| 摘要 |
PURPOSE: A vertical takeoff and landing aircraft is provided to have a safe structure without damages and to make a transition flight mode possible. CONSTITUTION: A vertical takeoff and landing aircraft comprises a cyclic duct(1), a rotor assembly, a stator assembly, a control vane assembly, a battery mount, an acceleration sensor, and a control part. The rotor assembly comprises a propeller which is rotated by a motor and power source. The stator assembly is located in the lower part of the propeller and buffers the reaction of the movement of the duct. The control vane assembly is located in the lower part of the stator assembly and changes the direction of a propelling force generated by the rotation of the propeller. The acceleration sensor is electrically connected to the battery and senses collision. The control part is electrically connected to the battery. |
