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COST-EFFICIENT PROJECTIL LEADER AND OPERATING PROCEDURE

机译:具有成本效益的项目负责人和操作程序

摘要

A guiding assembly is adapted to be connected to a projectile and comprising a rear main unit adapted to be connected to the front end of the projectile, and a front main unit rotatably connected at its rear end to the front end of the rear main unit. The front main unit is adapted to rotate about a central longitudinal axis. A relative speed control unit is operable between the rear main unit and the front main unit and capable of providing spin braking force to slow the relative speed of rotation of the front main unit. An at least one guiding fin radially extends from the front main unit. The pitch angle of the fin is controllable by a return spring connected to the fin so that the pitch angle of the fin is growing as the aerodynamic pressure on the fin lowers and it is growing smaller as the aerodynamic pressure on the fin gets bigger.
机译:引导组件适于连接至弹丸,并且包括适于连接至弹丸的前端的后主体,以及在其后端可旋转地连接至后主体的前端的前主体。前主体适于绕中央纵向轴线旋转。相对速度控制单元在后主体和前主体之间可操作,并且能够提供旋转制动力以减慢前主体的相对旋转速度。至少一个引导翅片从前主体径向地延伸。翅片的俯仰角可通过连接至翅片的复位弹簧来控制,使得翅片的俯仰角随着翅片上的气动压力降低而增大,并且随着翅片上的气动压力变大而逐渐减小。

著录项

  • 公开/公告号DK2938960T3

    专利类型

  • 公开/公告日2018-12-03

    原文格式PDF

  • 申请/专利权人 BAE SYSTEMS ROKAR INTERNATIONAL LTD.;

    申请/专利号DK20130869242T

  • 发明设计人 WURZEL GIL;MALUL ASSAF;

    申请日2013-10-27

  • 分类号F42B10/64;F42B10/26;

  • 国家 DK

  • 入库时间 2022-08-21 12:02:41

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