CN202442648U - Air defense projectile launcher - Google Patents
Air defense projectile launcher Download PDFInfo
- Publication number
- CN202442648U CN202442648U CN2012200396378U CN201220039637U CN202442648U CN 202442648 U CN202442648 U CN 202442648U CN 2012200396378 U CN2012200396378 U CN 2012200396378U CN 201220039637 U CN201220039637 U CN 201220039637U CN 202442648 U CN202442648 U CN 202442648U
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- CN
- China
- Prior art keywords
- air
- projectiles
- launch tube
- guide pipe
- bullet
- 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 discloses an air defense projectile launcher which comprises a launching guide pipe that is provided with a hopper-shaped magazine at the rear end, wherein spherical iron projectiles are filled in the hopper-shaped magazine; a plurality of groups of electromagnetic coils are arranged in a sequence from the rear part of the launching guide pipe to the front end of the launching guide pipe outside the launching guide pipe; and the electromagnetic coils are electrically connected with a power supply controller through a power supply conductor. By adopting the air defense projectile launcher, high kinetic energy iron projectiles are launched, so that the projectiles form a projectile curtain wall in close air, and air attack weapons are intercepted by utilizing the projectile curtain wall; and moreover, the air attack weapons are directly impacted and detonated by utilizing the kinetic energy of the projectiles, and aims of intercepting and destroying the attack of the air attack weapons comprising guided missiles, projectiles, bombs and the like are fulfilled.
Description
Technical field
The utility model belongs to close air defense weapon technical field, is specifically related to a kind of antiaircraft pellet injector.
Background technology
Air attack is the important means of modern war.Its main mode has missile attack, shell and bomb bombing etc.The antagonism air attack just must be used antiaircraft weapon.The antiaircraft weapon of existing antagonism missile attack mainly is to use air defence missile.Air defence missile relies on that precise guidance is man-to-man is tackling attacker at a distance, follows the trail of when intercepting offensive missile when air defence missile, and air defence missile relies on the explosive charge demolition offensive missile that detonates self-contained, reaches the purpose of antagonism air attack.The attack of antagonism shell or bomb does not have the effective weapons of system basically at present, can only adopt the mode of evading to avoid attack.
Summary of the invention
The purpose of the utility model is to provide a kind of antiaircraft pellet injector; It is with emission kinetic energy irony bullet; Make bullet closely form the bullet curtain wall in the air; Utilize bullet curtain wall interception offensive air weapon, and utilize the kinetic energy of bullet directly to clash into the ignition offensive air weapon, reach interception and destroy the purpose that offensive air weapons such as comprising guided missile, shell, bomb is attacked.
The technical scheme that realizes above-mentioned purpose is: a kind of antiaircraft pellet injector; It has one be equipped with the infundibulate magazine in the rear end launch tube; In the infundibulate magazine, be filled with spherical irony bullet; Front end in the outside of launch tube by rear portion to the launch tube of launch tube is arranged with the plurality of electromagnetic coil in proper order, and each solenoid is electrically connected with power-supply controller through current supply line
The bullet of this antiaircraft pellet injector is deposited in the magazine; Bullet relies on gravity to get into launch tube; The plurality of electromagnetic coil produces under the control of power-supply controller by the directed magnetic kinetic force that moves of launch tube rear portion to launch tube front end; Drive bullet in launch tube by the rear portion to mouth of pipe accelerated motion, accomplish outwards emission bullet.Form antiaircraft bullet curtain wall transmitter assembly with a plurality of transmitter multi packs, handle antiaircraft bullet curtain wall transmitter assembly and volley, can form antiaircraft bullet curtain wall.
Since the power-supply controller of this antiaircraft pellet injector be by launch tube rear portion to launch tube front end order successively to the solenoid power supply, the magnetic field that the solenoid group produces is the rectilinear motion magnetic field of spontaneous emission pipe rear portion to the orientation of launching the mouth of pipe.Thereby guaranteed that bullet is to get into launch tube from magazine all the time, outwards launches from the mouth of pipe.Open power-supply controller continuously, this antiaircraft pellet injector can be launched continuously.
The bullet of this antiaircraft pellet injector does not load explosive charge and other flammable and explosive substance, and bullet emission kinetic energy is electromagnetism kinetic energy, and emission process need not use various flammable and explosive substances, need not load any dangerous material in the transmitter yet.Therefore, the bullet of this antiaircraft pellet injector and transmitter have very high security in transportation, keeping and in using.
The bullet of this antiaircraft pellet injector is without any need for specific packing.Transportation, keeping and very easy to use.
The bullet of this antiaircraft pellet injector is deposited in the magazine with disordered state, and bullet relies on self gravitation under the situation of filling operation, getting into launch tube automatically, need not load operations such as bullet, percussion, igniting in the emission process.Therefore, this antiaircraft pellet injector can be realized for a long time emission continuously, forms continuous antiaircraft bullet curtain wall aloft.
Description of drawings
Accompanying drawing is this antiaircraft pellet injector structural representation.
The specific embodiment
Describe below in conjunction with the specific embodiment of accompanying drawing this antiaircraft pellet injector.
Like accompanying drawing; This antiaircraft pellet injector has the launch tube 2 of circular cross section; The infundibulate magazine 1 that is communicated with launch tube 2 is set above the rear end of launch tube 2, in infundibulate magazine 1, is filled with spherical irony bullet 3, plurality of electromagnetic coil 4 is installed in the outside of launch tube 2; This plurality of electromagnetic coil 4 is arranged by the front end of rear portion to the launch tube 2 of launch tube 2 in proper order, and each solenoid 4 is electrically connected with power-supply controller 5 through current supply line.
Claims (1)
1. antiaircraft pellet injector; It is characterized in that: it has a launch tube (2) at rear end assembling infundibulate magazine (1); In infundibulate magazine (1), be filled with spherical irony bullet (3); Front end in the outside of launch tube (2) by rear portion to the launch tube of launch tube is arranged with plurality of electromagnetic coil (4) in proper order, and each solenoid (4) is electrically connected with power-supply controller (5) through current supply line.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012200396378U CN202442648U (en) | 2012-02-04 | 2012-02-04 | Air defense projectile launcher |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012200396378U CN202442648U (en) | 2012-02-04 | 2012-02-04 | Air defense projectile launcher |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202442648U true CN202442648U (en) | 2012-09-19 |
Family
ID=46824092
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2012200396378U Expired - Fee Related CN202442648U (en) | 2012-02-04 | 2012-02-04 | Air defense projectile launcher |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202442648U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104457430A (en) * | 2014-11-05 | 2015-03-25 | 万家晨 | Electromagnetic defense method capable of being applied to external space layer |
| CN108387138A (en) * | 2018-02-07 | 2018-08-10 | 武汉大学 | Combined type asynchronous induction electromagnetic coil transmitter and its ignition method |
-
2012
- 2012-02-04 CN CN2012200396378U patent/CN202442648U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104457430A (en) * | 2014-11-05 | 2015-03-25 | 万家晨 | Electromagnetic defense method capable of being applied to external space layer |
| CN108387138A (en) * | 2018-02-07 | 2018-08-10 | 武汉大学 | Combined type asynchronous induction electromagnetic coil transmitter and its ignition method |
| CN108387138B (en) * | 2018-02-07 | 2019-12-10 | 武汉大学 | Combined asynchronous induction electromagnetic coil emitter and ignition method thereof |
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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: Li Lianzhong Document name: Notification of Termination of Patent Right |
|
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20120919 Termination date: 20140204 |