FIELD: alloys as structural materials. SUBSTANCE: invention relates to alloys based on Al/Zn/Mg/Cu system designed for use as structural material in aircraft and rocket engineering as well as in transport and instrumental mechanical engineering pieces. Alloy contains, wt.%: zinc, 7.6-8.6; magnesium, 1.6-2.3; copper, 1.4-1.95; zirconium, 0.08-0.20; manganese, 0.01-0.1; iron, 0.02-0.15; silicon, 0.01-0.1; chromium, 0.01-0.05; nickel, 0.0001-0.03; beryllium, 0.0001- 0.005; bismuth, 0.00005-0.0005; hydrogen 0,8•10-5-2,7•10-5, and at least one mineral from the group containing titanium, 0.005-0.06; and boron, 0.00-0.01; and aluminum, the balance, on condition that zinc+magnesium+copper sum does not exceed 12.5% and iron-to-silicon ratio should be at least 1.2. EFFECT: improved strength and other characteristics needed for principal power units of flying apparatuses in combination with sufficient workability. 5 cl, 3 tbl
Title | Year | Author | Number |
---|---|---|---|
ALUMINUM-BASE ALLOY AND ARTICLE MADE OF IT | 1999 |
|
RU2163940C1 |
HIGH-STRENGTH HEAT-TREATABLE ALUMINIUM ALLOY AND ARTICLE MADE THEREOF | 2014 |
|
RU2556849C1 |
HIGHLY STRING ALUMINIUM-BASED ALLOY AND PRODUCT MADE OF SAID ALLOY | 1999 |
|
RU2165995C1 |
ALUMINUM-BASED ALLOY AND METHOD OF MANUFACTURING INTERMEDIATE PRODUCTS FROM THIS ALLOY | 2000 |
|
RU2180930C1 |
ALUMINIUM-BASED ALLOY | 2014 |
|
RU2576286C2 |
HIGH-STRENGTH HEAT-TREATABLE ALUMINIUM ALLOY AND ARTICLE MADE THEREOF | 2014 |
|
RU2560485C1 |
ALUMINUM-BASE ALLOY AND ARTICLE MADE OF THEREOF | 2001 |
|
RU2215805C2 |
HIGH-STRENGTH ALUMINIUM ALLOY OF Al-Zn-Mg-Cu SYSTEM AND PRODUCTS MADE OF IT | 2022 |
|
RU2804669C1 |
HIGH-STRENGTH ALUMINIUM ALLOY AND ARTICLE MADE OF IT | 2015 |
|
RU2610190C1 |
Al-Cu-Li-INTERMETALLIDE-BASED ALLOY AND ARTICLES MADE THEREOF | 2014 |
|
RU2560481C1 |
Authors
Dates
2002-06-27—Published
2000-08-01—Filed