Energy-efficient gas turbines (GTs) with reduced emissions have significantly contributed to sustainable development. However, these advanced engines, operating at turbine inlet temperatures (TITs) as high as 1.600°C, require the development of highly creep-resistant materials for application in hotter-section components of GTs. This paper first reviews recent advancements in the development of creep-resistant superalloys and their microstructural control, including stable gamma-prime raft structures. Then a comparative analysis of recently developed SC superalloys is presented to enable GT designers to select appropriate materials for hotter energy-efficient GT engines. It is recommended to develop new creep-limited alloys based on the metals with higher melting temperatures (e.g., Mo and Nb alloyed with silicon); these future alloys are proposed as prospective candidates for hotter energy-efficient GTs. Keywords: energy-efficient gas turbines, gas-turbine blades, turbine inlet temperature, single-crystal superalloys Energetsko u~inkovite plinske turbine (angl. GT) z zmanj{animi emisijami so mo~no prispevale pri trajnostnem razvoju. Vendar pa ti napredni stroji, ki delujejo pri temperaturah do 1600°C v vstopnem delu turbine zahtevajo, za uporabo komponent v vro~em delu, razvoj materialov odpornih na lezenje.^lanek predstavlja prvi pregled trenutnega napredka pri razvoju na lezenje odpornih superzlitin in kontrolo njihovih mikrostruktur, vklju~no s stabilno zgradbo gama-prime. Predstavljena je analiza pred kratkim razvitih SC superzlitin, tako da je konstrukterjem GT omogo~ena izbira primernega materiala za bolj vro~e, energijsko u~inkovite GT stroje. Predlagan je razvoj novih zlitin z omejenim lezenjem, ki temeljijo na kovinah z vi{jo temperature tali{~a (npr. Mo in Nb legiran s silicijem); te bodo~e zlitine so predlagane kot perspektivne za bolj vro~e, energijsko u~inkovite GT. Klju~ne besede: energijsko u~inkovite plinske turbine, lopatice plinskih turbin, vhodna temperatura turbine, monokristalne superzlitine