The application relates to a force couple balance and longitudinal array push-pull vertical take-off and landing high-speed aircraft, belonging to the technical field of aircrafts, which comprises a
fuselage, a rotor, a
fixed wing, a steering controller and a
propeller. The rotor is installed at the top of the middle part of the
fuselage through a rotor shaft, and a
clutch is arranged between the rotor and a power
system and / or a
transmission system matched with the
fuselage, so as to be controlled to be disconnected or to transmit power to the rotor. The steering controller comprises a fixed base and a rotating base, and each of the
nose and the
tail has a set of the rotating base. The
propeller is provided with two propellers which are respectively installed on the rotating bases of the
nose and the
tail, and are controlled to rotate with the rotating bases relative to the fixed base. The force couple formed by the front and rear thrust vectors is used to balance the reverse torque brought by the rotor. When the
propeller is coaxial with the middle axis of the fuselage, the wind area of the single propeller obtains double thrust. The application can improve the energy
utilization rate, improve the
carrying capacity, improve the
flight safety performance and obtain a longer hovering time.