A tilting system for a propeller of an aircraft may include a propeller disposed forward of an opening portion of a housing and configured to be selectively tilted relative to the housing; a link assembly disposed in the interior space of the housing, a first end portion thereof being connected to the housing, and a second end portion thereof being connected to the propeller, and the link assembly being configured to tilt the propeller upward or downward when it extends from or retracts into the housing; and an actuator coupled to the link assembly and configured to provide power for extension or retraction to the link assembly.
一种用于飞行器的螺旋桨的倾斜系统,可以包括:螺旋桨,该螺旋桨设置在壳体的开口部分的前面,并且被配置成选择性地相对于壳体倾斜;连杆组件,该连杆组件设置在壳体的内部空间中,其第一端部部分连接到壳体,并且其第二端部部分连接到螺旋桨,并且连杆组件被配置成当其从壳体伸出或缩回到壳体中时使螺旋桨向上或向下倾斜;以及致动器,该致动器耦接到连杆组件并被配置成向连杆组件提供用于伸出或缩回的动力。
Tilting system for propeller of aircraft
用于飞行器的螺旋桨的倾斜系统
2022-06-21
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
Wing tilting device of multi-propeller tilting wing configuration aircraft and aircraft
European Patent Office | 2024
|MULTI-PROPELLER TILTING AIRCRAFT AND FLIGHT CONTROL METHOD THEREFOR
European Patent Office | 2024
|Tilting coaxial double-propeller multi-power duct manned aircraft
European Patent Office | 2021
|