6951 Aluminum Alloy Coil

 

6951 aluminum alloy is a Al-Mg-Si based system and is used as forgings and extrusions. The alloy is heat treatable. The microstructure has Mg2Si precipitates in addition to undissolved intermetallic particles consisting of Fe and Mn. 6951 aluminum alloy belongs to the 6000 series alloy class, which means its major alloy includes magnesium and silicon. Its modification includes 97.2% aluminum with magnesium, silicon, and iron among its major alloys with the addition of copper, manganese, and zinc. This alloy adds strength to increase sag resistance and makes it heat treatable (metal becomes stronger through heating and cooling).


Chemical Composition:

 

Chemical ElementsOriginal Value
Aluminum, Al <= 97 %
Copper, Cu 0.15 - 0.40 %
Iron, Fe <= 0.80 %
Magnesium, Mg 0.40 - 0.80 %
Manganese, Mn <= 0.10 %
Other, each <= 0.05 %
Other, total <= 0.15 %
Silicon, Si 0.20 - 0.50 %
Zinc, Zn <= 0.20 %

 

 Mechanical Properties:

 

Mechanical PropertiesOriginal ValueComments
Hardness, Brinell 82500 kg load with 10 mm ball
Hardness, Knoop 106Converted from Brinell Hardness Value
Hardness, Rockwell A 35.5Converted from Brinell Hardness Value
Hardness, Rockwell B 50Converted from Brinell Hardness Value
Hardness, Vickers 92Converted from Brinell Hardness Value
Tensile Strength, Ultimate 270 MPa 
Tensile Strength, Yield 230 MPa 
Elongation at Break 13 %In 5 cm; Sample 1.6 mm thick
Modulus of Elasticity 69.0 GPaAverage of Tension and Compression. In Al alloys, the compressive modulus is typically 2% greater than the tensile modulus. Estimated from trends in similar Al alloys.
Poissons Ratio 0.33Estimated from trends in similar Al alloys.
Shear Modulus 26.0 GPaEstimated from similar Al alloys.

 

Thermal Properties:

 

Thermal PropertiesOriginal ValueComments
CTE, linear 13.0 µin/in-°F
@Temperature 20.0 - 100 °C
AA; Typical; average over range
 25.0 µm/m-°C
@Temperature 20.0 - 300 °C
 
Specific Heat Capacity 0.890 J/g-°CEstimated from trends in similar Al alloys.
Thermal Conductivity 1370 BTU-in/hr-ft²-°FAA; Typical at 77°F
Melting Point 1140 - 1210 °FAA; Typical range based on typical composition for wrought products >= 1/4 in. thickness
Solidus 1140 °FAA; Typical
Liquidus 1210 °FAA; Typical

 


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