, the Smith Airline, and the Henrob (people who have used the latter find it a bit heavy). Unless you are already an accomplished welder, ignore suggestions to purchase an expensive TIG welding machine. It is not necessary and may lead to undesirable results unless you have already mastered the basics of welding with oxy-acetylene equipment. I use a small TIG machine and like it, but I also use it for other things (like aluminum and automotive projects) and had quite a bit of oxy/acetylene experience before trying it. If I couldn't afford a TIG unit, I would weld together my airframe using oxy/acetylene with no hesitation. ---------------------------------------------------- Del Rawlins- Remove _kills_spammers_ to reply via email. Unofficial Bearhawk FAQ website: http://www.rawlinsbrothers.org/bhfaq/ |
#5
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I'm going to assume you will be welding 4130 steel structures
exclusively. If you are a relative novice to welding, use oxy-acetylene equipment and mild steel rod. Do a Google search on this newsgroup, paying extra close attention to posts by Bruce Frank and a guy named "Highflier." Also, the EAA puts out an excellent publication on aircraft welding. Thanks Del. That's what I was looking for. I did a Google search and just came up on too many hits. I was hoping that I might get it narrowed down and you've done just that for me. Unless you are already an accomplished welder, ignore suggestions to purchase an expensive TIG welding machine. It is not necessary and may lead to undesirable results unless you have already mastered the basics of welding with oxy-acetylene equipment. I use a small TIG machine and like it, but I also use it for other things (like aluminum and automotive projects) and had quite a bit of oxy/acetylene experience before trying it. If I couldn't afford a TIG unit, I would weld together my airframe using oxy/acetylene with no hesitation. Luckily I've got a buddy who is going to build with me and he is a master welder. I plan on learning a lot from him. As for my experience, well, most of it is on farm equipment and about all I've ever used oxy/acetylene for was cutting stuff up. I'm a fair stick welder but I know I've got a lot to learn. And I'm looking forward to it. Done properly, do you feel that there is any difference in the quality of weld produced by oxy/ace vs. TIG? Is the TIG just less hassle or what? |
#6
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#7
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On 30 Aug 2003 11:08 AM, Building The Perfect Beast posted the following:
Done properly, do you feel that there is any difference in the quality of weld produced by oxy/ace vs. TIG? Is the TIG just less hassle or what? Well, many knowledgable and experienced welders believe that the narrower heat effected zone (HAZ) causes more stresses to be concentrated right next to the weld, rather than spread out over a wider area adjacent to the weld. The problem is that while the weld may be sound, these stress concentrations might cause cracking right next to the TIG welds. The cure for this is to either weld using oxy-acetylene, or to post heat the TIG welds using an O/A torch with the "rosebud" heating attachment, which stress relieves the joint, moving the stresses away from the more highly loaded weld clusters, and preventing the cracking. For every welder who holds this opinion, you can probably find another equally qualified welder (including the guy who helped FAA revise the welding portion of AC43.13) who believes it to be a non-issue and the post heating to be unnecessary. As a mostly self-taught amateur welder, my position is that I don't know enough to say either way, but that nobody has been able to convince me there is a downside to post heating the TIG welded joints, other than the time and cost of the gases used. My plan is to do as Bruce has suggested in the past, and not worry about it for the most part, but to also go over some of the more highly stressed critical areas with the rosebud. Places like the wing and landing gear attach fittings, and the tailspring and engine mount points. For the record, I *really* like my TIG unit (a Lincoln square wave 175) and I feel that the precision, cleanliness, and convenience of the TIG process outweighs the disadvantages of cost and possible need to strain relieve welds. But in your case, since you will need to develop oxy/ acetylene skills anyway before you can even think about trying the TIG, you should just use the O/A torch for your welding since it is easier and more forgiving. I already had plenty of O/A welding experience under my belt and I did quite a bit of welding on non-aviation stuff with the TIG before I ever started putting aircraft parts together with it. ---------------------------------------------------- Del Rawlins- Remove _kills_spammers_ to reply via email. Unofficial Bearhawk FAQ website: http://www.rawlinsbrothers.org/bhfaq/ |
#8
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#9
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