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    • 1. 发明公开
    • Homing submunition
    • Zielsuchende子弹药。
    • EP0252036A2
    • 1988-01-07
    • EP87850087.5
    • 1987-03-17
    • Aktiebolaget Bofors
    • Persson, Per-OlofAlbrektsson, KjellAxinger, JanFixell, Jan-OlofHyvärinen, Jari
    • F42B12/58F41G7/22
    • F42B30/006F42B10/50F42C13/006
    • The disclosure relates to a submunition disposed to be separated from an aeronautical body, for example a shell carrier canister or the like above a target area, the submunition essentially including a warhead (5), a target detector (6) and a device which imparts to the submunition rotation for scanning the target area in a helical pattern (4) during the fall of the submunition towards the target area. The target detector (6) is pivotally disposed on a carrying shaft (12a) parallel to the line of symmetry (5a) of the warhead in order to permit outward activation of the target detector (6) from a collapsed position where the optical axis of the target detector coincides with the line of symmetry (5a) of the warhead to an activated position where the optical axis of the target detector is parallel with the line of symmetry (5a) of the warhead, so as to permit free scanning vision for the target detector (6) beside the warhead (5).
    • 本公开涉及一种设置成与目标区域上方的航空体例如壳载体罐等分离的子弹药,子弹药基本上包括弹头(5),目标探测器(6)和赋予 以在子弹药向着目标区域坠落期间以螺旋图案(4)扫描目标区域的子弹药旋转。 目标探测器(6)可枢转地设置在平行于弹头的对称线(5a)的承载轴(12a)上,以允许目标探测器(6)从折叠位置向外激活,其中光轴 目标检测器与弹头的对称线(5a)重合到目标检测器的光轴与弹头的对称线(5a)平行的激活位置,以便允许对于弹头的自由扫描视觉 弹头(5)旁边的目标探测器(6)。
    • 2. 发明公开
    • Subwarhead
    • EP0424336A3
    • 1992-02-19
    • EP90850324.6
    • 1990-10-03
    • Aktiebolaget Bofors
    • Axinger, Jan
    • F42B10/50F42B12/04F42B12/58
    • F42B30/006F42B10/50
    • The invention relates to a subwarhead which is arranged to be separated from a missile, for example a carrier shell or the like, over a target area. The subwarhead comprises an active part, a target detector (2) and an aerofoil (3), both the target detector (2) and the aerofoil (3) each being pivotably arranged on its own bearing shaft (4, 5) parallel with the line of symmetry of the active part in order to allow pivoting out of target detector (2) and aerofoil (3) from a folded-in position to a folded-out position at the side of the active part in order to allow a controlled movement of scanning of the target area. The target detector (2) and/or the aerofoil (3) are/is provided with one or more displaceably arranged extra aerofoils (7, 8, 9, 10, 13, 14) for the purpose of increasing the braking area of the subwarhead.
    • 本发明涉及一种被布置成与目标区域上的导弹(例如载体外壳等)分开的副偏转头。 所述副臂包括主动部分,目标探测器(2)和翼型件(3),所述目标探测器(2)和翼型件(3)均可枢转地布置在其自己的轴承轴(4,5)上, 为了允许从目标检测器(2)和机翼(3)从活动部分侧面处的折叠位置枢转到折叠位置以允许受控运动 扫描目标区域。 目标探测器(2)和/或机翼(3)设置有一个或多个可移动地布置的额外翼面(7,8,9,10,13,14),用于增加副翼头的制动面积 。
    • 5. 发明公开
    • Subwarhead
    • Subgefechtskopf。
    • EP0424336A2
    • 1991-04-24
    • EP90850324.6
    • 1990-10-03
    • Aktiebolaget Bofors
    • Axinger, Jan
    • F42B10/50F42B12/04F42B12/58
    • F42B30/006F42B10/50
    • The invention relates to a subwarhead which is arranged to be separated from a missile, for example a carrier shell or the like, over a target area. The subwarhead comprises an active part, a target detector (2) and an aerofoil (3), both the target detector (2) and the aerofoil (3) each being pivotably arranged on its own bearing shaft (4, 5) parallel with the line of symmetry of the active part in order to allow pivoting out of target detector (2) and aerofoil (3) from a folded-in position to a folded-out position at the side of the active part in order to allow a controlled movement of scanning of the target area. The target detector (2) and/or the aerofoil (3) are/is provided with one or more displaceably arranged extra aerofoils (7, 8, 9, 10, 13, 14) for the purpose of increasing the braking area of the subwarhead.
    • 本发明涉及一种子导弹,其被布置成在目标区域上与导弹(例如载体壳体等)分离。 副标题包括活动部分,目标检测器(2)和机翼(3),目标检测器(2)和机翼(3)均可枢转地布置在其自身的轴承轴(4,5)上,平行于 有源部分的对称线,以便允许从目标检测器(2)和机翼(3)从折叠位置枢转到活动部分侧面的折叠位置,以允许受控的移动 扫描目标区域。 目标检测器(2)和/或机翼(3)设置有一个或多个可置换排列的额外机翼(7,8,9,10,13,14),以增加副驾驶的制动面积 。