US2019316232A1PendingUtilityA1
Lower wing skin metal with improved damage tolerance properties
Est. expirySep 30, 2033(~7.2 yrs left)· nominal 20-yr term from priority
Inventors:Bernard Bes
C22F 1/04C22C 21/12B64C 3/26C22C 21/16C22F 1/057B22D 27/20C22C 21/14B22D 21/007
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Claims
Abstract
The invention relates to a rolled product with state T351, having thickness of between 15 and 50 mm, made from aluminium alloy having the following composition, in % by weight, Cu: 3.85-4.15; Mg: 0.95-1.25; Mn: 0.45-0.57; Zr: 0.09-0.16; Ti: 0.005-0.1; Fe: <0.070; Si: <0.060; with Cu+Mg≤5.15; other lesser elements 0.05 each and less than 0.15 in total, the remainder being aluminium.
Claims
exact text as granted — not AI-modified1 . A manufacturing process for a rolled product in T351 temper, comprising:
preparing and casting an aluminum alloy of thickness from 15 to 50 mm comprising, as a percentage by weight, Cu: 3.85-4.15, Mg: 0.95-1.25, Mn: 0.45-0.57, Zr: 0.09-0.16, Ti: 0.005-0.1, Fe: <0.070, Si: <0.060, with Cu+Mg 5≤5.15, other elements <0.05 each and less than 0.15 in total, the remainder being aluminum; adding a grain-refining agent of AlTiB type to obtain a rolling slab; optionally homogenizing said slab at a temperature from 480° C. to 510° C.; optionally hot rolling said homogenized slab to obtain a plate of thickness e from 15 to 50 mm; solution heat treating said plate at a temperature from 480 to 505° C. for a time t in hours such that t≥e/7; quenching said solution heat treated plate; cold stretching said quenched plate with a deformation of from 1.5 to 3%; and carrying out natural aging at room temperature.
2 . The process according to claim 1 , wherein said solution heat treatment is performed at a temperature from 495° C. to 505° C.
3 . The process according to claim 2 , wherein said time t is such that t≤e/t≤4.5.
4 . The process according to claim 2 , wherein said time t is such that t≤e/5.0.
5 . The process according to claim 2 , wherein said time t is such that t≤e/5.5.
6 . The method according to claim 1 , wherein hot rolling is performed.
7 . The method according to claim 6 , wherein an average temperature during hot rolling to thickness 60 mm is at least 450° C.
8 . The method according to claim 6 , wherein during hot rolling, an outgoing temperature is at least 410° C.
9 . The method according to claim 1 , wherein homogenizing is performed.
10 . The method according to claim 6 , wherein homogenizing is performed.
11 . The method according to claim 9 , wherein homogenizing occurs at a temperature in a range from 480 to 510° C.
12 . The method according to claim 9 , wherein homogenizing occurs at a temperature in a range from 490 to 508° C.
13 . The method according to claim 1 , wherein thickness e is in a range from 20 to 40 mm.
14 . The method according to claim 1 , wherein the plate has a ratio of UTS(L) to TYS(L) at 0.2% elongation greater than 1.25.
15 . The method according to claim 14 , wherein the ratio is greater than 1.30.
16 . The method according to claim 14 , wherein TYS(L) at 0.2% elongation is at least 350 MPa.
17 . The method according to claim 14 , wherein TYS(L) at 0.2% elongation is at least 365 MPa.
18 . An aluminum rolled product in T351 temper, prepared by the process according to claim 1 .
19 . An aluminum rolled product in T351 temper, prepared by the process according to claim 10 .
20 . The aluminum rolled product of claim 18 , wherein TYS(L) at 0.2% elongation is at least 350 MPa.Cited by (0)
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