NAUTICAL PROPULSION SYSTEM FOR SURFACE AND/OR UNDERWATER NAVIGATION
    1.
    发明申请
    NAUTICAL PROPULSION SYSTEM FOR SURFACE AND/OR UNDERWATER NAVIGATION 审中-公开
    用于表面和/或水下导航的NAUTICAL推进系统

    公开(公告)号:WO2008017916A3

    公开(公告)日:2008-04-17

    申请号:PCT/IB2007002216

    申请日:2007-08-02

    CPC classification number: B63H11/02 B63H1/30 B63H11/04

    Abstract: The nautical propulsion system apparatus for surface and/or underwater navigation comprises a propulsion system body (101), a unit (1) for feeding a delivery or primary flow to the propulsion system body (101); the feed unit (1) comprising an internal combustion engine (2) and a pump (3) driven by the internal combustion engine (2).

    Abstract translation: 用于表面和/或水下导航的航海推进系统装置包括推进系统主体(101),用于将输送或主流供给到推进系统主体(101)的单元(1); 所述进料单元(1)包括内燃机(2)和由所述内燃机(2)驱动的泵(3)。

    ROTOR BLADE WITH AERODYNAMIC FLOW STATIC DIVERTER, IN PARTICULAR BLADE FOR VERTICAL AXIS AEOLIC ROTOR, AND VERTICAL AXIS AEOLIC ROTOR WITH STATIC FLOW DIVERTERS
    2.
    发明申请
    ROTOR BLADE WITH AERODYNAMIC FLOW STATIC DIVERTER, IN PARTICULAR BLADE FOR VERTICAL AXIS AEOLIC ROTOR, AND VERTICAL AXIS AEOLIC ROTOR WITH STATIC FLOW DIVERTERS 审中-公开
    具有空气流动静力分流器的转子叶片,用于垂直轴非线性转子的特定叶片,以及具有静态流量的垂直轴非线性转子

    公开(公告)号:WO2010125599A2

    公开(公告)日:2010-11-04

    申请号:PCT/IT2010000177

    申请日:2010-04-23

    Abstract: The present invention relates to a rotor (3) blade (2) with aerodynamic flow static diverter (1), in particular blade (2) for vertical axis aeolic rotor (3), characterised in that said aerodynamic flow static diverter (1) is fixedly coupled with said rotor (3) blade (2), said diverter (1) being positioned inside with respect to said rotor (3), close to the blade (2) leading edge, and having an aerodynamic shape extending substantially parallel with respect to the profile portion of said blade (2) corresponding, and faced toward, the same diverter (1).

    Abstract translation: 本发明涉及一种具有空气动力学流动静态分流器(1)的转子(3)叶片(2),特别是涉及用于垂直轴线轴向转子(3)的叶片(2),其特征在于,所述空气动力学流动静态分流器(1) 与所述转子(3)叶片(2)固定地联接,所述转向器(1)相对于所述转子(3)位于所述转子(3)的内部,靠近所述叶片(2)的前缘,并且具有基本上平行延伸的空气动力学形状 到所述刀片(2)的与所述相同转向器(1)相对应并面向所述刀片(2)的轮廓部分。

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