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    • 92. 发明授权
    • ROTOR MIT GESPALTENEM ROTORBLATT
    • EP1196696B1
    • 2003-05-07
    • EP00945889.4
    • 2000-07-06
    • Bannasch, Rudolf
    • Bannasch, Rudolf
    • F16D1/00
    • F01D5/141B63H1/26B63H1/265B63H3/00B64C11/16B64C27/00F03D1/0608F04D29/242Y02E10/721Y02T50/673
    • The invention relates to a rotor (1) through which a fluid flows in a main direction of flow (H) and which is provided with at least one rotor blade (4), said rotor blade being arranged in such a way that it can rotate about a rotor axis. The rotor blade (4) extends away from the axis of rotation (2), into the fluid, at least in sections. The rotation (D) of the rotor blade (4) about the axis of rotation (2) in a predetermined direction of rotation produces a propulsive thrust in the opposite direction to the main direction of flow, or a torque is produced about the axis of rotation as a result of the flow. The aim of the invention is to reduce the trailed tip vortex at the end of the rotor blades of rotors of this type and therefore to reduce the fluidic losses and flow noise. To this end, the rotor blade (4) extends in at least two partial blades (5, 6) at a set distance from the axis of rotation and forms a loop. One partial blade (5) extends in the direction of rotation (D) in relation to the rotor blade, at least in one area close to the rotor blade. The other partial blade extends in the opposite direction to the direction of rotation (D) in relation to the rotor blade (4), at least in one area close to the rotor blade (4). The two partial blades (5, 6) are interconnected in one piece at their ends so that they encompass a loop surface (12) through which the fluid flows, said loop surface extending essentially crosswise to the main direction of flow.
    • 转子,其中流体沿主流动方向流动,设置有至少一个转子叶片,所述转子叶片布置成围绕转子轴线旋转。 转子叶片从旋转轴线延伸到现场。 为了减小转子叶片端部的尾端涡流,流体损失和流动噪声,转子叶片在距旋转轴线一定距离处的至少两个局部叶片中分裂,形成一个回路。 一个部分叶片相对于转子叶片在旋转方向上延伸。 另一部分叶片沿着与转子叶片的旋转方向相反的方向延伸。 两个部分叶片在其端部以一体的方式相互连接,以包围基本上横向于主流动方向延伸的环表面,流体流过该环形表面。
    • 97. 发明申请
    • DEVICE FOR PREVENTING A SHAFT ROTATION
    • 用于防止轴转动的装置
    • US20140291079A1
    • 2014-10-02
    • US14127587
    • 2011-06-29
    • Massimiliano Bianchi
    • Massimiliano Bianchi
    • B63H23/35B63H3/00
    • B63H23/35B63H3/00F16D49/16F16D2065/024F16D2127/002
    • A device for preventing and/or stopping rotation of a shaft coupled to a motor, of the type having a first fixed element with respect to this shaft, and a moving element, and means to constrain the moving element to the shaft in such a manner as to rotate integrally with this shaft and at the same time be able to move between a position of friction contact with the fixed element, to allow stopping of the shaft, and a position of disengagement from this fixed element, to allow release of the shaft is disclosed. The device advantageously provides that the means to constrain the moving element to the shaft include a link for movement of the moving element along a direction having a radial component with respect to the shaft.
    • 用于防止和/或停止联接到电动机的轴的旋转装置,该电动机具有相对于该轴的第一固定元件和移动元件,以及以这种方式将移动元件限制到轴的装置 与该轴一体地旋转,同时能够在与固定元件摩擦接触的位置之间移动,以允许轴的停止以及从该固定元件脱离的位置,以允许轴的释放 被披露。 该装置有利地提供将移动元件约束到轴的装置包括用于沿着具有相对于轴的径向分量的方向移动移动元件的连杆。
    • 98. 发明申请
    • HUB FIN DEVICE
    • HUB FIN设备
    • US20110182747A1
    • 2011-07-28
    • US13122167
    • 2009-09-10
    • Walter S. Gearhart
    • Walter S. Gearhart
    • B63H1/28
    • B63H1/28B63H1/26B63H3/00
    • The present invention discloses a hub fin device for improving the efficiency of a propeller. The hub fin device can include a propeller having a hub and a plurality of propeller blades that extend radially outward from the hub. Each of the plurality of propeller blades has a trailing edge region. A fin can also be included and located in the trailing edge region of at least one of the plurality of propeller blades. The fin extends radially outward from the hub and reduces or eliminates a hub vortex that is normally present during operation of the propeller.
    • 本发明公开了一种用于提高螺旋桨效率的轮毂翅片装置。 轮毂翅片装置可以包括具有毂的螺旋桨和从轮毂径向向外延伸的多个螺旋桨叶片。 多个螺旋桨叶片中的每一个具有后缘区域。 还可以包括翅片并且位于多个螺旋桨叶片中的至少一个的后缘区域中。 翅片从轮毂径向向外延伸并且减少或消除了在螺旋桨操作期间通常存在的轮毂涡流。