Hybrid air vehicle

A hybrid air vehicle (1) comprising a body (2) on the air vehicle;

• at least one motor (3) which provides required power for the flight of the body (2) on the air vehicle;
• at least one rotor (4) extending outward from the body (2) on the air vehicle, connected to the motor (3), and rotating around itself;
• a plurality of blades (5) located on the rotor (4);
• a helicopter mode (H) in which the body (2) on the air vehicle performs tasks such as vertical landing and take-off, autorotation and hovering;
• an anti-torque system (6) on the body (2) on the air vehicle, which creates anti-torque when the body (2) on the air vehicle is in helicopter mode (H);
• an airplane mode (A) in which the rotor (4) is stopped and the blades (5) are used as fixed wings;
• at least one propulsion system (7) that provides thrust for the movement of the body (2) when the body (2) on the air vehicle is in airplane mode (A);
• a transition mode (T) in which the rotor (4) is stopped and the propulsion system (7) is activated while the body (2) on the air vehicle is switched from helicopter mode (H) to airplane mode (A);
• at least one canard (8) located in the nose area of the body (2) on the air vehicle and providing lift to the body (2) on the air vehicle, wherein at least one control surface (9) located in the canard (8) to extend outwards from the canard (8), control surface (9) that moves along the direction in which the wing (8) extends outward from the body (2) while the body (2) on the air vehicle is in transition mode (T) and thus moves from the closed position (C) to the open position (O), thus increasing the aerodynamic surface area of the wing (8) and providing additional load-bearing force to the body (2) on the air vehicle:
• a closed position (C) in which the control surface (9) is located in the canard (8);
• an open position (O) in which the control surface (9) is moved from the closed position (C) and extends outward from the canard (8) when the body (2) on the air vehicle is in helicopter mode (H), transition mode (T), or airplane mode (A).