| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 781 | 一种交流的高压电击器 | CN93213735.0 | 1993-05-27 | CN2175915Y | 1994-08-31 | 郑建贞 |
| 一种交流的高压电击器，装在电击器内的橡胶筒配备辐射载体，这种橡胶筒可随时拆卸更换，橡胶筒两旁设置液压板，液压板与扣压齿条相连，高压器件与极板电路相通，喷射嘴则与触点接触，驱动轮是与扣压齿条相啮合，它是由电机通过变速轮驱动。这种交流高压电击器作用距离远，效果显著，使用起来安全、可靠、方便。 | ||||||
| 782 | 防卫电击枪 | CN92224052.3 | 1992-06-10 | CN2126530Y | 1993-01-06 | 曾潇; 李上仁; 周游; 鲁明; 刘建荣; 王道远 |
| 一种由绝缘枪体、扳机、电池、高压发生器、带电极的子弹及枪栓组成的防卫电击枪。枪体内腔分成弹膛、枪栓膛、电池仓和高压发生器仓四部分，其子弹由“T”型弹头、弹壳、电极连线和引爆器组成，弹头前部有电极，后部有尾翼，弹头电极通过与其相连的电极连线与高压发生器输出实现电气连接。在电致引爆器推动下，子弹头连着电极连线一同射出弹膛，在击中目标同时也将高压电引向目标。本实用新型用于武警公安人员防暴自卫，具有可迅速连续实施远距电攻击的优点。 | ||||||
| 783 | 远作用距离电击枪 | CN92208371.1 | 1992-05-04 | CN2126529Y | 1993-01-06 | 刘雅萍 |
| 远作用距离电击枪，由枪体、扳机、保险机等构成。其特征在于装有良导电液体的两个贮液筒外侧下沿各有一条导轨，沿导槽装入枪体，两个工作液缸装在贮液筒下，通过绝缘墙隔离安装，工作液缸内装有工作活塞，枪体的击发液缸内装有击发活塞，枪体内还装有高压发生电路，电路产生的直流高压，通过输出导线与工作液缸的喷嘴相接，通过加压击发装置，从喷嘴射出的高压液体流与被击物形成回路，从而使人体局部肌肉受到强刺激，造成心理恐慌、动作迟缓，达到制服罪犯的目的。 | ||||||
| 784 | 水下自卫电鞭 | CN92223681.X | 1992-05-30 | CN2124449U | 1992-12-09 | 林青 |
| 一种水下自卫电鞭，在绝缘杆前端设置的两个放电电极分别与绝缘杆内的逆变升压电路的高压输出端连接，绝缘杆内有电池组、手柄上有控制开关，两放电极的间距与绝缘杆长度成一定比例关系。在水下使用该电鞭会比通常使用的水枪和潜水刀更能有效而无破坏性的制服或驱走凶猛鱼类，特别是对付鱼群的攻击时，更能避免使用水枪和潜水刀时的应接不暇、顾此失彼的危险，而使用者本身不会受到电击，是水下自卫和捕鱼的优良装备。 | ||||||
| 785 | 远程电击器 | CN90223511.7 | 1990-11-11 | CN2098665U | 1992-03-11 | 冯克伟 |
| 一种远程电击器，其外形近似塑料道具手枪，主要由两根枪管、推进活塞、射水管、贮水室、固定电极、弹簧、电池、扳机、电子脉冲高压发生器等部件构成。扣动扳机，便可使固定电极通过射水管喷射出两条中间绝缘的带有高压电脉冲的水柱，将对手制服。具有结构简单、体积小、重量轻、便于携带、作用距离远、威力特别大等优点。 | ||||||
| 786 | 远距离射击型高压电击枪 | CN90218206.4 | 1990-08-17 | CN2081521U | 1991-07-24 | 何新法 |
| 一种不需近身即能用高压液体射流束发射来电击敌手的远距防暴擒敌高压电击枪(器)。该枪(器)在常规电击枪上装有两支导电液体发射装置，并与放电点连接，扣动扳机时射出两支带高压电的射流束，可在8米范围内电击敌手以防暴自卫或公安擒敌。该枪(器)体积小，使用方便，成本低而威力强，适用于自身防卫及公安擒敌。 | ||||||
| 787 | EFFICIENT ENERGY RECOVERY METHOD AND SYSTEM BASED ON ELECTROMAGNETIC EMITTER | PCT/CN2024104364 | 2024-07-09 | WO2025077320A1 | 2025-04-17 | SUN ZHIQIANG |
| The present invention relates to the technical field of energy recovery and utilization. Disclosed is an efficient energy recovery method based on an electromagnetic emitter. The method comprises: starting an electromagnetic emitter to generate magnetic energy; collecting residual electric energy in a magnetoresistive coil by means of an electric-energy recovery module, and delivering the collected residual electric energy to an energy storage capacitor; next, using magnetic-energy collection apparatuses to collect residual magnetic energy of the electromagnetic emitter; injecting the collected residual magnetic energy into a permanent magnet, and on the basis of the magnetic field intensity, adjusting the position and movement speed of a moving armature, so as to obtain a target induced electromotive force; then conducting an energy conversion circuit to convert the target induced electromotive force into electric energy, and recovering the electric energy to the energy storage capacitor; at the same time, turning on a heat engine to collect heat energy generated by the moving armature, converting the heat energy into electric energy, and recovering the electric energy to the energy storage capacitor; finally, connecting to an energy delivery module to transmit the electric energy in the energy storage capacitor to an energy storage power source, thereby implementing efficient energy recovery for the electromagnetic emitter. By means of the present invention, energy of an electromagnetic emitter can be efficiently recovered and used. | ||||||
| 788 | RESONANCE DEVICE SUITABLE FOR MINIATURIZED MULTISTAGE ELECTROMAGNETIC GUN, AND OPERATION METHOD FOR RESONANCE DEVICE | PCT/CN2024074569 | 2024-01-30 | WO2024193234A1 | 2024-09-26 | YANG QINHAO; PAN YONGSHENG |
| Disclosed in the present invention are a resonance device suitable for a miniaturized multistage electromagnetic gun, and an operation method for the resonance device. The resonance device comprises an energy storage unit, a resonance unit, a first switch circuit, a second switch circuit, and at least one stage of acceleration circuit; the acceleration circuit comprises a first oscillation branch and a second oscillation branch; the first oscillation branches of the stages of acceleration circuits are connected in parallel and then are connected in series to the resonance unit and the first switch circuit to form a first loop; the second oscillation branches of the stages of acceleration circuits are connected in parallel and then are connected in series to the resonance unit and the second switch circuit to form a second loop; and the first loop and the second loop are connected in parallel to two ends of the energy storage unit. Such a design simplifies the structure and circuitry of the device, and provides theoretical support for miniaturization design. The first switch circuit and the second switch circuit are alternately switched on and off, so that the acceleration circuit can be ensured to be always provided with a working oscillation branch. By multiplexing the resonance unit, energy recovery is carried out during resonance, thereby improving the energy conversion efficiency. | ||||||
| 789 | SUPERCONDUCTING MAGLEV CIRCULAR MASS ACCELERATOR AND LAUNCHER | PCT/IB2023050759 | 2023-01-29 | WO2024157057A1 | 2024-08-02 | RAHMANI NEJAD AKBAR |
| The present disclosure relates to a launch system and method. A mass accelerator for launching objects, such as a payload, satellite or drone via centrifugal acceleration by a circular-path MAGLEV propulsion and levitation method. The system may comprise a chamber maintained at near vacuum pressure and cryogenic span of temperature. The projectile can be any mass such as a rocket or a hypersonic drone. The projectile is placed on a tether. The tether is accelerated on a circular-path MAGLEV rail. The tether is rotated by MAGLEV method on rails around a hub. The payload may be released from the tether upon reaching the desired launch speed and may exit the chamber through an exit port that is opened briefly to allow the payload to exit. In various embodiments, the circular mass acceleration system can be used to launch a payload into space orbit. By employing rotational acceleration via a mechanical approach, the acceleration system provides a cost -effective reusable system for launching objects. A new approach for ultra-low-cost access to space-Maglev Launch-magnetically accelerates levitated projectile to orbital speeds, 8 km/sec (Mach 23.3) or more (https://ui.adsabs.harvard.edu/abs/2010AIPC.1208..121P/abstract). Compared to the Mach 8 launching speed Spinlaunch system, this system has a much higher launch speed. Technically, this invention is based on SpinLaunch system, giving a crucial modification that implementation of Internal combustion Motor, is substituted by the superconducting magnetic levitation (Maglev) technology of which the limit of initial velocity is increased from target speed, Mach 8 to Mach 25 and theoretically much beyond, and the energy consumed by system is ameliorated. | ||||||
| 790 | A METHOD FOR DETECTING THE POSITION OF A METAL OBJECT WITHOUT AN IN-COIL SENSOR | PCT/TR2022050488 | 2022-05-26 | WO2022265600A3 | 2023-02-02 | TEMURTAŞ FEYZULLAH; DALCALI ADEM; ÇETİN ONURSAL; ÖZBAY HARUN |
| The present invention relates to a method for determining the position of an object contained in electromagnetic launchers or coil-style structures, the feature of which is; the ejected object (2), placed in the coil (1), and coil (1), drawing current from the network (power supply) (4), creating a force on the ejected object (2) as a result of the current drawn, and the ejected object (2) moves as a result of the force generated, and changes in current values drawn from the network (power supply) (4) using machine learning method (7) determining the location of the ejected object (2) involves processing steps. | ||||||
| 791 | CAPTURE DEVICE | PCT/JP2021027392 | 2021-07-21 | WO2022054425A1 | 2022-03-17 | TSUDA KUNINORI |
| The purpose of the present invention is to provide a capture device capable of capturing an object to be captured without directly contacting the object to be captured. This capture device which captures an object with a wire comprises a housing that detachably holds a cartridge, and a launcher that fires the wire with weights at both ends stored in the cartridge. The launcher fires the wire using a magnetic field generated by passing an electric current through a coil. | ||||||
| 792 | 一种基于多摄像头跟踪定位的反无人机装置及方法 | PCT/CN2018/082657 | 2018-04-11 | WO2018201868A1 | 2018-11-08 | 郭森; 任仙怡; 胡涛 |
一种基于多摄像头跟踪定位的反无人机装置及方法，该反无人机装置包括：包括：支架，其定义有圆心、环绕该圆心的圆周以及贯穿该圆心的中心轴；至少三个摄像头，这些摄像头均匀分布，并是向外倾斜地设置在该支架的圆周上，这些摄像头的中心视线形成一倒锥；定向天线，设置在该支架的中心轴上；电磁模块，与该定向天线耦合；云台，与该支架的圆心相连，用于带动该支架旋转；以及控制单元，用于根据这些摄像头提供的视频图像，控制该云台对目标进行跟踪并锁定目标，进而控制该电磁模块对目标进行攻击。本发明能够大大提高跟踪、瞄准和攻击的自动化程度。 |
||||||
| 793 | SYSTEMS AND METHODS FOR IMPROVING EFFICIENCY OF ELECTROANTIMAGNETIC LAUNCHERS | PCT/IB2018/051354 | 2018-03-02 | WO2018158746A1 | 2018-09-07 | PALMER, Miles R.; HOSIE, Cam |
The present disclosure relates launch systems, launch vehicles for use with the launch system, and methods of launching articles utilizing the launch vehicle and/or the launch system. In particular, various improvements for electroantimagnetic launch systems, vehicles, and methods are provided. |
||||||
| 794 | SPRÜHGERÄT | PCT/EP2017/084467 | 2017-12-22 | WO2018115481A1 | 2018-06-28 | THOMANN, Jürg |
Eine Vorrichtung (100) zum Verschiessen eines Projektils auf einen Zielkörper, insbesondere ein Fluidprojektil oder Feststoffprojektil, umfasst ein Handgerät (100) zum Verschiessen des Projektils, wobei das Handgerät (100) einen Antrieb (114) zum Beschleunigen des Projektils und eine Distanzmesseinrichtung (112) zum Messen einer Distanz zwischen dem Handgerät (100) und dem Zielkörper umfasst. Die Vorrichtung (100) umfasst weiter einen Energiespeicher (120) zum Betreiben des Antriebs (114), wobei der Antrieb (114) eine Steuereinheit (115) umfasst, womit der Antrieb (114) in Abhängigkeit der gemessenen Distanz steuerbar ist. |
||||||
| 795 | A METHOD OF SLOWING DOWN A MOVING PROJECTILE | PCT/GB2017/053579 | 2017-11-28 | WO2018109434A1 | 2018-06-21 | DAVIES, Raymond Charles |
A method of slowing down a projectile (12) moving within an electromagnetic railgun (14) after being fired from a gun (10) is provided. The method comprising: using an electromagnetic field generated by the railgun (14) to slow down the projectile (12), wherein the projectile (12) is a munitions projectile, and/or a carrier (30) for catching the munitions projectile (12). The method allows a "soft" recovery of the projectile (12) for testing purposes and for applying diagnostic techniques afterwards. |
||||||
| 796 | DISPOSITIF DE PROJECTION D'UN PROJECTILE PAR AIR COMPRIME PAR COMPRESSION PAR PISTON ELECTROMAGNETIQUE, PROCEDE DE PILOTAGE ASSOCIE | PCT/EP2016/078034 | 2016-11-17 | WO2017085202A1 | 2017-05-26 | LEMARQUAND, Guy |
L'objet de l'invention est un dispositif de projection d'un projectile B par air comprimé, notamment prévu pour être intégré dans une réplique d'arme, associé à une source d'énergie électrique, caractérisé en ce qu'il comprend un fourreau (10) qui reçoit à l'intérieur des moyens (12) électromagnétiques de déplacement d'un piston (34) mobile dans ledit fourreau (10) entre un nez de poussée (14), obturant l'avant (10‐1) dudit fourreau muni d'un tube de projection et une culasse (18) obturant l'arrière (10‐2) dudit fourreau. L'invention couvre également un procédé de pilotage dudit dispositif. |
||||||
| 797 | 모의 총기용 적외선 발사유닛 | PCT/KR2014/000951 | 2014-02-04 | WO2015093680A1 | 2015-06-25 | 오민석 |
본 발명은 모의 총기에 구비되어 있는 방아쇠 조작에 따른 격발음과 공기압을 동시에 감지하여 적외선이 발사되도록 함으로써 어린아이들의 전쟁놀이는 물론 서바이벌 게임 등에 활용할 수 있도록 한 모의 총기용 적외선 발사유닛에 관한 것이다. 본 발명은 스위치 조작에 따라 전원을 공급하는 배터리와, 모의 총기에 장착된 방아쇠 조작에 의한 격발음 및 총열을 따라 이동하는 공기압을 동시에 감지하여 신호를 송출하는 센서와, 이 센서의 신호를 인지하여 작동 여부를 판단하는 마이컴이 하나의 기판 상에 배치되고, 상기 기판을 수용하여 배치됨과 동시에 마이컴의 제어신호에 따라 적외선을 발사하도록 일측 선단에 접속된 다이오드를 포함하여 구성된 홀더 및 상기 기판과 홀더를 수용하기 위한 케이싱으로 이루어져 있다. |
||||||
| 798 | SYSTEMS AND METHODS FOR AREA DENIAL | PCT/US2007/080661 | 2007-10-07 | WO2008097377A2 | 2008-08-14 | WILLIAMS, Kevin E.; NACHE D. SHEKARRI; BALDWIN, Christopher W. |
Systems and methods inhibit locomotion of a human or animal target in a denial zone. Acquiring the target includes forming a prediction of at least two locations of impact on the target and testing the prediction according to criteria that may include whether the locations are within a boundary corresponding to the target and whether the locations are separated by a minimum physical and/or electrical distance. |
||||||
| 799 | LAUNCHING A FLIGHT VEHICLE | PCT/IB2007052827 | 2007-07-16 | WO2008010180A8 | 2008-04-17 | LEUSCHNER ANDRIES HERMANN |
| This invention relates to launching of a flight vehicle, such as a rocket, an aircraft and the like, from a generally upwardly directed subterranean launch shaft of at least 300 m length, preferably of a length of 500 m or more. Preferably, the launch shaft is an amortized mine shaft. Launching is by means of one of, or a combination of, several possible propulsion systems. For each system, at least some components are external of the flight vehicle and associated with or mounted in the launch shaft. One kind of propulsion system may use expansion of gas in the launch shaft behind the flight vehicle. Other propulsion systems use electromagnetism or Lorentz-type actuators, such as a coil gun or gauss gun, a linear induction motor or linear synchronous motor, or a rail gun. The launch shaft mounts guiding means for guiding the flight vehicle along the launch shaft. | ||||||
| 800 | LAUNCHING A FLIGHT VEHICLE | PCT/IB2007052827 | 2007-07-16 | WO2008010180A3 | 2008-03-06 | LEUSCHNER ANDRIES HERMANN |
| This invention relates to launching of a flight vehicle, such as a rocket, an aircraft and the like, from a generally upwardly directed subterranean launch shaft of at least 300 m length, preferably of a length of 500 m or more. Preferably, the launch shaft is an amortized mine shaft. Launching is by means of one of, or a combination of, several possible propulsion systems. For each system, at least some components are external of the flight vehicle and associated with or mounted in the launch shaft. One kind of propulsion system may use expansion of gas in the launch shaft behind the flight vehicle. Other propulsion systems use electromagnetism or Lorentz-type actuators, such as a coil gun or gauss gun, a linear induction motor or linear synchronous motor, or a rail gun. The launch shaft mounts guiding means for guiding the flight vehicle along the launch shaft. | ||||||
