The nickel base superalloys are developed for critical applications in
gas turbines and are presently being used at temperatures up to about
1400 K. This is about 80% of the absolute melting temperature (1726 K
) of nickel. Only marginal increase in their high temperature capabili
ty is therefore possible. The alternative groups of materials are stil
l in developmental stage. More effective use of the superalloys in ter
ms of increased service life can be achieved through a better understa
nding of the processes of deformation and damage in these alloys. The
characteristics of their deformation behaviour at elevated temperature
s and its present understanding are discussed.