首页> 外国专利> Projectile fin deployment mechanism has fin support that pivots about axis perpendicular to lengthwise axis of projectile

Projectile fin deployment mechanism has fin support that pivots about axis perpendicular to lengthwise axis of projectile

机译:弹丸鳍片展开机构具有鳍片支撑件,该鳍片支撑件绕垂直于弹丸纵向轴线的轴线枢转

摘要

A mechanism (2) for deploying the fin of a projectile (1) between launch and trajectory positions comprises a fin support (5) that pivots about an axis (7) perpendicular to the lengthwise axis (4) of the projectile. The fin is connected to the support by a rod (8) that lies parallel to the projectile's axis in the launch position and perpendicular to it when deployed. The rod can also be made to rotate relative to the support as it is deployed, with the rotation controlled by a drive, and it can be moved lengthwise by a head (9) interacting with a cam surface (14).
机译:用于在发射位置和弹道位置之间展开弹丸(1)的鳍片的机构(2)包括鳍片支撑件(5),该鳍片支撑件(5)绕垂直于弹丸的纵向轴线(4)的轴线(7)枢转。散热片通过杆(8)连接到支撑,杆在发射位置平行于弹丸的轴线,展开时垂直于弹丸的轴线。当杆被展开时,杆也可以相对于支撑件旋转,其中旋转由驱动器控制,并且杆可以由与凸轮表面(14)相互作用的头部(9)沿长度方向移动。

著录项

  • 公开/公告号FR2860577A1

    专利类型

  • 公开/公告日2005-04-08

    原文格式PDF

  • 申请/专利权人 GIAT INDUSTRIES;

    申请/专利号FR20030011642

  • 发明设计人 TROUILLOT CHRISTIAN;

    申请日2003-10-06

  • 分类号F42B10/14;

  • 国家 FR

  • 入库时间 2022-08-21 21:58:22

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