1 )- Technical Field of the Invention

The present invention relates to a Gliding and Balancing Wing with a single or multiple wing structure that can be positioned based on the condition of the device with which it will be used and that allows for preventing the shaking resulting from the movement by gliding and vibrations in all winged structures operating in a vertical (vertical) or horizontal (horizontal) position by the effect of air currents, in other words, for balancing.

2)- Available Practices and Their Deficiencies:

Today, many products such as turbines, helicopters, aircraft, etc. are available that generate power in many areas, especially electricity generation, by using wind power and utilising it for different purposes. While these winged structures turn wind power into kinetic energy, or the ability to do other work, they also impose a load on the device on which they are mounted and cause major turbulence and oscillations due to different fluctuations brought on by air currents. Large passenger aircraft manufactured recently to address this problem have their wing tips bent upward in an L-shape. Due to the manufacturing structure of some wings, this function is partially favoured by their ability to glide through the air. Although these applications offer local remedies to solve the problem, they fail to fully achieve the desired function. These deficiencies outlined above lead to a significant portion of the power generated by the air currents being wasted for moving the device weights and the loss of user comfort.

3)- Solutions offered by the invention and the developed technical designs:

The Gliding and Balancing Wings achieved by our invention can be produced from materials consisting of all kinds of wooden, metal, plastic, fabric and textile chemicals components, and can be shaped depending on the need with the use of wings in different sizes and dimensions, offer flexible use based on the position of the device, whether vertical or horizontal, provides great efficiency improvements and user comfort due to the features of the wings, which highly reduce the load of the device to which it is attached by gliding in the air together with the device to which it is connected or integrated, and minimise the effect of vibration and turbulence by using the airflow in both directions, prevent malfunctions and facilitate its usage.

4)- Description of the figures (drawings):

Figure: 1 - View of the Gliding and Balancing Wing (KA/1 )

Figure: 2 - Combined use of the Gliding and Balancing Wing (KA/2) Figure: 3 - Vertical use of the Gliding and Balancing Wing (KA/3)

Figure: 4 - Horizontal use of the Gliding and Balancing Wing (KAM) 5)- Description of References in Figures:

The parts in the figures are enumerated and described below.

6)- Description of the Invention:

The present invention is a wing structure, suitable for use in vertical (vertical) or horizontal (horizontal) positions, resembling an eagle wing, consisting of wing tips (1 ) and a fuselage (2) including the joints to the main device in which such tips are integrated and turned into a wing. (KA1 ) These wings can be used together in different numbers (KA2) and function to prevent shaking resulting from the movement by gliding and vibrations. It is possible to use them in either vertical (KA3) or horizontal position (KA4) depending on the device to be used together. The system composed of those wings is erected on the structures (3) as a mast or platform on which the main device stands.

7)- Industrial Applications of the Invention:

The wing structure, which can be produced from different materials in different sizes and dimensions, can be used in combination with all winged structures, resembling an eagle wing, allows for weight bearing and balancing, and is a device to be used in many fields of industry. The raw materials and components that are used during its production are easily available on the market.