Pulse motor-turbine engine for aircraft has air fed from compressor to turbine through combustors with opening and closing flap valves operated by electromagnets with numerical control system

摘要

The pulse motor-turbine engine uses intermittent combustion with the air fed from the compressor in pulses towards the turbine after pulsed combustion in one or more groups of combustion chambers. The chambers have opening and closing flap valves operated by electromagnets with a numerical control system.