首页> 外国专利> Payload delivering ring airfoil projectile

Payload delivering ring airfoil projectile

机译:有效载荷传递环翼型弹丸

摘要

A ring airfoil projectile is defined by an annular body which defines a central passage. The body is constructed so that a center of pressure is substantially coincident with a center of gravity thereof. The body is preferably constructed of a nose section and tail section, the nose section of a material having a higher density than the material forming the tail section. The ring airfoil projectile is configured to deliver a payload to a target. Cavities extend inwardly from the outer surface of the airfoil, preferably in the nose section. The cavities accept payload or a strip containing payload. The ring airfoil projectile is configured to travel with minimum path dispersion, and to deliver the payload upon impacting a target.
机译:环形翼型射弹由环形主体限定,该环形主体限定中央通道。主体构造成使得压力中心与其重心基本重合。主体优选地由鼻部和尾部构成,鼻部的材料的密度高于形成尾部的材料的密度。环形翼型弹丸配置为将有效载荷传递到目标。空腔从翼型件的外表面向内延伸,优选在机头部分。腔接受有效负载或包含有效负载的条带。环形翼型弹丸配置为以最小的路径分散传播,并在撞击目标时传递有效载荷。

著录项

  • 公开/公告号US2005183615A1

    专利类型

  • 公开/公告日2005-08-25

    原文格式PDF

  • 申请/专利权人 ABRAHAM FLATAU;

    申请/专利号US20040769399

  • 发明设计人 ABRAHAM FLATAU;

    申请日2004-01-30

  • 分类号F42B8/00;

  • 国家 US

  • 入库时间 2022-08-21 22:25:16

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号