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    • 1. 发明授权
    • Sabot for reducing the parasitic weight of a kinetic energy projectile
    • 减少动能弹丸的寄生重量
    • US07013811B1
    • 2006-03-21
    • US10604576
    • 2003-07-31
    • Anthony SebastoStewart GilmanLeon ManoleMohan PalathingalRobert Marchak
    • Anthony SebastoStewart GilmanLeon ManoleMohan PalathingalRobert Marchak
    • F42B13/16
    • F42B14/061F42B14/068
    • An energetic sabot allows part of the sabot to burn away at a controlled rate, adding propellant energy to the gun while at the same time completely support the projectile rod. The energetic sabot is thicker or larger at shot start to support the projectile without breaking. As the energetic sabot travels up the gun tube, the energetic sabot then thins out or otherwise decreases in mass as the force on the energetic sabot decreases. The weight of the projectile consequently decreases as it travels up the gun tube, allowing the gun gases to push a lighter projectile, giving the projectile a higher velocity. Due to its continually decreasing weight in the gun tube, the projectile experiences greater acceleration and exits the gun with a higher muzzle velocity. A secondary effect comes from increased pressure in the gun tube from the gases relinquished in the burning of the sabot, further increasing the velocity of the projectile. This higher velocity in turn leads to greater projectile velocity at target impact, and thus a greater penetration depth. The energetic sabot is “doped” with energetic materials by sprinkling either explosive, propulsive, or pyrotechnic agents between layers of the composite material in the energetic sabot. These agents ignite upon propulsion; their composition is determined from their burn rates. The burn rate may be designed proportional to the decrease in chamber pressure; the less pressure in the tube, the more material that can be relinquished.
    • 一个精力充沛的sabot允许部分燃烧器以受控的速率燃烧,向喷枪添加推进剂能量,同时完全支撑射弹棒。 精力充沛的炮弹在射击开始时更厚或更大,以支撑射弹而不破裂。 当精力充沛的鞋子向上移动枪管时,随着精力充沛的力量上的力量减小,精力充沛的尸体随之消失或以其他方式减小。 射弹的重量因此随着喷枪管的上升而减小,从而允许枪气弹射较轻的射弹,从而使射弹具有更高的速度。 由于其枪管重量不断减小,射弹体现出更大的加速度,并以较高的枪口速度离开枪。 二次效应来自于枪管中从在燃烧火焰中放出的气体中增加的压力增加的压力,进一步增加了射弹的速度。 这种更高的速度又导致在目标冲击下更大的射弹速度,并因此导致更大的穿透深度。 精力充沛的s ot。。。。。。。。。。。。。。。。。。。。。。。。。。。。。。。。。。。。。。。 这些物质在推进时点燃; 它们的组成由其烧伤率确定。 燃烧速率可以设计成与腔室压力的降低成正比; 管中的压力越小,可以放弃的材料越多。
    • 2. 发明授权
    • Low collateral damage air defense projectile
    • 低附带损害防空弹
    • US08640624B1
    • 2014-02-04
    • US13332772
    • 2011-12-21
    • Ahmed HassanMarco DucaMohan PalathingalDaniel VoAnthony Vella
    • Ahmed HassanMarco DucaMohan PalathingalDaniel VoAnthony Vella
    • F42B12/02F42B30/02
    • F42B12/06F42B5/025F42B5/03F42B8/14F42B12/62
    • A kinetic energy penetrator with a longitudinal axis may include a forward segment having a lateral surface, a rear surface, and at least one air bleed channel extending from the lateral surface to the rear surface. A second segment may be disposed aft of and torsionally engaged with the forward segment. The second segment may include a front surface adjacent the rear surface of the forward segment. The forward and second segments may each be asymmetric about the longitudinal axis of the penetrator. When the penetrator is in flight, bleed air through the bleed channels may impinge on the front surface of the second segment. The second segment may separate from the front segment. Kinetic energies of each of the forward and second segments may be less than about 75 joules upon impact with a ground surface.
    • 具有纵向轴线的动能穿透器可以包括具有侧表面,后表面和从侧表面延伸到后表面的至少一个排气通道的前段。 第二段可以被布置在前部的后部并与前部段扭转接合。 第二段可以包括邻近前段的后表面的前表面。 前进和第二段可以各自围绕穿透器的纵向轴线是不对称的。 当穿透器处于飞行状态时,通过排放通道排出空气可能会撞击到第二段的前表面。 第二段可能与前段分离。 每个前段和第二段的动能在与地面碰撞时可能小于约75焦耳。