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    • 1. 发明授权
    • Projectile or war-head
    • 射弹或战头
    • US06789484B2
    • 2004-09-14
    • US10633973
    • 2003-08-04
    • Gerd Kellner
    • Gerd Kellner
    • F42B1204
    • F42B12/367F42B12/06F42B12/204F42B12/34
    • Projectiles or war-heads with an inner arrangement for the formation of bulging zones (4,4a) are proposed, comprised of an enclosed bulging medium (1) which is terminal-ballistically substantially ineffective and is radially enclosed by a penetration material (2) which is terminal-ballistically effective, with the bulging medium (1) having a lower density as compared with the enclosing penetration material (2). This leads to the effect that on impact or on penetrating a target plate (3) the bulging medium (1) remains behind relative to the encompassing terminal-ballistic effective body (2) and is laterally increasingly bulged by the bulging material (1) which continues to flow in from behind. As a result of the high pressures, a conical (crowned) pressure and bulging zone (4,4a) is formed dynamically, which zone radially widens or fragments the passing ambient effective material (5,5a).
    • 提出了具有用于形成凸起区域(4,4a)的内部布置的弹头或战头,包括端子弹性基本上无效的并且由穿透材料(2)径向封闭的封闭的凸起介质(1) 与封闭的穿透材料(2)相比,膨胀介质(1)具有较低的密度,其具有终端弹性有效性。 这导致如下效果:在冲击或穿透目标板(3)时,凸起介质(1)相对于包围的末端弹道有效体(2)保持在后面,并且由膨胀材料(1)横向越来越大地凸出, 从后面继续流入。 作为高压的结果,动态地形成锥形(凸起)的压力和凸出区域(4,4a),该区域径向地使通过的环境有效材料(5,5a)变宽或分裂。
    • 2. 发明授权
    • Projectile or war-head
    • 射弹或战头
    • US06772695B2
    • 2004-08-10
    • US10633974
    • 2003-08-04
    • Gerd Kellner
    • Gerd Kellner
    • F42B1204
    • F42B12/367F42B12/06F42B12/204F42B12/34
    • Projectiles or war-heads with an inner arrangement for the formation of bulging zones (4,4a) are proposed, comprised of an enclosed bulging medium (1) which is terminal-effective ballistically substantially ineffective and is radially enclosed by a penetration material (2) which is terminal-ballistically effective, with the bulging medium (1) having a lower density as compared with the enclosing penetration material (2). This leads to the effect that on impact or on penetrating a target plate (3) the bulging medium (1) remains behind relative to the encompassing terminal-ballistic effective body (2) and is laterally increasingly bulged by the bulging material (1) which continues to flow in from behind. As a result of the high pressures, a conical (crowned) pressure and bulging zone (4,4a) is formed dynamically, which zone radially widens or fragments the passing ambient effective material (5,5a).
    • 提出了具有用于形成凸起区域(4,4a)的内部布置的弹头或战头,其包括封闭的膨胀介质(1),其终端有效弹道基本上无效并且被穿透材料(2 ),与封闭的穿透材料(2)相比,膨胀介质(1)具有较低的密度。 这导致如下效果:在冲击或穿透目标板(3)时,凸起介质(1)相对于包围的末端弹道有效体(2)保持在后面,并且由膨胀材料(1)横向越来越大地凸出, 从后面继续流入。 作为高压的结果,动态地形成锥形(凸起)的压力和凸出区域(4,4a),该区域径向地使通过的环境有效材料(5,5a)变宽或分裂。
    • 4. 发明授权
    • Increased velocity-performance-range bullet
    • 增加速度性能范围子弹
    • US06244187B1
    • 2001-06-12
    • US09346182
    • 1999-07-01
    • Lawrence P. Head
    • Lawrence P. Head
    • F42B1204
    • F42B12/34F42B12/78
    • A mushrooming bullet having a highly improved performance in the retention of the lead core within the bullet jacket subsequent to impact, and in performing effectively over a substantially wider velocity range, the bullet retaining its lead core within its jacket substantially 98-100% of its firings at high velocities, and mushrooming more effectively at lower velocities than conventionally manufactured bullets. The jacket is characterized by a base portion which has a substantially larger interior diameter than its shank portion, and a mouth portion which is substantially softer than its shank portion. The mushrooming of the nose portion of the core and the mouth portion of the jacket is effectively arrested by the harder thick shank portion when the bullet strikes a target, and thereby minimizes the loss of lead from the core. The jacket is further characterized by an annular transition shoulder which extends inwardly from the jacket's base portion to its shank portion at an angle to the longitudinal axis of the jacket of at least 7.5 degrees and a radial distance of at least 0.020″, to thereby effectively lock the core within the jacket. The shank portion has a hardness at its rear end of about 145 DPH, which decreases gradually until it joins the mouth portion, at which it has a DPH of about 125 DPH. The mouth portion has a hardness of about 125 DPH at its rear end, which increases gradually to the tip of its mouth at which it has a hardness of about 145 DPH.
    • 在冲击后保持引线芯在子弹夹克内,并在有效地在更大的速度范围内有效地实现了高度改进的性能的子弹,子弹将其引线芯保持在其外壳内基本上为其98-100% 以高速度发射,并以比传统制造的子弹更低的速度更有效地起飞。 护套的特征在于具有比其柄部大得多的内径的基部,以及比其柄部大致更软的口部。 当子弹撞击目标时,芯部的鼻部和夹套的口部的松动被较硬的厚柄部分有效地阻挡,从而使得从芯部损失的铅最小化。 该外套的特征还在于一个环形过渡肩部,其从护套的基部向内延伸至其柄部分,其与护套的纵向轴线至少为7.5度,径向距离至少为0.020“ 有效地将芯子锁在外套内。 柄部分的后端的硬度约为145DPH,其逐渐减小直至其接合嘴部,DPH为约125DPH。 嘴部在其后端具有约125DPH的硬度,其逐渐增加到其口部的尖端,其硬度为约145DPH。
    • 6. 发明授权
    • Lightweight warhead assembly
    • 轻型弹头总成
    • US06227119B1
    • 2001-05-08
    • US09182206
    • 1998-10-30
    • Bruce E. Schmacker
    • Bruce E. Schmacker
    • F42B1204
    • F42B25/00F42B30/08
    • The present invention is devoted to providing projectiles which can be configured as relatively lightweight warhead assemblies that are comparable to heavier warhead assemblies in target-destruction effectiveness. In accordance with exemplary embodiments, the lightweight warhead assemblies can be more efficiently carried in greater numbers on, for example, aircraft platforms. Because these lightweight warhead assemblies can replace existing, larger warhead assemblies, a standard size warhead assembly can be used to attack different types of targets. In addition, various submunitions or unitary warheads can be incorporated into payload containers having a common external shape with common aerodynamic and mass properties, as well as common guidance, sensor, fuzing, and mechanical and electrical interfaces. A standardized, or modular approach improves the interchangeability of various warhead assemblies, reduces costs of configuring and operating the aircraft platform, and enables a reduction in the size of internal weapon bays of aircraft platforms.
    • 本发明致力于提供可以配置为相对轻量级的弹头组件的弹丸,其与具有目标销毁效能的较重的弹头组件相当。 根据示例性实施例,轻型弹头组件可以在例如飞机平台上更多地更有效地承载。 因为这些轻型弹头组件可以替代现有的较大的弹头组件,所以可以使用标准尺寸的弹头组件来攻击不同类型的目标。 此外,各种子弹药或单体弹头可以并入具有共同的外部形状的有效载荷容器中,具有共同的空气动力学和质量特性,以及常见的指导,传感器,辅助和机械和电气界面。 标准化或模块化的方法提高了各种弹头组件的可互换性,降低了飞机平台的配置和操作成本,并且能够减少飞机平台内部武器舱的尺寸。
    • 7. 发明授权
    • Projectile or war-head
    • 射弹或战头
    • US06659013B1
    • 2003-12-09
    • US09087090
    • 1998-05-29
    • Gerd Kellner
    • Gerd Kellner
    • F42B1204
    • F42B12/367F42B12/06F42B12/204F42B12/34
    • Projectiles or war-heads with an inner arrangement for the formation of bulging zones (4,4a) are proposed, comprised of an enclosed bulging medium (1) which is terminal-ballistically substantially ineffective and is radially enclosed by a penetration material (2) which is terminal-ballistically effective, with the bulging medium (1) having a lower density as compared with the enclosing penetration material (2). This leads to the effect that on impact or on penetrating a target plate (3) the bulging medium (1) remains behind relative to the encompassing terminal-ballistic effective body (2) and is laterally increasingly bulged by the bulging material (1) which continues to flow in from behind. As a result of the high pressures, a conical (crowned) pressure and bulging zone (4,4a) is formed dynamically, which zone radially widens or fragments the passing ambient effective material (5,5a).
    • 提出了具有用于形成凸起区域(4,4a)的内部布置的弹头或战头,包括端子弹性基本上无效的并且由穿透材料(2)径向封闭的封闭的凸起介质(1) 与封闭的穿透材料(2)相比,膨胀介质(1)具有较低的密度,其具有终端弹性有效性。 这导致如下效果:在冲击或穿透目标板(3)时,凸起介质(1)相对于包围的末端弹道有效体(2)保持在后面,并且由膨胀材料(1)横向越来越大地凸出, 从后面继续流入。 作为高压的结果,动态地形成锥形(凸起)的压力和凸出区域(4,4a),该区域径向地使通过的环境有效材料(5,5a)变宽或分裂。
    • 8. 发明授权
    • Warhead
    • US06536351B2
    • 2003-03-25
    • US09989755
    • 2001-11-21
    • Jürgen BöckerPaul Wanninger
    • Jürgen BöckerPaul Wanninger
    • F42B1204
    • F42B12/22
    • A warhead (1) having a warhead casing (2) that encloses an explosive charge (5). To ensure that, during the detonation of the explosive charge (5), the warhead (1) effects a rapid acceleration of the fragments flying in the flight direction, and a lesser acceleration of the fragments flying away laterally from the warhead, and/or generates a relatively intense lateral pressure wave, the charge has at least two different partial charges (7, 8-10) corresponding to the intended use of the warhead (1). The first partial charge (7), which is disposed in the region of the tip of the warhead (1), and comprises, for example, octogen (HMX), possesses a high detonation speed in order, when detonated, to accelerate heavy-metal fragments (preferably WSM spherical fragments) disposed in front of the partial charge very rapidly forward. In contrast, the second partial charge (8-10), which adjoins the rear of the first partial charge (7), is a far less costly charge, e.g., RDX, is required solely for accelerating the fragments, comprising steel, for example, that are flying away laterally, or only to generate an intense lateral pressure wave.