CN115479505A - Explosive device for increasing fragment density of warhead of killing and killing blasting - Google Patents

Explosive device for increasing fragment density of warhead of killing and killing blasting Download PDF

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Publication number
CN115479505A
CN115479505A CN202211107353.2A CN202211107353A CN115479505A CN 115479505 A CN115479505 A CN 115479505A CN 202211107353 A CN202211107353 A CN 202211107353A CN 115479505 A CN115479505 A CN 115479505A
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CN
China
Prior art keywords
detonation
explosive
warhead
shell
killing
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Granted
Application number
CN202211107353.2A
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Chinese (zh)
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CN115479505B (en
Inventor
沈慧铭
王涛
余文力
王金涛
薛海建
杭贵云
刘欣
张小宁
张青
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Rocket Force University of Engineering of PLA
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Rocket Force University of Engineering of PLA
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Priority to CN202211107353.2A priority Critical patent/CN115479505B/en
Publication of CN115479505A publication Critical patent/CN115479505A/en
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Publication of CN115479505B publication Critical patent/CN115479505B/en
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • CCHEMISTRY; METALLURGY
    • C06EXPLOSIVES; MATCHES
    • C06BEXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B25/00Compositions containing a nitrated organic compound
    • C06B25/34Compositions containing a nitrated organic compound the compound being a nitrated acyclic, alicyclic or heterocyclic amine
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B3/00Blasting cartridges, i.e. case and explosive

Abstract

The utility model provides an promote explosive device that kills and kill and explode warhead fragment density, it relates to explosive technical field, concretely relates to promote explosive device that kills and explode warhead fragment density. The explosive comprises a rupture disc, a shell, high-detonation-velocity explosives, low-detonation-velocity explosives, an explosion network and a detonator seat, wherein the rupture disc is arranged at the top end of the shell, the high-detonation-velocity explosives are arranged on the inner side of the shell, the low-detonation-velocity explosives are arranged on the inner side of the high-detonation-velocity explosives, the explosion network is fixedly arranged at the bottom end of the shell, and the lower end of the explosion network is fixedly connected with the detonator seat. After the technical scheme is adopted, the invention has the beneficial effects that: the warhead adopts compound powder charge structural design and annular multiple spot detonating mode, forms indent detonation waveform, can control fragment direction of scattering and promote fragment density.

Description

Explosive device for improving fragment density of warhead of killing and killing blasting
Technical Field
The invention relates to the technical field of explosives, in particular to an explosive device for improving the fragment density of a warhead of killing and blasting.
Background
The existing directional warhead can be divided into three types of eccentric detonating type, deformable type and follow-up directional type. With the development of guidance technology, intelligent fuzes and artificial intelligence, the warhead intellectualization enables the follow-up directional killing and blasting warhead to gradually become a hotspot field of the research of the modern air defense guided missile warhead. The follow-up directional warhead is arranged in a front cabin of the missile and can follow up with the seeker to aim at the target position in real time, the seeker is used for probing and giving information such as the position and the speed of a target to be struck, then the warhead follows the target to aim and detonate, and the high-speed fragments fly away towards the aimed target after explosion, so that the maximum utilization rate of the fragments is realized. Compared with the axial symmetrical layout of the fragments of the eccentric detonation directional warhead and the deformable directional warhead, the damage efficiency is greatly improved.
Although the utilization rate of fragments of the follow-up directional killing blasting warhead is greatly improved compared with the conventional fragment killing blasting warhead which uniformly scatters in the circumferential direction, the fragment scattering direction is not controllable, the concentration of the fragments in the target direction is not high, and the fragment density is not high. If a small number of fragments hit the target, the target can not be damaged or partially damaged, and the effect of air defense and reverse guidance is greatly influenced.
Disclosure of Invention
The invention aims to provide an explosive device for improving the fragment density of a warhead of a killing and blasting aiming at the defects and shortcomings of the prior art, and the explosive device has the advantages of controlling the fragment flying direction and improving the fragment density.
In order to achieve the purpose, the invention adopts the following technical scheme: the utility model provides a promote explosive device that kills and kill and explode blast warhead fragment density, it includes fragment 1, casing 2, high detonation velocity explosive 3, low detonation velocity explosive 4, explosion network 5, detonator seat 6, fragment 1 installs in the top of casing 2, the inboard of casing 2 is provided with high detonation velocity explosive 3, the inboard of high detonation velocity explosive 3 is provided with low detonation velocity explosive 4, explosion network 5 is fixed to be set up in the bottom of casing 2, the lower extreme fixedly connected with detonator seat 6 of explosion network 5.
The high-detonation-velocity explosive 3 is in a hollow cylindrical shape, and the low-detonation-velocity explosive 4 is in a cylindrical shape. The high-detonation-velocity explosive 3 is explosive with high detonation velocity, such as hexogen or octogen, and the thickness of the high-detonation-velocity explosive 3 is about 10-60mm; the diameter of the low detonation velocity explosive 4 is about 120-220mm; the detonation velocity of the high detonation velocity explosive 3 is higher than that of the low detonation velocity explosive 4, an inwards concave detonation waveform can be formed inside during explosion, the detonation wave of the high detonation velocity explosive 3 is firstly propagated to the upper shell 21 to break the upper shell 21 and drive the edge rupture disc to move forwards and to move centrally, and then the detonation wave of the low detonation velocity explosive 4 is propagated to the upper shell 21 to break the shell and drive the central rupture disc to move forwards, so that the density of the rupture disc is improved.
The fragment 1 is square or spherical. The fragment 1 is positioned at the head of the warhead, is made of steel, tungsten alloy materials or oxide ceramics and is a main killing element for killing and blasting the warhead.
The upper end of the shell 2 is provided with a plurality of fragments 1. The arrangement of a plurality of fragments 1 can greatly improve the killing power of the warhead.
The shell 2 comprises an upper shell 21 and a lower shell 22, the upper shell 21 is in a hollow cylindrical shape, the lower shell 22 is in a cylindrical shape, the lower shell 22 is installed on the inner side of the bottom end of the upper shell 21, and the lower shell 22 is provided with the explosion network 5. The shell 2 is made of aluminum alloy materials and is used for restraining high-detonation velocity explosive 3 and low-detonation velocity explosive 4.
The explosive network 5 is composed of a plurality of identical detonating cords. The center detonating cord in the explosion network 5 is used for detonating the low detonation velocity explosive 4, other detonating cords are uniformly distributed and used for simultaneously detonating the high detonation velocity explosive 3, and the detonating cords are the same in length and can simultaneously detonate the high detonation velocity explosive 3 and the low detonation velocity explosive 4.
The working principle of the invention is as follows: when in use, a user detonates a detonator inserted into the detonator seat; the detonators explode, thereby exploding the explosive network. And meanwhile, the high-detonation-velocity explosive and the low-detonation-velocity explosive are detonated by the detonation network, wherein the center point of the low-detonation-velocity explosive is detonated, and the high-detonation-velocity explosive is detonated at six circumferential points.
Because the detonation velocity of the high detonation velocity explosive is higher than that of the low detonation velocity explosive, a concave detonation wave shape is formed inside the explosive, the detonation wave of the high detonation velocity explosive is firstly transmitted to the upper shell to break the upper shell and drive the edge rupture disc to move forwards and the center to move, and then the detonation wave of the low detonation velocity explosive is transmitted to the upper shell to break the shell and drive the center rupture disc to move forwards, so that the density of the rupture discs is also improved.
After the technical scheme is adopted, the invention has the beneficial effects that: the warhead adopts compound powder charge structural design and annular multiple spot detonating mode, forms indent detonation waveform, can control fragment direction of scattering and promote fragment density.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without creative efforts.
Figure 1 is a schematic view of the structure of the present invention,
fig. 2 is an enlarged view of a in fig. 1.
Description of reference numerals: the explosive comprises a fragment 1, a shell 2, an upper shell 21, a lower shell 22, high-detonation-velocity explosive 3, low-detonation-velocity explosive 4, an explosion network 5 and a detonator seat 6.
Detailed Description
Referring to fig. 1-2, the technical solution adopted by the present embodiment is: the explosive device comprises a fragment 1, a shell 2, high-detonation-velocity explosives 3, low-detonation-velocity explosives 4, an explosion network 5 and a detonator seat 6, wherein a plurality of fragments 1 are arranged at the top end of the shell 2, and the fragments 1 are square or spherical. The killing power of the warhead can be greatly improved by installing a plurality of fragments 1; the fragment 1 is positioned at the head of the warhead, is made of steel, tungsten alloy materials or oxide ceramics and is a main killing element for killing and blasting the warhead.
The inboard of casing 2 is provided with high detonation velocity explosive 3, and the inboard of high detonation velocity explosive 3 is provided with low detonation velocity explosive 4, and explosion network 5 is fixed to be set up in the bottom of casing 2. The high detonation velocity explosive 3 is in a hollow cylindrical shape, and the low detonation velocity explosive 4 is in a cylindrical shape. The high-detonation-velocity explosive 3 is explosive with high detonation velocity, such as hexogen or octogen, and the thickness of the high-detonation-velocity explosive 3 is about 10-60mm; the diameter of the low detonation velocity explosive 4 is about 120-220mm; the detonation velocity of the high detonation velocity explosive 3 is higher than that of the low detonation velocity explosive 4, an inwards concave detonation waveform can be formed inside the high detonation velocity explosive 3 during detonation, the detonation wave of the high detonation velocity explosive 3 is firstly propagated to the upper shell 21 to crush the upper shell 21 and drive the edge fragments to move forwards and the center to move, and then the detonation wave of the low detonation velocity explosive 4 is propagated to the upper shell 1 to crush the shell and drive the center fragments to move forwards, so that the density of the fragments is improved.
Casing 2 includes that upper housing 21 and lower casing 22 constitute, and upper housing 21 is hollow circular cylinder, and lower casing 22 is cylindric, and lower casing 22 is installed in upper housing 21's bottom inboard, and upper housing 21 is inside to be provided with high detonation velocity explosive 3 and low detonation velocity explosive 4, installs explosion network 5 down on the casing 22. The shell 2 is made of aluminum alloy materials and is used for restraining high-detonation velocity explosive 3 and low-detonation velocity explosive 4.
The lower end of the explosion network 5 is fixedly connected with a detonator seat 6; the explosion network 5 consists of several identical detonating cords. A detonating cord in the center of the explosion network 5 is used for detonating the low detonation velocity explosive 4, other detonating cords are uniformly distributed and used for simultaneously detonating the high detonation velocity explosive 3, and the detonating cords are the same in length and can simultaneously detonate the high detonation velocity explosive 3 and the low detonation velocity explosive 4.
This embodiment adopts compound powder charge structural design and annular multiple spot mode of initiating explosion for the warhead, forms indent detonation wave form, can control fragment direction of scattering and promote fragment density.
The above description is only for illustrating the technical solution of the present invention and not for limiting, and other modifications or equivalent substitutions made by the technical solution of the present invention by those of ordinary skill in the art should be covered within the scope of the claims of the present invention as long as they do not depart from the spirit and scope of the technical solution of the present invention.

Claims (6)

1. The utility model provides a promote and kill and explode explosive device of blasting warhead fragment density which characterized in that: the explosive comprises a fragment (1), a shell (2), a high-detonation-velocity explosive (3), a low-detonation-velocity explosive (4), an explosion network (5) and a detonator seat (6), wherein the fragment (1) is installed at the top end of the shell (2), the high-detonation-velocity explosive (3) is arranged on the inner side of the shell (2), the low-detonation-velocity explosive (4) is arranged on the inner side of the high-detonation-velocity explosive (3), the explosion network (5) is fixedly arranged at the bottom end of the shell (2), and the lower end of the explosion network (5) is fixedly connected with the detonator seat (6).
2. The explosive device for increasing the fragment density of the warhead of the killing blasting according to claim 1, wherein: the high detonation velocity explosive (3) is in a hollow cylindrical shape, and the low detonation velocity explosive (4) is in a cylindrical shape.
3. The explosive device for increasing the fragment density of the warhead of the killing blasting according to claim 1, wherein: the fragments (1) are square or spherical.
4. The explosive device for increasing the fragment density of the warhead of the killing blasting according to claim 1, wherein: the upper end of the shell (2) is provided with a plurality of fragments (1).
5. The explosive device for increasing the fragment density of the warhead of the killing blasting according to claim 1, wherein: casing (2) include casing (21) and casing (22) down and constitute, go up casing (21) and be hollow circular cylinder, casing (22) are cylindric down, and lower casing (22) are installed in the bottom of last casing (21) inboard, install explosion network (5) down on casing (22).
6. The explosive device for increasing the fragment density of the warhead of the killing blasting according to claim 1, wherein: the explosion network (5) is composed of a plurality of same detonating cords.
CN202211107353.2A 2022-09-13 2022-09-13 Explosive device for improving fragment density of killing blasting warhead Active CN115479505B (en)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN116399182A (en) * 2023-06-09 2023-07-07 北京理工大学 Circumferential composite charge structure explosion device and method for improving breaking speed

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5229542A (en) * 1992-03-27 1993-07-20 The United States Of America As Represented By The United States Department Of Energy Selectable fragmentation warhead
WO2004109218A1 (en) * 2003-06-11 2004-12-16 Bofors Defence Ab Device for control of fragment discharge from main charge liners
US20060086279A1 (en) * 2001-08-23 2006-04-27 Lloyd Richard M Kinetic energy rod warhead with lower deployment angles
US7930978B1 (en) * 2008-05-19 2011-04-26 Raytheon Company Forward firing fragmentation warhead
GB2479966A (en) * 2010-04-27 2011-11-02 Qinetiq Ltd Warhead
CN109540965A (en) * 2018-11-15 2019-03-29 中国工程物理研究院化工材料研究所 Explosive fragmentation driving capability evaluating apparatus and method
CN110514071A (en) * 2019-08-12 2019-11-29 南京理工大学 A kind of device and method controlling fragmentation warhead fragmentation shape
US20210108904A1 (en) * 2019-10-14 2021-04-15 TDW Gesellschaft für verteidigungstechnische Wirksysteme mbH Fragmentation warhead for a missle

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5229542A (en) * 1992-03-27 1993-07-20 The United States Of America As Represented By The United States Department Of Energy Selectable fragmentation warhead
US20060086279A1 (en) * 2001-08-23 2006-04-27 Lloyd Richard M Kinetic energy rod warhead with lower deployment angles
WO2004109218A1 (en) * 2003-06-11 2004-12-16 Bofors Defence Ab Device for control of fragment discharge from main charge liners
US20060180045A1 (en) * 2003-06-11 2006-08-17 Bae Systems Bofors Ab Device for control of fragment discharge from main charge liners
US7930978B1 (en) * 2008-05-19 2011-04-26 Raytheon Company Forward firing fragmentation warhead
GB2479966A (en) * 2010-04-27 2011-11-02 Qinetiq Ltd Warhead
CN109540965A (en) * 2018-11-15 2019-03-29 中国工程物理研究院化工材料研究所 Explosive fragmentation driving capability evaluating apparatus and method
CN110514071A (en) * 2019-08-12 2019-11-29 南京理工大学 A kind of device and method controlling fragmentation warhead fragmentation shape
US20210108904A1 (en) * 2019-10-14 2021-04-15 TDW Gesellschaft für verteidigungstechnische Wirksysteme mbH Fragmentation warhead for a missle

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN116399182A (en) * 2023-06-09 2023-07-07 北京理工大学 Circumferential composite charge structure explosion device and method for improving breaking speed
CN116399182B (en) * 2023-06-09 2023-08-08 北京理工大学 Circumferential composite charge structure explosion device and method for improving breaking speed

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