FIELD: nonferrous metallurgy.
SUBSTANCE: invention relates to metallurgy of aluminum alloys, in particular to those containing lithium and copper employed in the form of rolled, pressed, and forged intermediate products for manufacturing load-bearing elements of riveted and welded structures from the field of aircraft and space engineering. Method of invention comprises casting ingots, homogenization, hot deformation at 250-470оС, intermediate annealing, cold deformation, heat treatment into solid solution, hardening and ageing at 100-200оС. Homogenization of ingots is effected in two steps, employing in the first step heating at temperature by 20-60оС and in the second step by 95-120оС higher than temperature Tx, while intermediate annealing in hot deformation operation is effected at temperature by 80-140оС higher than temperature Ty and heat treatment into solid solution effected at temperature by 65-140оС higher than temperature Tx, where Tx is temperature of minimal stability of solid solution in the region of existence of phase T2(Al6CuLi3) and Ty is temperature of minimal stability of solid solution in the region of existence of phase T1(Al2CuLi). In particular embodiments of invention, hot, cold deformation, and intermediate annealing are accomplished in one or more steps and hardening is effected at velocity ≥3.5 Vcrit wherein Vcrit denotes critical hardening velocity.
EFFECT: enabled manufacture of intermediate products with elevated plasticity and high corrosion resistance, fracture resistance, and cyclic crack growth resistance characteristics.
4 cl, 2 tbl
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METHOD OF THERMOMECHANICAL TREATMENT OF SEMI-FINISHED PRODUCTS MADE FROM ALUMINUM ALLOYS | 2004 |
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RU2571993C1 |
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Authors
Dates
2004-10-27—Published
2003-03-12—Filed