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23 times hypersonic speed scramjet pulse engine

An engine, high-speed motion technology, applied in ramjet engines, mechanical equipment, etc., can solve problems such as slow motion and achieve the effect of no electricity

Inactive Publication Date: 2014-07-30
罗国沛
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] The current turbojet fan ramjet propels the missile aircraft to fly with the reverse thrust of a single high-pressure gas jet, and the movement speed is relatively slow

Method used

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  • 23 times hypersonic speed scramjet pulse engine
  • 23 times hypersonic speed scramjet pulse engine
  • 23 times hypersonic speed scramjet pulse engine

Examples

Experimental program
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Effect test

Embodiment Construction

[0034]Gongyuan medicine package 1 is composed of low-level explosives, intermediate explosives, and high-level explosives in layered proportions, or mixed packages, and the explosion generates kinetic energy. The starting tube 2 is contained in the power source cartridge 1, and the power source cartridge 1 is detonated. Telescopic strong spring 3 is connected on the turn pole 11 chute bar 22, and the back pressure chute bar 22 resets downwards. 4 retaining columns are fixed on the limit of the merit cylinder bowl 7, and the power source medicine bag 1 is offside. Positive and negative electric wire 5 is connected on the upper and lower garden periphery of starting tube 2 medicine cover plates 6, and the starting tube 2 of electrification detonation. Medicine cover plate 6, paper metal etc. are formed, connect and cover power source medicine bag 1, and power supply magnet 18 sucks. Gong cylinder bowl 7, high temperature resistant alloy material, adorns power source medicine b...

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Abstract

The invention relates to a scramjet pulse engine. The explosive power is controlled and converted into kinetic energy capable of driving missiles and aircrafts to move at a high speed, the thrust generated by incident shock waves of an impact energy cylinder cup and the reverse thrust generated by reflected shock waves are applied to push the missiles and aircrafts to move and fly at the 23 times hypersonic speed and 28,260 km / h, accordingly, any missile can not catch and any radar can not detect the missiles and aircrafts. The power of detonation wave front of explosives is 1010 watts per square cm, and the thrust generated by explosion of 1 kg TNT is 800,000 kg. A cover type scramjet pulse engine catapults the aircrafts to take off, and a buffer spring extends to catapult the aircrafts again. An energy storage catapult aircraft device uses the explosion of explosives to compress a high pressure spring to retract to store all energy of explosion, and then releases tens of meters of the compressed spring to extend and continuously force to catapult the aircrafts about more than 100 meters to take off. The scramjet pulse engine is superior to the electromagnetic catapult.

Description

technical field [0001] The present invention relates to an open type and cover type sccrater pulse engine, and the power of the open type engine to control the explosion of explosives and convert it into kinetic energy driving the high-speed motion of the missile aircraft, and the thrust generated by the incident shock wave of the cylinder bowl impacted by the explosion of the explosives and The anti-thrust generated by the reflected shock wave propels the missile aircraft to fly at a speed up to 23 times the hypersonic speed and 28260 km / h; the cover-type super-combustion pulse engine uses the new technology of engine cover ejection aircraft take-off and energy storage ejection aircraft take-off. Background technique [0002] The current turbojet fan ramjet propels the missile aircraft to fly with the reverse thrust of a single high-pressure gas jet, and the speed of movement is relatively slow. The ramjet first decelerates and pressurizes the high-speed airflow through the...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F02K7/10
Inventor 罗国沛
Owner 罗国沛
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