Name: OEM 7475 Forged Aluminum Alloy Part For Automotive / Airplane/ Ship Metal Forging Parts
Brand: JimaFor
SKU: ALP
Availability: InStock

MOQ:	1PCS
Price:	Negotiations
Standard Packaging:	Wooden Pallet
Delivery Period:	10~20days
Payment Method:	T/T, L/C
Supply Capacity:	10000 pcs /per month

Details Information

Product Description

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

Others

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

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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

Product Description

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

Others

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

Tags: