CN110726340A - Energy-gathering follow-up killing warhead - Google Patents
Energy-gathering follow-up killing warhead Download PDFInfo
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- CN110726340A CN110726340A CN201911162432.1A CN201911162432A CN110726340A CN 110726340 A CN110726340 A CN 110726340A CN 201911162432 A CN201911162432 A CN 201911162432A CN 110726340 A CN110726340 A CN 110726340A
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- warhead
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- 239000012634 fragment Substances 0.000 claims abstract description 18
- 239000000843 powder Substances 0.000 claims description 9
- 230000000694 effects Effects 0.000 abstract description 7
- 238000007906 compression Methods 0.000 abstract description 3
- 229910000831 Steel Inorganic materials 0.000 abstract description 2
- 230000006835 compression Effects 0.000 abstract description 2
- 230000000149 penetrating effect Effects 0.000 abstract description 2
- 239000010959 steel Substances 0.000 abstract description 2
- 238000005474 detonation Methods 0.000 description 9
- 239000002360 explosive Substances 0.000 description 4
- 238000006243 chemical reaction Methods 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 238000003825 pressing Methods 0.000 description 3
- 230000000644 propagated effect Effects 0.000 description 3
- 230000035939 shock Effects 0.000 description 3
- 229920002379 silicone rubber Polymers 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000000306 component Substances 0.000 description 1
- 239000008358 core component Substances 0.000 description 1
- 238000004880 explosion Methods 0.000 description 1
- 239000003292 glue Substances 0.000 description 1
- 230000007774 longterm Effects 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000002311 subsequent effect Effects 0.000 description 1
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Aviation & Aerospace Engineering (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Radar Systems Or Details Thereof (AREA)
Abstract
The invention provides an energy-gathering follow-up killing warhead which comprises a warhead shell, a top-cutting shaped charge liner, a warhead charge and a fuse, wherein the top-cutting shaped charge liner is arranged at the front end of the warhead shell, the warhead charge is arranged between the warhead shell and the top-cutting shaped charge liner, the fuse is arranged at the rear end of the warhead shell, a follow-up ring is arranged in the warhead shell, and the follow-up ring is clamped at the front end of the top-cutting shaped charge liner through a compression ring. The energy-gathering follow-up killing warhead adopts the energy-gathering effect to drive fragments to follow up by increasing a follow-up ring at the front end of the truncated-cone liner, so that the follow-up killing elements fly around after penetrating through the through holes on the armor steel plate, thereby killing the inside of the armor. On the premise of not increasing dosage, caliber of the warhead, weight and volume of the missile, the killing power is improved, the development trend of the warhead is met, the structure of the warhead is further simplified, the processing and forming performance is good, the cost is low, and the application prospect is wide.
Description
Technical Field
The invention belongs to the technical field of ammunition, and particularly relates to an energy-gathering follow-up killing warhead.
Background
The warhead is an important component of the missile and finally completes the fighting task of the missile, the multifunctional warhead for killing, breaking and the like is one of the main development directions of the warheads at home and abroad, and the warheads of the type fully improve the cost-effectiveness ratio of the warheads. At present, a warhead of the type is developed and assembled in the field of small missiles such as ground-to-air missiles, air-to-ground missiles, air-to-air missiles, flight rounds and the like.
The warhead is a core component of a missile damage target, and the damage radius, the depth of a broken armor and the subsequent effect capability of the broken armor of the warhead directly determine the damage efficiency of the missile. At present, the power of the warhead is improved mainly by researching novel high-energy explosives, novel high-density fragments and novel model cover materials, the research period is too long, and the stability of the novel materials cannot meet the requirement of long-term storage. Therefore, in order to improve the power of the missile, the traditional warhead usually increases the caliber of the warhead and the dosage. Meanwhile, the mass and the volume of the missile tend to increase, which makes the missile difficult to realize light weight and miniaturization.
Disclosure of Invention
In order to overcome the problems, the invention provides an energy-gathering follow-up killing warhead which can improve the power of the warhead and does not need to change the caliber and the dosage of the warhead too much, and the technical scheme is as follows:
the utility model provides an it kills warhead with advancing to gather, includes warhead casing, cuts top powder charge type cover, warhead powder charge and fuze, cut top powder charge type cover sets up in the front end of warhead casing, and warhead powder charge sets up between warhead casing and the top powder charge type cover, and the fuze sets up in the rear end of warhead casing, be equipped with in the warhead casing and advance the ring along with, advance the ring along with and pass through the clamping ring card in the front end of cutting top powder charge type cover.
Further, the follow-up ring is provided with a strip-shaped notch.
Further, the notches are uniformly distributed along the radial direction and/or the circumferential direction of the following ring.
Furthermore, the truncated-cone-shaped cover is a truncated-cone-shaped shell and is attached to the inner wall of the truncated-cone-shaped shell along with the feeding ring.
Furthermore, prefabricated fragments are filled between the follow-up ring and the truncated-cone-shaped cover.
Further, prefabricated fragments are filled between the warhead charge and the warhead shell.
Furthermore, the shape of the prefabricated fragments is one or the combination of a plurality of spheres, cylinders, cubic blocks and rhombohedrons.
The warhead charge is a warhead action energy source, when the detonator action initiates the warhead charge to generate detonation waves, the detonation waves are strong shock waves with high-speed chemical reaction regions, which are propagated in the explosive. The prefabricated fragments fly around at high speed under the action of detonation wave drive, and personnel outside the armor are killed. Meanwhile, under the action of the energy-gathering effect, the drug-shaped cover forms a damage element to penetrate a target to form an opening, the drug-shaped cover forms the damage element, the energy-gathering effect is torn and driven to move along with the advancing ring in the axial direction, and personnel and striking instrument equipment after the armor or the shelter is killed and damaged behind the opening of the armor or the shelter through the damage element.
The invention has the following beneficial effects: the energy-gathering follow-up killing warhead adopts the energy-gathering effect to drive fragments to follow up by increasing a follow-up ring at the front end of the truncated-cone liner, so that the follow-up killing elements fly around after penetrating through the through holes on the armor steel plate, thereby killing the inside of the armor. On the premise of not increasing dosage, caliber of the warhead, weight and volume of the missile, the killing power is improved, the development trend of the warhead is met, the structure of the warhead is further simplified, the processing and forming performance is good, the cost is low, and the application prospect is wide.
Drawings
FIG. 1 is a perspective view of the present invention;
FIG. 2 is a side view of the present invention;
in the figure: 1-warhead shell, 2-truncated-cone-shaped cover, 3-warhead charge, 4-fuze, 5-follow-up ring, 51-notch groove, 6-compression ring and 7-prefabricated fragment.
Detailed Description
The technical solution of the present invention will be further described in detail with reference to the following examples and accompanying drawings.
The energy-gathering follow-up killing warhead of the embodiment mainly comprises a warhead shell 1, a top-cutting liner 2, a warhead charge 3, a fuse 4, a follow-up ring 5, a pressure ring 6 and a prefabricated fragment 7. The top-cutting shaped charge liner 2 is arranged at the front end of the warhead shell 1, the warhead charge 3 is arranged between the warhead shell 1 and the top-cutting shaped charge liner 2, and the fuse 4 is arranged at the rear end of the warhead shell 1. Prefabricated fragments 7 are filled between the warhead charge 3 and the warhead shell 1 and between the following ring 5 and the truncated-cone-shaped cover 2. A follow-up ring 5 is arranged in the warhead shell 1, and the follow-up ring 5 is clamped at the front end of the truncated-cone-shaped cover 2 through a compression ring 6. The truncated-cone-shaped cover 2 is a truncated-cone-shaped shell, and is attached to the inner wall of the truncated-cone-shaped shell along with the feeding ring 5. The following ring 5 is provided with a strip-shaped notch 51, and the notch 51 is uniformly distributed along the circumferential direction of the following ring. The shape of the prefabricated fragments 7 can be one or the combination of a plurality of spheres, cylinders, cubic blocks and rhombohedrons.
The warhead shell 1 is a connecting part of the whole warhead, and the circumferential prefabricated fragments 7 are placed at corresponding positions through a die and fixed by special glue. The press-fit shaped warhead charge 3 is assembled to the warhead housing 1. The top-cutting shaped charge cover 2 and the following ring 5 are installed, when the top-cutting shaped charge cover is installed, the axis of the warhead charge 3, the axis of the warhead shell 1, the axis of the top-cutting shaped charge cover 2 and the axis of the following ring 5 are on the same straight line, then the top-cutting shaped charge cover is fixed by the pressing ring 6, when the pressing ring 6 is installed, silicon rubber is smeared around the threads to prevent the pressing ring 6 from loosening, and on the other hand, the front end of the warhead is sealed. Later, link to each other with detonator 4 through the screw thread, when installing detonator 4, scribble silicon rubber on the screw thread, prevent that the screw thread is not hard up, sealed warhead powder charge 2 again prevents it to wet.
The truncated liner 2 is the primary material forming the shaped jet, the payload charge 3 is the source of payload action energy, and the fuse 4 is the detonator for the payload charge 3. The warhead charge 3 will generate detonation waves after detonation, which are strong shock waves with high-speed chemical reaction zones propagated in the explosive. The detonation capability is transferred to the top-cutting liner 2, the top-cutting liner 2 is crushed by huge explosion energy and is converged in a smaller area in the axis direction to form a slender high-temperature high-pressure high-speed metal jet, so that a channel is opened on a target armor, and a path required by effective killing is opened for tearing and driving the follow-up ring 5 for energy-gathering effect.
The prefabricated fragments 7 are used for killing personnel outside the armor, when the fuse 4 acts to initiate the warhead charge 3 to generate detonation waves, and the detonation waves are strong shock waves with high-speed chemical reaction regions and are propagated in explosives. The prefabricated fragments 7 fly around at high speed under the action of detonation wave drive to kill personnel outside the armor.
The following ring 5 can form a following killing element, and the truncated liner 2 forms a damaging element under the energy gathering effect to penetrate the target armor to form a hole. When the truncated-cone-shaped cover 2 forms a damage element, the energy-gathering effect drives and tears the inlet ring 5 to move along the axial direction and enter the interior of the armor, the inlet ring 5 continuously tears into fragments in the process of leading to the interior of the armor, and the tearing direction is guided by the notch 51 to scatter around, so that target personnel after the armor can be killed and live in instruments and equipment.
Claims (7)
1. The utility model provides an it can along with killing and killing warhead to gather, includes warhead casing, cuts top shaped charge cover, warhead powder charge and fuze, cut top shaped charge cover and set up in the front end of warhead casing, and warhead powder charge sets up between warhead casing and the top shaped charge cover, and the fuze sets up in the rear end of warhead casing, its characterized in that: and a follow-in ring is arranged in the warhead shell and is clamped at the front end of the truncated-cone-shaped cover through a pressure ring.
2. The energy concentrating follow-on killing warhead of claim 1, wherein: the follow-up ring is provided with a strip-shaped notch.
3. The energy concentrating follow-on killing warhead of claim 2, wherein: the notches are uniformly distributed along the radial direction and/or the circumferential direction of the following ring.
4. The energy concentrating follow-on killing warhead of claim 1, wherein: the truncated-cone-shaped cover is a truncated-cone-shaped shell and is attached to the inner wall of the truncated-cone-shaped shell along with the feeding ring.
5. The energy concentrating follow-on killing warhead of claim 1, wherein: and a prefabricated fragment is filled between the following ring and the top-cutting shaped liner.
6. The energy concentrating follow-on killing warhead of claim 1, wherein: prefabricated fragments are filled between the warhead charge and the warhead shell.
7. The energy concentrating follow-on killer warhead according to any one of claims 5-6, wherein: the prefabricated fragments are in the shape of one or a combination of a plurality of spheres, cylinders, cubic blocks and rhombohedrons.
Priority Applications (1)
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CN201911162432.1A CN110726340A (en) | 2019-11-25 | 2019-11-25 | Energy-gathering follow-up killing warhead |
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CN201911162432.1A CN110726340A (en) | 2019-11-25 | 2019-11-25 | Energy-gathering follow-up killing warhead |
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Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111928738A (en) * | 2020-07-30 | 2020-11-13 | 南京理工大学 | Composite warhead device with adjustable damage power for killing broken armor |
CN112229279A (en) * | 2020-09-18 | 2021-01-15 | 西安近代化学研究所 | Liquid-phase charging warhead shell without using counterweight block, without changing charging amount and capable of adjusting mass center of mass |
CN112224412A (en) * | 2020-09-30 | 2021-01-15 | 北京理工大学 | Onboard anti-armor adsorbable warhead |
CN112414232A (en) * | 2020-11-05 | 2021-02-26 | 江西洪都航空工业股份有限公司 | Generation method of explosive-killing warhead flying angle and explosive-killing warhead |
CN114251983A (en) * | 2021-12-13 | 2022-03-29 | 北京理工大学 | Non-convolution energy-gathering explosion-killing multifunctional warhead |
CN114383474A (en) * | 2022-01-17 | 2022-04-22 | 中国工程物理研究院总体工程研究所 | Penetration and explosion killing multipurpose warhead |
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EP0218819A2 (en) * | 1985-07-25 | 1987-04-22 | Industrias Cardoen Limitada | Multipurpose bomb |
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CN211012680U (en) * | 2019-11-25 | 2020-07-14 | 湖南航天机电设备与特种材料研究所 | Energy-gathering follow-up killing warhead |
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2019
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Patent Citations (5)
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EP0218819A2 (en) * | 1985-07-25 | 1987-04-22 | Industrias Cardoen Limitada | Multipurpose bomb |
CN2310306Y (en) * | 1997-07-30 | 1999-03-10 | 薛小民 | Hollow explosive-filling armour-piercing part |
CN2521391Y (en) * | 2001-12-11 | 2002-11-20 | 河北第二机械厂 | Sand control perforating bullet for oil well use |
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Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111928738A (en) * | 2020-07-30 | 2020-11-13 | 南京理工大学 | Composite warhead device with adjustable damage power for killing broken armor |
CN112229279A (en) * | 2020-09-18 | 2021-01-15 | 西安近代化学研究所 | Liquid-phase charging warhead shell without using counterweight block, without changing charging amount and capable of adjusting mass center of mass |
CN112229279B (en) * | 2020-09-18 | 2022-08-19 | 西安近代化学研究所 | Liquid-phase powder-charging warhead shell device without using balancing weight, without changing charging amount and capable of adjusting mass and mass center |
CN112224412A (en) * | 2020-09-30 | 2021-01-15 | 北京理工大学 | Onboard anti-armor adsorbable warhead |
CN112224412B (en) * | 2020-09-30 | 2022-06-14 | 北京理工大学 | Onboard anti-armor adsorbable warhead |
CN112414232A (en) * | 2020-11-05 | 2021-02-26 | 江西洪都航空工业股份有限公司 | Generation method of explosive-killing warhead flying angle and explosive-killing warhead |
CN114251983A (en) * | 2021-12-13 | 2022-03-29 | 北京理工大学 | Non-convolution energy-gathering explosion-killing multifunctional warhead |
CN114251983B (en) * | 2021-12-13 | 2022-08-23 | 北京理工大学 | Non-convolution energy-gathering explosion-killing multifunctional warhead |
CN114383474A (en) * | 2022-01-17 | 2022-04-22 | 中国工程物理研究院总体工程研究所 | Penetration and explosion killing multipurpose warhead |
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