Hydropulse underwater propulsion system
    8.
    发明授权
    Hydropulse underwater propulsion system 失效
    水下水下推进系统

    公开(公告)号:US4341173A

    公开(公告)日:1982-07-27

    申请号:US126781

    申请日:1980-03-03

    CPC分类号: F42B19/26 B63H11/12

    摘要: A propulsion motor for an underwater vehicle such as an anti-submarine weapon. The motor includes a propulsion chamber into which water is admitted and then rapidly expelled through an exhaust nozzle, developing thrust to propel the vehicle. Gas generators are used to develop the successive hydropulses to expel the water following each filling of the motor chamber with water. In one particular embodiment of an anti-submarine weapon which is directed through the air to the vicinity of a submarine by a rocket motor, the hydropulse underwater propulsion system can use the same chamber as the rocket motor.

    摘要翻译: 用于水下航行器的推进电机,如反潜武器。 马达包括推进室,水被允许进入该推进室,然后通过排气喷嘴快速排出,产生推力以推动车辆。 气体发生器用于开发连续的水力,以便在每次用水充填电机室后排出水。 在由火箭发动机通过空气引导到潜艇附近的反潜武器的一个特定实施例中,水下脉冲水下推进系统可以使用与火箭发动机相同的腔室。

    Method and apparatus for destroying submarines
    9.
    发明授权
    Method and apparatus for destroying submarines 失效
    破坏子宫的方法和装置

    公开(公告)号:US3853081A

    公开(公告)日:1974-12-10

    申请号:US77023558

    申请日:1958-10-28

    申请人: US NAVY

    摘要: A submarine torpedo tube launched missile type weapon having a water-to-air-to-water flight path, comprising, a covered rocket motor wherein the rocket motor cover is explosively released by explosive bolt devices subsequent to launching and during an initial portion of water travel flight. The rocket propelled weapon incorporates electrically controlled vanes for water guidance by influence over the exhaust discharge of the rocket motor together with separation means for severance of the rocket motor portion from the missile during air travel and guidance system controlled aerodynamic control surfaces for guidance to a predetermined water re-entry point.

    摘要翻译: 潜艇鱼雷管发射具有水对空对水飞行路径的导弹型武器,包括覆盖的火箭发动机,其中火箭发动机盖在发射之后和在初始部分的水中爆炸性地释放 旅行飞行 火箭推进武器通过影响火箭发动机排气排放的电动控制叶片,并附有分离装置,用于在空中行驶期间将火箭发动机部分与导弹分开,并将导向系统控制的空气动力学控制表面引导到预定的 水再入点。