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    • 81. 发明授权
    • Shotgun cartridge with explosive shell
    • 霰弹枪筒带爆炸壳
    • US5000094A
    • 1991-03-19
    • US907736
    • 1986-08-21
    • Leroy J. Sullivan
    • Leroy J. Sullivan
    • F42B12/58F42B20060101F42B5/00F42B7/02F42B7/10F42B12/10F42C1/10
    • F42B12/10F42B7/10F42C1/10
    • A shotgun cartridge (1) has an armour piercing shell (11) which includes a main charge (17) arranged to be detonated or exploded by direct percussion of a primer (12). The cartridge (1) includes a bore safe cylindrical arming device (16) integrally formed with the obturator (6), which interrupts the detonation process after detonation of the primer (12). The arming device (16) is arranged to separate from the shell, to arm the shell, after firing of the shell (11) from the barrel of a gun, and the shell (11) includes an open base or rear portion to prevent shrapnel being thrown to the rear on detonation.
    • PCT No.PCT / EP85 / 00718 Sec。 371日期1986年8月21日 102(e)日期1986年8月21日PCT 1985年12月17日PCT PCT。 出版物WO86 / 03826 日期:1986年7月3日。霰弹枪筒(1)具有装甲穿刺壳(11),其包括通过底漆(12)的直接冲击而被引爆或爆炸的主要装药(17)。 盒(1)包括与封闭器(6)一体形成的孔安全圆柱形布置装置(16),其在引爆物(12)引爆之后中断爆震过程。 布置装置(16)布置成在从炮筒的枪身射出壳体(11)之后,与壳体分离,从而臂壳,并且壳体(11)包括开放的基部或后部以防止弹片 被引爆到后方。
    • 82. 发明授权
    • Cartridged ammunition
    • 彩色弹药
    • US4892038A
    • 1990-01-09
    • US287261
    • 1988-12-06
    • Willi Lubbers
    • Willi Lubbers
    • F42B20060101F42B5/067F42B5/16F42B8/00F42B12/48
    • F42B12/48F42B5/067
    • Cartridge ammunition 1 for a grenade pistol includes a casing 10 made, for example, of plastic, the casing having an opening. A projectile 11 disposed in the casing opening and includes a tracer charge and/or delayed-action charge 11b. A primer 13 and a propelling charge 14 the disposed in a cup 12 at the base of casing 10. The cup 12 is composed of two mutually concentric sleeves 12a, and 12b, with the inner sleeve 12b being mounted so as to be slidable in the outer sleeve 12a and extendable in the manner of a telescope. The outer sleeve 12a has a free end section which is provided, with an external thread 100 followed by an annular, predetermined, circumferential break location 12d. The base of projectile 11 includes a sleeve 17 provided with an internal thread which can be screwed onto the outer sleeve 12a of cup 12. A firing channel 12c is provided in the bottom or end wall 12e of the cup-shaped inner sleeve 12b, with such firing channel being oriented toward the tracer and/or delayed-action charge 11b. The result of this construction is that the ammunition can be assembled easily, and an almost constant initial velocity can be maintained despite fluctuating environmental conditions.
    • 87. 发明申请
    • Ammunition for pistols and carbines
    • 弹药和卡宾枪弹药
    • US20050016414A1
    • 2005-01-27
    • US10757427
    • 2004-01-15
    • Paul Leitner-Wise
    • Paul Leitner-Wise
    • F42B20060101F42B5/02F42B14/06
    • F42B5/025
    • The invention relates to improved ammunition for pistols and carbines to provide a cartridge that may be used within the restricted dimensions of these weapons while increasing the effective range normally associated with such ammunition. Additionally, the velocity increase creates sufficient projectile cross-sectional energy to allow the perforation of certain body armor types. The invention provides a cartridge which by means of diameter reduction of the case in the area of the front and the application of a sabot or bore carrier assembly allows a small diameter projectile, typically 5.56 millimeters, to be fired from a short compact ammunition that may be employed in a pistol size weapon. A weapon chamber is dimensioned to accept the cartridge as described at a tolerance between approximately 3 and 9 one thousandths of an inch.
    • 本发明涉及用于手枪和卡宾枪的改进的弹药,以提供可以在这些武器的限制尺寸内使用的弹药筒,同时增加与这种弹药通常相关联的有效范围。 另外,速度增加产生足够的射弹横截面能量,以允许穿孔某些身体护甲类型。 本发明提供了一种通过壳体在前部区域中的直径减小并且施加砧座或孔承载器组件的筒,其允许通过5.76毫米的小直径射弹从短的紧凑型弹药中射出, 被雇用在手枪尺寸的武器。 武器舱的尺寸设计为接受墨盒,如公差在大约3到9千分之一英寸之间。
    • 88. 发明授权
    • Process for guiding a flying object and flying objects
    • 引导飞行物体和飞行物体的过程
    • US5880396A
    • 1999-03-09
    • US63507
    • 1993-03-26
    • Athanassios Zacharias
    • Athanassios Zacharias
    • B64C15/14B64D17/80F41G20060101F41G7/22F42B20060101F42B10/02F42B10/66F42B15/00
    • F42B10/663
    • Process for guiding an elongated missile, equipped with booster motor, sustainer, power source, control electronics, payload, and search head, from above, upon a target, such as a helicopter, where the missile, after ballistic flight, is braked before the target area by a drogue chute and is diverted into a position that is essentially perpendicular to the earth's surface over the target area so that the search head of the missile, which is suspended from the drogue chute, will be pointed downward, whereupon, after the search head has locked on the target, the drogue chute is separated and the missile is guided to the target by the sustainer, characterized in that, immediately prior to, before, or after the moment of drogue chute deployment, a lateral motor, located in the center of gravity of the missile, is turned on so that, first of all, in order to accelerate the tilt-off of the missile into the vertical, there is generated a force that is added vectorially to the force of gravity and that thereupon one can counteract the missile's rolling, pitching, and yawing motions, that take place during the search phase that follows the tilt-off, so that the missile is stabilized, as well as missile for performance of said process.
    • 用于引导从上方装备有增压马达,维持器,动力源,控制电子装置,有效载荷和搜索头的细长导弹到诸如直升机的目标,其中弹道飞行之后的导弹在 目标区域由转向滑道引导到基本上垂直于目标区域上的地球表面的位置,使得从冷冻滑槽悬挂的导弹的搜索头将向下指向,于是,在 搜索头已经锁定在目标上,分离滑道被分离,导弹由导向器引导到目标,其特征在于,在紧急滑槽滑行部分之前,之前或之后,位于 导弹的重心被打开,首先,为了加速导弹向垂直方向的倾斜,产生了一个向量力向重力加上的力 因此,可以在导弹的倾斜关闭后的搜索阶段抵消导弹的滚动,俯仰和偏航运动,从而使导弹稳定下来,并且导弹能够执行所述过程。