THE TRANSFORMATION OF THE TURBO-PROPELLER ENGINE TO POWER GAS TURBINE

Abstract

This work is dedicated to the transformation of aviation turbo-propeller engine AI-24 for energy purposes. The paper provides an analysis of engine construction, design modifications analysis of main components for energy use, as well as analysis of major engine systems. Thermal cycle engine is calculated for first cruise mode. And also it discusses the legislative formalities associated with aircraft engine modifications for energy purposes. The paper processed requirements for such equipment. It is the establishment of framework proposal facilities for electricity production based on the use of turbo-propeller engine AI-24 and describes the different elements of the proposal. The work is also devoted to analysing the actual state of the engine and its inspection. It is a procedure for checking the actual condition of the air turboshaft engine. In the end, it evaluates the use of motor AI-24 for power generation purposes and proposes the possibilities for solving problems of implementation of aircraft turboprop engines for energy purposes.