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公开(公告)号：US4362107A
公开(公告)日：1982-12-07
申请号：US84758
申请日：1979-10-15
申请人： Rudolf Romer , Christian Jaeneke , Gunter Sikorski
发明人： Rudolf Romer , Christian Jaeneke , Gunter Sikorski
摘要： Practice projectile for target practice, which corresponds in shape and weight to a normal combat projectile, particularly to a sub-caliber combat projectile. The projectile upon impact disintegrates at preset breaking points. The projectile is unitary, but has at least one preset breaking point along its length. The projectile may be constructed as a tail-stabilized arrow-shaped projectile with a propulsive sabot extending over the preset breaking line and the preset breaking line may be positioned in the zone of the minimum firing loading.
摘要翻译： 对于目标实践的射弹，其形状和重量对应于正常的作战射弹，特别是对于低射炮作战射弹。 撞击后的弹丸在预先设定的断点处分解。 射弹是一体的，但沿其长度至少有一个预设的断点。 抛射体可以被构造为具有延伸在预设断裂线上的推进式突起的尾部稳定的箭头状射弹，并且预设的断裂线可以定位在最小燃烧负载的区域中。
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公开(公告)号：US4616567A
公开(公告)日：1986-10-14
申请号：US747565
申请日：1985-06-20
CPC分类号： F42B12/58
摘要： A method and apparatus for covering a target area with ammunition, wherein a container, which contains active bodies W arranged on different decks 30.1, 30.2 and which is to be brought over the target area, releases the active bodies W through release openings 34 on its sides to become effective from above on respective individual flight paths against objects, for example armored vehicles, present in the target area.
摘要翻译： 一种用弹药覆盖目标区域的方法和装置，其中包含布置在不同甲板30.1,30.2上并且将被覆盖在目标区域上的活动物体W的容器通过其上的释放开口34释放活性物体W 双方将在相应的个别飞行路线上从对上述目标区域内的物体（例如装甲车辆）开始生效。
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公开(公告)号：US4242960A
公开(公告)日：1981-01-06
申请号：US970182
申请日：1978-12-18
CPC分类号： F42B8/14
摘要： There is disclosed a missile which automatically disintegrates after a predetermined flight time. The missile is made up of several parts which are positively secured together by a locking means which is released at a predetermined time after the firing of the missile by the action of the air through which the missile passes during its flight. The invention may by used to advantage in both practice missiles and service missiles.
摘要翻译： 公开了一种在预定飞行时间后自动分解的导弹。 导弹由多个部件组成，这些部件通过锁定装置牢固地固定在一起，该锁定装置在导弹通过飞行中通过的空气的作用而被射击之后的预定时间被释放。 本发明可以在实践导弹和服务导弹中有利地使用。
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公开(公告)号：US4555971A
公开(公告)日：1985-12-03
申请号：US398242
申请日：1982-07-14
CPC分类号： F42B12/58
摘要： In the method and apparatus for covering a target area with ammunition, a container, which contains active bodies W arranged on different decks 30.1, 30.2 and which is to be brought over the target area, releases the active bodies W through release openings 34 on its sides to become effective from above on respective individual flight paths against objects, for example armored vehicles, present in the target area.
摘要翻译： 在用弹药覆盖目标区域的方法和装置中，包含布置在不同甲板30.1,30.2上并将被覆盖在目标区域上的活动物体W的容器通过其上的释放开口34将活性物体W释放 双方将在相应的个别飞行路线上从对上述目标区域内的物体（例如装甲车辆）开始生效。
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公开(公告)号：US4177733A
公开(公告)日：1979-12-11
申请号：US834496
申请日：1977-09-19
申请人： Rudolf Romer , Manfred Moll , Christian Jaeneke
发明人： Rudolf Romer , Manfred Moll , Christian Jaeneke
CPC分类号： F42B14/064 , F42B14/02
摘要： There is described a spin stabilized projectile assembly including a projectile, a sabot, and a guide ring. The projectile is provided with a shoulder at the rear end of which abuts the sabot, the projectile and sabot being connected by the guide ring which extends around the projectile and part of the sabot. The guide ring is arranged so that after the projectile assembly has been fired and has left the barrel of the weapon the sabot and the projectile separate. The sabot has a diameter substantially equal to that of the projectile; the guide ring is secured to the sabot against relative movement in a longitudinal direction but is rotatable with respect to the sabot.
摘要翻译： 描述了一种自旋稳定的射弹组件，其包括抛射物，破坏物和引导环。 抛射体在其后端设有一个肩部，其肩部与导弹环相连，弹丸和突起通过围绕射弹和部分炮弹延伸的引导环连接。 引导环布置成使得在射弹组装已经被射出并且已经离开武器的枪管之后，将弹药和弹丸分开。 炮弹的直径与射弹的直径基本相等; 引导环固定到砧座上以防止在纵向方向上的相对运动，但是可以相对于砧座旋转。
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公开(公告)号：US4153223A
公开(公告)日：1979-05-08
申请号：US801426
申请日：1977-05-27
摘要： There is disclosed a limited range, high-speed projectile with a flat trajectory. The range is limited by controlling the air resistance of the projectile, so that the air resistance increases markedly when the projectile speed drops below a certain value.
摘要翻译： 公开了一种有限范围的，具有平坦轨迹的高速射弹。 通过控制射弹的空气阻力来限制射程，当射弹速度低于一定值时，空气阻力显着增加。
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