Structure and mechanical properties of NiAl and Ni3Al-based alloys

被引:74
作者
Czeppe, T [1 ]
Wierzbinski, S [1 ]
机构
[1] Polish Acad Sci, A Krupkowski Inst Met & Mat Sci, PL-30059 Krakow, Poland
关键词
nickel aluminides based on NiAl and Ni(3)Al; mechanical properties at elevated temperature; microstructural evolution;
D O I
10.1016/S0020-7403(99)00087-9
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
The investigation of Ni-Al-Fe-Ti-B alloys was carried out to determine the influence of iron and small titanium and boron additions on the phase composition, microstructure and mechanical characteristic, particularly with respect to high-temperature deformation conditions. These alloys, containing Al 35.8 at% and Fe 3.6-8.6-17.6 at% were prepared from high-purity components and Al master alloy containing Ti(2)B particles. The influence of alloying additions of chromium and iron on the mechanical properties of directionally solidified Ni-Al-Cr-Fe alloy was investigated. Additions of both Cr 8 at% and Fe 2 at% result in higher strength than exhibited by unalloyed Ni, Al. However, the ductility is reduced by the formation of the beta' phase. The typical, lamellar structure of Ni-20Al-8Cr-2Fe alloy undergoes coagulation during a high-temperature deformation process. The sequence of structural changes of NiAl and Ni, Al-based alloys has been correlated with mechanical characteristics of high-temperature deformation process, determined in uni-axial compression tests. Two ranges of work hardening have been identified on the stress-strain curves of these alloys. It has been found that the first range of the deformation of Ni-Al-Fe-Ti-B alloys corresponds to the intergranular slip system operating within individual grains, while the second one is connected with transgranular slip. In the directionally solidified Ni-20Al-8Cr-2Fe alloy similar work hardening curves were observed in relation to the microstructural evolution from the lamellae shape, through elliptical shape into circular shape. (C) 2000 Elsevier Science Ltd. All rights reserved.
引用
收藏
页码:1499 / 1518
页数:20
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