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Missile stowage and launcher system

机译:导弹积载和发射系统

摘要

A plurality of missiles stowed within and adapted to be launched from a carrier aircraft, are arranged in cone-shaped clusters, that are in turn nested together to achieve a high density payload. The various clusters are independently rotatable about the conical axes so that individual missiles can be selected at random and moved into a launching position. For this purpose each missile cluster is assembled and secured on an annular support, that in turn is rotatably mounted on an annular bearing structure, wherein each cluster support and associated bearing structure have registerable circumferential gaps congruently disposed with a launching port in an exterior wall of the aircraft. Individual missiles of an inner nested cluster are thus movable, by rotating the associated cluster, into registry with the gaps in adjacent clusters and hence with the launching port and are then transversely and outwardly ejected from the cluster and through the port. The conical clustering of the missiles is used to advantage for high density payload delta-wafer shaped missiles, which are arranged in each cluster so that the longitudinal axes of the missiles lie along the slant of the cone pointing toward the cone apex and the aft ends are disposed in a step- wise circular array around the base of the cone.
机译:装在载机中并适合从载机发射的多枚导弹排列成圆锥形,然后嵌套在一起以实现高密度的有效载荷。各个簇可围绕圆锥轴独立旋转,因此可以随机选择单个导弹并将其移到发射位置。为此,将每个导弹组组装并固定在环形支架上,然后将其可旋转地安装在环形轴承结构上,其中,每个导弹组支架和相关的轴承结构具有可对准的周向间隙,该周向间隙与发射端口一致地布置在导弹的外壁上。飞机。因此,内部嵌套簇的各个导弹可通过旋转关联的簇而移动,与相邻簇中的间隙并因此与发射端口对准,然后从簇中横向向外弹出并通过端口。导弹的圆锥形聚束有利于高密度有效载荷三角晶片形导弹的排列,每个导弹都排列成这样,使得导弹的纵轴沿着圆锥形的斜线指向圆锥形顶点和尾端围绕圆锥体的底部以逐步的圆形阵列布置。

著录项

  • 公开/公告号US4409880A

    专利类型

  • 公开/公告日1983-10-18

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY;

    申请/专利号US19800217242

  • 发明设计人 ROBERT F. FETTERLY;

    申请日1980-12-17

  • 分类号F41F3/06;

  • 国家 US

  • 入库时间 2022-08-22 09:48:28

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