CN104787345A - Electromagnetic power space shuttle - Google Patents
Electromagnetic power space shuttle Download PDFInfo
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- CN104787345A CN104787345A CN201510209334.4A CN201510209334A CN104787345A CN 104787345 A CN104787345 A CN 104787345A CN 201510209334 A CN201510209334 A CN 201510209334A CN 104787345 A CN104787345 A CN 104787345A
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- space shuttle
- electromagnetic power
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- electric field
- power space
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
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Abstract
The invention belongs to the technical field of aircrafts, and relates to a space shuttle, in particular to an electromagnetic power space shuttle. According to the specific technical scheme, the electromagnetic power space shuttle comprises a shuttle body, a vertical lifting electromagnetic plate and a transverse horizontal motion electromagnetic plate, the vertical lifting electromagnetic plate controls lifting motion of the space shuttle, and the transverse horizontal motion electromagnetic plate controls transverse motion of the space shuttle. According to the electromagnetic power space shuttle, a negative electricity ion field inside an earth mantle layer is sufficiently utilized, negative electricity ions inside the space shuttle and negative electricity ions inside the mantle generate repulsive force, and the space shuttle is provided with a vertical lifting electricity repulsion device and also provided with a transverse motion magnetic field force device, so that the electromagnetic power space shuttle is quite practical. The electromagnetic power space shuttle is not affected by weather, has good economic benefits for emergency, disaster relief and transportation, is safer and more stable, can be widely applied and popularized and is a novel pioneer of transportation equipment in the future.
Description
Technical field
The invention belongs to vehicle technology field, relate to a kind of space shuttle, be specifically related to a kind of space shuttle of electromagnetic power.
Background technology
Existing aircraft is all utilize the antagonistic force on aerodynamics basis to produce propulsive force, its range of operation is only limitted in earth atmosphere, namely range of operation is only limitted in earth atmosphere, namely based on antagonistic force produce lift rocketry also must cruelly swollen from air based on, do not depart from pneumatic category yet.
Magnetic field of the prior art power mainly has application in magnetic suspension train, according to physics principle, the electric current in electricity is similar to due to the magnetic line of force in magnetic field, if electromagnet has silicon steel as the words of iron core, magnetic-field intensity will increase several times, so magnetic line of force the same with electric current be flow-like, there is the feature of fluid.Therefore, the magnetic force based on the magnetic suspension train under magnetic pole application force runs off quite serious, loses more than gain.The earth's electric field application force is then different, no matter uses or does not use, and the electric field of the earth is always constant, intensity stabilization and free of losses.
In addition, according to physical knowledge, the earth can be divided into the earth's crust, earth mantle and the earth's core three part, and for a large amount of negative ions is assembled in the mantle reservoir being in fluid, these negative ions are also the places that the earth produces magnetic pole.Therefore, the earth is a huge negative electricity inherently, and south poles has strong magnetic pole.
Summary of the invention
The present invention overcomes the deficiency that prior art exists, and aims to provide a kind of electromagnetic power space shuttle utilizing earth negative electricity subfield.
In order to solve the problems of the technologies described above, the technical solution used in the present invention is: a kind of electromagnetic power space shuttle, comprise body, be arranged on vertical lifting magnetic board in body and transverse translation magnetic board, vertical lifting magnetic board controls the dipping and heaving of space shuttle, and transverse translation magnetic board controls the cross motion of space shuttle.
Wherein, the structure of vertical lifting magnetic board is: comprise negative electric field lift plate, and the inside and outside two-layer of negative electric field lift plate is provided with insulating barrier, and insulating barrier can ensure that the negative electron in negative electric field lift plate can not be lost and leak outside.Negative electric field lift plate is loop configuration, the inner ring of negative electric field lift plate is provided with adjustable condenser, negative electric field lift plate is connected with adjustable condenser, adjustable condenser regulates the negative electron capacity in negative electric field lift plate, when the negative electron capacity in negative electric field lift plate is enough large, negative ion in negative electric field lift plate and mantle reservoir forms antagonistic force, and when this antagonistic force is greater than the gravity of space shuttle, space shuttle can rise.
The structure of transverse translation magnetic board is: body and the multiple adjustable electric magnets be arranged in body, adjustable electromagnetic bag is drawn together negative electricity circle and is arranged on the dielectric layers inside and outside negative electricity circle, positive pole battery core is inserted with in negative electricity circle, the outer ring of positive pole battery core is provided with magnet-wire cutter sweep, is controlled the magnetic force size produced in transverse translation magnetic board by magnet-wire cutter sweep.
Wherein, magnet-wire cutter sweep can rotate relative to negative electricity circle and regulate electromagnetic quantities.
Wherein, magnet-wire cutter sweep is silicon steel baffle liner, and silicon steel is as the iron core of magnet, and the intensity in magnetic field is large, the compact conformation of transverse translation magnetic board.
Wherein, silicon steel baffle liner is C type structure, the upper end of silicon steel baffle liner and lower end are all placed in the center of negative electricity circle, by the electromagnetic force regulating the fit angle of silicon steel baffle liner and negative electricity circle to regulate transverse translation magnetic board to produce, and then regulate the lateral stressed direction of body and stressed size.
Wherein, as preferably, transverse translation magnetic board is arranged on the wing of body,
The present invention compared with prior art has following beneficial effect: the present invention makes full use of the negative ion field in earth mantle reservoir, repulsive force is produced by the negative ion in space shuttle and the negative ion in earth mantle, space shuttle there is the electric repulsion device of vertical lifting, also there is the magnetic field force device of cross motion simultaneously, very practical.The present invention is not by meteorological effect, and for speedily carrying out rescue work, the disaster relief and transport all have good economic benefit, more safety and stable, and can be widely used, be also the pioneer of following new transport equipment.
Accompanying drawing explanation
Below in conjunction with accompanying drawing, the present invention will be further described in detail.
Fig. 1 is structural representation of the present invention.
Fig. 2 is the structural representation of vertical lifting magnetic board in Fig. 1.
Fig. 3 is the structural representation of transverse translation magnetic board in Fig. 1.
Fig. 4 is the inner structure schematic diagram 1 of transverse translation magnetic board in Fig. 3.
Fig. 5 is the inner structure schematic diagram 2 of transverse translation magnetic board in Fig. 3.
In figure: 1 is body, 2 is vertical lifting magnetic board, and 3 is transverse translation magnetic board, and 4 is negative electric field lift plate, and 5 is insulating barrier, and 6 is adjustable condenser, and 7 is adjustable electric magnet, and 8 is negative electricity circle, and 9 is positive pole battery core, and 10 is magnet-wire cutter sweep, and 11 is wing.
Detailed description of the invention
In conjunction with the accompanying drawings, the present invention is further detailed explanation, and accompanying drawing is the schematic diagram simplified, and only basic structure of the present invention is described in a schematic way, therefore it only shows the formation relevant with the present invention.
As Figure 1-5, a kind of electromagnetic power space shuttle, comprise body 1, be arranged on vertical lifting magnetic board 2 in body 1 and transverse translation magnetic board 3, vertical lifting magnetic board 2 controls the dipping and heaving of space shuttle, and transverse translation magnetic board controls the cross motion of space shuttle.
Wherein, the structure of vertical lifting magnetic board 2 is: comprise negative electric field lift plate 4, and the inside and outside two-layer of negative electric field lift plate 4 is provided with insulating barrier 5, and insulating barrier 5 can ensure that the negative electron in negative electric field lift plate 4 can not be lost and leak outside.Negative electric field lift plate 4 is loop configuration, the inner ring of negative electric field lift plate 4 is provided with adjustable condenser 6, negative electric field lift plate 4 is connected with adjustable condenser 6, negative electron capacity in adjustable condenser 6 pairs of negative electric field lift plates 4 regulates, when the negative electron capacity in negative electric field lift plate 4 is enough large, negative electric field lift plate 4 forms antagonistic force with the negative ion in mantle reservoir, and when this antagonistic force is greater than the gravity of space shuttle, space shuttle can rise.
The structure of transverse translation magnetic board 3 is: body 1 and the multiple adjustable electric magnets 7 be arranged in body 1, the dielectric layers 5 that adjustable electromagnetic bag is drawn together negative electricity circle 8 and is arranged on inside and outside negative electricity circle 8, positive pole battery core 9 is inserted with in negative electricity circle 8, the outer ring of positive pole battery core 9 is provided with magnet-wire cutter sweep 10, is controlled the magnetic force size produced in transverse translation magnetic board 3 by magnet-wire cutter sweep 10.
Wherein, magnet-wire cutter sweep 10 can rotate relative to negative electricity circle 8 and regulate electromagnetic quantities.
Wherein, magnet-wire cutter sweep 10 is silicon steel baffle liner, and silicon steel is as the iron core of magnet, and the intensity in magnetic field is large, the compact conformation of transverse translation magnetic board 3.
Wherein, silicon steel baffle liner is C type structure, the upper end of silicon steel baffle liner and lower end are all placed in the center of negative electricity circle 8, by the electromagnetic force regulating the fit angle of silicon steel baffle liner and negative electricity circle 8 to regulate transverse translation magnetic board 3 to produce, and then regulate the lateral stressed direction of body 1 and stressed size.
Wherein, as preferably, transverse translation magnetic board 3 is arranged on the wing 11 of body 1,
The present invention makes full use of the negative ion field in earth mantle reservoir, repulsive force is produced by the negative ion in space shuttle and the negative ion in earth mantle, space shuttle there is the electric repulsion device of vertical lifting, also have the magnetic field force device of cross motion simultaneously, very practical.The present invention is not by meteorological effect, and for speedily carrying out rescue work, the disaster relief and transport all have good economic benefit, more safety and stable, and can be widely used, be also the pioneer of following new transport equipment.
By reference to the accompanying drawings embodiments of the invention are explained in detail above, but the present invention is not limited to above-described embodiment, in the ken that those of ordinary skill in the art possess, can also makes a variety of changes under the prerequisite not departing from present inventive concept.
Claims (5)
1. an electromagnetic power space shuttle, it is characterized in that, comprise body (1), be arranged on the vertical lifting magnetic board (2) in body (1) and transverse translation magnetic board (3), the structure of described vertical lifting magnetic board (2) is: comprise negative electric field lift plate (4), the inside and outside two-layer of described negative electric field lift plate (4) is provided with insulating barrier (5), described negative electric field lift plate (4) is loop configuration, the inner ring of described negative electric field lift plate (4) is provided with adjustable condenser (6), described negative electric field lift plate (4) is connected with adjustable condenser (6), negative electron capacity in described negative electric field lift plate (4) is controlled by adjustable condenser (6), the structure of described transverse translation magnetic board (3) is: body (1) and the multiple adjustable electric magnets (7) be arranged in body (1), described adjustable electric magnet (7) comprises negative electricity circle (8) and is arranged on the dielectric layers (5) inside and outside negative electricity circle (8), positive pole battery core (9) is inserted with in described negative electricity circle (8), the outer ring of described positive pole battery core (9) is provided with magnet-wire cutter sweep (10).
2. a kind of electromagnetic power space shuttle according to claim 1, is characterized in that, described magnet-wire cutter sweep (10) can be rotated relative to negative electricity circle (8) and regulate electromagnetic quantities.
3. a kind of electromagnetic power space shuttle according to claim 2, is characterized in that, described magnet-wire cutter sweep (10) is silicon steel baffle liner.
4. a kind of electromagnetic power space shuttle according to claim 3, is characterized in that, described silicon steel baffle liner is C type structure, and the upper end of silicon steel baffle liner and lower end are all placed in the center of negative electricity circle (8).
5. a kind of electromagnetic power space shuttle according to claim 3, is characterized in that, described transverse translation magnetic board (3) is arranged on the wing (11) of body (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510209334.4A CN104787345A (en) | 2015-04-29 | 2015-04-29 | Electromagnetic power space shuttle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510209334.4A CN104787345A (en) | 2015-04-29 | 2015-04-29 | Electromagnetic power space shuttle |
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| Publication Number | Publication Date |
|---|---|
| CN104787345A true CN104787345A (en) | 2015-07-22 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510209334.4A Pending CN104787345A (en) | 2015-04-29 | 2015-04-29 | Electromagnetic power space shuttle |
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| Country | Link |
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| CN (1) | CN104787345A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111907732A (en) * | 2020-04-30 | 2020-11-10 | 蓝箭航天空间科技股份有限公司 | Space verification aircraft |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1325810A (en) * | 2001-05-31 | 2001-12-12 | 谭新民 | Flying vehicle with built-in magnetic power |
| EP1247737A2 (en) * | 2001-01-25 | 2002-10-09 | Albert Owen Sanders | Lift generating means for aircraft |
| CN103991559A (en) * | 2014-05-28 | 2014-08-20 | 中国人民解放军国防科学技术大学 | Hovering control method for Lorentz spacecraft |
-
2015
- 2015-04-29 CN CN201510209334.4A patent/CN104787345A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1247737A2 (en) * | 2001-01-25 | 2002-10-09 | Albert Owen Sanders | Lift generating means for aircraft |
| EP1247737A3 (en) * | 2001-01-25 | 2003-01-22 | Albert Owen Sanders | Lift generating means for aircraft |
| CN1325810A (en) * | 2001-05-31 | 2001-12-12 | 谭新民 | Flying vehicle with built-in magnetic power |
| CN103991559A (en) * | 2014-05-28 | 2014-08-20 | 中国人民解放军国防科学技术大学 | Hovering control method for Lorentz spacecraft |
Non-Patent Citations (3)
| Title |
|---|
| 刘有忠: "带同种电荷的物体相互排斥吗", 《昭通师专学报》 * |
| 张雄: "带同种电荷的物体一定相互排斥吗？", 《物理教学》 * |
| 朱浩: "点电荷与带同种电荷的金属导体一定相互排斥吗？", 《物理教师》 * |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111907732A (en) * | 2020-04-30 | 2020-11-10 | 蓝箭航天空间科技股份有限公司 | Space verification aircraft |
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Application publication date: 20150722 |