The invention relates to a hybrid drone for transporting or delivering objects (124), comprising: at least one first wing (102) having an airfoil; at least one first longitudinal drive unit (104) and one second longitudinal drive unit (104), the first longitudinal drive unit (104) and the second longitudinal drive unit (104) being arranged on the at least one wing (102); an object holding device (110) which is arranged between the first longitudinal drive unit (104) and the second longitudinal drive unit (104) on the top or on the bottom and which is designed to hold an object (124); and a control unit designed to control the hybrid drone, more particularly the drive unit, on the basis of the control signal. The hybrid drone also has at least one first vertical drive unit (105). The first vertical drive unit (105) is oriented or pivotably oriented in such a way that a thrust force that can be generated by means of the vertical drive unit (105) acts substantially orthogonally to the longitudinal direction (106) and substantially parallel to a vertical axis (116) of the hybrid drone, and the first vertical drive unit (105) is arranged with a defined lever distance with respect to the center of gravity of the hybrid drone. The pitch angle of the hybrid drone can be adjusted during flight by means of a first vertical drive unit (105). The invention also relates to at least one holding means assigned to the underside in the front region of said hybrid drone, which holding means is designed to releasably position, more particularly hang, the hybrid drone on a vertical receiving structure terminating in an upward direction.
本发明涉及一种用于运输或投递物体(124)的混合动力无人机,该混合动力无人机包括:具有翼面的至少一个第一机翼(102);至少一个第一纵向驱动单元(104)和一个第二纵向驱动单元(104),第一纵向驱动单元(104)和第二纵向驱动单元(104)被设置在至少一个机翼(102)上;物体保持装置(110),该物体保持装置上面上或下面上被设置在第一纵向驱动单元(104)与第二纵向驱动单元(104)之间,并且被设计成保持物体(124);以及控制单元,该控制单元被设计成基于控制信号来控制混合动力无人机,更特别地控制驱动单元。该混合动力无人机还具有至少一个第一竖直驱动单元(105)。第一竖直驱动单元(105)以这样的方式定向或者可枢转定向,即,可以借助于竖直驱动单元(105)生成的推力基本上正交于纵向方向(106)并且基本上平行于混合动力无人机的竖直轴线(116)起作用,并且第一竖直驱动单元(105)被设置为相对于混合动力无人机的重心具有限定杠杆距离。在飞行期间可以借助于第一竖直驱动单元(105)来调整混合动力无人机的俯仰角。本发明还涉及至少一个保持部件,该保持部件被指派给所述混合动力无人机的前部区域中的底面,该保持部件被设计成使混合动力无人机可释放地位于、更特别地挂到沿向上方向终止的竖直接收结构上。
Hybrid drone for landing on vertical structure
用于降落在竖直结构上的混合动力无人机
2023-04-04
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
HYBRID VERTICAL TAKE-OFF AND LANDING (VTOL) FIXED-WING DRONE
European Patent Office | 2022
|