Vertical take-off and landing vehicle

Abstract

A vertical take-off and landing vehicle (100) includes a hollow fuselage (102) accommodating a power source (112-1,112-2); a fixed wing (106) is perpendicularly configured on the hollow fuselage (102) which accommodates avionics; a payload (110) detachably fixed to a mounting holder (108) of the fixed wing (106) through a vertical cavity (104) of the hollow fuselage (102). The fixed-wing (106) configured on the hollow fuselage (102) enables electrical communication from the power source (112-1,112-2) to the avionics for lifting and vertical landing of the payload (110) by the vehicle (100). An unmanned aerial vehicle (UAV) (200) includes a fuselage (202) having a tail rotor (204) inclinedly positioned where a rotational axis of the tail rotor (204) is positioned at a first predefined angle (X) relative to a horizontal axis of the fuselage (202) for providing axial thrust to facilitate horizontal movement of the UAV (200) and aerodynamics with reduced drag.

Dependencies are inferred from the claim text.