STAND-OFF DELIVERY OF UNMANNED UNDERWATER VEHICLES
    1.
    发明申请
    STAND-OFF DELIVERY OF UNMANNED UNDERWATER VEHICLES 审中-公开
    未经规定的水下车辆的交付

    公开(公告)号:WO2015147970A1

    公开(公告)日:2015-10-01

    申请号:PCT/US2015/011603

    申请日:2015-01-15

    Inventor: STOWERS, Kyle

    Abstract: A projectile (100) that includes a guidance kit (102,103) that directs the projectile in flight. The projectile further includes a shell and a hollow nose cone (106). The shell mates with the guidance kit and the nose cone couples with the shell. The nose cone includes an interior surface configured to house a UUV (202). The projectile further includes a controller (108) that identifies a condition for deploying the UUV in flight, and detaches the nose cone from the shell in response to determining that the condition is satisfied.

    Abstract translation: 射弹(100),其中包括指挥飞行员的指导工具(102,103)。 射弹还包括壳体和中空鼻锥体(106)。 外壳与指导套件配合,鼻锥与外壳配合。 鼻锥包括被配置为容纳UUV(202)的内表面。 弹丸还包括识别用于在飞行中部署UUV的状况的控制器(108),并且响应于确定满足条件而将鼻锥从壳体分离。

    SUPERCAVITATING UNDERWATER PROJECTILE
    3.
    发明申请
    SUPERCAVITATING UNDERWATER PROJECTILE 审中-公开
    超级水下项目

    公开(公告)号:WO02068896A2

    公开(公告)日:2002-09-06

    申请号:PCT/US0132639

    申请日:2001-10-25

    CPC classification number: F42B10/38 F42B15/20 F42B17/00

    Abstract: A supercavitating underwater projectile (10) adapted to be fired from a gun or the like, comprising a front end or nose portion (12) and a rear end portion (18). An auxilary rocket motor is disposed within the rear end portion (18) of the projectile (10) for providing additional thrust after the projectile (10) has been fired. Vents (28) are disposed within the projectile (10) and are in communication with the rocket motor and the exterior of the projectile (10) for venting some of the combustion gases from the rocket motor to the exterior of the projectile (10) near the nose portion (12) thereof to increase the size of the cavitation bubble formed as the projectile (10) travels through the water and thereby reduce hydrodynamic drag on the projectile.

    Abstract translation: 一种适用于从枪等发射的超空腔水下射弹(10),包括前端或鼻部(12)和后端部分(18)。 辅助火箭发动机设置在射弹(10)的后端部分(18)中,用于在射弹(10)被击发之后提供额外的推力。 通风口(28)设置在射弹(10)内并且与火箭发动机和射弹(10)的外部连通,用于将一些燃烧气体从火箭发动机排放到射弹(10)的外部附近 其鼻部(12)用于增加随着射弹(10)穿过水而形成的空化气泡的尺寸,从而减少射弹上的流体动力学阻力。

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