Advanced weldable damage tolerant AlMgLi alloy for aircraft application

Materials Science Forum

Volumn 242, Issue , 1997, Pages 249-254

  Fridlyander, J N ^a   Kolobnev, N I ^a   Grushko, O E ^a   Davydov, V G ^b  

^a ALL RUSSIAN SCIENTIFIC RESEARCH INSTITUTE OF AVIATION MATERIALS   (Russian Federation)

^b All Russia Institute of Light Alloys   (Russian Federation)

Author keywords

Aeroplane; Aluminium Lithium Alloy; Application; Density; Rocket; Weldability

Indexed keywords

AIRCRAFT PARTS AND EQUIPMENT; DENSITY (SPECIFIC GRAVITY); ELASTIC MODULI; GRAIN SIZE AND SHAPE; LITHIUM ALLOYS; SCANDIUM; STRENGTH OF MATERIALS; SUPERPLASTICITY; WELDABILITY;

DAMAGE TOLERANCE; MILITARY PLANES; PASSENGER PLANES; SUPERPLASTIC DEFORMATION; WELDABLE ALLOYS; WELDED FUSELAGE;

ALUMINUM ALLOYS;

EID: 0030671848     PISSN: 02555476     EISSN: 16629752     Source Type: Book Series    
DOI: 10.4028/www.scientific.net/msf.242.249     Document Type: Article

References (4)

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2. J.N.Fridlyander, N.V.Shiryaeva, V.S.Sandler, Promyshlennye aluminievye splavy (Industrial aluminium alloys), Metallurgya, 1984, p.220
3. J.N.Fridlyander, N.I.Kolobnev, A.L.Berezina, K.V.Chuistov, Aluminium-Lithium 6-th Conf.,v.1,1992,FRG
4. O.E.Grushko, Metals Science Basis of High Modulus, Low Density Aluminium-Lithium Alloys Ingots and Semiproducts Production, Doctor's dissertation, VIAM, Moscow, 1989, 505 p