Study of the Structure and Properties of Especially Strong Aluminum Alloys of the Al–Zn–Mg–Cu System


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Resumo

Especially strong aluminum alloys of experimental compositions are studied, wt.%: Al – (8.0–9.5) Zn – (1.6–2.2) Mg – (1.2–2.0) Cu – (0.08–0.15) Zr – 0.17 Sc – 0.24 Ag – (0.05–0.07) Ti – (0.03–0.04) Mn – (0.05–0.12) Fe – (0.01–0.02) Si. Heat treatment regimes are selected. The effect of alloying and artificial ageing regimes on the structure and properties of experimental alloys are determined. It is shown that especially strong alloys of the Al–Zn–Mg–Cu system after ageing by a single-stage regime (T1) exhibit maximum strength (σu up to 700 MPa). Two-stage softening regime of type T22 provides a high level of mechanical properties combined with satisfactory corrosion resistance.

Sobre autores

O. Senatorova

State Research Center of the Russian Federation – All-Russia Research Institute of Aviation Materials (VIAM)

Autor responsável pela correspondência
Email: org80@viam.ru
Rússia, Moscow

A. Bronz

State Research Center of the Russian Federation – All-Russia Research Institute of Aviation Materials (VIAM)

Email: org80@viam.ru
Rússia, Moscow

V. Cheverikin

National University of Science and Technology MISiS

Email: org80@viam.ru
Rússia, Moscow

A. Somov

State Research Center of the Russian Federation – All-Russia Research Institute of Aviation Materials (VIAM)

Email: org80@viam.ru
Rússia, Moscow

N. Blinova

State Research Center of the Russian Federation – All-Russia Research Institute of Aviation Materials (VIAM)

Email: org80@viam.ru
Rússia, Moscow

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