УЧЁТ ВЛИЯНИЯ ТЕМПЕРАТУРЫ ГАЗА В МОДЕЛИ МАССЫ ГТД СО СВОБОДНОЙ ТУРБИНОЙ ДЛЯ ВЕРТОЛЁТОВ

Abstract

The achievement of the best performance of aircraft engines in terms of economy is realized to a large extent due to the development of ever higher gas temperatures at the entrance to the turbine. There are two ways to solve this problem - the organization of systems for intensive cooling of turbine elements, and the use of new technologies and materials capable of ensuring reliable operation of all GTE elements. The article describes the nature of the effect of various elements to the cooling system of the engine masses.