Gun, artillery and rocket jet engines, steam turbines, internal combustion engines and air vehicles with additional magnetic device

A technology of magnetism and magnets, which is used in the fields of guns, rockets, jet engines, steam turbines, internal combustion engines and aircrafts with additional magnetic devices, and can solve the problems of high temperature of combustion chamber, high speed of hot gas, and waste of energy.

Inactive Publication Date: 2016-11-23
田景华
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0014] The existing "pulse detonation engine" that is in the ascendant also has the problem of high temperature in the combustion chamber: "(7) Cooling problem: the speed of the hot gas after the detonation wave is extremely high, which causes an increase in the heat of the tube wall, so efficient cooling measures must be taken
However, a considerable part of the energy of these gases is not directly used to push the piston to do work, but is used to generate high temperature and high pressure in the gas itself, which is obviously a waste of energy
For example, according to "http: / / wenku.baidu.com / link?url=rMtf5-Y8b5RwZQwzEbO3zuPHbX8aEUoQN4EXmDShJ7T91KW_vi288WhFrsdNJC8BDYg4Ku-_zVSAiblQJfperV91JQN6CbvoNyMWbcFNA-W there are the following problems in the structure and principle of a jet engine with three belts or a diesel engine: " The internal energy (that is, the internal energy of the exhaust gas) accounts for more than half, which objectively limits the efficiency of the internal combustion engine to less than 50% (gasoline engine is 20% to 30%, diesel engine is 30% to 45%); the second is that the internal combustion engine has heat loss, Such as cylinders, pistons, etc. will still dissipate heat...
But causing huge pressure in these directions is a waste of energy! What's more, the huge pressure has greatly increased the requirements for the material, thickness and strength of the inner wall of the container under the high pressure of the gas in the eight major types of devices; it has also increased their cost and weight, etc.

Method used

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  • Gun, artillery and rocket jet engines, steam turbines, internal combustion engines and air vehicles with additional magnetic device
  • Gun, artillery and rocket jet engines, steam turbines, internal combustion engines and air vehicles with additional magnetic device
  • Gun, artillery and rocket jet engines, steam turbines, internal combustion engines and air vehicles with additional magnetic device

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Embodiment Construction

[0252] Object one of the present invention is implemented like this, according to " http: / / www.baike.com / wiki / magnet ": there are " solenoid, Helmholtz coil, electromagnet, bit magnet, permanent magnet, There are seven kinds of magnets including pulse field magnets and superconducting magnets; in addition, there are magnetic paints and / or magnetic paints, etc. Among the above eight kinds of magnets, "permanent magnets" and "magnetic paints or magnetic paints" do not require power consumption, so they are collectively referred to as "generalized permanent magnets". The remaining six kinds of "solenoids, Helmholtz coils, electromagnets, bit magnets, pulse field magnets, and superconducting magnets" that require power consumption are collectively referred to as "generalized electromagnets."

[0253] In Equation (15) regarding "magnetic field superposition", the source of magnetism, that is, the type of magnets, is not limited, nor is the number of magnets that can be superimposed...

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Abstract

The invention provides gun, artillery and rocket jet engines, steam turbines, internal combustion engines and air vehicles with an additional magnetic device. A magnet is included, translational motion, through Lorentz force, rotation and vibration of fluid molecules near the magnet in the direction of being perpendicular to the micro-flow direction of fluid are strongly inhibited, and pressure and temperature of the fluid molecules in the direction of being perpendicular to the micro-flow direction of the fluid are significantly lowered, so that the speed that the fluid molecules diffuse in the needed micro-flow direction is significantly increased. Viscous friction, turbulent shear stress, friction force and heat conduction in a boundary layer and shock waves, resistance generated by the shock waves and negative influences of heating on relative movement between air flow and an object are eliminated fundamentally in the microcosmic level or at least weakened greatly. By equipping the magnet on various gun, artillery and rocket engines, jet engines, turbines, gasoline engines, diesel engines and the like, radial pressure and temperature must be significantly lowered, the initial speed of pills is significantly increased, the power and the speed of the rock engines and the jet engines are increased, the energy utilization rate of the gas turbines, the turbines and the internal combustion engines is increased, and various resistances borne by the air vehicles and heating of the air vehicles are significantly reduced.

Description

technical field [0001] The invention belongs to using a special magnetic device to improve barrel weapons such as guns and cannons; improve various rocket engines and jet engines; improve various gas turbines and steam turbines; improve various diesel engines and gasoline engines; It is the technical field of related components in supersonic aircraft and other equipment and / or devices. Background technique [0002] Though the kind of existing firearms is various, the initial velocity of their firing bullet projectile is all quite limited. According to "http: / / lxyd.imech.ac.cn / in how fast the shell can fly" said: "...the initial velocity of the projectile when it leaves the muzzle): rifle 600-900 m / s, sniper rifle 1000-1200 m / s (there are very few that reach 1450 m / s)...." [0003] The existing metal storm weapon system can greatly improve the number of projectiles fired per unit time. But its principle of launching projectiles with traditional propellant powder is no diff...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H01F7/00F02M27/04
CPCY02T10/12
Inventor 田景华
Owner 田景华
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