摘要 |
A vertical take-off and landing aircraft comprises an aircraft body (6), a main thrust device (7) that provides a main thrust for the aircraft, and a posture control device. The posture control device comprises multiple posture alignment units (2) for adjusting rolling and pitching postures of the aircraft. The posture alignment unit comprises blades driven by a motor (3). By means of the aircraft of the present invention, the mechanical structure is simplified in the aspect of posture adjustment and the manufacturing difficulty and maintenance cost are reduced. |