The invention relates to a self-rotor system assisted by a vertical axis fan and an aircraft, the self-rotor system comprises a propeller disc bin B, a first driving assembly, a rotor rotating shaft, two main propeller rotor blades and a second driving assembly, a lower self-aligning bearing with a seat is arranged in the propeller disc bin B, and an upper self-aligning bearing with a seat is mounted at the top of the propeller disc bin B; the first driving assembly is used for driving the lower belt seat self-aligning bearing to move; a rotor rotating shaft is arranged on the upper plummer block self-aligning bearing and the lower plummer block self-aligning bearing in a penetrating manner and is sleeved and fixed with the upper plummer block self-aligning bearing and the lower plummer block self-aligning bearing, and the other end of the rotor rotating shaft is arranged in the propeller hub bin A in a penetrating manner and is fixed with a rotating shaft top disc arranged in the propeller hub bin A; the main propeller rotor wing blades are connected to the propeller hub bin A, fan blades are arranged at the ends of the main propeller rotor wing blades, and the second driving assembly is used for driving the main propeller rotor wing blades to rotate. The device assists the flight of the aircraft so as to reduce the energy consumption of the aircraft.
本发明涉及一种垂直轴风机助力的自旋翼系统及飞行器,包括:桨盘仓B、第一驱动组件、旋翼转轴、两个主桨旋翼叶片以及第二驱动组件,桨盘仓B内设置有下带座调心轴承,其顶部安装有上带座调心轴承;第一驱动组件用于驱动下带座调心轴承移动;旋翼转轴穿设在上带座调心轴承和下带座调心轴承上,且与上带座调心轴承和下带座调心轴承套装固定,旋翼转轴的另一端穿设在桨毂仓A内,与桨毂仓A内设置的转轴顶盘固定;主桨旋翼叶片连接在桨毂仓A上,且端部设置有风机叶片,第二驱动组件用于驱动主桨旋翼叶片转动。本装置辅助飞行器飞行,以降低飞行器自带能源的能耗。
Spin wing system assisted by vertical axis fan and aircraft
一种垂直轴风机助力的自旋翼系统及飞行器
2023-10-10
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
Europäisches Patentamt | 2015
|MORPHING WING, WING OF AIRCRAFT, VERTICAL TAKE OFF AND LANDING AIRCRAFT AND AIRCRAFT
Europäisches Patentamt | 2017
|