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    • 3. 发明公开
    • CENTRAL WING PANEL FOR A FLYING VEHICLE AND METHOD OF ITS CONTROL
    • 一种飞行器的中央翼面板及其控制方法
    • EP3204246A1
    • 2017-08-16
    • EP15801514.9
    • 2015-10-08
    • AeroMobil, s.r.o.
    • KLEIN, Stefan
    • B60F5/02B64C3/56B64C37/00
    • B64C3/56B60F5/02B64C37/00Y02T50/14
    • A central wing panel for a hybrid transportation vehicle for ground and air transportation configured to enable transitioning between an air mode and a ground mode. The central wing panel has a front frame section and a rear frame section connected by one or more cross members. The central wing panel is configured to rotate enabling adjustment of an angle of attack of the vehicle. The rear frame section is configured to rotate enabling coupling and uncoupling of the rear frame section from a first wing and a second wing for transitioning between the air mode and the ground mode. The central wing panel is also configured to allow rotation of ailerons and flaps so that they fold over onto the top front portion of the wings.
    • 用于地面和空中运输的混合运输车辆的中央翼板。 中央翼片具有由一个或多个横向构件连接的前框架部分和后框架部分。 中央翼片还可以具有第一竖直轴线和第二竖直轴线,第一竖直轴线和第二竖直轴线定位在前部框架区段的相对端部附近,其中第一翼部构造成围绕第一竖直轴线旋转并且第二翼部构造成围绕第一竖直轴线旋转 第二垂直轴,用于在空气模式和地面模式之间转换。 中央翼片还可以具有第一水平轴线,该第一水平轴线沿着前框架部分的下部基本平行地延伸,其中中央翼片构造成围绕第一水平轴线旋转,从而能够调节车辆的迎角。 中央翼片还可具有沿后部框架部分的下部延伸的第二水平轴线,其中后部框架部分构造成绕第二水平轴线旋转以使后部框架部分能够与第一机翼 以及用于在空气模式和地面模式之间转换的第二机翼。 中央翼片还可以具有沿着翼的后缘延伸的第三水平轴线,从而允许副翼和翼片旋转,使得它们折叠到翼的顶部前部上,从而减小翼的深度。
    • 4. 发明公开
    • A DIRECTIONAL CONTROL SYSTEM AND METHOD FOR A HYBRID AIR AND GROUND TRANSPORTATION VEHICLE
    • 一种混合式空中和地面运输车辆的方向控制系统和方法
    • EP3204245A2
    • 2017-08-16
    • EP15801513.1
    • 2015-10-08
    • Aeromobil S.r.o.
    • KLEIN, Stefan
    • B60F5/02
    • B62D1/16B60F5/02B62D3/02B64C13/0423B64C25/50B64C37/00
    • A directional control system for a hybrid transportation vehicle for ground and air transportation. The vehicle has at least one steerable wheel for use in ground operation, the wheel being connected to a steering mechanism, wings having moveable control surfaces, and a tail having a moveable control surface. The system has a first shaft having a first control input at one end, wherein the first shaft is linked to the steering mechanism and a second shaft that extends through the first shaft and is independently rotatable and slidable with respect to the first shaft. The second shaft has a second control input at one end, a first linkage configured to transmit a rotational movement of the second shaft to control the moveable control surfaces on the wings, and a second linkage configured to transmit an axial movement of the second shaft to control the moveable control surface on the tail.
    • 提供了用于地面和空中运输的混合运输车辆的方向控制系统。 该车辆具有至少一个用于地面操作的可转向车轮,该车轮连接至转向机构,具有可移动控制表面的机翼以及具有至少一个可移动控制表面的尾部。 方向控制系统具有第一轴和第二轴,第一轴在一端具有第一控制输入,其中第一轴连接至转向机构,第二轴延伸穿过第一轴并且可相对于第一轴独立地旋转和滑动。 第二轴在一端处具有第二控制输入,第一连杆被构造成传递第二轴的旋转运动以控制机翼上的可移动控制表面,以及第二连杆,其被配置为将第二轴的轴向移动传递到 控制尾部上的可移动控制表面。
    • 6. 发明公开
    • HYBRID TRANSPORTATION VEHICLE FOR GROUND AND AIR, AND METHOD OF TRANSFORMING SUCH A VEHICLE
    • 混合运输车辆用于陆地和空中和方法取得的运输这些车辆的转型
    • EP2977239A1
    • 2016-01-27
    • EP15184918.9
    • 2012-08-22
    • Aeromobil S.r.o.
    • KLEIN, Stefan
    • B60F5/02B64C37/00B64C3/56
    • B60F5/02B60F5/003B64C3/385B64C3/54B64C3/56B64C25/04B64C25/54B64C37/00B64C2025/003Y02T50/14
    • Hybrid transportation vehicle for ground and air consisting of a body (4), cabin (6), retractable wings (1), chassis and driving unit (8) with switching of the torque transfer between a propeller (9) situated at the rear of the vehicle and driven wheels (5), the vehicle containing reciprocal transformation mechanisms for transformation into an automobile or into an aircraft, where one or two first reciprocal transformation mechanisms for retraction and expansion of the wings (1) from or to a flying position are situated in the middle of the body (4); each first reciprocal transformation mechanism contains a first actuator and a vertical axis (2) for retraction and expansion of the wing (1) by tilting around the vertical axis between a flying position in which the axis of the wing is approximately perpendicular to the longitudinal axis of the vehicle, and a retracted position in which the wing axis is approximately parallel to the longitudinal axis of the vehicle; and two second reciprocal transformation mechanisms for changing the platform outline of the wings, each being situated separately in a wing body (1) and each containing a horizontal axis (3) of the wing and a second actuator, for tilting the rear part of each wing onto the top front part of the wing (1).
    • 用于地面和空气混合动力运输车辆组成的主体(4),机舱(8)与螺旋桨之间的扭矩传递的切换(9)位于后部(6),可伸缩的翼(1),机壳和驱动单元 车辆和从动轮(5),所述车辆包含对汽车或到在飞机上,其中一个或两个:(1)从或向飞行位置翼的收缩和膨胀第一倒数变换机构是倒数变换机制用于转化到 位于所述主体(4)的中间; 每个第一往复变换机构包含一个第一致动器和一个垂直轴(2),用于所述翼(1)由围绕一飞行位置之间的垂直轴线倾斜的收缩和膨胀,其中所述翼的轴线大致垂直于所述纵向轴线 的车辆中,和缩回位置,其中所述翼轴线平行于所述纵向轴线大致车辆的; 和用于改变机翼的平台轮廓2秒倒数变换机构,每个单独的翼体(1)位于和各含有一个水平轴(3)的翼部和第二致动器的,用于倾斜每个的后部 翼走上翼(1)的顶部前部。