Wing energy reutilization system

A method, comprising:

• receiving, by an energy reutilization system, wind, wherein the wind passes through a vortex rotor, which is part of the energy reutilization system, located at an edge of the wing that is furthest away from a body of an airplane, and wherein the vortex rotor is perpendicular to the wing span;
• rotating, by the energy reutilization system, the vortex rotor based on the received wind, wherein the rotation of the vortex rotor generates work;
• transferring, by the energy reutilization system, the generated work from the vortex rotor to a drive shaft, wherein the drive shaft is part of the energy reutilization system;
• rotating, by the energy reutilization system, the drive shaft;
• rotating, by the energy reutilization system, a first bevel gear, and a second bevel gear, wherein the first bevel gear and the second bevel gear are connected to the drive shaft;
• receiving, by the energy reutilization system, additional wind wherein the additional wind passes across a front portion of the wing;
• compressing, by the energy reutilization system, the additional wind;
• wherein the compression of the additional wind is done by a tooth and a compressing arm that are both part of the energy reutilization system;
• sending, by the energy reutilization system, the additional wind through a pressure valve;
• and
• sending by the energy reutilization system, the additional wind from the pressure valve to a reservoir, wherein the reservoir is part of the energy reutilization system.