Title of article :
Effects of Nb and Al on the microstructures and mechanical properties of high Nb containing TiAl base alloys
Author/Authors :
Liu، نويسنده , , Z.C. and Lin، نويسنده , , J.P. and Li، نويسنده , , S.J. and CHEN، نويسنده , , G.L.، نويسنده ,
Issue Information :
روزنامه با شماره پیاپی سال 2002
Pages :
7
From page :
653
To page :
659
Abstract :
The influence of Nb and Al contents on the microstructure and yield strength of high Nb containing TiAl base alloys was investigated. The experimental results show that the yield strength at 900 °C of the alloys with the same type of microstructure, such as fully lamellar (FL), nearly lamellar (NL) and degraded fully lamellar (DFL), increases with increasing Nb content and decreasing Al content in the composition range of 0–10 at.% Nb and 44–49 at.% Al. DFL is the degraded form of FL microstructure after exposure at 1050 °C for 30 h. It is shown that the Nb addition in the alloys increases the value of the σ0 term in the Hall–Petch relation of yield stress vs. lamellar spacing. This result has been related to TEM observations of dislocation structure in deformed specimens. The observations indicated that high level of Nb solute in the γ-TiAl matrix leads to a high critical resolved shear stress (CRSS) of dislocation loops. High Nb addition also reduces the degradation rate of FL microstructure after exposure at 1050 °C for 30 h. Both effects of high Nb addition are related to the change of the directionality of Ti–Ti (Nb) and Nb–Al bonds in the lattice. The decrease in Al content results in an increase in the volume fraction of α2 phase, which leads to a decrease in the lamellar spacing of the lamellar structure. The high temperature strength of the alloys is determined by the lamellar spacing λ through the Hall–Petch equation kλλ−1/2.
Keywords :
A. Titanium aluminides , B. Mechanical properties at high temperature , based on TiAl , B. Solid Solution hardening
Journal title :
Intermetallics
Serial Year :
2002
Journal title :
Intermetallics
Record number :
1501117
Link To Document :
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