公开(公告)号：US08433460B1

公开(公告)日：2013-04-30

申请号：US12943214

申请日：2010-11-10

申请人： Thomas Recchia ,  Wilfredo Toledo ,  Jason Cahayla ,  Eric Scheper

发明人： Thomas Recchia ,  Wilfredo Toledo ,  Jason Cahayla ,  Eric Scheper

IPC分类号： G05D1/00

CPC分类号： F41G7/34 ,  F42B15/01 ,  G01P3/665 ,  G01P5/16

摘要： 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.

摘要翻译： 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。

公开(公告)号：US09115968B1

公开(公告)日：2015-08-25

申请号：US14178968

申请日：2014-02-12

申请人： Benjamin Abruzzo ,  Thomas Recchia ,  Michael Pica ,  Mark Mellini ,  Eric Marshall ,  Jason DeVenezia ,  Sean Schumer ,  John Thomas

发明人： Benjamin Abruzzo ,  Thomas Recchia ,  Michael Pica ,  Mark Mellini ,  Eric Marshall ,  Jason DeVenezia ,  Sean Schumer ,  John Thomas

IPC分类号： F42B15/01 ,  F42B30/00 ,  F42C19/00

CPC分类号： F42B30/006 ,  F41G7/008 ,  F41G7/36 ,  F42B10/50 ,  G05D1/107

摘要： A new fuze that reduces projectile miss-distance to a target, by correcting for discrepancies in anticipated round velocities through its flight. As a result, the fuze-equipped projectile is nominally aimed at a target and maintains improved accuracy relative to a conventional round. The fuze adjusts for the discrepancies in velocity by using an internal electric motor to mechanically actuate a drag-altering surface on the fuze body. In order to adjust for errors in the anticipated velocity, the fuze compares its preprogrammed velocity to its actual velocity at a given point in time during flight. An anticipated velocity table versus time in flight is constantly referenced so that appropriate adjustments in velocity can be made.

摘要翻译： 一个新的引信，通过纠正通过其飞行的预期轮速的差异，减少与目标的射弹错过距离。 因此，引信装备的射弹名义上瞄准一个目标，并相对于常规赛保持提高的准确性。 引信通过使用内部电动机来机械地驱动引信体上的阻力变化表面来调节速度差异。 为了调整预期速度的误差，引信在飞行期间的给定时间点将其预编程速度与其实际速度进行比较。 不断参考飞行中预期的速度表与时间的关系，以便能够进行适当的速度调整。