The invention provides a vertical take-off and landing aircraft. In a vertical take-off and landing aircraft (10), a plurality of VTOL rotors (20) are divided into a plurality of groups, each VTOL rotor (20) is included in any one of the groups, and after wings (a front wing (14) and a rear wing (16)) generate lift force, a controller (46) sequentially stops the rotation of the plurality of VTOL rotors (20) in groups. Therefore, deterioration of riding comfort of the VTOL aircraft can be suppressed.
本发明提供一种垂直起降航空器。在垂直起降航空器(10)中,多个VTOL旋翼(20)被分为多个组,每个VTOL旋翼(20)包含于任一个组中,在机翼(前翼(14)、后翼(16))产生升力后,控制器(46)使多个VTOL旋翼(20)的旋转以组为单位依次停止。据此,能够抑制VTOL飞机的乘机舒适感的恶化。
Vertical take-off and landing aircraft
垂直起降航空器
2024-01-30
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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