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Brand Name : JIMA
Model Number : ALP
Certification : ISO9001-2008,SGS,ROHS.
Place of Origin : CHINA
MOQ : 1PCS
Price : Negotiations
Payment Terms : T/T, L/C
Supply Ability : 10000 pcs /per month
Delivery Time : 10~20days
Packaging Details : Wooden Pallet
Application : Airplane/Automotive/Ship
Name : OEM 7475 Forged Aluminum Alloy Part For Automotive / Airplane / Ship/Auto Parts/Metal Forging Parts
Standard : JIS, DIN, BS, ASTM, SAE
Alloy : 7175
Sample : Can Be Customized
Mould : Can Be Customized
Surface treatment : Anodizing,Plating,Satin,Painting,Powder Coating,Anodized etc
Process : Forging/Forged
OEM 7475 Forged Aluminum Alloy Part For Automotive/ Airplane/ Ship/Auto Parts/Metal Forging Parts
Product Details
| Material | Aluminum Alloy 7475 |
| 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 Need |
| MOQ | 1pcs |
| Sample | Can be Customized |
| Mold | Can be Customized |
| Lead Time | Mold for 15-20Days Process for 15-20Days |
| OEM | Can be Customized |
| Chemical Composition of 7475 | |||||||||||||
| Alloy | Si | Fe | Cu | Mn | Mg | Cr | Zn | Ti | Others | Al | |||
| Each | Total | ||||||||||||
| 7475 | 0.10max | 0.12max | 1.2-1.9 | 0.06max | 1.9-2.6 | 0.18-0.25 | 5.2-6.2 | 0.06max | 0.05 | 0.15 | Rest | ||
Technical Specifications of 7475-T7651
| Physical Properties | Metric | English | Comments |
| Density | 2.81 g/cc | 0.102 lb/in³ | AA; Typical |
Mechanical Properties | |||
| Hardness, Brinell | 140 | 140 | 500 kg load with 10 mm ball. Calculated value. |
| Hardness, Knoop | 177 | 177 | Converted from Brinell Hardness Value |
| Hardness, Rockwell A | 51.6 | 51.6 | Converted from Brinell Hardness Value |
| Hardness, Rockwell B | 84 | 84 | Converted from Brinell Hardness Value |
| Hardness, Vickers | 162 | 162 | Converted from Brinell Hardness Value |
| Ultimate Tensile Strength | 531 MPa | 77000 psi | AA; Typical |
| Tensile Yield Strength | 462 MPa | 67000 psi | AA; Typical |
| Elongation at Break | 12 % | 12 % | AA; Typical; 1/2 in. (12.7 mm) Diameter |
| Modulus of Elasticity | 71.7 GPa | 10400 ksi | AA; Typical; Average of tension and compression. The compression modulus is about 2% greater than tensile modulus. |
| Poisson's Ratio | 0.33 | 0.33 | |
| Machinability | 70 % | 70 % | 0-100 Scale of Aluminum Alloys |
| Shear Modulus | 27 GPa | 3920 ksi | |
| Shear Strength | 310 MPa | 45000 psi | Calculated value. |
Electrical Properties | |||
| Electrical Resistivity | 4.31e-006 ohm-cm | 4.31e-006 ohm-cm | |
Thermal Properties | |||
| CTE, linear 68°F | 23.2 µm/m-°C | 12.9 µin/in-°F | AA; Typical; Average over 68-212°F range. |
| CTE, linear 250°C | 25.2 µm/m-°C | 14 µin/in-°F | Average over the range 20-300ºC |
| Specific Heat Capacity | 0.88 J/g-°C | 0.21 BTU/lb-°F | Estimated from trends in similar Al alloys. |
| Thermal Conductivity | 163 W/m-K | 1130 BTU-in/hr-ft²-°F | |
| Melting Point | 477 - 635 °C | 890 - 1175 °F | AA; Typical range based on typical composition for wrought products 1/4 inch thickness or greater |
| Solidus | 477 °C | 890 °F | AA; Typical |
| Liquidus | 635 °C | 1175 °F | AA; Typical |
Processing Properties | |||
| Annealing Temperature | 413 °C | 775 °F | |
| Solution Temperature | 516 °C | 960 °F | must be preceded by a soak at 870 to 890°F |
| Aging Temperature | 121 - 177 °C | 250 - 350 °F | |


Surface Available

Application

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OEM 7475 Forged Aluminum Alloy Part For Automotive / Airplane/ Ship Metal Forging Parts Images |