Zobrazeno 1 - 10
of 15
pro vyhledávání: '"N. I. Kolobnev"'
Publikováno v:
Metal Science and Heat Treatment. 61:73-82
Models of structure of plane Guinier–Preston zones in Al – Li and Al – Cu – Li systems are suggested. The models are based on the structural and phase correspondence of volume fragments of the structures of δ-phase of the Al – Li system an
Publikováno v:
Welding International. 32:62-66
The effect of the friction stir welding (FSW) conditions on the structure of welded joint and mechanical properties of 1424 and V-1461 alloys is investigated. FSW is accompanied by the formation of...
Publikováno v:
Tsvetnye Metally. :83-87
Publikováno v:
Metal Science and Heat Treatment. 56:416-419
The effect of deformation on the structure, strength and fatigue properties, stresses on the surface and sensitivity to intercrystalline corrosion of sheets from alloy 1370 of the Al –Mg – Si – Cu – Zn system with one-side cladding is investi
Publikováno v:
Metal Science and Heat Treatment. 55:459-465
Third-generation aluminum alloys 1441, 1424 and V-1461, V-1469 of medium and high strength, respectively, which have been developed as an alternative to the base aluminum alloys 1163 and V95 widely used in the aircraft industry, are studied. The adva
Publikováno v:
Metallurgist. 56:336-341
Results are presented for a study by different methods of the structure and properties of third generation extruded semifinished products of aluminum-lithium alloys 1424 and B-1461 of the systems Al–Mg–Li–Zn and Al–Cu–Li–Zn in comparison
Autor:
N. I. Kolobnev
Publikováno v:
Metal Science and Heat Treatment. 44:297-299
Aluminum-lithium alloys with diminished density and high crack resistance characteristics are widely used in aircraft. Scandium additives to this alloy improve the strength properties and considerably enhance the weldability.
Publikováno v:
Metal Science and Heat Treatment. 38:168-170
Aluminum alloys with lithium are a promising light metallic alloy for aerospace engineering. At present about 10 lithium-alloyed aluminum alloys have been developed. These materials are distinguished from other aluminum alloys by an elevated toughnes
Autor:
V. A. Lototskaya, S. V. Sokolskiy, M. M. Chernic, N. I. Kolobnev, L. V. Skibina, Yu. A. Pokhil
Publikováno v:
Advances in Cryogenic Engineering Materials ISBN: 9781461369264
The paper is aimed to investigation of mechanical properties and microscopic fracture features of the superlight high-strength alloy of an Al-Cu-Li system and its welded joints as a function of temperature (293-20K) and orientation with respect to ro
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2512cc13a52c9e3e640ef0dc1f657152
https://doi.org/10.1007/978-1-4615-4293-3_13
https://doi.org/10.1007/978-1-4615-4293-3_13
Publikováno v:
Metal Science and Heat Treatment. 20:1031-1034
Plates of alloy VAD23 should be produced by treatment III with hot rolling at 400–490°, ensuring the necessary quality of the plates and the mechanical properties.