Mechanical Properties Analysis of the AA2519-AA1050-Ti6Al4V Explosive Welded Laminate

被引:12
|
作者
Szachogluchowicz, Ireneusz [1 ]
Sniezek, Lucjan [1 ]
Slezak, Tomasz [1 ]
Kluczynski, Janusz [1 ]
Grzelak, Krzysztof [1 ]
Torzewski, Janusz [1 ]
Fras, Teresa [2 ]
机构
[1] Mil Univ Technol, Inst Robots & Machine Design, Fac Mech Engn, 2 Gen S Kaliskiego St, PL-00908 Warsaw 46, Poland
[2] French German Res Inst St Louis ISL, 5 Rue Gen Cassagnou, F-68301 St Louis, France
关键词
deformation analysis; residual stresses measurement; AA2519; Ti6Al4V; explosive welding; layered laminate; CYCLE FATIGUE PROPERTIES; MICROSTRUCTURE; SIMULATION; IMPACT;
D O I
10.3390/ma13194348
中图分类号
O64 [物理化学(理论化学)、化学物理学];
学科分类号
070304 ; 081704 ;
摘要
Explosively welded layered materials made of (a) an AA2519 aluminum alloy (AlCuMgMn + ZrSc), (b) titanium alloy Ti6Al4V and (c) an intermediate layer composed of a thin aluminum alloyed AA1050 layer are considered herein. This study presents test results connected to measurement science including microstructural observations of the material combined with the explosive method, and a basic analysis of the strength properties based on microhardness and tensile tests. Owing to the joint's special manufacturing conditions, the laminate was subjected to deformation measurements with the digital image correlation (DIC) method. The research was supplemented by the residual stress measurements with the sin2 psi X-ray method based on the diffraction-reflection analysis that was verified by the bore trepanation method.
引用
收藏
页码:1 / 16
页数:16
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