Sub-combat unit
    2.
    发明授权
    Sub-combat unit 失效
    副作战部队

    公开(公告)号:US5280752A

    公开(公告)日:1994-01-25

    申请号:US957488

    申请日:1992-10-07

    IPC分类号: F42B10/50 F42B10/16

    CPC分类号: F42B10/50

    摘要: The invention relates to a sub-combat unit which is disposed to be separated from a flying body, for example a carrier shell or the like, over a target area, the sub-combat unit comprising a warhead (4), a target detector (5) and two diametrically located carrier surfaces (1, 2) which impart to the sub-combat unit a rotation for scanning the target area in a helical pattern during the fall of the sub-combat unit down towards the target area, and both of the carrier surfaces (1, 2) being pivotally disposed from a collapsed position to an opened position where both of the carrier surfaces form a retarding area for the fall velocity of the sub-combat unit. The sub-combat unit is designed such that the relationship between the largest main inertia moment and the other main inertia moments of the sub-combat unit lies within the range of between 1.05 and 1.15. Hereby, the direction of the axis of rotation of the sub-combat unit will, during a transitional phase, be deflected and assume an almost vertical direction, at the same time as pendulum movements in the axis are damped out.

    摘要翻译: 本发明涉及一种副作战单元,该副作战单元设置成与目标区域上的诸如载体壳等的飞行体分离,所述副作战单元包括弹头(4),目标探测器( 5)和两个径向定位的载体表面(1,2),其在副作战单元的坠落期间朝向目标区域向副作战单元施加旋转,用于以螺旋图案扫描目标区域,并且 所述载体表面(1,2)从折叠位置枢转地设置到打开位置,在所述打开位置,两个所述载体表面形成用于所述副作战单元的下落速度的延迟区域。 副作战单位的设计使得副作战部队的最大主惯性力矩与其他主惯性力矩的关系在1.05〜1.15之间。 因此,副作战单元的旋转轴线的方向在过渡阶段期间将被偏转并呈现几乎垂直的方向,同时摆动轴上的摆动运动被减弱。

    Sub-combat unit
    3.
    发明授权
    Sub-combat unit 失效
    副作战部队

    公开(公告)号:US5282422A

    公开(公告)日:1994-02-01

    申请号:US957487

    申请日:1992-10-07

    IPC分类号: B64C9/32 B64D19/02 F42B10/50

    CPC分类号: F42B10/50

    摘要: A sub-combat unit to be separated from a flying body, comprises a warhead, a target detector and two diametrically disposed carrier surfaces designed and arranged to impart to the sub-combat unit a rotation for scanning of the target area in a helical pattern during the fall of the sub-combat unit down towards the target area. The two carrier surfaces are pivotable between a closed position and an opened position in which the two carrier surfaces form a retarding area for controlling the fall velocity of the sub-combat unit and a flow influencing means is provided at at least one of the two carrier surfaces for creating a turbulent area immediately above the carrier surface for completely relieving the carrier surfaces even for large differences in the direction of the impinging wind.

    摘要翻译: 与飞行体分离的副作战单元包括弹头,目标探测器和设计和布置的两个径向设置的载体表面,以在副作战单元中施加旋转,以在螺旋图案期间扫描目标区域 副作战部队的下降朝向目标地区。 两个载体表面可以在闭合位置和打开位置之间枢转,在该位置中,两个载体表面形成用于控制副作战单元的下落速度的延迟区域,并且流动影响装置设置在两个载体 用于在载体表面正上方产生湍流区域的表面,以便即使在冲击风的方向上存在很大的差异也能完全消除载体表面。