公开(公告)号：US5111553A

公开(公告)日：1992-05-12

申请号：US589851

申请日：1990-09-28

申请人： David Muggeridge ,  William F. Ryan ,  Dieter Haase

发明人： David Muggeridge ,  William F. Ryan ,  Dieter Haase

IPC分类号： F42B10/64

CPC分类号： F42B10/663 ,  F42B10/64

摘要： Flight control apparatus (10) for a cannon-launched anti-tank projectile. A boom that structurally secures four fins (18) and four nozzles (20) to an afterbody (12) of the projectile, and that provides for fluid communication from the afterbody to the nozzles, is provided in the form of an assembly (14) comprising intersecured tubes (22, 24, 26, 28) which define a longitudinal axis (30) of the assembly. The boom assembly (14) considerably reduces the weight and fabrication cost associated with a conventional boom which is provided in the form of an integral multi-channeled cylinder.

摘要翻译： 用于大炮发射的反坦克炮弹的飞行控制装置（10）。 以组件（14）的形式提供结构上将四个翅片（18）和四个喷嘴（20）固定到射弹的后身（12）并且提供从后身体到喷嘴的流体连通的臂， 包括限定组件的纵向轴线（30）的相互连接的管（22,24,26,28）。 起重臂组件（14）显着地减少了以整体式多通道气缸的形式提供的常规起重臂相关联的重量和制造成本。