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Empennage (tail assembly) having wings which can be unfolded

机译:尾翼可以展开的尾翼(尾翼组件)

摘要

A wing 11, which can be folded in in a space-saving manner, of a missile or projectile 10 consists of two wing leaves 12, 12a which are connected to one another at an acute angle but which are attached to different mountings 17, 17a at their root end. One of the mountings 17a is a hinged fixed mounting, while the second mounting 17 is a hinged sliding guidance mounting. In the folded-up state, the wing leaves 12, 12a are wound up on the circumference of the missile 10 lying directly one above the other, the mountings 17, 17a lying closely adjacent to one another. When the wing 11 is in the unfolded state, the mountings 17, 17a are arranged at a distance from one another, so that the wing leaves 12, 12a are erected in the form of a roof. IMAGE
机译:可以以节省空间的方式折叠的导弹或射弹10的机翼11由两个机翼叶片12、12a组成,它们以锐角相互连接,但分别固定在不同的支架17、17a上在他们的根源。支架17a之一是铰链固定支架,而第二支架17是铰链滑动导向支架。在折叠状态下,翼片12、12a缠绕在导弹10的圆周上,彼此直接位于彼此之上,安装件17、17a彼此紧邻。当机翼11处于展开状态时,安装件17、17a彼此隔开一定距离布置,使得机翼叶片12、12a以屋顶的形式竖立。 <图像>

著录项

  • 公开/公告号DE3533994A1

    专利类型

  • 公开/公告日1986-04-30

    原文格式PDF

  • 申请/专利权人 RHEINMETALL GMBH;

    申请/专利号DE19853533994

  • 发明设计人 BOEDERDIETERDIPL.-ING.;

    申请日1985-09-24

  • 分类号F42B13/32;

  • 国家 DE

  • 入库时间 2022-08-22 07:31:48

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