An aircraft (100) with a rotary wing (40) is equipped with a propulsion system (10). The aircraft (100) includes a rotating mast (50) that rotates the rotor wing (40). The propulsion system (10) includes a pole (20) mechanically connected to the rotating mast (50) of the aircraft (100), where at least one end of the pole (20) is equipped with a motor (30) configured to rotate the pole (20) around the axis of the rotating mast (50) in such a way that the rotation of the pole (20) can be used to rotate the rotating wing (40). At each end of the pole (20) is placed a motor group (30), wherein each motor group (30) includes a pair of counter-rotating propellers (32, 32'), said pair of counter-rotating propellers (32, 32') being arranged in such a way as to generate a rotational torque to rotate the pole (20).
带有旋翼(40)的飞行器(100)配备有推进系统(10)。飞行器(100)包括使旋翼(40)旋转的旋转主轴(50)。推进系统(10)包括机械地连接到飞行器(100)的旋转主轴(50)的杆(20),其中,杆(20)的至少一端配备有马达(30),其配置成使杆(20)绕旋转主轴(50)的轴线旋转,使得杆(20)的旋转可用于使旋翼(40)旋转。在杆(20)的每一端放置了马达组(30),其中,每个马达组(30)包括成对的反向旋转的螺旋桨(32、32'),所述成对的反向旋转的螺旋桨(32、32')布置成产生旋转扭矩以使杆(20)旋转。
ROTARY WING AIRCRAFT WITH IMPROVED PROPULSION SYSTEM
带有改进的推进系统的旋翼飞行器
2021-06-22
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |