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    • 3. 发明授权
    • Aerodynamic projectile
    • 气动弹丸
    • US08875634B2
    • 2014-11-04
    • US12317868
    • 2008-12-29
    • Gary E. GibsonMichael A. Varacins
    • Gary E. GibsonMichael A. Varacins
    • F42B12/00F42B10/06F42B12/40
    • F42B10/06F42B12/40
    • An aerodynamic projectile is provided having a shell with an aerodynamic structure and a controlled center of gravity, and which exhibits improved aerodynamics and resulting accuracy, and which is suitable for less lethal uses. The projectile shell has a closed front cavity housing a payload, such as a marking agent, therein. The projectile shell also has an open rear portion to provide access to the open rear cavity, and to decrease the weight of the projectile and appropriately locate the center of gravity. The projectile shell also includes a plurality of fins on a sidewall member to enhance the accuracy of the projectile.
    • 提供了一种具有空气动力学结构和受控重心的外壳的空气动力学抛射体,其具有改善的空气动力学和所得精度,并且适用于较少致命的用途。 抛射体壳体具有封闭的前腔,其中容纳有效载荷,例如标记剂。 抛射体壳体还具有敞开的后部部分,以提供进入开放的后腔,并且减少弹丸的重量并适当地定位重心。 抛射体壳体还包括在侧壁构件上的多个翅片以增强射弹的精度。
    • 4. 发明申请
    • Aerodynamic projectile
    • 气动弹丸
    • US20120199034A1
    • 2012-08-09
    • US12317868
    • 2008-12-29
    • Gary E. GibsonMichael A. Varacins
    • Gary E. GibsonMichael A. Varacins
    • F42B12/40F42B12/72F42B10/04
    • F42B10/06F42B12/40
    • An aerodynamic projectile is provided having a shell with an aerodynamic structure and a controlled center of gravity, and which exhibits improved aerodynamics and resulting accuracy, and which is suitable for less lethal uses. The projectile shell has a closed front cavity housing a payload, such as a marking agent, therein. The projectile shell also has an open rear portion to provide access to the open rear cavity, and to decrease the weight of the projectile and appropriately locate the center of gravity. The projectile shell also includes a plurality of fins on a sidewall member to enhance the accuracy of the projectile.
    • 提供了具有空气动力学结构和受控重心的外壳的空气动力学抛射体,其具有改善的空气动力学和所得精度,并且适用于较少致命的用途。 抛射体壳体具有封闭的前腔,其中容纳有效载荷,例如标记剂。 抛射体壳体还具有敞开的后部部分,以提供进入开放的后腔,并且减少弹丸的重量并适当地定位重心。 抛射体壳体还包括在侧壁构件上的多个翅片以增强射弹的精度。