Compared to classical axial turbines, centrifugal turbines have a number of important advantages: compactness, higher energy efficiency (efficiency is usually above 90%) and lower cost. The development of centrifugal turbine designs for a wide range of aircraft gas turbine engines will help improve the efficiency and competitiveness of domestic aircraft engines and can also be used in the development and modernisation of engine flow parts for aerospace and military equipment.
Design of the flow part of hydraulic units No. 5-7 for the Dniester PSPP with increased (compared to hydraulic units No. 1-4) efficiency parameters and an extended range of operation in turbine mode within 40-100% of the rated capacity
