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

Categories Aluminum Forgings
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
Company Info.
JimaFor
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OEM 7475 Forged Aluminum Alloy Part For Automotive / Airplane/ Ship Metal Forging Parts

OEM 7475 Forged Aluminum Alloy Part For Automotive/ Airplane/ Ship/Auto Parts/Metal Forging Parts​

Product Details


MaterialAluminum Alloy 7475
ProcessForging+CNC+Heat Treatment
Surface TreatmentTransparent, Color Anodized, Hard Anodizing, Powder Coating;
Sandblasting, Laser Carving, Silk Screening;
Nickel-Plated, Chrome, Galvanized, Silver/Gold Plating;
Black Oxide Coating; Polishing; etc...
Manufacture AbilityDepends on The Complexity Of Different Products And Quantities
ExperienceAluminum Machining Service for 12 Years
PackagingStandard Export Wooden Pallets
Another Request According to Your Need
MOQ1pcs
SampleCan be Customized
MoldCan be Customized
Lead Time

Mold for 15-20Days

Process for 15-20Days

OEMCan be Customized

Chemical Composition of 7475
AlloySiFeCuMnMgCrZnTiOthersAl
EachTotal
74750.10max0.12max1.2-1.90.06max1.9-2.60.18-0.255.2-6.20.06max0.050.15Rest

Technical Specifications of 7475-T7651


Physical PropertiesMetricEnglishComments
Density2.81 g/cc0.102 lb/in³AA; Typical

Mechanical Properties
Hardness, Brinell140140500 kg load with 10 mm ball. Calculated value.
Hardness, Knoop177177Converted from Brinell Hardness Value
Hardness, Rockwell A51.651.6Converted from Brinell Hardness Value
Hardness, Rockwell B8484Converted from Brinell Hardness Value
Hardness, Vickers162162Converted from Brinell Hardness Value
Ultimate Tensile Strength531 MPa77000 psiAA; Typical
Tensile Yield Strength462 MPa67000 psiAA; Typical
Elongation at Break12 %12 %AA; Typical; 1/2 in. (12.7 mm) Diameter
Modulus of Elasticity71.7 GPa10400 ksiAA; Typical; Average of tension and compression. The compression modulus is about 2% greater than tensile modulus.
Poisson's Ratio0.330.33
Machinability70 %70 %0-100 Scale of Aluminum Alloys
Shear Modulus27 GPa3920 ksi
Shear Strength310 MPa45000 psiCalculated value.

Electrical Properties
Electrical Resistivity4.31e-006 ohm-cm4.31e-006 ohm-cm

Thermal Properties
CTE, linear 68°F23.2 µm/m-°C12.9 µin/in-°FAA; Typical; Average over 68-212°F range.
CTE, linear 250°C25.2 µm/m-°C14 µin/in-°FAverage over the range 20-300ºC
Specific Heat Capacity0.88 J/g-°C0.21 BTU/lb-°FEstimated from trends in similar Al alloys.
Thermal Conductivity163 W/m-K1130 BTU-in/hr-ft²-°F
Melting Point477 - 635 °C890 - 1175 °FAA; Typical range based on typical composition for wrought products 1/4 inch thickness or greater
Solidus477 °C890 °FAA; Typical
Liquidus635 °C1175 °FAA; Typical

Processing Properties
Annealing Temperature413 °C775 °F
Solution Temperature516 °C960 °Fmust be preceded by a soak at 870 to 890°F
Aging Temperature121 - 177 °C250 - 350 °F
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