Electric fuel oil jet propeller

Abstract

The invention discloses an electric fuel oil jet propeller which comprises an air inlet, a fan, a motor, an air deflector, a combustion chamber and a tailpipe with the thrust of 1-50kg. The electric fuel oil jet propeller is characterized in that fan blades are fixed on a fan hub which is fixed on an outer rotor direct-current motor rotor; the motor is fixed on an air deflector inner support ring through a bolt; an air deflector outer ring is embedded on the inner wall of a ducted casing; a heat insulation shield is arranged at the rear end of the air deflector inner support ring; the combustion chamber is arranged at the middle-rear end of the ducted casing; a pneumatic fuel oil nozzle ring is arranged at the front section of the combustion chamber and communicated with an oil pipeline; a falcate flame stabilizer is arranged at the rear end of the pneumatic fuel oil nozzle ring; an igniter is arranged at the rear end of the falcate flame stabilizer, passes through the combustion chamber and the ducted casing and is fixed on the outer wall surface of the ducted casing; and the inner wall of the ducted casing adopts a heat insulation coating. The propeller can be used as main power of small and middle size delivery tools and has simple structure, small size, light weight and large working thrust.

Description

technical field [0001] The present invention relates to a propeller, more particularly to an electric fuel jet propeller. Background technique [0002] With the continuous development of aircraft design and manufacturing technology, higher requirements are put forward for its propulsion device. Both propulsion efficiency and economic performance have risen to higher requirements. Like the usual large and medium-sized aviation jet engines, they have high technical difficulty, complex structure, difficult processing, high production cost, and it is difficult to enter the market at a low price. However, due to its simple structure, easy processing, and low production cost, driven by the development of high-energy-density batteries, electric ducted fan engines are widely used as the main power source for small unmanned aerial vehicles. The working efficiency of the electric ducted fan engine is still relatively low, and the thrust produced is relatively small, so it is difficu...

AI Technical Summary

Problems solved by technology

Like the usual large and medium-sized aviation jet engines, they have high technical difficulty, complex structure, difficult processing, high production cost, and it is difficult to enter the market at a low price

However, due to its simple structure, easy processing, and low production cost, driven by the development of high-energy-density batteries, electric ducted fan engines are widely used as the main power source for small unmanned aerial vehicles. The working efficiency of the electric ducted fan engine is still relatively low, and the thrust produced is relatively small, so it is difficult to use it on larger-sized aircraft

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