UDC 620.172.251.2 and S. G. Kiselevskaya aThe results of creep-rupture data processing for heat-resistant nickel alloys by parametric methods, by the Trunin and base diagram methods are presented. The line of investigations to establish the relation between the chemical composition and creep rupture strength is considered.Comparatively high creep-rupture strength of heat-resistant nickel alloys is reached by multicomponent alloying. Expensive refractory metals are often used as major alloying elements, however, their high melting temperature cannot always ensure high heat resistance.The present study considers alloying as one of the means to enhance the creep-rupture strength of heat-resistant nickel alloys. Nickel-base alloys are hardened accounting for the nickel ability to solve great quantities of other metals and to produce solid solutions. The Co, Al, Cr, Mo, and W elements form the γ-solid solution (NiAl) with Ni. The Al, Ti, Nb, Ta, and Hf elements enter into the composition of the ′ γ -phase (Ni 3 Al) [1].A great number of alloying elements and their combinations complicates true estimation of their effect on strain-softening of the above alloys. The objective of the present investigation is discussing the potentials of this estimation.The effect of alloying elements on the hardening of the γ-solid solution, composition and quantity of disperse phases, their stability under different conditions is rather complex and uncertain. It is established that in the Ni 3 Al structure, titanium hafnium, zirconium, niobium, and tantalum substitute only for aluminum, cobalt and copper do only for nickel, while chromium and iron substitute for nickel and aluminum. The redistribution of elements in case of multicomponent alloying would be individual for each alloy [2].Since tungsten and molybdenum suppress the diffusion mobility of nickel, the strength of interatomic bonds increases in all the structural components of dispersion-hardened iron-nickel alloys and a decrease in plasticity grow adds to their mechanical properties [3].The Cr, Mo, W, Nb, Ti, and Ta elements form MC carbides, which decompose into M 23 C 6 and M 6 C on thermal treatment and aggregate along grain boundaries. This gives a different retardation response of softening to the above phenomena under long high-temperature loading.The Al and Cr elements are responsible for the protective oxide layers formed on the surface of alloys and their oxidation resistance [4]. For instance, Al is the major element providing scale resistance for ZhS aviation alloys [5]. However high-temperature loading effects give rise to rather intensive diffusion processes, which lead to the oxide phase decomposition, to their spalling in operation of gas turbine blades. Thus, one of the issues consists in the improvement of alloying, which could contribute to a slower decomposition of protective oxide layers [6].Creep-rupture prediction for the aviation alloys remains a rather complicated problem due to a wide scatter of test results caused by low plasticity. Therefore, the cho...