| 摘要 |
manufacture of bars, stampings, bracings and other components of aviation equipment. SUBSTANCE: alloy comprises, wt.% aluminium, 2.2-3.8; vanadium, 4.5-5.9; molybdenum, 4.5-5.9; chrome, 2.0-3.6; iron, 0.2-0.8; zirconium, 0.01-0.08; carbon, 0.01-0.25 oxygen, 0.03-0.025, and titanium, the balance. Alloy is capable of being subjected to volumetric deformation may be adequately rolled to form bar, contains no high-melting inclusions and is readily strengthened by thermal methods. EFFECT: high strength and plastic properties of the alloy. 1 tbl
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