OEM 6151 Aluminum Metal Parts For Airplane Engine Box Metal Aluminum Forging Part
Price:
Negotiations
MOQ:
1PCS
Delivery Time:
15~30days
Brand:
JIMA
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 |
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Company
JimaFor
Location
No.60 Guoxia Road, Yangpu District, Shanghai,China.
Contact Person
Annie