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公开(公告)号：US20230280122A1
公开(公告)日：2023-09-07
申请号：US18110212
申请日：2023-02-15
申请人： RUAG Ammotec GmbH
发明人： Henning Rost , Andreas Winter
IPC分类号： F41A19/60
摘要： The present invention relates to a method for providing a predetermined pyrotechnic energy output to a pyrotechnic separating device for separating an electrical line, such as a cable, a wire, a conductor path or the like, leading to an electrical energy source, such as a battery or an accumulator, for outputting and/or receiving electrical energy, in which: a temperature of or in the vicinity of the electrical energy source is detected; and, when the detected temperature exceeds a predetermined temperature threshold, the pyrotechnic separating device is remotely activated to separate the electrical line at a location spatially remote from the electrical energy source.
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公开(公告)号：US07338288B1
公开(公告)日：2008-03-04
申请号：US11647184
申请日：2006-12-29
申请人： Shih-Che Kung , Wei-Hung Chung
发明人： Shih-Che Kung , Wei-Hung Chung
IPC分类号： H01R39/00
摘要： The present invention provides an improved battery connecting structure, structured from a frontal disposed portion, an abutting joint portion and a joining portion. A movement device is configured interior of the frontal disposed portion, and conducting wires extend therefrom and connect to connecting holes corresponding to conductive contact tags of the joining portion, and turning shafts are located on the frontal disposed portion corresponding to the conductive contact tags of the connecting holes. Conducting wires further extend from connecting holes of the joining portion and connect to a power supply member. Accordingly, when a rotating movement is performed on the frontal disposed portion and the joining portion by means of the turning shafts, then the conductive contact tags of the abutting joint portion serve to realize an electric circuit, thererby achieving objectives of preventing exposing and damaging the conducting wires, and providing convenience of use and portability.
摘要翻译： 本发明提供一种由前部设置部分构成的改进的电池连接结构，抵接接合部分和接合部分。 运动装置配置在正面设置部分的内部，并且导线从其延伸并连接到对应于接合部分的导电接触标签的连接孔，并且转轴位于对应于 连接孔。 导电线从连接部的连接孔进一步延伸，并与电源部件连接。 因此，当通过转动轴在前置设置部分和接合部分上进行旋转运动时，抵靠接合部分的导电接触标签用于实现电路，从而实现防止暴露和损坏的目的 导线，并提供使用和便携性的便利。
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公开(公告)号：US11674769B2
公开(公告)日：2023-06-13
申请号：US17957805
申请日：2022-09-30
申请人： T. Dashon Howard , Chris Seely
发明人： T. Dashon Howard , Chris Seely
摘要： A projectile propulsion system comprises a housing defining a chamber, a propulsive charge including a propulsive charge material loadable into the chamber, a projectile loadable into the chamber proximate to the propulsive charge material, an electric pulse discharge subsystem that provides an electric pulse having a specified pulse amperage for a specified pulse period, a current delivery subsystem electrically connecting the electric pulse discharge subsystem to the chamber to deliver the electric pulse to the propulsive charge material, wherein the specified pulse amperage and the specified pulse period are sufficient to cause at least a portion of the propulsive charge material to generate a propulsive force that is at least partially directed onto the projectile to drive the projectile out of the chamber, and a barrel in fluid communication with the chamber configured to receive the projectile as it is driven from the chamber.
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公开(公告)号：US09551547B2
公开(公告)日：2017-01-24
申请号：US14368925
申请日：2012-12-17
发明人： Denny Aberg
摘要： The invention relates to a method for the repeatable initiation of propellent charges in a weapon system, for example in the firing of projectiles from a barrel weapon, through electrical discharge between a rear electrode (22) and a front electrode (21) in a combustion chamber channel (3) filled with filler gas and comprising a combustion chamber combustion element (30), in which the filler gas in the combustion chamber channel (3) is ionized via a high-voltage potential from at least one ionizing electrode (100, 101, 102, 103), which ionization increases the electrical conductivity in the combustion chamber channel (3) so that an electrical flashover, through electrical discharge via a high-voltage generator (5) between the rear electrode (22) and the front electrode (21), is generated from the rear electrode (22) via at least one ionizing electrode (100, 101, 102, 103) onward to the front electrode (21), which results in hot ignition gas with plasma-like state being expelled from the combustion chamber channel (3). The invention also relates to a plasma generator for the said method, and to an ammunition unit comprising the said plasma generator.
摘要翻译： 本发明涉及一种用于在武器系统中可重复启动推进剂装料的方法，例如在从枪管武器射出的射弹中，通过燃烧中的后电极（22）和前电极（21）之间的放电 填充有填充气体并包括燃烧室燃烧元件（30）的室通道（3），其中燃烧室通道（3）中的填充气体通过来自至少一个电离电极（100）的高电压电离， 101,102,103），其电离增加了燃烧室通道（3）中的导电性，使得通过经由后电极（22）和前电极（22）之间的高压发生器（5）的放电而电气闪络 （21）经由至少一个离子电极（100,101,102,103）从前电极（21）从后电极（22）产生，导致具有等离子体状态的热点燃气体被排出 从th 燃烧室通道（3）。 本发明还涉及用于所述方法的等离子体发生器以及包括所述等离子体发生器的弹药单元。
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公开(公告)号：US3786717A
公开(公告)日：1974-01-22
申请号：US3786717D
申请日：1972-08-29
申请人： US ARMY
CPC分类号： F41A19/60
摘要： Electrical firing mechanism for a light weight, portable, rocket launcher. The mechanism includes means for actuating a battery for supplying an electrical pulse to the rocket carried in the launcher for ignition of the rocket motor.
摘要翻译： 电动发射机构，重量轻，便携式，火箭发射器。 该机构包括用于致动用于向发射器中携带的用于点燃火箭发动机的火箭提供电脉冲的电池的装置。
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公开(公告)号：US12007187B1
公开(公告)日：2024-06-11
申请号：US17813431
申请日：2022-07-19
摘要： The present disclosure provides systems and techniques for monitoring the transfer of electric charge and determining whether a threshold amount of electric charge has been transferred. Aspects of the present disclosure may be performed by a fire control system, and the fire control system may be implemented in a gun. The fire control system may generate an integrated voltage using an integrator to integrate a current induced voltage that is present across a resistor, compare the integrated voltage against a reference voltage to determine whether the integrated voltage exceeds the reference voltage, and generate an output voltage that indicates whether the integrated voltage exceeds the reference voltage. The output voltage may be generated based on comparing the integrated voltage against the reference voltage using a comparator circuit, and the reference voltage may correspond to a threshold amount of electric charge.
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公开(公告)号：US20140352564A1
公开(公告)日：2014-12-04
申请号：US14368925
申请日：2012-12-17
发明人： Denny Åberg
摘要： The invention relates to a method for the repeatable initiation of propellent charges in a weapon system, for example in the firing of projectiles from a barrel weapon, through electrical discharge between a rear electrode (22) and a front electrode (21) in a combustion chamber channel (3) filled with filler gas and comprising a combustion chamber combustion element (30), in which the filler gas in the combustion chamber channel (3) is ionized via a high-voltage potential from at least one ionizing electrode (100, 101, 102, 103), which ionization increases the electrical conductivity in the combustion chamber channel (3) so that an electrical flashover, through electrical discharge via a high-voltage generator (5) between the rear electrode (22) and the front electrode (21), is generated from the rear electrode (22) via at least one ionizing electrode (100, 101, 102, 103) onward to the front electrode (21), which results in hot ignition gas with plasma-like state being expelled from the combustion chamber channel (3). The invention also relates to a plasma generator for the said method, and to an ammunition unit comprising the said plasma generator.
摘要翻译： 本发明涉及一种用于在武器系统中可重复启动推进剂装料的方法，例如在从枪管武器射出的射弹中，通过燃烧中的后电极（22）和前电极（21）之间的放电 填充有填充气体并包括燃烧室燃烧元件（30）的室通道（3），其中燃烧室通道（3）中的填充气体通过来自至少一个电离电极（100）的高电压电离， 101,102,103），其电离增加了燃烧室通道（3）中的导电性，使得通过经由后电极（22）和前电极（22）之间的高压发生器（5）的放电而产生电闪络 （21）经由至少一个离子电极（100,101,102,103）从前电极（21）从后电极（22）产生，导致具有等离子体状态的热点燃气体被排出 从th 燃烧室通道（3）。 本发明还涉及用于所述方法的等离子体发生器以及包括所述等离子体发生器的弹药单元。
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公开(公告)号：US08707602B1
公开(公告)日：2014-04-29
申请号：US13841384
申请日：2013-03-15
申请人： Sean Robertson
发明人： Sean Robertson
摘要： An electrically-ignited muzzle loader is provided having a stock portion, a trigger assembly, and a barrel portion. The trigger assembly is electrically coupled to a spark plug which extends partially into the barrel portion of the gun. Within the stock is a hand cranked magneto for generating an electric charge. The magneto is electrically coupled to capacitor and coil portions to configure the electrical charge so as to cause the spark plug to generate an igniting spark.
摘要翻译： 提供了一种电点火枪口装载机，其具有储存部分，触发器组件和筒部分。 触发器组件电耦合到部分地延伸到枪的枪管部分中的火花塞。 在股票内部是用于产生电荷的手摇头磁铁。 磁电耦合到电容器和线圈部分以配置电荷，从而使火花塞产生点火火花。
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公开(公告)号：US3783310A
公开(公告)日：1974-01-01
申请号：US3783310D
申请日：1972-06-23
申请人： US NAVY
发明人： SEWELL C , VILLARROEL F , CAMPAGNUOLO C , MCKINDRA C , WOOLSTON L
CPC分类号： F42C15/29 , F41A19/60 , H02K7/1892 , H02K35/06
摘要： A system for firing aircraft rockets including a fluidic generator exposed to the airstream passing the launching aircraft in flight for generating the electrical power necessary to operate the firing circuit. The fluidic generator, produces a voltage output when a predetermined minimum air speed is achieved to charge capacitors in the firing circuit. Silicon controlled rectifiers are shunted across the capacitors to immediately discharge them when the aircraft decelerates below the predetermined minimum air speed.
摘要翻译： 一种用于发射飞机火箭的系统，包括暴露于通过飞行中的发射飞机的气流的流体发生器，用于产生操作击发电路所需的电力。 当实现预定的最小空气速度以对点火回路中的电容器充电时，流体发电机产生电压输出。 可控硅整流器在电容器之间分流，以便当飞机减速至预定的最低空气速度以下时立即将其排出。
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公开(公告)号：US3712170A
公开(公告)日：1973-01-23
申请号：US3712170D
申请日：1970-06-09
申请人： US NAVY
发明人： CAMPAGNUOLO C , MCKINDRA C , WOOLSTON L , SEWELL C , VILLARROEL F
CPC分类号： F42C15/29 , F41A19/60 , H02K7/1892 , H02K35/06
摘要： A system for firing aircraft rockets including a fluidic generator exposed to the airstream passing the launching aircraft in flight for generating the electrical power necessary to operate the firing circuit. The fluidic generator produces a voltage output when a predetermined minimum air speed is achieved to charge capacitors in the firing circuit. Silicon controlled rectifiers are shunted across the capacitors to immediately discharge them when the aircraft decelerates below the predetermined minimum air speed.
摘要翻译： 一种用于发射飞机火箭的系统，包括暴露于通过飞行中的发射飞机的气流的流体发生器，用于产生操作击发电路所需的电力。 当达到预定的最小空气速度以对点火回路中的电容器充电时，流体发生器产生电压输出。 可控硅整流器在电容器之间分流，以便当飞机减速至预定的最低空气速度以下时立即将其排出。
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