首页> 外国专利> Steerable projectile with a rotatable nose cone having a flat formation extending off-axis from the tip of the nose

Steerable projectile with a rotatable nose cone having a flat formation extending off-axis from the tip of the nose

机译:具有可旋转鼻锥的可控弹丸,鼻锥具有从鼻尖偏轴延伸的平坦结构

摘要

A steerable bullet 30 comprises a cylindrical body portion 32 and a nose portion 34. The body 32 and nose 34 are substantially coaxially arranged and rotatable relative to one another about their co-axis. The nose 34 further comprises an asymmetric formation 36 operable to enable the bullet 30 to be subjected to off-axis drag during flight. The nose 34 may be ellipsoidal in profile, with a flat formation extending off-axis from the tip of the nose. In use, the bullet 30, on expulsion from a gun barrel, will rotate about its elongate axis. The nose 34 may counter rotate relative to the body 32 during flight by means of DC motor (46,Fig.4). The nose may thus be rendered stationary with respect to the ground such that the asymmetric formation 36 can impart a steering force onto the bullet 30. Rotation of the nose 34 may be controlled by control electronics (42,Fig.4) which may act on information received from an optical detection system 40 and a laser guidance means.
机译:可操纵子弹30包括圆柱形主体部分32和鼻状部分34。主体32和鼻状部分34基本上同轴布置并且可绕它们的同轴线相对于彼此旋转。机头34还包括非对称结构36,该非对称结构36可操作以使子弹30在飞行过程中受到离轴阻力。鼻部34的轮廓可以是椭圆形的,具有从鼻部的尖端离轴延伸的平坦结构。在使用中,子弹30从枪管中排出后,将绕其细长轴旋转。机头34可以在飞行过程中通过DC电动机(图4,46)相对于主体32反向旋转。因此,可以使机头相对于地面静止,从而非对称结构36可以将转向力施加到子弹30上。机头34的旋转可以由控制电子设备(图4中的42)控制,该电子设备可以作用在机头上。从光学检测系统40和激光引导装置接收的信息。

著录项

  • 公开/公告号GB2458332A

    专利类型

  • 公开/公告日2009-09-16

    原文格式PDF

  • 申请/专利权人 THALES HOLDINGS UK PLC;

    申请/专利号GB20080004951

  • 发明设计人 PADDY MALLON;

    申请日2008-03-13

  • 分类号F42B10/62;F41G7/22;

  • 国家 GB

  • 入库时间 2022-08-21 19:06:33

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