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Metalworking (rec.crafts.metalworking) Discuss various aspects of working with metal, such as machining, welding, metal joining, screwing, casting, hardening/tempering, blacksmithing/forging, spinning and hammer work, sheet metal work. |
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#41
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Strength of aircraft grade versus 6061 aluminum?
"John Doe" wrote in message ... Jim Wilkins wrote: As I understand it, 6061 is the strongest alloy that doesn't have corrosion, brittleness and joining issues requiring extra engineering analysis. Sounds like a good general purpose aluminum for making stuff. I suppose 6063 isn't much different. At McMaster, 6063 comes in a few additional desirable forms for a non-machinist. FWIW, 6063 has a little less strength than 6061 and a little less elongation (ductility). But it's a bit more weldable, having lower zinc and copper content. It's basically an extrusion grade, with a little extra corrosion resistance over 6061. Machineability is rated "fair" by ASM. -- Ed Huntress |
#42
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Strength of aircraft grade versus 6061 aluminum?
On Oct 7, 10:08 pm, "Stupendous Man" wrote:
The boss got me a ten foot sheet of aluminum to make some odd shaped cargo boxes for his 61 Land Rover. I laid out a nice pattern to make them with as few riveted seams as possible, thought it seemed a bit tough to cut but has no grade markings on it. I test bent a piece and it cracked. I called the office and asked what was on the receipt. He got 1/8 6061 T6 on sale. I guess I will be annealing all the bend seams in the morning with a rosebud. No, no, Not so much heat. It'll melt. Make a black mark with a Jiffy marker and heat the area until the mark starts to disappear. It takes very little heat to anneal this stuff. You can ruin it so easily. I use a simple propane torch and am careful with that. Dan |
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