CN113587736B - A composite anti-riot kinetic energy bomb with delayed boost function - Google Patents

A composite anti-riot kinetic energy bomb with delayed boost function Download PDF

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CN113587736B
CN113587736B CN202110980569.9A CN202110980569A CN113587736B CN 113587736 B CN113587736 B CN 113587736B CN 202110980569 A CN202110980569 A CN 202110980569A CN 113587736 B CN113587736 B CN 113587736B
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assembly
cavity
warhead
propellant
bullet
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CN113587736A (en
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汪送
马永忠
樊向武
李阿楠
刘星雨
贾晓玲
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Engineering University of Chinese Peoples Armed Police Force
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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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/02Stabilising arrangements
    • F42B10/04Stabilising arrangements using fixed fins
    • F42B10/06Tail fins
    • 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
    • F42B12/72Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the material
    • F42B12/76Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the material of the casing
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B5/00Cartridge ammunition, e.g. separately-loaded propellant charges
    • F42B5/02Cartridges, i.e. cases with charge and missile
    • F42B5/10Cartridges, i.e. cases with charge and missile with self-propelled bullet
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B5/00Cartridge ammunition, e.g. separately-loaded propellant charges
    • F42B5/02Cartridges, i.e. cases with charge and missile
    • F42B5/16Cartridges, i.e. cases with charge and missile characterised by composition or physical dimensions or form of propellant charge, with or without projectile, or powder

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  • General Engineering & Computer Science (AREA)
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  • Combustion & Propulsion (AREA)
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  • Fluid Mechanics (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

本发明公开了一种具有延迟助推功能的复合型防暴动能弹,包括发射组件、弹体组件、护板组件和弹头组件,所述弹体组件套接发射组件,所述弹头组件黏附弹体组件,所述护板组件包裹弹头组件和弹体组件,所述弹体组件内置两级延迟助推机构,一级延迟助推机构实现弹体组件和弹头组件的一次助推,二级迟助推机构实现弹头组件和弹体组件的分离和对弹头组件的二次助推,所述弹头组件内置高压气瓶和刺激剂载荷腔,通过弹头压缩带动撞针实现气瓶爆破和刺激粉喷洒,近距离冲击速度较低不易造成过度伤害,中等距离通过一次助推加速,远距离通过二次助推加速,有效解决了近距离威力过大、远距离效能不足的问题,终点处具有动能、爆震和催泪驱散多重作用功效。

Figure 202110980569

The invention discloses a composite anti-riot kinetic energy bomb with a delayed boost function, comprising a launch component, a projectile body component, a guard plate component and a warhead component. The shield assembly wraps the warhead assembly and the projectile assembly. The projectile assembly has a built-in two-stage delay booster mechanism. The push mechanism realizes the separation of the warhead assembly and the projectile body assembly and the secondary boosting of the warhead assembly. The warhead assembly has a built-in high-pressure gas cylinder and a stimulant loading chamber, and the firing pin is driven by the warhead to compress to realize the cylinder blasting and stimulating powder spraying. The impact speed at distance is low and it is not easy to cause excessive damage. The medium distance is accelerated by one boost, and the long distance is accelerated by the second boost, which effectively solves the problems of excessive power at close range and insufficient performance at long distance. The end point has kinetic energy and detonation. And tear gas to disperse multi-action effect.

Figure 202110980569

Description

一种具有延迟助推功能的复合型防暴动能弹A composite anti-riot kinetic energy bomb with delayed boost function

技术领域technical field

本发明涉及防暴弹技术领域,具体为一种具有延迟助推功能的复合型防暴动能弹。The invention relates to the technical field of anti-riot bombs, in particular to a composite anti-riot kinetic energy bomb with a delay boost function.

背景技术Background technique

橡皮弹和布袋弹作为在役的主流防暴动能弹,因为有效射程范围较短、打击精度较差、作用效应单一而逐渐被新一代复合型防暴动能弹所取代。复合型防暴动能弹复合软质弹头和硬质弹头两种材料,在不同射距下由于碰击速度不同,产生不同冲击力进而迫使弹头产生不同程度的形变,以耗散冲击能量。近距离高速冲击时弹头变形较大,耗散能量较多,可减小对目标产生的意外伤害,远距离低速冲击时弹头变形较小,耗散能量较少,可将更高比例的冲击能量转移到目标体内,以达到预期的致痛效果。因此,复合型防暴动能弹在一定程度上解决了现役防暴动能弹近距离威力过大、远距离效能不足的问题,但要达到理想的耗能效果,对弹头材料有着极为特殊的要求,仅通过优化弹头材料来获得理想的弹头冲击响应特性难以从本质上解决近距离威力过大的问题,因为弹头即使发生了极限压缩形变,由于弹丸出口速度较高,也不足以完全避免对有生目标产生过度伤害,因此需要进一步优化弹丸结构设计,使得“近距离威力过大、远距离效能不足”的问题能得到更好地解决,同时有效解决现有防暴动能弹终点效应单一的问题。As the mainstream anti-riot kinetic energy bombs in service, rubber bullets and sack bombs are gradually replaced by a new generation of composite anti-riot kinetic energy bombs because of their short effective range, poor strike accuracy and single effect. The composite anti-riot kinetic energy bullet is composed of two materials: soft warhead and hard warhead. Due to different impact speeds at different firing distances, different impact forces are generated and the warheads are forced to deform to different degrees to dissipate the impact energy. In the case of high-speed impact at close range, the warhead deforms greatly and dissipates more energy, which can reduce accidental damage to the target. In the case of long-distance low-speed impact, the warhead deforms less and dissipates less energy, which can convert a higher proportion of impact energy. Transfer to the target body to achieve the desired pain-inducing effect. Therefore, the composite anti-riot kinetic energy projectile solves to a certain extent the problems that the active anti-riot kinetic energy projectile is too powerful at close range and insufficient in long-distance efficiency, but to achieve the ideal energy consumption effect, there are very special requirements for the warhead material. It is difficult to solve the problem of excessive close-range power by optimizing the material of the warhead to obtain the ideal impact response characteristics of the warhead, because even if the warhead undergoes extreme compression deformation, due to the high exit velocity of the projectile, it is not enough to completely avoid the impact on the living target. Excessive damage, so it is necessary to further optimize the projectile structure design, so that the problem of "too much power at close range and insufficient performance at long distance" can be better solved, and at the same time, it can effectively solve the problem of the single end effect of the existing anti-riot kinetic energy projectile.

发明内容SUMMARY OF THE INVENTION

本发明的目的在于提供一种具有延迟助推功能的复合型防暴动能弹,以解决上述背景技术中提出的问题。The purpose of the present invention is to provide a composite anti-riot kinetic energy bomb with a delayed boost function, so as to solve the above-mentioned problems in the background art.

为实现上述目的,本发明提供如下技术方案:一种具有延迟助推功能的复合型防暴动能弹,包括发射组件、弹体组件、护板组件和弹头组件,其特征在于:In order to achieve the above object, the present invention provides the following technical solutions: a composite anti-riot kinetic energy bomb with a delayed boost function, comprising a launch assembly, a projectile body assembly, a guard plate assembly and a warhead assembly, and is characterized in that:

所述发射组件包括发射药筒、底火孔、底火、高压室、发射药、轴向传火孔、斜向传火孔、低压室和O型垫圈,所述发射药筒由不锈钢材料加工制作,所述发射药筒由上、中、下三个外径依次增大的圆柱体构成,所述发射药筒下部中轴线上开设柱状的底火孔,所述底火孔后部轴心处铆接底火,所述底火为机械撞击式底火,所述底火孔上侧的前部球面、后部柱面的空腔即为高压室,所述高压室内部装填发射药,所述发射药为黑火药和无烟火药的混合物,所述发射药筒中部圆柱体开设连通高压室和低压室的轴向传火孔和斜向传火孔,所述斜向传火孔与发射药筒的中轴线呈40°夹角,所述斜向传火孔的数量为6个,6个所述斜向传火孔沿发射药筒的中轴线呈圆周式阵列分布,所述轴向传火孔和斜向传火孔由黄铜薄膜密封,所述发射药筒下部设置有与防暴枪枪管坡膛相匹配的底缘,所述底缘上侧套装O型垫圈,所述发射组件上侧套接弹体组件;The launching assembly includes a propellant cartridge, a primer hole, a primer, a high-pressure chamber, a propellant, an axial fire-passing hole, an oblique fire-passing hole, a low-pressure chamber and an O-ring, and the propellant cartridge is made of stainless steel. The propellant cartridge is composed of three cylinders whose outer diameters increase in turn, the upper, middle and lower outer diameters. A columnar primer hole is opened on the central axis of the lower part of the propellant cartridge, and the primer is riveted at the axis at the rear of the primer hole. The primer is a mechanical impact primer, and the cavities of the front spherical surface and the rear cylindrical surface on the upper side of the primer hole are the high-pressure chamber, and the high-pressure chamber is filled with propellant, and the propellant is black powder and non-ferrous powder. A mixture of pyrotechnic powder, the cylinder in the middle of the propellant cartridge is provided with an axial fire-passing hole and an oblique fire-passing hole that communicate with the high-pressure chamber and the low-pressure chamber, and the oblique fire-passing hole and the central axis of the propellant cartridge are at 40° The included angle, the number of the oblique fire-passing holes is 6, and the six oblique fire-passing holes are distributed in a circular array along the central axis of the propellant cartridge. The axial fire-passing holes and the oblique fire-passing holes The hole is sealed by a brass film, the lower part of the propellant cartridge is provided with a bottom edge that matches the ramp of the anti-riot gun barrel, the bottom edge is covered with an O-shaped gasket, and the upper side of the launch assembly is sleeved with the bullet body assembly ;

所述弹体组件包括主弹体、弹体壁、弹带、第一延期管插孔、第一延期管、推进剂腔、推进剂、后喷孔、第二延期管和扩爆药,所述主弹体、弹体壁和弹带由硬质耐高温塑料加工制作,所述第一延期管插孔、推进剂腔和后喷孔为主弹体内的预留空腔,所述弹体壁为主弹体向后延伸的圆柱体空腔,所述弹体壁套接发射药筒,所述弹体壁内侧与发射药筒外侧壁接触面上部采用热熔胶密封,所述弹体壁下端面抵靠O型垫圈,所述主弹体外侧壁突出设置有环状弹带,所述弹带与防暴枪阴膛线配合赋予弹体组件自旋速度,所述主弹体下部中轴线上开设第一延期管插孔,所述第一延期管插孔内部卡装第一延期管,所述第一延期管头部朝向低压室,所述第一延期管由发射药燃烧产生的火药气体点燃,所述第一延期管的延期时间为1s,所述第一延期管后部朝向推进剂腔,所述推进剂腔为前部球面、后部柱面的空腔,所述推进剂腔内装推进剂,所述推进剂腔下侧、主弹体下部开设后喷孔,所述后喷孔内置单向阀,所述单向阀可阻挡发射药燃烧产生的火药气体进入推进剂腔,所述后喷孔的数量为6个,6个所述后喷孔沿主弹体的中轴线呈圆周式阵列分布,所述推进剂腔上侧中轴线上开设第二延期管插孔,所述第二延期管插孔卡装第二延期管,所述第二延期管的延期时间为1s,所述主弹体上端面中心开设凹腔,所述凹腔内装微量扩爆药,所述第二延期管头部朝向推进剂腔,所述第二延期管尾部朝向凹腔,所述第一延期管和第二延期管均为火焰延期管,所述弹体组件上侧抵靠并粘附连接有弹头组件;The projectile body assembly includes a main projectile body, projectile body wall, elastic belt, a first delay tube insertion hole, a first delay tube, a propellant cavity, a propellant, a rear nozzle, a second delay tube and an explosive charge, so The main projectile body, the projectile body wall and the elastic belt are made of hard high temperature resistant plastics. The main wall is a cylindrical cavity extending backward from the projectile body, the projectile body wall is sleeved with the propellant cartridge, and the upper part of the contact surface between the inner side of the projectile body wall and the outer side wall of the propellant cartridge is sealed with hot melt glue. The lower end face of the wall abuts the O-shaped washer, the outer side wall of the main projectile is protruded with a ring-shaped elastic band, and the elastic band cooperates with the rifling of the anti-riot gun to give the projectile assembly a spin speed, and the central axis of the lower part of the main projectile body A first extension pipe jack is opened on the top, and a first extension pipe is clamped inside the first extension pipe jack, the head of the first extension pipe faces the low pressure chamber, and the first extension pipe is produced by the gunpowder produced by the combustion of the propellant. The gas is ignited, the delay time of the first extension tube is 1s, the rear of the first extension tube faces the propellant cavity, and the propellant cavity is the cavity of the front spherical surface and the rear cylindrical surface, and the propellant The cavity is filled with propellant. The lower side of the propellant cavity and the lower part of the main projectile are provided with rear nozzle holes. , the number of the rear nozzles is 6, and the 6 rear nozzles are distributed in a circular array along the central axis of the main projectile body, and a second extension tube jack is provided on the central axis of the upper side of the propellant cavity, The second extension tube jack is clamped with a second extension tube, and the extension time of the second extension tube is 1s. The center of the upper end face of the main projectile is provided with a concave cavity, and the concave cavity is filled with micro-explosive explosives, so The head of the second extension tube faces the propellant cavity, the tail of the second extension tube faces the concave cavity, the first extension tube and the second extension tube are both flame extension tubes, and the upper side of the projectile assembly abuts against the concave cavity. A warhead assembly is adhesively attached;

所述弹头组件包括弹头体、弹头壁、弹头内腔、高压气瓶、双针头撞针、刺激剂载荷腔、OC刺激粉末、弹头尾翼和斜向喷管,所述弹头体由软质橡胶材料加工制作,所述弹头体呈前部半球形、中部柱形和后部圆台形的结构,所述弹头壁由硬质橡胶材料加工制作,所述弹头壁为粘附在弹头体外壁上的薄层覆盖物,所述弹头壁外壁上下部分别开设有上卡槽和下卡槽,所述上卡槽和下卡槽均为方形圆环槽,所述弹头体内部中轴线上开设的圆柱形空腔即为弹头内腔,所述弹头内腔从上至下依次嵌入有高压气瓶、双针头撞针和刺激剂载荷腔,所述高压气瓶内装压缩性CO2气体,所述压缩性CO2气体的储存压力为2.0Mpa,所述高压气瓶由易碎瓶盖密封,所述双针头撞针为固定嵌入在弹头内腔侧壁中的金属部件,所述双针头撞针处于高压气瓶和刺激剂载荷腔中部,所述双针头撞针包括上撞针、撞针板、下撞针和泄压孔,所述上撞针、撞针板和下撞针由高硬度金属材料一体化加工成型,所述上撞针针尖朝向高压气瓶的易碎瓶盖,所述撞针板卡入并胶粘在弹头内腔侧壁中,所述下撞针针尖朝向刺激剂载荷腔上端面,所述泄压孔为撞针板上开设的圆形孔,所述撞针板同一径向方向上开设3个泄压孔,3个所述泄压孔构成一个泄压孔组,所述泄压孔组的数量为8个,8个所述泄压孔组沿撞针板的中轴线呈圆周式阵列分布,所述刺激剂载荷腔为长方体空腔,所述刺激剂载荷腔腔壁由聚苯乙烯材料整体注塑成型,所述刺激剂载荷腔外侧面与弹头体接触面之间、所述刺激剂载荷腔底端面与弹头壁接触面之间采用814胶胶粘固定,所述刺激剂载荷腔内装OC刺激粉末,所述弹头壁下部一体化设置弹头尾翼,所述弹头尾翼为斜边为圆弧的直角三角形尾翼,所述弹头尾翼的数量为8个,8个所述弹头尾翼沿弹头壁的中轴线呈圆周式阵列分布,所述双针头撞针下侧、刺激剂载荷腔上侧沿弹头内腔侧壁开设有贯穿弹头体和弹头壁的斜向喷管,所述斜向喷管与弹头体的中轴线呈40°夹角,所述斜向喷管沿弹头体轴向方向平行布设有2根,2根平行布设的所述斜向喷管构成一个斜向喷管组,所述斜向喷管组的数量为8个,8个所述斜向喷管组沿弹头体的中轴线呈圆周式阵列分布,所述弹体组件上侧、弹头组件外侧设置有护板组件;The warhead assembly includes a warhead body, a warhead wall, a warhead inner cavity, a high-pressure gas cylinder, a double-needle striker, a stimulant loading cavity, an OC stimulation powder, a warhead fin and an oblique nozzle, and the warhead body is processed by a soft rubber material The bullet body is in the shape of a hemisphere in the front, a cylindrical shape in the middle and a truncated cone in the rear. The bullet wall is made of hard rubber material, and the bullet wall is a thin layer that adheres to the outer wall of the bullet. Cover, the upper and lower parts of the outer wall of the bullet wall are respectively provided with an upper card slot and a lower card slot, the upper card slot and the lower card slot are both square ring grooves, and the inner center axis of the bullet body is provided with a cylindrical hollow. The cavity is the inner cavity of the warhead. The inner cavity of the warhead is sequentially embedded with a high-pressure gas cylinder, a double-needle striker and a stimulant loading cavity from top to bottom. The high-pressure gas cylinder is filled with compressed CO 2 gas, and the The storage pressure of the gas is 2.0Mpa, the high-pressure gas cylinder is sealed by a frangible cap, and the double-needle striker is a metal part that is fixedly embedded in the side wall of the inner cavity of the warhead, and the double-needle striker is in the high-pressure cylinder and stimulated. In the middle of the agent loading cavity, the double-needle striker includes an upper striker, a striker plate, a lower striker and a pressure relief hole, the upper striker, striker plate and lower striker are integrally formed from high-hardness metal materials, and the tip of the upper striker faces toward The fragile cap of the high-pressure gas cylinder, the striker plate is snapped into and glued to the side wall of the inner cavity of the warhead, the lower striker tip faces the upper end face of the stimulant load cavity, and the pressure relief hole is opened on the striker plate. A circular hole, the striker plate is provided with three pressure relief holes in the same radial direction, and the three pressure relief holes constitute a pressure relief hole group. The pressure relief hole group is distributed in a circular array along the central axis of the striker plate, the stimulant loading cavity is a cuboid cavity, the cavity wall of the stimulant loading cavity is integrally injection-molded by polystyrene material, and the stimulant loading cavity 814 glue is used to fix between the outer side and the contact surface of the bullet body, the bottom end surface of the stimulant load cavity and the contact surface of the bullet wall, the stimulant load cavity is filled with OC stimulation powder, and the lower part of the bullet wall is integrated A warhead tail fin is provided, and the warhead tail fin is a right-angled triangle tail fin whose hypotenuse is a circular arc. The number of the warhead tail fins is 8, and the 8 bullet tail fins are distributed in a circular array along the central axis of the warhead wall. The lower side of the needle striker and the upper side of the stimulant loading cavity are provided with an oblique nozzle penetrating the bullet body and the bullet wall along the side wall of the bullet cavity. The two oblique nozzles are arranged in parallel along the axial direction of the warhead body, and the two oblique nozzles arranged in parallel form an oblique nozzle group, and the number of the oblique nozzle groups is 8, 8 Each of the oblique nozzle groups is distributed in a circular array along the central axis of the bullet body, and a guard plate assembly is provided on the upper side of the bullet body assembly and on the outer side of the bullet assembly;

所述护板组件包括护板、上卡扣和下卡扣,所述护板为1/4圆弧板,4个所述护板侧壁拼接构成一个空心圆柱体,所述空心圆柱体包裹弹体组件的上部和弹头组件的中下部,所述上卡扣和下卡扣为护板内壁突出设置的方形1/4圆弧状凸起,所述上卡扣与上卡槽尺寸匹配,所述上卡扣卡入上卡槽中,所述下卡扣与下卡槽尺寸匹配,所述下卡扣卡入下卡槽中,所述护板下端部自由抵靠弹带上端面,所述护板组件由轻质塑料加工制作,所述护板组件用于防止弹头组件在枪管中高速飞行时发生挤压破坏;The guard plate assembly includes a guard plate, an upper buckle and a lower buckle. The shield is a 1/4 arc plate, and four side walls of the shield are spliced to form a hollow cylinder, and the hollow cylinder wraps The upper part of the bullet body assembly and the middle and lower part of the bullet assembly, the upper buckle and the lower buckle are square 1/4 arc-shaped protrusions protruding from the inner wall of the guard plate, and the upper buckle matches the size of the upper card slot, The upper clip is clipped into the upper clip slot, the lower clip matches the size of the lower clip slot, the lower clip clips into the lower clip slot, and the lower end of the guard plate freely abuts against the upper end surface of the elastic band, The guard plate assembly is made of lightweight plastic, and the guard plate assembly is used to prevent the warhead assembly from being crushed when it flies at a high speed in the barrel;

优选的,所述发射组件、弹体组件、护板组件和弹头组件均为轴对称结构,所述发射组件、弹体组件、护板组件和弹头组件的中轴线重合。Preferably, the launching assembly, the projectile assembly, the shield assembly and the warhead assembly are all axisymmetric structures, and the central axes of the launching assembly, the projectile assembly, the shield assembly and the warhead assembly are coincident.

优选的,所述推进剂腔内壁面、弹头壁下端面涂抹耐高温涂层。Preferably, the inner wall surface of the propellant cavity and the lower end surface of the warhead wall are coated with a high temperature resistant coating.

优选的,所述第一延期管、推进剂腔、推进剂和后喷孔构成第一延迟助推机构,所述第二延期管和扩爆药构成第一延迟助推机构。Preferably, the first delay tube, the propellant cavity, the propellant and the rear nozzle constitute a first delay boosting mechanism, and the second delay tube and the expanding explosive constitute a first delay boosting mechanism.

优选的,所述扩爆药被第二延期管点燃后所产生的火药燃气用于分离弹头组件和弹体组件。Preferably, the gunpowder gas generated after the expansion charge is ignited by the second extension tube is used to separate the warhead assembly and the projectile body assembly.

优选的,所述护板在弹体组件和弹头组件飞离枪管后,受离心力作用自动脱落。Preferably, after the projectile body assembly and the warhead assembly fly away from the barrel, the protective plate is automatically detached under the action of centrifugal force.

本发明与现有技术相比具有如下优点:Compared with the prior art, the present invention has the following advantages:

1.本发明创新性设计了两级延迟助推机构,通过设计装药量较小的高压室,采用高低压系统赋予弹头组件和弹体组件一个中等大小的出口速度,以确保近距离冲击时,碰击能量中等,结合弹头组件冲击形变耗散部分冲击能量,大为减小了对有生目标造成极为严重过度伤害的概率,从而从根本上解决近距离威力过大的问题;在经过1s的延期时间后,第一延期管发火,点燃助推剂,实现对弹头组件和弹体组件的一次助推,以弥补速度上的衰减,在此阶段如果冲击有生目标,可获得与近距离冲击时相同的冲击效果;发生一级助推后,第二延期管经历1s的延期时间,点燃扩爆药,在迫使弹头组件和弹体组件分离的同时,对弹头组件实现二次助推,以进一步弥补远距离冲击时速度下降,并取得一定程度上的致痛效果。因此,本发明可在近、中、远不同射击距离下,取得近乎相同的动能打击效果,进而从根本上解决了现有防暴动能弹“近距离威力过大、远距离效能不足”的现实问题;1. The present invention innovatively designs a two-stage delayed booster mechanism. By designing a high-pressure chamber with a small charge, a high-low pressure system is used to give the warhead assembly and the projectile assembly a medium-sized exit velocity to ensure that when impacted at close range. , the impact energy is medium, combined with the impact deformation of the warhead assembly to dissipate part of the impact energy, greatly reducing the probability of causing extremely serious excessive damage to living targets, thus fundamentally solving the problem of excessive close-range power; after 1s After the delay time, the first delay tube fires, ignites the propellant, and realizes a boost to the warhead assembly and the projectile assembly to make up for the attenuation in speed. The same impact effect during impact; after the first-level boost occurs, the second delay tube experiences a delay time of 1s, ignites the explosive charge, and while forcing the separation of the warhead assembly and the projectile assembly, achieves a secondary boost to the warhead assembly, In order to further compensate for the drop in speed during long-distance impact, and achieve a certain degree of pain. Therefore, the present invention can achieve almost the same kinetic energy striking effect at different shooting distances at close, medium and long distances, thereby fundamentally solving the practical problem of "excessive close-range power and insufficient long-range effectiveness" of the existing anti-riot kinetic energy projectiles ;

2.本发明通过在弹头组件中嵌入高压气瓶和刺激剂载荷腔,通过弹头体的压缩形变,带动双针头撞针击碎高压气瓶和刺激剂载荷腔,发出较大的爆破声响和喷射令人难以仍受的催泪粉末,从而使得本发明具有动能打击、爆破威慑和催泪驱散三重非致命作用功效,较好解决了现有防暴动能弹终点作用效应单一的问题;2. The present invention drives the double-needle striker to smash the high-pressure gas cylinder and the stimulant loading cavity by embedding the high-pressure gas cylinder and the stimulant loading cavity in the bullet assembly, and through the compression deformation of the warhead body, and emits a larger blasting sound and ejection order. The tear-promoting powder that is difficult for people to still receive, so that the present invention has three non-lethal effects of kinetic energy strike, blasting deterrence and tear-repellent dispersal, and better solves the problem of single end effect of the existing anti-riot kinetic energy bomb;

3.本发明采用线膛防暴枪进行发射,弹带与防暴枪枪管的阴膛线配合,赋予弹体组件一定的自旋速度,弹头组件采用球面设计,具有较好的气动外形,弹头组件设置尾翼,可进一步提高飞行稳定性,使得本发明具有较高的打击精度,具有瞄哪打哪的显著优点;3. The present invention uses a rifled anti-riot gun to launch, and the elastic belt cooperates with the female rifling of the barrel of the anti-riot gun to give the bullet body assembly a certain spin speed. The bullet assembly adopts a spherical design and has a better aerodynamic shape. , which can further improve the flight stability, so that the present invention has higher strike accuracy, and has the significant advantages of aiming where to shoot;

4.本发明高低压系统采用中部轴向传火孔和周边周布斜向传火孔的设计,通过黄铜薄膜密封传火孔,可利于形成较为平稳的火药燃气推力;发射药采用黑火药和无烟火药的混合物,既可获得较高的膛压,以提高弹丸的出口速度,又可获得一致性较好的拔弹力,使得本发明具有较为优良的内弹道特性,同时枪口烟量较少,不会干扰使用人员正常的战术动作,本发明在枪管中不产生过量的火药残渣,从而不会影响重复射击和射弹精度,进而使得本发明具有较高的战场适用性;4. The high-low pressure system of the present invention adopts the design of the central axial fire-passing hole and the oblique fire-passing holes around the periphery, and the fire-passing hole is sealed by the brass film, which can help to form a relatively stable gunpowder gas thrust; the propellant adopts black powder and The mixture of smokeless gunpowder can not only obtain a higher chamber pressure to improve the exit speed of the projectile, but also obtain a consistent pulling force, so that the present invention has relatively excellent internal ballistic characteristics, and at the same time, the muzzle smoke volume is relatively high. It does not interfere with the normal tactical action of the user, and the present invention does not produce excessive gunpowder residues in the barrel, thereby not affecting the repeated shooting and projectile accuracy, thereby making the present invention have higher battlefield applicability;

5.本发明弹体组件和发射组件之间设置O型垫圈,可起到较好的缓冲作用;后喷孔内置单向阀,可防止发射药燃烧产生的火药燃气直接点燃推进剂;护板包裹弹体组件,可防止弹头组件在防暴枪枪管中受到挤压而触发双针头撞针,进而引发炸膛事件,因此本发明具有较好的勤务性能和较高的使用可靠性。5. An O-shaped gasket is arranged between the projectile assembly and the launching assembly of the present invention, which can play a better buffering effect; the rear nozzle has a built-in one-way valve, which can prevent the gunpowder gas generated by the combustion of the propellant from directly igniting the propellant; the guard plate By wrapping the bullet body assembly, the bullet assembly can be prevented from being squeezed in the barrel of the anti-riot gun to trigger the double-needle striker, thereby triggering a chamber explosion event, so the present invention has better service performance and higher use reliability.

附图说明Description of drawings

图1为本发明的立体示意图;Fig. 1 is the three-dimensional schematic diagram of the present invention;

图2为本发明的结构示意图;Fig. 2 is the structural representation of the present invention;

图3为本发明中发射组件1的立体示意图;FIG. 3 is a three-dimensional schematic diagram of the launch assembly 1 in the present invention;

图4为本发明中弹体组件2的立体示意图;FIG. 4 is a perspective view of the projectile body assembly 2 of the present invention;

图5为本发明中弹头组件4的立体示意图;5 is a perspective view of the warhead assembly 4 in the present invention;

图6为本发明中双针头撞针4-5的立体示意图。FIG. 6 is a schematic perspective view of the double-needle striker 4-5 in the present invention.

图中:1、发射组件,1-1、发射药筒,1-2、底火孔,1-3、底火,1-4、高压室,1-5、发射药,1-6、轴向传火孔,1-7、斜向传火孔,1-8、低压室,1-9、O型垫圈,2、弹体组件,2-1、主弹体,2-2、弹体壁,2-3、弹带,2-4、第一延期管插孔,2-5、第一延期管,2-6、推进剂腔,2-7、推进剂,2-8、后喷孔,2-9、第二延期管,2-10、扩爆药,3、护板组件,3-1、护板,3-2、上卡扣,3-3、下卡扣,4、弹头组件,4-1、弹头体,4-2、弹头壁,4-2-1、上卡槽,4-2-2、下卡槽,4-3、弹头内腔,4-4、高压气瓶,4-5、双针头撞针,4-5-1、上撞针,4-5-2、撞针板,4-5-3、下撞针,4-5-4、泄压孔,4-6、刺激剂载荷腔,4-7、OC刺激粉末,4-8、弹头尾翼,4-9、斜向喷管。In the picture: 1. Launching assembly, 1-1, Propellant cartridge, 1-2, Primer hole, 1-3, Primer, 1-4, High pressure chamber, 1-5, Propellant, 1-6, Axial transmission Fire hole, 1-7, oblique fire hole, 1-8, low pressure chamber, 1-9, O-ring, 2, projectile assembly, 2-1, main projectile, 2-2, projectile wall, 2-3, elastic belt, 2-4, first extension tube jack, 2-5, first extension tube, 2-6, propellant cavity, 2-7, propellant, 2-8, rear nozzle, 2-9, Second extension tube, 2-10, Explosives, 3, Guard plate assembly, 3-1, Guard plate, 3-2, Upper buckle, 3-3, Lower buckle, 4, Warhead assembly , 4-1, warhead body, 4-2, warhead wall, 4-2-1, upper card slot, 4-2-2, lower card slot, 4-3, warhead cavity, 4-4, high pressure gas cylinder , 4-5, double-needle striker, 4-5-1, upper striker, 4-5-2, striker plate, 4-5-3, lower striker, 4-5-4, pressure relief hole, 4-6, Stimulant loading chamber, 4-7, OC stimulation powder, 4-8, warhead tail, 4-9, oblique nozzle.

具体实施方式Detailed ways

下面将结合本发明实施例中的附图,对本发明实施例中的技术方案进行清楚、完整地描述,显然,所描述的实施例仅仅是本发明一部分实施例,而不是全部的实施例。基于本发明中的实施例,本领域普通技术人员在没有做出创造性劳动前提下所获得的所有其他实施例,都属于本发明保护的范围。The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, but not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.

请参阅图1-6,本发明提供一种技术方案:一种具有延迟助推功能的复合型防暴动能弹,包括发射组件1、弹体组件2、护板组件3和弹头组件4,其特征在于:1-6, the present invention provides a technical solution: a composite anti-riot kinetic energy bomb with a delayed boost function, comprising a launch assembly 1, a projectile body assembly 2, a guard plate assembly 3 and a warhead assembly 4. in:

所述发射组件1包括发射药筒1-1、底火孔1-2、底火1-3、高压室1-4、发射药1-5、轴向传火孔1-6、斜向传火孔1-7、低压室1-8和O型垫圈1-9,所述发射药筒1-1由不锈钢材料加工制作,所述发射药筒1-1由上、中、下三个外径依次增大的圆柱体构成,所述发射药筒1-1下部中轴线上开设柱状的底火孔1-2,所述底火孔1-2内铆接底火1-3,所述底火1-3为机械撞击式底火,所述底火孔1-2上侧的前部球面、后部柱面的空腔即为高压室1-4,所述高压室1-4内部装填发射药1-5,所述发射药1-5为黑火药和无烟火药的混合物,所述发射药筒1-1中部圆柱体开设连通高压室1-4和低压室1-8的轴向传火孔1-6和斜向传火孔1-7,所述斜向传火孔1-7与发射药筒1-1的中轴线呈40°夹角,所述斜向传火孔1-7的数量为6个,6个所述斜向传火孔1-7沿发射药筒1-1的中轴线呈圆周式阵列分布,所述轴向传火孔1-6和斜向传火孔1-7由黄铜薄膜密封,所述发射药筒1-1下部设置有与防暴枪枪管坡膛相匹配的底缘,所述底缘上侧套装O型垫圈1-9,所述发射组件1上侧套接弹体组件2;The launching assembly 1 includes a propellant cartridge 1-1, a primer hole 1-2, a primer 1-3, a high pressure chamber 1-4, a propellant 1-5, an axial fire transfer hole 1-6, and an oblique fire transfer hole. 1-7. Low pressure chamber 1-8 and O-shaped gasket 1-9, the propellant cartridge 1-1 is made of stainless steel material, and the propellant cartridge 1-1 has three outer diameters of upper, middle and lower in order It is composed of an enlarged cylinder, and a cylindrical primer hole 1-2 is opened on the central axis of the lower part of the propellant cartridge 1-1. The primer hole 1-2 is riveted with the primer 1-3, and the primer 1-3 is a mechanical Impact primer, the cavities of the front spherical surface and the rear cylindrical surface on the upper side of the primer hole 1-2 are the high pressure chambers 1-4. The high pressure chambers 1-4 are filled with propellants 1-5. The propellant 1-5 is a mixture of black powder and smokeless powder, and the central cylinder of the propellant cartridge 1-1 is provided with an axial fire-passing hole 1-6 and an oblique hole 1-6 connecting the high-pressure chamber 1-4 and the low-pressure chamber 1-8. Towards the fire-passing holes 1-7, the oblique fire-passing holes 1-7 form an included angle of 40° with the central axis of the propellant cartridge 1-1, and the number of the oblique fire-passing holes 1-7 is 6, The six oblique fire-passing holes 1-7 are distributed in a circular array along the central axis of the propellant cartridge 1-1, and the axial fire-passing holes 1-6 and the oblique fire-passing holes 1-7 are made of brass. The film is sealed, the lower part of the propellant cartridge 1-1 is provided with a bottom edge that matches the slope of the anti-riot gun barrel, the O-shaped gasket 1-9 is sleeved on the upper side of the bottom edge, and the upper side of the launch assembly 1 is sleeved projectile assembly 2;

所述弹体组件2包括主弹体2-1、弹体壁2-2、弹带2-3、第一延期管插孔2-4、第一延期管2-5、推进剂腔2-6、推进剂2-7、后喷孔2-8、第二延期管2-9和扩爆药2-10,所述主弹体2-1、弹体壁2-2和弹带2-3由硬质耐高温塑料加工制作,所述第一延期管插孔2-4、推进剂腔2-6和后喷孔2-8为主弹体2-1内的预留空腔,所述弹体壁2-2为主弹体2-1向后延伸的圆柱体空腔,所述弹体壁2-2套接发射药筒1-1,所述弹体壁2-2内侧与发射药筒1-1外侧壁接触面上部采用热熔胶密封,所述弹体壁2-2下端面抵靠O型垫圈1-9,所述主弹体2-1外侧壁突出设置有环状弹带2-3,所述弹带2-3与防暴枪阴膛线配合赋予弹体组件2自旋速度,所述主弹体2-1下部中轴线上开设第一延期管插孔2-4,所述第一延期管插孔2-4内部卡装第一延期管2-5,所述第一延期管2-5的延期时间为1s,所述第一延期管2-5头部朝向低压室1-8,所述第一延期管2-5由发射药1-5燃烧产生的火药气体点燃,所述第一延期管2-5后部朝向推进剂腔2-6,所述推进剂腔2-6为前部球面、后部柱面的空腔,所述推进剂腔2-6内装推进剂2-7,所述推进剂腔2-6下侧、主弹体2-1下部开设后喷孔2-8,所述后喷孔2-8内置单向阀,所述单向阀可阻挡发射药1-5燃烧产生的火药气体进入推进剂腔2-6,所述后喷孔2-8的数量为6个,6个所述后喷孔2-8沿主弹体2-1的中轴线呈圆周式阵列分布,所述推进剂腔2-6上侧中轴线上开设第二延期管插孔,所述第二延期管插孔卡装第二延期管2-9,所述第二延期管2-9的延期时间为1s,所述主弹体2-1上端面中心开设凹腔,所述凹腔内装微量扩爆药2-10,所述第二延期管2-9头部朝向推进剂腔2-6,所述第二延期管2-9尾部朝向凹腔,所述第一延期管2-5和第二延期管2-9均为火焰延期管,所述弹体组件2上侧抵靠有粘附连接有弹头组件4;The bullet body assembly 2 includes a main bullet body 2-1, a bullet body wall 2-2, an elastic belt 2-3, a first extension tube insertion hole 2-4, a first extension tube 2-5, and a propellant cavity 2- 6. The propellant 2-7, the rear nozzle hole 2-8, the second extension pipe 2-9 and the explosive charge 2-10, the main projectile body 2-1, the projectile body wall 2-2 and the spring belt 2- 3. It is made of hard high temperature-resistant plastic. The first extension tube insertion hole 2-4, the propellant cavity 2-6 and the rear nozzle hole 2-8 are reserved cavities in the main bomb body 2-1. The projectile wall 2-2 is a cylindrical cavity extending backward from the projectile body 2-1. The upper part of the contact surface of the outer side wall of the propellant cartridge 1-1 is sealed with hot melt adhesive, the lower end surface of the projectile wall 2-2 abuts the O-shaped gasket 1-9, and the outer wall of the main projectile 2-1 is protruded with a ring. The elastic belt 2-3, the elastic belt 2-3 cooperates with the rifling of the anti-riot gun to give the bullet body assembly 2 a spin speed, and the central axis of the lower part of the main bullet body 2-1 is provided with a first extension pipe jack 2- 4. A first extension tube 2-5 is clamped inside the first extension tube insertion hole 2-4, the extension time of the first extension tube 2-5 is 1s, and the head of the first extension tube 2-5 is Facing the low pressure chamber 1-8, the first extension tube 2-5 is ignited by the gunpowder gas generated by the combustion of the propellant 1-5, and the rear of the first extension tube 2-5 faces the propellant cavity 2-6, the The propellant cavity 2-6 is a cavity with a spherical surface at the front and a cylindrical surface at the rear. The propellant cavity 2-6 is filled with a propellant 2-7. 1. A rear nozzle hole 2-8 is provided in the lower part. The rear nozzle hole 2-8 has a built-in one-way valve. The one-way valve can prevent the gunpowder gas generated by the combustion of the propellant 1-5 from entering the propellant cavity 2-6. The number of rear nozzle holes 2-8 is 6, and the 6 rear nozzle holes 2-8 are distributed in a circular array along the central axis of the main bomb body 2-1, and the central axis of the upper side of the propellant cavity 2-6 A second extension pipe jack is opened on the top, the second extension pipe jack is clamped with a second extension pipe 2-9, the extension time of the second extension pipe 2-9 is 1s, and the main body 2-1 A concave cavity is opened in the center of the upper end face, and the cavity is filled with micro-explosive explosives 2-10, the head of the second extension tube 2-9 faces the propellant cavity 2-6, and the tail of the second extension tube 2-9 faces The cavity, the first extension pipe 2-5 and the second extension pipe 2-9 are both flame extension pipes, and the bullet assembly 4 is adhered and connected to the upper side of the bullet body assembly 2;

所述弹头组件4包括弹头体4-1、弹头壁4-2、弹头内腔4-3、高压气瓶4-4、双针头撞针4-5、刺激剂载荷腔4-6、OC刺激粉末4-7、弹头尾翼4-8和斜向喷管4-9,所述弹头体4-1由软质橡胶材料加工制作,所述弹头体4-1呈前部半球形、中部柱形和后部圆台形的结构,所述弹头壁4-2由硬质橡胶材料加工制作,所述弹头壁4-2为粘附在弹头体4-1外壁上的薄层覆盖物,所述弹头壁4-2外壁上下部分别开设有上卡槽4-2-1和下卡槽4-2-2,所述上卡槽4-2-1和下卡槽4-2-2均为方形圆环槽,所述弹头体4-1内部中轴线上开设的圆柱形空腔即为弹头内腔4-3,所述弹头内腔4-3从上至下依次嵌入有高压气瓶4-4、双针头撞针4-5和刺激剂载荷腔4-6,所述高压气瓶4-4内装压缩性CO2气体,所述压缩性CO2气体的储存压力为2.0Mpa,所述高压气瓶4-4由易碎瓶盖密封,所述双针头撞针4-5为固定嵌入在弹头内腔4-3侧壁中的金属部件,所述双针头撞针4-5处于高压气瓶4-4和刺激剂载荷腔4-6中部,所述双针头撞针4-5包括上撞针4-5-1、撞针板4-5-2、下撞针4-5-3和泄压孔4-5-4,所述上撞针4-5-1、撞针板4-5-2和下撞针4-5-3由高硬度金属材料一体化加工成型,所述上撞针4-5-1针尖朝向高压气瓶4-4的易碎瓶盖,所述撞针板4-5-2卡入并胶粘在弹头内腔4-3侧壁中,所述下撞针4-5-3针尖朝向刺激剂载荷腔4-6上端面,所述泄压孔4-5-4为撞针板4-5-2上开设的圆形孔,所述撞针板4-5-2同一径向方向上开设3个泄压孔4-5-4,3个所述泄压孔4-5-4构成一个泄压孔组,所述泄压孔组的数量为8个,8个所述泄压孔组沿撞针板4-5-2的中轴线呈圆周式阵列分布,所述刺激剂载荷腔4-6为长方体空腔,所述刺激剂载荷腔4-6腔壁由聚苯乙烯材料整体注塑成型,所述刺激剂载荷腔4-6外侧面与弹头体4-1接触面之间、所述刺激剂载荷腔4-6底端面与弹头壁4-2接触面之间采用814胶胶粘固定,所述刺激剂载荷腔4-6内装OC刺激粉末4-7,所述弹头壁4-2下部一体化设置弹头尾翼4-8,所述弹头尾翼4-8为斜边为圆弧的直角三角形尾翼,所述弹头尾翼4-8的数量为8个,8个所述弹头尾翼4-8沿弹头壁4-2的中轴线呈圆周式阵列分布,所述双针头撞针4-5下侧、刺激剂载荷腔4-6上侧沿弹头内腔4-3侧壁开设有贯穿弹头体4-1和弹头壁4-2的斜向喷管4-9,所述斜向喷管4-9与弹头体4-1的中轴线呈40°夹角,所述斜向喷管4-9沿弹头体4-1轴向方向平行布设有2根,2根平行布设的所述斜向喷管4-9构成一个斜向喷管组,所述斜向喷管组的数量为8个,8个所述斜向喷管组沿弹头体4-1的中轴线呈圆周式阵列分布,所述弹体组件2上侧、弹头组件4外侧设置有护板组件3;The bullet assembly 4 includes a bullet body 4-1, a bullet wall 4-2, a bullet inner cavity 4-3, a high-pressure gas cylinder 4-4, a double-needle striker 4-5, a stimulant load cavity 4-6, and an OC stimulation powder. 4-7. The warhead tail 4-8 and the oblique nozzle 4-9. The warhead body 4-1 is made of soft rubber material. The rear conical structure, the bullet wall 4-2 is made of hard rubber material, and the bullet wall 4-2 is a thin layer covering adhered to the outer wall of the bullet body 4-1. 4-2 The upper and lower parts of the outer wall are respectively provided with an upper card slot 4-2-1 and a lower card slot 4-2-2, the upper card slot 4-2-1 and the lower card slot 4-2-2 are both square and round Ring groove, the cylindrical cavity opened on the inner central axis of the bullet body 4-1 is the bullet inner cavity 4-3, and the bullet inner cavity 4-3 is sequentially embedded with high-pressure gas cylinders 4-4 from top to bottom , a double-needle striker 4-5 and a stimulant load chamber 4-6, the high-pressure gas cylinder 4-4 is filled with compressed CO 2 gas, and the storage pressure of the compressed CO 2 gas is 2.0Mpa, and the high-pressure gas cylinder 4-4 is sealed by a frangible bottle cap, the double-needle striker 4-5 is a metal part that is fixedly embedded in the side wall of the warhead cavity 4-3, and the double-needle striker 4-5 is located in the high-pressure gas cylinder 4-4. and the middle of the stimulant loading chamber 4-6, the double-needle striker 4-5 includes an upper striker 4-5-1, a striker plate 4-5-2, a lower striker 4-5-3 and a pressure relief hole 4-5- 4. The upper striker 4-5-1, the striker plate 4-5-2 and the lower striker 4-5-3 are integrally formed from high-hardness metal materials, and the needle tip of the upper striker 4-5-1 faces the high-pressure gas The frangible cap of the bottle 4-4, the firing pin plate 4-5-2 is snapped into and glued in the side wall of the inner cavity 4-3 of the bullet, and the needle tip of the lower firing pin 4-5-3 faces the stimulant loading cavity 4-6 On the upper end face, the pressure relief hole 4-5-4 is a circular hole opened on the striker plate 4-5-2, and the striker plate 4-5-2 has three pressure relief holes in the same radial direction Holes 4-5-4, three of the pressure relief holes 4-5-4 constitute a pressure relief hole group, the number of the pressure relief hole groups is 8, and the 8 pressure relief hole groups are along the striker plate 4 The central axis of -5-2 is distributed in a circular array, the stimulant loading cavity 4-6 is a cuboid cavity, and the cavity wall of the stimulant loading cavity 4-6 is integrally injection-molded by polystyrene material. 814 glue is used to fix between the outer side of the agent loading cavity 4-6 and the contact surface of the bullet body 4-1, and between the bottom end surface of the stimulant loading cavity 4-6 and the contact surface of the bullet wall 4-2. The OC stimulation powder 4-7 is installed in the agent load cavity 4-6, the lower part of the warhead wall 4-2 is integrally provided with a warhead tail 4-8, and the warhead tail 4-8 is a right-angled triangle tail with a hypotenuse as an arc, so The number of the bullet fins 4-8 is 8, and the 8 bullet fins 4-8 are distributed in a circular array along the central axis of the bullet wall 4-2. The upper side of cavity 4-6 is along the side of inner cavity 4-3 of the warhead The wall is provided with an oblique nozzle 4-9 penetrating the warhead body 4-1 and the warhead wall 4-2. Two oblique nozzles 4-9 are arranged in parallel along the axial direction of the warhead body 4-1, and the two oblique nozzles 4-9 arranged in parallel form an oblique nozzle group, and the oblique nozzles The number of groups is 8, and the 8 oblique nozzle groups are distributed in a circular array along the central axis of the bullet body 4-1. The upper side of the bullet body assembly 2 and the outer side of the bullet assembly 4 are provided with a guard plate assembly 3. ;

所述护板组件3包括护板3-1、上卡扣3-2和下卡扣3-3,所述护板3-1为1/4圆弧板,4个所述护板3-1侧壁拼接构成一个空心圆柱体,所述空心圆柱体包裹弹体组件2的上部和弹头组件4的中下部,所述上卡扣3-2和下卡扣3-3为护板3-1内壁突出设置的方形1/4圆弧状凸起,所述上卡扣3-2与上卡槽4-2-1尺寸匹配,所述上卡扣3-2卡入上卡槽4-2-1中,所述下卡扣3-3与下卡槽4-2-2尺寸匹配,所述下卡扣3-3卡入下卡槽4-2-2中,所述护板3-1下端部自由抵靠弹带2-3上端面,所述护板组件3由轻质塑料加工制作,所述护板组件3用于防止弹头组件4在枪管中高速飞行时发生挤压破坏;The shield assembly 3 includes a shield 3-1, an upper buckle 3-2 and a lower buckle 3-3. The shield 3-1 is a 1/4 arc plate, and four shields 3- 1. The side walls are spliced together to form a hollow cylinder, and the hollow cylinder wraps the upper part of the bullet body assembly 2 and the middle and lower parts of the bullet assembly 4, and the upper buckle 3-2 and the lower buckle 3-3 are the guard plate 3- 1 A square 1/4 arc-shaped protrusion protruding from the inner wall, the upper buckle 3-2 matches the size of the upper slot 4-2-1, and the upper buckle 3-2 is inserted into the upper slot 4- In 2-1, the lower clip 3-3 matches the size of the lower slot 4-2-2, the lower clip 3-3 is clipped into the lower slot 4-2-2, and the guard plate 3 -1 The lower end freely rests against the upper end surface of the elastic band 2-3, the guard plate assembly 3 is made of light plastic, and the guard plate assembly 3 is used to prevent the bullet assembly 4 from being squeezed when it flies at a high speed in the barrel destroy;

结合图1和图2,所述发射组件1、弹体组件2、护板组件3和弹头组件4均为轴对称结构,所述发射组件1、弹体组件2、护板组件3和弹头组件4的中轴线重合。1 and 2, the launching assembly 1, the bullet body assembly 2, the guard plate assembly 3 and the warhead assembly 4 are all axisymmetric structures, and the launching assembly 1, the bullet body assembly 2, the guard plate assembly 3 and the warhead assembly The central axes of 4 are coincident.

本实施例中,所述推进剂腔2-6内壁面、弹头壁4-2下端面涂抹耐高温涂层。In this embodiment, the inner wall surface of the propellant chamber 2-6 and the lower end surface of the warhead wall 4-2 are coated with a high temperature resistant coating.

本实施例中,所述第一延期管2-5、推进剂腔2-6、推进剂2-7和后喷孔构成第一延迟助推机构,所述第二延期管2-9和扩爆药2-10构成第一延迟助推机构。In this embodiment, the first extension tube 2-5, the propellant cavity 2-6, the propellant 2-7 and the rear nozzle constitute a first delay boosting mechanism, and the second extension tube 2-9 and the expansion The explosives 2-10 constitute the first delay boosting mechanism.

本实施例中,所述扩爆药2-10被第二延期管2-9点燃后所产生的火药燃气用于分离弹头组件4和弹体组件2。In this embodiment, the gunpowder gas generated after the expansion charge 2-10 is ignited by the second extension pipe 2-9 is used to separate the warhead assembly 4 and the projectile assembly 2.

本实施例中,所述护板3-1在弹体组件2和弹头组件4飞离枪管后,受离心力作用自动脱落。In this embodiment, after the bullet body assembly 2 and the warhead assembly 4 fly away from the gun barrel, the protective plate 3-1 automatically falls off under the action of centrifugal force.

工作原理:working principle:

首先将本发明装入适配的线膛防暴枪,闭锁枪膛,扣动防暴枪扳机,击针撞击底火1-3,底火1-3引燃发射药1-5,发射药1-5猛烈燃烧,在达到预定压力后,冲破密封轴向传火孔1-6和斜向传火孔1-7的黄铜薄膜,火药燃气进入低压室1-8,烧蚀连接发射药筒1-1和主弹体2-1的热熔胶,在达到预定压力后,推动主弹体2-1与发射药筒1-1脱离,同时火药燃气点燃第一延期管2-5,弹带2-3挤入防暴枪阴膛线,促进弹体组件2带动护板组件3和弹头组件4产生自旋,在弹体组件2、护板组件3和弹头组件4脱离枪管后,受离心力作用所述护板组件3与弹体组件2和弹头组件4分离并脱落,所述第一延期管2-5经过1s的延期时间后,后部发火,点燃推进剂腔2-6内装的推进剂2-7,所述推进剂2-7猛烈燃烧,产生火药燃气从后喷孔2-8高速喷出,实现对弹体组件2和弹头组件4的一次助推,火药燃气同时点燃第二延期管2-9,所述第二延期管2-9经过1s的延期时间后,后部发火,点燃扩爆药2-10,所述扩爆药2-10猛烈燃烧,产生瞬时高压,迫使弹体组件2和弹头组件4分离,并实现对弹头组件4的二次助推,得益于有弹头尾翼4-8的作用,弹头组件4继续平稳飞行,直至击中目标,实现对目标的动能打击,随后弹头体4-1受压发生较大挤压变形,所述上撞针4-5-1击碎高压气瓶4-4的易碎瓶盖,发出较大爆破声响,实现对目标的震慑,所述下撞针4-5-3击碎刺激剂载荷腔4-6的上端面,由于弹头体4-1发生压缩,所述斜向喷管4-9暂时封闭,在所述弹头组件4回弹过程中,弹头体4-1逐渐恢复原状,受高压气体作用,所述OC刺激粉末4-7从斜向喷管4-9高速喷出,实现对本发明前侧群体性目标的刺激驱散。因此,本发明在终点处具有动能打击、爆震威慑和刺激驱散三重非致命作用功效。First put the present invention into a suitable rifled anti-riot gun, lock the chamber, pull the trigger of the anti-riot gun, the firing pin hits the primer 1-3, the primer 1-3 ignites the propellant 1-5, and the propellant 1-5 burns violently , after reaching the predetermined pressure, the brass film sealing the axial fire-passing holes 1-6 and the oblique fire-passing holes 1-7 is broken, the gunpowder gas enters the low pressure chamber 1-8, and the propellant cartridges 1-1 and 1-1 are connected by ablation. After the hot melt adhesive of the main bomb body 2-1 reaches a predetermined pressure, it pushes the main bomb body 2-1 to separate from the propellant cartridge 1-1, and at the same time the gunpowder gas ignites the first extension tube 2-5 and the elastic belt 2-3 Squeeze into the female rifling of the anti-riot gun, and promote the bullet body assembly 2 to drive the guard plate assembly 3 and the warhead assembly 4 to spin. The plate assembly 3 is separated from the projectile assembly 2 and the warhead assembly 4 and falls off. After the delay time of 1 s, the first extension tube 2-5 fires at the rear, igniting the propellant 2-7 in the propellant chamber 2-6. , the propellant 2-7 is violently burned, and the gunpowder gas is ejected from the rear nozzle hole 2-8 at a high speed, realizing a boost to the projectile body assembly 2 and the warhead assembly 4, and the gunpowder gas simultaneously ignites the second extension pipe 2- 9. After the delay time of 1s, the second extension tube 2-9 fires at the rear, ignites the explosive expansion agent 2-10, and the explosive expansion agent 2-10 burns violently, generating instantaneous high pressure, forcing the projectile assembly 2 It is separated from the warhead assembly 4 and realizes the secondary boost to the warhead assembly 4. Thanks to the effect of the warhead tail 4-8, the warhead assembly 4 continues to fly smoothly until it hits the target and achieves a kinetic energy strike on the target. The warhead body 4-1 is compressed and deformed greatly, and the upper striker 4-5-1 smashes the fragile cap of the high-pressure gas cylinder 4-4, and makes a loud blasting sound to achieve shock and deterrence to the target. The lower striker 4-5-3 smashes the upper end face of the stimulant load chamber 4-6. Due to the compression of the bullet body 4-1, the oblique nozzle 4-9 is temporarily closed, and the bullet assembly 4 rebounds. During the process, the warhead body 4-1 gradually returns to its original state, and under the action of high-pressure gas, the OC stimulating powder 4-7 is ejected at high speed from the oblique nozzle 4-9 to achieve the stimulation and dispersal of the front-side mass target of the present invention. Therefore, the present invention has the triple non-lethal effect of kinetic energy strike, detonation deterrence and stimulus dispersal at the end point.

本发明近距离冲击有生目标时,由于发射药1-5装药量较少,所述弹体组件2和弹头组件4初速较低,加之弹头组件4受击变形耗散部分冲击能力,因此不易对目标产生过度伤害;由于一级延迟助推机构的作用,使得弹体组件2和弹头组件4在中等射距下有一个加速过程,以及二级延迟助推机构的作用,使得弹头组件4在远距离下有一个二次加速过程,从而使得中远程距离下可获得与近距离时相同的动能打击效果,加之终点处的多重非致命作用功效,使得本发明较好解决了现有防暴动能弹“近距离威力过大、远距离效能不足”的现实问题,且具备较好的战术灵活性。When the present invention impacts a living target at close range, due to the small amount of propellants 1-5, the initial velocity of the projectile assembly 2 and the warhead assembly 4 are relatively low, and the warhead assembly 4 is deformed to dissipate part of the impact capacity. It is not easy to cause excessive damage to the target; due to the action of the first-stage delay booster mechanism, the projectile assembly 2 and the warhead assembly 4 have an acceleration process at medium firing distances, and the action of the second-stage delay booster mechanism makes the warhead assembly 4 There is a secondary acceleration process at long distance, so that the same kinetic energy strike effect as that at short distance can be obtained at medium and long distance. In addition, multiple non-lethal effects at the end point make the present invention better solve the existing anti-riot kinetic energy It has the practical problem of "too much power at close range and insufficient effectiveness at long range", and has good tactical flexibility.

尽管已经示出和描述了本发明的实施例,对于本领域的普通技术人员而言,可以理解在不脱离本发明的原理和精神的情况下可以对这些实施例进行多种变化、修改、替换和变型,本发明的范围由所附权利要求及其等同物限定。Although embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, and substitutions can be made in these embodiments without departing from the principle and spirit of the invention and modifications, the scope of the invention is defined by the appended claims and their equivalents.

Claims (6)

1.一种具有延迟助推功能的复合型防暴动能弹,包括发射组件(1)、弹体组件(2)、护板组件(3)和弹头组件(4),其特征在于:1. a composite anti-riot kinetic energy bomb with delayed boosting function, comprising launch assembly (1), projectile body assembly (2), guard plate assembly (3) and warhead assembly (4), it is characterized in that: 所述发射组件(1)包括发射药筒(1-1)、底火孔(1-2)、底火(1-3)、高压室(1-4)、发射药(1-5)、轴向传火孔(1-6)、斜向传火孔(1-7)、低压室(1-8)和O型垫圈(1-9),所述发射药筒(1-1)由不锈钢材料加工制作,所述发射药筒(1-1)由上、中、下三个外径依次增大的圆柱体构成,所述发射药筒(1-1)下部中轴线上开设柱状的底火孔(1-2),所述底火孔(1-2)内铆接底火(1-3),所述底火(1-3)为机械撞击式底火,所述底火孔(1-2)上侧的前部球面、后部柱面的空腔即为高压室(1-4),所述高压室(1-4)内部装填发射药(1-5),所述发射药(1-5)为黑火药和无烟火药的混合物,所述发射药筒(1-1)中部圆柱体开设连通高压室(1-4)和低压室(1-8)的轴向传火孔(1-6)和斜向传火孔(1-7),所述斜向传火孔(1-7)与发射药筒(1-1)的中轴线呈40°夹角,所述斜向传火孔(1-7)的数量为6个,6个所述斜向传火孔(1-7)沿发射药筒(1-1)的中轴线呈圆周式阵列分布,所述轴向传火孔(1-6)和斜向传火孔(1-7)由黄铜薄膜密封,所述发射药筒(1-1)下部设置有与防暴枪枪管坡膛相匹配的底缘,所述底缘上侧套装O型垫圈(1-9),所述发射组件(1)上侧套接弹体组件(2);The launching assembly (1) includes a propellant cartridge (1-1), a primer hole (1-2), a primer (1-3), a high pressure chamber (1-4), a propellant (1-5), an axial The fire transmission hole (1-6), the oblique fire transmission hole (1-7), the low pressure chamber (1-8) and the O-ring (1-9), the propellant cartridge (1-1) is made of stainless steel Processed and manufactured, the propellant cartridge (1-1) is composed of three cylinders whose outer diameters are increased in order of upper, middle and lower outer diameters, and a cylindrical primer hole is provided on the central axis of the lower part of the propellant cartridge (1-1). (1-2), the primer (1-3) is riveted in the primer hole (1-2), the primer (1-3) is a mechanical impact primer, and the primer on the upper side of the primer hole (1-2) The cavity of the front spherical surface and the rear cylindrical surface is the high pressure chamber (1-4), the high pressure chamber (1-4) is filled with propellant (1-5), and the propellant (1-5) is A mixture of black powder and smokeless powder, the central cylinder of the propellant cartridge (1-1) is provided with an axial fire-passing hole (1-6) that communicates with the high-pressure chamber (1-4) and the low-pressure chamber (1-8) and the oblique fire transmission hole (1-7), which forms an included angle of 40° with the central axis of the propellant cartridge (1-1), and the oblique fire transmission hole (1-7) The number of 1-7) is 6, and the 6 oblique fire-passing holes (1-7) are distributed in a circular array along the central axis of the propellant cartridge (1-1). 1-6) and the oblique fire-passing hole (1-7) are sealed by a brass film, the lower part of the propellant cartridge (1-1) is provided with a bottom edge that matches the sloping chamber of the anti-riot gun barrel, the bottom part is An O-shaped gasket (1-9) is sleeved on the upper side of the edge, and the projectile assembly (2) is sleeved on the upper side of the launching assembly (1); 所述弹体组件(2)包括主弹体(2-1)、弹体壁(2-2)、弹带(2-3)、第一延期管插孔(2-4)、第一延期管(2-5)、推进剂腔(2-6)、推进剂(2-7)、后喷孔(2-8)、第二延期管(2-9)和扩爆药(2-10),所述主弹体(2-1)、弹体壁(2-2)和弹带(2-3)由硬质耐高温塑料加工制作,所述第一延期管插孔(2-4)、推进剂腔(2-6)和后喷孔(2-8)为主弹体(2-1)内的预留空腔,所述弹体壁(2-2)为主弹体(2-1)向后延伸的圆柱体空腔,所述弹体壁(2-2)套接发射药筒(1-1),所述弹体壁(2-2)内侧与发射药筒(1-1)外侧壁接触面上部采用热熔胶密封,所述弹体壁(2-2)下端面抵靠O型垫圈(1-9),所述主弹体(2-1)外侧壁突出设置有环状弹带(2-3),所述弹带(2-3)与防暴枪阴膛线配合赋予弹体组件(2)自旋速度,所述主弹体(2-1)下部中轴线上开设第一延期管插孔(2-4),所述第一延期管插孔(2-4)内部卡装第一延期管(2-5),所述第一延期管(2-5)头部朝向低压室(1-8),所述第一延期管(2-5)由发射药(1-5)燃烧产生的火药气体点燃,所述第一延期管(2-5)的延期时间为1s,所述第一延期管(2-5)后部朝向推进剂腔(2-6),所述推进剂腔(2-6)为前部球面、后部柱面的空腔,所述推进剂腔(2-6)内装推进剂(2-7),所述推进剂腔(2-6)下侧、主弹体(2-1)下部开设后喷孔(2-8),所述后喷孔(2-8)内置单向阀,所述单向阀可阻挡发射药(1-5)燃烧产生的火药气体进入推进剂腔(2-6),所述后喷孔(2-8)的数量为6个,6个所述后喷孔(2-8)沿主弹体(2-1)的中轴线呈圆周式阵列分布,所述推进剂腔(2-6)上侧中轴线上开设第二延期管插孔,所述第二延期管插孔卡装第二延期管(2-9),所述第二延期管(2-9)的延期时间为1s,所述主弹体(2-1)上端面中心开设凹腔,所述凹腔内装微量扩爆药(2-10),所述第二延期管(2-9)头部朝向推进剂腔(2-6),所述第二延期管(2-9)尾部朝向凹腔,所述第一延期管(2-5)和第二延期管(2-9)均为火焰延期管,所述弹体组件(2)上侧抵靠并粘附连接有弹头组件(4);The projectile body assembly (2) includes a main projectile body (2-1), a projectile body wall (2-2), an elastic band (2-3), a first extension tube insertion hole (2-4), a first extension tube Tube (2-5), propellant chamber (2-6), propellant (2-7), rear nozzle (2-8), second extension tube (2-9) and expansion charge (2-10) ), the main body (2-1), the body wall (2-2) and the elastic band (2-3) are made of hard high temperature resistant plastics, and the first extension tube insertion hole (2-4) ), the propellant cavity (2-6) and the rear nozzle hole (2-8) are reserved cavities in the main projectile (2-1), and the projectile wall (2-2) is the main projectile (2-2). 2-1) A cylindrical cavity extending backward, the projectile wall (2-2) is sleeved with the propellant cartridge (1-1), and the inner side of the projectile wall (2-2) is connected to the propellant cartridge ( 1-1) The upper part of the contact surface of the outer side wall is sealed with hot melt adhesive, the lower end surface of the body wall (2-2) abuts the O-shaped gasket (1-9), and the outer side wall of the main body (2-1) A ring-shaped elastic belt (2-3) is protrudingly arranged, and the elastic belt (2-3) cooperates with the female rifling of the anti-riot gun to give the bullet body assembly (2) a spin speed. The lower part of the main bullet body (2-1) A first extension pipe insertion hole (2-4) is provided on the central axis, a first extension pipe (2-5) is clamped inside the first extension pipe insertion hole (2-4), and the first extension pipe (2-4) is installed inside the first extension pipe insertion hole (2-4). -5) The head faces the low pressure chamber (1-8), the first extension pipe (2-5) is ignited by the gunpowder gas generated by the combustion of the propellant (1-5), the first extension pipe (2-5) ), the delay time is 1s, the rear part of the first delay tube (2-5) faces the propellant cavity (2-6), and the propellant cavity (2-6) is spherical in the front and cylindrical in the rear. A cavity, a propellant (2-7) is contained in the propellant cavity (2-6), and a rear spray hole (2) is provided on the lower side of the propellant cavity (2-6) and the lower part of the main projectile (2-1). -8), the rear nozzle (2-8) has a built-in one-way valve, and the one-way valve can prevent the gunpowder gas generated by the combustion of the propellant (1-5) from entering the propellant cavity (2-6), the The number of rear nozzle holes (2-8) is six, and the six rear nozzle holes (2-8) are distributed in a circular array along the central axis of the main projectile body (2-1). 2-6) A second extension pipe insertion hole is provided on the central axis of the upper side, the second extension pipe insertion hole is clamped with a second extension pipe (2-9), and the extension of the second extension pipe (2-9) The time is 1s, the center of the upper end face of the main projectile (2-1) is provided with a concave cavity, the concave cavity is filled with a micro-explosive explosive (2-10), and the head of the second extension tube (2-9) is facing The propellant cavity (2-6), the tail of the second extension tube (2-9) faces the concave cavity, the first extension tube (2-5) and the second extension tube (2-9) are both flame extension a pipe, the bullet assembly (4) is attached to the upper side of the bullet body assembly (2) against and adheredly connected; 所述弹头组件(4)包括弹头体(4-1)、弹头壁(4-2)、弹头内腔(4-3)、高压气瓶(4-4)、双针头撞针(4-5)、刺激剂载荷腔(4-6)、OC刺激粉末(4-7)、弹头尾翼(4-8)和斜向喷管(4-9),所述弹头体(4-1)由软质橡胶材料加工制作,所述弹头体(4-1)呈前部半球形、中部柱形和后部圆台形的结构,所述弹头壁(4-2)由硬质橡胶材料加工制作,所述弹头壁(4-2)为粘附在弹头体(4-1)外壁上的薄层覆盖物,所述弹头壁(4-2)外壁上下部分别开设有上卡槽(4-2-1)和下卡槽(4-2-2),所述上卡槽(4-2-1)和下卡槽(4-2-2)均为方形圆环槽,所述弹头体(4-1)内部中轴线上开设的圆柱形空腔即为弹头内腔(4-3),所述弹头内腔(4-3)从上至下依次嵌入有高压气瓶(4-4)、双针头撞针(4-5)和刺激剂载荷腔(4-6),所述高压气瓶(4-4)内装压缩性CO2气体,所述压缩性CO2气体的储存压力为2.0Mpa,所述高压气瓶(4-4)由易碎瓶盖密封,所述双针头撞针(4-5)为固定嵌入在弹头内腔(4-3)侧壁中的金属部件,所述双针头撞针(4-5)处于高压气瓶(4-4)和刺激剂载荷腔(4-6)中部,所述双针头撞针(4-5)包括上撞针(4-5-1)、撞针板(4-5-2)、下撞针(4-5-3)和泄压孔(4-5-4),所述上撞针(4-5-1)、撞针板(4-5-2)和下撞针(4-5-3)由高硬度金属材料一体化加工成型,所述上撞针(4-5-1)针尖朝向高压气瓶(4-4)的易碎瓶盖,所述撞针板(4-5-2)卡入并胶粘在弹头内腔(4-3)侧壁中,所述下撞针(4-5-3)针尖朝向刺激剂载荷腔(4-6)上端面,所述泄压孔(4-5-4)为撞针板(4-5-2)上开设的圆形孔,所述撞针板(4-5-2)同一径向方向上开设3个泄压孔(4-5-4),3个所述泄压孔(4-5-4)构成一个泄压孔组,所述泄压孔组的数量为8个,8个所述泄压孔组沿撞针板(4-5-2)的中轴线呈圆周式阵列分布,所述刺激剂载荷腔(4-6)为长方体空腔,所述刺激剂载荷腔(4-6)腔壁由聚苯乙烯材料整体注塑成型,所述刺激剂载荷腔(4-6)外侧面与弹头体(4-1)接触面之间、所述刺激剂载荷腔(4-6)底端面与弹头壁(4-2)接触面之间采用814胶胶粘固定,所述刺激剂载荷腔(4-6)内装OC刺激粉末(4-7),所述弹头壁(4-2)下部一体化设置弹头尾翼(4-8),所述弹头尾翼(4-8)为斜边为圆弧的直角三角形尾翼,所述弹头尾翼(4-8)的数量为8个,8个所述弹头尾翼(4-8)沿弹头壁(4-2)的中轴线呈圆周式阵列分布,所述双针头撞针(4-5)下侧、刺激剂载荷腔(4-6)上侧沿弹头内腔(4-3)侧壁开设有贯穿弹头体(4-1)和弹头壁(4-2)的斜向喷管(4-9),所述斜向喷管(4-9)与弹头体(4-1)的中轴线呈40°夹角,所述斜向喷管(4-9)沿弹头体(4-1)轴向方向平行布设有2根,2根平行布设的所述斜向喷管(4-9)构成一个斜向喷管组,所述斜向喷管组的数量为8个,8个所述斜向喷管组沿弹头体(4-1)的中轴线呈圆周式阵列分布,所述弹体组件(2)上侧、弹头组件(4)外侧设置有护板组件(3);The bullet assembly (4) includes a bullet body (4-1), a bullet wall (4-2), a bullet inner cavity (4-3), a high-pressure gas cylinder (4-4), and a double-needle striker (4-5) , stimulant loading chamber (4-6), OC stimulation powder (4-7), warhead tail (4-8) and oblique nozzle (4-9), the warhead body (4-1) is made of soft The bullet body (4-1) is in the shape of a hemisphere in the front, a cylindrical shape in the middle and a truncated cone in the rear, and the bullet wall (4-2) is processed and manufactured from a hard rubber material. The bullet wall (4-2) is a thin-layer covering adhered to the outer wall of the bullet body (4-1), and the upper and lower parts of the outer wall of the bullet wall (4-2) are respectively provided with upper card slots (4-2-1). ) and the lower card slot (4-2-2), the upper card slot (4-2-1) and the lower card slot (4-2-2) are both square ring grooves, the bullet body (4- 1) The cylindrical cavity opened on the inner central axis is the warhead inner cavity (4-3), and the bullet inner cavity (4-3) is sequentially embedded with high-pressure gas cylinders (4-4), double The needle striker (4-5) and the stimulant loading chamber (4-6), the high-pressure gas cylinder (4-4) is filled with compressed CO 2 gas, and the storage pressure of the compressed CO 2 gas is 2.0Mpa, so the The high-pressure gas cylinder (4-4) is sealed by a frangible cap, the double-needle striker (4-5) is a metal part that is fixedly embedded in the side wall of the warhead cavity (4-3), and the double-needle striker (4-5) is located in the middle of the high-pressure gas cylinder (4-4) and the stimulant loading chamber (4-6), the double-needle striker (4-5) includes an upper striker (4-5-1), a striker plate ( 4-5-2), lower striker (4-5-3) and pressure relief hole (4-5-4), the upper striker (4-5-1), striker plate (4-5-2) and The lower striker (4-5-3) is integrally formed by high-hardness metal materials, the tip of the upper striker (4-5-1) faces the fragile cap of the high-pressure gas cylinder (4-4), and the striker plate (4-5-2) clipped and glued in the side wall of the inner cavity (4-3) of the bullet, the needle tip of the lower striker (4-5-3) faces the upper end surface of the stimulant loading cavity (4-6), The pressure relief hole (4-5-4) is a circular hole opened on the striker plate (4-5-2), and the striker plate (4-5-2) is provided with three pressure relief holes in the same radial direction Hole (4-5-4), 3 of the pressure relief holes (4-5-4) constitute a pressure relief hole group, the number of the pressure relief hole group is 8, and the 8 pressure relief hole groups Distributed in a circular array along the central axis of the striker plate (4-5-2), the stimulant loading cavity (4-6) is a rectangular parallelepiped cavity, and the cavity wall of the stimulant loading cavity (4-6) is composed of a polyhedron. The styrene material is integrally injection-molded, and between the outer surface of the stimulant loading cavity (4-6) and the contact surface of the bullet body (4-1), the bottom end surface of the stimulant loading cavity (4-6) and the bullet wall ( 4-2) 814 glue is used to fix the contact surfaces, the stimulant loading cavity (4-6) is filled with OC stimulation powder (4-7), and the wall of the bullet is (4-2) The lower part is integrally provided with a warhead tail (4-8), the warhead tail (4-8) is a right-angled triangular tail with a hypotenuse as an arc, and the number of the warhead tails (4-8) is 8 , 8 of the warhead fins (4-8) are distributed in a circular array along the central axis of the warhead wall (4-2), the underside of the double-needle striker (4-5), the stimulant load cavity (4-5) 6) The upper side is provided with an oblique nozzle (4-9) penetrating the bullet body (4-1) and the bullet wall (4-2) along the side wall of the warhead cavity (4-3). The oblique nozzle (4-9) forms an included angle of 40° with the central axis of the bullet body (4-1), and two oblique nozzles (4-9) are arranged in parallel along the axial direction of the bullet body (4-1), The two oblique nozzles (4-9) arranged in parallel form an oblique nozzle group, the number of the oblique nozzle groups is 8, and the 8 oblique nozzle groups are arranged along the warhead body ( 4-1) The central axis is distributed in a circular array, and a guard plate assembly (3) is provided on the upper side of the bullet body assembly (2) and the outer side of the bullet assembly (4); 所述护板组件(3)包括护板(3-1)、上卡扣(3-2)和下卡扣(3-3),所述护板(3-1)为1/4圆弧板,4个所述护板(3-1)侧壁拼接构成一个空心圆柱体,所述空心圆柱体包裹弹体组件(2)的上部和弹头组件(4)的中下部,所述上卡扣(3-2)和下卡扣(3-3)为护板(3-1)内壁突出设置的方形1/4圆弧状凸起,所述上卡扣(3-2)与上卡槽(4-2-1)尺寸匹配,所述上卡扣(3-2)卡入上卡槽(4-2-1)中,所述下卡扣(3-3)与下卡槽(4-2-2)尺寸匹配,所述下卡扣(3-3)卡入下卡槽(4-2-2)中,所述护板(3-1)下端部自由抵靠弹带(2-3)上端面,所述护板组件(3)由轻质塑料加工制作,所述护板组件(3)用于防止弹头组件(4)在枪管中高速飞行时发生挤压破坏。The guard plate assembly (3) includes a guard plate (3-1), an upper buckle (3-2) and a lower buckle (3-3), and the shield plate (3-1) is a 1/4 arc plate, four side walls of the guard plates (3-1) are spliced together to form a hollow cylinder, the hollow cylinder wraps the upper part of the projectile assembly (2) and the middle and lower parts of the projectile assembly (4), and the upper card The buckle (3-2) and the lower buckle (3-3) are square 1/4 arc-shaped protrusions protruding from the inner wall of the guard plate (3-1), and the upper buckle (3-2) is connected to the upper buckle The size of the slot (4-2-1) is matched, the upper buckle (3-2) is snapped into the upper slot (4-2-1), and the lower buckle (3-3) is connected to the lower slot ( 4-2-2) Size matching, the lower buckle (3-3) is snapped into the lower slot (4-2-2), and the lower end of the guard plate (3-1) freely abuts against the elastic belt ( 2-3) On the upper end surface, the guard plate assembly (3) is made of lightweight plastic, and the guard plate assembly (3) is used to prevent the warhead assembly (4) from being crushed and damaged when it flies in the barrel at high speed. 2.根据权利要求1所述的一种具有延迟助推功能的复合型防暴动能弹,其特征在于:所述发射组件(1)、弹体组件(2)、护板组件(3)和弹头组件(4)均为轴对称结构,所述发射组件(1)、弹体组件(2)、护板组件(3)和弹头组件(4)的中轴线重合。2. A composite anti-riot kinetic energy bomb with delayed boosting function according to claim 1, characterized in that: the launching assembly (1), the projectile assembly (2), the guard plate assembly (3) and the warhead The components (4) are all axisymmetric structures, and the central axes of the launching component (1), the projectile component (2), the shield component (3) and the warhead component (4) are coincident. 3.根据权利要求1所述的一种具有延迟助推功能的复合型防暴动能弹,其特征在于:所述推进剂腔(2-6)内壁面、弹头壁(4-2)下端面涂抹耐高温涂层。3. A composite anti-riot kinetic energy bomb with delayed boosting function according to claim 1, characterized in that: the inner wall surface of the propellant cavity (2-6) and the lower end surface of the warhead wall (4-2) are smeared High temperature resistant coating. 4.根据权利要求1所述的一种具有延迟助推功能的复合型防暴动能弹,其特征在于:所述第一延期管(2-5)、推进剂腔(2-6)、推进剂(2-7)和后喷孔构成第一延迟助推机构,所述第二延期管(2-9)和扩爆药(2-10)构成第二延迟助推机构。4. A composite anti-riot kinetic energy bomb with a delayed boost function according to claim 1, characterized in that: the first delay tube (2-5), the propellant cavity (2-6), the propellant (2-7) and the rear spray hole constitute a first delay boosting mechanism, and the second delay pipe (2-9) and the expanding explosive (2-10) constitute a second delay boosting mechanism. 5.根据权利要求1所述的一种具有延迟助推功能的复合型防暴动能弹,其特征在于:所述扩爆药(2-10)被第二延期管(2-9)点燃后所产生的火药燃气用于分离弹头组件(4)和弹体组件(2)。5. The composite anti-riot kinetic energy bomb with a delayed boosting function according to claim 1, wherein the explosive charge (2-10) is ignited by the second extension tube (2-9) after being ignited. The generated gunpowder gas is used to separate the warhead assembly (4) and the projectile assembly (2). 6.根据权利要求1所述的一种具有延迟助推功能的复合型防暴动能弹,其特征在于:所述护板(3-1)在弹体组件(2)和弹头组件(4)飞离枪管后,受离心力作用自动脱落。6. The composite anti-riot kinetic energy bomb with delayed boosting function according to claim 1, characterized in that: the guard plate (3-1) is flying between the projectile body assembly (2) and the warhead assembly (4) After leaving the barrel, it falls off automatically by centrifugal force.
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