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OEM 2024/2A12 Forged Aluminum Alloy Part For Automotive / Airplane / Wheel / Ordnance/Auto Parts/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/Truck Hub/Railway Vehicle
Name: OEM 2024/2A12 Forged Aluminum Alloy Part For Automotive / Airplane / Wheel / Ordnance/Auto Parts/Metal Forging Parts
Standard: JIS, DIN, BS, ASTM, SAE
Alloy: 2024/2A12
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 2024/2A12 Forged Aluminum Alloy Part For Automotive / Airplane / Wheel / Ordnance/Auto Parts/Metal Forging Parts


OEM 2024/2A12 Forged Aluminum Alloy Part For Automotive / Airplane / Wheel / Ordnance/Auto Parts/Metal Forging Parts​


Product Details


MaterialAluminum Alloy 2024/2A12
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 2024/2A12
AlloySiFeCuMnMgCrZnTiOthersAl
EachTotal
2024/2A120.50.53.8-4.90.3-0.91.2-1.80.100.250.150.050.15Rest

Material properties2024/2A12 Aluminum alloy
Yield strength483 MPa
Modulus of Elasticity73.1 GPa
Thermal conductivity121-202 W/(m·K)
Melting point500 - 650°C
Hardness (Brinell)120-150HB
MachinabilityGood

Physical propertyValue
Tensile strength MPA470
0.2% yield strength Mpa325
Elongation (%)10
Fatigue strength105
Conductivity 20℃30
20℃ resistivity nΩ.m48
Elastic modulus GPa68

Physical propertyValue
2024 H112 aluminum sheet plate HB85
2024 T4 aluminum sheet plate HB120~145
2024 T351 aluminum sheet plate HB120~145
2024 O aluminium sheet HB40

PropertiesMetricEnglishComments
Density2.78 g/cc0.1 lb/in³AA; Typical
Mechanical Properties
Hardness, Brinell120120AA; Typical; 500 g load; 10 mm ball
Hardness, Knoop150150Converted from Brinell Hardness Value
Hardness, Rockwell A46.846.8Converted from Brinell Hardness Value
Hardness, Rockwell B7575Converted from Brinell Hardness Value
Hardness, Vickers137137Converted from Brinell Hardness Value
Ultimate Tensile Strength469 MPa68000 psiAA; Typical
Tensile Yield Strength324 MPa47000 psiAA; Typical
Elongation at Break19 %19 %AA; Typical; 1/2 in. (12.7 mm) Diameter
Elongation at Break20 %20 %AA; Typical; 1/16 in. (1.6 mm) Thickness
Modulus of Elasticity73.1 GPa10600 ksiAA; Typical; Average of tension and compression. The compression modulus is about 2% greater than the tensile modulus.
Ultimate Bearing Strength814 MPa118000 psiEdge distance/pin diameter = 2.0
Bearing Yield Strength441 MPa64000 psiEdge distance/pin diameter = 2.0
Poisson's Ratio0.330.33
Fatigue Strength138 MPa20000 psiAA; 500,000,000 cycles completely reversed stress; RR Moore machine/specimen
Fracture Toughness26 MPa-m½23.7 ksi-in½K(IC) in S-L Direction
Fracture Toughness32 MPa-m½29.1 ksi-in½K(IC) in T-L Direction
Fracture Toughness37 MPa-m½33.7 ksi-in½K(IC) in L-T Direction
Machinability70 %70 %0-100 Scale of Aluminum Alloys
Shear Modulus28 GPa4060 ksi
Shear Strength283 MPa41000 psiAA; Typical
Electrical Properties
Electrical Resistivity5.82e-006 ohm-cm5.82e-006 ohm-cmAA; Typical at 68°F
Thermal Properties
CTE, linear 68°F23.2 µm/m-°C12.9 µin/in-°FAA; Typical; Average over 68-212°F range.
CTE, linear 250°C24.7 µm/m-°C13.7 µin/in-°FAverage over the range 20-300ºC
Specific Heat Capacity0.875 J/g-°C0.209 BTU/lb-°F
Thermal Conductivity121 W/m-K840 BTU-in/hr-ft²-°FAA; Typical at 77°F
Melting Point502 - 638 °C935 - 1180 °FAA; Typical range based on typical composition for wrought products 1/4 inch thickness or greater. Eutectic melting is not eliminated by homogenization.
Solidus502 °C935 °FAA; Typical
Liquidus638 °C1180 °FAA; Typical
Processing Properties
Annealing Temperature413 °C775 °F
Solution Temperature256 °C493 °F

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