CN203422027U - Novel warhead structure - Google Patents
Novel warhead structure Download PDFInfo
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- CN203422027U CN203422027U CN201320385952.0U CN201320385952U CN203422027U CN 203422027 U CN203422027 U CN 203422027U CN 201320385952 U CN201320385952 U CN 201320385952U CN 203422027 U CN203422027 U CN 203422027U
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- penetration body
- warhead
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Abstract
The utility model relates to a novel warhead structure which structurally comprises a turbine generator, a penetration body, a grain, a connecting wire and a fuze. The penetration body serves as a cartridge case, an air inlet and an air outlet are formed in the front end of the penetration body, the air inlet and the air outlet are communicated with an inner cavity of the penetration body, the turbine generator is located in the front of the inner cavity of the penetration body, the fuze is located in the back of the inner cavity of the penetration body, and a connecting wire of the fuze is connected with a wire of the turbine generator. According to the novel warhead structure, the kinetic barrier breaking principle is adopted, all parts of a warhead are installed in the penetration body, a rectification cartridge case on the outer portion of the penetration body is eliminated, bomb-fuze integration is achieved, and the novel warhead structure can be applied to a small kinetic barrier breaking bomb. The novel warhead structure removes invalid weight, improves the effective mass ratio, and is simpler in structure. According to the design, the structure of a barrier breaking antipersonnel warhead is simplified, the novel warhead structure can be applied to small ammunitions with high requirements for weight, and therefore the novel warhead structure is more suitable for being applied to city street battles, close combats and anti-terrorism fights.
Description
Technical field
The utility model relates to a kind of weaponry, specifically a kind of novel structure of warhead.
Background technology
Warhead be all kinds of ammunitions and guided missile injure target finally injure unit, mainly by housing, destruction package, apparatus to cause bursting and safeties, formed.Modern war is had higher requirement to the lethal power of warhead or damage efficiency, also requires to optimize coordinating of fuse and warhead simultaneously.Barrier-breaking antipersonnel warhead a kind ofly penetrates target by kinetic energy, detonates after wearing barrier under fuse effect, forms high-explosive fragmentation, injures target effective force strength below and the bullet of weaponry.
For adapting to the battlefield surroundings of local war complexity and the needs of fight-terrorism warfare, existing barrier-breaking antipersonnel warhead is generally the tandem warhead that adopts multiple charge.Zhe Lei warhead by explosive fried wear obstacle, to realize fragmentation effect with entering to kill and wound bullet.Such as: street barricade/street fighting howitzer of the reaming bullet of the U.S., Germany and Muscovite aimed missile etc.Powder charge design and two fuses that this plural serial stage warhead has two or three independently, action principle is different, its complex structure, production cost is higher.And, the barrier-breaking mechanism of the barrier-breaking level of plural serial stage warhead (first order or first and second level) is by shaped-charge, blast perforating before target, and this will produce larger additional injuring before target, thus limited the use of this weapon in city street fighting and fight-terrorism warfare.
Summary of the invention
The purpose of this utility model is just to provide a kind of novel structure of warhead, the complex structure and the limited problem of effect that to solve plural serial stage warhead, exist.
The utility model is achieved in that a kind of novel structure of warhead, comprise turbogenerator, penetration body, powder column, connection wire and fuse, using described penetration body as shell case, front end at described penetration body has air admission hole and the steam vent communicating with penetration intracoelomic cavity, described turbogenerator is positioned at the front portion of described penetration intracoelomic cavity, described fuse is positioned at the rear portion of described penetration intracoelomic cavity, and the connecting line of described fuse and the wire of described turbogenerator link together.
Described fuse is threaded in the afterbody of described penetration intracoelomic cavity.
Front end at described penetration body has the air admission hole that blows described turbogenerator rotation.
All parts of the present utility model are all contained in penetration body, and penetration body is as the shell of warhead; Turbogenerator is positioned at the front portion of penetration intracoelomic cavity, and when projectile flight, the air admission hole of air-flow by penetration body blows turbine generates electricity turbogenerator, and electric energy is passed to fuse by connecting wire, makes fuze circuit work.
What the utility model adopted is kinetic energy barrier-breaking principle, and whole parts of warhead are installed in penetration body, have cancelled the rectification shell case of penetration external body, realized bullet, draw integrated, can be on small-sized kinetic energy barrier-breaking bullet adapted.The utility model has reduced inert weight, has improved effective mass ratio, and structure is simpler; The structure of barrier-breaking antipersonnel warhead had both been simplified in this design, was adapted at again weight and required to use on high Small ammunitions, thereby be more suitable for using in military operations in urban terrain, close combat and anti-probably operation.The utility model relies on turbogenerator generating that power supply is provided, and makes the circuit design of fuse more convenient.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model.
The specific embodiment
As shown in Figure 1, the utility model comprises turbogenerator 1, penetration body 2, powder column 3, fuse 5, penetration body 2 as shell case at outermost layer; At the front end of penetration body 2, have the air admission hole 7 of 2-4 inclinations that communicate with penetration intracoelomic cavity, and have a venthole 6 communicating with penetration intracoelomic cavity that quantity is identical, to form gas channel, blowing turbogenerator rotates, make motor obtain enough air flow powers, and be unlikely to weaken the intensity of penetration body head.Turbogenerator 1 is arranged on the front portion of penetration intracoelomic cavity, is secondly powder column 3, and fuse 5 is positioned at the rear portion of penetration intracoelomic cavity, links together with the tailing screw flight of penetration intracoelomic cavity.On the sidewall of penetration intracoelomic cavity, have axial wire casing 4, to accept the wire of turbogenerator 1, fuse 5 is after packing into, and the wire of the connecting line on it and turbogenerator 1 links together, and forms and is electrically connected to.
At the rear portion of penetration body 1 outer wall, get on the bus and be shaped with external screw thread, on being threaded, after empennage, form a complete bullet.
Claims (3)
1. a novel structure of warhead, comprise turbogenerator, penetration body, powder column, connection wire and fuse, it is characterized in that, using described penetration body as shell case, front end at described penetration body has air admission hole and the steam vent communicating with penetration intracoelomic cavity, described turbogenerator is positioned at the front portion of described penetration intracoelomic cavity, and described fuse is positioned at the rear portion of described penetration intracoelomic cavity, and the connecting line of described fuse and the wire of described turbogenerator link together.
2. novel structure of warhead according to claim 1, is characterized in that, described fuse is threaded in the afterbody of described penetration intracoelomic cavity.
3. novel structure of warhead according to claim 1, is characterized in that, at the front end of described penetration body, has and blows the air admission hole that described turbogenerator rotates.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201320385952.0U CN203422027U (en) | 2013-07-01 | 2013-07-01 | Novel warhead structure |
Applications Claiming Priority (1)
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CN201320385952.0U CN203422027U (en) | 2013-07-01 | 2013-07-01 | Novel warhead structure |
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CN203422027U true CN203422027U (en) | 2014-02-05 |
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CN201320385952.0U Expired - Lifetime CN203422027U (en) | 2013-07-01 | 2013-07-01 | Novel warhead structure |
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Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105043170A (en) * | 2015-08-04 | 2015-11-11 | 北京航天长征飞行器研究所 | Integrated type warhead |
CN105115367A (en) * | 2015-08-04 | 2015-12-02 | 北京航天长征飞行器研究所 | Partition plate type warhead cabin capable of carrying recovery storage devices |
CN105606469A (en) * | 2015-12-17 | 2016-05-25 | 北京理工大学 | Method for qualitative characterization of warhead penetrating property |
CN105115368B (en) * | 2015-06-04 | 2016-09-14 | 西安近代化学研究所 | A kind of gun launched missile weapon platform warhead |
KR101713529B1 (en) * | 2016-10-28 | 2017-03-08 | 주식회사 두레텍 | Bullets using a fluid of flowing surface of warhead and a method of maufacture |
CN108507425A (en) * | 2018-03-26 | 2018-09-07 | 西安工业大学 | A kind of magnetic susceptibility layer metering device for penetration fuse |
CN110108174A (en) * | 2019-04-28 | 2019-08-09 | 芜湖博高光电科技股份有限公司 | A kind of integration body fuze millimeter wave antenna structure |
CN111551077A (en) * | 2020-05-11 | 2020-08-18 | 西安近代化学研究所 | Thin shell adherable warhead fragment |
-
2013
- 2013-07-01 CN CN201320385952.0U patent/CN203422027U/en not_active Expired - Lifetime
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105115368B (en) * | 2015-06-04 | 2016-09-14 | 西安近代化学研究所 | A kind of gun launched missile weapon platform warhead |
CN105043170A (en) * | 2015-08-04 | 2015-11-11 | 北京航天长征飞行器研究所 | Integrated type warhead |
CN105115367A (en) * | 2015-08-04 | 2015-12-02 | 北京航天长征飞行器研究所 | Partition plate type warhead cabin capable of carrying recovery storage devices |
CN105043170B (en) * | 2015-08-04 | 2016-08-24 | 北京航天长征飞行器研究所 | A kind of monoblock type warhead |
CN105606469A (en) * | 2015-12-17 | 2016-05-25 | 北京理工大学 | Method for qualitative characterization of warhead penetrating property |
KR101713529B1 (en) * | 2016-10-28 | 2017-03-08 | 주식회사 두레텍 | Bullets using a fluid of flowing surface of warhead and a method of maufacture |
WO2018079957A1 (en) * | 2016-10-28 | 2018-05-03 | 주식회사 두레텍 | Bullet having bullet surface fluid inflow path and manufacturing method therefor |
CN108507425A (en) * | 2018-03-26 | 2018-09-07 | 西安工业大学 | A kind of magnetic susceptibility layer metering device for penetration fuse |
CN108507425B (en) * | 2018-03-26 | 2019-10-25 | 西安工业大学 | A kind of magnetic susceptibility layer metering device for penetration fuse |
CN110108174A (en) * | 2019-04-28 | 2019-08-09 | 芜湖博高光电科技股份有限公司 | A kind of integration body fuze millimeter wave antenna structure |
CN110108174B (en) * | 2019-04-28 | 2021-05-04 | 芜湖博高光电科技股份有限公司 | Integrated projectile body fuse millimeter wave antenna structure |
CN111551077A (en) * | 2020-05-11 | 2020-08-18 | 西安近代化学研究所 | Thin shell adherable warhead fragment |
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Granted publication date: 20140205 |
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CX01 | Expiry of patent term |