FIELD: construction materials in aviacosmetic engineering and transport vehicles. SUBSTANCE: highly string Al-Zn-Mg-Cu-based alloy comprises, wt.%; zinc, 5.0-7.0; magnesium, 1.8-2.8; copper, 1.4- 2.0; chromium, 0.1-0.25 iron, 0.05-0.25; titanium, 0.005-0.07; silicon, 0.02-0.1; manganese, 0.2-0.6; and the balance, manganese to chromium ratio being more or equal to 1.3. Iron to silicon ratio is more or equal to 1.5. EFFECT: improved technological characteristics of alloy during casting, cracking resistance, plasticity, corrosion resistance and desired level of strength for all types of semiproducts. 4 cl, 1 ex, 2 tbl
Title | Year | Author | Number |
---|---|---|---|
ALUMINUM-BASED HIGH-STRENGTH ALLOY AND PRODUCT MANUFACTURED THEREFROM | 2000 |
|
RU2184166C2 |
HIGHLY STRING ALUMINIUM-BASED ALLOY AND PRODUCT MADE OF SAID ALLOY | 1999 |
|
RU2165995C1 |
HIGH-STRENGTH HEAT-TREATABLE ALUMINIUM ALLOY AND ARTICLE MADE THEREOF | 2014 |
|
RU2556849C1 |
ALUMINUM-BASED ALLOY AND PRODUCT THEREFROM | 2001 |
|
RU2215055C2 |
ALUMINUM-BASE ALLOY AND ARTICLE MADE OF IT | 1999 |
|
RU2163940C1 |
ALUMINUM-BASED ALLOY AND ARTICLE MADE THEREFROM | 2005 |
|
RU2299256C1 |
CORROSION-RESISTANT ALUMINUM-BASE ALLOY, METHOD OF PRODUCTION OF SEMIFINISHED PRODUCTS AND ARTICLE FOR THIS ALLOY | 1999 |
|
RU2163938C1 |
ALUMINUM-BASE ALLOY, METHOD OF PRODUCTION OF SEMIFINISHED PRODUCTS AND ARTICLE FROM THIS ALLOY | 1999 |
|
RU2163939C1 |
ALUMINUM-BASE HIGH-STRENGTH ALLOY AND ARTICLE MADE OF THIS ALLOY | 2002 |
|
RU2233902C1 |
ALUMINIUM-BASED ALLOY AND PRODUCT MADE FROM THE SAME | 2003 |
|
RU2243278C1 |
Authors
Dates
2001-04-27—Published
1999-10-05—Filed