CN113251872A - Anti-unmanned aerial vehicle's soft ammunition structure of damaging - Google Patents
Anti-unmanned aerial vehicle's soft ammunition structure of damaging Download PDFInfo
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- CN113251872A CN113251872A CN202110273542.6A CN202110273542A CN113251872A CN 113251872 A CN113251872 A CN 113251872A CN 202110273542 A CN202110273542 A CN 202110273542A CN 113251872 A CN113251872 A CN 113251872A
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- bomb
- ammunition
- powder
- cartridge
- projectile body
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
- F42B12/56—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing discrete solid bodies
Abstract
The invention relates to a novel anti-soft damage ammunition structure of an unmanned aerial vehicle, which comprises a launching cartridge, primer, a combustible solid medicine plate, an ammunition body, a delay cartridge, a separated medicine bag, a catching net, an elastic belt and a tightening ring, wherein the launching cartridge is arranged on the primer; the primer is pressed at the center of the bottom of the emission cartridge, and the top end of the emission cartridge is provided with a combustible solid medicine plate; the projectile body is arranged above the combustible solid medicine plate and is divided into five symmetrical petals which are fixed by a projectile band and a tightening ring from the periphery; the separated medicine bag is filled in the medicine cavity; the lower end of the delay explosive tube penetrates through the bottom of the bomb body and is flush with the bottom, and the upper end of the delay explosive tube is placed in the bomb body and is intersected with the separated explosive package; the catching net is stacked at the middle rear part of the inner cavity of the projectile body, five traction wires are led out from the pentagon and are respectively connected with the tail part of the five-petal structure of the projectile body; the ammunition belongs to a soft damage anti-braking device, can retain target unmanned software and hardware information to the maximum extent, and has the advantages of simple structure, low processing cost, high capture probability, no influence on the environment, high reliability, no free fragment, extremely low collateral damage and improved safety.
Description
Technical Field
The invention belongs to the field of structural design of non-lethal soft-damage ammunition, and relates to a novel soft-damage ammunition structure of an anti-unmanned aerial vehicle, which is used for various anti-unmanned aerial vehicle tasks.
Background
In recent years, the unmanned aerial vehicle can be controlled to a certain extent by using soft damage means such as an aerial shooting rope net, an electronic interference gun, a waiting type interception net floating in the air and the like of the small unmanned aerial vehicle, but the action efficiency of the unmanned aerial vehicle is greatly influenced by the environment, and especially the unmanned aerial vehicle with beyond visual range, burstiness and bee colony type cannot be effectively controlled. Although the military kinetic energy bomb hard damage mode can effectively counter various unmanned aerial vehicles, the kinetic energy bombs emitted by the military kinetic energy bomb can cause a large amount of collateral damage, and the hard damage mode can only eliminate the unmanned aerial vehicles and cannot acquire the mission attempts of the unmanned aerial vehicles.
Disclosure of Invention
In order to solve the technical problem, the invention provides a soft damage ammunition structure for an anti-unmanned aerial vehicle, which can not only counter the unmanned aerial vehicle, but also reserve target unmanned software and hardware information to the maximum extent and eliminate potential safety hazards.
In order to achieve the purpose, the invention adopts the following technical scheme:
a soft damage ammunition structure of an anti-unmanned aerial vehicle comprises a launching component and a fighting component, wherein the launching component comprises a launching cartridge, primer, propellant powder and a combustible solid powder plate, and the fighting component comprises an ammunition body, delay powder, a delay powder pipe, a separation powder bag, a catching net, a belt and a tightening ring; the primer is pressed at the center of the bottom of the emission cartridge, the emission powder is arranged in the emission cartridge, and the top end of the emission cartridge is provided with a combustible solid powder plate; the projectile body is arranged above the combustible powder fixing plate, is divided into five symmetrical petals and is fixed from the periphery by a belt and a tightening ring, the belt is positioned at the bottom of the projectile body, the tightening ring is positioned at the head of the projectile body, the projectile body is made of conventional shell steel materials, and the appearance of the projectile body is similar to that of a conventional grenade; the separation medicine bag consists of a cotton cloth bag and a black gunpowder column and is filled in a separation medicine cavity in the position of a fastening ring at the head of the projectile body; the delay powder tube is arranged at the bottom of the projectile body, the lower end of the delay powder tube penetrates through the bottom of the projectile body and is flush with the bottom, the upper end of the delay powder tube is arranged in the projectile body and is intersected with the separated powder package, and the delay powder is arranged in the delay powder tube; the catching net is of a net regular pentagon structure and is stacked at the middle rear part of the inner cavity of the projectile body, five traction wires led out from the pentagon are respectively connected with the tail part of the five-petal structure of the projectile body and tied at the part of a belt pressing groove of the five-petal projectile body.
The size of the tightening ring structure is determined according to different launching strengths and the pressure required by the separation of the projectile body in the air, and the separation pressure of the projectiles with different calibers and different ranges is calculated by a design principle formula of the closed explosion container.
The catching net is woven by carbon fiber yarns.
The working principle is as follows: the delayed powder tube at the tail section of the high-temperature and high-pressure gas ignition bomb in the bore when in launching ignites the separated powder package by the delayed powder tube, black powder in the separated powder package burns to do work to cut off the fastening hoop and separate five sections of the head of the bomb body, windward airflow enters the bomb body to enable each section of the bomb body to generate overturning moment to cut off a rear bomb band, and finally the five sections of the bomb body are separated and fly and unfold the catching net along different directions under the action of inertia force; catch the net and fly to target unmanned aerial vehicle under five lamella projectile body pulls, with unmanned aerial vehicle aircraft bonnet in the net to through the passive winding of silk screen make unmanned aerial vehicle lose mobility until falling, accomplish anti-unmanned aerial vehicle task.
Compared with the prior art, the invention has the beneficial effects that:
1. belongs to a soft damage countermeasures device, and can reserve the unmanned software and hardware information of the target to the maximum extent;
2. the conventional ammunition launching platform and launching appliance are adopted, a matched device is not needed, and the use cost is greatly reduced;
3. the structure is simple, the projectile body does not need to be maintained, the number of parts is small, and the processing cost is low;
4. the explosive and fuse elements are not used, so that no dangerous accident occurs in the processes of storage, transportation and carrying, the production and the assembly are safe, and the explosive and fuse can be used by military and civilian;
5. the mesh physical winding is adopted to disable the target unmanned aerial vehicle, so that the capturing probability is high, no new attached product exists, the environment is not influenced, and the action process is not influenced by the environment;
6. the opening time of the catching net is controlled by timing combustion of the delay agent in the delay agent tube, the catching net is free from interference of external environment, the reliability is high, once the reverse bomb is launched, the delay agent can continuously burn until the separated explosive package is ignited, free fragments are avoided, collateral damage is extremely low, and the safety is improved.
Drawings
FIG. 1 is a diagram of a model of a rebound product of the present invention;
FIG. 2 is a two-dimensional assembled cross-sectional view of the present invention;
1. a body of elastomer; 2. primer; 3. propellant powder; 4. a firing cartridge; 5. a delay cartridge; 6. separating the medicine package; 7. a belt; 8. a catching net; 9. a combustible medicine fixing plate; 10. a delay agent; 11. and (5) tightening the hoop.
Detailed Description
The invention is further described below with reference to the figures and examples.
As shown in fig. 1 and 2, a soft damage ammunition structure of an anti-unmanned aerial vehicle comprises an ammunition body 1, a primer 2, a propellant powder 3, a propellant cartridge 4, a delay powder tube 5, a separation powder package 6, a cartridge belt 7, a catching net 8, a combustible powder fixing plate 9, a delay powder 10 and a tightening ring 11, wherein a propellant component comprises the primer 2, the propellant powder 3, the propellant cartridge 4 and the combustible powder fixing plate 9, and a battle component comprises the ammunition body 1, the delay powder 10, the delay powder tube 5, the separation powder package 6, the catching net 8, the cartridge belt 7 and the tightening ring 11; the primer 2 is pressed at the center of the bottom of the emission cartridge 4, the emission powder 3 is arranged in the emission cartridge 4, and the top end of the emission cartridge 4 is provided with a combustible solid powder plate 9; the projectile body 1 is arranged above the combustible powder fixing plate 9, the projectile body 1 is divided into five symmetrical petals and is fixed from the periphery by a belt and a hoop, the belt is positioned at the bottom of the projectile body, the hoop is positioned at the head of the projectile body, the projectile body 1 is made of conventional projectile steel materials, and the appearance of the projectile body is similar to that of a conventional grenade; the separation explosive bag 6 consists of a cotton cloth bag and a black explosive column and is filled in a separation explosive cavity in the position of the head fastening hoop 11 of the projectile body; the delay powder tube 5 is placed at the bottom of the projectile body 1, the lower end of the delay powder tube 5 penetrates through the bottom of the projectile body 1 and is flush with the bottom, the upper end of the delay powder tube 5 is placed in the projectile body and is intersected with the separated powder package 6, and the delay powder 10 is directly extruded into the delay powder tube 5; through the five-segment separation of the projectile body, the projectile body is respectively connected by five traction ropes of the catching net, and the fragment formed by the collapsed projectile band and the hooping ring has small mass, so that ground personnel or buildings in the fragment scattering range cannot be damaged; the opening time of the catching net is controlled by timing combustion of the delay agent in the delay agent pipe, the catching net is not interfered by external environment, the reliability is high, once the reverse bomb is launched, the delay agent can continuously burn until the separated explosive package is ignited, and the problem of cleaning safety of the non-separated bomb falling to the ground does not exist; through the stability of the projectile flying in the air by the belt and the tightening environmental protection certificate, the precision of the reverse process is improved.
The catching net 8 is a net-shaped regular pentagon structure woven by carbon fiber yarns, is stacked in the inner cavity of the projectile body 1, five traction yarns led out from the pentagon are respectively connected with the tail part of the five-petal structure of the projectile body and tied at the position of a belt pressing groove of the five-petal projectile body; the physical winding of the capture net ensures that the capture probability is high, no additional new product exists, the environment is not influenced, the action process is not influenced by the environment, and the use universality is increased.
Claims (3)
1. A soft damage ammunition structure of an anti-unmanned aerial vehicle is characterized by comprising a launching component and a fighting component, wherein the launching component comprises a launching cartridge (4), a primer (2), a propellant powder (3) and a combustible powder fixing plate (9), and the fighting component comprises an ammunition body (1), a delay powder (10), a delay powder pipe (5), a separation cartridge (6), a catching net (8), an ammunition band (7) and a tightening ring (11); the primer (2) is pressed at the center of the bottom of the emission cartridge (4), the emission powder (3) is arranged in the emission cartridge (4), and the top end of the emission cartridge (4) is provided with a combustible solid powder plate (9); the bomb body (1) is arranged above the combustible medicine fixing plate (9), the bomb body (1) is divided into five symmetrical petals and is fixed by a bomb belt (7) and a tightening ring (11) from the periphery, the bomb belt (7) is positioned at the bottom of the bomb body (1), the tightening ring (11) is positioned at the head of the bomb body (1), grooves are formed in the bomb body (1) corresponding to the bomb belt (7) and the tightening ring (11), the bomb body (1) is made of conventional bomb steel materials, and the appearance of the bomb body is similar to that of a conventional grenade; the separation explosive bag (6) consists of a cotton cloth bag and a black explosive column and is filled in a separation explosive cavity in the position of the head fastening hoop (11) of the projectile body (1); the delay powder tube (5) is arranged at the bottom of the projectile body (1), the lower end of the delay powder tube penetrates through the bottom of the projectile body (1) and is flush with the bottom, the upper end of the delay powder tube is arranged in the projectile body (1) and is intersected with the separated powder package (6), and the delay powder (10) is arranged in the delay powder tube (5); the catching net (8) is of a net regular pentagon structure and is stacked at the middle rear part of the inner cavity of the projectile body (1), five traction wires led out from the pentagon are respectively connected with the tail part of the five-petal structure of the projectile body and tied at the pressing groove of the belt (7) of the five-petal projectile body.
2. The anti-unmanned aerial vehicle soft damage ammunition structure as claimed in claim 1, wherein the clamping ring (11) can be replaced as required, the structural size is determined according to different launching strengths and the pressure required by the separation of the ammunition bodies in the air, and the separation pressure of the ammunition balls with different calibers and different ranges is calculated according to a design principle formula of a closed explosion container.
3. Anti-unmanned aerial vehicle's soft-defacing ammunition structure according to claim 1, characterized in that the catching net (8) is woven from carbon fiber filaments.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110273542.6A CN113251872A (en) | 2021-03-15 | 2021-03-15 | Anti-unmanned aerial vehicle's soft ammunition structure of damaging |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110273542.6A CN113251872A (en) | 2021-03-15 | 2021-03-15 | Anti-unmanned aerial vehicle's soft ammunition structure of damaging |
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| CN113251872A true CN113251872A (en) | 2021-08-13 |
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| CN202110273542.6A Pending CN113251872A (en) | 2021-03-15 | 2021-03-15 | Anti-unmanned aerial vehicle's soft ammunition structure of damaging |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114251981A (en) * | 2022-01-07 | 2022-03-29 | 湖南洪源远大科技有限公司 | Anti-unmanned aerial vehicle group ammunition |
| CN114812280A (en) * | 2022-05-24 | 2022-07-29 | 刘加凯 | Fixed-point air-blast anti-rotor unmanned aerial vehicle fiber bomb system |
| CN115247982A (en) * | 2021-12-31 | 2022-10-28 | 南京工业职业技术大学 | Novel harmless bird catching bomb for airport |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0872705A2 (en) * | 1997-04-19 | 1998-10-21 | Diehl Stiftung & Co. | Catching device for neutralising self-propelled mines |
| CN204027458U (en) * | 2014-07-23 | 2014-12-17 | 黄超 | Shelling netting cartridge |
| CN109029159A (en) * | 2018-09-29 | 2018-12-18 | 中国空空导弹研究院 | A kind of flying mesh injures formula missile armament |
| CN110108165A (en) * | 2019-05-10 | 2019-08-09 | 南京理工大学 | Novel net bullet is caught for what anti-unmanned plane caught that net device continuously emits |
| CN111551079A (en) * | 2020-05-20 | 2020-08-18 | 湖南兵器跃进机电有限公司 | Secondary gunpowder launching part, catching net bomb and secondary starting method thereof |
-
2021
- 2021-03-15 CN CN202110273542.6A patent/CN113251872A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0872705A2 (en) * | 1997-04-19 | 1998-10-21 | Diehl Stiftung & Co. | Catching device for neutralising self-propelled mines |
| CN204027458U (en) * | 2014-07-23 | 2014-12-17 | 黄超 | Shelling netting cartridge |
| CN109029159A (en) * | 2018-09-29 | 2018-12-18 | 中国空空导弹研究院 | A kind of flying mesh injures formula missile armament |
| CN110108165A (en) * | 2019-05-10 | 2019-08-09 | 南京理工大学 | Novel net bullet is caught for what anti-unmanned plane caught that net device continuously emits |
| CN111551079A (en) * | 2020-05-20 | 2020-08-18 | 湖南兵器跃进机电有限公司 | Secondary gunpowder launching part, catching net bomb and secondary starting method thereof |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115247982A (en) * | 2021-12-31 | 2022-10-28 | 南京工业职业技术大学 | Novel harmless bird catching bomb for airport |
| CN115247982B (en) * | 2021-12-31 | 2023-08-04 | 南京工业职业技术大学 | Novel harmless bird catching bomb for airport |
| CN114251981A (en) * | 2022-01-07 | 2022-03-29 | 湖南洪源远大科技有限公司 | Anti-unmanned aerial vehicle group ammunition |
| CN114812280A (en) * | 2022-05-24 | 2022-07-29 | 刘加凯 | Fixed-point air-blast anti-rotor unmanned aerial vehicle fiber bomb system |
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Application publication date: 20210813 |