CN101798998B - Annular atmospheric power machine - Google Patents
Annular atmospheric power machine Download PDFInfo
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- CN101798998B CN101798998B CN2010101225377A CN201010122537A CN101798998B CN 101798998 B CN101798998 B CN 101798998B CN 2010101225377 A CN2010101225377 A CN 2010101225377A CN 201010122537 A CN201010122537 A CN 201010122537A CN 101798998 B CN101798998 B CN 101798998B
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Abstract
The invention discloses an annular atmospheric power machine, which is a power machine for generating the power by the atmospheric pressure difference. An annular air passage is surrounded by an outer annular plate and an inner annular plate on an annular bottom plate; after the external air is ionized, the cationic air flow is blown to the annular passage. The high-voltage positive plates repel and continuously and circularly speed up the air flow, so that the atmospheric pressure on the soleplate is reduced and has the atmospheric pressure difference with the natural atmospheric pressure outside the lower side of the soleplate to form the power. An environment-friendly and energy-saving power supply enables an aircraft to have no engine and mechanical elements of rotation, transmission and motion, lift vertically, hover and fly in multiple directions; and the aircraft is simple and convenient to control and manipulate. Many layers can be connected in series or in parallel; one layer or a plurality of layers is/are adjusted aslant to generate the lifting force and the pushing force. The annular atmospheric power machine is specially suitable for boosters and thrusters of a disc-shaped aircraft, a rotor wing of a helicopter, a flying car, a marine and air aircraft and a land, marine and air aircraft. The invention can be widely applied to the national defense and military, the civil use, the agriculture and industry and the national economy.
Description
Technical field:
The present invention is a kind of motor, particularly a kind of power engine that produces power with atm difference.
Background technique:
The power engine kind is a lot, applies very extensive.Utilize atm difference to produce power, the mankind are application to some extent very early.Especially on aviation aircraft, aircraft wing utilizes top barometric pressure to produce lift less than following barometric pressure, and lifting airscrew namely produces lift, and thrust is arranged again.The 5th kind of high-lift new principle that occurs, only reduce barometric pressure on object, be below that a clean atmosphere is pressed, and utilizes this atm difference power, as lift and thrust, some patents arranged in recent years.Make working medium be ionized into ion, with electric field acceleration, produce high velocity air, the U.S. " father of rocket " Ge Dade had just put forward in 1906, and had completed original reason test.Now be applied on the Aerospace Satellite electrical rocket, the gas flow of ejection, ion current, plasma Flow Velocity can reach several kms of per second to several myriametres.Recently Plasma Stealth Technology is done intimately aboard, especially makes the air ionization technology very ripe, and the states such as the U.S., Russia, English, method have obtained some breakthrough achievements in the plasma research field.
Chinese invention patent " atmosphere power machine " CN1264790A of my application in 2000, reflected and utilized these very ripe technology to create atmosphere power machine.Introduce all-sidely and stepped on July 18th, 2008 in " science China net " (www.cichi.com) in " the new ideas aircraft " in " the reader world ".
Summary of the invention:
The present invention is on " atmosphere power machine " basis, has carried out larger improvement, and " atmosphere power machine " only utilized approximately 1/5th oxygen of duty gas, makes its part negative ionization.Gas flow directly sprays into the external world, and loss 90% multi-energy, cause again to external world dangerous, and use value is little.
The present invention, for solving these technical problems, has adopted following concrete technical measures.Surround the air-flow circuit by outer ring plate and inner ring plate on annular bottom plate, be connected to air-flow extend neck, sealing extend neck on outer ring plate.Make the electric drier fan that ambient air is blown into the air plasma generator by power supply by switch, after absorbing the negatron device, the positive aeroion air-flow enters annular pass, the high voltage that is produced by high-voltage generator again accesses on the positive plate that seals in extend neck, two like magnetic poles repel each other, constantly accelerate the positive aeroion air-flow of circulation, and by the potentiometer of belt switch, controlled.
The beneficial effect that produces like this, solved the shortcoming of prior art, by power supply make air-flow in circuit constantly circulation accelerate, environmental protection and energy saving, be conducive to improve airspeed, more reduce the atmospheric pressure on annular bottom plate, clean atmosphere is pressed and is produced larger atm difference power below base plate.Can make aircraft without motor, without mechanical parts such as rotation, transmission, motions, vertical takeoff and landing, can hover, and capable of flying in multi-direction is controlled manipulation simple and convenient.
Description of drawings:
Fig. 1 is top view of the present invention
Fig. 2 is front view of the present invention
Fig. 3 is electrical appliance part top view of the present invention
Fig. 4 is the high-voltage generator basic circuit diagram
in figure: 1, annular bottom plate, 2, outer ring plate, 3, inner ring plate, 4, the sealing extend neck, 5, the air-flow extend neck, 6, the high-voltage anode plate, 7, the electric drier fan, 8, the air plasma generator, 9, absorb the negatron device, 10, high-voltage generator, 11, power supply, 12, potentiometer with switch, 13, electric drier fan switch, 14, the High-Voltage Insulation electric wire, 15, the potentiometer resistance part is connected electric wire with circuit board, 16, potentiometer switch is connected electric wire with circuit board with power supply, 17, the electric drier fan is connected electric wire with power supply, a, ambient air, b, the positive aeroion air-flow
Embodiment is described in further detail invention below in conjunction with accompanying drawing:
With reference to Fig. 1, Fig. 2, annular bottom plate (1) is upper surrounds the air-flow circuit by outer ring plate (2) and inner ring plate (3), by the air-flow extend neck (5) that connects on outer ring plate (2), ambient air (a) is blown over air plasma generator (8) by electric drier fan (7), make its ionization, through absorbing negatron device (9), negatron is sponged, remaining positive aeroion air-flow (b) enters circuit.
With reference to Fig. 1, Fig. 2, Fig. 3, the positive high voltage that high-voltage generator (10) produces, received on sealing extend neck (4) interior high-voltage anode plates (6) positive ion in the positive aeroion air-flow (b) in positive electric field and circuit, two like magnetic poles repel each other by High-Voltage Insulation electric wire (14), give Driving force, make the constantly circulation acceleration of positive aeroion air-flow (b) in circuit.Cause the upper barometric pressure of annular bottom plate (1) in circuit to reduce, the clean atmosphere below annular bottom plate (1) is pressed and is produced atm difference power, as power.Electric drier fan (7) is connected electric wire (17) by the electric drier fan and is connected with power supply (11) with power supply, wherein fan switch (13) control by electric drier for one.Electric drier fan (7) is used as to start, while reaching certain speed, will be negative pressure in air-flow extend neck (5) when positive aeroion air-flow (b) in circuit, automatically suck ambient air (a), at this moment can close electric drier fan (7), save this part electric energy.Air plasma generator (8) can adopt the radioisotope raw materials such as polonium-210, curium-242, Strontium-90 to make air ionization, produces plasma, and this part need take Anti-Radiation Countermeasures and corresponding material.Absorb negatron device (9) varied, can adopt positive electrode plate to absorb, also can adopt the Aerospace Satellite electrical rocket to go out the negatron method.
With reference to Fig. 1, Fig. 3, Fig. 4, its K switch of potentiometer with switch (12) is connected electric wire (16) and is connected with circuit board with power supply (11) (E in circuit) with power supply with circuit board by potentiometer switch, the potentiometer resistance part is connected electric wire (15), potentiometer W in connecting circuit board by the potentiometer resistance part with circuit board.Triode BG, resistance R and potentiometer W, transformer B coil L
1, L
2Form vibrator circuit, the alternating voltage of generation is at L
3Induce higher alternating voltage, through capacitor C and the multistage multiplication of voltage of diode D, boost, at the positive high voltage e of final stage output.Potentiometer W is a biasing resistance part on BG pipe base stage, regulates it and can change the gain of amplifier, thereby make L
3Voltage change, cause high-voltage anode plate (6) potential change, and this has just changed in circuit positive aeroion air-flow (b) Driving force of repelling each other, thus the size variation of regulating and controlling annular atmosphere power machine power.The annular atmosphere power machine material should be selected high strength, and high voltage withstanding material, protect.
Application example:
The most suitable disc-shaped flying craft of doing of the present invention, as 2 meters of outer ring diameters, 16 meters of interior ring diameters, the annular bottom plate area is 11304 square metres.In circuit, the positive aeroion airspeed reaches 30 meter per seconds, approximately 63 kilograms of its lift.
The present invention has three kinds to improve the lift method: 1, strengthens annular base areas 2, increases the positive aeroion airspeed, and above example, airspeed is 100 meter per seconds, during 200 meter per second, lift is about respectively 701 kilograms, 2804 kilograms.3, annular atmosphere power machine can a plurality of series and parallels.As above the example serial connection is 5 layers, the 315 kilograms of lift of just having an appointment.Available one or more layers, can regulate inclination, produce and namely to have lift that thrust (quite lifting airscrew) is arranged again, whole electrical appliance part should be placed on suitable position easy to control.
Annular atmosphere power machine of the present invention, the electricity consumption environment-friendly and energy-saving, can replace lifting airscrew, and the saloon car of can flying and air-sea are dual-purpose, booster and the thruster of land, sea and air three use aircraft.Be widely used in national defense and military, civilian, the many aspects of industrial or agricultural and national economy.
Claims (1)
1. atmosphere power machine, comprise the electric drier fan (7) that sucks ambient air, electric drier fan switch (13), make the air plasma generator (8) of air ionization and absorb negatron device (9), high-voltage generator (10), power supply (11), potentiometer with switch (12), it is characterized in that: high-speed air positive ion stream reduces the lower outside clean atmosphere of barometric pressure and plate on plate and presses the annular bottom plate (1) that produces atm difference power, outer ring plate (2), inner ring plate (3) surrounds the air-flow circuit, be connected on outer ring plate (2) the air-flow extend neck (5) that place to produce the positive aeroion member and in the sealing extend neck (4) of acceleration positive aeroion high-voltage anode plate (6) is arranged.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010101225377A CN101798998B (en) | 2010-03-12 | 2010-03-12 | Annular atmospheric power machine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010101225377A CN101798998B (en) | 2010-03-12 | 2010-03-12 | Annular atmospheric power machine |
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| Publication Number | Publication Date |
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| CN101798998A CN101798998A (en) | 2010-08-11 |
| CN101798998B true CN101798998B (en) | 2013-11-13 |
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| CN2010101225377A Active CN101798998B (en) | 2010-03-12 | 2010-03-12 | Annular atmospheric power machine |
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Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101813074B (en) * | 2010-03-25 | 2013-01-09 | 张玉福 | Simplified annular atmosphere power machine |
| CN105691585A (en) * | 2015-12-30 | 2016-06-22 | 龚炳新 | Hydrogen ion gas-filled aircraft |
| CN107054657A (en) * | 2017-01-17 | 2017-08-18 | 南昌航空大学 | A kind of environmentally friendly unmanned plane for being used to administer haze |
| CN111425367A (en) * | 2019-01-10 | 2020-07-17 | 张玉福 | Step electrode annular big air power machine |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1993021475A1 (en) * | 1992-01-15 | 1993-10-28 | Valentin Semenovich Gorelykh | Method and device for production of energy |
| CN1120632A (en) * | 1994-10-12 | 1996-04-17 | 谷鹏 | Atmospheric compressed energy unit used for generating electricity or as wind tunnel |
| CN1264790A (en) * | 2000-02-24 | 2000-08-30 | 张玉福 | Atmospheric power machine |
| CN100360797C (en) * | 2006-08-25 | 2008-01-09 | 初志江 | Engine of air pressure difference |
-
2010
- 2010-03-12 CN CN2010101225377A patent/CN101798998B/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1993021475A1 (en) * | 1992-01-15 | 1993-10-28 | Valentin Semenovich Gorelykh | Method and device for production of energy |
| CN1120632A (en) * | 1994-10-12 | 1996-04-17 | 谷鹏 | Atmospheric compressed energy unit used for generating electricity or as wind tunnel |
| CN1264790A (en) * | 2000-02-24 | 2000-08-30 | 张玉福 | Atmospheric power machine |
| CN100360797C (en) * | 2006-08-25 | 2008-01-09 | 初志江 | Engine of air pressure difference |
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| CN101798998A (en) | 2010-08-11 |
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Effective date of registration: 20201120 Address after: Jingjiang City, Jiangsu province 214500 Maqiao town Taizhou city Lunluxi No. 1 Patentee after: JINGJIANG YUEDA SECURITY EQUIPMENT Co.,Ltd. Address before: 250014 Shandong city of Ji'nan province by the ten Science Institute of Shandong Academy of Sciences Road No. 19 dormitory room 9-1-601 Patentee before: Zhang Yufu |
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