Thrust generators Airplane method for generating thrust and method for improving the driving efficiency of an aircraft.

摘要

It will create a thruster. The thruster includes an air inlet (78) configured to introduce air (80) into the thruster and a chamber (72) configured to receive exhaust from a gas generator and the exhaust via a coanda Profile (74). The Coanda profile (74) is configured to facilitate adhesion of the exhaust gas to the Coanda profile (74). As a result, a boundary layer is formed and the incoming air (80) from the air inlet (78) is entrained to generate thrust.