Journal of Aeronautical Materials (Oct 2017)

Interphase Constituent of Laminated Composites Ti<sub>46</sub>Zr<sub>26</sub>Cu<sub>17</sub>Ni<sub>11</sub>

  • XU Bingtong,
  • ZHANG Rongxia,
  • WU Wei,
  • CHEN Fulong

DOI
https://doi.org/10.11868/j.issn.1005-5053.2016.000172
Journal volume & issue
Vol. 37, no. 5
pp. 15 – 21

Abstract

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Thermal analysis of the Ti46Zr26Cu17Ni11 amorphous ribbon prepared by melt spinning was conducted by using DSC. Accordingly the amorphous alloy was treated by vacuum heat treatment at 693 K (Tg), 753 K (Tg-Tx1) and 813 K (> Tx1) for different time to analyze the crystallization behavior. Taking Ti46Zr26Cu17Ni11 amorphous alloy, TA2 and pure Al as raw materials, laminated composites were fabricated by Gleeble-3500 thermal simulator at 873 K, 10 MPa and 8 h. The phase composition, precipitation order and properties of interface layers were investigated by SEM, TEM, micro hardness tester, combined thermodynamics and element diffusion theory. The results indicate that the glass transition temperature Tg of Ti46Zr26Cu17Ni11 amorphous is 720 K and the initial crystallization temperature Tx1 is 788 K. The I phase is crystallized from the amorphous at first, followed by a ternary or quaternary Laves phase and a TiNi phase precipited. After hot pressing, the interface between pure Al and crystallization layer is divided into two parts, which are Al3Ni with small thickness and Al3(Ti0.6Zr0.4) with fine grain and uniform microstructure. The interfaces are straight and there are no defects, with a thickness ratio of about 6.5:1 compared with interface layer between pure Ti with Al. The hardness of Al3(Ti0.6Zr0.4) and Al3Ti are 564.2HV and 579.8HV respectively. The plasticity of Al3(Ti0.6Zr0.4) layer is better.

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