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    • 11. 发明申请
    • BISTABLE PITCH PROPELLER SYSTEM WITH UNIDIRECTIONAL PROPELLER ROTATION
    • 具有单向螺旋桨旋转的双柔性螺旋桨系统
    • WO2018026398A1
    • 2018-02-08
    • PCT/US2017/022332
    • 2017-03-14
    • KITTY HAWK CORPORATION
    • VANDER LIND, DamonREICHERT, Todd
    • B64C11/30B64C11/20B64C11/32B64C11/44
    • A propeller includes a blade free to rotate about a longitudinal axis of the blade. The propeller also includes a mechanical stop positioned to engage mechanically a first portion of the blade and/or a first structure coupled mechanically to the blade when the blade is in a first position. The propeller also includes a magnetic stop positioned to engage magnetically a second portion of the blade and/or a second structure coupled mechanically to the blade when the blade is in a second position. The blade rotates to the first position against the mechanical stop when the propeller is rotated at a first rotational speed and the blade rotates to the second position against the magnetic stop when the propeller is rotated at a second rotational speed in a same direction as when the blade is in the first position.
    • 螺旋桨包括刀片,该刀片围绕刀片的纵向轴线自由旋转。 螺旋桨还包括机械挡块,该机械挡块被定位成机械地接合叶片的第一部分和/或当叶片处于第一位置时机械地联接到叶片的第一结构。 螺旋桨还包括磁性止动件,磁性止动件定位成当叶片处于第二位置时磁力地接合叶片的第二部分和/或机械地联接至叶片的第二结构。 当螺旋桨以第一旋转速度旋转时,叶片抵抗机械止动件旋转到第一位置,并且当螺旋桨以与第二旋转速度相同的方向旋转时,叶片抵抗磁性止动件旋转到第二位置 刀片处于第一位。
    • 18. 发明申请
    • VENTILATED ROTOR MOUNTING BOOM FOR PERSONAL AIRCRAFT
    • 用于个人飞机的通风转子安装臂
    • WO2018075413A1
    • 2018-04-26
    • PCT/US2017/056818
    • 2017-10-16
    • KITTY HAWK CORPORATION
    • TIGHE, James, JosephLONG, Geoffrey, AlanTZARNOTZKY, Uri
    • B64C29/00B64D27/24B64D27/26B64D33/10
    • Described embodiments provide a rotor mounting boom assembly for a personal aircraft. The rotor mounting boom assembly includes a rotor mounting boom releasably attachable to a wing of the personal aircraft, one or more vertical lift rotors, and one or more rotor controller assemblies. Controller assemblies for each rotor are positioned on the rotor mounting booms such that downwash from the rotor causes increased airflow across the controller assembly to cool the controller assembly components. A rotor controller enclosure includes an air inlet and an air outlet to allow airflow through the enclosure to cool the controller components. The air inlet is positioned relative to the path of the rotor blades such that the downwash from the rotor that flows into the air inlet is maximized. The structure of the enclosure includes features for increasing the airflow through the enclosure.
    • 所描述的实施例提供了用于个人飞机的转子安装悬臂组件。 该转子安装吊杆组件包括可拆卸地连接到该个人飞机的机翼的转子安装吊杆,一个或多个竖直提升转子以及一个或多个转子控制器组件。 每个转子的控制器组件定位在转子安装吊杆上,使得来自转子的下洗气导致增加通过控制器组件的气流以冷却控制器组件组件。 转子控制器外壳包括进气口和出气口,以允许气流通过外壳来冷却控制器组件。 空气入口相对于转子叶片的路径定位成使得流​​入空气入口的来自转子的下洗气最大化。 外壳的结构包括增加通过外壳的气流的功能。