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    • 1. 发明申请
    • ROTARY-WING VEHICLE AND SYSTEM
    • 旋翼式车辆和系统
    • WO2017165039A2
    • 2017-09-28
    • PCT/US2017/018653
    • 2017-02-21
    • GEOSCOUT, INC.HAUER, IstvanBLANK, CyrilVAITSES, Allan
    • HAUER, IstvanBLANK, CyrilVAITSES, Allan
    • B62B19/04B62D65/02
    • B62B19/04B62D65/02B62K13/00B62M2027/021B62M2027/025
    • An apparatus comprising a body defining a first vertical axis, two or more frame members each having a longitudinal axis and having an inner-end and an outer- end connected to the body at the inner-end and where a first horizontal geometrical plane is generally coincident with the longitudinal axis of each of the two or more frame members and where the first horizontal geometrical plane is generally orthogonal to the first vertical axis, two or more rotary-wings each comprising one or more blades whose rotation defines a first rotational axis which is configurable to be nearly parallel with the first vertical axis and comprising a second rotational axis which is configurable to be approximately parallel first horizontal geometrical plane where a first of the two or more rotary-wings having a blade-inner-end and a first blade-outer-end rotatably connected by its blade-inner-end to a first transmission is disposed substantially on the outer-end of a first of the two or more frame members, a second of the two or more rotary-wings having a blade-inner-end and a blade-outer-end rotatably connected by its blade-inner-end to a second transmission is disposed substantially on the outer-end of a second of the two or more frame members, where each of the first rotational axes is disposed on the opposite side of plane which is coincident with the first vertical axis, where the direction of rotation of a first of the two or more rotary-wings about its first rotational axis is opposite of that of the second of the two or more rotary-wings about its first rotational axis, and, where the rotational disk defined by the rotation of the blade-outer- end of the first of the two or more rotary-wings is at least partially coincident with rotational disk defined by the rotation of the blade-outer-end of the second of the two or more rotary-wings.
    • 一种设备,其包括限定第一竖直轴线的主体,两个或更多个框架构件,每个框架构件均具有纵向轴线并且具有在内端处连接到主体的内端和外端以及 其中第一水平几何平面通常与两个或更多个框架构件中的每一个的纵向轴线重合,并且其中第一水平几何平面大致垂直于第一竖直轴线,两个或更多个旋转翼,每个旋转翼包括一个或更多个叶片 其旋转限定第一旋转轴线,该第一旋转轴线可配置成与第一垂直轴线几乎平行并且包括第二旋转轴线,该第二旋转轴线可配置为近似平行的第一水平几何平面,其中两个或更多个旋转翼中的第一旋翼具有叶片 通过其刀片内端可旋转地连接到第一变速器的第一刀片外端和第一刀片外端大致设置在两个或更多个第一传动装置中的第一个的外端上 所述两个或更多个旋转翼中的第二个旋转翼具有通过其叶片内端可旋转地连接到第二变速器的叶片内端和叶片外端, 所述两个或更多个框架构件中的第二个,其中每个所述第一旋转轴线设置在与所述第一竖直轴线重合的平面的相对侧上,其中所述两个或更多个旋转翼板中的第一个的旋转方向围绕 其第一旋转轴线与两个或更多个旋转翼中的第二旋转翼的第一旋转轴线围绕其第一旋转轴线的旋转轴线相反,并且在旋转盘由两个或更多个中的第一个的叶片外端 旋转翼至少部分地与由两个或更多个旋转翼中的第二个的叶片外端的旋转限定的旋转盘重合。
    • 2. 发明申请
    • ROTARY-WING VEHICLE AND SYSTEM
    • WO2017165039A9
    • 2017-09-28
    • PCT/US2017/018653
    • 2017-02-21
    • GEOSCOUT, INC.HAUER, IstvanBLANK, CyrilVAITSES, Allan
    • HAUER, IstvanBLANK, CyrilVAITSES, Allan
    • B62B19/04B62D65/02
    • An apparatus comprising a body defining a first vertical axis, two or more frame members each having a longitudinal axis and having an inner-end and an outer- end connected to the body at the inner-end and where a first horizontal geometrical plane is generally coincident with the longitudinal axis of each of the two or more frame members and where the first horizontal geometrical plane is generally orthogonal to the first vertical axis, two or more rotary-wings each comprising one or more blades whose rotation defines a first rotational axis which is configurable to be nearly parallel with the first vertical axis and comprising a second rotational axis which is configurable to be approximately parallel first horizontal geometrical plane where a first of the two or more rotary-wings having a blade-inner-end and a first blade-outer-end rotatably connected by its blade-inner-end to a first transmission is disposed substantially on the outer-end of a first of the two or more frame members, a second of the two or more rotary-wings having a blade-inner-end and a blade-outer-end rotatably connected by its blade-inner-end to a second transmission is disposed substantially on the outer-end of a second of the two or more frame members, where each of the first rotational axes is disposed on the opposite side of plane which is coincident with the first vertical axis, where the direction of rotation of a first of the two or more rotary-wings about its first rotational axis is opposite of that of the second of the two or more rotary-wings about its first rotational axis, and, where the rotational disk defined by the rotation of the blade-outer- end of the first of the two or more rotary-wings is at least partially coincident with rotational disk defined by the rotation of the blade-outer-end of the second of the two or more rotary-wings.