Plasma recombination boosting turbine fan jet aerial engine

Abstract

A plasma compound afterburning turbofan jet aircraft engine, which includes a low-pressure fan, a high-pressure compressor, a combustion chamber, a turbine, and a tail nozzle, is characterized in that: an inner cone shaft center duct is set in the turbine shaft of the engine, and the The front end of the axial duct is fixed with an impeller, the nano permanent magnet steel rotor is assembled on the turbine shaft, and the superconducting material stator is assembled on the outer periphery of the nano permanent magnetic steel rotor to form an aero-generator. An arc plasma generator is assembled at the rear end, and a power helix guide bar is arranged on the periphery of the rear flow channel of the turbine, and the output end of the aviation generator supplies power to the arc plasma generator through the guide bar. The invention can use the air in the space as the afterburner, save more than 50% of the fuel, and the gas fluid is high-temperature and high-speed, so that the hypersonic flight of the fighter can be realized, the pollution to the atmosphere can be reduced, and the aircraft has the effect of stealth. The generator can be used as a laser weapon power supply , Laser weapons can capture targets quickly, and the high-temperature, high-speed, high-pressure laser beam can destroy various enemy aircraft.

Description

technical field [0001] The invention belongs to an aeroengine, in particular to a plasma compound afterburning turbofan jet aeroengine. Background technique [0002] At present, the aeroengine of the fighter jet adopts a turbofan jet engine, and its fuel adopts aviation kerosene, which consumes a lot of cruising and afterburning fuel, and its range (without afterburner) reaches 3,000-6,000 kilometers at one refueling. It can be refueled in the air, and at the same time, due to the large amount of fuel carried, it affects its combat maneuverability. The maximum flying speed of the aero-engine of the existing structure is that the Mach number reaches Ma5, and the engine exhaust contains a large amount of environmental pollutants such as sulfur dioxide and hydrocarbons, which is more serious to air pollution. Contents of the invention [0003] The purpose of the present invention is to provide a plasma composite afterburning turbofan jet aircraft engine, which can significan...

AI Technical Summary

Problems solved by technology

[0002] At present, the aeroengine of the fighter jet adopts a turbofan jet engine, and its fuel adopts aviation kerosene, which consumes a lot of cruising and afterburning fuel, and its range (without afterburner) reaches 3,000-6,000 kilometers at one refueling. It can be refueled in the air, and at the same time, due to the large amount of fuel, it affects its combat maneuverability

The maximum flight speed of the aero-engine with the existing structure is that the Mach number reaches Ma5, and the exhaust gas of the engine contains a large amount of environmental pollutants such as sulfur dioxide and hydrocarbons, which are more serious to air pollution.

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