FIELD: metallurgy, in particular high strength, corrosion resistant magnesium-based alloys for aircraft industry.
SUBSTANCE: claimed alloy contains (mass %): zinc 6,5-9.5; cadmium 0.01-1.4; zirconium 0.7-1.2; 0.01-0.6; titanium 0.004-beryllium 0.0006-0.001; and additionally bismuth 0.01-0.8 and niobium 0.01; and balance: magnesium.
EFFECT: magnesium-based alloy with low content of iron, silicium and copper impurities; as well as improved corrosion strength and mechanical properties at room and elevated temperature.
2 cl, 2 tbl, 1 ex
| Title | Year | Author | Number |
|---|---|---|---|
| MAGNESIUM-BASED ALLOY AND PRODUCT MANUFACTURED THEREFROM | 2003 |
|
RU2230814C1 |
| ALLOY ON THE BASIS OF MAGNESIUM AND THE ARTICLE PRODUCED OUT OF IT | 2006 |
|
RU2318031C1 |
| ALLOY ON BASE OF MAGNESIUM | 2010 |
|
RU2425903C1 |
| ALUMINUM-BASED HIGH-STRENGTH ALLOY AND PRODUCT MANUFACTURED THEREFROM | 2000 |
|
RU2184166C2 |
| MAGNESIUM-BASED ALLOY AND ARTICLE MADE FROM THIS ALLOY | 2001 |
|
RU2198234C2 |
| MAGNESIUM-BASED ALLOY AND PRODUCT MADE FROM IT | 2014 |
|
RU2554269C1 |
| HIGH-STRENGTH DEFORMABLE ALLOY BASED ON ALUMINIUM WITH LOWER DENSITY AND METHOD OF ITS PROCESSING | 2011 |
|
RU2468107C1 |
| ALUMINIUM-BASED ALLOY AND PRODUCT MADE FROM THE SAME | 2003 |
|
RU2243278C1 |
| ALUMINUM-BASE CASTING ALLOY | 2003 |
|
RU2247789C1 |
| HEAT RESISTANT NICKEL-BASED ALLOY FOR PRODUCING BOILER PARTS AND STEAM TURBINES OPERATING UNDER ULTRA-SUPERCRITICAL STEAM PARAMETERS | 2017 |
|
RU2637844C1 |
