Bow type tilt rotor aircraft

The utility model relates to the technical field of electric vertical take-off and landing aircrafts, and particularly discloses a bow-type tilt-rotor aircraft, which comprises an aircraft body, a main wing, a bow-type aileron, a first thrust device and a second thrust device, two sides of the fuselage are respectively connected with a main wing and a bow-type aileron, and the bow-type aileron is connected with the main wing; the main wing is connected with a first thrust device and a second thrust device, and the bow-type aileron is connected with the first thrust device; the first thrust device is used for providing advancing and ascending thrust in a selectable mode; the second thrust device is used for providing rising thrust. When the aircraft flies horizontally, the second thrust device independently controls the rolling action of the aircraft, the situation that the first thrust device additionally tilts the power direction to control rolling is avoided, horizontal propelling power is kept, reduction o