| 摘要 |
The present invention relates to a tilt-rotor aircraft. The present invention includes a pair of rotary wings arranged on both sides of the fuselage to rotate in the opposite directions to each other; a pair of servo motors for tilting the rotary wings to enable each rotary wing to rotate around an axis vertical to the progressing direction of the fuselage; and a pair of rotors for calibrating the posture of the fuselage to stably maintain the aircraft. |
