Electromagnetic hypersonic thrust vector jet engine

Abstract

The invention discloses an electromagnetic hypersonic thrust vector jet engine. The engine comprises a shell, an adjustable air inlet, an electromagnetic turbofan, a force bearing frame, an outer duct, an inner duct, an air compressor, an oxygen supply and oil supply pipe, a thrust augmentation nozzle, a combustion chamber, a generator, a double-turbine engine, a thrust vectoring nozzle, an adjustable nozzle, a main shaft, a bearing, a frequency converter, a transmission, a sparking plug, an oil sprayer, a lithium battery, a charger, a computer, a cable, an instrument and an electronic switch. Compared with an existing turbojet engine, the electromagnetic hypersonic thrust vector jet engine is more advanced, simple in structure, easy to machine, manufacture and maintain, low in cost and capable of controlling airflow balance of an air inlet and an air outlet and regulating and controlling the temperature of fuel gas in a combustion chamber and the supercharge ratio of an air compressor, so that the fuel gas achieves subsonic combustion or scramjet, the heat efficiency and the propelling efficiency of the turbojet engine are improved, the fuel gas is utilized to generate power for an electromagnetic turbofan, the lithium battery and the computer, and the electromagnetic hypersonic thrust vector jet engine which is low in noise, low in oil consumption, high in efficiency, high in reliability and good in running performance can be achieved.

Description

technical field [0001] The invention relates to an electromagnetic type hypersonic thrust vectoring jet engine and a gas type twin-turbine engine. Background technique [0002] The supersonic jet engines currently on the market do not have jet engines with an electromagnetic structure, but all of them are jet engines with a turbine structure. Because the manufacture of turbines and shafts requires a large amount of high-temperature-resistant materials, these materials are as expensive as gold, so the production Manufacture of turbojet engine is a worldwide problem due to its complex structure and high technical difficulty, resulting in difficult processing, manufacturing and maintenance. The current turbojet engine is an oil tiger. It relies entirely on the high-temperature and high-pressure gas generated by the explosion of the fuel mixture in the combustion chamber to drive the turbine to rotate. The turbine rotates to drive the shaft, fan and compressor to rotate together...

AI Technical Summary

Problems solved by technology

[0002] The supersonic jet engines currently on the market do not have jet engines with an electromagnetic structure, but all of them are jet engines with a turbine structure. Because the manufacture of turbines and shafts requires a large amount of high-temperature-resistant materials, these materials are as expensive as gold, so the production Manufacture of turbojet engine, its complex structure, high technical difficulty, resulting in difficult processing, difficult manufacturing, difficult maintenance, is a worldwide problem

The current turbojet engine is an oil tiger. It relies entirely on the high-temperature and high-pressure gas generated by the explosion of the fuel mixture in the combustion chamber to drive the turbine to rotate. The turbine rotates to drive the shaft, fan and compressor to rotate together. The turbine produces high-temperature gas discharge. Resistance also produces noise and consumes part of the energy, resulting in high fuel consumption, low efficiency, low thrust, high noise, large volume, and high cost of the turbojet engine. Since the high-temperature turbine is on the same shaft as the compressor and the fan, Therefore, it is impossible to control the balance of the air flow entering the air inlet and the gas flow discharged from the exhaust port, and it is also impossible to control the temperature of the gas in the combustion chamber and the boost ratio of the compressor, and it is also impossible to control whether the gas in the combustion chamber reaches sub-combustion state or superburn state, it is impossible to improve the thermal efficiency and propulsion efficiency of the turbojet engine

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