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公开(公告)号：US20160320165A1
公开(公告)日：2016-11-03
申请号：US15108656
申请日：2015-01-01
发明人： Jacob Rovinsky
CPC分类号： F42B12/22 , B64C39/024 , B64C2201/121 , F41G7/001 , F41G7/20 , F42B10/26 , F42B12/202 , F42B12/32 , F42C19/095
摘要： A fragmentation warhead is provided, capable of being mounted in a carrier vehicle, the warhead having a longitudinal axis. In at least one example the warhead includes a shell that extends along the longitudinal axis. The shell includes a fixed shell portion and a fragmentation portion, and defines therebetween a cavity for accommodating therein an explosive charge. The fragmentation portion includes at least one set of serially adjacent fragments in correspondingly serially contiguous relationship in the fragmentation portion and in generally helical relationship with respect to the longitudinal axis. A corresponding carrier vehicle and a corresponding missile are also provided.
摘要翻译： 提供了能够安装在载体车辆中的分裂弹头，该弹头具有纵向轴线。 在至少一个示例中，弹头包括沿着纵向轴线延伸的壳体。 壳体包括固定壳体部分和碎裂部分，并且在其间限定用于在其中容纳炸药的空腔。 碎裂部分包括在碎裂部分中以相应的串联连续关系的至少一组串联相邻碎片，并且相对于纵向轴线呈大致螺旋关系。 还提供了相应的载体车辆和相应的导弹。
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公开(公告)号：US20140144311A1
公开(公告)日：2014-05-29
申请号：US14232286
申请日：2012-07-04
申请人： Nahum Orlev , Alon Orlev
发明人： Nahum Orlev , Alon Orlev
摘要： A weapon system includes a number of WAN components, each WAN component includes a warhead, a launch mechanism for launching the warhead, an aiming mechanism for aiming the launch mechanism to launch the warhead in a desired direction, and a controller that, upon receipt of a command to aim and launch the warhead, operates the aiming mechanism to aim the warhead in the desired direction and then operates the launch mechanism to launch the warhead. The weapon system also includes a WAN component deployment mechanism for deploying the plurality of WAN components in a defended area; and a command center for instructing the controller of one or more of the WAN components to aim and launch the warhead of the each WAN component at a target that has been detected in the defended area.
摘要翻译： 武器系统包括多个WAN组件，每个WAN组件包括弹头，用于发射弹头的发射机构，用于瞄准发射机构以期望的方向发射弹头的瞄准机构，以及控制器，在接收到 瞄准和发射弹头的指挥，实施瞄准机制，将弹头瞄准所需方向，然后运行发射机制发射弹头。 武器系统还包括用于在防御区域中部署多个WAN组件的WAN组件部署机制; 以及命令中心，用于指示所述WAN组件中的一个或多个的控制器在所述被防御区域中检测到的目标上瞄准并发射所述每个WAN组件的所述弹头。
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公开(公告)号：US4023492A
公开(公告)日：1977-05-17
申请号：US777212
申请日：1968-11-18
申请人： Marvin L. Kempton
发明人： Marvin L. Kempton
CPC分类号： F41H11/02 , F42B12/201 , F42B12/202 , F42B12/22 , Y10S102/701
摘要： A warhead which upon detonation imparts such high velocities to particles magnesium that they expand outwardly faster than the gas from the explosion. The particles are positioned so that they are propelled in predetermined directions. The burning particles precondition the air thus allowing the gaseous explosion products to expand in the particle paths at a much more rapid rate than normal. Larger aluminum particles are also positioned to travel in predetermined directions upon detonation. As the magnesium particles travel outward they lose their effect on the gas cloud because of the distance between them and the expanding gas cloud. The aluminum particles then emerge from the slowing gas cloud and precondition the air to promote more rapid and further expansion of the gas cloud in the paths of the aluminum particles.
摘要翻译： 爆炸时爆炸时会发出高速度的镁弹，使其比爆炸气体向外扩张的速度更快。 颗粒被定位成使得它们在预定方向上被推进。 燃烧的颗粒预处理空气，从而允许气体爆炸产物以比正常更快的速率在颗粒路径中膨胀。 较大的铝颗粒也被定位成在爆炸时沿预定方向行进。 随着镁颗粒向外移动，由于它们之间的距离和气云的膨胀，它们对气云的影响不大。 然后，铝颗粒从缓慢的气体云中出现，并预处理空气，以促进铝颗粒路径中气云的更快速和进一步的膨胀。
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公开(公告)号：US3750587A
公开(公告)日：1973-08-07
申请号：US3750587D
申请日：1971-10-06
发明人： WALDE E
CPC分类号： F42B12/26 , F42B12/202 , F42B12/204 , F42B12/22 , F42B12/32 , F42B12/66
摘要： An explosive projectile member comprising a flexible explosive enclosed in a flexible envelope or casing that enables the whole projectile to change its size and shape from the condition that it was in before launching to another condition after launch. The projectile member is of such construction that it can be compressed to such an extent as to enable it to be placed in a narrow pocket in a mother projectile and/or can be expelled from a short firing tube. After the projectile member has been expelled it is spread out or developed by means of the air drag and elastic forces assisted by additional resilient means provided in the elastic casing.
摘要翻译： 一种爆炸性射弹构件，包括一个封装在柔性封套或外壳内的柔性炸药，使整个射弹能够在发射后发射到另一种状态之前改变其尺寸和形状。 射弹构件具有这样的结构，即可以将其压缩到使其能够放置在母弹射体中的窄口袋中和/或可以从短的发射管排出的程度。 在射弹构件被排出之后，通过设置在弹性外壳中的附加弹性装置辅助的空气阻力和弹性力将其展开或展开。
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5.发明授权Aerodynamic directional grenade, launcher therefor and weapons system utilizing the same 失效航空方向绿色航空公司，其使用者及其使用的武器系统
公开(公告)号：US3646888A
公开(公告)日：1972-03-07
申请号：US3646888D
申请日：1969-03-27
申请人： EXPLOSIVE TECH
CPC分类号： F42B12/24 , F41B3/04 , F41F5/00 , F42B12/202 , F42B12/204 , F42B12/32 , F42B30/10
摘要： An aerodynamic directional grenade in the form of a body formed of a high-energy explosive material, said grenade having a generally saucerlike configuration with upper and lower surfaces that are adapted to sail through the air, the upper surface having a length in the direction of airflow which is greater than the length of the lower surface in the direction of airflow, whereby, when the body is propelled through the air an aerodynamic lift is imparted to the body. Fragment forming means is carried adjacent to one portion of the body, and means is carried by the body for detonating the body. A launcher is provided for the aerodynamic directional grenade and has a launcher housing which carries a magazine that is adapted to receive a plurality of the grenades stacked one above the other, the housing having a discharge opening through which the grenades can be discharged. Means is mounted on the housing for receiving the grenades one by one from the magazine and discharging the same through the said opening at a speed so that the grenades are propelled aerodynamically through the air. Means is further included in said launcher to impart to the aerodynamic directional grenade a degree of rotation resulting in gyroscopic stability about an axis generally transverse to the direction of aerodynamic flight, requisite to maintaining a favorable aerodynamic flight orientation and desired orientation at detonation. Means is mounted on the housing for initiating operation, on or before the grenade leaves the housing, of the means carried by the body for detonating the body. The weapons system may typically be used on a vehicle on which at least one launcher is carried by the vehicle and in which the launcher includes a means for launching the grenades sequentially from said magazine and to disperse the grenades automatically over a predetermined area within reasonably immediate range of the vehicle within a relatively short period of time. A plurality of the launchers can be provided to cover all the immediate area around the vehicle. The weapons system is capable of saturating the area immediately in the vicinity of the launcher with lethal fragments within a very short period of time.
摘要翻译： 一种由高能爆炸材料形成的身体形式的空气动力学定向手榴弹，所述手榴弹具有通常为茶碟形构造，上表面和下表面适于通过空气航行，上表面的长度方向为 气流大于气流方向的下表面的长度，从而当身体通过空气推进时，空气动力升高被赋予身体。 片段形成装置靠近身体的一部分，并且装置由身体携带以引爆身体。
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公开(公告)号：US20240219148A1
公开(公告)日：2024-07-04
申请号：US18426419
申请日：2024-01-30
IPC分类号： F41G3/14 , F41G3/02 , F41G3/06 , F41G3/12 , F41G3/22 , F42B12/20 , F42C13/02 , F42C13/04 , F42C13/08
CPC分类号： F41G3/142 , F41G3/02 , F41G3/06 , F41G3/12 , F41G3/22 , F42C13/026 , F42C13/047 , F42C13/08 , F42B12/20 , F42B12/202
摘要： The method and apparatus for a remote weapon station or incorporated into manually-aimed weapons. The methodology requires use of a muzzle velocity sensor that refines the aiming of the second and subsequent fires or volleys fired from weapon systems. When firing the first volley a weapon uses an estimated velocity and, at firing, the muzzle velocity of a projectile is measured. When firing the second volley a weapon's fire control calculates an aiming point using the measured velocity of the first volley.
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公开(公告)号：US11821716B2
公开(公告)日：2023-11-21
申请号：US17415929
申请日：2019-12-18
申请人： BAE SYSTEMS plc
IPC分类号： F42B12/36 , F42B10/48 , F42B12/20 , F42B21/00 , F42B30/08 , F42C5/00 , F42C7/00 , F42C13/06 , F42C13/08 , F42C9/00
CPC分类号： F42B12/365 , F42B10/48 , F42B12/202 , F42B21/00 , F42B30/08 , F42C5/00 , F42C7/00 , F42C13/06 , F42C13/08 , F42C9/00
摘要： According to an aspect of the invention, there is provided a method of triggering an explosive charge of each of a plurality of munitions, the method comprising: launching a first munition, into the air, from a first gun barrel, and into water to engage with a target location, the first munition comprising a first explosive charge and a first fuze system, adapted to trigger the first explosive charge in the water, launching a second munition, into the air, from a second gun barrel, and into water to engage with the target location, the second munition comprising an second explosive charge and a second fuze system, adapted to trigger the second explosive charge in the water, the method comprising co-ordinating the timing of the triggering of the first explosive charge and the second explosive charge to establish a co-ordinated explosive event at the target location.
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公开(公告)号：US09464873B2
公开(公告)日：2016-10-11
申请号：US14232286
申请日：2012-07-04
申请人： Nahum Orlev , Alon Orlev
发明人： Nahum Orlev , Alon Orlev
摘要： A weapon system includes a number of WAN components, each WAN component includes a warhead, a launch mechanism for launching the warhead, an aiming mechanism for aiming the launch mechanism to launch the warhead in a desired direction, and a controller that, upon receipt of a command to aim and launch the warhead, operates the aiming mechanism to aim the warhead in the desired direction and then operates the launch mechanism to launch the warhead. The weapon system also includes a WAN component deployment mechanism for deploying the plurality of WAN components in a defended area; and a command center for instructing the controller of one or more of the WAN components to aim and launch the warhead of the each WAN component at a target that has been detected in the defended area.
摘要翻译： 武器系统包括多个WAN组件，每个WAN组件包括弹头，用于发射弹头的发射机构，用于瞄准发射机构以期望的方向发射弹头的瞄准机构，以及控制器，在接收到 瞄准和发射弹头的指挥，实施瞄准机制，将弹头瞄准所需方向，然后运行发射机制发射弹头。 武器系统还包括用于在防御区域中部署多个WAN组件的WAN组件部署机制; 以及命令中心，用于指示所述WAN组件中的一个或多个的控制器在所述被防御区域中检测到的目标上瞄准并发射所述每个WAN组件的所述弹头。
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公开(公告)号：US20140083402A1
公开(公告)日：2014-03-27
申请号：US13624936
申请日：2012-09-23
申请人： L.H.B. LTD.
发明人： Ofer Fridman , Yariv Ben Yehuda
摘要： A crowd control projectile includes a payload carrier, an incapacitating agent inside the payload carrier, and an activating mechanism for activating the incapacitating agent. The activating mechanism includes a sensor and a timer. The timer delays the activation until a predetermined delay after the sensor senses that the projectile has been launched. Alternatively, the activating mechanism includes a receiver for receiving an activation signal after the projectile has been launched. Preferably, the projectile has the shape of a clay pigeon. A launcher of such a projectile includes a communication mechanism for transmitting a timing signal or an activation signal to the projectile and an arm for launching the projectile by direct contact. To control a crowd, the projectile is launched over the crowd by direct contact with a solid arm and the activating mechanism is used to activate the incapacitating agent when the projectile is above the crowd.
摘要翻译： 人群控制射弹包括有效载荷载体，有效载荷载体内的失能剂，以及用于激活失能剂的活化机构。 激活机构包括传感器和计时器。 定时器延迟激活，直到传感器感测到弹丸已被启动之后的预定延迟。 或者，激活机构包括用于在发射弹体之后接收激活信号的接收器。 优选地，抛射体具有粘土鸽的形状。 这种射弹的发射器包括用于将定时信号或激活信号发射到射弹的通信机构和用于通过直接接触发射射弹的臂。 为了控制人群，射弹通过与实心臂直接接触而在人群中发射，当弹丸高于人群时，激活机构用于激活失能剂。
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公开(公告)号：US3818833A
公开(公告)日：1974-06-25
申请号：US28190472
申请日：1972-08-18
申请人： FMC CORP
发明人： THRONER G
CPC分类号： F42B12/202 , F42B10/56 , F42B12/204 , F42B12/208 , F42B12/58
摘要： A missile carries a plurality of independent explosive heads which when fired direct fragments only in a forward direction. The missile releases all heads either in response to a timed delay from drop or launch or in response to movement of the missile to a predetermined position relative to the target. Upon release the explosive heads are rotated to swing each head away from the other heads while retaining orientation of each head so that firing of the dispersed heads will cause fragments to discharge forwardly toward the target without undue interference with the fragments from other heads.
摘要翻译： 导弹携带多个独立的爆炸头，当直接向前发射直接碎片时。 导弹释放所有的头部，以响应于下降或发射的定时延迟或者响应于导弹相对于目标的预定位置的运动。 当释放时，爆炸头被旋转以使每个头部远离其他头部，同时保持每个头部的取向，使得分散的头部的点火将导致碎片向前朝向靶材排出，而不会不适当地干扰来自其他头部的碎片。
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