CN104729364B - A kind of pneumatic separation bullet holder of light-gas gun - Google Patents
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Abstract
Description
技术领域technical field
本发明属于爆炸与冲击动力学领域,具体涉及一种轻气炮弹托结构的改进。The invention belongs to the field of explosion and impact dynamics, and in particular relates to an improvement of a light gas projectile support structure.
背景技术Background technique
弹托的作用是在炮管内对弹丸起定心引导作用,传递高压气体压力,使弹丸获得较高初速,并在出炮口到撞靶的过程中脱离弹丸,使其具有良好的外弹道性能,以避免弹托动能进一步加载到弹丸上。现有的方法主要采取附加分离装置进行分离,该技术存在的主要问题有:附加分离方法是在炮管与靶室之间设置机械装置,通过撞击使得弹托破碎分离。分离后形成的碎片仍会跟进并再一次作用在弹丸上,影响弹丸的外弹道性能。这类装置内孔与炮管同轴度要求较高,同时附加分离装置增加了轻气炮系统的复杂性,占用靶室空间,多次试验后还需更换易损部件,提高了发射成本。The role of the bullet rest is to center and guide the projectile in the barrel, transmit high-pressure gas pressure, make the projectile obtain a higher initial velocity, and separate from the projectile during the process from exiting the muzzle to hitting the target, so that it has good external ballistic performance , in order to avoid further loading of the kinetic energy of the bullet rest on the projectile. The existing method mainly adopts an additional separation device for separation. The main problems of this technology are: the additional separation method is to install a mechanical device between the gun barrel and the target chamber, and the bullet holder is broken and separated by impact. The fragments formed after separation will still follow up and act on the projectile again, affecting the external ballistic performance of the projectile. The coaxiality between the inner hole and the gun barrel of this type of device is relatively high. At the same time, the additional separation device increases the complexity of the light gas gun system, occupies the space in the target room, and needs to replace vulnerable parts after multiple tests, which increases the launch cost.
发明内容Contents of the invention
为解决现有轻气炮弹托分离困难,需借助于其它机械装置进行分离且分离效果差,轻气炮系统结构复杂的技术问题,本发明提供一种气动分离弹托,在发射弹丸出炮口到撞靶过程中能够顺利实现弹托与弹丸的自动分离。In order to solve the technical problems of the separation difficulty of the existing light gas gun shell holder, which needs to be separated by means of other mechanical devices and the separation effect is poor, and the structure of the light gas gun system is complicated, the invention provides a pneumatically separated bullet holder, which can In the process of hitting the target, the automatic separation of the bullet holder and the projectile can be smoothly realized.
本发明的技术方案如下:Technical scheme of the present invention is as follows:
一种轻气炮气动分离弹托,其特殊之处在于:包括上托瓣、下托瓣及底板,所述上托瓣、下托瓣相扣合形成外径与炮管内径相匹配的圆柱体,所述圆柱体沿长度方向从前至后开设有气涡结构及盲孔形的弹丸孔,所述气涡结构为从圆柱体前端向后开设的第一空腔,所述第一空腔的尺寸从圆柱体前端向后逐渐变小,所述底板设置在圆柱体的底部的后端。A kind of aerodynamic separation bullet holder for a light gas gun, which is special in that it includes an upper holder flap, a lower holder flap and a bottom plate, and the upper holder flap and the lower holder flap are buckled together to form a cylinder whose outer diameter matches the inner diameter of the gun barrel body, the cylinder is provided with an air vortex structure and blind hole-shaped projectile holes from front to back along the length direction, the air vortex structure is a first cavity opened from the front end of the cylinder backward, and the first cavity The size gradually becomes smaller from the front end of the cylinder to the rear, and the bottom plate is arranged at the rear end of the bottom of the cylinder.
以上为本发明的基本技术方案,基于该技术方案,本发明还可以下作出以下改进:The above is the basic technical solution of the present invention, based on the technical solution, the present invention can also make the following improvements:
上述轻气炮气动分离弹托还包括沿圆柱体长度方向开设的第二空腔,所述第二空腔的径向尺寸大于弹丸孔的直径,所述第二空腔与第一空腔及圆柱体的后端均有一段距离。Above-mentioned light gas cannon aerodynamic separation ball support also comprises the second cavity that offers along cylinder length direction, and the radial dimension of described second cavity is greater than the diameter of projectile hole, and described second cavity and first cavity and There is a certain distance between the rear ends of the cylinders.
上述第一空腔、弹丸孔及第二空腔的轴线均与圆柱体的轴线重合。这一限定主要是为了保证弹丸装配后与炮管的同轴度,以及整个发射弹在炮管运行过程中受力的对称。The axes of the first cavity, the projectile hole and the second cavity are all coincident with the axis of the cylinder. This limitation is mainly to ensure the coaxiality of the projectile and the barrel after assembly, and the symmetry of the force on the entire projectile during the operation of the barrel.
上述第一空腔的形状为回转体,回转体的母线为弧线或直线,母线为弧线或直线是基于加工难易程度考虑。The shape of the above-mentioned first cavity is a revolving body, and the generatrix of the revolving body is an arc or a straight line, and the reason for the generatrix being an arc or a straight line is based on the ease of processing.
上述回转体的弧线母线与圆柱体相切,其弦与圆柱体外壁的夹角为30°~45°;所述回转体的直线母线与圆柱体外壁的夹角为30°~45°。该结构限定主要是综合考虑第一空腔的气动性能和结构强度,若是角度太小,前端锥角部分强度可能不够,角度太大产生的分离作用力有限,不能很好地实现分离,该角度通过试验验证可行.The arc generatrix of the above-mentioned revolving body is tangent to the cylinder, and the angle between the chord and the outer wall of the cylinder is 30°-45°; the angle between the straight-line generatrix of the revolving body and the outer wall of the cylinder is 30°-45°. This structural limitation is mainly based on comprehensive consideration of the aerodynamic performance and structural strength of the first cavity. If the angle is too small, the strength of the front cone may not be sufficient. If the angle is too large, the separation force will be limited and the separation cannot be achieved well. It is proved feasible by experiments.
上述第二空腔的形状为圆柱形。第二空腔可以采用其它的形状,母线为向外凹或向内凸的弧线以及带角度的直线都可以,该圆柱状主要用于减少弹托的消极重量,同时在分离过程中形成第二气涡,加速弹托分离。The above-mentioned second cavity is cylindrical in shape. The second cavity can adopt other shapes, and the generatrix can be an outwardly concave or inwardly convex arc or a straight line with an angle. The cylindrical shape is mainly used to reduce the negative weight of the bullet holder and form the first The two air vortexes accelerate the separation of the bullet holder.
上述上托瓣包括半圆缺,所述半圆缺设置在上托瓣的后端,所述下托瓣包括与半圆缺相适配的凸台,所述上托瓣与下托瓣的通过半圆缺与凸台的配合扣合成圆柱体。上托瓣和下托瓣必须扣合成一个完整的圆柱状,但可以采用其他的形式实现。下托瓣可以是凸条,上托瓣可以是相配合的凹槽。The above-mentioned upper support flap includes a semicircle, and the semicircle is arranged at the rear end of the upper support flap, and the lower support flap includes a boss that is adapted to the semicircle, and the passage between the upper support flap and the lower support flap The matching buckle with the boss forms a cylinder. The upper tray and the lower tray must be buckled into a complete cylinder, but other forms can be used. The lower support flap can be a convex strip, and the upper support flap can be a matching groove.
所述底板与下托瓣构成一个整体。The bottom plate and the lower support flap form an integral body.
上述底板上设置有至少一道环向密封槽。At least one circumferential sealing groove is provided on the bottom plate.
上述上托瓣、下托瓣和底板材质均为尼龙。The above-mentioned upper support valve, lower support valve and bottom plate are made of nylon.
本发明的优点如下:The advantages of the present invention are as follows:
1、本发明气涡结构能快速响应空气阻力,在前端形成高压气涡,产生径向的分离作用力,实现上下托瓣和底板的自动分离;1. The air vortex structure of the present invention can quickly respond to air resistance, form a high-pressure air vortex at the front end, generate radial separation force, and realize the automatic separation of the upper and lower support valves and the bottom plate;
2、本发明在保证弹托结构强度的同时,将径向部分掏成中空结构,减轻弹托消极重量,同时分离过程中还可以形成附加气涡,进一步加剧弹托的分离;2. While ensuring the structural strength of the bullet holder, the present invention digs out the radial part into a hollow structure to reduce the negative weight of the bullet holder. At the same time, an additional air vortex can be formed during the separation process to further aggravate the separation of the bullet holder;
3、本发明将下托瓣与底板构成一个整体,底板在下托瓣分离时附带分离,不需再采取额外办法对底板进行分离;3. In the present invention, the lower support flap and the bottom plate are integrated, and the bottom plate is separated when the lower support flap is separated, and no additional measures are needed to separate the bottom plate;
4、本发明设计两道密封槽,解决了单道密封漏气的问题。4. The invention designs two sealing grooves, which solves the problem of air leakage of single sealing.
5、本发明弹托采用高比强度材料尼龙作为主体材料,既减轻了弹托的消极重量,同时又保证了弹托的结构强度;5. The bullet holder of the present invention adopts high-specific-strength material nylon as the main material, which not only reduces the negative weight of the bullet holder, but also ensures the structural strength of the bullet holder;
6、本发明通过改变弹丸孔直径和轴向长度,可以适用不同尺寸的弹丸,通用性强。6. The present invention can be applied to projectiles of different sizes by changing the diameter and axial length of the projectile hole, and has strong versatility.
附图说明Description of drawings
图1为130mm轻气炮气动分离弹托三维结构示意图;Figure 1 is a schematic diagram of the three-dimensional structure of the aerodynamic separation bullet holder of a 130mm light gas gun;
图2为130mm轻气炮气动分离弹托二维剖面示意图;Figure 2 is a schematic diagram of a two-dimensional cross-section of a 130mm light gas gun with aerodynamically separated bullet holder;
图3为130mm轻气炮气动分离弹托炮管中装配示意图;Figure 3 is a schematic diagram of the assembly in the barrel of the 130mm light gas gun with aerodynamically separated bullet holder;
图4为130mm轻气炮气动分离弹托开始分离示意图;Figure 4 is a schematic diagram of the start of separation of the 130mm light gas gun aerodynamic separation bullet holder;
图5为130mm轻气炮气动分离弹托进一步分离示意图;Figure 5 is a schematic diagram of the further separation of the aerodynamic separation bullet holder of the 130mm light gas gun;
图6为本发明轻气炮气动分离弹托的另一种扣合结构。Fig. 6 is another fastening structure of the light gas gun aerodynamic separation bullet holder of the present invention.
附图标记如下:1-上托瓣,2-下托瓣,3-底板,4-上半弹丸孔,5-下半弹丸孔,6-上半中空结构,7-下半中空结构,8-密封槽,9-半圆缺,10-凸台,11-上半气涡结构,12-下半气涡结构,13-弹丸,14-密封圈,15-炮管,16-高压气体,17-炮管前端,18-空气阻力,19-气涡,20-托瓣外表面气流,21-凸条、22-凹槽。The reference signs are as follows: 1-upper support valve, 2-lower support valve, 3-bottom plate, 4-upper half projectile hole, 5-lower half projectile hole, 6-upper half hollow structure, 7-lower half hollow structure, 8 -Sealing groove, 9-semi-round gap, 10-boss, 11-upper half air vortex structure, 12-lower half air vortex structure, 13-projectile, 14-sealing ring, 15-barrel, 16-high pressure gas, 17 - the front end of the gun barrel, 18 - air resistance, 19 - air vortex, 20 - airflow on the outer surface of the support flap, 21 - convex strip, 22 - groove.
具体实施方式detailed description
弹托是一个受力很复杂的结构件,受高压气体的推力作用,驱动弹托带动弹丸在膛内运动。弹托必须具有一定的发射强度,保证在膛压最恶劣的条件下保持完整,不致破裂,这样才能正确引导弹丸在炮管运动。弹托是发射弹丸的重要部件,但它属于“非战斗部件”,它的重量是消极重量,所以在弹托的设计过程中,在保证发射强度的条件下,应从结构和材料出发,最大限度降低它的消极重量。The bullet holder is a structural part with very complicated force. It is driven by the thrust of the high-pressure gas to drive the bullet to move in the chamber. The bullet support must have a certain firing strength to ensure that it remains intact under the worst conditions of the chamber pressure and will not break, so that it can correctly guide the movement of the projectile in the barrel. The bullet holder is an important part of launching projectiles, but it is a "non-combat component", and its weight is negative weight. Therefore, in the design process of the bullet holder, under the condition of ensuring the launch strength, it should be based on the structure and materials. Lower its negative weight.
基于上述考虑,本发明气动分离弹托采取分瓣中空形状,前端设计了一个气涡结构,在发射弹丸出炮口后驱动弹托与弹丸分离,同时中间部分被掏成中空结构,减少弹托的消极重量并加剧分离,在高速状态下利用空气阻力可以实现自动分离,且分离过程基本不影响弹丸的外弹道性能。Based on the above considerations, the pneumatic separation bullet holder of the present invention adopts a split hollow shape, and an air vortex structure is designed at the front end to drive the bullet holder to separate from the projectile after the projectile is fired out of the muzzle. At the same time, the middle part is hollowed out to reduce the number of bullet holders The negative weight of the projectile will intensify the separation, and the automatic separation can be realized by using the air resistance at high speed, and the separation process basically does not affect the external ballistic performance of the projectile.
实施例一:(参见图1、图2)本实施例由上托瓣1、下托瓣2和底板3组成;上托瓣1和下托瓣2是两个对应的半圆柱体,上托瓣1前端设计有气涡结构11,中心开有弹丸孔4;下托瓣2与底板3构成一个整体,底板在本发明中是必须的,起传递高压气体压力的作用,下托瓣2前端设计有与上托瓣1相对应的气涡结构12,中心开有弹丸孔5;底板3刻有两个密封槽8。上托瓣1的上半弹丸孔4与下托瓣2的下半弹丸孔5相对应,上托瓣1半圆缺9与下托瓣2凸台10卡合。所述上托瓣1、下托瓣2和底板3材质均为尼龙。Embodiment 1: (see Fig. 1, Fig. 2) this embodiment is made up of upper support valve 1, lower support valve 2 and base plate 3; Upper support valve 1 and lower support valve 2 are two corresponding half cylinders, and upper support valve The front end of the petal 1 is designed with an air vortex structure 11, and the center is provided with a projectile hole 4; the lower support valve 2 and the bottom plate 3 form an integral body, and the bottom plate is necessary in the present invention, and plays the role of transmitting high-pressure gas pressure. The front end of the lower support valve 2 It is designed with an air vortex structure 12 corresponding to the upper support valve 1, and a bullet hole 5 is opened in the center; the bottom plate 3 is engraved with two sealing grooves 8. The upper half of the projectile hole 4 of the upper support valve 1 corresponds to the lower half of the projectile hole 5 of the lower support valve 2, and the semicircular gap 9 of the upper support valve 1 is engaged with the boss 10 of the lower support valve 2. The materials of the upper support valve 1, the lower support valve 2 and the bottom plate 3 are nylon.
实施例二:(参见图2)本实施例与上一实施例的不同点在于,气涡结构11和气涡结构12的构造线可以为直线和弧线。直线与托瓣外壁夹角为30°~45°;弧线与托瓣外壁相切,其弦与托瓣外壁夹角为30°~45°。Embodiment 2: (see FIG. 2 ) The difference between this embodiment and the previous embodiment is that the construction lines of the air vortex structure 11 and the air vortex structure 12 can be straight lines or arcs. The angle between the straight line and the outer wall of the support valve is 30°-45°; the arc is tangent to the outer wall of the support valve, and the angle between the chord and the outer wall of the support valve is 30°-45°.
实施例三:(参见图1、图2)本实施例三与实施例一的不同点在于,上托瓣1中间被掏成中空结构6,下托瓣2中间被掏成与上托瓣1相对应的中空结构7。Embodiment 3: (see Fig. 1, Fig. 2) The difference between the present embodiment 3 and embodiment 1 is that the middle of the upper support valve 1 is hollowed out into a hollow structure 6, and the middle of the lower support valve 2 is hollowed out to be the same as that of the upper support valve 1. The corresponding hollow structure 7.
实施例四:(参见图1、图6)本实施例与实施例一的不同点在于,上托瓣和下托瓣必须扣合成完整的圆柱状的方式不同,下托瓣为凸条21,上托瓣是与凸条相配合的凹槽22。Embodiment four: (referring to Fig. 1, Fig. 6) the difference between this embodiment and embodiment one is that the way that the upper support valve and the lower support valve must be buckled into a complete cylindrical shape is different, and the lower support valve is a convex strip 21, The upper support flap is a groove 22 matched with the protruding strip.
工作原理:如图3所示,发射弹由弹丸和弹托组成,整体装配于炮管中,依靠炮管的约束使得上下托瓣卡合,炮管前端被抽成真空环境。当轻气炮启动发射指令后,弹托底部受到高压气体的作用,推动发射弹在炮管中加速运动。如图4所示,发射弹出炮口后,根据空气动力学原理,空气阻力进入气涡结构中,流速降低并形成气涡;托瓣外表面空气阻力未受影响,流速基本不变。因此,在气涡结构中会形成一个相对托瓣外壁的高压,产生径向的张力以及轴向的阻力,使得上托瓣和下托瓣分别向上和向下张开,形成较大的分离角,并沿轴向分离。气流进一步进入中空结构中,也会产生高压气涡,加剧上下两托瓣的分离。如图5所示,在飞行过程中,在空气阻力作用下,弹丸与弹托进一步分离,只要炮口与靶板之间距离足够,弹丸会彻底摆脱弹托束缚,保证在弹丸撞靶后,弹托动能不会再一次加载到弹丸上,影响弹丸的外弹道性能。Working principle: As shown in Figure 3, the projectile is composed of a projectile and a bullet holder, which are integrally assembled in the gun barrel. Relying on the constraints of the gun barrel, the upper and lower brackets are engaged, and the front end of the gun barrel is evacuated into a vacuum environment. When the light gas gun activates the firing command, the bottom of the bullet holder is affected by the high-pressure gas, which pushes the firing bullet to accelerate in the barrel. As shown in Figure 4, after the launch ejects from the muzzle, according to the principle of aerodynamics, the air resistance enters the air vortex structure, the flow velocity decreases and an air vortex is formed; the air resistance on the outer surface of the support flap is not affected, and the flow velocity basically remains unchanged. Therefore, in the air vortex structure, a high pressure will be formed against the outer wall of the supporting valve, which will generate radial tension and axial resistance, so that the upper supporting valve and the lower supporting valve will open upward and downward respectively, forming a large separation angle. , and are separated axially. When the airflow further enters the hollow structure, a high-pressure air vortex will also be generated, which will intensify the separation of the upper and lower trays. As shown in Figure 5, during the flight, under the action of air resistance, the projectile and the carrier are further separated. As long as the distance between the muzzle and the target plate is sufficient, the projectile will completely get rid of the restraint of the carrier, ensuring that after the projectile hits the target, The kinetic energy of the bullet rest will not be loaded on the projectile again, affecting the external ballistic performance of the projectile.
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CN100370214C (en) * | 2005-04-29 | 2008-02-20 | 哈尔滨工业大学 | Curved shape self-separating bomb holder |
CN201081633Y (en) * | 2007-07-04 | 2008-07-02 | 齐齐哈尔雄鹰猎弹有限公司 | Moving bomb holder |
CN102062565B (en) * | 2010-11-08 | 2013-04-03 | 西安近代化学研究所 | Separator for preventing sabot from following |
CN204240872U (en) * | 2014-11-19 | 2015-04-01 | 哈尔滨工业大学 | The holder of one tooth engagement under water resilient separation bullet |
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