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| Categories | Aluminum Forgings |
|---|---|
| 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 |
| Company Info. |
| JimaFor |
| Verified Supplier |
| View Contact Details |
| Product List |
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 |
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 |
303 MPa | Die forgings; Axis parallel to grain flow | |
303 MPa | Die forgings; Axis not parallel to grain flow | |
303 MPa | Rolled rings; Tangential; T6 and T652 | |
303 MPa | Rolled rings; Axial; T6 and T652 | |
330 MPa | ||
28.0 MPa | ||
34.0 MPa | ||
45.0 MPa | ||
95.0 MPa | ||
195 MPa | ||
295 MPa | ||
330 MPa | ||
340 MPa | ||
345 MPa | ||
395 MPa | ||
Tensile Strength, Yield | 241 MPa | Rolled rings; Axial; T6 and T652 |
241 MPa | Rolled rings; Radial; T6 and T652 | |
255 MPa | Die forgings; Axis parallel to grain flow | |
255 MPa | Die forgings; Axis not parallel to grain flow | |
255 MPa | Rolled rings; Tangential; T6 and T652 | |
295 MPa | ||
22.0 MPa | ||
27.0 MPa | ||
34.0 MPa | ||
85.0 MPa | ||
185 MPa | ||
275 MPa | ||
298 MPa | ||
310 MPa | ||
315 MPa | ||
345 MPa | ||
Elongation at Break | 2.0 % | Rolled rings; Radial; T6 and T652 |
4.0 % | Rolled rings; Axial; T6 and T652 | |
5.0 % | Rolled rings; Tangential; T6 and T652 | |
6.0 % | Die forgings; Axis not parallel to grain flow | |
10 % | Die forgings; Axis parallel to grain flow | |
17 % | ||
17 % | ||
17 % | ||
17 % | ||
20 % | ||
20 % | ||
30 % | ||
35 % | ||
43 % | ||
50 % | ||
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 | |
Shear Modulus | 26.0 GPa | Estimated from similar Al alloys. |
Shear Strength | 220 MPa | |
Electrical Properties | Original Value | Comments |
Electrical Resistivity | 23.0 ohm-cir-mil/ft | AA; Typical |
Thermal Properties | Original Value | Comments |
CTE, linear | 12.9 µin/in-°F | AA; Typical; average over range |
21.8 µm/m-°C | ||
23.0 µm/m-°C | ||
24.1 µm/m-°C | ||
25.0 µm/m-°C | ||
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 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 |
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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