Метод формирования рационального облика турбокомпрессора малоразмерных газотурбинных двигателей

Abstract

The article describes method of turbocompressor layout forming of a small-scale gas turbine engines, that includes four nested tasks: thermogasdynamic designing, structural and parametric optimization and turbocompressor parameters matching. Great structural diversity of small-scale engines makes the development of appropriate computer-aided systems a task of a high importance. Some problems associated with a conceptual design phase of a turbocompressor of a small-scale gas turbine engine has been also described.