Wing energy reutilization system

Patent metadata

Field	Value
Publication number	US-12270385-B2
Application number	US-202318110965-A
Country	US
Kind code	B2
Filing date	Feb 17, 2023
Priority date	Feb 17, 2023
Publication date	Apr 8, 2025
Grant date	Apr 8, 2025

Abstract

An apparatus, including a vertex rotor. The apparatus includes a transmission system, with the transmission system connected to the vertex rotor. The apparatus includes a drive shaft, with the drive shaft connected to the transmission system. The apparatus includes a first bevel gear and a second bevel gear. The first bevel gear and the second bevel gear are connected to the drive shaft.

First claim

What is claimed is:

1. 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.

2. The method of claim 1 , further comprising:
sending, by the energy reutilization system, the additional wind to a nozzle,
wherein the nozzle is connected to the reservoir via a piping system;
pushing, by the energy reutilization system, the additional wind out of the nozzle,
wherein the additional wind pushed out of the nozzle is used as an air flow field over the wing.

Assignees

• Abu Dhabi Univ

Inventors

• Elghazali Ahmed Fawzi Abdulmoati Abdellatif

Classifications

• F04B39/00 Primary

  Component parts, details, or accessories, of pumps or pumping systems specially adapted for elastic fluids, not otherwise provided for in, or of interest apart from, groups F04B25/00 - F04B37/00 · CPC title

• B64D41/007

  Ram air turbines · CPC title

• B64C21/025

  for simultaneous blowing and sucking · CPC title

• F03D3/002

  the axis being horizontal · CPC title

• F05B2240/923

  which is a vehicle · CPC title