A link rotor head and an unmanned aerial vehicle are disclosed. The link rotor head includes a main shaft, a rotor hub arranged at an upper end of the main shaft, a rotor assembly rotatably arranged on the rotor hub, a swashplate assembly movably arranged around the main shaft, and a link assembly. The swashplate assembly drives the rotor assembly to rotate via the link assembly. The link assembly includes a phase link, a phase rocker and a pitch link. The phase rocker is rotatably arranged on the rotor hub, with one end of the phase rocker movably connected with the swashplate assembly via the phase link and with an other end of the phase rocker movably connected with the rotor assembly via the pitch link.
LINK ROTOR HEAD AND UNMANNED AERIAL VEHICLE
2023-03-23
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
European Patent Office | 2023
|Multi-rotor unmanned aerial vehicle and multi-rotor unmanned aerial vehicle system
European Patent Office | 2020
|Unmanned aerial vehicle rotor assembly and unmanned aerial vehicle
European Patent Office | 2024
|