rbattelle
TDR MEMBER
I constantly hear people and companies spout off about using "6061-T6" aluminum parts, as though that particular alloy is some special grade.
So I thought I would post some information about Al-6061-T6.
According to Machinery's Handbook (26th ed. , page 549):
The 4-digit designation system for aluminum alloys is decoded as follows:
The first digit indicates the alloy type:
1 - 99% or greater pure aluminum
2 - copper
3 - manganese
4 - silicon
5 - magnesium
6 - magnesium and silicon
7 - zinc
8 - some other element
If the second digit is 0 (as in 6061), it indicates there's no control on individual impurities. The last 2 digits have no significance other than identification.
Something like 6066-T6 is about 27% stronger in tensile stress and 13% better shear stress. 7049-T73 is 67% higher tensile stress and 30% better shear stress. Meanwhile 7178-T6 gives you 96% better tensile stress than 6061-T6 (and you get impurities control too!).
Now, to you manufacturers out there. If you really want to impress me with an aluminum alloy, how about using 7075-T6? 84% better tensilte stress and 60% better shear stress than 6061-T6.
General purpose 6061-T6 is a great alloy... but not that great.
-Ryan
So I thought I would post some information about Al-6061-T6.
According to Machinery's Handbook (26th ed. , page 549):
6000 Series: Alloys in this group contain silicon and magnesium in approximate proportions to form magnesium silicide, thus making them capable of being heat treated. The major alloys in this series are 6061, one of the most versatile of the heat-treatable alloys. Though less strong than most of the 2000 or 7000 alloys, the magnesium-silicon (or magnesium-silicide) alloys possess good formability and corrosion resistance, with medium strength. Alloys in this heat-treatable group may be formed in the -T4 temper (solution heat treated by not artificially aged) and then reach full -T6 properties by artificial aging.
The 4-digit designation system for aluminum alloys is decoded as follows:
The first digit indicates the alloy type:
1 - 99% or greater pure aluminum
2 - copper
3 - manganese
4 - silicon
5 - magnesium
6 - magnesium and silicon
7 - zinc
8 - some other element
If the second digit is 0 (as in 6061), it indicates there's no control on individual impurities. The last 2 digits have no significance other than identification.
Something like 6066-T6 is about 27% stronger in tensile stress and 13% better shear stress. 7049-T73 is 67% higher tensile stress and 30% better shear stress. Meanwhile 7178-T6 gives you 96% better tensile stress than 6061-T6 (and you get impurities control too!).
Now, to you manufacturers out there. If you really want to impress me with an aluminum alloy, how about using 7075-T6? 84% better tensilte stress and 60% better shear stress than 6061-T6.
General purpose 6061-T6 is a great alloy... but not that great.

-Ryan