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1. 发明公开

US20240027159A1 FIREARM FIRING CONTROL SYSTEM AND RED DOT POSITIONING ASSEMBLY 审中-公开
公开(公告)号：US20240027159A1
公开(公告)日：2024-01-25
申请号：US17869688
申请日：2022-07-20
申请人： Maia Pellegrini
发明人： Maia Pellegrini
IPC分类号： F41A19/63 , F41A19/59
CPC分类号： F41A19/63 , F41A19/59
摘要： A firearm firing control system includes a touchless sensor firing control assembly for touchless control of firing the firearm. The sensor is electrically connected to a power source and a load. When the sensor senses input (e.g., movement), an activation voltage from the power source causes the load to mechanically operate the trigger mechanism of the firearm. Circuit logic electrically resets the sensor, and the action of the slide mechanically resets the load.

2. 发明申请

US20090300961A1 BOLT ACTION PART FOR ELECRICAL OR LASER-BASED CARTRIDGE 审中-公开
标题翻译：用于激光或激光打标的螺栓动作部件
公开(公告)号：US20090300961A1
公开(公告)日：2009-12-10
申请号：US12523570
申请日：2008-01-18
申请人： Alfons Ruhland , Michael Obergantschnig
发明人： Alfons Ruhland , Michael Obergantschnig
IPC分类号： F41A19/63 , F41A19/62 , F41A19/60 , F41A17/00 , F41A17/06 , F41A17/30 , F41A17/64 , F41A17/74 , F41A9/00
CPC分类号： F41A3/16 , F41A19/58 , F41A19/63
摘要： Disclosed is a chamber closing piece (1) for firearms. Said chamber closing piece (1) can be rotatably and reversibly moved forward in the direction of the barrel muzzle (3) and rearward in the direction of the rear stock (4) and comprises one or several mechanisms (8) for indirectly or directly firing a bullet (9) that faces the muzzle in relation to the chamber closing piece (1). Said mechanism (8) for firing the ammunition is based on an electrical and/or thermal and/or optical and/or laser-based active principle.
摘要翻译：公开了一种用于枪支的室封闭件（1）。所述腔室闭合件（1）可以沿着枪管枪口（3）的方向可旋转地和可逆地向前移动，并且在后部药品（4）的方向上向后移动，并且包括用于间接或直接燃烧的一个或多个机构（8）相对于室闭合件（1）面向枪口的子弹（9）。用于发射弹药的所述机构（8）基于基于电和/或热和/或光学和/或基于激光的有源原理。

3. 发明授权

US06962112B1 Entirely combustible inductive primer 有权
标题翻译：完全可燃性感应底漆
公开(公告)号：US06962112B1
公开(公告)日：2005-11-08
申请号：US10048168
申请日：2000-07-12
申请人： Heinz Kern
发明人： Heinz Kern
IPC分类号： C06B45/12 , C06C9/00 , F41A19/63 , F42B5/08 , F42C19/12 , H01F5/00 , H01F27/28
CPC分类号： F41A19/63 , C06B45/12 , C06C9/00 , F42B5/08 , F42C19/12
摘要： A pyrotechnical primer for igniting propellant powder for sleeveless ammunition comprises an igniting element (4) and a coil (1). The energy required for triggering is transmitted in an electromagnetic manner (inductively). The inductive primer is cost-effective, entirely combustible, easy to produce and is not provided with residues that damage the functioning of the weapons. The primer has a base construction such that the primer can be used in all conventional weapons calibres. To this end, the ignition element (4) and the coil (1) are located on a mutual, flat, combustible consumable or support material (5).
摘要翻译：用于点燃用于无袖弹药的推进剂粉末的烟火底漆包括点火元件（4）和线圈（1）。触发所需的能量以电磁方式（电感式）传输。感应底漆具有成本效益，完全可燃，易于生产，不具有损坏武器功能的残留物。底漆具有基底结构，使得底漆可以用于所有常规武器口径。为此，点火元件（4）和线圈（1）位于相互平坦的可燃消耗品或支撑材料（5）上。

4. 发明授权

US4685395A Controlled inductive coupling device 失效
标题翻译：受控感应耦合器件
公开(公告)号：US4685395A
公开(公告)日：1987-08-11
申请号：US708054
申请日：1985-03-04
申请人： Alan G. King
发明人： Alan G. King
IPC分类号： H01F38/12 , F41A19/63 , F42B3/12 , F42B3/18 , F42D1/045 , H01F21/08 , F42C15/40 , F42D5/00
CPC分类号： F41A19/63 , H01F21/08
摘要： An inductive coupling device is provided wherein the transmission of energy through the device is controlled by the application of a steady magnetic field within the magnetically permeable core of the device, transmission being inhibited at high magnetic field intensity and restored when the magnetic field intensity is reduced to a low value. The device is especially advantageous for the safe coupling of ignition elements, such as blasting detonators, to an a.c. firing energy source.
摘要翻译：提供了一种电感耦合器件，其中通过在器件的可渗透芯内施加稳定磁场来控制通过器件的能量传输，传输在高磁场强度下被抑制，并且当磁场强度减小时被恢复低价值。该装置对于诸如爆破雷管的点火元件的安全联接特别有利。射击能源。

5. 发明授权

US4445434A Arrangement for the contactless transmission of electric energy to missiles during firing thereof 失效
标题翻译：发射过程中电能对导弹的非接触传输的布置
公开(公告)号：US4445434A
公开(公告)日：1984-05-01
申请号：US277863
申请日：1981-06-26
申请人： Uwe Brede , Gerhard Kordel
发明人： Uwe Brede , Gerhard Kordel
IPC分类号： F41A19/63 , F42C15/40 , F42C19/12
CPC分类号： F42C15/40 , F41A19/63
摘要： An arrangement for the contactless transmission of electrical energy to a missile during the firing thereof from a firing device including a transformer-like coil system having a primary coil system connected to the firing device and a secondary coil system connected to the missile. The primary coil system is supplied with electric energy and the secondary coil system is responsive to the electric energy developed in the primary coil system for developing electrical energy therein. A partition is arranged between the primary coil system and the secondary coil system and is formed of a nonmagnetic material capable of withstanding thermal and mechanical stresses of repeated firings by the firing device. The partition is fixedly connected with the firing device and disposed for sealing the primary coil system with respect to the missile at least during the firing of the missile from the firing device.
摘要翻译：一种用于在从包括具有连接到点火装置的初级线圈系统的变压器状线圈系统和连接到该导弹的次级线圈系统的点火装置的点火装置中将电能非接触地传输到导弹的装置。初级线圈系统被提供有电能，次级线圈系统响应于在初级线圈系统中产生的电能，用于在其中显现电能。分隔件布置在初级线圈系统和次级线圈系统之间，并且由能够承受由点火装置重复发出的热和机械应力的非磁性材料形成。分隔件固定地连接着点火装置，并设置成至少在从点火装置射出导弹时相对于导弹密封初级线圈系统。

6. 发明授权

US4377113A Rocket firing system 失效
标题翻译：火箭发射系统
公开(公告)号：US4377113A
公开(公告)日：1983-03-22
申请号：US232846
申请日：1981-02-09
申请人： John R. Florence
发明人： John R. Florence
IPC分类号： F41A19/00 , F41A19/63 , F42C19/12
CPC分类号： F41A19/00 , F41A19/63
摘要： A rocket firing system comprises a magnetic core, a co-axial driver coil and a sensor coil or coils which are connected to a detector device which detects the presence and the desired state of a further coil which is inductively linked to the magnetic core. In use a low-power signal voltage is first applied to the driver coil. Subject to the detector device indicating the presence and desired state of a firing circuit of a rocket including the further coil, an operating power voltage is then applied to the driver coil to induce a firing voltage in the firing circuit.
摘要翻译：火箭发射系统包括磁芯，同轴驱动器线圈和传感器线圈或线圈，其连接到检测器装置，该检测器装置检测感应地连接到磁芯的另外的线圈的存在和期望状态。在使用中，首先将低功率信号电压施加到驱动器线圈。受检测器装置指示包括另外的线圈的火箭的点火电路的存在和期望状态，然后将工作电源电压施加到驱动器线圈以在点火电路中引发点火电压。

7. 发明授权

US4087774A Information transmitting system 失效
标题翻译：信息传输系统
公开(公告)号：US4087774A
公开(公告)日：1978-05-02
申请号：US703133
申请日：1976-07-07
申请人： Roger Beuchat
发明人： Roger Beuchat
IPC分类号： H04B5/00 , F41A19/63 , F42C17/04 , G06K7/08 , H01F27/38 , H01F27/40 , H01F38/14 , H02J17/00 , H01F27/28
CPC分类号： G06K7/10336 , F42C17/04 , H01F27/38 , H01F27/40 , H01F38/14 , H01F2038/143 , Y10S336/02
摘要： An information transmitting system by means of a coded magnetic signal permitting adjusting the options in a fuze. A primary winding magnetically induces a coded current in a secondary winding located within a housing. A conductive short-circuit ring is located between both windings for concentrating the magnetic flux within the receiving winding, and thus reducing the magnetic losses.
摘要翻译：一种通过编码磁信号的信息发送系统，允许调整引信中的选项。初级绕组在位于壳体内的次级绕组中磁感应地产生编码电流。导电短路环位于两个绕组之间，用于将磁通集中在接收绕组内，从而减小磁损耗。

8. 发明授权

US3148619A High frequency immune squib 失效
标题翻译：高频免疫爆管
公开(公告)号：US3148619A
公开(公告)日：1964-09-15
申请号：US11758161
申请日：1961-06-16
申请人： BJORKSTEN RES LAB FOR INDUSTRY
发明人： HOLINBECK DALE G
IPC分类号： F41A19/63 , F42B3/18
CPC分类号： F42B3/18 , F41A19/63

9. 发明授权

US2690124A Induction firing means for rockets 失效
标题翻译：火箭发射装置
公开(公告)号：US2690124A
公开(公告)日：1954-09-28
申请号：US19091650
申请日：1950-10-19
申请人： US ARMY
发明人： MELICK JOHN M
IPC分类号： F41A19/63 , F41F3/052
CPC分类号： F41A19/63 , F41F3/052

10. 发明授权

US11725896B2 Repeatable plasma generator 有权
公开(公告)号：US11725896B2
公开(公告)日：2023-08-15
申请号：US17781817
申请日：2020-12-01
申请人： BAE SYSTEMS BOFORS AB
发明人： Mats Jansson
IPC分类号： F41A19/63 , F42C19/08
CPC分类号： F41A19/63 , F42C19/0811 , F42C19/0823
摘要： A plasma generator is provided for initiation of propellant charges in a weapons system, for example when launching projectiles from a barrel weapon, by electrical discharge between a rear electrode and a front electrode in a combustion chamber channel enclosed in a combustion chamber body and filled with filling gas, designed to ignite at least one propellant charge. An ammunition unit and a launching device including the plasma generator are also provided.

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