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    • 4. 发明授权
    • Method and apparatus for guided missile and/or net shield
    • 导弹和​​/或网盾的方法和装置
    • US09091513B2
    • 2015-07-28
    • US13605097
    • 2012-09-06
    • Jason J. Shand
    • Jason J. Shand
    • F41H13/00F42B10/60F42B12/20F42B12/56F42B10/00F42B12/00
    • F41H13/0006
    • An apparatus including a body portion, a plurality of missiles attached to the body portion in a manner which allows the plurality of missiles to detach from the body portion, a net having a plurality of locations, wherein each missile is attached to the net at a different location of the plurality of locations, and means for controlling a flight direction and a flight speed of each of the plurality of missiles. The means for controlling the flight direction and the flight speed of each of the plurality of missiles may include a computer processor attached to each of the plurality of missiles. A majority of the net may lie inside of an inner chamber inside of the body portion, and the at least a majority of the net may be configured to come out of the inner chamber in response to a command from a control device.
    • 一种装置,包括主体部分,以允许多个导弹从主体部分分离的方式附接到主体部分的多个导弹,具有多个位置的网,其中每个导弹附接到网 多个位置的不同位置,以及用于控制多个导弹中的每一个的飞行方向和飞行速度的装置。 用于控制多个导弹中的每一个的飞行方向和飞行速度的装置可以包括附接到多个导弹中的每一个的计算机处理器。 网的大部分可以位于主体部分内的内室的内部,并且网的至少大部分可以被配置为响应于来自控制装置的命令而从内腔中出来。
    • 5. 发明申请
    • METHOD AND APPARATUS FOR GUIDED MISSILE AND/OR NET SHIELD
    • 指导性和/或网盾的方法和装置
    • US20140231575A1
    • 2014-08-21
    • US13605097
    • 2012-09-06
    • Jason J. Shand
    • Jason J. Shand
    • F42B12/56F42B10/60F42B12/20F41H13/00
    • F41H13/0006
    • An apparatus including a body portion, a plurality of missiles attached to the body portion in a manner which allows the plurality of missiles to detach from the body portion, a net having a plurality of locations, wherein each missile is attached to the net at a different location of the plurality of locations, and means for controlling a flight direction and a flight speed of each of the plurality of missiles. The means for controlling the flight direction and the flight speed of each of the plurality of missiles may include a computer processor attached to each of the plurality of missiles. A majority of the net may lie inside of an inner chamber inside of the body portion, and the at least a majority of the net may be configured to come out of the inner chamber in response to a command from a control device.
    • 一种装置,包括主体部分,以允许多个导弹从主体部分分离的方式附接到主体部分的多个导弹,具有多个位置的网,其中每个导弹附接到网 多个位置的不同位置,以及用于控制多个导弹中的每一个的飞行方向和飞行速度的装置。 用于控制多个导弹中的每一个的飞行方向和飞行速度的装置可以包括附接到多个导弹中的每一个的计算机处理器。 网的大部分可以位于主体部分内的内室的内部,并且网的至少大部分可以被配置为响应于来自控制装置的命令而从内腔中出来。
    • 6. 发明申请
    • Partial decomposition projectile with a double core
    • 具有双核的部分分解弹丸
    • US20090293754A1
    • 2009-12-03
    • US10567089
    • 2004-07-30
    • Heinz RiessErich Muskat
    • Heinz RiessErich Muskat
    • F42B12/56
    • F42B12/74F42B12/34F42B12/367
    • The decomposition of a projectile in a target body, particularly a hunting projectile in wild animals after penetration therein, determines the energy output of the projectile and thereby the effect of the shot. For projectiles with double cores, the properties of the ingredients used in the cores decisively affect the decomposition and particularly the deformation behaviour of the cores. According to the invention, a partial decomposition projectile comprising two cores is provided with one solid core (3) made of a material suited to said projectile and the other core (4;22) is divided up into two areas (4a,4b;22a;22b), whereby one area (4a;22a) is made of ball-shaped elements made of a metal material granulate (5;23) and the second area (4b;22b) is made of a metal or ceramic powder and the ball-shaped elements or granulates (5;23) are pressed to become free of shrink holes, in order to improve decomposition behaviour control.
    • 射弹在目标体内的分解,特别是野生动物在其中穿透后的狩猎射弹,决定了射弹的能量输出,从而决定了射击的效果。 对于具有双核的抛射体,芯中使用的成分的性质决定性地影响芯的分解,特别是影响芯的变形行为。 根据本发明,包括两个芯的部分分解抛射体设置有由适于所述抛射体的材料制成的一个实芯(3),另一个芯(4; 22)被分成两个区域(4a,4b; 22a ; 22b),其中一个区域(4a; 22a)由由金属材料颗粒(5; 23)制成的球形元件制成,并且第二区域(4b; 22b)由金属或陶瓷粉末制成,并且球 形状的元件或颗粒(5; 23)被压制成没有收缩孔,以改善分解行为的控制。
    • 8. 发明授权
    • Deterrent ammunition
    • 威慑弹药
    • US3894492A
    • 1975-07-15
    • US37845373
    • 1973-07-12
    • AAI CORP
    • BARR IRWIN RBROWN PAUL LSCHNEPPE JR ROBERT W
    • F42B12/50F42B12/56F42B14/02F42B14/06F42B31/00
    • F42B14/064F42B12/50F42B12/56F42B14/02F42B14/068
    • Deterrent ammunition, including a projectile of soft elastic rupturable material, such as natural or synthetic rubber or plastic, having a charge of flowable material, such as finely divided particulate or powder, carried in a cross-sectionally polygonal cavity having relatively thin longitudinal rupture wall zones along the corners of the cavity and thicker longitudinal strengthening zones bounding the cavity straight wall surface sections, with a generally ogive-forming nose section having an easily flexible annular wall connecting with a thicker and more rigid piston-forming nose end of lesser lateral crosssection than the interior cavity cross-section at the rear end of the flexible annular wall for ease of rearward piston movement of the pistonforming nose end on target impact. The projectile is carried in a cartridge by a bore-riding segmented sabot of low density, low mass material and is ejected from the cartridge by ignition of propellant in the cartridge, which effects gas pressure on an obturating pusher disc engaging with the rear of the segmented sabot.
    • 包括弹性弹性材料的射弹,例如天然或合成橡胶或塑料的弹性材料,其具有可流动材料的电荷,例如细碎的颗粒或粉末,在具有相对薄的纵向破裂壁的横截面多边形腔中 沿着腔体的角部的区域和包围腔体直壁表面部分的较厚的纵向加强区域,其具有通常成形的鼻部部分,其具有容易柔性的环形壁,其与更小和更刚性的形成较小横向横截面的活塞形成鼻端连接 比在柔性环形壁的后端处的内腔横截面更容易地使活塞成形鼻端的后活塞运动在目标冲击上。 抛射体通过低密度,低质量材料的穿孔分段式炮塔携带在筒中,并且通过点燃推进剂在筒中而从筒中弹出,这使得气密压在与后面的 分段的sabot。