Thin sheets made of aluminium-copper-lithium alloy for aircraft fuselage manufacture
The invention concerns a method for manufacturing a thin sheet made of aluminium-based alloy comprising, in percent by weight, 2.3 to 2.7% Cu, 1.3 to 1.6% Li, 0.2 to 0.5% Mg, 0.1 to 0.5% Mn, 0.01 to 0.15% Ti, a quantity of Zn less than 0.3, a quantity of Fe and of Si less than or equal to 0.1% each, and unavoidable impurities at a content less than or equal to 0.05% by weight each and 0.15% by weight in total, wherein, in particular, the hot-rolling input temperature is between 400° C. and 445° C. and the hot-rolling output temperature is less than 300° C. The sheets according to the invention have advantageous mechanical properties and are used, in particular, for the manufacture of aircraft fuselage panels.
1. A method for manufacturing a thin sheet with a thickness of 4 to 8 mm from an aluminum-based alloy wherein, successively
a) a liquid metal bath is produced, comprising
2.3 to 2.7% by weight Cu,
1.3 to 1.6% by weight Li,
0.2 to 0.5% by weight Mg,
0.1 to 0.5% by weight Mn,
0.01 to 0.15% by weight Ti,
a quantity of Zn of less than 0.3% by weight, a quantity of Fe and Si of less than or equal to 0.1% by weight each, and unavoidable impurities with a content of less than or equal to 0.05% by weight each and 0.15% by weight in total, and a remainder Al,
b) a plate is cast from said liquid metal bath;
c) said plate is homogenized at a temperature of between 490° C. and 535° C.;
d) said plate is rolled by hot rolling into a sheet having a thickness of between 4 and 8 mm, the entry temperature of the hot rolling being between 420° C. and 445° C. and the exit temperature of the hot rolling being between 250° C. and 290° C.;
e) said sheet is solution heat treated at a temperature of between 450° C. and 515° C. and said sheet is quenched;
f) said sheet is stretched in a controlled manner with a permanent deformation of 0.5 to 6%, total cold deformation after solution heat treatment and quenching being less than 15%;
g) aging is carried out, comprising heating at a temperature of between 130° and 170° C. for 5 to 100 hours.
2. The method according to claim 1 , wherein the copper content is between 2.45 and 2.65% by weight.
3. The method according to claim 1 , wherein the lithium content is between 1.35 and 1.55% by weight.
4. The method according to claim 1 , wherein the magnesium content is between 0.25 and 0.45% by weight.
5. The method according to claim 1 , wherein the manganese content is between 0.2 and 0.4% by weight.
6. The method according to claim 1 , wherein the zinc content is less than 0.1% by weight.
7. The method according to claim 1 , wherein the hot-rolling entry temperature is between 420° C. and 440° C. and/or the hot-rolling exit temperature is between 250° C. and 280° C.
8. The method according to claim 1 , wherein the liquid metal bath comprises:
2.45 to 2.65% by weight Cu,
1.35 to 1.55% by weight Li,
0.25 to 0.45% by weight Mg,
0.2 to 0.4% by weight Mn,
0.01 to 0.15% by weight Ti,
a quantity of Zn of less than 0.3% by weight, a quantity of Fe and Si of less than or equal to 0.1% by weight each, and unavoidable impurities with a content of less than or equal to 0.05% by weight each and 0.15% by weight in total, and a remainder Al.
9. The method according to claim 8 , wherein the liquid metal bath comprises:
2.50 to 2.60% by weight Cu,
1.40 to 1.50% by weight Li,
0.25 to 0.35% by weight Mg,
0.25 to 0.35% by weight Mn,
0.01 to 0.15% by weight Ti,
a quantity of Zn of less than 0.3% by weight, a quantity of Fe and Si of less than or equal to 0.1% by weight each, and unavoidable impurities with a content of less than or equal to 0.05% by weight each and 0.15% by weight in total, and a remainder Al.
10. The method according to claim 1 , wherein the hot-rolling exit temperature is between 269° C. and 280° C.
11. The method according to claim 1 , wherein the thin sheet has a yield strength R p0.2 in the TL direction of at least 370 MPa, and a plane strain fracture toughness K R60 , measured on test pieces of the CCT760 type (2ao=253 mm), of at least 170 MPa √m in the T-L direction and in the L-T direction.
12. The method according to claim 1 , wherein g) aging is carried out, comprising heating at a temperature of between 150° C. and 160° C. for 10 to 40 h.