The results of a study of dispersion-hardening high-temperature nickel
alloys EI698, EP742, and EP741 after thermomechanical treatment (TMT)
are considered. The alloys differ from the EI437BU type by a higher c
ontent of the strengthening gamma'-phase and considerably higher tempe
ratures of recrystallization and complete dissolution of the gamma'-ph
ase. The alloys studied are used for disks of aircraft engines.