The invention belongs to the field of aerodynamic
layout design of aircrafts, and particularly relates to a vector ducted
tail rotor high-speed helicopter which comprises a
fuselage, a main rotor, lift wings, a horizontal empennage, a vertical empennage and a ducted fan, and an air inlet of the ducted fan faces the
fuselage, is rotatably connected with the upper portion of the
tail of the
fuselage and can horizontally rotate above the
tail of the fuselage; when the helicopter flies forwards at a high speed, an
angle alpha is formed between the central axis of the ducted fan and the central axis of the fuselage and is larger than or equal to 0 degree and smaller than 90 degrees, and alpha is equal to 90 degrees during hovering and low-speed flying.
Vector control of tail thrust is achieved by horizontally rotating the whole ducted fan, the defect of a common ducted
tail rotor in control efficiency is overcome, control efficiency and action efficiency are improved, and the
flight speed is greatly increased. In addition, the number of control channels of the vector ducted
tail rotor system is relatively small, and the operation steps of a
pilot are simplified; and as the tail of the ducted fan is not provided with a pneumatic control surface,
airflow in a wake flow area is more stable and uniform, and flight is
safer.