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OEM 6151 Aluminum Metal Parts For Airplane Engine Box Metal Aluminum Forging Part

OEM 6151 Aluminum Metal Parts For Airplane Engine Box Metal Aluminum Forging Part

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 6151 Forging Aluminum Parts For Airplane Engine Box/Auto Parts/Metal Forging Part/Aluminum Forging Part
Standard:
JIS, DIN, BS, ASTM, SAE.
Alloy:
6151
Surface Treatment:
Anodizing,Plating,Satin,Painting,Powder Coating,Anodized Etc
Process:
Forging/Forged
Mold:
Can Be Customized
Sample:
Can Be Customized
Highlight:

OEM Forging Aluminum Metal Parts

,

Airplane Engine Box Aluminum Metal Parts

,

6151 Aluminum Metal Parts

Product Description
OEM 6151 Aluminum Metal Parts For Airplane Engine Box Metal Aluminum Forging Part
OEM 6151 Forging Aluminum Parts For Airplane Engine Box/Auto Parts/Metal Forging Part/Aluminum Forging Part
Product Details
Material Aluminum Alloy 6151
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 6151
Alloy Si Fe Cu Mn Mg Cr Zn Ti Others Each Total Al
6151 0.5-1.2 0.10max 0.35max 0.20max 0.45-0.80 0.15-0.35 0.25max 0.15max 0.05max 0.15max Rest
Technical Specifications of 6151-T6
Physical Properties
Property Value Comments
Density 2.71 g/cc AA; Typical
Mechanical Properties
Property Value Comments
Hardness, Brinell 100 500 kg load with 10 mm ball
Hardness, Knoop 126 Converted from Brinell Hardness Number
Hardness, Rockwell A 41.3 Converted from Brinell Hardness Value
Hardness, Rockwell B 63 Converted from Brinell Hardness Value
Hardness, Vickers 112 Converted from Brinell Hardness Value
Tensile Strength, Ultimate 290-395 MPa Various conditions and temperatures
Tensile Strength, Yield 241-345 MPa Various conditions and temperatures
Elongation at Break 2.0-50% Various conditions and temperatures
Modulus of Elasticity 69.0 GPa Average of Tension and Compression
Poissons Ratio 0.33 Estimated from trends in similar Al alloys
Fatigue Strength 85.0 MPa @# of Cycles 5.00e+8
Shear Modulus 26.0 GPa Estimated from similar Al alloys
Shear Strength 220 MPa
Electrical Properties
Property Value Comments
Electrical Resistivity 23.0 ohm-cir-mil/ft @Temperature 20.0 °C; AA; Typical
Thermal Properties
Property Value Comments
CTE, linear 12.9-25.0 µin/in-°F Various temperature ranges
Specific Heat Capacity 0.895 J/g-°C
Thermal Conductivity 1190 BTU-in/hr-ft²-°F AA; Typical at 77°F
Melting Point 1090 - 1200 °F AA; Typical range
Solidus 1090 °F AA; Typical
Liquidus 1200 °F AA; Typical
Processing Properties
Property Value Comments
Annealing Temperature 775 °F hold at temperature 2 to 3 hr; furnace cool to 500°F at 50°F per hour max
Solution Temperature 950 - 975 °F hold at temperature for 4 min, and quench in cold water; for heavy or complicated forgings, quench in water at 150 to 212°F
Aging Temperature 300 - 345 °F hold at temperature 8 to 12 hr
Hot-Working Temperature 500 - 900 °F
Product Showcase
OEM 6151 Aluminum Metal Parts For Airplane Engine Box Metal Aluminum Forging Part 0
OEM 6151 Aluminum Metal Parts For Airplane Engine Box Metal Aluminum Forging Part 1
Products
PRODUCTS DETAILS
OEM 6151 Aluminum Metal Parts For Airplane Engine Box Metal Aluminum Forging Part
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 6151 Forging Aluminum Parts For Airplane Engine Box/Auto Parts/Metal Forging Part/Aluminum Forging Part
Standard:
JIS, DIN, BS, ASTM, SAE.
Alloy:
6151
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

OEM Forging Aluminum Metal Parts

,

Airplane Engine Box Aluminum Metal Parts

,

6151 Aluminum Metal Parts

Product Description
OEM 6151 Aluminum Metal Parts For Airplane Engine Box Metal Aluminum Forging Part
OEM 6151 Forging Aluminum Parts For Airplane Engine Box/Auto Parts/Metal Forging Part/Aluminum Forging Part
Product Details
Material Aluminum Alloy 6151
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 6151
Alloy Si Fe Cu Mn Mg Cr Zn Ti Others Each Total Al
6151 0.5-1.2 0.10max 0.35max 0.20max 0.45-0.80 0.15-0.35 0.25max 0.15max 0.05max 0.15max Rest
Technical Specifications of 6151-T6
Physical Properties
Property Value Comments
Density 2.71 g/cc AA; Typical
Mechanical Properties
Property Value Comments
Hardness, Brinell 100 500 kg load with 10 mm ball
Hardness, Knoop 126 Converted from Brinell Hardness Number
Hardness, Rockwell A 41.3 Converted from Brinell Hardness Value
Hardness, Rockwell B 63 Converted from Brinell Hardness Value
Hardness, Vickers 112 Converted from Brinell Hardness Value
Tensile Strength, Ultimate 290-395 MPa Various conditions and temperatures
Tensile Strength, Yield 241-345 MPa Various conditions and temperatures
Elongation at Break 2.0-50% Various conditions and temperatures
Modulus of Elasticity 69.0 GPa Average of Tension and Compression
Poissons Ratio 0.33 Estimated from trends in similar Al alloys
Fatigue Strength 85.0 MPa @# of Cycles 5.00e+8
Shear Modulus 26.0 GPa Estimated from similar Al alloys
Shear Strength 220 MPa
Electrical Properties
Property Value Comments
Electrical Resistivity 23.0 ohm-cir-mil/ft @Temperature 20.0 °C; AA; Typical
Thermal Properties
Property Value Comments
CTE, linear 12.9-25.0 µin/in-°F Various temperature ranges
Specific Heat Capacity 0.895 J/g-°C
Thermal Conductivity 1190 BTU-in/hr-ft²-°F AA; Typical at 77°F
Melting Point 1090 - 1200 °F AA; Typical range
Solidus 1090 °F AA; Typical
Liquidus 1200 °F AA; Typical
Processing Properties
Property Value Comments
Annealing Temperature 775 °F hold at temperature 2 to 3 hr; furnace cool to 500°F at 50°F per hour max
Solution Temperature 950 - 975 °F hold at temperature for 4 min, and quench in cold water; for heavy or complicated forgings, quench in water at 150 to 212°F
Aging Temperature 300 - 345 °F hold at temperature 8 to 12 hr
Hot-Working Temperature 500 - 900 °F
Product Showcase
OEM 6151 Aluminum Metal Parts For Airplane Engine Box Metal Aluminum Forging Part 0
OEM 6151 Aluminum Metal Parts For Airplane Engine Box Metal Aluminum Forging Part 1
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