阅读说明：本技术 一种自增焓持续动燃推进装置 (Self-enthalpy-increasing continuous dynamic combustion propulsion device ) 是由 马宏昊 陈子俊 王鲁庆 赵凯 孙玉玲 沈兆武 于 2021-02-07 设计创作，主要内容包括：本发明公开了一种自增焓持续动燃推进装置,包括：在身管内壁规则布置装药结构,装药形式可以是凹槽、药室等。弹丸被底火推进后,前方形成冲击波,在弹底高温高压燃气和固体微粒以及冲击波压缩下装药结构被引燃,降低由于弹丸高速运动弹后空间形成的压力梯度,削弱稀疏波影响,在弹底部形成一个较高的、近似恒定的压力,并增加弹丸后方体系的焓值,提高总温,使弹丸达到较高速度。所述结构装药可以是利用炮管内膛线之间的缝隙,也可以是凹槽、凹坑等,布置形式根据需要而定,比如螺旋分布、直线分布等。本发明不仅提高了弹丸的出口速度,而且还降低了主药室的膛压。(The invention discloses an auto enthalpy-increasing continuous dynamic combustion propulsion device, which comprises: the charging structure is regularly arranged on the inner wall of the barrel, and the charging form can be a groove, a medicine chamber and the like. After the projectile is propelled by the primer, the front part forms shock waves, the charge structure is ignited under the compression of high-temperature and high-pressure gas and solid particles at the bottom of the projectile and the shock waves, the pressure gradient formed by the space behind the projectile moving at high speed is reduced, the influence of rarefaction waves is weakened, higher and approximately constant pressure is formed at the bottom of the projectile, the enthalpy value of a system behind the projectile is increased, the total temperature is increased, and the projectile reaches higher speed. The structural charging can be performed by utilizing gaps between bore lines of the gun barrel, and can also be performed by utilizing grooves, pits and the like, and the arrangement form is determined according to the requirement, such as spiral distribution, linear distribution and the like. The invention not only improves the outlet speed of the projectile, but also reduces the chamber pressure of the main medicine chamber.)

1. An automatic enthalpy-increasing continuous dynamic combustion propulsion device is characterized in that: and the charging structures are regularly arranged on the inner wall of the barrel, the charging structures can be gaps, grooves or pits between rifling lines in the barrel, and the arrangement form of the charging structures is determined according to the requirement.

2. The self-enthalpy-increasing continuous dynamic combustion propulsion device according to claim 1, characterized in that: the enthalpy of the self-increasing refers to the continuous reaction generated at the bottom of the projectile, the energy is continuously released, the enthalpy value of a medium at the bottom area of the projectile is increased, and the influence of sparse waves is weakened.

3. The self-enthalpy-increasing continuous dynamic combustion propulsion device according to claim 1, characterized in that: regularly arrange charge structure at the barrel inner wall, the shot is propelled the back by the primer, and the place ahead forms the shock wave, and charge structure is ignited under the compression of bullet end high temperature high pressure gas and solid particle and shock wave, provides the propulsive force that lasts for the shot bottom simultaneously to increase the enthalpy value of shot rear system, improve total temperature, weaken the rarefaction wave influence, guarantee that the shot has the driving force that lasts, reach higher speed.

4. The self-enthalpy-increasing continuous dynamic combustion propulsion device according to claim 1, characterized in that: the arrangement form of the charge structures is spiral distribution or linear distribution.

Technical Field

The invention belongs to the technical field of launching, and particularly relates to an auto-enthalpy-increasing continuous dynamic combustion propulsion device.

Background

Since the high initial velocity projectile launching device has undoubted superiority in modern technology, researchers in various countries around the world are constantly exploring and researching how to improve the launching velocity of the projectile or fragment. A series of new acceleration means have been developed from early artillery, light gas cannon, to late electromagnetic cannon, electric heating chemical cannon, etc. Although the existing means have advantages, the technology is still difficult to be applied to the impact experiment research of the actual combat and engineering damage terminal effect in a short time due to the influence of the current basic conditions, the expenses, the application and the like.

The current launching devices are mainly artillery, light gas artillery and electromagnetic artillery. In the weapon technology, a large amount of high-temperature and high-pressure gas generated during detonation of gunpowder is used for expansion to work, and the projectile is pushed linearly along the barrel to realize high-speed motion. The technology for improving the initial speed of the shot mainly focuses on the aspects of improving the combustion area of gunpowder, increasing the loading amount in a bore, improving the combustion speed of the gunpowder, improving the combustion heat of the gunpowder and the like for many years, and through the development of decades, the launching speed of the common shot is only about 1800 m/s. Experts have recognized that the performance of conventional artillery is approaching its limits. The traditional light gas gun pushes the projectile to move through compressed gas, and the projectile is launched by using a projectile support separation technology to carry out ballistic test on a protective structure. Although the existing light-gas cannon can launch ultra-high-speed projectiles, and has good consistency and speed stability, the existing light-gas cannon can only accelerate gram-mass-level projectiles, is high in cost and difficult to protect, and requires a cannon opening mechanism to be large in instant valve opening and high in speed, so that the acceleration of the large-mass projectiles is difficult to realize. The electromagnetic cannon accelerates the metal shot by using ampere force generated by an electromagnetic field in an electromagnetic system. Because the shape of the loaded broken piece or bullet is not restricted by the shape of the barrel, the device has stable work, good repeatability and easy adjustment of the firing range, and is widely regarded. However, the acceleration of the electromagnetic cannon requires the acceleration of the projectile through a multi-stage coil, the operation of the acceleration process is very complex, the ultrahigh-speed launching can be only carried out on gram-mass-level fragments, and the current is very large when the capacitor charges and discharges the coil, so that overheating can be generated, and the service life of the electromagnetic cannon is shortened.

Disclosure of Invention

The launching process of the shot takes gunpowder as energy. Under the action of proper external energy, the gunpowder is quickly and regularly burnt, and simultaneously, a large amount of high-temperature fuel gas is generated. To launch a projectile, a primer is first fired by mechanically (or electrically, optically, etc.) acting on the primer. After the primer is fired, the flame generated by the primer ignites the ignition powder in the gunpowder bed, so that the ignition powder is combusted to generate high-temperature and high-pressure gas and solid particles, the propellant powder close to the ignition powder is ignited in a convection and radiation mode, and then the whole gunpowder bed is further ignited. Along with the burning of gunpowder, a large amount of high-temperature and high-pressure gas is generated, and the gas in the space behind the bullet expands rapidly to drive the bullet to move at high speed in the barrel.

During the high-speed movement of the projectile, the solid gunpowder in the space behind the projectile continuously burns and continuously supplements high-temperature gas, and the rapid expansion of the high-temperature high-pressure gas enables the projectile and the barrel to generate various complex movements, including the movement of the projectile, the friction between the projectile and the barrel, the movement of the burning solid gunpowder and gas, the heat exchange between gunpowder gas and the barrel, the backseat of the cannon and the like. These movements occur simultaneously and interact with each other, which characterizes the pressure variations in the chamber. The rate of propellant gas generation and the rate of increase in post-projectile space due to projectile motion are among the two main factors that determine this variation. The increase of the gas generation rate increases the pressure in the bore, the increase of the space behind the projectile decreases the pressure in the bore, and the change of the bore pressure adversely affects the generation rate of the gunpowder gas and the movement of the projectile. At the beginning, the post-projectile pressure will rise continuously as the gas generation rate of the gunpowder exceeds the post-projectile space increase. When these two effects reach equilibrium, the pressure of the bullet bottom will reach maximum, i.e. p ═ p_m. And the space behind the projectile is continuously increased along with the continuous increase of the speed of the projectile, and the pressure in the chamber begins to reduce under the action of rarefaction waves continuously generated behind the bottom of the projectile, so that the acceleration of the projectile is reduced.

According to the internal ballistic theory, to increase the initial velocity of the projectile, the area under the p-l curve needs to be increased. For the powder charge itself, the p-l curve can be suitably directed upwardsShifting (increasing the amount of powder gas) and by changing the shape of the p-l curve (changing the law of generation of the gas). The ideal scheme is to keep the pressure after the bullet in the moving process of the bullet in the barrel unchanged, namely p is p_mI.e. a so-called pressure plateau effect is formed. According to classical internal ballistics, the equation of motion of the projectile:

in the formula (I), the compound is shown in the specification,is the virtual mass coefficient of the projectile, m is the projectile mass, v is the projectile velocity, S is the barrel internal cross-sectional area, and p is the projectile bottom pressure. The initial velocity attained by the projectile at this point is the maximum velocity possible at a given pressure. However, in practical situations, it is not possible to achieve a pressure plateau using existing powder and charge technology. However, it is possible to appropriately change the shape of the p-l curve so that the curve becomes gentle in the vicinity of the maximum pressure.

The invention provides an enthalpy-increasing continuous dynamic combustion propelling device, which is based on the principle and aims at solving the problems of propelling a projectile launching device in the prior art, and the main idea is that the projectile launching and charging structure is adjusted necessarily: regularly arrange charge structure at the barrel inner wall, the charge form can be recess, medicine room etc. and the pellet is propelled the back by the primer, and the place ahead forms the shock wave, and charge structure is lighted under the compression of bullet end high temperature high pressure gas and solid particle and shock wave, provides the propulsive force that lasts for the pellet bottom simultaneously to increase the enthalpy value of pellet rear system, improve total temperature, weaken the sparse wave influence, guarantee that the pellet has the driving force that lasts, reach higher speed. The charging structure can be formed by utilizing gaps among rifling lines in the gun barrel, or grooves, pits and the like, and the arrangement form is determined according to the requirement, such as spiral distribution, linear distribution and the like.

The technical scheme adopted by the invention is as follows: an auto-enthalpy sustained dynamic combustion propulsion device, comprising: and the charging structures are regularly arranged on the inner wall of the barrel, the charging structures can be gaps, grooves or pits between rifling lines in the barrel, and the arrangement form of the charging structures is determined according to the requirement.

Furthermore, the enthalpy of the self-increasing refers to the continuous reaction generated at the bottom of the projectile, the energy is continuously released, the enthalpy value of a medium in the bottom area of the projectile is increased, and the influence of rarefaction waves is weakened.

Furthermore, the explosive charging structures are regularly arranged on the inner wall of the barrel, after the projectile is propelled by primer, shock waves are formed in the front of the projectile, the explosive charging structures are ignited under the compression of high-temperature and high-pressure gas and solid particles at the bottom of the projectile and the shock waves, continuous propelling force is provided for the bottom of the projectile, the enthalpy value of a rear system of the projectile is increased, the total temperature is increased, the influence of rarefaction waves is weakened, continuous propelling force of the projectile is guaranteed, and high speed is achieved.

Further, the arrangement form of the charging structures is spiral distribution or linear distribution.

The invention relates to an auto enthalpy-increasing continuous dynamic combustion propulsion device, which can bring about a dramatic effect by application:

(1) according to the device, the high gradual powder is adopted for charging the main powder chamber, the generation rule of fuel gas is changed, the time interval from the beginning of the movement of the shot to the maximum pressure in the body pipe is shortened, and the area of a p-l curve is increased.

(2) According to the device, the blocking tablet is arranged between the medicine chamber and the barrel medicine chamber, so that the medicine charging safety is ensured, the leakage of gunpowder in a loose state is avoided, and the certain pulling elasticity and initial pressure of the projectile are ensured, so that the preset projectile speed is obtained, and the purposes of stable inner trajectory performance and initial speed are achieved.

(3) According to the device, groove gunpowder charging is carried out in the barrel. High-temperature and high-pressure gas generated by the impact wave before the projectile and the main charge after the projectile act on the ignition barrel groove charge in the projectile motion process, the pressure gradient formed in the space behind the projectile in high-speed motion of the projectile is reduced, high and approximately constant pressure is formed, and the projectile speed is further improved.

(4) According to the device, the design of the groove charging inside the barrel accords with the principle of adjustable energy, different grooves or pits and the charging density and the length under the charging of different grooves or pits are designed according to the specific experimental charging at each time, so that the required projectile speed is obtained.

(5) According to the device, compared with the existing projectile launching technology device which utilizes gunpowder or propellant powder as energy, the projectile launching technology device not only improves the projectile outlet speed, but also reduces the chamber pressure of the main explosive chamber.

Drawings

FIG. 1 is a schematic diagram of a direct charge of an auto-enthalpy sustained dynamic combustion propulsion unit according to the present invention;

FIG. 2 is a schematic diagram of the incremental charging of an auto enthalpy-increasing continuous dynamic combustion propulsion unit according to the present invention;

FIG. 3 is a schematic diagram of a pit charge of an auto enthalpy-increasing continuous dynamic combustion propelling device according to the present invention.

Wherein the reference numerals have the meanings: the launching mechanism 1, the pill blocking sheet 2, the barrel 3, the pill 4, the propellant powder 5 and the groove or pit charge 6.

Detailed Description

In practical application, the self-enthalpy-increasing continuous dynamic combustion propelling device carries out groove charging on the barrel inner shell. The device can process barrels of different specifications, gunpowder or propellant powder charging is carried out in the barrel of certain length as required, the length and the density of the barrel of the charging can be adjusted as required, so that the speed of the projectile reaches the expected requirement, and compared with the existing projectile launching technical device which takes the gunpowder or the propellant powder as energy, the device not only greatly improves the outlet speed of the projectile, but also reduces the bore pressure of a main medicine chamber.

The invention is further described with reference to the following figures and detailed description.

Example 1

Referring to fig. 1, firstly, a barrel 3 is selected, a straight square groove is processed in the barrel 3, groove charging 6 is carried out, and a projectile 4 is placed at one end of the barrel 3; then, propellant powder is charged in the launching mechanism 1, and the tablet blocking piece 2 is arranged between the launching mechanism 1 and the barrel 3; then, a section of combined barrel with the projectile 4 is embedded into the launching mechanism 1 through threads; then fixing the installed device; finally, detonation is carried out through the detonator.

Example 2

Referring to fig. 2, a barrel 3 is selected first, a groove with gradually increasing size is processed inside the barrel 3, groove charging 6 is carried out, and a projectile 4 is placed at one end of the barrel 3; then, propellant powder is charged in the launching mechanism 1, and the tablet blocking piece 2 is arranged between the launching mechanism 1 and the barrel 3; then, a section of combined barrel with the projectile 4 is embedded into the launching mechanism 1 through threads; then fixing the installed device; finally, detonation is carried out through the detonator.

Example 3

Referring to fig. 3, firstly, a barrel 3 is selected, pits with certain size and depth are formed in the barrel 3, the pits are distributed in a spiral manner, pit charging 6 is carried out, and a projectile 4 is placed at one end of the barrel 3; then, propellant powder is charged in the launching mechanism 1, and the tablet blocking piece 2 is arranged between the launching mechanism 1 and the barrel 3; then, a section of combined barrel with the projectile 4 is embedded into the launching mechanism 1 through threads; then fixing the installed device; finally, detonation is carried out through the detonator.

In the above embodiments, the propellant powder in the propellant mechanism 1 generates high-temperature and high-pressure gas under the action of the exploder, and the gas shears the powder blocking piece 2 along the axis direction of the barrel 3, so that the sheared wafer pushes the projectile 4 to move at high speed under the action of the high-pressure gas, and a certain pulling elasticity and initial starting pressure are ensured. In the process of high-speed movement of the projectile 4, high-temperature and high-pressure gas generated by the impact wave before the projectile and the main charge after the projectile and solid particles act to ignite the barrel groove charge 6, so that the pressure gradient formed in the space behind the projectile in high-speed movement is reduced, a higher and approximately constant pressure is formed, and the projectile speed is further improved.

The embodiments of the present invention are not limited to the above-described embodiments, but the embodiments are described in detail with reference to the accompanying drawings. Modifications, variations, improvements and the like to those skilled in the art can be made without departing from the spirit and scope of the invention.