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    • 1. 发明授权
    • Underwater two phase ramjet engine
    • 水下双相冲压发动机
    • US5692371A
    • 1997-12-02
    • US736115
    • 1996-10-24
    • Hezi VarshayAlon Gany
    • Hezi VarshayAlon Gany
    • B63H11/09B63B1/24B63H11/00B63H11/103B63H11/12
    • B63H11/103B63B1/246B63H11/00B63H11/12
    • An underwater two-phase ramjet engine propulsion unit, including an inlet for receiving a flow of water, compressed gas injector for injecting compressed gas into the flow of water, a mixing chamber for mixing the compressed gas with the flow of water to provide a two-phase flow of working fluid and a nozzle for accelerating the two-phase flow of working fluid so as to generate a two-phase jet. The propulsion unit can be implemented with a fixed geometry or with a variable geometry. The propulsion unit includes a supersonic gas injector as well as a subsonic gas injector. The propulsion unit includes a control system for controlling the compressor, supersonic gas injector, the subsonic gas injector, the geometry of the propulsion unit, and the direction of the thrust vector.
    • 一种水下双相冲压喷气发动机推进装置,包括用于接收水流的入口,用于将压缩气体注入到水流中的压缩气体喷射器,用于将压缩气体与水流混合的混合室,以提供两个 工作流体的相流和用于加速工作流体的两相流的喷嘴,以产生两相射流。 推进单元可以用固定几何形状或可变几何形状实现。 推进单元包括超音速气体喷射器以及亚音速气体喷射器。 推进单元包括用于控制压缩机,超音速气体喷射器,亚音速气体喷射器,推进单元的几何形状和推力矢量的方向的控制系统。
    • 2. 发明授权
    • Underwater two phase ramjet engine
    • 水下双相冲压发动机
    • US5598700A
    • 1997-02-04
    • US268586
    • 1994-06-30
    • Hezi VarshayAlon Gany
    • Hezi VarshayAlon Gany
    • B63H11/09B63B1/24B63H11/00B63H11/103B63H11/12
    • B63H11/103B63B1/246B63H11/00B63H11/12
    • An underwater two-phase ramjet engine propulsion unit, includes an inlet for receiving a flow of water, compressed gas injector for injecting compressed gas into the flow of water, a mixing chamber for mixing the compressed gas with the flow of water to provide a two-phase flow of working fluid and a nozzle for accelerating the two-phase flow of working fluid so as to generate a two-phase jet. The propulsion unit can be implemented with a fixed geometry or with a variable geometry. The propulsion unit includes a supersonic gas injector as well as a subsonic gas injector. The propulsion unit includes a control system the controlling the compressor, supersonic gas injector, the subsonic gas injector, the geometry of the propulsion unit, and the direction of the thrust vector.
    • 水下双相冲压式发动机推进装置,包括用于接收水流的入口,用于将压缩气体注入到水流中的压缩气体喷射器,用于将压缩气体与水流混合的混合室,以提供两个 工作流体的相流和用于加速工作流体的两相流的喷嘴,以产生两相射流。 推进单元可以用固定几何形状或可变几何形状实现。 推进单元包括超音速气体喷射器以及亚音速气体喷射器。 推进单元包括控制压缩机,超音速气体喷射器,亚音速气体喷射器,推进单元的几何形状和推力矢量的方向的控制系统。
    • 7. 发明授权
    • Underwater pulse jet motor
    • 水下脉冲喷射马达
    • US3872665A
    • 1975-03-25
    • US43560374
    • 1974-01-22
    • MOTEUR MODERNE LE
    • JARRY PHILIPPE
    • B63H11/09B63H11/12B63H11/02
    • B63H11/12
    • An underwater pulse jet motor comprises a stator and, within the stator, a rotor which has axially extending ducts at its periphery. The stator includes a closing segment which closes off the forward ends of the ducts successively as they pass it during rotation of the rotor. Gas under pressure is injected into the ducts through an injection passage formed in the stator in alignment with the closing segment, injection openings in the ducts coming successively into register with the injection passage for this purpose. In order to form a buffer of water in each duct between the closing segment and the injection opening, the opening is disposed downstream of the upstream end of the duct, and an efficient seal against the escape of the gas between the upstream ends of the ducts and the closing segment is thus achieved. The buffer water can be arranged to flow at a restricted rate downstream into the central passage to provide an ejector effect to increase the water flow through the central passage at low forward speeds of the motor.
    • 水下脉冲喷射马达包括定子,并且在定子内部具有在其周边处具有轴向延伸的管道的转子。 定子包括一个闭合段,当转子旋转时它们通过管道的前端而连续关闭。 在压力下的气体通过形成在定子中的与注射段对准的注射通道注入管道中,为此目的,管道中的注射开口依次与注射通道对齐。 为了在闭合段和注射开口之间的每个管道中形成水的缓冲液,开口设置在管道的上游端的下游,并且有效的密封抵抗气体在管道的上游端之间的逸出 从而实现闭合段。 缓冲水可以布置成以限制的速率在中心通道下游流动,以提供喷射器效果,以在马达的低速前进速度增加通过中心通道的水流。
    • 8. 发明授权
    • Marine propulsion system
    • 船舶推进系统
    • US08545279B2
    • 2013-10-01
    • US13304185
    • 2011-11-23
    • Codrin-Gruie CantemirGildo Pallanca
    • Codrin-Gruie CantemirGildo Pallanca
    • B63H11/14B63H11/00B63H11/09B63H11/103
    • B63H11/14B63H21/38B63H2011/002
    • A marine propulsion system comprising, in one embodiment: a fuel-filled tank; an air compressor that generates compressed air; an engine that receives fuel from the tank, wherein the air compressor is powered by the engine; and at least one hot gas generator that receives compressed air from the air compressor, the hot gas generator comprising: (a) a combustion chamber having an inlet and an outlet, the compressed air injected into the combustion chamber at the inlet, the combustion chamber adapted to produce hot gas; (b) an injection nozzle that receives fuel from the tank, the injection nozzle positioned proximate to the inlet of the combustion chamber, the injection nozzle adapted to spray the fuel into the combustion chamber; and (c) an exhaust Coanda nozzle positioned at the outlet of the combustion chamber through which the hot gas produced in the combustion chamber is discharged from the hot gas generator.
    • 一种船舶推进系统,在一个实施例中包括燃料填充的罐; 产生压缩空气的空气压缩机; 从所述罐接收燃料的发动机,其中所述空气压缩机由所述发动机供电; 以及至少一个从空气压缩机接收压缩空气的热气发生器,所述热气发生器包括:(a)具有入口和出口的燃烧室,在入口处喷射到燃烧室中的压缩空气,燃烧室 适应生产热气体; (b)喷嘴,其从所述罐接收燃料,所述喷嘴位于所述燃烧室的入口附近,所述喷嘴适于将所述燃料喷射到所述燃烧室中; 和(c)位于燃烧室出口处的排气柯恩达喷嘴,燃烧室中产生的热气体通过燃烧室从热气体发生器排出。