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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

MOQ: 1PCS
Price: Negotiations
Standard Packaging: wooden pallet
Delivery Period: 10~20days
Payment Method: T/T, L/C
Supply Capacity: 10000 pcs /per month
Detail Information
Place of Origin
CHINA
Brand Name
JIMA
Certification
ISO9001-2008,SGS,ROHS.
Model Number
ALP
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
Highlight:

2A12 Forged Aluminum Alloy Part

,

OEM Forging Metal Parts

,

Ordnance Aluminum Alloy Part

Product Description

 

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


Product Details

 

Material Aluminum Alloy 2024/2A12
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 2024/2A12
Alloy Si Fe Cu Mn Mg Cr Zn Ti Others Al
Each Total
2024/2A12 0.5 0.5 3.8-4.9 0.3-0.9 1.2-1.8 0.10 0.25 0.15 0.05 0.15 Rest

 

Material properties 2024/2A12 Aluminum alloy
Yield strength 483 MPa
Modulus of Elasticity 73.1 GPa
Thermal conductivity 121-202 W/(m·K)
Melting point 500 - 650°C
Hardness (Brinell) 120-150HB
Machinability Good

 

 

Physical property Value
Tensile strength MPA 470
0.2% yield strength Mpa 325
Elongation (%) 10
Fatigue strength 105
Conductivity 20℃ 30
20℃ resistivity nΩ.m 48
Elastic modulus GPa 68

 

Physical property Value
2024 H112 aluminum sheet plate HB 85
2024 T4 aluminum sheet plate HB 120~145
2024 T351 aluminum sheet plate HB 120~145
2024 O aluminium sheet HB 40

 

 

Properties Metric English Comments
Density 2.78 g/cc 0.1 lb/in³ AA; Typical
Mechanical Properties
Hardness, Brinell 120 120 AA; Typical; 500 g load; 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
Ultimate Tensile Strength 469 MPa 68000 psi AA; Typical
Tensile Yield Strength 324 MPa 47000 psi AA; Typical
Elongation at Break 19 % 19 % AA; Typical; 1/2 in. (12.7 mm) Diameter
Elongation at Break 20 % 20 % AA; Typical; 1/16 in. (1.6 mm) Thickness
Modulus of Elasticity 73.1 GPa 10600 ksi AA; Typical; Average of tension and compression. The compression modulus is about 2% greater than the tensile modulus.
Ultimate Bearing Strength 814 MPa 118000 psi Edge distance/pin diameter = 2.0
Bearing Yield Strength 441 MPa 64000 psi Edge distance/pin diameter = 2.0
Poisson's Ratio 0.33 0.33  
Fatigue Strength 138 MPa 20000 psi AA; 500,000,000 cycles completely reversed stress; RR Moore machine/specimen
Fracture Toughness 26 MPa-m½ 23.7 ksi-in½ K(IC) in S-L Direction
Fracture Toughness 32 MPa-m½ 29.1 ksi-in½ K(IC) in T-L Direction
Fracture Toughness 37 MPa-m½ 33.7 ksi-in½ K(IC) in L-T Direction
Machinability 70 % 70 % 0-100 Scale of Aluminum Alloys
Shear Modulus 28 GPa 4060 ksi  
Shear Strength 283 MPa 41000 psi AA; Typical
Electrical Properties
Electrical Resistivity 5.82e-006 ohm-cm 5.82e-006 ohm-cm AA; Typical at 68°F
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 24.7 µm/m-°C 13.7 µin/in-°F Average over the range 20-300ºC
Specific Heat Capacity 0.875 J/g-°C 0.209 BTU/lb-°F  
Thermal Conductivity 121 W/m-K 840 BTU-in/hr-ft²-°F AA; Typical at 77°F
Melting Point 502 - 638 °C 935 - 1180 °F AA; Typical range based on typical composition for wrought products 1/4 inch thickness or greater. Eutectic melting is not eliminated by homogenization.
Solidus 502 °C 935 °F AA; Typical
Liquidus 638 °C 1180 °F AA; Typical
Processing Properties
Annealing Temperature 413 °C 775 °F  
Solution Temperature 256 °C 493 °F  

 

 

Product Show

 

OEM 2024/2A12 Forged Aluminum Alloy Part For Automotive / Airplane / Wheel / Ordnance/Auto Parts/Metal Forging Parts 0

 

OEM 2024/2A12 Forged Aluminum Alloy Part For Automotive / Airplane / Wheel / Ordnance/Auto Parts/Metal Forging Parts 1

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

 

Application

 

OEM 2024/2A12 Forged Aluminum Alloy Part For Automotive / Airplane / Wheel / Ordnance/Auto Parts/Metal Forging Parts 3

OEM 2024/2A12 Forged Aluminum Alloy Part For Automotive / Airplane / Wheel / Ordnance/Auto Parts/Metal Forging Parts 4

 

 

products
PRODUCTS DETAILS
OEM 2024/2A12 Forged Aluminum Alloy Part For Automotive / Airplane / Wheel / Ordnance/Auto Parts/Metal Forging Parts
MOQ: 1PCS
Price: Negotiations
Standard Packaging: wooden pallet
Delivery Period: 10~20days
Payment Method: T/T, L/C
Supply Capacity: 10000 pcs /per month
Detail Information
Place of Origin
CHINA
Brand Name
JIMA
Certification
ISO9001-2008,SGS,ROHS.
Model Number
ALP
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
Minimum Order Quantity:
1PCS
Price:
Negotiations
Packaging Details:
wooden pallet
Delivery Time:
10~20days
Payment Terms:
T/T, L/C
Supply Ability:
10000 pcs /per month
Highlight

2A12 Forged Aluminum Alloy Part

,

OEM Forging Metal Parts

,

Ordnance Aluminum Alloy Part

Product Description

 

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


Product Details

 

Material Aluminum Alloy 2024/2A12
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 2024/2A12
Alloy Si Fe Cu Mn Mg Cr Zn Ti Others Al
Each Total
2024/2A12 0.5 0.5 3.8-4.9 0.3-0.9 1.2-1.8 0.10 0.25 0.15 0.05 0.15 Rest

 

Material properties 2024/2A12 Aluminum alloy
Yield strength 483 MPa
Modulus of Elasticity 73.1 GPa
Thermal conductivity 121-202 W/(m·K)
Melting point 500 - 650°C
Hardness (Brinell) 120-150HB
Machinability Good

 

 

Physical property Value
Tensile strength MPA 470
0.2% yield strength Mpa 325
Elongation (%) 10
Fatigue strength 105
Conductivity 20℃ 30
20℃ resistivity nΩ.m 48
Elastic modulus GPa 68

 

Physical property Value
2024 H112 aluminum sheet plate HB 85
2024 T4 aluminum sheet plate HB 120~145
2024 T351 aluminum sheet plate HB 120~145
2024 O aluminium sheet HB 40

 

 

Properties Metric English Comments
Density 2.78 g/cc 0.1 lb/in³ AA; Typical
Mechanical Properties
Hardness, Brinell 120 120 AA; Typical; 500 g load; 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
Ultimate Tensile Strength 469 MPa 68000 psi AA; Typical
Tensile Yield Strength 324 MPa 47000 psi AA; Typical
Elongation at Break 19 % 19 % AA; Typical; 1/2 in. (12.7 mm) Diameter
Elongation at Break 20 % 20 % AA; Typical; 1/16 in. (1.6 mm) Thickness
Modulus of Elasticity 73.1 GPa 10600 ksi AA; Typical; Average of tension and compression. The compression modulus is about 2% greater than the tensile modulus.
Ultimate Bearing Strength 814 MPa 118000 psi Edge distance/pin diameter = 2.0
Bearing Yield Strength 441 MPa 64000 psi Edge distance/pin diameter = 2.0
Poisson's Ratio 0.33 0.33  
Fatigue Strength 138 MPa 20000 psi AA; 500,000,000 cycles completely reversed stress; RR Moore machine/specimen
Fracture Toughness 26 MPa-m½ 23.7 ksi-in½ K(IC) in S-L Direction
Fracture Toughness 32 MPa-m½ 29.1 ksi-in½ K(IC) in T-L Direction
Fracture Toughness 37 MPa-m½ 33.7 ksi-in½ K(IC) in L-T Direction
Machinability 70 % 70 % 0-100 Scale of Aluminum Alloys
Shear Modulus 28 GPa 4060 ksi  
Shear Strength 283 MPa 41000 psi AA; Typical
Electrical Properties
Electrical Resistivity 5.82e-006 ohm-cm 5.82e-006 ohm-cm AA; Typical at 68°F
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 24.7 µm/m-°C 13.7 µin/in-°F Average over the range 20-300ºC
Specific Heat Capacity 0.875 J/g-°C 0.209 BTU/lb-°F  
Thermal Conductivity 121 W/m-K 840 BTU-in/hr-ft²-°F AA; Typical at 77°F
Melting Point 502 - 638 °C 935 - 1180 °F AA; Typical range based on typical composition for wrought products 1/4 inch thickness or greater. Eutectic melting is not eliminated by homogenization.
Solidus 502 °C 935 °F AA; Typical
Liquidus 638 °C 1180 °F AA; Typical
Processing Properties
Annealing Temperature 413 °C 775 °F  
Solution Temperature 256 °C 493 °F  

 

 

Product Show

 

OEM 2024/2A12 Forged Aluminum Alloy Part For Automotive / Airplane / Wheel / Ordnance/Auto Parts/Metal Forging Parts 0

 

OEM 2024/2A12 Forged Aluminum Alloy Part For Automotive / Airplane / Wheel / Ordnance/Auto Parts/Metal Forging Parts 1

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

 

Application

 

OEM 2024/2A12 Forged Aluminum Alloy Part For Automotive / Airplane / Wheel / Ordnance/Auto Parts/Metal Forging Parts 3

OEM 2024/2A12 Forged Aluminum Alloy Part For Automotive / Airplane / Wheel / Ordnance/Auto Parts/Metal Forging Parts 4