Electromagnetic hypersonic thrust vector jet engine

A jet engine and hypersonic technology, applied in the direction of engine ignition, engine components, machines/engines, etc., can solve problems such as low thrust, inability to control the air inlet, and high technical difficulty

Pending Publication Date: 2021-10-19
SHAOYANG UNIV
View PDF0 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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...

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Electromagnetic hypersonic thrust vector jet engine
  • Electromagnetic hypersonic thrust vector jet engine
  • Electromagnetic hypersonic thrust vector jet engine

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0010] Such as figure 1 , 2As shown, an electromagnetic hypersonic thrust vector jet engine includes a casing 1, an adjustable air inlet, an electromagnetic turbofan 2, a stator 3, a permanent magnet rotor 4, a fan blade 5, a load-bearing frame 6, and an outer casing Road 7, inner channel 8, compressor 9, oxygen supply and oil supply pipe 10, afterburner nozzle 11, combustion chamber 12, generator 13, main shaft gear 14, twin-turbine engine, turbine 15, vortex blade 16, main shaft gear 17. Vector nozzle 18, adjustable nozzle 19, main shaft 20, bearing 21, lever gear 22, chain 23, connecting gear 24, frequency converter, transmission, spark plug, fuel injector, lithium battery, charger, computer, cable , instruments and electronic switches, the electromagnetic is composed of an armature and a permanent magnet, which uses the moving magnetic field generated by the current to drive the permanent magnet to rotate. The electromagnetic turbofan 2 is composed of a shell 1, a stator ...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

PUM

No PUM Login to view more

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...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

Application Information

Patent Timeline
no application Login to view more
IPC IPC(8): F02K3/06F02K3/12F02C6/00F02C7/26F02C7/36
CPCF02K3/06F02K3/12F02C6/00F02C7/26F02C7/36
Inventor 林立夏建国
Owner SHAOYANG UNIV
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products