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US 12,116,122 B2Granted
Aluminum-copper-lithium alloy product for a lower wing skin element with improved properties
AssigneeConstellium Issoire
InventorNicolas Bayona-Carrillo
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Abstract
The invention relates to a method for manufacturing a laminated or forged material, the thickness of which is 14 to 100 mm. The materials according to the invention are particularly suitable for manufacturing airplane underwing elements.
Claims18
A rolled and/or forged product having a thickness of between 20 and 100 mm, wherein at mid-thickness the volume fraction of grains having a brass texture is between 25 and 40% and the texture index is between 12 and 18,
- wherein the rolled and/or forged product is produced by a process comprising
- (a) casting a slab of alloy comprising, as a percentage by weight,
- Cu:
- 1.9-2.3
- Li:
- 1.3-1.8
- Mg:
- 0.1-0.5
- Mn:
- <0.05
- Zr:
- 0.10-0.16
- Ag:
- 0-0.5
- Zn:
- <0.20
- Ti:
- 0.01-0.15
- Fe:
- <0.1
- Si:
- ≤0.1
- other elements<0.05 each and <0.15 total, the remainder aluminum with a density less than 2.670 g/cm3,
- (b) homogenizing said slab at 480 to 540° C. for 5 to 60 hours,
- (c) hot working said slab by rolling and/or forging, the hot working conditions being such that a final hot working temperature is at the most 400° C. to obtain a rolled and/or forged product having a thickness of between 20 and 100 mm,
- (d) solution-heat treating said product at 490 to 530° C. for 15 minutes to 8 hours,
- (e) quenching said product with water,
- (f) controlled stretching said product with a permanent deformation of 1 to 6%,
- (g) right after controlled stretching said product, artificially aging said product by heat treatment at 120 to 170° C. for 20 to 60 hours.
26 more elements
Dependencies are inferred from the claim text.