| 摘要 |
<p>A vertical take-off and landing aircraft with tiltrotor power for use on land and in the air comprising: a body (3) equipped with a driving device, controlled wheels (8) for allowing the body to move on the ground, a front thruster (1) and a rear thruster (2) for controlling the flight of the body or the take-off and landing thereof, transmission support rods (5) provided on the two sides of the body, a first pivot shaft (9) laterally passing through the body, with the first pivot shaft connected with the transmission support rods on the two sides of the body; the front thruster is fixedly connected to the front ends of the transmission support rods, and the rear thruster is fixedly connected to the rear ends of the transmission support rods; and the central axes of the front and rear thrusters are perpendicular to the plane formed by the two transmission support rods. By controlling the rotation angles of the front and rear thrusters, the aircraft has the major basic functions of both vertical take-off and landing as well as horizontal flight, and achieves a simple conversion between driving on land and flying in the air. During flight, the body of the aircraft always remains in a horizontal state, so that the drivers and passengers feel comfortable and have a wide field of vision, facilitating safe driving.</p> |
