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2017 T4 Aluminum Solid Round Bar High Strength Fair Workability For Aerospace Components
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xProduct Details
| Surface Treatment | Mill Finish | Machining characteristics | Good |
|---|---|---|---|
| Applications | strength structural components, aircraft, machine construction, military equipment, rivets. | Welding | suitable for welding only by resistance welding |
| Workability | Fair | ||
| Fremhæv | aluminium hexagon bar |
||
Product Description
2017 T4 Aluminum Solid Round Bar High Strength Fair Workability For Aerospace Components
Aluminum 2017 is a heat treatable wrought alloy that offers decent strength, ductility, and good machinability. Aluminum 2017 offers more strength than Aluminum 2011, and has fair workability and corrosion resistance.
Aluminum 2017 Applications:
- Aerospace components
- Rivets
- General structural components
- Transportation
- Fasteners
- Screw machine products
- Gauges
- Pulleys
- Needles for knitting
Aluminum 2017 chemical composition that consists of:
- Al 91.5-95.5%
- Cu 3.5-4.5%
- Mn 0.4-1%
- Fe 0.7% max
- Mg 0.4-0.8%
- Zn 0.25% max
- Ti 0.15%
- Cr 0.1%
| Chemical Composition Limits | |||||||||||
| Weight% | Al | Si | Fe | Cu | Mn | Mg | Cr | Zn | Ti | Others Each | Other Total |
| 2017 USA | Rem | 0.20-0.8 | 0.7 max | 3.5-4.5 | 0.40-1.0 | 0.40-0.8 | 0.10 max | 0.25 max | 0.15 max | 0.05 max | 0.15 max |
| Weight% | Al | Si | Fe | Cu | Mn | Mg | Cr | Zn | Zr + Ti | Others Each | Other Total |
| 2017A EAA | Rem | 0.20-0.8 | 0.7 max | 3.5-4.5 | 0.40-1.0 | 0.40-1.0 | 0.10 max | 0.25 max | 0.25 max | 0.05 max | 0.15 max |
Typical Mechanical Properties
| Material | Condition | Tensile Strength (N/mm²) min | Yield Strength | Elongation in 4D % | ||
| ksi | Mpa | ksi | Mpa | |||
| 2017 | 2017-T4 Bar | 55 | 379 | 32 | 221 | 12 |
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