Theoretical research of possibility of creation small high-rise jet-piston power engine for UAV

Аuthors

Bodrov A. V.^*, Lapushkin V. N.

Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

*e-mail: dron_b@mail.ru

Abstract

Experimentally-theoretical research of possibility ofpressurisation small duple engine, is conducted by the centrifugal compressor resulted by it. The superfluous blowing-off mix cooling gas exhaust path and burnt in the pulsing jet chamber is burnt together with products of combustion of exhaust piston power engine. Thereby, creating a resultant draught the power.

Keywords:

thermal processes, air jet engine, unmanned aircraft vehicle