The invention relates to a tilting mechanism of an electric vertical take-off and landing aircraft, which comprises an upper fixed support arm, a lower fixed support arm and a motor seat, the upper fixed support arm and the lower fixed support arm are fixedly supported in a nacelle of the aircraft, a power mechanism is arranged on the lower fixed support arm, and the power mechanism is connected with the motor seat through a transmission mechanism. And the output of the control power mechanism drives the motor base to tilt. The aircraft with the tilting mechanism can take off and land conventionally in an area with an airport; under the condition that runway conditions are insufficient, vertical take-off and landing can be achieved.
本发明涉及一种电动垂直起降飞行器的倾转机构,包括上固定支臂、下固定支臂、电机座,上固定支臂和下固定支臂固支于飞行器短舱内,下固定支臂上设置有动力机构,动力机构通过传动机构与电机座连接,控制动力机构的输出带动电机座倾转。具有该倾转机构的飞行器在有机场的地区,可以常规起降;在跑道条件不足的情况下,可以垂直起降。
Tilting mechanism of electric vertical take-off and landing aircraft
一种电动垂直起降飞行器的倾转机构
2024-07-12
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
Tilting mechanism of electric vertical take-off and landing aircraft for integrally tilting wings
European Patent Office | 2024
|European Patent Office | 2025
|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
|Self-tilting vertical take-off and landing aircraft and take-off and landing method
European Patent Office | 2023
|