Coaxial aircraft

The invention discloses a coaxial aircraft. The coaxial aircraft comprises a fuselage, a supporting rod, a propeller mechanism and a rotor wing mechanism. One end of the supporting rod is fixedly connected to the machine body and extends in the direction away from the machine body. The propeller mechanism comprises a machine arm, a first motor assembly and a propeller assembly, the machine arm is fixedly connected to the supporting rod, the first motor assembly is arranged on the machine arm, and the propeller assembly is arranged on the first motor assembly. The rotor mechanism comprises a second motor assembly and a rotor assembly, the second motor assembly is arranged on the supporting rod, and the rotor assembly is arranged on the second motor assembly. In this way, the coaxial aircraft can fly in different attitudes. 本申请公开了一种共轴飞行器。该共轴飞行器包括机身、支撑杆、螺旋桨机构和旋翼机构。其中，支撑杆的一端固定连接于机身并沿远离机身的方向延伸。螺旋桨机构包括机臂、第一电机组件和螺旋桨组件，机臂固定连接于支撑杆，第一电机组件设置于机臂，螺旋桨组件设置于第一电机组件。旋翼机构包括第二电机组件和旋翼组件，第二电机组件设置于支撑杆，旋翼组件设置于第二电机组件。通过上述方式，能够实现共轴飞行器