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OEM 7050 Forging Aluminum Parts For High Stress Component / Forging Metal Spare Parts

OEM 7050 Forging Aluminum Parts For High Stress Component / Forging Metal Spare Parts

MOQ: 1PCS
Price: Negotiations
Standard Packaging: Standard Export Wooden Pallet
Delivery Period: 15~30days
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:
Automotive/Railway/Aerospace
Name:
OEM 7050 Forging Aluminum Parts For High Stress Component /Forging Metal Parts/Forging Spare Parts
Standard:
JIS, DIN, BS, ASTM, SAE.
Alloy:
7050
Surface Treatment:
Anodizing,Plating,Satin,Painting,Powder Coating,Anodized Etc
Process:
Forging/Forged
Mold:
Can Be Customized
Sample:
Can Be Customized
Highlight:

7050 Forging Aluminum Metal Parts

,

OEM Aluminum Forging Spare Parts

,

Anodizing Forging Aluminum Parts

Product Description

 

OEM 7050 Forging Aluminum Parts For High-Stress Component /Forging Metal Parts/Forging Spare Parts

 

Product Details

 

Material

Aluminum Alloy 7050

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 Needs

MOQ

1pcs

Sample

Can Be Customized

Mold

Can Be Customized

Lead Time

Mold for 15-20 Days

Process for 15-20 Days

OEM

Can Be Customized

 

Chemical Composition of 7050

Alloy

Si

Fe

Cu

Mn

Mg

Cr

Zn

Ti

Zr

Others

Al

Each

Total

7050

0.12max

0.15max

2.00-2.60

0.10max

1.90-2.60

0.04max

5.70-6.70

0.06max

0.08-0.15

0.05max

0.15max

Rest

 

 

Technical Specifications of 7050-T7451

 

Physical Properties

Metric

English

Comments

Density

2.83 g/cc

0.102 lb/in³

AA; Typical

 

Mechanical Properties

Metric

English

Comments

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

Tensile Strength, Ultimate

524 MPa

76000 psi

AA; Typical

Tensile Strength, Yield

469 MPa

68000 psi

AA; Typical

Elongation at Break

11 %
@Diameter 12.7 mm

11 %
@Diameter 0.500 in

AA; Typical

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.

Poissons Ratio

0.33

0.33

 

Fracture Toughness

>= 22.0 MPa-m½

>= 20.0 ksi-in½

S-L

 

>= 24.2 MPa-m½

>= 22.0 ksi-in½

T-L

 

>= 26.4 MPa-m½

>= 24.0 ksi-in½

L-T

 

28.0 MPa-m½

25.5 ksi-in½

K(IC) in S-L Direction

 

28.6 MPa-m½

26.0 ksi-in½

average; S-L

 

29.7 MPa-m½

27.0 ksi-in½

average; T-L

 

31.0 MPa-m½

28.2 ksi-in½

K(IC) in T-L Direction

 

35.0 MPa-m½

31.9 ksi-in½

K(IC) in L-T Direction

 

35.2 MPa-m½

32.0 ksi-in½

average; L-T

Shear Modulus

26.9 GPa

3900 ksi

 

Shear Strength

303 MPa

44000 psi

AA; Typical

 

Electrical Properties

Metric

English

Comments

Electrical Resistivity

0.00000430 ohm-cm

0.00000430 ohm-cm

 

 

Thermal Properties

Metric

English

Comments

CTE, linear OEM 7050 Forging Aluminum Parts For High Stress Component / Forging Metal Spare Parts 0

21.7 µm/m-°C
@Temperature -50.0 - 20.0 °C

12.1 µin/in-°F
@Temperature -58.0 - 68.0 °F

 

 

23.0 µm/m-°C
@Temperature 20.0 - 100 °C

12.8 µin/in-°F
@Temperature 68.0 - 212 °F

AA; Typical; average over range

 

23.5 µm/m-°C
@Temperature 20.0 - 100 °C

13.1 µin/in-°F
@Temperature 68.0 - 212 °F

 

 

24.4 µm/m-°C
@Temperature 20.0 - 200 °C

13.6 µin/in-°F
@Temperature 68.0 - 392 °F

 

 

25.4 µm/m-°C
@Temperature 20.0 - 300 °C

14.1 µin/in-°F
@Temperature 68.0 - 572 °F

 

Specific Heat Capacity

0.860 J/g-°C

0.206 BTU/lb-°F

 

Thermal Conductivity

157 W/m-K

1090 BTU-in/hr-ft²-°F

 

Melting Point

488 - 629.4 °C

910 - 1165 °F

AA; Typical range based on typical composition for wrought products >= 1/4 in. thickness

Solidus

488 °C

910 °F

AA; Typical

Liquidus

629.4 °C

1165 °F

AA; Typical

 

Processing Properties

Metric

English

Comments

Annealing Temperature

413 °C

775 °F

 

Solution Temperature

477 °C

890 °F

 

Aging Temperature

121 - 177 °C

250 - 350 °F

 

 

 

Product Show

 

OEM 7050 Forging Aluminum Parts For High Stress Component / Forging Metal Spare Parts 1

OEM 7050 Forging Aluminum Parts For High Stress Component / Forging Metal Spare Parts 2

 

OEM 7050 Forging Aluminum Parts For High Stress Component / Forging Metal Spare Parts 3

 

 

products
PRODUCTS DETAILS
OEM 7050 Forging Aluminum Parts For High Stress Component / Forging Metal Spare Parts
MOQ: 1PCS
Price: Negotiations
Standard Packaging: Standard Export Wooden Pallet
Delivery Period: 15~30days
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:
Automotive/Railway/Aerospace
Name:
OEM 7050 Forging Aluminum Parts For High Stress Component /Forging Metal Parts/Forging Spare Parts
Standard:
JIS, DIN, BS, ASTM, SAE.
Alloy:
7050
Surface Treatment:
Anodizing,Plating,Satin,Painting,Powder Coating,Anodized Etc
Process:
Forging/Forged
Mold:
Can Be Customized
Sample:
Can Be Customized
Minimum Order Quantity:
1PCS
Price:
Negotiations
Packaging Details:
Standard Export Wooden Pallet
Delivery Time:
15~30days
Payment Terms:
T/T, L/C
Supply Ability:
10000 pcs /per month
Highlight

7050 Forging Aluminum Metal Parts

,

OEM Aluminum Forging Spare Parts

,

Anodizing Forging Aluminum Parts

Product Description

 

OEM 7050 Forging Aluminum Parts For High-Stress Component /Forging Metal Parts/Forging Spare Parts

 

Product Details

 

Material

Aluminum Alloy 7050

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 Needs

MOQ

1pcs

Sample

Can Be Customized

Mold

Can Be Customized

Lead Time

Mold for 15-20 Days

Process for 15-20 Days

OEM

Can Be Customized

 

Chemical Composition of 7050

Alloy

Si

Fe

Cu

Mn

Mg

Cr

Zn

Ti

Zr

Others

Al

Each

Total

7050

0.12max

0.15max

2.00-2.60

0.10max

1.90-2.60

0.04max

5.70-6.70

0.06max

0.08-0.15

0.05max

0.15max

Rest

 

 

Technical Specifications of 7050-T7451

 

Physical Properties

Metric

English

Comments

Density

2.83 g/cc

0.102 lb/in³

AA; Typical

 

Mechanical Properties

Metric

English

Comments

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

Tensile Strength, Ultimate

524 MPa

76000 psi

AA; Typical

Tensile Strength, Yield

469 MPa

68000 psi

AA; Typical

Elongation at Break

11 %
@Diameter 12.7 mm

11 %
@Diameter 0.500 in

AA; Typical

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.

Poissons Ratio

0.33

0.33

 

Fracture Toughness

>= 22.0 MPa-m½

>= 20.0 ksi-in½

S-L

 

>= 24.2 MPa-m½

>= 22.0 ksi-in½

T-L

 

>= 26.4 MPa-m½

>= 24.0 ksi-in½

L-T

 

28.0 MPa-m½

25.5 ksi-in½

K(IC) in S-L Direction

 

28.6 MPa-m½

26.0 ksi-in½

average; S-L

 

29.7 MPa-m½

27.0 ksi-in½

average; T-L

 

31.0 MPa-m½

28.2 ksi-in½

K(IC) in T-L Direction

 

35.0 MPa-m½

31.9 ksi-in½

K(IC) in L-T Direction

 

35.2 MPa-m½

32.0 ksi-in½

average; L-T

Shear Modulus

26.9 GPa

3900 ksi

 

Shear Strength

303 MPa

44000 psi

AA; Typical

 

Electrical Properties

Metric

English

Comments

Electrical Resistivity

0.00000430 ohm-cm

0.00000430 ohm-cm

 

 

Thermal Properties

Metric

English

Comments

CTE, linear OEM 7050 Forging Aluminum Parts For High Stress Component / Forging Metal Spare Parts 0

21.7 µm/m-°C
@Temperature -50.0 - 20.0 °C

12.1 µin/in-°F
@Temperature -58.0 - 68.0 °F

 

 

23.0 µm/m-°C
@Temperature 20.0 - 100 °C

12.8 µin/in-°F
@Temperature 68.0 - 212 °F

AA; Typical; average over range

 

23.5 µm/m-°C
@Temperature 20.0 - 100 °C

13.1 µin/in-°F
@Temperature 68.0 - 212 °F

 

 

24.4 µm/m-°C
@Temperature 20.0 - 200 °C

13.6 µin/in-°F
@Temperature 68.0 - 392 °F

 

 

25.4 µm/m-°C
@Temperature 20.0 - 300 °C

14.1 µin/in-°F
@Temperature 68.0 - 572 °F

 

Specific Heat Capacity

0.860 J/g-°C

0.206 BTU/lb-°F

 

Thermal Conductivity

157 W/m-K

1090 BTU-in/hr-ft²-°F

 

Melting Point

488 - 629.4 °C

910 - 1165 °F

AA; Typical range based on typical composition for wrought products >= 1/4 in. thickness

Solidus

488 °C

910 °F

AA; Typical

Liquidus

629.4 °C

1165 °F

AA; Typical

 

Processing Properties

Metric

English

Comments

Annealing Temperature

413 °C

775 °F

 

Solution Temperature

477 °C

890 °F

 

Aging Temperature

121 - 177 °C

250 - 350 °F

 

 

 

Product Show

 

OEM 7050 Forging Aluminum Parts For High Stress Component / Forging Metal Spare Parts 1

OEM 7050 Forging Aluminum Parts For High Stress Component / Forging Metal Spare Parts 2

 

OEM 7050 Forging Aluminum Parts For High Stress Component / Forging Metal Spare Parts 3