US2011108170A1PendingUtilityA1
Method of preparation prior to the welding of lithium-aluminium alloy products
Est. expiryJul 7, 2028(~2 yrs left)· nominal 20-yr term from priority
B23K 9/23C21D 1/72B23K 15/0093B23K 31/02B23K 9/235Y10T428/12764C22F 1/04C22C 21/00C21D 1/68B23K 2103/10B23K 26/60B32B 15/016B23K 26/32B23K 11/185B23K 11/34B23K 15/0033
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Claims
Abstract
The present invention relates to aluminum-lithium alloys in general and, in particular, such products as used in the aircraft industry and the welding of these.
Claims
exact text as granted — not AI-modified1 . Process for preparing an aluminum lithium alloy product to be fusion-welded comprising:
(i) procuring a hot-worked aluminum alloy product including at least 0.8% of lithium by weight, (ii) optionally cold-working the product so obtained, (iii) cleaning at least one surface to be welded of the product so obtained, (iv) covering at least one cleaned surface of the product so obtained with a coating whose characteristics when dry are a quantity ranging from 0.1 to 5 mg/cm 2 and a fluorine concentration of at least 10% by weight, (v) performing a solution heat-treatment at a temperature greater than approximately 450° C. followed by quenching of the product so obtained.
2 . Process according to the claim 1 in which said aluminum lithium alloy comprises at least 1.4% of lithium by weight.
3 . Process according to claim 2 in which said aluminum lithium alloy is selected from the group consisting of alloys 2090, 2091, 2196, 2097, 2197, 2297, 2397, 2099, 2199, 8090, 8091, and 8093.
4 . Process according to claim 1 in which the hot-worked and optionally cold-worked product is a flat-rolled or extruded product with thickness lower than 5 mm.
5 . Process according to claim 1 in which the cleaning of (iii) is carried out by treating with an aqueous solution with a pH greater than 9.
6 . Process according to claim 1 in which (iii) and (iv) are carried out on the majority of, or optionally on the whole, surface of said product.
7 . Process according to claim 1 in which said coating comprises a binder whose concentration when dry ranges from 5% to 50% by weight.
8 . Process according to claim 1 in which said coating comprises when dry, as a percentage by weight, from 75% to 95% of NaBF4, from 0 to 15% by weight of carboxymethyl cellulose and from 0 to 15% of a silane.
9 . Process according to claim 1 in which said coating comprises after drying, as a percentage by weight, from 50% to 100% of KxAlyFz, from 0 to 5% by weight of CsxAlyFz and from 0 to 50% of a binder.
10 . Process according to claim 9 in which said binder is an alkyl silicone resin.
11 . Process according to claim 9 in which said coating is deposited by electrostatic powdering.
12 . Fusion-welded assembly between a first aluminum alloy member comprising at least 1.4% of lithium by weight and at least one second metal alloy member, said first member being a flat-rolled or extruded product of a thickness less than 5 mm, the first member having been prepared by the process according to claim 1 wherein a weld between said members is substantially free from porosities.
13 . Welded assembly according to claim 12 in which the thickness tolerance of said first member is plus or minus 0.20 mm.
14 . Welded assembly according to claim 12 including at least one second aluminum alloy member including at least 0.8% of lithium by weight.
15 . Welded assembly according to claim 12 in which said first member is an extruded section and said second member is a sheet or an extruded section.
16 . Fuselage panel including a welded assembly according to claim 14 .
17 . Welded assembly according to claim 12 in which the thickness tolerance of said first member is plus or minus 0.15 mm.
18 . Welded assembly according to claim 12 in which the thickness tolerance of said first member is plus or minus 0.10 mm.
19 . Welded assembly of claim 12 , wherein said first member comprises a flat-rolled or extruded product of a thickness less than 2 mm.Cited by (0)
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