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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 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/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
Highlight:

7475 Forged Aluminum Alloy Part

,

OEM Forged Aluminum Alloy Part

,

Automotive Metal Forging Parts

Product Description

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  
 
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OEM 7475 Forged Aluminum Alloy Part For Automotive / Airplane/ Ship Metal Forging Parts 0

OEM 7475 Forged Aluminum Alloy Part For Automotive / Airplane/ Ship Metal Forging Parts 1

 

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OEM 7475 Forged Aluminum Alloy Part For Automotive / Airplane/ Ship Metal Forging Parts 2

 

Application

 

 

OEM 7475 Forged Aluminum Alloy Part For Automotive / Airplane/ Ship Metal Forging Parts 3

 

 

products
PRODUCTS DETAILS
OEM 7475 Forged Aluminum Alloy Part For Automotive / Airplane/ Ship 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/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
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

7475 Forged Aluminum Alloy Part

,

OEM Forged Aluminum Alloy Part

,

Automotive Metal Forging Parts

Product Description

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  
 
Product Show

 

OEM 7475 Forged Aluminum Alloy Part For Automotive / Airplane/ Ship Metal Forging Parts 0

OEM 7475 Forged Aluminum Alloy Part For Automotive / Airplane/ Ship Metal Forging Parts 1

 

Surface Available

OEM 7475 Forged Aluminum Alloy Part For Automotive / Airplane/ Ship Metal Forging Parts 2

 

Application

 

 

OEM 7475 Forged Aluminum Alloy Part For Automotive / Airplane/ Ship Metal Forging Parts 3