CN207315585U - A kind of high-frequency and high-voltage electromagnetism microwave antigravity propulsion system - Google Patents
A kind of high-frequency and high-voltage electromagnetism microwave antigravity propulsion system Download PDFInfo
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- CN207315585U CN207315585U CN201721220029.6U CN201721220029U CN207315585U CN 207315585 U CN207315585 U CN 207315585U CN 201721220029 U CN201721220029 U CN 201721220029U CN 207315585 U CN207315585 U CN 207315585U
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- output terminal
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Abstract
The utility model discloses a kind of high-frequency and high-voltage electromagnetism microwave antigravity propulsion system, include power supply, rf control unit, radiator fan, propeller, High voltage output terminal and dual pressure controller, the power supply respectively with rf control unit, radiator fan is connected with dual pressure controller, the rf control unit is connected by conducting wire with propeller, dual pressure controller is connected by conducting wire with High voltage output terminal, control the voltage swing of High voltage output terminal output, current strength and output power, High voltage output terminal is connected by high-voltage conducting wires with propeller, the high voltage electric energy that High voltage output terminal exports is transferred to propeller.The utility model establishes the antigravity propulsion mode based on not against any chemical fuel, the plasma that this propulsion mode produces can absorbing radar wave, generate the additional benefit for radar invisible.So that the aircraft for being provided with this propulsion mode has the efficiency of evading radar detection.
Description
Technical field
It the utility model is related to antigravity and promote field, frequency microwave field, the intersection skill of asymmetry capacitor area
Art field, more particularly to a kind of high-frequency and high-voltage electromagnetism microwave antigravity propulsion system.
Background technology
Existing asymmetry capacitor under the loading effect of high-voltage electricity there is certain propulsive force and antigravity to imitate
Fruit, this antigravity effect come from the formation of ion wind.But ion wind thrust caused by existing asymmetry capacitor is very
Faint, Energy Efficiency Ratio is extremely low.In the case where increasing two-plate voltage, the thrust and antigravity effect of ion wind can be improved, but
When too big, cause the air dielectric layer between pole plate breakdown, it is impossible to play the effect of asymmetry capacitor.Therefore usually pass through
Increase the mode of polar plate voltage, improve the thrust of asymmetry capacitor, its room for promotion is very limited.
And RF emission system only, any thrust and antigravity effect can not be produced.The utility model is creatively
Both are combined so that for whole device under air normal pressure environment, the continual and steady radio frequency first appeared as mystery is micro-
Ripple electrical fire flame sprays, which is different from the faint state of pale blue of general air glow discharge flame instability, it stablizes bright
It is bright, in the case of daytime sunlight strong, can naked eyes as it can be seen that night it is more bright.
Since existing general asymmetry capacitor has the ability of ionization surrounding air, produce air plasma and
It is directed toward the faint thrust of large area pole plate.But the thrust that the high-frequency and high-voltage electromagnetism microwave antigravity propulsion system in this example produces,
The thrust bigger produced than existing general asymmetry capacitor, specific size are related to the microwave power that radio frequency source is launched.
The microwave power for adjusting radio frequency source transmitting adjusts the size of thrust output, easily realizes controllableization of thrust output.Cause
This utility model also can be as the research and development basis of complete electric thrust bob-weight force engine.
Utility model content
A kind of the defects of the utility model aim is exactly to make up prior art, there is provided high-frequency and high-voltage electromagnetism microwave bob-weight
Power propulsion system.
The utility model is achieved through the following technical solutions：
A kind of high-frequency and high-voltage electromagnetism microwave antigravity propulsion system, includes power supply, rf control unit, radiator fan, pushes away
Into device, High voltage output terminal and dual pressure controller, the power supply respectively with rf control unit, radiator fan and dual pressure controller
Connection, the rf control unit are connected by conducting wire with propeller, and dual pressure controller is connected by conducting wire and High voltage output terminal
Connect, voltage swing, current strength and the output power of the terminal output of control High voltage output, High voltage output terminal pass through high-voltage conducting wires
It is connected with propeller, the high voltage electric energy that High voltage output terminal exports is transferred to propeller, the radiator fan is positioned at propulsion
The side of device.
The propeller includes magnetron, small area transmitting pin, pressure-resistant insulating sleeve, coaxial connector, large area
Receiving cavity, fluid inlet directing plate, fluid outlet directing plate, magnetic control pipe holder and outlets direct board mount, the magnetic control
Pipe is installed on magnetic control pipe holder, the rf control unit described in the power input connection of magnetron, fluid inlet directing plate peace
Mounted in the lower end of magnetic control pipe holder, large area receiving cavity is installed on below fluid inlet directing plate, small area hair
Pin upper end is penetrated to be blunt nosed, lower end is tip, the blunt nosed emitting head that magnetron is connected by coaxial connector, and small area transmitting pin is worn
Cross fluid inlet directing plate to enter in large area receiving cavity, the tip of small area transmitting pin is located in large area receiving cavity
At the heart, the pressure-resistant insulating sleeve nesting is wrapped in the outside of small area transmitting pin, and High voltage output terminal passes through high-voltage conducting wires
It is connected, is provided with the bottom inside of large area receiving cavity by outlets direct board mount described with large area receiving cavity
Fluid outlet directing plate.
The power input connection rf control unit of magnetron, receives Power Control and tune that rf control unit grants it
Section；Small area transmitting pin one end is blunt nosed, and for connecting magnetron head, the other end is tip, for being received to large area
Cavity carries out ionic discharge；With with good conductivity coaxially connected between the blunt nosed magnetron head with connection of small area transmitting pin
Device locking connection is fixed；Pressure-resistant insulating sleeve nesting is wrapped in outside small area transmitting pin, prevents small area from launching pin from non-point
Externally discharge the part at end；Large area receiving cavity and times pressure cylinder or heap such as are bored at other High voltage output terminals with conducting wire
It is connected；The distance between two tips of large area receiving cavity inner wall and small area transmitting pin are equal to the radius R of large area receiving cavity, when
During energization work, bright electrical fire flame, and stronger ion wind can be produced in the metric space that this radius is R.
The magnetic control pipe holder, fluid inlet directing plate, fluid outlet directing plate, outlets direct board mount and it is pressure-resistant absolutely
Edge sleeve is fabricated by nonmetallic pressure-resistant insulating materials；Large area receiving cavity is manufactured by metal material with good conductivity
Form；Fluid outlet directing plate, pressure-resistant insulating sleeve are formed by the material manufacture with high-temperature stability；Small area launch pin by
Electric conductivity is good and there is the metal material of high-temperature stability to be fabricated.
The fluid inlet directing plate is middle porose ring-shaped structure, and has the curved cross section of c-type, is had
The gentle ability for flowing to small area transmitting pin needle point flowing of guiding ion wind.
Fluid outlet directing plate is up-small and down-big cone-shaped structure, and drainage circular arc is arranged at bottom, have guiding ion wind and
Ability of the air-flow to the output flow of large area receiving cavity bottom.
The High voltage output terminal bores outlet terminal for times pressure cylinder or heap.
During energization work, there is powerful ion wind, and produce thrust in the exit of large area receiving cavity bottom.
Environmental gas enters large area by the cavity on the inside of magnetic control pipe holder and the hole among fluid inlet directing plate
Receiving cavity simultaneously forms negative pressure at the hole among cavity and fluid inlet directing plate, produces certain vacuum degree, this negative pressure
The environmental gas outside large area receiving cavity is further attracted to enter its inner cavity with vacuum.
Small area transmitting both the pin and large area receiving cavity forms an asymmetry capacitor module.
Other High voltage output terminals, high-voltage conducting wires, and the dual pressure controller such as times pressure cylinder or heap cone form one
High pressure generator module.
The radio-frequency transmissions source component of the rf control unit, conducting wire, radiator fan, magnetron or other forms, coaxially connects
Connect device, pressure-resistant insulating sleeve, and small area transmitting pin and form a radiofrequency launcher.
The radiator fan is used for the radio-frequency transmissions source component radiating and cooling to magnetron or other forms, and radiating mode
The form of fan is not limited only to, such as water cooling component of other forms can also be changed into or cooled plate carries out being directed to microwave radio
The water cooling method of emitting module.
Asymmetry capacitor and radio-frequency transmissions antenna terminal are combined.
Function combination comprising asymmetry capacitor and radio-frequency transmissions antenna terminal, in the energization course of work, and
In the case of without the supply of other chemical fuels, it can launch to produce around pin in small area and stablize bright electrical fire flame, the electricity
Flame has propulsive force.
The size of the volume range size of electrical fire flame, light levels and jet propulsion power, the frequency supplied by adjusting radio frequency
Rate and power, and the mode of the output voltage of high pressure generator and electric current, can adjusted and control.
The thrust that the propeller is produced by bottom plasma injection, promotes as aircraft plasma antigravity and starts
During machine, the plasma that engine produces has the function that absorbing radar wave at the same time, aircraft can be protected to avoid some specific
The detection of radar on direction, realizes the Plasma Stealth function of aircraft so that aircraft has stealthy scouting, stealthy assault
Efficiency.
The conducting wire for forming small area transmitting pin should have suitable length, ensure by coaxial connector and small area hair
The antenna system of pin composition is penetrated, there is suitable matching impedance, and beneficial to the energy that radio frequency source is launched, can present to greatest extent
It is sent in discharge tip, without being reflected back magnetron.
In the case of keeping high voltage power supply output voltage constant, by the tranmitting frequency or the output that adjust the magnetron
Power, can adjust the electric current flowed through between asymmetry capacitor two-plate, the final injection speed for adjusting and controlling plasma
The output of the thrust of degree and propeller.
Input, output power calculate idea and method and are：Input the electric energy of the device and will be converted into and export the device
Energy, the energy of output includes thermal energy, luminous energy, mechanical kinetic energy and electromagenetic wave radiation energy, wherein the kinetic energy and thermal energy that export account for
Major part, that is, haveThe mechanical energy that interionic mutually collided and made jet motion is also converted into thermal energy
In the case of, electric energy which exports high pressure generator, Efficient Conversion is the mechanical energy that propulsion system finally obtains, that is, is represented
ForWherein parameter interpretation is：
The voltage loaded between U- asymmetry capacitor two-plates,
The electric current flowed through between I- asymmetry capacitor two-plates,
The resistance of gas ion medium between R- pole plates,
The quality of gas ion between m- pole plates,
Between R- pole plates between pole plate gas ion movement velocity.
During device energization operation, between two pole plates of asymmetry capacitor, very strong ion wind, ion can be produced
The thrust size that wind produces and the voltage of two interpolar of asymmetry capacitor loading, loop current related to loop current size
It is again related to the transmission power of radio frequency source.Therefore, we can by adjust the voltage of asymmetry capacitor, electric current and
Radio-frequency emission power, to adjust and control the thrust size that the device exports.When the ionic that complete electric push type is manufactured with it
During bob-weight force engine, it is possible to achieve controllableization and adjustable state of motor power output.
The utility model has the advantages that：1. full electric drive, it is not necessary to any other chemical fuel or gas it is combustion-supporting.No
Need to rely on the combustion-supporting of any third party's media operation gas and fuel, you can it is dynamic to produce the ionization igniting based on environmental gas
Make and ion wind propulsive force.
2. under normal pressure or hyperbaric environment can produce plasma torch and propulsive force, it is not necessary to as some plasmas are sent out
Raw device needs low pressure and vacuum discharge room environmental.
3. for general asymmetry capacitor, he can in the case of identical polar plate voltage, can load and
The electric current of tolerance bigger, without the air dielectric layer between puncturing two-plate, can be produced than general asymmetry more by two-plate
Big ion wind thrust.Moreover, the size of this ion wind thrust can be reached by adjusting the fed power in radio-frequency transmissions source
To controllable state.The power of radio-frequency transmissions source magnetron is bigger, and the electric current between asymmetry capacitor two-plate is got over
Greatly, the plasma torch obtained is stronger, ion wind thrust also bigger.
4. a high-voltage electromagnetic microwave plasma flame jet propulsion unit structure type can be flexible and changeable.As long as meet electrode
With energy supply requirement, which can be designed to multiple structural forms.This reality
With the propulsion system of a new simply basic version.More multi-form propulsion can be improved out on the basis of the utility model
Device, optimizes the aerodynamic arrangement of large area receiving cavity, so as to produce stronger Plasma propulsion power.
5. based on the sub- sparking mode such as the full electricity in the utility model, can also manufacture without gasoline, diesel oil or its
The internal combustion engine form engine of its chemical fuel supply, it is only necessary to drive compressed air to be lighted a fire with full electricity, driving internal combustion engine operating,
Produce mechanical output output.
6. based on the sub- sparking mode such as the full electricity in the utility model, can also manufacture without Aviation Fuel or other
The turbogenerator of chemical fuel supply, it is only necessary to drive compressed air to be lighted a fire with full electricity, driving turbogenerator operating, produces
Continue thrust and mechanical output output.
7. the utility model establishes the antigravity propulsion mode based on not against any chemical fuel, this propulsion
The plasma that mode produces can absorbing radar wave, generate the additional benefit for radar invisible.So that it is provided with this
The aircraft of propulsion mode has the efficiency of evading radar detection.
Brief description of the drawings
Fig. 1 is the structure diagram of the utility model.
Fig. 2 is propeller structure figure.
Embodiment
As shown in Figure 1, a kind of high-frequency and high-voltage electromagnetism microwave antigravity propulsion system, include power supply 1, rf control unit 2,
Radiator fan 4, propeller 6, High voltage output terminal 8 and dual pressure controller 9, the power supply 1 respectively with rf control unit 2, dissipate
Hot-air fan 4 and dual pressure controller 9 connect, and the rf control unit 2 is connected by conducting wire 3 with propeller 6, dual pressure controller 9
It is connected by conducting wire 3 with High voltage output terminal 8, voltage swing, current strength and the output work of 8 output of control High voltage output terminal
Rate, High voltage output terminal are connected with propeller 6 by high-voltage conducting wires 7, the high voltage electric energy that High voltage output terminal 8 exports are transferred to
Propeller 6, the radiator fan 4 are located at the side of propeller 6.
As shown in Fig. 2, the propeller 6 includes magnetron 5, small area transmitting pin 14, pressure-resistant insulating sleeve 15, same
Mandrel connector 17, large area receiving cavity 10, fluid inlet directing plate 16, fluid outlet directing plate 11,18 and of magnetic control pipe holder
Outlets direct board mount 13, the magnetron 5 are installed on magnetic control pipe holder 18, the power input connection institute of magnetron 5
The rf control unit 2 stated, fluid inlet directing plate 16 are installed on the lower end of magnetic control pipe holder 18, and large area receiving cavity 10 is installed
Below fluid inlet directing plate 16, the small area 14 upper end of transmitting pin is blunt nosed, and lower end is tip, blunt nosed by same
Mandrel connector 17 connects the emitting head of magnetron 5, and small area transmitting pin 14 connects through fluid inlet directing plate 16 into large area
Receive in cavity 10, the tip of small area transmitting pin 14 is located at the center of large area receiving cavity 10, the pressure-resistant insulation sleeve
15 nestings of cylinder are wrapped in the outside of small area transmitting pin 14, and High voltage output terminal 8 passes through high-voltage conducting wires 7 and large area receiving cavity
10 connections, are provided with the fluid outlet by outlets direct board mount 13 in the bottom inside of large area receiving cavity 10 and draw
Guide plate 11.
The magnetic control pipe holder 18, fluid inlet directing plate 16, fluid outlet directing plate 11, outlets direct board mount 13
It is fabricated with pressure-resistant insulating sleeve 15 by nonmetallic pressure-resistant insulating materials；Large area receiving cavity 10 is by with good conductivity
Metal material is fabricated；Small area launch that pin 14 is good by electric conductivity and metal material manufacture with high-temperature stability and
Into.
The fluid inlet directing plate 16 is middle porose ring-shaped structure, and has the curved cross section of c-type.
Fluid outlet directing plate 11 is up-small and down-big cone-shaped structure, and drainage circular arc is arranged at bottom.
The High voltage output terminal 8 bores outlet terminal for times pressure cylinder or heap.
Embodiment one：
Device power-up operation order is：First, dual pressure controller 9 is opened, allows times pressure cylinder 8 to launching 14 He of pin by small area
The asymmetry capacitor that large area receiving cavity 10 is formed is loaded into horizontal high voltage, allows it to be operated in corona of ions discharge mode
Under, and do not puncture air dielectric therein；Then, radiator fan and rf control unit, the radio frequency for allowing magnetron 5 to launch are opened
The transmission of electromagnetic field, radio-frequency maser and coaxial connector, launches stronger radio frequency electromagnetic field on 14 tip of small area transmitting pin,
So as to excite the air of plasma state, produce bright plasma torch, and greatly improve the generation of asymmetry capacitor from
Sub- thrust；Finally, rf control unit is adjusted by operating, to change the radio-frequency electromagnetic field intensity that magnetron 5 is launched, Jin Erke
The thrust size to be formed is sprayed to change the plasma antigravity of asymmetry capacitor generation.
Embodiment two：
By adjusting the electric current flowed through between asymmetry capacitor two-plate, the injection of plasma can be adjusted and controlled
Speed, and the thrust output that propeller 6 is final.
When the microwave for removing the transmitting of magnetron 5, when only retaining the high pressure of asymmetry capacitor, asymmetry capacitance is flowed through
The electric current of device has been reduced, while the voltage at capacitor both ends can remain unchanged；When increase radio frequency source 5 launch microwave intensity,
When the output voltage of asymmetric capacitor and other conditions remain unchanged, do not causing asymmetry capacitor high-voltage breakdown
In the case of, flow through the electric current of asymmetry capacitor increases therewith, finally causes the ion thrust of propeller 6 to export and carries therewith
It is high.
Claims (6)
- A kind of 1. high-frequency and high-voltage electromagnetism microwave antigravity propulsion system, it is characterised in that：Include power supply, rf control unit, dissipate Hot-air fan, propeller, High voltage output terminal and dual pressure controller, the power supply respectively with rf control unit, radiator fan and Dual pressure controller connects, and the rf control unit is connected by conducting wire with propeller, and dual pressure controller passes through conducting wire and high pressure Outlet terminal connects, and voltage swing, current strength and the output power of the terminal output of control High voltage output, High voltage output terminal are led to Cross high-voltage conducting wires to be connected with propeller, the high voltage electric energy that High voltage output terminal exports is transferred to propeller, the radiation air Fan is positioned at the side of propeller.
- A kind of 2. high-frequency and high-voltage electromagnetism microwave antigravity propulsion system according to claim 1, it is characterised in that：Described Propeller includes magnetron, small area transmitting pin, pressure-resistant insulating sleeve, coaxial connector, large area receiving cavity, fluid and enters Mouth directing plate, fluid outlet directing plate, magnetic control pipe holder and outlets direct board mount, the magnetron are installed on magnetron branch On frame, the rf control unit described in the power input connection of magnetron, fluid inlet directing plate is installed on magnetic control pipe holder Lower end, large area receiving cavity are installed on below fluid inlet directing plate, and the small area launches pin upper end to be blunt nosed, under Hold and pass through fluid inlet directing plate for tip, the blunt nosed emitting head that magnetron is connected by coaxial connector, small area transmitting pin Into in large area receiving cavity, the tip of small area transmitting pin is located at the center of large area receiving cavity, and described is pressure-resistant Insulating sleeve nesting is wrapped in the outside of small area transmitting pin, and High voltage output terminal passes through high-voltage conducting wires and large area receiving cavity Connection, the fluid outlet directing plate is provided with by outlets direct board mount in the bottom inside of large area receiving cavity.
- A kind of 3. high-frequency and high-voltage electromagnetism microwave antigravity propulsion system according to claim 2, it is characterised in that：Described Magnetic control pipe holder, fluid inlet directing plate, fluid outlet directing plate, outlets direct board mount and pressure-resistant insulating sleeve are by non-gold Belong to pressure-resistant insulating materials to be fabricated；Large area receiving cavity is fabricated by metal material with good conductivity；Small area is sent out Penetrate that pin is good by electric conductivity and metal material with high-temperature stability is fabricated.
- A kind of 4. high-frequency and high-voltage electromagnetism microwave antigravity propulsion system according to claim 2, it is characterised in that：Described Fluid inlet directing plate is middle porose ring-shaped structure, and has the curved cross section of c-type.
- A kind of 5. high-frequency and high-voltage electromagnetism microwave antigravity propulsion system according to claim 2, it is characterised in that：Fluid goes out Mouth directing plate is up-small and down-big cone-shaped structure, and drainage circular arc is arranged at bottom.
- A kind of 6. high-frequency and high-voltage electromagnetism microwave antigravity propulsion system according to claim 2, it is characterised in that：Described High voltage output terminal bores outlet terminal for times pressure cylinder or heap.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721220029.6U CN207315585U (en) | 2017-09-22 | 2017-09-22 | A kind of high-frequency and high-voltage electromagnetism microwave antigravity propulsion system |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721220029.6U CN207315585U (en) | 2017-09-22 | 2017-09-22 | A kind of high-frequency and high-voltage electromagnetism microwave antigravity propulsion system |
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| CN207315585U true CN207315585U (en) | 2018-05-04 |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107476945A (en) * | 2017-09-22 | 2017-12-15 | 中国科学院合肥物质科学研究院 | A kind of high-frequency and high-voltage electromagnetism microwave antigravity propulsion system |
| CN111765058A (en) * | 2019-04-02 | 2020-10-13 | 哈尔滨工业大学 | Cusp field thruster for microwave-enhanced auxiliary ionization |
-
2017
- 2017-09-22 CN CN201721220029.6U patent/CN207315585U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107476945A (en) * | 2017-09-22 | 2017-12-15 | 中国科学院合肥物质科学研究院 | A kind of high-frequency and high-voltage electromagnetism microwave antigravity propulsion system |
| CN107476945B (en) * | 2017-09-22 | 2023-08-11 | 中国科学院合肥物质科学研究院 | High-frequency high-voltage electromagnetic microwave antigravity propulsion system |
| CN111765058A (en) * | 2019-04-02 | 2020-10-13 | 哈尔滨工业大学 | Cusp field thruster for microwave-enhanced auxiliary ionization |
| CN111765058B (en) * | 2019-04-02 | 2022-07-05 | 哈尔滨工业大学 | Cusp field thruster for microwave-enhanced auxiliary ionization |
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