CN201426103Y - Novel aerospace power unit - Google Patents
Novel aerospace power unit Download PDFInfo
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- CN201426103Y CN201426103Y CN200920149662XU CN200920149662U CN201426103Y CN 201426103 Y CN201426103 Y CN 201426103Y CN 200920149662X U CN200920149662X U CN 200920149662XU CN 200920149662 U CN200920149662 U CN 200920149662U CN 201426103 Y CN201426103 Y CN 201426103Y
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Abstract
A novel aerospace power unit utilizes a magnetic field or electric field with a carrier or a magnetic field or electric field without a carrier to generate observable mechanical effect, namely a parallel uniform magnetic field or parallel uniform electric field and a vortex magnetic field or vortex electric field are interacted. A vortex magnetic field generated by utilizing a polar plate type capacitor and a magnetic field generated by a permanent magnet are interacted. The novel aerospace power unit can generate driving force without propellant.
Description
Technical field
The utility model relates to the new power of a kind of space flight, utilizes a kind of electromagnet phenomenon to produce motive force.
Background technology
Present human detection device carries out remote interplanetary flight and mainly adopts three kinds of means: one, utilize near the gravitation of celestial body to obtain certain speed and arrive at the destination; Two, utilize plasma engine to produce motive force; It is to produce more lasting motive force with a spot of plasma fuel, but the as received basis heating and decomposition need be obtained plasma, and the powerful electric field of usefulness quickens it then, sprays at a high speed from jet pipe.Three, utilize solar energy sailboard, produce light radiation pressure to the windsurfing by solar radiation and promote airship; The electronics that comes down in the electromagnetic field acceleration windsurfing obtains power, but its thrust is faint, and is of a high price.
At present technical the break-through point is arranged be: utilizes and between lack of parallelisme plate electric capacity, strengthen voltage and obtain unusual motive force, but its required voltage is generally more than several ten thousand volts.
Summary of the invention
Because limited fuel restriction spacecraft carries out remote interplanetary flight, can utilize a kind of electromagnet phenomenon to produce motive force.The utility model is to utilize magnetic field that carrier is arranged or electric field and DNAcarrier free magnetic field or electric field that observable mechanics effect takes place.Just parallel uniform magnetic field or parallel uniform electric field interact with magnetic field of volution or eddy electric field.Its technical scheme is: polar-plate-type electric capacity and a pair of permanent magnet at first are set, and two permanent magnets lay respectively at the both sides of polar-plate-type electric capacity; Described permanent magnet lays respectively at the left and right sides of closed screen, and polar-plate-type electric capacity lays respectively at the both sides up and down of screen; Also be provided with the reflector around the inboard of described screen; Center position at polar-plate-type electric capacity is provided with one group of soft magnetism ring; Be added with high-frequency pulse voltage Ui on the described polar-plate-type electric capacity.
Screen is to prevent that external magnetic field from doing negative work to rotational field; The reflector is to avoid rotational field to external radiation; Soft magnetism ring or hollow soft magnetism ball are on the plane that the magnetic field of permanent magnet and magnetic field of volution are all constrained in the soft magnetism ring or soft magnetism spheroid central authorities, avoid taking place Faraday effect so that its two interact.
Operation principle
1, microscopic explanation: principle end to end, the head repels each other, the tail tail repels each other, suction mutually end to end, just having begun rotational field does not move, occupied in the ring by original magnetic field or electric field, ring internal force and the opposite and equal and opposite in direction of ring external force all directions are after moment, because the interaction in the ring, make in the ring and can not arrive magnetic field or the electric field that (disappearances) acts on, owing to parallel flux lines or power line are provided on both side by magnet or charged object, thereby external magnetic field forms the geometric figure of a symmetry in one aspect.If the different concentric circles of radius is that rotational field annulus inside is failed to invade in interactional magnetic field, other still invade wherein but do not interact.Owing to the interaction of power, also there is momentum the field again, also sets up so active force is directly proportional with the intensity of field.
2 macroscopic views are explained: magnetic field can only interact with magnetic field, electric field can only interact with electric field, is not that any interaction does not take place in the field of same nature, and the direction of rotational field right half part is opposite with the parallel field direction, cancel out each other, and then the density of right-hand part another arena is weakened.The direction of the rotational field of left-half is identical with the direction of parallel field, and density increases, and the rotational field line of force of left-half is subjected to repelling rotational field is moved right.The interaction of any two fields may be summarized to be: (1) series connection equidirectional low close be gravitation to highly dense athletic performance.(2) series connection is highly dense in the other direction is repulsion to low close athletic performance.(3) in parallel equidirectional highly dense be repulsion to low close athletic performance.(4) it is gravitation to highly dense athletic performance that parallel connection opposite direction is hanged down close.More than the curvature that all will consider of four kinds of situations reverse.Series and parallel is represented two position relation, and equidirectional expression two magnetic directions are identical, represent that two magnetic directions are opposite in the other direction.
The utility model meets the following conditions: 1, the inseparable fragility of photon; 2, rotational field does not have carrier; When having the rotational field of carrier stressed, can drive the carrier spacecraft that flies out.The carrier in the magnetic field that excites as current in wire is the electric charge of motion.Can excite magnetic field of volution by the electric field (displacement current) that changes, but it not the carrier of magnetic field of volution yet.When evenly reducing as electric field, produce stable magnetic field B, E＞0 also reduces gradually, and up to E=0 constantly, B=K is constant.To E＜0 o'clock, B=K is constant.When evenly reducing as magnetic field, produce stable electric field E, Φ＞0 also reduces gradually, and up to Φ=0 constantly, E=K is constant.To Φ＜0 o'clock, E=K is constant.Change an E=0 or Φ=0 o'clock has stable rotational field in the same old way, illustrate that the rotational field by the differential relationship generation does not have carrier.Changing the field is not the carrier of rotational field.3, the direction of rotational field can not change; The 4 no thrusts that will avoid Faraday rotation effect to bring; 5 avoid external magnetic field that device is done negative work.
Between them the interaction of a kind of " inanition ", photon quality m ≈ 0, no matter whether m is 0, but thrust F exists, and it is the test that non-mechanical momentum is converted into mechanical momentum.Because the interaction between the electromagnetic field produces with the exchange virtual photon, illustrate that two magnetic fields have exchanged energy with the form of exchange virtual photon in 0＜t＜τ, τ=1/f, f are the frequency of photon.The part energy that is rotational field exchanges to steady magnetic field with the form of exchange virtual photon under active force.Δ E=h. Δ f, Δ f=f-f ', f ' is the photon frequency after reducing.
Beneficial effect: the utility model is that spacecraft does not need electric energy effectively to be converted into the device of motive force under the situation of propellant in starry sky.Can carry out remote interplanetary flight.
Description of drawings
Figure (1) is a structural representation of the present utility model.
Figure (2) is the another kind of structural representation of the utility model embodiment.
Figure (3) is steady magnetic field of the present utility model and magnetic field of volution interaction principle figure.
Wherein: the 1-permanent magnet; 2-soft magnetism ring; 3-polar-plate-type electric capacity; The 4-screen; The 5-reflector.
Embodiment
Figure (1) is a structural representation of the present utility model.
The new power of a kind of space flight is made up of permanent magnet 1 that is positioned at screen 4 inboards and polar-plate-type electric capacity 3; Described permanent magnet 1 lays respectively at the left and right sides of screen 4, and polar-plate-type electric capacity 3 lays respectively at the both sides up and down of screen, the two mutually orthogonal arrangement; Also be provided with reflector 5 around the inboard of described screen 4, center position is provided with one group of soft magnetism ring 2; Described polar-plate-type electric capacity 3 is added with high-frequency pulse voltage Ui.
High-frequency pulse voltage Ui adopts high frequency hard pulse voltage.
Described permanent magnet 1 adopts rubber magnet.
Embodiment
In figure (2),, be placed on the next door of polar-plate-type electric capacity 3 with the magnetic pole side of a bar-shaped magnet 1 interelectrode space facing to polar-plate-type electric capacity 3.Attract the principle of postrotational small magnetic needle to make permanent magnet 1 stressed according to electromotion straight wire, it is gravitation to highly dense athletic performance that opposite direction just in parallel is hanged down close.
Claims (5)
1, the new power of a kind of space flight is formed by being positioned at screen (4) inboard two permanent magnets (1) and polar-plate-type electric capacity (3); Two permanent magnets (1) lay respectively at the both sides of polar-plate-type electric capacity (3); Described two permanent magnets (1) lay respectively at the left and right sides of screen (4), and polar-plate-type electric capacity (3) lays respectively at the both sides up and down of screen; Also be provided with reflector (5) around the inboard of described screen (4); The center position of polar-plate-type electric capacity (3) is provided with one group of soft magnetism ring (2); Be added with high-frequency pulse voltage Ui on the described polar-plate-type electric capacity (3).
2, the new power of space flight according to claim 1 is characterized in that: described high-frequency pulse voltage Ui is a high frequency hard pulse voltage.
3, the new power of space flight according to claim 1 is characterized in that: described soft magnetism ring (2) is replaced by hollow soft magnetism ball.
4, the new power of space flight according to claim 1 is characterized in that: described permanent magnet (1) inner surface is a circular arc.
5, the new power of space flight according to claim 1 is characterized in that: the next door of described polar-plate-type electric capacity (3) is provided with a bar-shaped magnet, and its magnetic pole side is relative with polar-plate-type electric capacity (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN200920149662XU CN201426103Y (en) | 2009-04-15 | 2009-04-15 | Novel aerospace power unit |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN200920149662XU CN201426103Y (en) | 2009-04-15 | 2009-04-15 | Novel aerospace power unit |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201426103Y true CN201426103Y (en) | 2010-03-17 |
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ID=42025558
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN200920149662XU Expired - Fee Related CN201426103Y (en) | 2009-04-15 | 2009-04-15 | Novel aerospace power unit |
Country Status (1)
| Country | Link |
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| CN (1) | CN201426103Y (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111720282A (en) * | 2020-06-28 | 2020-09-29 | 哈尔滨工业大学 | Ionic wind thrust device based on needle-ring-net structure |
| CN112786308A (en) * | 2020-12-29 | 2021-05-11 | 西北核技术研究所 | Magnetic voltage connection electrode structure, peaking capacitor and megavolt electromagnetic pulse simulator |
-
2009
- 2009-04-15 CN CN200920149662XU patent/CN201426103Y/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111720282A (en) * | 2020-06-28 | 2020-09-29 | 哈尔滨工业大学 | Ionic wind thrust device based on needle-ring-net structure |
| CN112786308A (en) * | 2020-12-29 | 2021-05-11 | 西北核技术研究所 | Magnetic voltage connection electrode structure, peaking capacitor and megavolt electromagnetic pulse simulator |
| CN112786308B (en) * | 2020-12-29 | 2022-04-01 | 西北核技术研究所 | Magnetic voltage connection electrode structure, peaking capacitor and megavolt electromagnetic pulse simulator |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20100317 Termination date: 20120415 |