CN103994692B - A kind of electromagnetic launch system - Google Patents
A kind of electromagnetic launch system Download PDFInfo
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- CN103994692B CN103994692B CN201410255263.7A CN201410255263A CN103994692B CN 103994692 B CN103994692 B CN 103994692B CN 201410255263 A CN201410255263 A CN 201410255263A CN 103994692 B CN103994692 B CN 103994692B
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Abstract
A kind of electromagnetic launch system, belong to electromagnetic application technical field, the resource solving electromagnetic force acting function-repulsive interaction can not make full use of problem, technical scheme is: electric supply S interface is arranged in silicon rectifier module, module electrodes exports, power control switch K, line bag power interface is connected with active magnetic polar curve bag by wire, described active magnetic polar body is arranged on the central authorities of pedestal, launching carrier is arranged in launching trajectory, the passive natural magnetic pole N of launching carrier is placed in bottom launching carrier, and contact with active magnetic pole N, launching trajectory control is set in launching trajectory to bearing, be provided with magnetic force pressurized control bearing and launching carrier head tank, magnetic force pressurized control carriage spring.The present invention has the function-repulsive interaction that electromagnetic force to be done work and makes full use of, and defines well clean resource, the advantage such as to bring benefit to the people.
Description
Technical field
The invention belongs to electromagnetic application technical field, be specifically related to a kind of electromagnetic launch system with ejecting function utilizing electromagnetism repulsive interaction.
Background technology
Electromagnetic force a kind ofly clean does function source, and it is at modern communications, satellite, broadcast, TV, and the transmission of electromagnetic signal and the acting of electromagnetic force are carried out, for modern society has made very large contribution in the daily life aspect of communications and transportation, safety etc., another important acting function-repulsive interaction of electromagnetic force, we well do not use, and a kind of well clean resource does not form productivity, to bring benefit to the people.
Summary of the invention
The resource that the object of the invention is for solving electromagnetic force acting function-repulsive interaction can not make full use of, and provides a kind of electromagnetic launch system with ejecting function.
For achieving the above object, the technical solution adopted in the present invention is: a kind of electromagnetic launch system, be characterized in: comprise initiatively magnetic pole N (1), active magnetic polar body (2), pedestal (3), silicon rectifier module (4), module electrodes exports (5), power control switch K (6), line bag power interface (7), electric supply S interface (8), wire (9), active magnetic polar curve bag (10), the passive natural magnetic pole N (11) of launching carrier, launching trajectory control is to bearing (12), magnetic force pressurized control bearing (13), launching carrier head tank (14), magnetic force pressurized control carriage spring (15), launching carrier (16), launching trajectory (17), described electric supply S interface (8) is arranged in silicon rectifier module (4), module electrodes exports (5), power control switch K (6), line bag power interface (7) is connected with active magnetic polar curve bag (10) by wire (9), described active magnetic polar body (2) is arranged on the central authorities of pedestal (3), launching carrier (16) is arranged in launching trajectory (17), the passive natural magnetic pole N (11) of launching carrier is placed in launching carrier (16) bottom, and contact with active magnetic pole N (1), launching trajectory control is set in launching trajectory (17) to bearing (12), be provided with magnetic force pressurized control bearing (13), with launching carrier head tank (14), magnetic force pressurized control carriage spring (15).
Compared with prior art, the present invention's function-repulsive interaction that electromagnetic force done work makes full use of, and defines well clean resource, to bring benefit to the people.
Accompanying drawing explanation
Fig. 1 is structural representation of the present invention;
Fig. 2 is launching trajectory floor map of the present invention.
Detailed description of the invention
As shown in Figure 1 and Figure 2, in the present embodiment, a kind of electromagnetic launch system, comprises initiatively magnetic pole N1, active magnetic polar body 2, pedestal 3, silicon rectifier module 4, module electrodes exports 5, power control switch K6, line bag power interface 7, electric supply S interface 8, wire 9, active magnetic polar curve bag 10, the passive natural magnetic pole N11 of launching carrier, launching trajectory control to bearing 12, magnetic force pressurized control bearing 13, launching carrier head tank 14, magnetic force pressurized control carriage spring 15, launching carrier 16, launching trajectory 17, described electric supply S interface 8 is arranged in silicon rectifier module 4, module electrodes exports 5, power control switch K6, line bag power interface 7 is connected with active magnetic polar curve bag 10 by wire 9, described active magnetic polar body 2 is arranged on the central authorities of pedestal 3, launching carrier 16 is arranged in launching trajectory 17, the passive natural magnetic pole N11 of launching carrier is placed in bottom launching carrier 16, and contact with active magnetic pole N1, launching trajectory control is set in launching trajectory 17 to bearing 12, be provided with magnetic force pressurized control bearing 13, with launching carrier head tank 14, magnetic force pressurized control carriage spring 15.
The present invention, applied power source enters silicon rectifier module 4 by electric supply S interface 8 and carries out rectification, AC power is made to be converted to high-power DC power supply, 5 are exported again by module electrodes, power control switch K6, line bag power interface 7 is connected with active magnetic polar curve bag 10 by connection wire 9, electromagnetic force is produced under the effect of active magnetic polar body 2, launching carrier 16 fills in launching trajectory 17, the passive natural magnetic pole N11 of launching carrier is placed in bottom launching carrier 16, contact with active magnetic pole N1, the electromagnetic repulsive force produced under the effect of electric current between them, launching carrier 16 is launched.
In order to limit the irregular operation of electromagnetic repulsive force, we with equilateral triangle angle, are provided with launching trajectory control to bearing 12 to control its direction of motion and to reduce the resistance of motion in launching trajectory 17.In order to strengthen, control the ejecting function of electromagnetic force, we are with same equilateral triangle angle, stress to be provided with magnetic force pressurized control bearing 13, with launching carrier head tank 14, magnetic force pressurized control carriage spring 15, in launching carrier head tank 14, magnetic force pressurized control bearing 13 is under the elastic force effect of magnetic force pressurized control carriage spring 15, limit the careless effect of launching carrier 16 due to the mutually exclusive power of active magnetic pole N1 and the passive natural magnetic pole N11 of launching carrier, when the mutually exclusive power of electromagnetism produced under effect at electric current between active magnetic pole N1 and the passive natural magnetic pole N11 of launching carrier obtains certain pressure, just by launching trajectory 17, launching carrier 16 can be launched.
Claims (1)
1. an electromagnetic launch system, it is characterized in that: comprise initiatively magnetic pole N (1), active magnetic polar body (2), pedestal (3), silicon rectifier module (4), module electrodes exports (5), power control switch K (6), line bag power interface (7), electric supply S interface (8), wire (9), active magnetic polar curve bag (10), the passive natural magnetic pole N (11) of launching carrier, launching trajectory control is to bearing (12), magnetic force pressurized control bearing (13), launching carrier head tank (14), magnetic force pressurized control carriage spring (15), launching carrier (16), launching trajectory (17), described electric supply S interface (8) is arranged in silicon rectifier module (4), module electrodes exports (5), power control switch K (6), line bag power interface (7) is connected with active magnetic polar curve bag (10) by wire (9), described active magnetic polar body (2) is arranged on the central authorities of pedestal (3), launching carrier (16) is arranged in launching trajectory (17), the passive natural magnetic pole N (11) of launching carrier is placed in launching carrier (16) bottom, and contact with active magnetic pole N (1), launching trajectory control is set in launching trajectory (17) to bearing (12), be provided with magnetic force pressurized control bearing (13), with launching carrier head tank (14), magnetic force pressurized control carriage spring (15).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410255263.7A CN103994692B (en) | 2014-06-10 | 2014-06-10 | A kind of electromagnetic launch system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410255263.7A CN103994692B (en) | 2014-06-10 | 2014-06-10 | A kind of electromagnetic launch system |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103994692A CN103994692A (en) | 2014-08-20 |
| CN103994692B true CN103994692B (en) | 2015-08-26 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410255263.7A Active CN103994692B (en) | 2014-06-10 | 2014-06-10 | A kind of electromagnetic launch system |
Country Status (1)
| Country | Link |
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| CN (1) | CN103994692B (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106546127A (en) * | 2016-10-10 | 2017-03-29 | 华中科技大学 | A kind of open-loop electromagnet catapult-launching gear |
| CN109323618A (en) * | 2017-08-01 | 2019-02-12 | 邓志昌 | A kind of multistage electromagnetic launch system |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7966922B2 (en) * | 2007-05-24 | 2011-06-28 | Lockheed Martin Corporation | Electro-magnetic restraint |
| CN102226668A (en) * | 2009-11-02 | 2011-10-26 | 蔡春林 | Magnetic force cannon |
| CN102486357A (en) * | 2009-11-18 | 2012-06-06 | 蔡春林 | Vertical type magnetic force cannon |
| CN102645131A (en) * | 2011-02-22 | 2012-08-22 | 卓向东 | Catapult trigger device based on principle of repulsion of different polarities and attraction of like polarities |
| CN204115573U (en) * | 2014-06-10 | 2015-01-21 | 沁源县翔宇种植有限公司 | A kind of electromagnetic launch system |
-
2014
- 2014-06-10 CN CN201410255263.7A patent/CN103994692B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7966922B2 (en) * | 2007-05-24 | 2011-06-28 | Lockheed Martin Corporation | Electro-magnetic restraint |
| CN102226668A (en) * | 2009-11-02 | 2011-10-26 | 蔡春林 | Magnetic force cannon |
| CN102486357A (en) * | 2009-11-18 | 2012-06-06 | 蔡春林 | Vertical type magnetic force cannon |
| CN102645131A (en) * | 2011-02-22 | 2012-08-22 | 卓向东 | Catapult trigger device based on principle of repulsion of different polarities and attraction of like polarities |
| CN204115573U (en) * | 2014-06-10 | 2015-01-21 | 沁源县翔宇种植有限公司 | A kind of electromagnetic launch system |
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| CN103994692A (en) | 2014-08-20 |
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Effective date of registration: 20200721 Address after: 215500 Qiuzhen building, Southeast campus, Changshu Institute of technology, No. 99, Hushan Road, Changshu Southeast Economic Development Zone, Suzhou City, Jiangsu Province Patentee after: Changshu southeast high tech Venture Service Co., Ltd Address before: Shanxi city of Changzhi province Qinyuan 046505 Dao Zhen Guo Guo Dao Cun County Patentee before: QINYUAN COUNTY XIANGYU CULTIVATION Co.,Ltd. |