FIELD: aluminum-magnesium alloys with high resistance to corrosion and corrosion separation into layers under stress. SUBSTANCE: aluminum-magnesium alloy has components in the following ratio, wt.%: Mg, 5.0-6.0; Mn, above 0.6-1.2; Zn, 0.4-1.5; Zr, 0.05-0.25; Cr, 0.3 max; Ti, 0.2 max; Fe, 0.5 max; Si, 0.5 max; Cu, 0.4 max; aluminum and inevitable impurities, the balance. Technical result consists in production of plate or extrusion profile from said alloy possessing strength considerably higher than standard alloy AA5083, after high-temperature tempering and after mechanical hardening. EFFECT: higher strength of alloy and welded construction from said alloy. 17 cl, 5 tbl, 3 ex
| Title | Year | Author | Number |
|---|---|---|---|
| ARTICLE FROM Al-Mg ALLOY FOR USE AS ARMOUR PLATE | 2008 |
|
RU2461638C2 |
| COMPOSITE ALUMINUM PANEL | 1999 |
|
RU2237578C2 |
| METHOD OF MANUFACTURING PRODUCTS FROM ALUMINUM/MAGNESIUM/LITHIUM ALLOY | 1999 |
|
RU2232828C2 |
| ALLOY Al-Zn-Mg-Cu | 2004 |
|
RU2353693C2 |
| PRODUCT MADE OF DEFORM HIGH-STRENGTH ALLOY Al-Zn AND MANUFACTURING METHOD OF SUCH PRODUCT | 2004 |
|
RU2353699C2 |
| 7xxx SERIES ALUMINUM ALLOY PRODUCT | 2020 |
|
RU2778466C1 |
| PRODUCT MADE OF ALUMINIUM ALLOY WITH HIGH RESISTANCE AGAINST DAMAGES, PARTICULARLY, FOR APPLICATION IN AEROSPACE INDUSTRY | 2004 |
|
RU2353700C2 |
| PRODUCT FROM ALUMINIUM ALLOY WITH HIGH RESISTANCE TO DAMAGES, NAMELY TO BE USED IN AVIATION AND SPACE INDUSTRY | 2004 |
|
RU2477331C2 |
| ALUMINIUM ALLOY RESISTANT TO INTERCRYSTALLINE CORROSION | 2013 |
|
RU2634822C2 |
| HOT-RESISTANT ALUMINIUM ALLOY | 2008 |
|
RU2458171C2 |
