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High-frequency and high-voltage electromagnetic microwave antigravity propelling system

A high-frequency high-pressure, propulsion system technology, applied in thrust reversers, using plasma, machines/engines, etc., can solve problems such as inability to generate thrust and anti-gravity effects, limited lifting space, and breakdown of air medium layers.

Pending Publication Date: 2017-12-15
HEFEI INSTITUTES OF PHYSICAL SCIENCE - CHINESE ACAD OF SCI
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In the case of increasing the voltage of the two plates, the thrust and anti-gravity effect of the ion wind can be improved, but if it is too large, the air dielectric layer between the plates will be broken down, and the role of an asymmetric capacitor cannot be played.
Therefore, the thrust of the asymmetric capacitor is usually increased by increasing the plate voltage, and the improvement space is very limited.
[0003] And the radio frequency launch system alone cannot produce any thrust and anti-gravity effects

Method used

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Examples

Experimental program
Comparison scheme
Effect test

Embodiment approach 1

[0049] The start-up operation sequence of the equipment is as follows: First, open the high-voltage controller 9, let the pressure doubler cylinder 8 carry out high-voltage loading on the asymmetrical capacitor composed of the small-area emitting needle 14 and the large-area receiving cavity 10, and let it work in the ion corona Under the discharge mode, and do not break down the air medium therein; then, turn on the cooling fan and the radio frequency controller, let the radio frequency electromagnetic field emitted by the magnetron 5, the transmission of the radio frequency head and the coaxial connector, launch pin 14 in a small area A strong radio frequency electromagnetic field is emitted from the tip, thereby exciting the air in the plasma state, producing a bright plasma flame, and greatly increasing the ion thrust generated by the asymmetric capacitor; finally, by operating and adjusting the radio frequency controller, the magnetron 5 can be changed The intensity of the...

Embodiment approach 2

[0051] By adjusting the current flowing between the two plates of the asymmetrical capacitor, the ejection speed of the plasma and the final thrust output of the thruster 6 can be adjusted and controlled.

[0052] When removing the microwave emitted by the magnetron 5 and only retaining the high voltage of the asymmetric capacitor, the current flowing through the asymmetric capacitor is reduced, while the voltage at both ends of the capacitor can remain constant; when increasing the microwave emitted by the radio frequency source 5 When the intensity, the output voltage of the asymmetric capacitor and other conditions are kept constant, the current flowing through the asymmetric capacitor will increase without causing the high voltage breakdown of the asymmetric capacitor, and finally the ions of the thruster 6 The thrust output increases accordingly.

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Abstract

The invention discloses a high-frequency and high-voltage electromagnetic microwave antigravity propelling system. The high-frequency and high-voltage electromagnetic microwave antigravity propelling system comprises a power source, a radio frequency controller, a cooling fan, a propeller, a high-voltage output terminal and a high-voltage controller. The power source is connected with the radio frequency controller, the cooling fan and the high-voltage controller. The radio frequency controller is connected with the propeller through a wire. The high-voltage controller is connected with the high-voltage output terminal through a wire, the voltage, the current intensity and the output power output by the high-voltage output terminal are controlled, the high-voltage output terminal is connected with the propeller through a high-voltage wire, and high-voltage electric energy output by the high-voltage output terminal can be transmitted to the propeller. The antigravity propelling manner on the basis of independence from chemical fuel is established, plasma generated through the propelling manner can absorb radar waves, and the addition effect for radar concealment is generated. An aircraft with the propelling manner has the effect of radar detection avoiding.

Description

technical field [0001] The present invention relates to the intersecting technical fields of anti-gravity propulsion field, radio frequency microwave field and asymmetric capacitor field, in particular to a high-frequency high-voltage electromagnetic microwave anti-gravity propulsion system. Background technique [0002] The existing asymmetric capacitor has a certain propulsion force and anti-gravity effect under the action of high-voltage loading, and this anti-gravity effect originates from the formation of ion wind. However, the ion wind thrust produced by the existing asymmetric capacitor is very weak, and the energy efficiency ratio is extremely low. In the case of increasing the voltage of the two plates, the thrust and anti-gravity effect of the ion wind can be improved, but if it is too large, the air dielectric layer between the plates will be broken down, and the role of an asymmetric capacitor cannot be played. Therefore, the thrust of the asymmetric capacitor i...

Claims

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Application Information

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IPC IPC(8): F03H1/00
CPCF03H1/0081
Inventor 程翔宇黄鹏程陈文革孙玉平匡光力盛志高张燕
Owner HEFEI INSTITUTES OF PHYSICAL SCIENCE - CHINESE ACAD OF SCI