Hot hardness and creep studies were carried out on Fe3Al and Fe3Al containi
ng Cr or Ti. Indentation and impression creep testing methods were employed
to characterize the creep behaviour. Compared to the binary alloy, Fe3Al-C
r exhibits a lower hardness indicating solid-solution softening effect of C
r. On the other hand, solid-solution hardening effect of Ti is significant
in the temperature range 300-900 K. Results from indentation creep indicate
s that a power-law creep behaviour (n between 6 and 8) is observed in the b
inary and Cr containing alloys at temperatures greater than 753 K. At lower
temperatures in the above two alloys and in the Ti-containing alloy even a
t higher temperatures, there is a power-law break down. On the other hand a
t low stress levels covered in the impression creep studies, power-law cree
p is observed in all the alloys in the stress and temperature range of inve
stigation. Under these conditions, all the alloys exhibit a stress exponent
value of around 3 for the steady state creep rate. The activation energy f
or creep is estimated to be in the range 325 and 375 kJ mel. Among the allo
ys studied, Fe3Al-Ti exhibits the best creep resistance. The results indica
te that in the B2 region, viscous glide controls the creep rate at low stre
sses while climb of dislocations may be rate controlling at higher stresses
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