Title of article
Creep behavior of Ti–6Al–4V and a comparison with titanium matrix composites
Author/Authors
Barboza، نويسنده , , M.J.R. and Perez، نويسنده , , E.A.C. and Medeiros، نويسنده , , M.M. and Reis-Henriques، نويسنده , , D.A.P. and Nono، نويسنده , , M.C.A. and Neto، نويسنده , , F. Piorino and Silva، نويسنده , , C.R.M.، نويسنده ,
Issue Information
روزنامه با شماره پیاپی سال 2006
Pages
8
From page
319
To page
326
Abstract
Creep behavior of the conventional Ti–6Al–4V alloy with a Widmanstätten microstructure has been investigated in air under constant load tensile tests. The stress exponent values of 11.3 and 5.2 were obtained at 500 and 600 °C, respectively. By incorporating the threshold stress into analysis, the creep data can be rationalized to stress exponents of 4.4 at 500 °C and 4.1 at 600 °C, which are consistent with the lattice diffusion controlled dislocation climb process in α-Ti. In the preliminary study, creep properties of α-Ti, TiBw/Ti and TiCp/Ti–6Al–4V have been collected from literature and compared with those of Ti–6Al–4V obtained in this work in the applied stress range of 97–472 MPa. Creep strain rates of the conventional Ti–6Al–4V alloy are lower than those of the α-Ti and composites. Apparently, the higher creep resistance of Ti–6Al–4V can be attributed to α/β interfaces acting as obstacles to dislocation motion and to the average grain size of 395 μm, which reduces the grain boundary sliding, dislocations sources and the rate of oxygen diffusion along grain boundaries.
Keywords
Creep , Ti–6Al–4V , Composite
Journal title
MATERIALS SCIENCE & ENGINEERING: A
Serial Year
2006
Journal title
MATERIALS SCIENCE & ENGINEERING: A
Record number
2149974
Link To Document