CN209027377U - A kind of impact-fired extended-range anti-riot grenade - Google Patents

本实用新型公开了一种撞击击发式增程防暴枪榴弹，包括：尾管、尾翼、推进部和打击部，所述尾翼焊接安装在尾管尾部的外壁上，所述尾管前端焊接安装在推进部的尾部，所述打击部嵌入安装在推进部的前端，所述推进部内置火箭推进器，实现增程目的；所述推进部和打击部之间装填染色剂，实现染色标记；所述打击部内部设置爆震弹体和催泪弹体，实现爆震和催泪驱散；所述打击部前端设置有击发端，用于击发打击部。本实用新型结构设计合理，具有多级推进、射程远、稳定性高、兼具染色、震晕、催泪多重打击效果等优点，可有效解决现有防暴弹药功能单一、震慑效果差、射程短、弹道稳定性差等棘手问题，可大为灵活远距离防暴战斗战术战法，并催生新型战斗力生成。

The utility model discloses an impact-fired extended-range anti-riot grenade, comprising: a tail pipe, a tail fin, a propulsion part and a striking part. At the tail of the propulsion part, the striking part is embedded and installed at the front end of the propulsion part, and the propulsion part has a built-in rocket propeller to achieve the purpose of extending the range; the propulsion part and the striking part are filled with dye to achieve dyeing marks; the striking part A detonation projectile and a tear gas projectile are arranged inside the part to realize detonation and tear gas dispersion; the front end of the striking part is provided with a firing end for firing the striking part. The utility model has the advantages of reasonable structure design, multi-stage propulsion, long range, high stability, dyeing, shock stun, tear-inducing multi-strike effects, etc. Difficult problems such as poor ballistic stability can be greatly flexible and long-distance anti-riot combat tactics and tactics, and spawn new combat power generation.

一种撞击击发式增程防暴枪榴弹A kind of impact-fired extended-range anti-riot grenade

技术领域technical field

本实用新型涉及防暴器材技术领域，更具体的说，尤其涉及一种撞击击发式增程防暴枪榴弹。The utility model relates to the technical field of anti-riot equipment, in particular to an impact-fired extended-range anti-riot gun grenade.

背景技术Background technique

枪榴弹是用枪和枪弹或空包弹发射的一种超口径弹药，初速是靠枪内火药气体的作用和子弹的动能得到的，主要用于对付有生目标、装甲目标和非装甲目标等。枪榴弹在结构上与尾翼稳定式炮弹基本相似，所不同的是多了一个用于发射的尾管装置，尾管内装有缓冲器和子弹收集器。射击前将枪榴弹套在枪管上，击发时子弹撞击收集器，并在火药气体作用下使其获得一定的初速。Grenade is a kind of super-caliber ammunition fired by guns and bullets or blank bullets. The initial velocity is obtained by the action of gunpowder gas in the gun and the kinetic energy of bullets. It is mainly used to deal with living targets, armored targets and non-armored targets. The grenade is basically similar in structure to the tail-stabilized shell, except that there is an additional tailpipe device for launching, and the tailpipe is equipped with a buffer and a bullet collector. The grenade is put on the barrel before shooting, and the bullet hits the collector when firing, and makes it gain a certain initial velocity under the action of gunpowder gas.

防暴枪榴弹则主要用于使群体或个体目标暂时失能，而不产生永久性伤残，属于非致命弹药范畴。当前，非致命弹药在军队、武警、公安遂行反恐、处突、维稳、海上维权等任务中发挥着重要作用，但普遍存在射程较短、精度较低、功能较为单一等问题，对于射程较短的手投防暴弹，为达到预期的战术效果，投掷者不得不抵近犯罪嫌疑人或暴骚乱人群，从而使自身暴露于对方的打击范围(如砖头、石块、玻璃瓶的攻击)之内。枪发的防暴弹为规避炸膛事故，通常为燃烧型弹药，不能对远距离目标形成较大威慑，而威慑性较大的爆炸型非致命弹药，如爆震弹、爆催弹又因为采用手投方式，而大大缩短了其投掷距离，且存在炸手等重大安全隐患，因此，这些非致命弹药均不能有效应对日益复杂多变的反恐、维稳局势。Anti-riot grenades are mainly used to temporarily incapacitate group or individual targets without causing permanent disability and belong to the category of non-lethal ammunition. At present, non-lethal ammunition plays an important role in the military, armed police, and public security in carrying out tasks such as counter-terrorism, emergency response, stability maintenance, and maritime rights protection. In order to achieve the expected tactical effect, the thrower has to approach the criminal suspect or the rioting crowd, thereby exposing himself to the opponent's attack range (such as the attack of bricks, stones, glass bottles) . In order to avoid the explosion accident, the anti-riot ammunition fired by the gun is usually incendiary ammunition, which cannot form a greater deterrent to long-distance targets, while the explosive non-lethal ammunition with greater deterrence, such as detonation bombs and detonation bombs, is also used. However, the throwing distance is greatly shortened, and there are major safety hazards such as bombing hands. Therefore, these non-lethal ammunition cannot effectively deal with the increasingly complex and changeable situation of anti-terrorism and stability maintenance.

防暴枪榴弹是常见的防暴器材之一，与杀伤弹药相比，防暴枪榴弹结构简单、成本低，适用于各种突发状况及防暴需求，但是现有的防暴枪榴弹功能较为单一，对一些极端恐怖分子的震慑效果较为一般，并且现有的防暴枪榴弹普遍射程较短，射速较慢，战技指标偏低，不便于灵活其战术战法。Anti-riot grenades are one of the common anti-riot equipment. Compared with killing ammunition, anti-riot grenades are simple in structure and low in cost. They are suitable for various emergencies and anti-riot needs. The deterrent effect is relatively general, and the existing anti-riot grenades generally have a short range, a slow rate of fire, and low combat technical indicators, which are inconvenient to flex their tactical tactics.

有鉴于此，针对现有的问题予以研究改良，提供一种撞击击发式增程防暴枪榴弹，旨在通过该技术，达到解决问题与提高实用价值性的目的。In view of this, research and improvement are carried out in view of the existing problems, and an impact-fired extended-range anti-riot grenade is provided, which aims to solve the problem and improve the practical value through this technology.

实用新型内容Utility model content

本实用新型的目的在于提供一种撞击击发式增程防暴枪榴弹，以解决上述背景技术中提出的现有的防暴枪榴弹功能较为单一，对一些极端恐怖分子的震慑效果较为一般，并且现有的防暴枪榴弹普遍射程较短，射速较慢，使用时存在较大的局限性的问题和不足。The purpose of this utility model is to provide a kind of impact-fired extended-range anti-riot grenade, in order to solve the problem that the existing anti-riot grenade proposed in the above-mentioned background technology is relatively single in function, and has a relatively general deterrent effect on some extreme terrorists, and the existing anti-riot grenade The grenade generally has a short range and a slow rate of fire, and there are large limitations and shortcomings when using it.

为实现上述目的，本实用新型提供了一种撞击击发式增程防暴枪榴弹，由以下具体技术手段所达成：In order to achieve the above-mentioned purpose, the utility model provides a kind of impact firing type extended-range anti-riot grenade, which is achieved by the following specific technical means:

一种撞击击发式增程防暴枪榴弹，包括：尾管、尾翼、子弹收集器、密封环、缓冲器、后置击针、基座、底火砧座、底火杯、引然药、封装、引火孔、延期管、推进部、飞行翼、火箭推进器、燃料仓、喷管、隔板、高压室、传火孔、低压室、打击部、嵌板、爆震弹体、催泪弹体、爆炸室、引爆器、击发端、轴向弹簧、前置击针、火帽、扩爆管、平衡销、径向弹簧、密封盖箔；所述尾翼焊接安装在尾管尾部的外壁上；所述子弹收集器嵌入安装在尾管前端的内侧；所述缓冲器嵌入安装在尾管前端的内侧，且缓冲器位于子弹收集器的前侧；所述密封环安装在子弹收集器与缓冲器之间；所述后置击针嵌入安装在子弹收集器的内侧，且后置击针通过贯穿方式与子弹收集器、缓冲器活动连接；所述尾管的前端焊接安装在推进部的尾部；所述推进部内部设置有火箭推进器，且燃料仓位于火箭推进器的前侧；所述飞行翼在推进部尾部的外壁上呈环形阵列状设置有四处，且喷管贯通设置在飞行翼的内侧；所述基座嵌入安装在推进部的尾部，且底火杯嵌入安装在基座尾部的内侧；所述引然药设置在底火杯的内侧，且封装覆盖在引然药的外侧；所述底火砧座设置在基座的内侧，且引火孔在底火砧座与基座之间呈环形阵列状分布设置有四处；所述隔板嵌入安装在推进部前端的内侧，且高压室设置在隔板前端的内侧；所述密封盖箔设置在高压室的内壁上；所述延期管位于火箭推进器、燃料仓的内侧，且延期管的一端与引火孔连接，延期管的另一端与高压室连接；所述打击部的尾部嵌入安装在推进部的前端；所述低压室位于隔板与打击部之间；所述传火孔贯通设置在隔板的前端，且传火孔的一端与高压室连接，传火孔的另一端与低压室连接；所述嵌板嵌入安装在打击部内侧的中间位置；所述爆震弹体、催泪弹体嵌入安装在嵌板尾部的外壁上；所述两处引爆器呈对称状嵌入安装在嵌板上，且引爆器与嵌板活动连接，引爆器的尾部与爆震弹体、催泪弹体连接；所述爆炸室设置在打击部的内侧，且扩爆管嵌入安装在爆炸室的内侧；所述平衡销的底部嵌入安装在扩爆管尾部的外壁上；所述径向弹簧的一端嵌入安装在爆炸室的内壁上，且径向弹簧的另一端与平衡销连接；所述火帽嵌入安装在扩爆管的端部；所述击发端设置在打击部的前端，且击发端与打击部通过轴向弹簧相连接；所述前置击针的一端嵌入安装在击发端的尾部，且前置击针嵌入安装在打击部的内侧。An impact-fired extended-range anti-riot grenade, comprising: a tail pipe, a tail fin, a bullet collector, a sealing ring, a buffer, a rear firing pin, a base, a primer anvil, a primer cup, a primer, a package, and a primer hole , delay tube, propulsion section, flying wing, rocket thruster, fuel tank, nozzle, partition, high pressure chamber, fire port, low pressure chamber, strike section, panel, detonation projectile, tear gas projectile, explosion chamber, Detonator, firing end, axial spring, front firing pin, flash cap, detonator, balance pin, radial spring, sealing cover foil; the tail fin is welded and installed on the outer wall of the tail pipe tail; the bullet collects The buffer is embedded and installed on the inner side of the front end of the tail pipe; the buffer is embedded and installed on the inner side of the front end of the tail pipe, and the buffer is located on the front side of the bullet collector; the sealing ring is installed between the bullet collector and the buffer; The rear firing pin is embedded and installed on the inner side of the bullet collector, and the rear firing pin is movably connected with the bullet collector and the buffer by means of penetration; A rocket propeller is arranged inside, and the fuel tank is located on the front side of the rocket propeller; the flying wing is arranged in four places in an annular array on the outer wall of the tail of the propelling part, and the nozzle is arranged through the inner side of the flying wing; the The base is embedded and installed at the tail of the propulsion part, and the primer cup is embedded and installed on the inner side of the tail of the base; the primer is arranged on the inner side of the primer cup, and the encapsulation covers the outside of the primer; the primer anvil is provided with On the inner side of the base, there are four ignition holes distributed in an annular array between the primer anvil and the base; the partition is embedded and installed on the inner side of the front end of the propulsion part, and the high-pressure chamber is arranged on the inner side of the front end of the partition plate. The sealing cover foil is arranged on the inner wall of the high pressure chamber; the delay tube is located on the inner side of the rocket propeller and the fuel tank, and one end of the delay tube is connected with the ignition hole, and the other end of the delay tube is connected with the high pressure chamber; the The tail of the striking part is embedded in the front end of the propulsion part; the low pressure chamber is located between the partition plate and the striking part; the fire transmission hole is arranged through the front end of the partition plate, and one end of the fire transmission hole is connected with the high pressure chamber, The other end of the fire hole is connected to the low pressure chamber; the panel is embedded and installed in the middle position of the inner side of the striking part; the detonation projectile and the tear gas projectile are embedded and installed on the outer wall of the tail of the panel; Symmetrically embedded and installed on the panel, and the detonator is movably connected to the panel, and the tail of the detonator is connected to the detonation bomb body and the tear gas bomb body; the explosion chamber is arranged on the inner side of the striking part, and the detonator is embedded and installed in the The inner side of the explosion chamber; the bottom of the balance pin is embedded and installed on the outer wall of the tail of the explosion tube; one end of the radial spring is embedded and installed on the inner wall of the explosion chamber, and the other end of the radial spring is connected with the balance pin; The flash cap is embedded and installed at the end of the explosion tube; the firing end is arranged at the front end of the striking part, and the firing end and the striking part are connected by an axial spring; one end of the front firing pin is embedded and installed in the firing part. The tail of the end, and the front firing pin is embedded in the inner side of the striking part.

作为本技术方案的进一步优化，本实用新型一种撞击击发式增程防暴枪榴弹，所述延期管内部装填延期药，所述延期管的延期时间为5S，5S的延期时间对应于推进部的助推时间，助推过程完成500m的飞行距离。As a further optimization of this technical solution, the utility model is an impact-fired extended-range anti-riot grenade. The delay tube is filled with delay medicine, the delay time of the delay tube is 5S, and the delay time of 5S corresponds to the assistance of the propulsion part. Pushing time, the boosting process completes a flight distance of 500m.

作为本技术方案的进一步优化，本实用新型一种撞击击发式增程防暴枪榴弹，所述高压室为拱形结构，且高压室的内部填充有扩爆药，扩爆药爆炸后迫使打击部与推进部分离，能够对打击部再次起到推动作用，实现了对打击部的连续推进，可有效提高射程。As a further optimization of this technical solution, the utility model is an impact-fired extended-range anti-riot grenade. The high-pressure chamber is an arched structure, and the interior of the high-pressure chamber is filled with explosives. The separation of the propulsion part can promote the strike part again, realize the continuous propulsion of the strike part, and effectively increase the range.

作为本技术方案的进一步优化，本实用新型一种撞击击发式增程防暴枪榴弹，所述低压室的内部填充有粉态染色剂，粉态染色剂受到冲击力随着打击部的脱离而炸散，对群体或单个目标进行染色标记，提高装置的功能性。As a further optimization of the technical solution, the utility model is an impact-fired extended-range anti-riot grenade. The interior of the low-pressure chamber is filled with a powdery coloring agent, and the powdery coloring agent is blown away by the impact force along with the detachment of the striking part. , to stain and label groups or individual targets to improve device functionality.

作为本技术方案的进一步优化，本实用新型一种撞击击发式增程防暴枪榴弹，所述打击部为中空式结构，且打击部的前端呈锥形，打击部的中部呈圆台状，打击部的尾部呈弧形，并且打击部中部的外壁上呈环形阵列状贯通设置有N处圆孔，打击部前端呈锥形能够有效减小飞行时的风阻，提高飞行速度，同时还能保证飞行稳定性，提高射击精度，而成环形阵列状分布的圆孔以便爆震弹体引爆时的巨响和强光以及催泪弹体引爆时散发的催泪气体更充分的释放出来。As a further optimization of the technical solution, the present invention provides an impact-fired extended-range anti-riot grenade, wherein the striking portion is a hollow structure, the front end of the striking portion is tapered, the middle portion of the striking portion is in the shape of a cone, and the striking portion is in the shape of a cone. The tail is arc-shaped, and the outer wall of the middle part of the striking part is provided with N round holes in a circular array. The front end of the striking part is tapered, which can effectively reduce the wind resistance during flight, improve the flight speed, and at the same time ensure the flight stability. , improve the shooting accuracy, and form a circular array of circular holes so that the loud noise and strong light when the detonation projectile is detonated and the tear gas emitted when the tear gas projectile is detonated can be released more fully.

作为本技术方案的进一步优化，本实用新型一种撞击击发式增程防暴枪榴弹，所述爆震弹体内部装填闪光剂，所述催泪弹体内部装填OC刺激粉末，所述爆震弹体和催泪弹体的壳体均由薄壁易碎复合材料加工制作，易碎壳体在扩爆管爆炸威力作用下迅速解体，释放内部装药。所述爆震弹体和催泪弹体内部中轴线上设置有可由引爆器引爆的内装扩爆药的扩爆药盒。As a further optimization of the technical solution, the present invention is an impact-fired extended-range anti-riot grenade. The detonation bomb body is filled with flashing agent, the tear gas body is filled with OC stimulation powder, and the detonation bomb body and the tear gas bomb are filled with OC stimulation powder. The shell of the body is made of thin-walled and fragile composite materials, and the fragile shell is rapidly disintegrated under the action of the explosive power of the expansion tube, releasing the internal charge. The detonation projectile body and the tear gas projectile body are provided with an expansion cartridge with a built-in expanding explosive that can be detonated by a detonator on the inner central axis.

作为本技术方案的进一步优化，本实用新型一种撞击击发式增程防暴枪榴弹，所述尾翼为矩形板状结构，且尾翼共设置有六处，尾翼在尾管尾部的外壁上呈环形阵列状分布，并且其中两处尾翼上贯通设置有圆孔，尾翼的设置提高了装置飞行时的稳定性，而圆孔用来安放瞄准用标尺，方便使用。As a further optimization of the technical solution, the utility model is an impact-fired extended-range anti-riot grenade. The tail is a rectangular plate-like structure, and the tail is provided at six places. The tail is in a ring-shaped array on the outer wall of the tail pipe. Two of the fins are provided with round holes through them. The arrangement of the fins improves the stability of the device during flight, and the round holes are used to place the aiming ruler, which is convenient for use.

作为本技术方案的进一步优化，本实用新型一种撞击击发式增程防暴枪榴弹，所述平衡销共设置有四处，且平衡销在扩爆管的外壁上呈环形阵列状分布，增强扩爆管的平衡性，起到保险的作用，避免扩爆管在非引爆状态受力发生引爆，提高装置的安全性。As a further optimization of the technical solution, the utility model is an impact-fired extended-range anti-riot grenade. The balance pins are arranged in four places, and the balance pins are distributed in an annular array on the outer wall of the explosion tube to strengthen the explosion tube. The balance of the device plays an insurance role, preventing the explosion tube from being detonated under the force of the non-detonation state, and improving the safety of the device.

作为本技术方案的进一步优化，本实用新型一种撞击击发式增程防暴枪榴弹，所述爆炸室的前端呈圆柱形，爆炸室的后端呈拱形，且爆炸室前端的内壁上设置有阶梯状环形凸起，阶梯状环形凸起对前置击针起到导向作用，防止撞针击发时发生偏移。As a further optimization of the technical solution, the utility model is an impact-fired extended-range anti-riot grenade. The front end of the explosion chamber is cylindrical, the rear end of the explosion chamber is arched, and a step is arranged on the inner wall of the front end of the explosion chamber. The stepped annular protrusion plays a guiding role for the front firing pin to prevent the firing pin from shifting when it is fired.

作为本技术方案的进一步优化，本实用新型一种撞击击发式增程防暴枪榴弹，所述密封盖箔的材质为铜，稳定性强，牢固性强，避免粉态染色剂进入高压室。As a further optimization of the technical solution, the utility model is an impact-fired extended-range anti-riot grenade. The sealing cover foil is made of copper, which has strong stability and firmness, and prevents powdery dyes from entering the high-pressure chamber.

由于上述技术方案的运用，本实用新型与现有技术相比具有下列优点：Due to the application of the above-mentioned technical solutions, the present invention has the following advantages compared with the prior art:

1、本实用新型火箭推进器嵌入安装在推进部的内侧，同时高压室为拱形结构，且高压室的内部填充有扩爆药的设置，击发时打击部能够受到子弹撞击、火箭推进器以及扩爆药爆炸的多级推力，具有较强的推进效果，进一步提高打击部的飞行速度，射程大为提高。1. The rocket propeller of the present invention is embedded and installed on the inner side of the propulsion portion, and the high-pressure chamber is an arched structure simultaneously, and the interior of the high-pressure chamber is filled with the setting of explosives, and the striking portion can be hit by bullets, rocket propellers and The multi-stage thrust of the explosive charge explosion has a strong propulsive effect, which further improves the flight speed of the strike section and greatly increases the range.

2、本实用新型低压室的内部填充有粉态染色剂，同时爆震弹体、催泪弹体嵌入安装在嵌板尾部的外壁上的设置，使装置具有染色、震晕、催泪的效果，功能全面，复合打击效果好，有效提高防暴效果。2. The interior of the low-pressure chamber of the utility model is filled with powdery dye, and the detonation bomb and the tear gas bomb are embedded and installed on the outer wall of the tail of the panel, so that the device has the effects of dyeing, shocking and tearing, and has comprehensive functions. , The compound strike effect is good, and the anti-riot effect is effectively improved.

3、本实用新型打击部为中空式结构，且打击部的前端呈锥形，打击部的中部呈圆台状，打击部的尾部呈弧形，并且打击部中部的外壁上呈环形阵列状贯通设置有N处圆孔的设置，打击部前端呈锥形能够有效减小飞行时的风阻，提高飞行速度，同时还能保证飞行精准度，提高射击精度，而成环形阵列状分布的圆孔以便爆震弹体引爆时的巨响和强光以及催泪弹体引爆时散发的催泪气体更充分的释放出来。3. The striking part of the present invention is a hollow structure, and the front end of the striking part is tapered, the middle part of the striking part is in the shape of a cone, the tail part of the striking part is arc-shaped, and the outer wall of the middle part of the striking part is arranged in a circular array. There are N round holes, and the front end of the striking part is tapered, which can effectively reduce the wind resistance during flight, improve the flight speed, and at the same time ensure the flight accuracy and improve the shooting accuracy. The loud noise and strong light when the shock bomb is detonated and the tear gas emitted when the tear gas is detonated are released more fully.

4、本实用新型通过对防暴榴弹的改进，具有结构设计合理、具有多级推进，飞行速度快，飞行稳定性强、功能全面，复合打击效果好，具有染色、震晕、催泪的效果，防暴效果好，实用性强的优点，从而有效的解决了本实用新型在背景技术一项中提出的问题和不足。4. Through the improvement of the anti-riot grenade, the utility model has reasonable structure design, multi-stage propulsion, fast flight speed, strong flight stability, comprehensive functions, good compound strike effect, and has the effects of dyeing, shocking, tearing, and anti-riot. It has the advantages of good effect and strong practicability, thereby effectively solving the problems and deficiencies raised in the background art of the present invention.

附图说明Description of drawings

图1为本实用新型的剖面结构示意图；Fig. 1 is the sectional structure schematic diagram of the present utility model;

图2为本实用新型的结构示意图；Fig. 2 is the structural representation of the utility model;

图3为本实用新型的打击部结构示意图；3 is a schematic structural diagram of a striking portion of the present invention;

图4为本实用新型的A处放大结构示意图；Fig. 4 is the enlarged structure schematic diagram of A place of the present utility model;

图5为本实用新型的B处放大结构示意图。FIG. 5 is a schematic view of the enlarged structure of B of the present invention.

图中：尾管1、尾翼2、子弹收集器3、密封环4、缓冲器5、后置击针6、基座7、底火砧座8、底火杯9、引然药10、封装11、引火孔12、延期管13、推进部14、飞行翼15、火箭推进器16、燃料仓17、喷管18、隔板19、高压室20、传火孔21、低压室22、打击部23、嵌板24、爆震弹体25、催泪弹体26、爆炸室27、引爆器28、击发端29、轴向弹簧30、前置击针31、火帽32、扩爆管33、平衡销34、径向弹簧35、密封盖箔36。In the figure: tail pipe 1, tail fin 2, bullet collector 3, sealing ring 4, buffer 5, rear firing pin 6, base 7, primer anvil 8, primer cup 9, primer 10, package 11, Flare hole 12, extension pipe 13, propulsion part 14, flying wing 15, rocket thruster 16, fuel tank 17, nozzle 18, baffle 19, high pressure chamber 20, fire hole 21, low pressure chamber 22, striking part 23, Panel 24, detonation projectile 25, tear gas projectile 26, explosion chamber 27, detonator 28, firing end 29, axial spring 30, front firing pin 31, flash cap 32, expansion tube 33, balance pin 34, Radial spring 35 , sealing cover foil 36 .

具体实施方式Detailed ways

下面将结合本实用新型实施例中的附图，对本实用新型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实用新型一部分实施例，而不是全部的实施例。基于本实用新型中的实施例，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，都属于本实用新型保护的范围。The technical solutions in the embodiments of the present utility model will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present utility model. Obviously, the described embodiments are only a part of the embodiments of the present utility model, rather than all the implementations. example. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative work fall within the protection scope of the present invention.

需要说明的是，在本实用新型的描述中，除非另有说明，“多个”的含义是两个或两个以上；术语“上”、“下”、“左”、“右”、“内”、“外”、“前端”、“后端”、“头部”、“尾部”等指示的方位或位置关系为基于附图所示的方位或位置关系，仅是为了便于描述本实用新型和简化描述，而不是指示或暗示所指的装置或元件必须具有特定的方位、以特定的方位构造和操作，因此不能理解为对本实用新型的限制。It should be noted that, in the description of the present utility model, unless otherwise specified, the meaning of "plurality" is two or more; the terms "upper", "lower", "left", "right", " The orientation or positional relationship indicated by "inside", "outside", "front end", "rear end", "head", "tail", etc. is based on the orientation or positional relationship shown in the accompanying drawings, and is only for the convenience of describing the present utility. The novel and simplified description does not indicate or imply that the device or element referred to must have a particular orientation, be constructed and operate in a particular orientation, and therefore should not be construed as limiting the invention.

此外，术语“第一”、“第二”、“第三”等仅用于描述目的，而不能理解为指示或暗示相对重要性。Furthermore, the terms "first," "second," "third," etc. are used for descriptive purposes only and should not be construed to indicate or imply relative importance.

同时，在本实用新型的描述中，除非另有明确的规定和限定，术语“相连”、“连接”应做广义理解，例如，可以是固定连接，也可以是可拆卸连接，或一体地连接；可以是机械连接，也可以是电性连接；可以是直接相连，也可以通过中间媒介间接相连。对于本领域的普通技术人员而言，可以具体情况理解上述术语在本实用新型中的具体含义。Meanwhile, in the description of the present invention, unless otherwise expressly specified and limited, the terms "connected" and "connected" should be understood in a broad sense, for example, it may be a fixed connection, a detachable connection, or an integral connection ; It can be a mechanical connection or an electrical connection; it can be directly connected or indirectly connected through an intermediate medium. For those of ordinary skill in the art, the specific meanings of the above terms in the present invention can be understood in specific situations.

请参见图1至图5，本实用新型提供一种撞击击发式增程防暴枪榴弹的具体技术实施方案：Please refer to Fig. 1 to Fig. 5, the present utility model provides a specific technical implementation scheme of an impact-fired extended-range anti-riot gun grenade:

一种撞击击发式增程防暴枪榴弹，包括：尾管1、尾翼2、子弹收集器3、密封环4、缓冲器5、后置击针6、基座7、底火砧座8、底火杯9、引然药10、封装11、引火孔12、延期管13、推进部14、飞行翼15、火箭推进器16、燃料仓17、喷管18、隔板19、高压室20、传火孔21、低压室22、打击部23、嵌板24、爆震弹体25、催泪弹体26、爆炸室27、引爆器28、击发端29、轴向弹簧30、前置击针31、火帽32、扩爆管33、平衡销34、径向弹簧35、密封盖箔36；尾翼2焊接安装在尾管1尾部的外壁上，提高飞行时的稳定性；子弹收集器3嵌入安装在尾管1前端的内侧，用于接收及收集子弹，并挤压缓冲器5，将动能传递至缓冲器5；缓冲器5嵌入安装在尾管1前端的内侧，且缓冲器5位于子弹收集器3的前侧，缓冲效果好，在承受挤压力时使本实用新型获得一定的初速度；密封环4安装在子弹收集器3与缓冲器5之间，增强密封效果；后置击针6嵌入安装在子弹收集器3的内侧，且后置击针6通过贯穿方式与子弹收集器3、缓冲器5活动连接，受子弹冲击力影响发生位移，并击发底火杯9，实现对火箭推进器16的点火；尾管1的前端焊接安装在推进部14的尾部；推进部14内部设置有火箭推进器16，且燃料仓17位于火箭推进器16的前侧，燃料仓为火箭推进器16提供燃料，火箭推进器16有效提高了本实用新型的飞行速度和射程；飞行翼15在推进部14尾部的外壁上呈环形阵列状设置有四处，且喷管18贯通设置在飞行翼15的内侧；基座7嵌入安装在推进部4的尾部，且底火杯9嵌入安装在基座7尾部的内侧；引然药10设置在底火杯9的内侧，且封装11覆盖在引然药10的外侧，用于火箭推进器16的点火；底火砧座8设置在基座7的内侧，且引火孔12在底火砧座8与基座7之间呈环形阵列状分布设置有四处，引然药10燃烧时通过引火孔12点燃火箭推进器16；隔板19嵌入安装在推进部14前端的内侧，且高压室20设置在隔板19前端的内侧，起到分割作用；密封盖箔36设置在高压室20的内壁上，稳定性强，牢固性强，避免粉态染色剂进入高压室；延期管13位于火箭推进器16、燃料仓17的内侧，且延期管13的一端与引火孔12连接，延期管13的另一端与高压室20连接，在点燃火箭推进器16的同时延期管13随之点燃，燃烧5S后点燃高压室20内的扩爆药；打击部23的尾部嵌入安装在推进部14的前端，便于分离；低压室22位于隔板19与打击部23之间；传火孔21贯通设置在隔板19的前端，且传火孔21的一端与高压室20连接，传火孔21的另一端与低压室22连接，高压室20内的扩爆药爆炸，并通过传火孔21将爆炸力传输至低压室22，实现了打击部23的分离与推进；嵌板24嵌入安装在打击部23内侧的中间位置；爆震弹体25、催泪弹体26嵌入安装在嵌板24尾部的外壁上，提高装置的功能性；两处引爆器28呈对称状嵌入安装在嵌板24上，且引爆器28与嵌板24活动连接，引爆器28的尾部与爆震弹体25、催泪弹体26连接，通过活动实现了爆震弹体25、催泪弹体26的引爆；爆炸室27设置在打击部23的内侧，且扩爆管33嵌入安装在爆炸室27的内侧；平衡销34的底部嵌入安装在扩爆管33尾部的外壁上；径向弹簧35的一端嵌入安装在爆炸室27的内壁上，且径向弹簧35的另一端与平衡销34连接；火帽32嵌入安装在扩爆管33的端部；击发端29设置在打击部23的前端，且击发端29与打击部23通过轴向弹簧30相连接；前置击针31的一端嵌入安装在击发端29的尾部，且前置击针31嵌入安装在打击部23的内侧，前置击针31撞击火帽32实现了扩爆管33的爆炸。An impact-fired extended-range anti-riot grenade, comprising: a tail pipe 1, a tail fin 2, a bullet collector 3, a sealing ring 4, a buffer 5, a rear firing pin 6, a base 7, a primer anvil 8, and a primer cup 9 , primer 10, package 11, ignition hole 12, extension pipe 13, propulsion part 14, flying wing 15, rocket thruster 16, fuel tank 17, nozzle 18, partition 19, high pressure chamber 20, fire hole 21 , low pressure chamber 22, striking part 23, panel 24, detonation projectile 25, tear gas projectile 26, explosion chamber 27, detonator 28, firing end 29, axial spring 30, front firing pin 31, flash cap 32, The expansion tube 33, the balance pin 34, the radial spring 35, the sealing cover foil 36; the tail fin 2 is welded and installed on the outer wall of the tail part of the tail pipe 1 to improve the stability during flight; the bullet collector 3 is embedded in the front end of the tail pipe 1 The inner side of the tube is used to receive and collect bullets, and squeeze the buffer 5 to transfer kinetic energy to the buffer 5; the buffer 5 is embedded in the inner side of the front end of the tail pipe 1, and the buffer 5 is located on the front side of the bullet collector 3 , the buffer effect is good, and the utility model can obtain a certain initial speed when it is subjected to the squeezing force; the sealing ring 4 is installed between the bullet collector 3 and the buffer 5 to enhance the sealing effect; the rear firing pin 6 is embedded in the bullet The inner side of the collector 3, and the rear firing pin 6 is movably connected with the bullet collector 3 and the buffer 5 through the penetration method, and is displaced by the impact force of the bullet, and the bottom fire cup 9 is fired to realize the ignition of the rocket propeller 16; The front end of the tail pipe 1 is welded and installed at the rear of the propulsion part 14; the propulsion part 14 is provided with a rocket thruster 16, and the fuel tank 17 is located on the front side of the rocket thruster 16. The fuel tank provides fuel for the rocket thruster 16, and the rocket propulsion The device 16 effectively improves the flight speed and range of the present utility model; the flying wings 15 are arranged in an annular array at four places on the outer wall of the rear end of the propulsion part 14, and the nozzles 18 are arranged through the inner side of the flying wings 15; the base 7 is embedded Installed at the tail of the propulsion part 4, and the primer cup 9 is embedded and installed on the inner side of the tail of the base 7; the primer 10 is arranged on the inner side of the primer cup 9, and the package 11 covers the outside of the primer 10 for rocket propulsion The primer 16 is ignited; the primer anvil 8 is arranged on the inner side of the base 7, and the ignition holes 12 are distributed in four places in an annular array between the primer anvil 8 and the base 7, and the primer 10 passes through the ignition holes when burning. 12 Ignite the rocket thruster 16; the partition plate 19 is embedded and installed on the inner side of the front end of the propulsion part 14, and the high pressure chamber 20 is arranged on the inner side of the front end of the partition plate 19, which plays a dividing role; the sealing cover foil 36 is arranged on the inner wall of the high pressure chamber 20 , strong stability, strong firmness, preventing powdery dyes from entering the high pressure chamber; the extension pipe 13 is located inside the rocket propeller 16 and the fuel tank 17, and one end of the extension pipe 13 is connected with the ignition hole 12, and the other end of the extension pipe 13 One end is connected to the high-pressure chamber 20, the extension tube 13 is ignited when the rocket thruster 16 is ignited, and the explosive charge in the high-pressure chamber 20 is ignited after burning for 5 seconds; separation; low pressure chamber 22 is located between the partition plate 19 and the striking part 23; the fire transmission hole 21 is arranged through the front end of the partition plate 19, and one end of the fire transmission hole 21 is connected with the high pressure chamber 20, and the other end of the fire transmission hole 21 is connected with the low pressure chamber 22 , the explosive charge in the high pressure chamber 20 explodes, and the explosive force is transmitted to the low pressure chamber 22 through the fire transmission hole 21, so as to realize the separation and advancement of the striking portion 23; the panel 24 is embedded in the middle position of the inside of the striking portion 23; The detonation bomb body 25 and the tear gas bomb body 26 are embedded and installed on the outer wall of the rear part of the panel 24 to improve the functionality of the device; Actively connected, the tail of the detonator 28 is connected with the detonation bomb body 25 and the tear gas bomb body 26, and the detonation of the detonation bomb body 25 and the tear gas bomb body 26 is realized through the activity; the explosion chamber 27 is arranged on the inner side of the striking part 23, and the explosion is expanded The tube 33 is embedded and installed on the inner side of the explosion chamber 27; the bottom of the balance pin 34 is embedded and installed on the outer wall of the tail of the expansion tube 33; one end of the radial spring 35 is embedded and installed on the inner wall of the explosion chamber 27, and the radial spring 35 The other end is connected with the balance pin 34; the fire cap 32 is embedded and installed at the end of the explosion tube 33; One end of the firing pin 31 is embedded and installed at the tail of the firing end 29 , and the front firing pin 31 is embedded and installed inside the striking portion 23 .

具体的，请参见图3，扩爆管33在平衡销34以及径向弹簧35的固定下平稳安装在爆炸室27内，并且由图可见火帽32的底部安装有环形板防止意外触发，当击发端29受到较大力冲击，扩爆管33和火帽32会在惯性作用下前移，与向后推动的前置击针31接触，实现引爆。Specifically, please refer to FIG. 3 , the expansion tube 33 is smoothly installed in the explosion chamber 27 under the fixing of the balance pin 34 and the radial spring 35, and it can be seen from the figure that the bottom of the flash cap 32 is installed with an annular plate to prevent accidental triggering. When the firing end 29 is impacted by a relatively large force, the expansion tube 33 and the flash cap 32 will move forward under the action of inertia, and come into contact with the front firing pin 31 pushed backwards to achieve detonation.

具体实施步骤：Specific implementation steps:

将尾管1套合安装到枪械的枪口，尾管1起到导向的作用，然后扣动枪械扳机发射子弹，子弹高速冲击后置击针6，后置击针6在子弹强大的冲击力下向前推进，子弹收集器3起到收集子弹的作用，用于接收及收集子弹，并挤压缓冲器5，将动能传递至缓冲器5，缓冲器5起到缓冲效果，后置击针6推进，针尖撞击底火杯9，致使引然药10燃烧，引然药10产生的燃气通过引火孔12将火箭推进器16点燃，火箭推进器16对本实用新型起到增程作用，提高本实用新型的飞行速度和射程，延期管13在火箭推进器16点燃的同时点燃，本实用新型到达预定范围后高压室20内的扩爆药被延期管13点燃，爆炸力通过传火孔21传递至低压室22，将打击部23推出，打击部23在爆炸力的作用下再次经过推进，与此同时低压室22内的粉态染色剂随着打击部23的脱离而炸出，对目标范围染色，打击部23接触坚硬物质时，击发端29受到较大力冲击，扩爆管33和火帽32会在惯性作用下前移，与向后推动的前置击针31接触，实现引爆，引爆器28受爆炸力的作用将爆震弹体25、催泪弹体26引爆，对目标区域内的群体(获个体)目标进行震晕和催泪驱散。Fit the tail pipe 1 to the muzzle of the firearm, the tail pipe 1 plays a guiding role, then pull the trigger of the firearm to fire the bullet, the bullet hits the rear firing pin 6 at a high speed, and the rear firing pin 6 has a strong impact on the bullet. Push down and move forward, the bullet collector 3 plays the role of collecting bullets, which is used to receive and collect bullets, and squeeze the buffer 5 to transfer the kinetic energy to the buffer 5. The buffer 5 plays a buffering effect, and the firing pin is placed behind. 6. Propulsion, the needle tip hits the bottom fire cup 9, causing the primer 10 to burn, and the gas generated by the primer 10 ignites the rocket propeller 16 through the ignition hole 12. With the new flight speed and range, the delay tube 13 is ignited when the rocket propeller 16 is ignited. After the utility model reaches the predetermined range, the explosive charge in the high-pressure chamber 20 is ignited by the delay tube 13, and the explosive force is transmitted to the rocket through the fire transmission hole 21. The low-pressure chamber 22 pushes out the striking portion 23, and the striking portion 23 is pushed forward again under the action of the explosive force. At the same time, the powdery dye in the low-pressure chamber 22 is blown out along with the detachment of the striking portion 23, which dyes the target area. , when the striking part 23 is in contact with the hard material, the firing end 29 is impacted by a large force, and the detonator 33 and the flash cap 32 will move forward under the action of inertia, and contact with the front firing pin 31 pushed back to achieve detonation. 28 Under the action of the explosive force, the detonation projectile 25 and the tear gas projectile 26 are detonated, and the group (individual) targets in the target area are stunned and dispelled by tear gas.

综上所述：该一种撞击击发式增程防暴枪榴弹，通过火箭推进器嵌入安装在推进部的内侧，同时高压室为拱形结构，且高压室的内部填充有扩爆药的设置，击发时打击部能够受到子弹撞击、火箭推进器以及扩爆药爆炸的多级推力，具有较好的增程效果，进一步提高打击部的飞行速度，提高防暴效果；通过低压室的内部填充有粉态染色剂，同时爆震弹体、催泪弹体嵌入安装在嵌板尾部的外壁上的设置，使装置具有染色、震晕、催泪的效果，功能全面，复合打击效果好，有效提高防暴效果；通过打击部为中空式结构，且打击部的前端呈锥形，打击部的中部呈圆台状，打击部的尾部呈弧形，并且打击部中部的外壁上呈环形阵列状贯通设置有N处圆孔的设置，打击部前端呈锥形能够有效减小飞行时的风阻，提高飞行速度，同时还能保证飞行精准度，提高射击精度，而成环形阵列状分布的圆孔以便爆震弹体引爆时的巨响和强光以及催泪弹体引爆时散发的催泪气体更充分的释放出来；通过对防暴榴弹的改进，具有结构设计合理、具有多级推进，飞行速度快，飞行稳定性强、功能全面，复合打击效果好，具有染色、震晕、催泪的效果，防暴效果好，实用性强的优点，从而有效的解决了本实用新型在背景技术一项中提出的问题和不足。To sum up: this kind of impact-fired extended-range anti-riot grenade is embedded and installed on the inner side of the propulsion part through the rocket thruster, and the high-pressure chamber is an arched structure, and the interior of the high-pressure chamber is filled with a setting for expanding explosives. When the strike part can be impacted by bullets, rocket thrusters and multi-stage thrust of the explosion of explosives, it has a good range extension effect, which further improves the flight speed of the strike part and improves the anti-riot effect; the interior of the low pressure chamber is filled with powder state. The dyeing agent, the detonation projectile and the tear gas projectile are embedded in the outer wall of the rear of the panel, so that the device has the effects of dyeing, shocking and tearing. The front part of the striking part is a hollow structure, the front end of the striking part is tapered, the middle part of the striking part is in the shape of a cone, the tail part of the striking part is arc-shaped, and the outer wall of the middle part of the striking part is in an annular array shape through which there are N circular holes. Setting, the front end of the striking part is tapered, which can effectively reduce the wind resistance during flight, improve the flight speed, and at the same time ensure the flight accuracy and improve the shooting accuracy. Loud noise and strong light, as well as the tear gas emitted when the tear gas body is detonated, are more fully released; through the improvement of the anti-riot grenade, it has a reasonable structure design, multi-stage propulsion, fast flight speed, strong flight stability, comprehensive functions, compound It has the advantages of good striking effect, dyeing, shocking and tear-inducing effects, good anti-riot effect and strong practicability, thus effectively solving the problems and deficiencies proposed in the background art of the present invention.

尽管参照前述实施例对本实用新型进行了详细的说明，对于本领域的技术人员来说，其依然可以对前述各实施例所记载的技术方案进行修改，或者对其中部分技术特征进行等同替换，凡在本实用新型的精神和原则之内，所作的任何修改、等同替换、改进等，均应包含在本实用新型的保护范围之内。Although the present invention has been described in detail with reference to the foregoing embodiments, for those skilled in the art, it is still possible to modify the technical solutions described in the foregoing embodiments, or perform equivalent replacements for some of the technical features. Within the spirit and principle of the present utility model, any modifications, equivalent replacements, improvements, etc. made shall be included within the protection scope of the present utility model.