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公开(公告)号：WO1997012194A1
公开(公告)日：1997-04-03
申请号：PCT/GB1996002406
申请日：1996-09-30
Inventor： BROWN, Keith, Edwin, Frank
IPC: F41B06/00
Abstract: A fluid projectile launcher (10) comprises a barrel having an open end and a closed end defining a breech portion (50). The breech portion (50) is arranged to hold a dosage of fluid (56) in the form of an ionizing medium for rendering the fluid electrically conductive and an active substance which induces a physiological reaction in living organisms. The projectile launcher (10) includes a launching initiation circuit in the form of a capacitor (22) and an inductance (36), and a pair of electrodes (38A, 38B) forming part of the breech portion (50). Trigger means (40) are provided for allowing the energy storage means (22) to discharge into the dosage of fluid (56) in the breech portion (50) via the electrodes (52, 38A, 38B) so as to cause the dosage of fluid (56) to be projected from the open end of the barrel as a fluid projectile. The leads (38A, 38B) connecting the capacitor (22) and inductance (36) are arranged in a radially symmetrical pattern about a tubular first electrode so as to create an electromagnetic field which is functionally symmetrical in the plane normal to the central axis of the barrel. The launcher may be in the form of a portable hand held device.
Abstract translation: 流体抛射发射器（10）包括具有开口端的筒体和限定臀部部分（50）的封闭端。 后膛部分（50）被布置成保持电离介质形式的流体（56）的剂量，以使流体导电，以及在活生物体中诱导生理反应的活性物质。 射弹发射器（10）包括形成电容器（22）和电感（36）形式的发射启动电路和形成后膛部分（50）的一部分的一对电极（38A，38B）。 提供触发装置（40），用于允许能量存储装置（22）经由电极（52,38A，38B）排放到后膛部分（50）中的流体（56）的剂量中，以使剂量 流体（56）作为流体抛射体从筒的开口端突出。 连接电容器（22）和电感（36）的引线（38A，38B）围绕管状第一电极以径向对称的方式布置，以便产生在垂直于中心轴的平面中的功能上对称的电磁场 桶。 发射器可以是便携式手持装置的形式。
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公开(公告)号：WO1993007436A1
公开(公告)日：1993-04-15
申请号：PCT/US1992007446
申请日：1992-09-04
Applicant: OLIN CORPORATION
Inventor： OLIN CORPORATION , MCELROY, Hugh, A.
IPC: F41B06/00
CPC classification number: F41B6/00 , Y10S102/70
Abstract: An electrothermal chemical propulsion apparatus (10) comprises a projectile (12), at least one chemical propellant module (20), an extensible energy coupling device (22) therebetween, and an electrical power supply (24) electrically connected to the device so as to vaporize the device creating a plasma augmenting the gas expansion behind the accelerating projectile at a predetermined time after ignition of the chemical propellant. The method of propelling a projectile includes the steps of providing an extensible conductor (22) between a power supply and the rear of the projectile (12), igniting the propelling charge to generate a gas pressure in the chamber (16), extending the conductor behind the projectile (12), and passing an electrical current pulse through the conductor (22) when the conductor is fully extended.
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公开(公告)号：WO2016182327A1
公开(公告)日：2016-11-17
申请号：PCT/KR2016/004907
申请日：2016-05-11
Applicant: 이영택 , (주)크리티컬퍼실리티서비스
Inventor： 이영택
Abstract: 본 발명은 발사장치에 관한 것으로서, 특히 안전하면서도 저전력으로 구동이 가능하도록 내부가 비고 비자성체 소재로 이루어진 관이 나선형으로 감겨진 가속관과, 상기 가속관의 외측을 둘러싸도록 복수 개의 코일이 감겨져 전류 인가시 자화되어 자기장을 형성하는 고정자와, 상기 자기장에 의해 힘을 받아 가속관을 따라 회전하며 외부로 발사되는 자성체를 포함하는 것을 특징으로 하는 회전 자성체를 이용한 발사장치에 관한 것이다.
Abstract translation: 本发明涉及一种发射装置，特别涉及一种发射装置，包括：加速管，其中由非磁性材料制成的中空管螺旋缠绕以便能够以低功耗安全驾驶; 定子，其包括围绕所述加速管的外部的多个缠绕线圈，以便当施加电流时通过被磁化而形成磁场; 以及由于由磁场施加的力而沿加速管旋转而向外部发射的磁体。
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公开(公告)号：WO2014056335A1
公开(公告)日：2014-04-17
申请号：PCT/CN2013/078961
申请日：2013-07-07
Applicant: 广州微点焊设备有限公司 , 杨诚
CPC classification number: B60L13/10 , B23K11/31 , B23K11/36 , B60K31/00 , B60T7/22 , B60T13/748 , F16D49/00 , F16D63/002 , F16D2121/20 , F41B6/00 , H02K33/00 , H02K41/00
Abstract: 本发明公开了一种悬浮电磁力动力装置，其包括：一体化电磁铁结构，包括安装框架、可相对于安装框架往返运动且延伸出安装框架的动力引出轴，以及相对设置的二个电磁铁，二个电磁铁中的一个电磁铁组接在安装框架的一侧形成固定电磁铁，另一个电磁铁与动力引出轴紧固形成活动电磁铁，活动电磁铁通过动力引出轴安装在安装框架的另一侧并可相对于固定电磁铁往返运动；辅助动力结构，驱动活动电磁铁相对于固定电磁铁作往返运动；以及电源控制结构，为一体化电磁铁结构和/或辅助动力结构提供电源。本发明悬浮电磁力动力装置不仅结构筒单、操作方便、响应迅速、安全耐用，而且无噪音、无污染、环保节能，是一种全新的动力装置。
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公开(公告)号：WO2008010180A2
公开(公告)日：2008-01-24
申请号：PCT/IB2007/052827
申请日：2007-07-16
Inventor： LEUSCHNER, Andries, Hermann
Abstract: 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.
Abstract translation: 本发明涉及从长度至少为300米，优选长度为500米或更大的一般向上定向的地下发射轴发射飞行器，例如火箭，飞行器等。 优选地，发射轴是分期的矿井。 通过几种可能的推进系统中的一种或其组合来发射。 对于每个系统，至少一些组件在飞行器车辆的外部并且与发射轴相关联或安装在发射轴中。 一种推进系统可以在飞行器后面的发射井中使用气体的扩张。 其他推进系统使用电磁或洛伦兹式致动器，例如线圈枪或高斯枪，线性感应电动机或线性同步电动机或轨道枪。 发射轴安装用于沿着发射轴引导飞行器的引导装置。
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Patent Agency Ranking
公开(公告)号：WO2014187195A1
公开(公告)日：2014-11-27
申请号：PCT/CN2014/074497
申请日：2014-03-31
Applicant: 广州微点焊设备有限公司 , 杨诚
CPC classification number: B23K11/31 , B60L1/20 , B60L7/24 , B60L2270/145 , F41A19/00 , F41B6/00 , H01F7/066 , H01F2007/1692
Abstract: 一种悬浮电磁力动力装置，其包括：一体化电磁铁结构（100），其包括二个电磁铁（102）、动力引出轴（101）和安装框架（103），其中，二个电磁铁相向设置并分别与动力引出轴和安装框架组接成活动电磁铁和固定电磁铁，活动电磁铁可相对于固定电磁铁作往返运动；辅助动力结构（110），与动力引出轴连接，可驱动活动电磁铁相对于固定电磁铁作往返运动；以及电源控制结构（120），为一体化电磁铁结构和/或辅助动力结构提供电源。悬浮电磁力具有能直接以电讯号控制和响应极其迅速这二个其它动力不具备或无法与之相比的特点，悬浮电磁力动力装置具有结构简单、操作方便、安全耐用，无噪音、无污染、环保节能等优点。
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公开(公告)号：WO2007011398A3
公开(公告)日：2007-05-10
申请号：PCT/US2005037591
申请日：2005-10-21
Applicant: DEKA PRODUCTS LP , LANIGAN RICHARD J , KAMEN DEAN , GRAY LARRY B
Inventor： LANIGAN RICHARD J , KAMEN DEAN , GRAY LARRY B
CPC classification number: F41B11/00 , A63G31/08 , A63J3/00 , F41B6/00 , F41B7/00 , F41B15/00 , F41F7/00
Abstract: A controllable launcher for propelling a payload through a predictable and repeatable trajectory to a desired height. The launcher has an energy source for propelling a carriage and a piston in substantially opposing directions and a controller for controlling the trajectory of the propelled payload to enable the payload to land gently at a safe impact distance from the edge of a destination structure.
Abstract translation: 一种可控的发射器，用于通过可预测和可重复的轨迹将有效载荷推进到所需的高度。 发射器具有用于在基本上相反的方向上推动滑架和活塞的能源，以及用于控制推进式有效载荷的轨迹的控制器，以使有效载荷能够以距离目的地结构的边缘安全的撞击距离轻轻着陆。
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公开(公告)号：WO2003071218A1
公开(公告)日：2003-08-28
申请号：PCT/ZA2003/000027
申请日：2003-02-20
Applicant: DENEL (PTY) LTD , BREYTENBACH, Frederik, Gert, Johannes , MÜLLER, Ernst, Johann, Heinrich
IPC: F41B6/00
Abstract: This invention relates to a breech assembly (10) of a gun adapted to fire caseless charges, ignited and enhanced with electrothermal chemical (ETC) charges. The gun utilises charges as propellant and a plasma generator cartridge (PGC) (17) for generating plasma when an electrical current is applied thereto. The breech assembly (10) comprises a breech ring (13), a tilting block assembly (14), with a spindle (15) installed and a sliding block (16) for supporting or locking the tilting block assembly (14) in a sealed position. The tilting block assembly (14) is movable between a PGC firing orientation and a PGC loading/removal orientation. The breech assembly (10) further includes a crank means, which includes a guide means (26) for rotating the tilting block assembly (14) from the PGC firing orientation to the PGC loading/removal orientation.
Abstract translation: 本发明涉及一种枪的后枪组件（10），其适于用电热化学（ETC）充电来点燃和增强无烟电荷。 当施加电流时，枪利用作为推进剂和等离子体发生器盒（PGC）（17）的电荷来产生等离子体。 后膛组件（10）包括后膛环（13），安装有心轴（15）的倾斜块组件（14）和用于将倾斜块组件（14）支撑或锁定在密封件中的滑动块（16） 位置。 倾斜块组件（14）可以在PGC燃烧方向和PGC加载/移除取向之间移动。 后膛组件（10）还包括曲柄装置，该曲柄装置包括用于使倾斜块组件（14）从PGC燃烧方向旋转到PGC装载/移除取向的引导装置（26）。
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公开(公告)号：WO1990005278A1
公开(公告)日：1990-05-17
申请号：PCT/EP1989000516
申请日：1989-05-11
Applicant: IGENWERT GMBH , IGENBERGS, Eduard , ROTT, Martin
Inventor： IGENWERT GMBH
IPC: F41B06/00
Abstract: Electrothermal accelerator, preferably two-stage. The first stage is an electrothermal accelerator, in particular an electrothermal accelerator with electromagnetic amplification, and the second stage is a light-gas accelerator.
Abstract translation: 电热加速器，最好是两级。 第一阶段是电热加速器，特别是具有电磁放大的电热加速器，第二阶段是光气加速器。
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10.发明申请LAUNCH VEHICLE AND SYSTEM AND METHOD FOR ECONOMICALLY EFFICIENT LAUNCH THEREOF 审中-公开发射车辆及其经济有效发射的系统及方法
公开(公告)号：WO2014152778A1
公开(公告)日：2014-09-25
申请号：PCT/US2014/027721
申请日：2014-03-14
Applicant: PALMER LABS, LLC , 8 RIVERS CAPITAL, LLC
Inventor： PALMER, Miles R. , BROWN, JR., Glenn William
CPC classification number: B64G1/409 , B64G1/002 , B64G1/402 , B64G1/406 , F02K9/95 , F41A1/04 , F41B6/00 , F41B6/006 , F41F1/00 , F41F3/04 , F41F3/0406 , F42B6/006 , F42B15/10 , F42B15/12 , F42C11/00 , F42C11/04
Abstract: The present disclosure relates to a launch system (20), a launch vehicle (200) for use with the launch system (20), and methods of launching a payload utilizing the launch vehicle (200) and/or the launch system. The disclosure can provide for delivery of the payload at a terrestrial location, an Earth orbital location, or an extraorbital location. The launch vehicle (200) can comprise a payload (240), a propellant tank (230), an electrical heater (220) wherein propellant, such as a light gas (e.g., hydrogen) is electrically heated, and an exhaust nozzle (210) from which the heated propellant expands to provide an exhaust velocity of, for example, 7-16 km/sec. The launch vehicle can be utilized with the launch system, which can further comprise a launch tube (100) formed of at least one tube (110, 130), which can be electrically conductive and which can be combined with at least one insulator tube (120). An electrical energy source (300) also can be provided.
Abstract translation: 本公开涉及一种与发射系统（20）一起使用的发射系统（20），运载火箭（200）以及使用运载火箭（200）和/或发射系统发射有效载荷的方法。 本公开可以提供在地面位置，地球轨道位置或眶外位置处的有效载荷的传送。 运载火箭（200）可以包括有效载荷（240），推进剂罐（230），电加热器（220），其中推进剂，例如轻气体（例如氢）被电加热，以及排气喷嘴 ），其中加热的推进剂从其膨胀以提供例如7-16km / sec的排气速度。 运载火箭可以与发射系统一起使用，该发射系统还可以包括由至少一个管（110,130）形成的发射管（100），其可以是导电的并且可以与至少一个绝缘管（ 120）。 也可以提供电能源（300）。
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