TY - JOUR
T1 - NiTiAl intermetallic alloys strengthened by Mo replacement
AU - Song, Xiaoyun
AU - Li, Yan
AU - Zhang, Fei
AU - Li, Shusuo
PY - 2010/12
Y1 - 2010/12
N2 - NiTiAl based alloys have attracted attention as potential high temperature structural materials. Alloying is an effective way to improve their mechanical properties. The microstructures and mechanical properties of Ni 50Ti44-xAl6Mox (x = 0, 0.5, 1, 1.5, 3) alloys have been investigated by X-ray diffraction (XRD), scanning electron microscope (SEM), transmission electron microscope (TEM) and compressive tests. It is found that Ni50Ti44-xAl6Mox alloy is composed of NiTi (B2) and Ti2Ni (FCC) phases when Mo content is no more than 1 at. The effect of Mo solid solution hardening at room temperature has been indicated by the rise of yield strength and the fall of plasticity with increasing Mo content. For Ni50Ti 42.5Al6Mo1.5 and Ni50Ti 41Al6Mo3 alloys, a Mo solid solution appears and increases the yield strength by precipitation strengthening. The maximum yield strength at 600 °C and elevated temperatures is presented in Ni 50Ti43Al6Mo1 alloy not in alloys with a higher Mo content, which is possibly due to the softness of Mo-Ti-Ni solid solution phase.
AB - NiTiAl based alloys have attracted attention as potential high temperature structural materials. Alloying is an effective way to improve their mechanical properties. The microstructures and mechanical properties of Ni 50Ti44-xAl6Mox (x = 0, 0.5, 1, 1.5, 3) alloys have been investigated by X-ray diffraction (XRD), scanning electron microscope (SEM), transmission electron microscope (TEM) and compressive tests. It is found that Ni50Ti44-xAl6Mox alloy is composed of NiTi (B2) and Ti2Ni (FCC) phases when Mo content is no more than 1 at. The effect of Mo solid solution hardening at room temperature has been indicated by the rise of yield strength and the fall of plasticity with increasing Mo content. For Ni50Ti 42.5Al6Mo1.5 and Ni50Ti 41Al6Mo3 alloys, a Mo solid solution appears and increases the yield strength by precipitation strengthening. The maximum yield strength at 600 °C and elevated temperatures is presented in Ni 50Ti43Al6Mo1 alloy not in alloys with a higher Mo content, which is possibly due to the softness of Mo-Ti-Ni solid solution phase.
KW - Mo solid solution
KW - NiTiAl alloy
KW - mechanical properties
KW - microstructure
KW - molybdenum
UR - https://www.scopus.com/pages/publications/78650835759
U2 - 10.1016/S1000-9361(09)60274-0
DO - 10.1016/S1000-9361(09)60274-0
M3 - 文章
AN - SCOPUS:78650835759
SN - 1000-9361
VL - 23
SP - 715
EP - 719
JO - Chinese Journal of Aeronautics
JF - Chinese Journal of Aeronautics
IS - 6
ER -