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Shock wave scoring apparatus employing dual concentric curved rod sensors

机译:采用双同心弯曲杆传感器的冲击波计分装置

摘要

This invention is an automatic gunnery system, responsive to airborne acoustic shock waves produced by a projectile passing through a target area. The invention relates specifically to the "hit" location of the said projectile for the condition when the flight path of the projectile is not perpendicular to the target area. Two pairs of concentric curved elongated acoustic energy conductors (curved sensor rods) are located adjacent to one side of said target area with acoustic transducers attached to the end portions thereof. Said transducers produce an electrical signal when a shock wave from the projectile reaches them through said energy conductors. Electrical signals from the transducers are connected to electronic circuitry and a calculating computer which calculates the intersection of two circles and determines the location of each "hit" on or near the target with each "hit" registered on a graphical display means.
机译:本发明是一种自动炮兵系统,它对由弹丸穿过目标区域产生的空中声冲击波作出反应。具体地,本发明涉及当弹丸的飞行路径不垂直于目标区域时的状况的所述弹丸的“命中”位置。两对同心弯曲的细长声能导体(弯曲的传感器棒)位于所述目标区域的一侧附近,并且声换能器附接到其末端部分。当来自弹丸的冲击波通过所述能量导体到达所述换能器时,所述换能器产生电信号。来自换能器的电信号连接到电子电路和计算计算机,计算计算机计算两个圆的交点,并确定每个“命中”在目标上或目标附近的位置,每个“命中”记录在图形显示装置上。

著录项

  • 公开/公告号US5944317A

    专利类型

  • 公开/公告日1999-08-31

    原文格式PDF

  • 申请/专利权人 ROHRBAUGH;GEORGE WILSON;

    申请/专利号US19970888416

  • 发明设计人 GEORGE WILSON ROHRBAUGH;

    申请日1997-07-07

  • 分类号G01S3/80;

  • 国家 US

  • 入库时间 2022-08-22 02:07:23

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