Wind turbine for energy generation

The wind turbine system efficiently generates energy, purifies air, and provides heating/cooling by integrating air pump systems and purification devices, overcoming limitations of traditional wind power plants.

DE202024002710U1Active Publication Date: 2026-04-02DIE PHILOSOPHISCHE PRAXIS - PHILOSOPHISCHE BELLETRISTISCHE WISSENSCHAFTLICHE TEXTE JEDWEDER ART KUNST- & BILDTEXTE E K
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Patent Information

Authority / Receiving Office
DE · DE
Patent Type
Utility models
Current Assignee / Owner
Filing Date
2024-05-17
Publication Date
2026-04-02

AI Technical Summary

Technical Problem

Existing wind power plants lack efficiency in energy generation and do not integrate air purification and heating/cooling functionalities effectively.

Method used

A wind turbine system that incorporates a wind tunnel with air pump systems, airflow regulation, and air purification devices, capable of generating electricity, purifying air, and providing heating/cooling by integrating cooling systems and heat pumps.

Benefits of technology

Enhances energy generation efficiency, integrates air purification, and provides heating/cooling capabilities, addressing multiple energy needs simultaneously.

✦ Generated by Eureka AI based on patent content.

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Abstract

Wind power plant for energy generation, comprising at least one air pump system 46, at least one wind energy system and at least one wind tunnel 1, wherein the at least one wind energy system is arranged within the at least one wind tunnel 1, on or in at least one air shaft of the wind power plant for energy generation, or within the at least one air pump system 46, wherein the at least one air pump system 46 is fluidically connected to the at least one wind energy system, and wherein the at least one wind energy system comprises at least one propeller system 96, 103, 108 for generating electrical energy.
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Description

[0001] The invention relates to a wind turbine for energy generation. Description of the invention

[0002] The purpose of the invention is to eliminate the disadvantages of the prior art and to provide an alternative wind power plant for energy generation.

[0003] This problem is solved by the features listed in the claims.

[0004] Depending on its advantageous embodiments, the wind turbine for energy generation can also be referred to as a wind turbine for energy generation and air purification (abbreviated: WKAzEL).

[0005] Cooling of heat-generating components of the WKAzEL can be achieved by placing the components in the wind tunnel or by coupling cooling systems to the WKAzEL.

[0006] In addition to its use as an energy generation plant and an air purification plant, the WKAzEL can also be designed as a (combined) heating and cooling plant.

[0007] The selection of the individual components, the type of assembly of the individual components of the WKAzEL and the size of the WKAzEL result primarily from the performance of the components, the intended use(s) of the WKAzEL, the amount of electricity required for the WKAzEL's own operation and the electricity demand of the respective end consumers. Implementation of the invention

[0008] The invention is explained in more detail using several exemplary embodiments. For this purpose, we show... Fig. 1 Wind turbine for energy generation (top view), Fig. 2 Wind turbines for energy generation according to Fig. 1 with a wind turbine in outdoor operation (frontal view), Fig. 3 Wind turbines for energy generation with a wind turbine in motor operation (top view), Fig. 4 Wind turbines for energy generation according to Fig. 3 (lateral), Fig. 5 Wind turbine for energy generation with compression and amplification system (top view), Fig. 6 Wind turbines for energy generation with induction system (frontal), Fig. 7 Wind turbine for energy generation with induction system (top view), Fig. 8 Wind turbine for energy generation with induction system and coupling to the air extraction shaft of a heat pump (lateral).

[0009] The description refers to the accompanying drawings, which illustrate specific embodiments in which the arrangement according to the invention can be implemented. In this respect, directional terminology such as "top," "bottom," etc., is used with reference to the orientation of the described drawings. This directional terminology serves for illustrative purposes and is in no way restrictive.

[0010] It is understood that other embodiments may be used and structural or logical modifications made without deviating from the scope of protection of the present invention. It is understood that the features of the various exemplary embodiments described herein may be combined with one another, unless specifically stated otherwise. The following detailed description is therefore not to be interpreted as restrictive, and the scope of protection of the present invention is defined by the appended claims.

[0011] In the figures, identical or similar elements are provided with identical reference symbols where appropriate.

[0012] The wind turbine according to the invention for energy generation is shown graphically in the Fig. Numbers 1 to 8 are shown.

[0013] The wind turbine for energy generation comprises at least one air pump system 46, at least one wind energy system, and at least one wind tunnel 1. The at least one wind energy system is arranged within the at least one wind tunnel 1, on or in at least one air duct of the wind turbine for energy generation, or within the at least one air pump system 46. The at least one air pump system 46 is fluidically connected to the at least one wind energy system. The at least one wind energy system comprises at least one propeller system 96, 103, 108 for generating electrical energy.

[0014] Wind tunnel 1 can be designed to be straight, polygonal, or circular. It can be installed in the floor, wall, and / or ceiling of a room. The shape and layout of wind tunnel 1 are determined by the space into which the WKAzEL is installed and by the air pump system 46 to which it is connected. Wind tunnel 1 is made of a non-flammable or flame-retardant material.

[0015] According to various embodiments, the wind turbine for energy generation further comprises at least one airflow regulation system. The at least one airflow regulation system is arranged within the at least one wind tunnel 1, on the at least one wind tunnel 1, within the at least one air pump system 46, on the at least one air pump system 46, or on or in the at least one air duct of the wind turbine and is configured to regulate an airflow.

[0016] According to various embodiments, the at least one air pump system 46 has at least one chamber. The at least one chamber has at least one air-permeable opening on each of its opposite sides. The at least one chamber has a movably mounted, air-compressing element. The air-compressing element is movably mounted such that movement of the air-compressing element creates an overpressure on a first side of the air-compressing element and a negative pressure on a side opposite the first side of the air-compressing element.

[0017] According to various embodiments, the at least one air pump system 46 has an induction system. The at least one air pump system 46 is designed such that the movement of the air-compressing element generates an electrical voltage.

[0018] According to various embodiments, the air-compressing element comprises at least one magnetic element. At least one inductive element is arranged in or on the at least one chamber along a direction of movement of the air-compressing element, such that the movement of the air-compressing element generates an electrical voltage.

[0019] According to various embodiments, the air-compressing element comprises at least one inductive element. In or on the at least one chamber, at least one magnetic element is arranged along a direction of movement of the air-compressing element, such that the movement of the air-compressing element generates an electrical voltage.

[0020] The at least one inductive element can be, for example, an induction coil or an induction roller. Furthermore, the wind turbine can have one or more magnetic field amplifiers and / or electromagnetic converters for energy generation.

[0021] According to various embodiments, a head area of ​​at least one wind turbine is designed to be directionally variable and / or height-variable.

[0022] According to various embodiments, at least one wind turbine has a motor.

[0023] According to various embodiments, the wind turbine for energy generation further comprises a compression and amplification system. The compression and amplification system is operatively connected to the at least one wind turbine via a first mechanical shaft. The compression and amplification system is configured to transfer mechanical energy from the first mechanical shaft to at least two second mechanical shafts. The at least two second mechanical shafts are operatively connected to a generator.

[0024] According to various embodiments, the compression and amplification system includes an induction system. The induction system is designed such that the movement of the compression and amplification system generates an electrical voltage.

[0025] According to various embodiments, at least one wind energy system has an induction system.

[0026] According to various embodiments, the wind turbine for energy generation further comprises at least one air purification device. The at least one air purification device is designed to remove at least one pollutant from the air flowing through it. The at least one air purification device is arranged in or on the at least one wind tunnel 1, in or on the at least one air pump system 46, or in or on the at least one air duct of the wind turbine.

[0027] According to various embodiments, the air purification device is designed to store and release the depleted pollutant in concentrated form.

[0028] In fluid and aerotechnical terms, an air purification system is a device for separating media and can be designed as a filter or filter system. Air purification can be single-stage or multi-stage. For example, a coarse filter can remove coarse contaminants such as pollen, insects, and the like from the air. A fine filter can be connected to the coarse filter to remove fine dust particles, for example. Air filtered in this way reduces the likelihood of mechanical defects in the wind turbine used for energy generation.

[0029] A chemical filter, such as an absorption and / or adsorption filter, can be connected to the fine filter. This filter can be specifically designed for one or more pollutants. These pollutants could include, for example, CO2, but also CO, NO. xIt could be SO2 or any other air pollutant. The chemical filter can be equivalent to a direct air capture device for CO2.

[0030] The air purification system can be configured to store and release the extracted pollutant in concentrated form. For example, CO2 filtered from the air via Direct Air Capture can be made available for use in a suitable refining plant to produce e-fuel. This suitable plant can be part of the wind turbine for energy generation or be connected to it.

[0031] According to various embodiments, the at least one wind tunnel 1 is connected to at least one building-side ventilation system or to at least one ventilation system of at least one technical device.

[0032] A building ventilation system can be, for example, a vertical or horizontal ventilation shaft, where wind and thermal buoyancy forces may overlap. However, a building ventilation system can also be an actively operated system, such as an exhaust system powered by at least one fan. The building ventilation system can be integrated into a building foundation or a building wall.

[0033] A ventilation system for a technical device could, for example, be the ventilation system of an exhaust air heat pump. Integrating the wind tunnel of a wind turbine is conceivable in principle wherever air is either drawn in (for example, to cool device components) and / or blown out.

[0034] Integration can take place on the supply air and / or exhaust air side.

[0035] According to various embodiments, the at least one air pump system 46 is designed to provide compression heat to at least one heat pump in order to support a heat / cold exchange of the at least one heat pump.

[0036] According to the embodiment according to Fig. The wind turbine for energy generation has an air pump system 46 with a quadruple air compression system, which is centrally located in the middle of the wind tunnel 1. The wind tunnel 1 has a wind tunnel cover 3 as an inspection opening. In the area of ​​the particulate filter 48, the CO2 filtration system 44, the CO2 to e-fuel conversion system 45 (which correspond to the air purification system), and the air exhaust 47, the wind tunnel 1 is hermetically sealed by a partition 2 to guide compressed air along a maximally long path through the wind tunnel 1 to the air exhaust 47. Another particulate filter 48 and a CO2 filtration system 44 are arranged diagonally opposite. The wind tunnel 1 is made of a non-flammable or only slightly flammable material.

[0037] The air compression system consists of an elongated, box-shaped, and airtight air compression chamber 4, in which four air compression chambers 5 are arranged, which are also airtight. The air compression chambers 5 correspond to at least one chamber of the air pump system 46. Each air compression chamber 5 is formed by an air compression wall 7, at least one guide rail for the air compression wall 8, a front wall of the air compression chamber 9, a rear wall of the air compression chamber 10, a fresh air supply area at the front 15, a fresh air supply area at the rear 18, an air supply flap at the front (open) 11 or an air supply flap at the front (closed) 12, and an air supply flap at the rear (open) 13.an air supply flap rear (closed) 14, an air resistance meter air compression chamber 21, a dust filter fresh air supply area front 17, a dust filter fresh air supply area rear 20, a connection to the motorization air compression chamber 22 (visible in . Fig. 2) and a connection to the control electronics air compression chamber 23. The air compression wall 7 corresponds to the movable, air-compressing element. Open flaps 11, 13 correspond to at least one air-permeable opening. Front and rear correspond to the first and second sides of the air-compressing element. Individual or all components of the air compression system may be provided multiple times.

[0038] The air compression wall 7 divides the air compression chamber 5 into two airtight areas, the first and second sides of the air-compressing element. Both areas contain air. During operation of the air pump system 46, the air compression wall 7 moves electronically on or along the guide rail of the air compression wall 8, continuously back and forth between the front wall of the air compression chamber 9 and the rear wall of the air compression chamber 10. As the air compression wall 7 moves towards the front wall of the air compression chamber 9, it pushes the air present in the area between the air compression wall 7 and the front wall of the air compression chamber 9 towards the front wall of the air compression chamber 9.During the phase in which the air compression wall 7 moves towards the rear wall of the air compression chamber 10, the air compression wall 7 pushes the air present in the area between the air compression wall 7 and the rear wall of the air compression chamber 10 towards the rear wall of the air compression chamber 10.

[0039] The guide rail air compression wall 8 is installed on the sides, in the floor area and / or in the ceiling area of ​​the air compression chamber 5 and forms an airtight connection between the air compression wall 7 and the inner walls of the air compression chamber 5.

[0040] The front wall of air compression chamber 9 separates the air compression chamber 5 in the front area, and the rear wall of air compression chamber 10 in the rear area, from the wind tunnel 1 adjacent to the air compression chamber 5 in an airtight manner.

[0041] The air supply flap front 11, 12 is installed in the front wall of air compression chamber 9. The air supply flap front 11, 12 forms the passage between air compression chamber 5 and wind tunnel 1 in the front area of ​​air compression chambers 5. The air supply flap front 11, 12 can be opened and closed electronically. The air supply flap front 11, 12 preferably opens and closes in a louvered, shell, or vortex manner. The air supply flap front 11, 12 and / or the air supply flap rear 13, 14 can have an air resistance sensor air compression chamber 21, which in the illustrated embodiment is arranged in the air compression wall 7. The air resistance meter air compression chamber 21 contributes to the regulation of the opening and closing movements of the air supply flap front 11,12 and the air supply flap rear 13,14.The air resistance sensor of air compression chamber 21 is coupled to the control electronics of air compression chamber 23. The air resistance sensor of air compression chamber 21 regulates the speed and the specific interaction of the components of air compression chamber 4 depending on the power requirement and in conjunction with the control electronics of the airlock gate 41 (shown in ). Fig. 3) and the control electronics of the propeller system 37. During the phase in which the air compression wall 7 moves towards the front wall of the air compression chamber 9, the air supply flap front (closed) 12 opens depending on the air resistance measured by the air resistance meter of the air compression chamber 21. The movement of the air compression wall 7 forces the air present in the air compression chamber 5 in the area between the air compression wall 7 and the front wall of the air compression chamber 9 into the wind tunnel 1 via the air supply flap front (open) 11. During the phase in which the air compression wall 7 moves towards the rear wall of the air compression chamber 10, the air supply flap rear (closed) 14 opens depending on the air resistance measured by the air resistance meter of the air compression chamber 21.By moving the air compression wall 7, the air present in the air compression chamber 5 in the area between air compression wall 7 and rear wall of air compression chamber 10 is forced into the wind tunnel 1 via the rear air supply flap (open) 13.

[0042] The fresh air supply area Front 15 is installed in the ceiling of air compression chamber 5 in the front section. The fresh air supply area Front 15 can be opened and closed electronically by a shut-off flap, Fresh Air Supply Area Front 16. The fresh air supply area Front 15 forms the passage between air compression chamber 5 and air intake area 24 in the front section of air compression chamber 5. During the phase in which the air compression wall 7 moves towards the rear wall of air compression chamber 10 and passes the fresh air supply area Front 15, the shut-off flap, Fresh Air Supply Area Front 16, opens, allowing air from air intake area 24 to flow into the respective air compression chamber 5 in the area between the front wall of air compression chamber 9 and air compression wall 7. The air supply flap Front (open) 11 or air supply flap Front (closed) 12 is closed during this phase.Opening the front fresh air supply flap (16) prevents a vacuum from forming in the air compression chamber (5). It also draws fresh air into the air compression chamber (5). The dust filter (17) is installed in the front fresh air supply area (15) and filters dust from the air, thus protecting the air compression chamber (5) from contamination. The same applies to the rear of the air compression chamber (5) with its corresponding rear fresh air supply flap (19).

[0043] The motorization air compression chamber 22 operates the movable, individual components of the air compression chamber 4 and can be installed in the floor, ceiling or side area of ​​the air compression chamber 4.

[0044] According to the embodiment according to Fig. 1. The air compression in the individual air compression chambers 5 occurs diagonally offset. When the air compression wall 7 of the first air compression chamber 5 is located at the front wall of air compression chamber 9, the air compression wall 7 of the second air compression chamber 5 is located in the middle of the second air compression chamber 5 with the direction of movement towards the front wall of air compression chamber 9, the air compression wall 7 of the third air compression chamber 5 is located in the middle of the third air compression chamber 5 with the direction of movement towards the rear wall of air compression chamber 10, and the air compression wall 7 of the fourth air compression chamber 5 is located at the rear wall of air compression chamber 10.When the air compression wall 7 of the first air compression chamber 5 is located at the rear wall of air compression chamber 10, the air compression wall 7 of the second air compression chamber 5 is located in the center of the second air compression chamber 5 with its movement direction towards the rear wall of air compression chamber 10, the air compression wall 7 of the third air compression chamber 5 is located in the center of the third air compression chamber 5 with its movement direction towards the front wall of air compression chamber 9, and the air compression wall 7 of the fourth air compression chamber 5 is located at the front wall of air compression chamber 9. This continuous, staggered movement of components of the individual air compression chambers 5 creates a staggered pumping motion. This staggered movement supplies a regular airflow to the wind tunnel 1. The airflow activates and operates the propeller system.

[0045] Aerial photography area 24 (visible in Fig. 2) is located above the air compression chamber 4. The air intake area 24 forms the connection between the air compression chamber 4 and the air compression chamber 5 and the ambient air. The air intake area 24 is permeable to air, but does not allow rainwater or similar substances to penetrate into the fresh air supply areas 15 and 18.

[0046] Weather protection aerial photography area 25 (visible in Fig. 2) is mounted above the air compression chamber 4 and at least above the fresh air supply areas 15,18.

[0047] The weather protection for aerial photography area 25 diverts rainwater and similar substances from aerial photography area 24.

[0048] According to the embodiment according to Fig. Figure 1 shows that the wind turbine for energy generation has a wind energy system with four propeller systems. The propeller systems drive the generator WKAzEL 38 (visible in Figure 1). Fig. 2) mechanical power. The propeller systems are used indoors. Depending on the design of the propeller system and the wind tunnel 1, a propeller system can also be used alternately indoors and outdoors. A propeller system is started and maintained by the airflow that is supplied to the wind tunnel 1 from the air compression chamber 4 through the front air intake flap (open) 11 and the rear air intake flap (open) 13 and directed to the propeller system via the airflow control system 39. In outdoor operation, a propeller system is started and maintained by the airflow supplied to the propeller system blades by the wind. A propeller system has several components. The propeller system hub 26 is the front end of the propeller system. The propeller system control electronics 37, which regulates the individual components of the propeller system, are installed in the propeller system hub 26.The control electronics of propeller system 37 coordinate the activity of the propeller system with the activity of the other propeller systems depending on the power requirements of the WKAzEL and the supplied wind quantity and wind speed. A propeller system can have different propeller system blades in its head area. Standard propeller system blades 27 are rotatable, allowing the amount of wind intake to be regulated. Extra propeller system blades 110 are foldable and / or extendable, allowing the propeller system to switch between indoor and outdoor operation in a space-saving manner and also increasing the wind intake capacity in outdoor operation. A standard propeller system shaft 28 is paired with an extra propeller system shaft 30, which is mounted to the swivel hinge propeller system 33 or to a ball hinge propeller system.The propeller system Extra 30 consists of a main shaft and at least one internal extension shaft, allowing the front part of the propeller system to be moved into outdoor operation via the propeller system Extra 30 shaft. The swivel hinge of propeller system 33 allows the front part of the propeller system to be rotated 90 degrees or more. A ball hinge allows the front part of the propeller system to be rotated flexibly in all directions. Both of these features allow the propeller system to be moved between indoor and outdoor operation in a space-saving manner and, in outdoor operation, to be oriented in different directions to capture the wind. A propeller system also includes a brake (propeller system 29), a gearbox (propeller system 32), and a mounting bracket (propeller system 49).

[0049] Fig. 2 shows the wind turbine for energy generation according to Fig. Figure 1 shows a propeller system in outdoor operation. The propeller systems depicted have a propeller system cage 31, which is attached between the propeller system blades and the swivel hinge propeller system 33 or ball hinge propeller system on the shaft propeller system standard 28 or shaft propeller system extra 30. During indoor operation of the propeller system, the propeller system cage 31 rests against the shaft propeller system standard 28 / shaft propeller system extra 30. For outdoor operation, the propeller system cage 31 can be extended so that it encloses the propeller system blades, allowing wind to pass through. This protects the propeller system blades from collisions with birds and other objects, and protects living beings from injury caused by collisions with the propeller system blades. A sliding roof wind tunnel 86 is integrated into wind tunnel 1 above the propeller system.The sliding roof of the wind tunnel 86 can be opened and closed electronically. The sliding roof of the wind tunnel 86 has a rubber seal (sliding roof 87) at the opening areas. The rubber seal (sliding roof 87) enables the wind tunnel 1 to be sealed watertight and airtight by the sliding roof of the wind tunnel 86. A rainwater drainage channel 36 is integrated into the shaft of the propeller system Extra 30, so that rainwater and similar substances do not run directly down the shaft of the propeller system Extra 30 and onto the rubber seal (sliding roof 87), but are instead diverted laterally. The generator WKAzEL 38 converts the mechanical power supplied to it by the propeller system into electricity. The generator WKAzEL 38 transmits the electricity to the motorization of the air compression chamber 22 and to the devices, businesses, households, factories, etc., connected to the WKAzEL. Two transformers 88 are provided for voltage conversion between individual components.The air pump system 46 can have its own generator, air pump system 62, as will be described in more detail later.

[0050] Fig. 3 and Fig. Figure 4 shows a further embodiment of the wind turbine for energy generation, which has a dual air compression system. The wind turbine for energy generation is arranged on a building wall 65 of a technical room 66. An airflow control system, in addition to the air pump system 46, regulates the amount of airflow supplied to the propeller system and includes an airlock 39, an air resistance sensor 40, control electronics 41, and an air accumulation zone 63. The airlock 39 is installed in front of the propeller system. The airlock 39 opens and closes in a louvered, shell, or vortex-like manner within the movement radius 42. The size of the opening and the speed of the opening and closing movement result from the strength of the activity of the air pump system 46.from the quantity and strength of the airflow supplied to the airlock barrier 39 and from the power requirement of the WKAzEL. Individual or all components of the airflow regulation system can be provided multiple times.

[0051] The air resistance sensor 40 is located on the air barrier 39 and measures the air resistance in the air stagnation zone 63 (the area immediately in front of the air barrier 39). It then transmits the measured values ​​to the control electronics 41, which are integrated into the air barrier 39 and regulate the opening and closing movements of the air barrier 39. The air stagnation zone 63 is the area in front of the air barrier 39 where the airflow supplied to the wind tunnel 1 stagnates before passing through the air barrier 39.

[0052] The air resistance sensor 21, located in the air compression wall 7 and also optionally on the front wall of the air compression chamber 9, measures the air resistance in the air compression chamber 5 in the area between the front wall of the air compression chamber 9 and the air compression wall 7 during the phase in which the air compression wall 7 moves towards the front wall of the air compression chamber 9. The air resistance sensor 21, together with the control electronics 64, regulates the opening and closing movements of the start and supply valve 50 and the speed of movement of the air compression wall 7 in relation to the power requirement of the WKAzEL.

[0053] The start and supply valve 50 is installed in the front wall of air compression chamber 9 and has electronic control. The start and supply valve 50 opens when the air compression wall 7 moves towards the front wall of air compression chamber 9 and the air resistance sensor in air compression chamber 21 detects a sufficiently strong air resistance at the start and supply valve 50. As soon as the start and supply valve 50 opens, it allows air to flow from air compression chamber 5 into the air storage area 63 of wind tunnel 1.

[0054] An air supply duct Front 51 is installed in a side wall at the front of air compression chamber 5. Depending on the layout of the space into which the WKAzEL is installed, the air supply duct Front 51 can alternatively be installed in the floor or ceiling at the front of air compression chamber 5. The air supply duct Front 51 can be opened and closed electronically by the closing flap Air Supply Duct Front 52. Air is drawn into air compression chamber 5 through the air supply duct Front 51 during the phase in which the air compression wall 7 moves towards the rear wall of air compression chamber 10. This prevents a vacuum from forming in air compression chamber 5 and also draws in fresh air. The closing flap Air Supply Duct Front 52 is open during the air intake phase.The start and supply valve 50 is closed. As soon as the air compression wall 7 reaches the rear wall air compression chamber 10, the front air supply duct 52 shuts off.

[0055] The front air supply duct closure flap 52 is installed outside air compression chamber 5, in front of the front air supply duct 51, and opens and closes the front air supply duct 51 electronically. During the phase in which the air compression wall 7 moves towards the rear wall of air compression chamber 10 and has passed the front air supply duct 51, the front air supply duct closure flap 52 opens, allowing air to flow into the air compression chamber 5 in the area between the front wall of air compression chamber 9 and air compression wall 7. The rear air supply duct closure flap 56 is open during this phase. Opening the front air supply duct closure flap 52 prevents a vacuum from forming in the air compression chamber 5 and also draws in fresh air. Air is drawn in until the air compression wall 7 reaches the rear wall of air compression chamber 10.The front flap 52 then closes, so that the air remains trapped in the air compression chamber 5 until, during the movement of the air compression wall 7 towards the front wall of the air compression chamber 9, it is forced through the air compression wall 7 against the start and supply valve 50 and through the opening of the start and supply valve 50 into the wind tunnel 1.

[0056] The rear air intake duct is installed in a side wall at the rear of the LKK. Depending on the layout of the space into which the WKAzEL is fitted, the rear air intake duct can alternatively be installed in the floor or ceiling at the rear of the LKK instead of in a side wall.

[0057] The rear air intake duct 53 can be opened and closed electronically by the rear air intake duct 56 closure flap. Air is drawn into the air compression chamber 5 through the rear air intake duct 53 during the phase in which the air compression wall 7 moves towards the front wall of the air compression chamber 9. This prevents a vacuum from forming. The rear air intake duct 53 is also open during the phase in which the air compression wall 7 moves towards the rear wall of the air compression chamber 10. This prevents air stagnation.

[0058] A grate air supply duct front 54 and a grate air supply duct rear 55 are mounted in the outer areas of the air supply duct front 51 and air supply duct rear 53 and prevent objects from entering the air compression chamber 5. A dust filter air supply duct front 57 and a dust filter air supply duct rear 58 are mounted in the air supply duct front 51 and air supply duct rear 53 and prevent dust from entering the air compression chamber 5. The air vent 44 also has a grate air vent 83.

[0059] The propeller system is started and maintained by the airflow supplied to wind tunnel 1 from air compression chamber 5 via the start and supply valve 50 and directed through the airlock gate 39. Additionally, a propeller system can be switched to motor operation and oriented in a different direction by 180 degrees or more within a range of motion of 61 via the rotary hinge propeller system 33 or the ball hinge propeller system 61. In motor operation, the propeller system is driven not by the air supply of the air pump system 46, but by a motor integrated into the propeller system 34, thus generating an airflow that activates or maintains the other propeller systems. The motor propeller system operates the propeller system.The motor propeller system 34 is integrated into the propeller system, directly into the pivot hinge propeller system 33, and connected to the generator WKAzEL 38. It is powered by the generator via the connection between the motor propeller system and the generator WKAzEL 59. The motor propeller system 34 is activated when the WKAzEL switches from the "Air Pump System Operation" mode to the "Auxiliary Motor Propeller System Operation" mode and the propeller system changes its orientation. In the WKAzEL's "Auxiliary Motor Propeller System Operation" mode, the propeller system, when running in motor mode, increases or maintains the activity of the other propeller systems by generating an airflow, supports or temporarily replaces the air pump system 46, and increases the overall power output of the WKAzEL. A shaft of the motor propeller system 35 supplies mechanical power to the air pump system 62 through the activity of the propeller system.The motor propeller system 35 incorporates the connection between the motor propeller system and the generator WKAzEL 59. The generator air pump system 62 supplies power to the air compression chamber motor 22 via the connection between the generator air pump system and the air compression chamber motor 60. The generator air pump system 62 is charged and operated by the mechanical power supplied to it by a propeller system. The generator WKAzEL 38 supplies power to the businesses and households connected to the WKAzEL. Additionally, the generator WKAzEL 38 supplies power to the motor 34 of the propeller system, which is connected to the generator air pump system 62.

[0060] According to Fig. 4 The wind turbine for energy generation is arranged on the ground side of a building foundation 84, with the two air compression chambers 5 arranged one above the other. The components of the air compression chamber 4 are controlled and regulated by the control electronics air compression chamber 23.

[0061] Fig. Figure 5 shows another embodiment of the wind turbine for energy generation, with a compression and amplification system. The wind tunnel is coupled to an air exhaust duct (heat pump 67), which is connected to an air intake duct (heat pump 69), which has a grate (air intake duct 70) and a dust filter (air intake duct 71). A ventilation flap (wind tunnel 68) is arranged on the wind tunnel 1, which can be opened and closed electronically or manually. The ventilation flap (wind tunnel 68) opens and closes in a louvered, shell, or vortex manner. Through the open ventilation flap wind tunnel 68, the air flowing into the wind tunnel 1 via the air exhaust shaft heat pump 67 can be released into an exterior building area 82, for example during phases in which the WKAzEL is temporarily switched off due to cleaning work etc. or when no or less air supply from the air exhaust shaft heat pump 67 is required for the operation of the WKAzEL.A CO2 filter (ventilation flap wind tunnel 85) and / or a fine dust filter (ventilation flap wind tunnel) and / or a grate (ventilation flap wind tunnel 89) can be installed in front of the ventilation flap wind tunnel 68.

[0062] The wind energy system comprises three propeller systems, each of which in turn incorporates a compression and amplification system. The compression and amplification system first compresses the mechanical power of the individual propeller systems onto the compression shaft 74 and then redirects the compressed mechanical power, before it reaches the generator WKAzEL 38, back onto individual amplification shafts 79. The compression shaft 74 corresponds to the first mechanical shaft, and the amplification shafts 79 correspond to at least two secondary mechanical shafts. Coupling hinges 72 connect the propeller systems to the compression shaft 74. Gearboxes 73 are installed in the coupling hinges, through which the compression shaft 74 is driven. The compression shaft 74 is the main shaft of the propeller system.The compression shaft 74 is installed in a separate channel, compression shaft 76, which runs parallel to the wind tunnel 1. The compression shaft 74 is driven by the individual propeller systems and concentrates the mechanical power of each propeller system. By using the compression shaft 74, larger and more complex modifications to building walls 65 can be avoided when the wind tunnel 1 is mounted externally. Furthermore, the performance of the entire propeller system can be increased. A swivel hinge, compression shaft 75, allows the compression shaft 74 to be routed around corners. A distribution gearbox adapter, compression shaft 77, is connected to the end of the channel, compression shaft 76, and to the end of the compression shaft 74. A gearbox power amplifier 78 is installed in the distribution gearbox adapter 77, to which the movement of the compression shaft 74 is transmitted.The gearbox power amplifier 78 is connected to separate amplifier shafts 79, via which mechanical power is supplied to the generator WKAzEL 38. The generator WKAzEL 38 is connected to a heat pump 80 by means of a supply line, generator WKAzEL 81. The heat pump 80 supplies air to the WKAzEL for the operation of the propeller system. The heat pump 80 supplies the businesses and households connected to it.

[0063] The coupling to the heat pump 80 can be implemented such that the heat generated by the movement of the air pump system 46 and the generator of the WKAzEL 36 provides the heat that the heat pump, in conventional operation, must draw from the ground, ambient air, or groundwater to heat the refrigerant within the heat pump. The WKAzEL can optionally also be connected directly to the heat pump's heat distribution and storage system. The movement of the air pump system 46 and the generator of the WKAzEL 36 generates heat within the heat distribution and storage system. This heat can (assist in) heating the water circulating in the heat pump's heat and storage system. If the temperature difference between the heat generated by the movement of the air pump system 46 and the generator of the WKAzEL, and the ambient air drawn in by the WKAzEL, is sufficiently large (e.g.,In cold regions and during the cold seasons, it may be possible to dispense with a refrigerant or reduce the amount of refrigerant in the heat pump. The heat-cold exchange required for energy generation when using a heat pump then occurs through the interaction of the warmer indoor air with the cold outdoor air.

[0064] Fig. Figure 6 shows the wind turbine for energy generation with an induction system integrated into the air pump system 46, which is located above the air compression chamber 5.

[0065] In the illustrated embodiment, the induction system comprises an induction roller system 90, induction rollers 91, a magnetic chamber 92, a magnetic field amplifier 93, and a magnetic field generator 95. The induction roller system 90 includes twelve induction rollers 91 and twelve induction roller holders 99, a magnetic chamber 92, and two magnetic field amplifiers 93. The induction rollers 91 are movably mounted in the induction roller holders 99, which are arranged side by side within the air compression wall guide rail 8, which runs along the entire area of ​​the air compression chamber 5. The air compression wall 7 moves back and forth within the air compression wall guide rail 8. The lower portion of the induction rollers 91 is arranged such that the induction rollers 91 and / or the induction roller holders 99 are set into rotation or movement by the movement of the air compression wall 7.The induction rollers 91 are surrounded by a magnetic field in the magnetic chamber 92. The magnetic chamber 92 can be the magnetic field generated by the generator WKAzEL magnetic field 95 located above the air pump system 46, provided that this field is strong enough to provide a magnetic field in the movement range of the induction rollers 91. The magnetic field can be amplified by magnetic field amplifiers 93, which are arranged on two opposite sides of the air compression wall guide rail 8 along the length of the air compression chamber 5. Alternatively, the magnetic field can also be generated solely by magnets 105. The movement of the air compression wall 7 in the air compression wall guide rail 8, and the resulting rotational movement or movement of the induction rollers 91 or the induction roller supports 99, changes the magnetic field in the magnetic chamber 92. This changing magnetic field provides an induced electrical voltage.This electrical charge can be used to operate the air pump system 46 or other technical equipment. To increase the usable electrical charge, electromagnetic converters 94 can be installed in the area of ​​the magnetic chamber. The negative pressure created by the movement of the air compression wall 7 draws air in through the grate air supply duct 100 and dust filter air supply duct 101 along the partition fresh air supply duct front 97 or partition fresh air supply duct rear 98, driving the vacuum propeller system 96.

[0066] Fig. Figure 7 shows the wind turbine for energy generation with an alternative embodiment of the induction system integrated into the air pump system 46. Here, the induction rollers 91 are arranged directly on the air compression wall 7. Magnetic field amplifiers 93 and magnets 105 are located on opposite sides of the air compression chamber 5. The movement of the air compression wall 7 changes the magnetic field in the air compression chamber 5, thus generating an induced voltage. The negative pressure created by the movement of the air compression wall 7 draws air in through the grate air supply shaft 100 and the dust filter air supply shaft 101, driving the vacuum propeller system 96. Compressed air drives two standard propeller systems 103 and passes through a CO2 filter 43 or a CO2 filtration system 44 before being discharged, among other methods, through the grate wind tunnel 102 into the environment.

[0067] The induction system can also be equipped differently, provided that the movement of the air compression wall 7 and / or the movement of another component of the wind turbine for energy generation creates or changes a magnetic field in such a way that an induced voltage is generated.

[0068] Fig. Figure 8 shows the wind turbine for energy generation with an induction system and coupling to the air exhaust duct of a heat pump 67. The inductive elements, induction coils 104 and magnets 105, are each arranged in an induction chamber 106. The induction coils 104 are connected to an induction drive thread 109. The induction chambers 106 are arranged above and below, respectively, in the outer region of the air compression chambers 5. The induction drive thread 109 extends along the long side of the air compression chamber 5 at both outer ends of the air compression wall guide rail 8. The induction drive thread 109 and the air compression wall guide rail 8 are arranged in a T-shape relative to each other on the long side of the air compression chamber 5. The inductive elements in the induction chamber 106 or the induction chambers 106 are connected to the air compression wall 7 of the air pump system 46 via the induction drive thread 109.The induction drive thread 109 is connected along its long side to the outer end of the air compression wall 7 via a toothed ball bearing 107 or another suitable element. The reciprocating movement of the air compression wall 7 within the air compression chamber 5 sets the induction drive thread 109 into (rotational) motion. The magnets 105 generate a magnetic field in the induction chamber 106. The (rotational) movement of the induction drive thread 109 changes the position of the induction coils 104 within the induction chamber 106. This change in the position of the induction coils 104 within the magnetic field in the induction chamber 106 generates an electrical voltage in the induction chamber 106. This electrical voltage can be used to operate the generator WKAzEL 38 or another connected device.

[0069] The exhaust duct of the heat pump 67 or the exhaust duct of another device with an exhaust air function is coupled to the air supply duct front 51 and the air supply duct rear 53 of the air compression chamber 5. The exhaust air is alternately directed into the air compression chamber 5 via the air supply duct front 51 and the air supply duct rear 53 into the area between the air compression wall 7 and the front wall of the air compression chamber 9, or into the area between the air compression wall 7 and the rear wall of the air compression chamber 10. During the phase in which the exhaust air flows into the air compression chamber 5 via the air supply duct front 51, it flows into the area between the air compression wall 7 and the front wall of the air compression chamber 9. The start and supply valve 50 on the front wall of the air compression chamber 9 is closed. The air supply duct rear 53 is closed. The start and supply valve 50 on the rear wall of air compression chamber 10 is open.The exhaust air pressure pushes the air compression wall 7 towards the rear wall of air compression chamber 10. The air in the area between air compression wall 7 and the rear wall of air compression wall 10 is then discharged via the start and supply valve 50 on the rear wall of air compression chamber 10 into the wind tunnel 1 connected to the start and supply valve 50. This discharged air sets the propeller system / wind energy system 108 in motion. After the air in the area between air compression wall 7 and the rear wall of air compression chamber 10 has been discharged into the wind tunnel 1, the front air supply duct 51 and the start and supply valve 50 on the rear wall of air compression chamber 10 close. The rear air supply duct 53 and the start and supply valve 50 on the front wall of air compression chamber 9 open. Exhaust air flows through the air supply shaft at the rear 53 into the area between the air compression wall 7 and the rear wall of the air compression chamber 10.The pressure of the exhaust air pushes the air compression wall 7 towards the front wall of the air compression chamber 9. The air in the area between the air compression wall 7 and the front wall of the air compression chamber 9 is then released via the start and supply valve 50 on the front wall of the air compression chamber 9 into the wind tunnel 1, which is connected via the start and supply valve 50. The released air sets the propeller system / wind energy system 108 in motion.

[0070] If at least two air compression chambers 5 are coupled to a common wind tunnel 1, the propeller system / wind energy system 108 can be operated continuously by alternately opening and closing the start and supply valve 50 on the front wall of air compression chamber 9 and the start and supply valve 50 on the rear wall of air compression chamber 10. Since the wind turbine has its own generator WKAzEL 38, the wind turbine can be operated both with and without exhaust air. In operation without exhaust air, the air required for the operation of the air pump system can be supplied to the air compression chamber via the wind tunnel through the start and supply valve on the front wall of the air compression chamber and the start and supply valve on the rear wall of the air compression chamber.

[0071] To increase energy gain, a variable-orientation propeller system 33 can be used. Alternatively, the connection between the air pump system 46 and the air exhaust duct 67 can be disconnected, allowing ambient air to enter the air compression chamber 5 via the front air intake duct 51 and the rear air intake duct 53.

[0072] According to a further embodiment of the wind turbine for energy generation, the inductive elements are connected to at least one wind energy system 108 by an induction drive thread 109. In the exemplary embodiment, a compression and amplification system according to Fig. 5 the induction drive thread 109. The induction drive thread 109 is operated by the (rotary) movement of the compression and amplification system. The induction drive thread 109 has inductive elements such as magnets 105 and induction coils 104. The induction drive thread 109 positions the inductive elements in such a way that they generate an electrical voltage. The electrical voltage is supplied to the generator 38. The embodiment also has an air pump system with inductive elements and coupling to an air exhaust duct according to Fig. 8, a wind energy system with outdoor operation according to Fig. 2, a wind energy system with integrated motor according to Fig. 3, an airflow regulation system, an air purification device, a CO2 processing device to e-fuel and an inlet of heat-generating components of the wind turbine into the wind tunnel 1. Reference sign 1 Wind tunnel 2 partition wall 3 wind tunnel covers 4 Air compression chamber 5 air compression chambers 6 Direction of movement Air compression wall 7 air compression wall 8 guide rail air compression wall 9 front wall air compression chamber 10 Rear wall air compression chamber 11 Air intake flap front (open) 12 Air intake flap front (closed) 13 Rear air intake flap (open) 14 Rear air intake flap (closed) 15 Fresh air supply area front 16. Front fresh air supply flap 17 dust filters, fresh air supply area, front 18 Fresh air intake area rear 19. Shut-off flap, fresh air supply area, rear 20 dust filters fresh air supply area rear 21 Air resistance meter Air compression chamber 22 Engine Air compression chamber 23 Control electronics air compression chamber 24 aerial photography area 25 Weather protection aerial photography area 26 Hub Propeller System 27 propeller system blades standard 28 shaft propeller system standard 29 Brake Propeller System 30 Shaft Propeller System Extra (Additional component for outdoor operation) 31 Propeller system cage (additional component for outdoor operation) 32 Gearbox Propeller System 33 Swivel hinge propeller system (additional components for flexible indoor operation, outdoor operation and engine operation) 34 Motor Propeller System (Additional component for motor operation) 35 shaft motor propeller system (additional component for motor operation) 36 Rainwater drainage channel propeller system (additional component for outdoor use) 37 Control electronics propeller system 38 Generator WKAzEL 39 Lock barrier 40 air resistance meters, lock gate 41 Control electronics for the lock gate 42 Movement radius of the lock barrier 43 CO2 filters 44 CO2 filtration system 45 Plant for processing CO2 into e-fuel 46 Air pump system 47 Air vent (integrated in 44) 48 fine dust filters 49 Propeller system bracket 50 Start and supply valve 51 Air intake duct front 52 Front air supply duct cover flap 53 Rear air intake duct 54 Rust Air Intake Shaft Front 55 Rust Air Intake Shaft Rear 56 Rear air intake flap 57 Dust filter Air intake duct front 58 Dust filter air intake duct rear 59 Connection Motor Propeller System - Generator WKAzEL 60 Connection Generator Air Pump System - Motorization Air Compression Chamber 61 Range of movement propeller system 62 Generator Air Pump System 63 Air stagnation area 64 Control electronics air compression chamber 65 Building wall 66 Technical Room 67 Air vent heat pump 68 Ventilation flap Wind tunnel 69 Air intake shaft heat pump 70 Rust air intake shaft 71 Dust filter air intake duct 72 Coupling hinge 73 Gearbox compression shaft 74 compression wave 75 Swivel hinge compression shaft 76-channel compression shaft 77 Transfer case adapter compression shaft 78 Gearbox Power Amplifier 79 Amplifier wave 80 Heat pump 81 Supply line generator WKAzEL to 80 82 Building exterior 83 Rust air vent 84 Building foundation 85 CO2 filter ventilation flap wind tunnel 86 Sunroof Wind Tunnel 87 Rubber coating sunroof wind tunnel 88 Transformer 89 Rust Ventilation flap Wind tunnel 90 induction roller system 91 Induction roller 92 Magnetic chamber 93 Magnetic field amplifiers 94 Electromagnetic Converter 95 Generator WKAzEL Magnetic field 96 Propeller system vacuum 97 Partition wall fresh air supply shaft front 98 Partition wall fresh air supply shaft rear 99 Induction roller bracket 100 grate air supply shaft 101 Dust filter air intake duct 102 Rust Wind Tunnel 103 Propeller system Standard 104 Induction coil 105 Magnet 106 Induction chamber 107 toothed ball bearing 108 Propeller system / Wind energy system 109 Induction drive threads 110 propeller system blades extra