PROPOSAL MODIFICATIONS TURBOSHAFT ENGINE TV3-117 ON ENERGY USE

Abstract

This work is dedicated to the treatment of aviation turboshaft engine TV3-117 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. There are mentioned various parts of the engine. Thermal cycle engine is calculated for 1. 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 engine TV3-117 and describes the different elements of the proposal. The work is also devoted to analyzing the actual state of the engine and its inspection. It is a procedure for checking the actual condition of the air turboshaft engine. The analysis of the actual state of the engine is to identify motor error. In the end, it evaluates the use of motor TV3-117 for power generation purposes and proposes the possibilities for solving problems of implementation of aircraft engines for energy purposes.