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    • 4. 发明授权
    • 40 mm low drag extended range projectile
    • 40毫米低阻力延伸射弹
    • US08887641B1
    • 2014-11-18
    • US13761736
    • 2013-02-07
    • Leon ManoleArthur Ricardo PizzaErnest Lee LogsdonGary Anthony PacellaAnthony J. SebastoWilfredo Toledo
    • Leon ManoleArthur Ricardo PizzaErnest Lee LogsdonGary Anthony PacellaAnthony J. SebastoWilfredo Toledo
    • F42B14/06
    • F42B14/06F42B5/073F42B10/06F42B12/20
    • A 40 mm ammunition projectile for firing without significant spin in an M203 or an M320 grenade launcher. The ammunition includes a projectile body having hollow inner cavity therein for an explosive warhead; a projectile fin assembly; a projectile nose element having a conically shaped front area thereon; a decoupled projectile sabot in two or more joining sabot petals enclosing the body; a base cartridge case having vent holes, a bowl area for placement of a copper closure cup containing propellant therein, and a closure plug for threading into the rear of said cartridge case. The projectile fin assembly may provide a canted angle on each fin blade to (relatively very slowly) spin up the round at less than 30 Hz. Projectiles with body length less than five inches may be launched in an M203 grenade launcher while projectiles with body length up to eight inches may be launched in an M320 grenade launcher.
    • 一枚40毫米弹药射弹,在M203或M320手榴弹发射器中无明显射击。 弹药包括一个其中具有用于爆炸弹头的空心内腔的射弹体; 弹丸组件; 在其上具有锥形正面区域的弹丸鼻元件; 两个或两个以上连接的破坏的花瓣围绕身体的脱离弹丸; 具有通气孔的底座盒壳体,用于放置其中包含推进剂的铜封闭杯的碗区域以及用于穿入所述盒壳体后部的封闭插头。 射弹翅片组件可以在每个翅片叶片上提供倾斜角度(相对非常缓慢地),以小于30Hz旋转圆形。 身体长度小于五英寸的弹体可以在M203手榴弹发射器中发射,同时可以在M320榴弹发射器中发射身长达八英寸的射弹。
    • 5. 发明授权
    • Onboard sensor suite for determining projectile velocity
    • 用于确定弹丸速度的板载传感器套件
    • US08433460B1
    • 2013-04-30
    • US12943214
    • 2010-11-10
    • Thomas RecchiaWilfredo ToledoJason CahaylaEric Scheper
    • Thomas RecchiaWilfredo ToledoJason CahaylaEric Scheper
    • G05D1/00
    • F41G7/34F42B15/01G01P3/665G01P5/16
    • An onboard sensor suite generally includes two main components: a proximity sensor suite for measuring the projectile muzzle velocity; and a pressure sensor suite for measuring the projectile airspeed. The flight velocity of the projectile can then be estimated with a high degree of accuracy using either the muzzle velocity by itself or the airspeed by itself, or, in a preferred embodiment, by using both the muzzle velocity and the airspeed. The proximity sensor suite includes proximity sensors that are mounted along a projectile body; a wire harness; and an onboard computer or CPU. The pressure sensor suite includes a Pitot pressure transducer and two static pressure transducers that are mounted within the projectile body; a wire harness; and a CPU.
    • 车载传感器套件通常包括两个主要部件:用于测量射弹枪口速度的接近传感器套件; 以及用于测量射弹空速的压力传感器套件。 然后可以使用本身的枪口速度或其自身的空速,或者在优选实施例中,通过使用枪口速度和空速两者来高精确度地估计射弹的飞行速度。 接近传感器套件包括沿着射弹体安装的接近传感器; 线束; 以及车载计算机或CPU。 压力传感器套件包括一个Pitot压力传感器和两个安装在射弹体内的静压传感器; 线束; 和一个CPU。