Properties of Al-Li alloy 1420 after different aging produces

Cailiao Kexue yu Gongyi/Material Science and Technology

Volumn 13, Issue 1, 2005, Pages

  Zhang, Lei ^a   Zhu, Ming Liang ^b   Huang, Zheng ^b  

^a Beijing Aeronautical Engineering Technical Research Center   (China)

^b BEIHANG UNIVERSITY   (China)

Author keywords

1420 Al Li alloys; Double aging; Open circuit potential; Strength

Indexed keywords

AGE HARDENING; ALUMINUM ALLOYS; CORROSION RESISTANCE; ELECTRIC POTENTIAL; ELECTROCHEMISTRY; LITHIUM ALLOYS; MECHANICAL PROPERTIES; MICROSTRUCTURE; SCANNING ELECTRON MICROSCOPY; TENSILE PROPERTIES; TRANSMISSION ELECTRON MICROSCOPY;

ALUMINUM LITHIUM ALLOYS; DOUBLE AGING; ELECTROCHEMISTRY TESTING; OPEN CIRCUIT POTENTIAL;

BINARY ALLOYS;

EID: 17244377604     PISSN: 10050299     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (8)

1. CUI Yu-sheng. Microstructure control of toughness in Al-Li Alloys[J]. Scripta Mater, 1996, 34(5): 781-786.
2. HULIDLIANGEL E N, SANDLEL W S, NIKOLSKAYA T E. Aluminum-Lithium based alloys for aerospace applications[J]. Metallography and Heat Treatment of Metals, 1971, 5(2): 118-125.
3. MAHALINGAM K. Strength Profile in Al-Li plate material[J]. Acta Metall, 1993, 35(2): 483-491.
4. THOMPSOM G E, NOBLE J B. The effect of grain structure on the fracture behavior and tensile properties of Al-Li-Cu alloy[J]. Inst of Matals, 1973, 2(1): 101-111.