Turbineless jet engines

A jet engine and engine technology, applied in the direction of machines/engines, jet propulsion devices, etc., can solve the problems of complex structure, loss of heat energy, energy consumption, etc., and achieve the effect of simple maintenance and operation, large thrust and low cost

Pending Publication Date: 2016-08-24
夏建国
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] The jet engines currently on the market are all jet engines with turbines. They are complex in structure, difficult to manufacture, difficult to maintain, small in thrust, loud in noise, high in fuel consumption, and high in cost. They all rely on the high-pressure gas in the combustion chamber to drive the turbine Rotation, the rotation of the turbine drives the shaft, the fan and the compressor to work, which consumes a huge amount of energy and also loses a lot of heat energy, which reduces the power of the jet engine, increases the fuel consumption, and increases the noise. If you want to reduce fuel consumption, reduce noise, and improve Thrust, only by removing the turbine behind the combustion chamber, can the resistance be removed. The simple structure can increase the thrust, reduce fuel consumption, and re

Method used

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Examples

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Effect test

Embodiment Construction

[0012] Such as figure 1 , 2 Shown, a kind of internal-combustion type non-turbine jet engine, it is by it to be combined into one by jet engine part and internal-combustion engine part, jet engine part: comprises housing 1, outer duct, adjustable air inlet 2 , internal combustion engine 3, turbofan 4, compressor 5, swirler 6, oxygen supply and oil supply pipe 7, afterburner nozzle 8, combustion chamber 9, adjustable nozzle 10, gas mixture pipe 11, union 12 , bearing, load-bearing frame, internal combustion engine 3 parts: including outer circle 13, flywheel 14, turbofan 4, shaft 15, gas mixture pipe 16, spring 17, gas ring 18, spark plug 19, injector 20, combustion chamber 21 , brushes, electric wires, computers, instruments and meters, and electronic switches are characterized in that: an air jet hole is arranged at the bottom of the combustion chamber 9, and an afterburner nozzle 8 and a spark plug are installed, and a part of the outer circle 13 of the internal combustion ...

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PUM

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Abstract

The invention relates to an internal combustion type turbineless jet engine and an electromagnetism type turbineless jet engine. The internal combustion type turbineless jet engine and the electromagnetism type turbineless jet engine do not need a turbine, so that the structure of a prior jet engine is changed completely. The internal combustion type turbineless jet engine and the electromagnetism type turbineless jet engine comprise shell bodies, force bearing frameworks, shafts, bearings, outer channels, adjustable air inlet ports, combustible gas mixture pipes, internal combustion type or electromagnetism type engine bodies, turbofans, gas compressors, cyclones, oxygen and oil supplying pipes, afterburning nozzles, combustion chambers, sparking plugs and adjustable injection pipes. When starting, under the control of a computer, the internal combustion type engine body or the electromagnetism type engine body rotates at high speed to drive the turbofan, the shaft and the gas compressor to run at high speed to convey air to the combustion chamber; the afterburning nozzle injects oil automatically, the sparking plug ignites and bursts automatically, and then the injection pipe would jet great air flow to push an airplane or a guided missile to fly at supersonic speed. The turbineless jet engines are simpler in structure, more scientific, lower in fuel consumption, greater in thrust, faster in speed, lower in noise and cost, easier to maintain, operate and manufacture, and great in commercial development value. The turbineless jet engines provided by the invention are the most advanced turbineless jet engines in the world.

Description

technical field [0001] The invention relates to an internal combustion type non-turbojet engine and an electromagnetic type non-turbojet engine. Background technique [0002] The jet engines currently on the market are all jet engines with turbines. They are complex in structure, difficult to manufacture, difficult to maintain, small in thrust, loud in noise, high in fuel consumption, and high in cost. They all rely on the high-pressure gas in the combustion chamber to drive the turbine Rotation, the rotation of the turbine drives the shaft, the fan and the compressor to work, which consumes a huge amount of energy and also loses a lot of heat energy, which reduces the power of the jet engine, increases the fuel consumption, and increases the noise. If you want to reduce fuel consumption, reduce noise, and improve Thrust, only by removing the turbine behind the combustion chamber, can the resistance be removed. The simple structure can increase the thrust, reduce fuel consum...

Claims

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Application Information

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IPC IPC(8): F02K5/00
CPCF02K5/00
Inventor 夏建国
Owner 夏建国
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