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Brand Name : JIMA
Model Number : ALP
Certification : ISO9001-2008,SGS,ROHS.
Place of Origin : CHINA
MOQ : 1PCS
Price : Negotiations
Payment Terms : T/T, L/C
Supply Ability : 10000 pcs /per month
Delivery Time : 15~30days
Packaging Details : Standard Export Wooden Pallet
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
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; |
| Manufacture Ability | Depends on The Complexity Of Different Products And Quantities |
| Experience | Aluminum Machining Service for 12 Years |
| Packaging | Standard Export Wooden Pallets |
| 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 | Al | |||
| Each | Total | ||||||||||||
| 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 | Original Value | Comments |
| Density | 2.71 g/cc | AA; Typical |
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| Mechanical Properties | Original 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 MPa | Rolled rings; Radial; T6 and T652 |
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| 303 MPa | Die forgings; Axis parallel to grain flow |
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| 303 MPa | Die forgings; Axis not parallel to grain flow |
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| 303 MPa | Rolled rings; Tangential; T6 and T652 |
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| 303 MPa | Rolled rings; Axial; T6 and T652 |
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| 330 MPa |
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| 28.0 MPa |
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| 34.0 MPa |
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| 45.0 MPa |
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| 95.0 MPa |
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| 195 MPa |
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| 295 MPa |
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| 330 MPa |
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| 340 MPa |
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| 345 MPa |
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| 395 MPa |
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| Tensile Strength, Yield | 241 MPa | Rolled rings; Axial; T6 and T652 |
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| 241 MPa | Rolled rings; Radial; T6 and T652 |
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| 255 MPa | Die forgings; Axis parallel to grain flow |
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| 255 MPa | Die forgings; Axis not parallel to grain flow |
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| 255 MPa | Rolled rings; Tangential; T6 and T652 |
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| 295 MPa |
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| 22.0 MPa |
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| 27.0 MPa |
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| 34.0 MPa |
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| 85.0 MPa |
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| 185 MPa |
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| 275 MPa |
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| 298 MPa |
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| 310 MPa |
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| 315 MPa |
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| 345 MPa |
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| Elongation at Break | 2.0 % | Rolled rings; Radial; T6 and T652 |
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| 4.0 % | Rolled rings; Axial; T6 and T652 |
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| 5.0 % | Rolled rings; Tangential; T6 and T652 |
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| 6.0 % | Die forgings; Axis not parallel to grain flow |
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| 10 % | Die forgings; Axis parallel to grain flow |
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| 17 % |
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| 17 % |
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| 17 % |
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| 17 % |
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| 20 % |
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| 20 % |
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| 30 % |
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| 35 % |
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| 43 % |
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| 50 % |
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| 17 % | In 5 cm |
| Modulus of Elasticity | 69.0 GPa | Average of Tension and Compression. In Al alloys, the compressive modulus is typically 2% greater than the tensile modulus. Estimated from trends in similar Al alloys. |
| Poissons Ratio | 0.33 | Estimated from trends in similar Al alloys. |
| Fatigue Strength | 85.0 MPa |
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| Shear Modulus | 26.0 GPa | Estimated from similar Al alloys. |
| Shear Strength | 220 MPa |
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| Electrical Properties | Original Value | Comments |
| Electrical Resistivity | 23.0 ohm-cir-mil/ft | AA; Typical |
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| Thermal Properties | Original Value | Comments |
| CTE, linear | 12.9 µin/in-°F | AA; Typical; average over range |
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| 21.8 µm/m-°C |
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| 23.0 µm/m-°C |
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| 24.1 µm/m-°C |
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| 25.0 µm/m-°C |
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| Specific Heat Capacity | 0.895 J/g-°C |
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| Thermal Conductivity | 1190 BTU-in/hr-ft²-°F | AA; Typical at 77°F |
| Melting Point | 1090 - 1200 °F | AA; Typical range based on typical composition for wrought products >= 1/4 in. thickness. Eutectic melting can be eliminated by homogenization. |
| Solidus | 1090 °F | AA; Typical |
| Liquidus | 1200 °F | AA; Typical |
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| Processing Properties | Original 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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Product Show


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