OEM 6070 Forging Aluminum Parts For Aerospace /Automobile/Railway
Vehicle/Metal Forging Part/Aluminum Forging Part
Our Advantages
1. 3 technical patents and 2 practical patents related to
high-silicon aluminum alloy melting, crystallization, and forging
2. Multiple professional presses adapted to the deformation speed
of high-silicon aluminum alloys
3. Two intermediate frequency heating furnaces suitable for heating
weak magnetic materials such as high-silicon aluminum alloys
4. Perfect forging process of various pistons and swash plates,
mold tooling technology, materials, and product inspection
standards.
5. The close cooperative relationship between the company and the
university scientific research is our strong technical backing.
6. We are high-tech enterprises
7. Development capability: aluminum alloy, titanium alloy, super
alloy, non-ferrous metal forging development
Product Details
Material | Aluminum Alloy 6070 |
Process | Forging+CNC+Heat Treatment |
Surface Treatment | Transparent, Color Anodized, Hard Anodizing, Powder Coating;
Sandblasting, Laser Carving, Silk Screening;
Nickel-Plated, Chrome, Galvanized, Silver/Gold Plating;
Black Oxide Coating, Polishing; etc... |
Manufacture Ability | Depends on The Complexity Of Different Products And Quantities |
Experience | Aluminum Machining Service for 12 Years |
Packaging | Standard Export Wooden Pallets
Another Request According to Your Needs |
MOQ | 1pcs |
Sample | Can Be Customized |
Mold | Can Be Customized |
Lead Time | Mold for 15-20 Days Process for 15-20 Days |
OEM | Can Be Customized |
Chemical Composition of 6070 |
Alloy | Si | Fe | Cu | Mn | Mg | Cr | Zn | Ti | Others | Al |
Each | Total |
6070 | 1.0-1.7 | 0.50max | 0.15-0.40 | 0.15max | 0.2-1.2 | 0.10max | 0.25max | 0.15max | 0.05max | 0.15max | Rest |
Technical Specifications of 6070-T6
Physical Properties | Metric | English | Comments |
Density | 2.71 g/cc | 0.0979 lb/in³ | AA; Typical |
|
Mechanical Properties | Metric | English | Comments |
Hardness, Brinell | 120 | 120 | 500 kg load with 10 mm ball |
Hardness, Knoop | 150 | 150 | Converted from Brinell Hardness Value |
Hardness, Rockwell A | 46.8 | 46.8 | Converted from Brinell Hardness Value |
Hardness, Rockwell B | 75 | 75 | Converted from Brinell Hardness Value |
Hardness, Vickers | 137 | 137 | Converted from Brinell Hardness Value |
Tensile Strength, Ultimate | 379 MPa | 55000 psi | AA; Typical |
Tensile Strength, Yield | 352 MPa | 51000 psi | AA; Typical |
Elongation at Break | 10 %
@Thickness 1.59 mm | 10 %
@Thickness 0.0625 in | AA; Typical |
Modulus of Elasticity | 68.9 GPa | 10000 ksi | AA; Typical; Average of tension and compression. The compression
modulus is about 2% greater than tensile modulus. |
Poissons Ratio | 0.33 | 0.33 | Estimated from trends in similar Al alloys. |
Fatigue Strength | 96.5 MPa
@# of Cycles 5.00e+8 | 14000 psi
@# of Cycles 5.00e+8 | completely reversed stress; RR Moore machine/specimen |
Shear Modulus | 26.0 GPa | 3770 ksi | Estimated from similar Al alloys. |
Shear Strength | 234 MPa | 34000 psi | AA; Typical |
|
Electrical Properties | Metric | English | Comments |
Electrical Resistivity | 0.00000390 ohm-cm | 0.00000390 ohm-cm |
|
|
Thermal Properties | Metric | English | Comments |
CTE, linear  | 23.2 µm/m-°C
@Temperature 20.0 - 100 °C | 12.9 µin/in-°F
@Temperature 68.0 - 212 °F |
|
| 24.8 µm/m-°C
@Temperature 20.0 - 300 °C | 13.8 µin/in-°F
@Temperature 68.0 - 572 °F |
|
Specific Heat Capacity | 0.891 J/g-°C | 0.213 BTU/lb-°F |
|
Thermal Conductivity | 172 W/m-K | 1190 BTU-in/hr-ft²-°F |
|
Melting Point | 566 - 649 °C | 1050 - 1200 °F | AA; Typical range based on typical composition for wrought products
>= 1/4 in. thickness. Eutectic melting is not eliminated by
homogenization. |
Solidus | 566 °C | 1050 °F | AA; Typical |
Liquidus | 649 °C | 1200 °F | AA; Typical |
|
Processing Properties | Metric | English | Comments |
Solution Temperature | 546.1 °C | 1015 °F | followed by quenching |
Aging Temperature | 160 °C | 320 °F | hold at temperature for 18 hr |
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