Abstract: The present invention discloses a drone, comprising a cyclical hull with one or more cyclical rings, an external structure, and a piezoelectric system. The external structure comprises a fixed wing and a rotary turbine construction. The external structure is securely and rotationally connected to the cyclic ring. The external structure is configured to rotate exponentially around the cyclical hull, thereby enabling a stabilization capability of the drone to forward in the desired direction. The piezoelectric system is mounted on the cyclical hull for efficiently analyzing onward wind direction, thereby effectively rotating the external structure at high speeds to enable the structural integrity of the drone. The drone further comprises one or more locking systems to unlock the cyclical rotational turbine based on an alert received from the piezoelectric system. Further, the drone comprises a camera for capturing a surrounding view of the drone.

Abstract: The present invention discloses an autonomous aerial vehicle system to provide a plurality of autonomous delivery vehicle, such as drone with a weight carrying capacity. The components of drone are disposed in the frisbee like shell which facilitates to take flight in the same manner and capacity as of a frisbee. The drone provides 360-degree rotation and the pioneering velocity driven movement capabilities. The system further comprises a management server in communication with the plurality of autonomous aerial vehicle via a wireless network to schedule a flight plan for the plurality of autonomous aerial vehicle. Each autonomous aerial vehicle comprises a control module in communication with the management server is configured to operates the autonomous aerial vehicle according to the flight plan data. The control module receives data comprising position data, battery status data, location data of the aerial vehicle to aid the autonomous vehicle to execute the flight plan.

Abstract: An unmanned aerial vehicle such as drone integrated with solar power unit, is disclosed. The solar power unit of the drone comprises a solar panel assembly positioned at a hull of the drone. The solar panel assembly is composed of a curtain-type shutter embedded with a plurality of photovoltaic cells. The shutter is formed of a plurality of slats having space between each of the slats, wherein the space facilitates for an effective dislocation of wind diffusion to maintain the stability of the hovering drone. The shutter further comprises a means for twisting and turning the shutter to provide balance for the hovering drone Further, the solar power unit comprises an energy storage unit operably coupled to the solar panel assembly for storage of the electrical energy from the solar panel. Further, the shutter is configured to spin cyclically diffusing the gust of wind harmlessly for stabilizing the hovering drone.

Abstract: An unmanned aerial vehicle such as drone integrated with solar power unit, is disclosed. The solar power unit of the drone comprises a solar panel assembly positioned at a hull of the drone. The solar panel assembly is composed of a curtain-type shutter embedded with a plurality of photovoltaic cells. The shutter is formed of a plurality of slats having space between each of the slats, wherein the space facilitates for an effective dislocation of wind diffusion to maintain the stability of the hovering drone. The shutter further comprises a means for twisting and turning the shutter to provide balance for the hovering drone Further, the solar power unit comprises an energy storage unit operably coupled to the solar panel assembly for storage of the electrical energy from the solar panel. Further, the shutter is configured to spin cyclically diffusing the gust of wind harmlessly for stabilizing the hovering drone.