The invention discloses a self-tilting vertical take-off and landing aircraft and a take-off and landing method. The self-tilting vertical take-off and landing aircraft comprises an aircraft body, a first set of undercarriages and a second set of undercarriages, and the first set of undercarriages and the second set of undercarriages are distributed in the length direction of the aircraft; the height of the first set of undercarriage is larger than that of the second set of undercarriage, the first set of undercarriage and the second set of undercarriage at least comprise buffer columns and airplane wheels, the buffer columns are arranged on the aircraft body, the ends, away from the aircraft body, of the buffer columns are arranged on the airplane wheels, and the second set of undercarriage further comprises locking mechanisms arranged on the airplane wheels. The height of the first group of undercarriages is greater than that of the second group of undercarriages, so that the nose part of the aircraft is higher than the tail part of the aircraft, a large stop angle is provided for the aircraft, and a certain height is formed between a front wing propeller and the ground when the aircraft takes off or lands; and the attitude change of the aircraft in taking off or landing is small.
本发明公开一种自倾转垂直起降飞行器、起飞及降落方法,包括飞行器本体,以及第一组起落架和第二组起落架,第一组起落架和第二组起落架沿着飞行器的长度方向分布;第一组起落架的高度大于第二组起落架的高度,第一组起落架和第二组起落架均至少包括缓冲柱和机轮,缓冲柱设在飞行器本体上,缓冲柱远离飞行器本体的一端设有机轮上,第二组起落架还包括设在机轮上的锁止机构。第一组起落架的高度大于第二组起落架的高度,这样可以使飞行器的机头部分高于机尾部分,给飞行器提供了较大停机角,能够使飞行器在起飞或者降落时前翼螺旋桨距离地面有一定的高度,并且使得飞行器起飞离地或降落接地的姿态变化较小。
Self-tilting vertical take-off and landing aircraft and take-off and landing method
一种自倾转垂直起降飞行器、起飞及降落方法
2023-10-24
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
Vertical take-off and landing tilting composite wing aircraft
European Patent Office | 2020
|Tilting vertical take-off and landing multi-rotor aircraft
European Patent Office | 2024
|