CN101893413A - Surface type coverage striking method and propulsion type bullet - Google Patents
Surface type coverage striking method and propulsion type bullet Download PDFInfo
- Publication number
- CN101893413A CN101893413A CN2010101758117A CN201010175811A CN101893413A CN 101893413 A CN101893413 A CN 101893413A CN 2010101758117 A CN2010101758117 A CN 2010101758117A CN 201010175811 A CN201010175811 A CN 201010175811A CN 101893413 A CN101893413 A CN 101893413A
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- bullet
- pusher
- fuse primer
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- propellant
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Abstract
The invention introduces a surface type coverage striking method and a propulsion type bullet, the surface type coverage striking method is realized by the propulsion type bullet transmitted by a conventional transmitter, and the propulsion type bullet carries out progressive and multi-propulsion and releases bullet bodies therein during the flight process, thereby gathering a plurality of the bullet bodies, carrying out surface type striking on flying space and a target region, having the characteristics of simple implementation, good sustained working performance and high resource utilization rate, and being capable of effectively improving the short-range defense and the striking capability against enemy of our army.
Description
Technical field
The present invention is a bullet class lift-off technology, belongs to the military weapon technical field.
Background technology
In present bullet class weapon delivery technology, see that with regard to the flight net synchronization capability feature of its bullet a class is that point type hits class, as the single-shot firearms, another kind of for wire strike class, as automatic gun and machine gun class running fire firearms, also have a class to hit class, as Shotgun for the face formula; For various types of cannons, guided missile, primary-secondary type guided missile, cluster bomb etc., though bigger damage area is arranged after arrival strikes target, but still point type in its flight course, the planar effect of its strike just just can embody after arriving the target area, for cluster bomb, be the airborne weapon that is used to enlarge to the ground installation damage area, do not possess the ability of the target of aerial and horizontal flight being implemented quick, the real-time strike of directive property; Hit weapon though Shotgun is an a kind of formula, effective range and remote destructive power are extremely limited; In the modern military technology, the heavier short range defense technique of looking in each national capital, and the face formula is hit technology, be to smash guided missile in closely, helicopter, the effective means of Fast Moving Objects such as low altitude aircraft, also can be used as and carry out regional effective means of hitting on a surface target, the quick firing gun technology is adopted in the short range defence mostly under present technical conditions, realize defence of face formula and the purpose of hitting with wire rapid fire or even multitube wire rapid fire scan mode, but because bullet is launched and the aloft time difference before and after in the wire rapid fire scan mode, can not really play the bullet that makes emission its flight space is carried out the effect that the face formula is defendd and the face formula is hit, with regard to " Metal Storm " technology of external high praise at present, poor because of not having on-the-spot filling capability continuation ability to work, though the bullet according to the emission some calculates shared launch time, draw the high inference of firing rate in its unit interval, but its actual bullet emission total amount is not high, therefore it is limited that it hits area, and discarded object is more in each emission back, and its resource utilization is lower; So, current techniques is necessary to do some improvement work.
Summary of the invention
In view of the foregoing, the object of the present invention is to provide a kind of formula coverage striking method and pusher bullet, can realize in flight course, forming face formula coverage striking, and have good sustained sex work ability and higher resource utilization flight space and target area when bullet.
For achieving the above object, the present invention introduces a kind of formula coverage striking method and pusher bullet, after it is characterized in that pusher bullet is by conventional transmitter emission, after propellant in the pusher bullet in the bodies at different levels is lighted a fire step by step, is broken out, realize step by step to pusher bullet propelling, bodies at different levels are opened the cabin step by step and discharge the bullet body of this grade body storage inside, the set of a plurality of bullet bodies that bodies at different levels discharge is step by step carried out face formula coverage striking to flight space and target area; In the pusher bullet multistage body and a self-desttruction equipment are arranged, there is one to advance and the storage internal weapon bays in every grade of body, one advances the chassis, a straight barrel type fuse primer, a spiral fuse primer, a plurality of bullet bodies, each fuse primer is that hollow and two ends are conducted, advancing the outer, chassis that a sealing ring is arranged, in straight barrel type fuse primer outside a plurality of empennages are arranged, each bullet body is streamlined and at its afterbody a plurality of empennages is arranged, in the space that advances and store up between internal weapon bays and the propelling chassis, be filled with propellant, in straight barrel type fuse primer and spiral fuse primer, be filled with and lead fiery agent, spiral fuse primer is arranged on propellant one side that advances and store up the internal weapon bays inner bottom part, one end of spiral fuse primer communicates with propellant space, another termination that is in the spiral fuse primer in the end one-level body of pusher bullet is by advancing and the hole of storage internal weapon bays bottom communicates with space outerpace, the inner space, a termination of straight barrel type fuse primer that is in the Kong Yuhou one-level body of the other end bottom propelling and storage internal weapon bays of the spiral fuse primer in the middle bodies at different levels of pusher bullet communicates, another termination of straight barrel type fuse primer communicates with space, propellant place by a hole that advances the chassis, each bullet body is outside and be positioned at and advance and storage internal weapon bays inside around being arranged on the straight barrel type fuse primer, advances the chassis to be arranged on to advance and the storage internal weapon bays is inner and be between propellant and the bullet body.
Operation principle of the present invention is: after described pusher bullet is by conventional transmitter emission, pusher bullet flies forward with certain rotation rotating speed, conventional transmitter described here is firearms, cannon, cannon and mortar etc., the pusher bullet fiery agent of leading that afterbody is led in the fire hole in emission is lighted, by after the spiral fuse primer time-delay propellant in the one-level body of end being lighted outburst, the gas that produces is pushed ahead the propelling of afterbody body and the propelling chassis in the storage internal weapon bays, and will advance and store up internal weapon bays to the rightabout promotion that advances the chassis operation, advance and store up internal weapon bays and advance oppositely moving of chassis, promptly make the part of propelling and the interior storage of storage internal weapon bays bullet body open the cabin after the disengaging, advance and the storage internal weapon bays in each bullet body under the force action of the rotation centrifugal force of pusher bullet and propulsion inertia force, promptly disperse to leave pusher bullet and reach oblique continuation flight forward, certain grade of body is when propellant is lighted outburst, also light the fiery agent of leading in the straight barrel type fuse primer that connects the previous stage body, light the fiery agent of leading in the spiral fuse primer of previous stage body by the fiery agent of leading in the straight barrel type fuse primer, so same process is carried out repeatedly continuously, promptly pusher bullet is produced repeatedly and advance, and each bullet body in the bodies at different levels opened the cabin step by step reach oblique flight forward after disperse breaking away from pusher bullet, the bullet body set that all fly out is the center with the flight axis direction of pusher bullet, tapered shape comes in spatial distribution and flies forward, each bullet body has the very little time difference awing, has promptly formed defence of face formula and strike to flight space and target; Advance and the storage internal weapon bays is and can repeatedly advancing acceleration to pusher bullet in the effect of propellant, will advance and store up internal weapon bays when it hits destructive power and open the cabin and emit each bullet body improving; Because described pusher bullet adopts conventional transmitter to launch, then there are good existing technical conditions guarantee and existing filling technology to utilize, also has continuation ability to work preferably, and after at every turn to pusher bullet emission, the discarded object that produces is identical when using with the routine of conventional transmitter, and is therefore higher to the utilization rate of resource.
Description of drawings
Fig. 1 is the face formula coverage striking method of one embodiment of the invention and the pusher bullet structure chart of pusher bullet.
Fig. 2 is the electronic ignition system pie graph in the pusher bullet of the present invention one face formula coverage striking method and pusher bullet.
The specific embodiment
Below be example explanation embodiments of the invention with the accompanying drawing:
Fig. 1 is the face formula coverage striking method of one embodiment of the invention and the pusher bullet structure chart of pusher bullet, this structure chart has shown a pusher bullet with three grades of bodies, what mark number 3～11 showed among the figure is interior each parts of end one-level body and the structure of this push type bullet, other bodies at different levels have identical parts and structure with end one-level body, and in accompanying drawing 1: 1-is the bullet of pusher bullet; 2-is a self-desttruction equipment, adopts the time-delay fuze destructor to form; 3-is the bullet body, adopts metal material to make streamlined contour; 4-adopts metal material processing to become disc-shape, and is drilled with an aperture in the centre for advancing the chassis; 5-is spiral fuse primer, adopts metal tube to make, and its inner hollow and two ends communicate; 6-adopts metal circular tube to make for advancing and the storage internal weapon bays, and the one end is opened, and the other end has base, and is drilled with an aperture on base; The propellant of 7-for filling adopts to advance to get final product with gunpowder; 8-is the straight barrel type fuse primer, adopts metal circular tube to make, and its inner hollow and two ends communicate; 9-is the empennage that is arranged on the straight barrel type fuse primer, adopts metal material to make; 10-is the empennage that is arranged on the bullet body, adopts metal material to make; 11-is arranged on the sealing ring that advances on the outer, chassis, adopts metal material to make; And, in straight barrel type fuse primer outside a plurality of empennages are arranged, each bullet body is streamlined and at its afterbody a plurality of empennages is arranged, in the space that advances and store up between internal weapon bays and the propelling chassis, be filled with propellant, in straight barrel type fuse primer and spiral fuse primer, be filled with and lead fiery agent, spiral fuse primer is arranged on propellant one side that advances and store up the internal weapon bays inner bottom part, one end of spiral fuse primer communicates with propellant space, another termination of spiral fuse primer of pusher bullet of end one-level that is in pusher bullet is by advancing and the hole of storage internal weapon bays bottom communicates with space outerpace, the other end of centre spiral fuse primers at different levels that is in pusher bullet is by advancing and the inner space, a termination of straight barrel type fuse primer of the Kong Yuhou one-level body of storage internal weapon bays bottom communicates, another termination of straight barrel type fuse primer communicates and communicates with space, propellant place with a hole that advances the chassis, each bullet body is outside and be positioned at and advance and storage internal weapon bays inside around being arranged on the straight barrel type fuse primer, advances the chassis to be arranged on to advance and the storage internal weapon bays is inner and be between propellant and the bullet body.
According to each parts of above-mentioned making, promptly obtain pusher bullet by structure shown in Figure 1 and above-mentioned explanation assembling, and with its as bullet be assemblied in corresponding, be filled with on the shell case of cast charge and initiator, adopt corresponding transmitter to be launched at last, promptly finish enforcement of the present invention.
The present invention has an electronic ignition system in pusher bullet, a pressure sensor is arranged in electronic ignition system, a velocity sensor, an acceleration transducer, a microprocessor, a plurality of electronic initiators, the voltage signal follower that detonates, the voltage signal follower that detonates has a plurality of voltage signal output ends that detonate, each electronic initiators is separately positioned in the interior space, propellant place of bodies at different levels, the electric signal input end of each electronic initiators also is connected pressure sensor with the different voltage signal output end that detonates of the voltage signal follower that detonates respectively, velocity sensor, the electrical signal of acceleration transducer is connected with one group of control signal input of microprocessor respectively, the work control end of voltage signal follower of detonating is connected with one group of control signal output of microprocessor respectively; The electric principle of electronic ignition system constitutes as shown in Figure 2, and wherein: (1), (2), (3) are respectively pressure sensor, velocity sensor and acceleration transducer; (4) be microprocessor; (5) be the voltage signal follower that detonates, the voltage signal follower that detonates has a plurality of voltage signal output ends that detonate; (6), (7), (8) are electronic initiators; Each electronic initiators is separately positioned in the space, propellant place of bodies at different levels; Adopt the advantage of electronic ignition system to be and can accurately to set and control the duration of ignition of the bodies at different levels of pusher bullet, distribution density that so just can the dispersion of antithetical phrase body be accurately controlled and is adjusted.
The present invention can also be that the bullet body in pusher bullet can be flame tracer, armor-piercing bullet, high-explosive projectile, firebomb, quench malicious bullet and mixed function bullet; Described mixed function bullet promptly refers to have the bullet body of multiple function, as: on the basis of armour-piercing, also have high quick-fried function, or on the basis of armour-piercing, also have and have combustion function, do like this, make purposes of the present invention more extensive.
The present invention can also be that the bullet body in pusher bullet can reach purposes as required and adopts various materials and make various sizes and shape, does like this, makes purposes of the present invention more extensive.
The present invention can also be that the bullet body in pusher bullet can be placed in the pusher bullet with various arrangement modes, as oblique laminated, ectonexine extended spread formula etc., can adjust distribution density and form that the bullet body disperses like this, make the present invention more practical.
The present invention has introduced a kind of formula coverage striking method and pusher bullet, the face formula coverage striking method of realizing by the pusher bullet of conventional transmitter emission, pusher bullet step by step, repeatedly advances in flight course and discharges wherein bullet body, the set that forms a plurality of bullet bodies is hit the face formula of flight space and target area, have implement simple, the continuous firing performance is good, the characteristics that resource utilization is high, the short range defence capability that can effectively improve my army reaches the striking capabilities to the enemy.
Claims (5)
1. a face formula coverage striking method and pusher bullet, after it is characterized in that pusher bullet is by conventional transmitter emission, after propellant in the pusher bullet in the bodies at different levels is lighted a fire step by step, is broken out, realize step by step to pusher bullet propelling, bodies at different levels are opened the cabin step by step and discharge the bullet body of this grade body storage inside, the set of a plurality of bullet bodies that bodies at different levels discharge is step by step carried out face formula coverage striking to flight space and target area; In the pusher bullet multistage body and a self-desttruction equipment are arranged, there is one to advance and the storage internal weapon bays in every grade of body, one advances the chassis, a straight barrel type fuse primer, a spiral fuse primer, a plurality of bullet bodies, each fuse primer is that hollow and two ends are conducted, advancing the outer, chassis that a sealing ring is arranged, in straight barrel type fuse primer outside a plurality of empennages are arranged, each bullet body is streamlined and at its afterbody a plurality of empennages is arranged, in the space that advances and store up between internal weapon bays and the propelling chassis, be filled with propellant, in straight barrel type fuse primer and spiral fuse primer, be filled with and lead fiery agent, spiral fuse primer is arranged on propellant one side that advances and store up the internal weapon bays inner bottom part, one end of spiral fuse primer communicates with propellant space, another termination that is in the spiral fuse primer in the end one-level body of pusher bullet is by advancing and the hole of storage internal weapon bays bottom communicates with space outerpace, the inner space, a termination of straight barrel type fuse primer that is in the Kong Yuhou one-level body of the other end bottom propelling and storage internal weapon bays of the spiral fuse primer in the middle bodies at different levels of pusher bullet communicates, another termination of straight barrel type fuse primer communicates with space, propellant place by a hole that advances the chassis, each bullet body is outside and be positioned at and advance and storage internal weapon bays inside around being arranged on the straight barrel type fuse primer, advances the chassis to be arranged on to advance and the storage internal weapon bays is inner and be between propellant and the bullet body.
2. as claimed in claim 1 formula coverage striking method and pusher bullet, it is characterized in that an electronic ignition system is arranged in the pusher bullet, a pressure sensor is arranged in electronic ignition system, a velocity sensor, an acceleration transducer, a microprocessor, a plurality of electronic initiators, the voltage signal follower that detonates, the voltage signal follower that detonates has a plurality of voltage signal output ends that detonate, each electronic initiators is separately positioned in the interior space, propellant place of bodies at different levels, the electric signal input end of each electronic initiators also is connected pressure sensor with the different voltage signal output end that detonates of the voltage signal follower that detonates respectively, velocity sensor, the electrical signal of acceleration transducer is connected with one group of control signal input of microprocessor respectively, the work control end of voltage signal follower of detonating is connected with one group of control signal output of microprocessor respectively.
3. as claimed in claim 1 formula coverage striking method and pusher bullet is characterized in that the bullet body in the pusher bullet can be flame tracer, armor-piercing bullet, high-explosive projectile, firebomb, quench malicious bullet and mixed function bullet.
4. as claimed in claim 1 formula coverage striking method and pusher bullet is characterized in that the bullet body in the pusher bullet can adopt various materials and make various sizes and shape.
5. as claim 1 or 2 or 3 or 4 described formula coverage striking methods and pusher bullet, it is characterized in that the bullet body in the pusher bullet can be placed in the pusher bullet with various arrangement modes.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010101758117A CN101893413A (en) | 2010-05-19 | 2010-05-19 | Surface type coverage striking method and propulsion type bullet |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010101758117A CN101893413A (en) | 2010-05-19 | 2010-05-19 | Surface type coverage striking method and propulsion type bullet |
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| Publication Number | Publication Date |
|---|---|
| CN101893413A true CN101893413A (en) | 2010-11-24 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2010101758117A Pending CN101893413A (en) | 2010-05-19 | 2010-05-19 | Surface type coverage striking method and propulsion type bullet |
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| Country | Link |
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| CN (1) | CN101893413A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103968714A (en) * | 2014-05-15 | 2014-08-06 | 刘少伟 | Defending bomb device hung in air |
| CN110036255A (en) * | 2016-10-06 | 2019-07-19 | 新技术全球***有限公司 | Biradical seat for mortar carrier vehicle transmission force to ground |
| CN110645838A (en) * | 2018-12-11 | 2020-01-03 | 陈黎 | Short-range defense device |
| CN113790639A (en) * | 2021-10-14 | 2021-12-14 | 湖南湘科科技研究院有限公司 | Efficient anti-unmanned aerial vehicle canister shot and working method thereof |
| CN115364400A (en) * | 2021-12-31 | 2022-11-22 | 南京工业职业技术大学 | Superfine dry powder fire extinguishing bomb for forest fire extinguishing |
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| WO2004005836A1 (en) * | 2002-07-05 | 2004-01-15 | Metal Storm Limited | Ignition arrangement for stacked projectiles |
| US7047885B1 (en) * | 2000-02-14 | 2006-05-23 | Alliant Techsystems Inc. | Multiple pulse cartridge ignition system |
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2010
- 2010-05-19 CN CN2010101758117A patent/CN101893413A/en active Pending
Patent Citations (6)
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| US694896A (en) * | 1900-12-21 | 1902-03-04 | Louis N D Williams | Gun-cartridge. |
| CN2095394U (en) * | 1990-10-06 | 1992-02-05 | 北京理工大学 | Intermittent after tow type hail-proof and rain rocket shrapnel |
| US7047885B1 (en) * | 2000-02-14 | 2006-05-23 | Alliant Techsystems Inc. | Multiple pulse cartridge ignition system |
| WO2004005836A1 (en) * | 2002-07-05 | 2004-01-15 | Metal Storm Limited | Ignition arrangement for stacked projectiles |
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Non-Patent Citations (1)
| Title |
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Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103968714A (en) * | 2014-05-15 | 2014-08-06 | 刘少伟 | Defending bomb device hung in air |
| CN110036255A (en) * | 2016-10-06 | 2019-07-19 | 新技术全球***有限公司 | Biradical seat for mortar carrier vehicle transmission force to ground |
| CN110036255B (en) * | 2016-10-06 | 2021-11-26 | 新技术全球***有限公司 | Omnidirectional dual base for mortar carrier vehicle |
| CN110645838A (en) * | 2018-12-11 | 2020-01-03 | 陈黎 | Short-range defense device |
| CN113790639A (en) * | 2021-10-14 | 2021-12-14 | 湖南湘科科技研究院有限公司 | Efficient anti-unmanned aerial vehicle canister shot and working method thereof |
| CN115364400A (en) * | 2021-12-31 | 2022-11-22 | 南京工业职业技术大学 | Superfine dry powder fire extinguishing bomb for forest fire extinguishing |
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Application publication date: 20101124 |