WO2022041649A1 - Modular multi-stage coil gun - Google Patents

Modular multi-stage coil gun Download PDF

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Publication number
WO2022041649A1
WO2022041649A1 PCT/CN2021/074077 CN2021074077W WO2022041649A1 WO 2022041649 A1 WO2022041649 A1 WO 2022041649A1 CN 2021074077 W CN2021074077 W CN 2021074077W WO 2022041649 A1 WO2022041649 A1 WO 2022041649A1
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propulsion
coil
modular multi
coil gun
module
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PCT/CN2021/074077
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French (fr)
Chinese (zh)
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祝凌云
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祝凌云
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41BWEAPONS FOR PROJECTING MISSILES WITHOUT USE OF EXPLOSIVE OR COMBUSTIBLE PROPELLANT CHARGE; WEAPONS NOT OTHERWISE PROVIDED FOR
    • F41B6/00Electromagnetic launchers ; Plasma-actuated launchers

Definitions

  • the invention belongs to the field of electromagnetic launch, in particular to a modular multi-stage coil gun.
  • electromagnetic guns are coil guns, which are usually used for physics teaching or research.
  • the commonly used implementation method is to charge the capacitor after the battery is boosted, and then use a thyristor or a field effect transistor as an electronic switch to instantly release the electrical energy stored in the capacitor into the coil, thereby forming a strong magnetic field to attract the projectile.
  • This type of implementation mainly has the following shortcomings.
  • the use of capacitor energy storage requires a long charging process and cannot be continuously fired in a short time; it cannot precisely control the opening and closing timing of the current in the coil, resulting in insufficient acceleration or even deceleration;
  • the acceleration systems do not communicate with each other and cannot effectively make adaptive adjustments. For example, if a certain stage fails, the latter stage cannot make timing adjustments.
  • the present invention provides a modular multi-stage coil gun, which has the characteristics of high firing rate, adjustable firing rate and power, and high reliability.
  • a modular multi-stage coil gun which is mainly composed of a projectile body, a plurality of propulsion modules, a battery pack, a controller, and a temperature sensor, and each propulsion module and the controller use a bus. connect.
  • the projectile body adopts a ferromagnetic body, which can be attracted by magnetic force.
  • the material can be iron, cobalt, nickel, or an alloy containing iron, cobalt, and nickel.
  • the shape of the projectile is a revolving body in the launching direction, such as a cylinder, or a non-revolving body, such as a pie shape and a cuboid; for a non-revolving body, since the shape is not annularly symmetrical relative to the launching direction, it is more susceptible to air disturbance after launch and form a large shape. It can cover a larger area when firing continuously at high speed, and can effectively increase the hit probability at close range.
  • the propulsion module is mainly composed of a propulsion coil, a position sensor, a microprocessor, an address coding switch, and a current switch assembly; the address coding switch is used to determine the address of this module, and different modules have different addresses.
  • the address coding switch is used to determine the address of this module, and different modules have different addresses.
  • the microprocessor will turn on the electronic switch to supply power to the coil, and turn on the position sensor to the projectile.
  • the position of the coil is observed in real time, and at the position where the projectile can leave at the maximum speed (usually this position is near the middle of the coil), the electronic switch is turned off to stop the power supply to the coil, and the feedback of the execution result is sent to the bus; the shape of the propulsion coil is also A body of revolution or non-rotation in the direction of emission.
  • the position sensor is an important part of the propulsion module, which is used for real-time and high-precision observation of the position of the projectile; the sensor is composed of two sets of coils with opposite winding directions and the same number of turns in series, located between the propulsion coil and the projectile launcher. Between the space envelopes formed, they are placed in sequence along the launch direction; when the propulsion coil works, a magnetic flux will be generated. When the projectile does not enter, the magnetic flux passing through the two sensor coils is the same, because the two coils of the sensor are wound in opposite directions.
  • the electromotive force generated by the change of magnetic flux cancels each other out, and the output electromotive force is zero;
  • the change of the magnetic flux through the two sensor coils will no longer be the same, and the generated electromotive force Can not be completely offset, so the electromotive force is output, and the size and phase of the electromotive force can be detected to determine the precise position of the projectile;
  • the shape of the sensor coil is also a revolving body or a non-revolving body along the launching direction.
  • the battery pack uses cells with extremely low internal resistance. This is because the coil requires hundreds of thousands or even tens of thousands of amps of current. Generally, the internal resistance of the cells is relatively high, which will cause a large voltage drop during operation, which cannot be Sufficient current is provided; the battery pack directly supplies power to the propulsion coil, and does not use the intermediate link of capacitor energy storage, which greatly reduces the time interval caused by charging between two launches.
  • the controller is connected to multiple propulsion modules through the bus, and information exchange can be achieved with each other; the main contents transmitted in the bus are: the address of the propulsion module, work instructions, execution results, self-check information, and fault codes;
  • the controller sends work instructions to each propulsion module in turn according to a certain sequence, so as to complete the multi-stage continuous propulsion of the projectile.
  • the sequence is adjusted and optimized to improve the launch efficiency.
  • the controller After receiving the information, the controller will disable this module during the transmission process, and adjust the transmission timing adaptively to ensure that the overall system can continue to work without being affected. If the module fails during the working process, a fault code will be sent. , the controller will also make adjustments to disable the module to ensure that the system can continue to run.
  • the temperature sensor feeds the collected temperature back to the controller.
  • the controller will actively limit the firing rate and power to ensure that the temperature will not continue to rise.
  • the battery pack directly supplies power to the coil, and does not use the intermediate link of capacitor energy storage, which greatly reduces the time interval caused by charging between two launches, so that high-speed continuous transmission can be achieved.
  • the bus system can realize the interaction between the propulsion module and the controller, coordinate the control logic in real time to achieve the optimal working state, and at the same time make timely responses and adjustments to the faults that occur.
  • the sensor used in the propulsion module can detect the position of the projectile in the propulsion coil in real time; at the same time, it does not need to be in the launch pipeline like the photoelectric sensor.
  • the upper opening affects the structure of the emission pipe, which improves the overall strength and sealing performance. In addition, it is hardly affected by external factors such as light and temperature, and the reliability and stability are greatly improved.
  • the synchronous coil gun belongs to the smoothbore type launching device without internal rifling.
  • the cylindrical projectile of the traditional revolving body has the shortcomings of insufficient accuracy at long distances and insufficient dispersion at close distances.
  • the non-revolving projectile used in the invention is a pie type. Or cuboid, it is more susceptible to air disturbance after exiting the chamber, and can form a larger scattering angle, which can effectively increase the probability of a large hit at close range.
  • the modular structure cooperates with the bus system, which has stronger adaptive performance and can easily expand the number of firing stages, which paves the way for the practical and commercialization of multi-stage coil guns.
  • Figure 1 is a block diagram of the system configuration.
  • Figure 2 is a schematic diagram of the composition of the position sensor.
  • FIG. 1 is a block diagram of the system structure.
  • the battery 1 supplies power to the propulsion module 3 and the controller 2.
  • the controller 2 and the propulsion module 3 are connected through the bus 4, and the temperature sensor 5 is connected to the controller 2.
  • the controller 2 is connected to the propulsion module through the bus 4 3
  • the projectile 6 can be launched; the propulsion module 3 and the bus 4 can be expanded to achieve multi-stage continuous propulsion.
  • FIG. 2 depicts the position sensor in the propulsion module 3 .
  • the position sensor consists of a sensor coil 201 and a sensor coil 202 , which are connected in series through a connection point 203 and placed in the propulsion coil 204 .

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Plasma & Fusion (AREA)
  • General Engineering & Computer Science (AREA)
  • Charge And Discharge Circuits For Batteries Or The Like (AREA)

Abstract

A modular multi-stage coil gun, comprising: a plurality of propulsion modules (3), a projectile body (6), a battery (1), a controller (2), and a temperature sensor (5), wherein each propulsion module is connected to the controller (2) by using a bus (4); and each propulsion module comprises a propulsion coil (204), a position sensor, a microprocessor, an address coding switch, and a current switch assembly. By means of the mode, a basic firing function is realized, and the functions of firing rate adjustment, power adjustment, temperature control, and self-checking are also provided, thereby improving the system reliability, extendibility, and practicability.

Description

一种模块化多级线圈炮A modular multistage coil gun 技术领域technical field
本发明属于电磁发射领域,具体是一种模块化多级线圈炮。The invention belongs to the field of electromagnetic launch, in particular to a modular multi-stage coil gun.
背景技术Background technique
一般所说的电磁炮就是线圈炮,通常用于物理教学或研究,它的基本原理,是使用通电线圈产生的磁场,吸引铁磁性物质,产生速度并抛射出去。Generally speaking, electromagnetic guns are coil guns, which are usually used for physics teaching or research.
目前普遍采用的实现方法是将电池升压后对电容充电,再利用可控硅或场效应管作为电子开关,将储存在电容中的电能瞬间释放至线圈中,从而形成强磁场吸引弹丸。At present, the commonly used implementation method is to charge the capacitor after the battery is boosted, and then use a thyristor or a field effect transistor as an electronic switch to instantly release the electrical energy stored in the capacitor into the coil, thereby forming a strong magnetic field to attract the projectile.
这类实现方法主要存在以下缺点,使用电容储能需要较长的充电过程,无法在短时间内连续发射;不能精准控制线圈中电流的开通及关断时机,导致加速不足甚至减速;对于多级加速系统,彼此之间没有通信,不能有效的做出自适应调整,例如某级出现故障,后级不能做出时序上的调整。This type of implementation mainly has the following shortcomings. The use of capacitor energy storage requires a long charging process and cannot be continuously fired in a short time; it cannot precisely control the opening and closing timing of the current in the coil, resulting in insufficient acceleration or even deceleration; The acceleration systems do not communicate with each other and cannot effectively make adaptive adjustments. For example, if a certain stage fails, the latter stage cannot make timing adjustments.
发明内容SUMMARY OF THE INVENTION
为解决上述现有技术的不足,本发明提供了一种模块化多级线圈炮,具有射速高、射速以及功率可调、高可靠性的特点。In order to solve the above-mentioned deficiencies of the prior art, the present invention provides a modular multi-stage coil gun, which has the characteristics of high firing rate, adjustable firing rate and power, and high reliability.
为实现上述目的,所采用的具体技术方案是:一种模块化多级线圈炮,主要由弹体、多个推进模块、电池组、控制器、温度传感器组成,各推进模块和控制器使用总线连接。In order to achieve the above purpose, the specific technical scheme adopted is: a modular multi-stage coil gun, which is mainly composed of a projectile body, a plurality of propulsion modules, a battery pack, a controller, and a temperature sensor, and each propulsion module and the controller use a bus. connect.
弹体采用铁磁体,能够被磁力吸引,材质可以是铁、钴、镍,或者含有铁、钴、镍的合金。弹体形状在发射方向上是回转体,例如圆柱体,或非回转体,例如饼型、长方体;对于非回转体,由于外形相对发射方向不是环形对称,发射之后更易受到空气的扰动而形成大的发射角,高速连续发射时可以覆盖更大的面积,在近距离上能有效增加命中概率。The projectile body adopts a ferromagnetic body, which can be attracted by magnetic force. The material can be iron, cobalt, nickel, or an alloy containing iron, cobalt, and nickel. The shape of the projectile is a revolving body in the launching direction, such as a cylinder, or a non-revolving body, such as a pie shape and a cuboid; for a non-revolving body, since the shape is not annularly symmetrical relative to the launching direction, it is more susceptible to air disturbance after launch and form a large shape. It can cover a larger area when firing continuously at high speed, and can effectively increase the hit probability at close range.
推进模块主要由推进线圈、位置传感器、微处理器、地址编码开关、电流开关组件构成;其中地址编码开关用于确定本模块的地址,不同模块具有不同的地址,对于总线上的信息,如其中的地址信息与本模块的地址相同时,即作为指令予以执行,否则不做处理;当收到总线上的工作指令后,微处理器会打开电子开关对线圈供电,并开启位置传感器对弹体的位置进行实时观测,在能够使弹体以最大速度离开的位置(通常这一位置在线圈中部附近),关闭电子开关停止对线圈供电,同时向总线发出执行结果的反馈;推进线圈的形状也是沿发射方向的回转体或非回转体。The propulsion module is mainly composed of a propulsion coil, a position sensor, a microprocessor, an address coding switch, and a current switch assembly; the address coding switch is used to determine the address of this module, and different modules have different addresses. For the information on the bus, such as where When the address information of the module is the same as the address of the module, it will be executed as an instruction, otherwise it will not be processed; after receiving the work instruction on the bus, the microprocessor will turn on the electronic switch to supply power to the coil, and turn on the position sensor to the projectile. The position of the coil is observed in real time, and at the position where the projectile can leave at the maximum speed (usually this position is near the middle of the coil), the electronic switch is turned off to stop the power supply to the coil, and the feedback of the execution result is sent to the bus; the shape of the propulsion coil is also A body of revolution or non-rotation in the direction of emission.
位置传感器是推进模块中的重要组成部分,用于对弹体位置进行实时的、高精度的观 测;传感器由绕线方向相反,匝数相同的两组线圈串联构成,位于推进线圈和弹体发射形成的空间包络之间,沿发射方向依次放置;当推进线圈工作时会产生磁通量,在弹体未进入时,通过两个传感器线圈的磁通量大小相同,由于传感器的两个线圈绕线方向相反,磁通量变化产生的电动势相互抵消,输出电动势为零;当铁磁体材质的弹体进入时,由于通过两个传感器线圈有先后顺序,会导致通过两个传感器线圈磁通量变化不再相同,所产生电动势不能完全抵消,从而输出电动势,对电动势的大小和相位进行检测即可以判断出弹体的精确位置;传感器线圈的形状也是沿发射方向的回转体或非回转体。The position sensor is an important part of the propulsion module, which is used for real-time and high-precision observation of the position of the projectile; the sensor is composed of two sets of coils with opposite winding directions and the same number of turns in series, located between the propulsion coil and the projectile launcher. Between the space envelopes formed, they are placed in sequence along the launch direction; when the propulsion coil works, a magnetic flux will be generated. When the projectile does not enter, the magnetic flux passing through the two sensor coils is the same, because the two coils of the sensor are wound in opposite directions. , the electromotive force generated by the change of magnetic flux cancels each other out, and the output electromotive force is zero; when the projectile made of ferromagnetic material enters, due to the sequence of passing through the two sensor coils, the change of the magnetic flux through the two sensor coils will no longer be the same, and the generated electromotive force Can not be completely offset, so the electromotive force is output, and the size and phase of the electromotive force can be detected to determine the precise position of the projectile; the shape of the sensor coil is also a revolving body or a non-revolving body along the launching direction.
电池组采用极低内阻的电芯,这是因为线圈工作时需要数百数千甚至上万安培的电流,一般电芯的内阻相对较高,工作时会造成很大的压降,无法提供足够的电流;电池组直接对推进线圈供电,不采用电容储能这一中间环节,极大减少了两次发射之间因充电导致的时间间隔。The battery pack uses cells with extremely low internal resistance. This is because the coil requires hundreds of thousands or even tens of thousands of amps of current. Generally, the internal resistance of the cells is relatively high, which will cause a large voltage drop during operation, which cannot be Sufficient current is provided; the battery pack directly supplies power to the propulsion coil, and does not use the intermediate link of capacitor energy storage, which greatly reduces the time interval caused by charging between two launches.
控制器通过总线和多个推进模块连接,相互间可以实现信息交互;总线中所传输的主要内容有:推进模块地址、工作指令、执行结果、自检信息、故障码;对于单颗弹体的发射,控制器根据一定的先后时序,依次对各个推进模块发出工作指令,就能完成对弹体的多级连续推进,同时根据推进模块反馈的执行结果,对时序做调整和优化,提升发射效率;不断重复这一指令序列即可实现多枚连续发射,改变这一重复过程的频率即可调整射速;控制器如果改变参与工作的推进模块数量以及时序,即可该变弹体的动能,实现发射功率的调整;降低发射功率就意味着部分模块在单次发射过程中不工作,对此,在多枚连续发射的过程中,按照每个模块的工作次数都相同或接近的原则,让它们相互交替工作,从而实现发热量的均衡,可以提高稳定性和延长使用寿命;系统开机时,推进模块会做一次自检,并将自检信息发送至总线,如果某个推进模块自检不能通过,控制器在收到信息后,在发射过程中将禁用此模块,并自适应调整发射时序,保证整体系统能够不受影响继续工作,如果在工作过程中模块出现故障,便会发送故障码,控制器也会做出禁用模块的调整,保证系统能够继续运行。The controller is connected to multiple propulsion modules through the bus, and information exchange can be achieved with each other; the main contents transmitted in the bus are: the address of the propulsion module, work instructions, execution results, self-check information, and fault codes; When launching, the controller sends work instructions to each propulsion module in turn according to a certain sequence, so as to complete the multi-stage continuous propulsion of the projectile. At the same time, according to the execution results fed back by the propulsion module, the sequence is adjusted and optimized to improve the launch efficiency. ; Repeating this sequence of instructions continuously can achieve multiple continuous launches, and changing the frequency of this repeating process can adjust the rate of fire; if the controller changes the number and timing of the propulsion modules involved in the work, the kinetic energy of the projectile can be changed, Realize the adjustment of transmission power; reducing the transmission power means that some modules do not work during a single transmission. For this, in the process of multiple continuous transmissions, according to the principle that the number of operations of each module is the same or close, let They work alternately to achieve a balance of heat generation, which can improve stability and prolong service life; when the system is turned on, the propulsion module will perform a self-check and send the self-check information to the bus. After receiving the information, the controller will disable this module during the transmission process, and adjust the transmission timing adaptively to ensure that the overall system can continue to work without being affected. If the module fails during the working process, a fault code will be sent. , the controller will also make adjustments to disable the module to ensure that the system can continue to run.
温度传感器将采集到的温度反馈给控制器,当温度过高可能会影响系统正常工作时,控制器会主动限制射速和发射功率,保证温度不再继续升高。The temperature sensor feeds the collected temperature back to the controller. When the temperature is too high, which may affect the normal operation of the system, the controller will actively limit the firing rate and power to ensure that the temperature will not continue to rise.
本发明的有益效果是:The beneficial effects of the present invention are:
一、电池组直接对线圈供电,不采用电容储能这一中间环节,极大减少了两次发射之间因充电导致的时间间隔,从而可以实现高速连续发射。1. The battery pack directly supplies power to the coil, and does not use the intermediate link of capacitor energy storage, which greatly reduces the time interval caused by charging between two launches, so that high-speed continuous transmission can be achieved.
二、总线式系统,可以实现推进模块和控制器之间的交互,实时协调控制逻辑以达到最优工作状态,同时对出现的故障做出及时应对和调整。2. The bus system can realize the interaction between the propulsion module and the controller, coordinate the control logic in real time to achieve the optimal working state, and at the same time make timely responses and adjustments to the faults that occur.
三、相对传统的光电位置传感器只能检测到一个位置而言,推进模块中所采用的传感器能够实时检测到弹体在推进线圈中的位置;同时,它不需要像光电传感器那样,在发射管道上开孔而影响发射管道的结构,提高了整体的的强度和密封性能,另外几乎不会受光线、温度等外界因素的影响,可靠性稳定性大大提高。3. Compared with the traditional photoelectric position sensor that can only detect one position, the sensor used in the propulsion module can detect the position of the projectile in the propulsion coil in real time; at the same time, it does not need to be in the launch pipeline like the photoelectric sensor. The upper opening affects the structure of the emission pipe, which improves the overall strength and sealing performance. In addition, it is hardly affected by external factors such as light and temperature, and the reliability and stability are greatly improved.
四、同步线圈炮属于滑膛型发射装置,没有内部膛线,传统回转体外形的圆柱弹体,有远距离不够准、近距离不够散的缺点,发明中采用的非回转体弹体,为饼型或长方体,出膛后更易受空气扰动,能形成较大的散射角,在近距离上能有效增加大命中概率。4. The synchronous coil gun belongs to the smoothbore type launching device without internal rifling. The cylindrical projectile of the traditional revolving body has the shortcomings of insufficient accuracy at long distances and insufficient dispersion at close distances. The non-revolving projectile used in the invention is a pie type. Or cuboid, it is more susceptible to air disturbance after exiting the chamber, and can form a larger scattering angle, which can effectively increase the probability of a large hit at close range.
五、模块化的架构配合总线式系统,具有更强的自适应性能,可方便的扩展发射级数,为多级线圈炮走向实用化和产品化铺平了道路。5. The modular structure cooperates with the bus system, which has stronger adaptive performance and can easily expand the number of firing stages, which paves the way for the practical and commercialization of multi-stage coil guns.
附图说明Description of drawings
图1是系统构成框图。Figure 1 is a block diagram of the system configuration.
图2是位置传感器组成示意图。Figure 2 is a schematic diagram of the composition of the position sensor.
图中:1、电池;2、控制器;3、推进模块;4、总线;5、温度传感器;6、弹体;201、传感器线圈1;202、传感器线圈2;203、连接点;204、推进线圈。In the figure: 1, battery; 2, controller; 3, propulsion module; 4, bus; 5, temperature sensor; 6, projectile; 201, sensor coil 1; 202, sensor coil 2; 203, connection point; 204, Advance the coil.
具体实施方式detailed description
下面结合附图对本发明进行阐述。The present invention will be described below with reference to the accompanying drawings.
图1是系统构成框图,电池1对推进模块3和控制器2供电,控制器2和推进模块3通过总线4连接,温度传感器5与控制器2连接,当控制器2通过总线4对推进模块3发送发射指令时,弹体6就能够被发射;推进模块3和总线4可以扩展,实现多级连续推进。Figure 1 is a block diagram of the system structure. The battery 1 supplies power to the propulsion module 3 and the controller 2. The controller 2 and the propulsion module 3 are connected through the bus 4, and the temperature sensor 5 is connected to the controller 2. When the controller 2 is connected to the propulsion module through the bus 4 3 When the launch command is sent, the projectile 6 can be launched; the propulsion module 3 and the bus 4 can be expanded to achieve multi-stage continuous propulsion.
图2描述了推进模块3当中的位置传感器,位置传感器由传感器线圈201和传感器线圈202组成,它们通过连接点203串联后,放置于推进线圈204之中。FIG. 2 depicts the position sensor in the propulsion module 3 . The position sensor consists of a sensor coil 201 and a sensor coil 202 , which are connected in series through a connection point 203 and placed in the propulsion coil 204 .

Claims (10)

  1. 一种线圈炮推进模块,其特征在于:包括推进线圈、位置传感器、微处理器、地址编码开关、电流开关组件;微处理器可控制电流开关组件对线圈进行电流的开通与关断操作,可根据位置传感器实时判断所发射弹体在线圈中的位置,可读取地址编码开关所设置的模块识别地址。A coil gun propulsion module is characterized in that: it includes a propulsion coil, a position sensor, a microprocessor, an address coding switch, and a current switch assembly; the microprocessor can control the current switch assembly to perform current on and off operations on the coil, and can The position of the projectile body in the coil can be judged in real time according to the position sensor, and the module identification address set by the address coding switch can be read.
  2. 根据权利要求1所述的一种线圈炮推进模块,其特征在于:位置传感器由两组线圈组成,位于推进线圈内侧,沿推进线圈轴向依次放置,两组线圈缠绕方向相反,串行连接。A coil gun propulsion module according to claim 1, characterized in that: the position sensor is composed of two sets of coils, located inside the propulsion coils, placed in sequence along the axial direction of the propulsion coils, and the two sets of coils are wound in opposite directions and are connected in series.
  3. 根据权利要求1所述的一种线圈炮推进模块,其特征在于:推进线圈和位置传感器的形状是沿发射方向的回转体或非回转体。A coil gun propulsion module according to claim 1, wherein the shape of the propulsion coil and the position sensor is a revolving body or a non-revolving body along the launching direction.
  4. 一种模块化多级线圈炮,其特征在于:包括多个如权利要求1所述的推进模块、弹体、电池、控制器、温度传感器,各推进模块和控制器使用总线连接。A modular multi-stage coil gun is characterized by comprising a plurality of propulsion modules, projectiles, batteries, controllers, and temperature sensors as claimed in claim 1, and each propulsion module and the controller are connected using a bus.
  5. 根据权利要求4所述的一种模块化多级线圈炮,其特征在于:推进模块中的推进线圈直接使用电池供电。A modular multi-stage coil gun according to claim 4, wherein the propulsion coil in the propulsion module is directly powered by a battery.
  6. 根据权利要求4所述的一种模块化多级线圈炮,其特征在于:总线所传输的内容包括推进模块的地址、电流开通指令、电流关断反馈、自检信息、故障码。A modular multi-stage coil gun according to claim 4, characterized in that: the content transmitted by the bus includes the address of the propulsion module, the current turn-on command, the current turn-off feedback, the self-check information, and the fault code.
  7. 根据权利要求4所述的一种模块化多级线圈炮,其特征在于:控制器通过改变电流开通指令序列的频率来调整射速,通过改变开通指令对应推进模块地址数量来调整发射功率。A modular multi-stage coil gun according to claim 4, wherein the controller adjusts the firing rate by changing the frequency of the current turn-on command sequence, and adjusts the firing power by changing the number of addresses of the propulsion modules corresponding to the turn-on command.
  8. 根据权利要求4所述的一种模块化多级线圈炮,其特征在于:控制器通过温度传感器获取温度,过热时降低射速和发射功率,并交替使用不同的推进模块避免温升过高。A modular multi-stage coil gun according to claim 4, characterized in that: the controller obtains the temperature through a temperature sensor, reduces the rate of fire and the launch power when overheating, and alternately uses different propulsion modules to avoid excessive temperature rise.
  9. 根据权利要求4所述的一种模块化多级线圈炮,其特征在于:弹体为铁磁体,材质是铁、钴、镍中的一种。A modular multi-stage coil gun according to claim 4, wherein the projectile body is a ferromagnetic body, and the material is one of iron, cobalt and nickel.
  10. 根据权利要求4所述的一种模块化多级线圈炮,其特征在于:弹体形状在发射方向上是回转体或非回转体,是圆柱体、长方体中的一种。A modular multi-stage coil gun according to claim 4, characterized in that: the shape of the projectile body is a revolving body or a non-revolving body in the firing direction, and is one of a cylinder and a rectangular parallelepiped.
PCT/CN2021/074077 2020-08-25 2021-01-28 Modular multi-stage coil gun WO2022041649A1 (en)

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US5158291A (en) * 1992-01-21 1992-10-27 William Electronics Games, Inc. Ball accelerator for rolling ball games
CN202109817U (en) * 2011-06-14 2012-01-11 胡生云 Rail type coil gun
CN105990984A (en) * 2015-03-05 2016-10-05 陈启星 Radial magnetic cylinder rotor-based linear motor
US20200025507A1 (en) * 2016-05-25 2020-01-23 Honeywell Federal Manufacturing & Technologies, Llc Electromagnetic launcher with spiral guideway
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