CN203615825U - Electromagnetic launcher - Google Patents
Electromagnetic launcher Download PDFInfo
- Publication number
- CN203615825U CN203615825U CN201320296288.2U CN201320296288U CN203615825U CN 203615825 U CN203615825 U CN 203615825U CN 201320296288 U CN201320296288 U CN 201320296288U CN 203615825 U CN203615825 U CN 203615825U
- Authority
- CN
- China
- Prior art keywords
- cake
- missile
- support
- electromagnetic launcher
- track pipe
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The utility model relates to a device carrying out emission by using the electromagnetic principle. Provided is an electromagnetic launcher which comprises a support, a coil, a switch, a power supply, and a track pipe installed on the support; a rotating accelerator is arranged at the back of the support; edge wings are arranged on the periphery of a missile cake; and the track pipe is of a duckbilled type structure. The rotating accelerator used for high-speed rotation of the missile cake is arranged at the back of the track pipe, and when rotating and being accelerated to a certain rotating speed, the missile cake is allowed to fly out of the track pipe via the magnetic force at a fast and stable flight speed; and in order to facilitate the flight of the missile cake, the edge wings arranged on the periphery of the missile cake are used for controlling the height and the direction of the electromagnetic launcher.
Description
Technical field
The utility model relates to a kind of device that utilizes electromagnetic principle to launch.
Background technology
Mostly pellet injection is to adopt gunpowder back pressure formula and electric firing device at present, and gunpowder back pressure formula is spiraling after making bullet go out thorax in the bore that has rifling with the thrust of the blast generation of gunpowder; Electric firing device, although realized the object with electronic transmitting bullet, its whole result and circuit are comparatively complicated, trip rod multiple impact bullet, easily causes damage, and its finite energy because transmitting, the emission rate that makes bullet is not very high.
Summary of the invention
The technical problems to be solved in the utility model is: for overcoming the shortcoming and defect of prior art, provide a kind of electromagnetic launcher that can make bullet high-speed flight can have again smooth flight track.
The technical scheme that the utility model solves the problems of the technologies described above is: a kind of electromagnetic launcher, comprise support, and coil, switch, power supply, also comprises rack-mount orbitron, is provided with Spin-up device at the rear portion of support, is provided with the limit wing at the periphery that plays cake.
Described orbitron is Duckbill type.
Technique effect of the present utility model is: be provided with Spin-up device at the rear portion of orbitron, be used for playing cake High Rotation Speed, Spin-up makes to play cake by magnetic force thrust during to certain rotating speed and flies out from orbitron, flying speed is fast, steadily, for the ease of playing cake flight, be provided with the limit wing and control height and the direction of electromagnetic launcher at the periphery that plays cake.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model.
Fig. 2 is the enlarged diagram that plays cake.
In figure: 1, orbitron, 2, coil, 3, switch, 4, play cake, 6, Spin-up device, 7, power supply, 8, support, 9, the limit wing.
The specific embodiment
Below in conjunction with drawings and Examples, the present invention will be further described.
In Fig. 1 and Fig. 2, a kind of electromagnetic launcher, comprises support 8, coil 2, and switch 3, power supply 7, also comprises the orbitron 1 being arranged on support 8, is provided with Spin-up device 6 at the rear portion of support 8, the periphery that plays cake 4 is provided with the limit wing 9.
Described orbitron 1 is Duckbill type.
The utility model is the explanation that the embodiment that mentions with reference to the accompanying drawings carries out, and this is part embodiment wherein just, and those skilled in the art can obtain inspiration from the present embodiment, are out of shape and obtain other embodiment.Therefore, protection domain of the present utility model should be determined according to the protection domain of claim.
Claims (2)
1. an electromagnetic launcher, comprises support, coil, and switch, power supply, is characterized in that: also comprise rack-mount orbitron, be provided with Spin-up device at the rear portion of support, be provided with the limit wing at the periphery that plays cake.
2. electromagnetic launcher according to claim 1, is characterized in that: described orbitron is Duckbill type.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320296288.2U CN203615825U (en) | 2013-05-21 | 2013-05-21 | Electromagnetic launcher |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320296288.2U CN203615825U (en) | 2013-05-21 | 2013-05-21 | Electromagnetic launcher |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203615825U true CN203615825U (en) | 2014-05-28 |
Family
ID=50768461
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320296288.2U Expired - Fee Related CN203615825U (en) | 2013-05-21 | 2013-05-21 | Electromagnetic launcher |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203615825U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105605969A (en) * | 2016-01-06 | 2016-05-25 | 哈尔滨理工大学 | High-speed spiral electromagnetic emission device |
| CN105627821A (en) * | 2016-03-21 | 2016-06-01 | 西南交通大学 | Multi-pellet electromagnetic launching device |
| CN106370383A (en) * | 2016-11-29 | 2017-02-01 | 浙江工业大学 | Multistage accelerating shot blasting device |
| CN106546127A (en) * | 2016-10-10 | 2017-03-29 | 华中科技大学 | A kind of open-loop electromagnet catapult-launching gear |
-
2013
- 2013-05-21 CN CN201320296288.2U patent/CN203615825U/en not_active Expired - Fee Related
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105605969A (en) * | 2016-01-06 | 2016-05-25 | 哈尔滨理工大学 | High-speed spiral electromagnetic emission device |
| CN105605969B (en) * | 2016-01-06 | 2017-07-07 | 哈尔滨理工大学 | Highspeed spiral type electromagnetic launch system |
| CN105627821A (en) * | 2016-03-21 | 2016-06-01 | 西南交通大学 | Multi-pellet electromagnetic launching device |
| CN106546127A (en) * | 2016-10-10 | 2017-03-29 | 华中科技大学 | A kind of open-loop electromagnet catapult-launching gear |
| CN106370383A (en) * | 2016-11-29 | 2017-02-01 | 浙江工业大学 | Multistage accelerating shot blasting device |
| CN106370383B (en) * | 2016-11-29 | 2018-11-27 | 浙江工业大学 | Multistage accelerates shot-blast unit |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| DD01 | Delivery of document by public notice |
Addressee: Wang Xianwen Document name: Notification to Pay the Fees |
|
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20140528 Termination date: 20160521 |