DE102005043444A1 - Wind power plant has at least one macro-ring and at least three rotor blade carriers fixed to macro-ring, wherein each rotor blade carrier has number of rotor blades with horizontal and/or vertical and/or inclined local axes - Google Patents

Abstract

The wind power plant has a vertical axis (2) like an annular rotor which has at least one macro-ring (12,16,116) and at least three rotor blade carriers (11) which have a fixed connection to the macro-ring. Each rotor blade carrier normally has a number of rotor blades (1,1K) which have horizontal and/or vertical and/or inclined local axes and are referred to in this case as a macro-grid. Each macro-ring has a main ring (161), an inner central ring (162) connected to the main ring, and in many cases an inner intermediate ring , and often additional inner and/or outer rings.

Description

The proposed invention or, more precisely, the proposed Complex of inventions, a previously unknown complicated Assemble system refers to the use of wind energy and more particularly to vertical axis wind turbines, i. Wind turbines with vertical wind rotor axes (vertical axis wind turbine or vertical axis windmill).

This Wind energy system represents a kind of vertical axis wind turbines which is called CIRCULAR WIND POWER PLANT or simply CIRCULAR PLANT could. This species can also be considered as a separate class, because they have many significant differences from most conventional ones Vertical axis wind turbines has. This invention overcomes many disadvantages of the conventional ones Vertical axis wind turbines and conventional horizontal axis wind turbines and introduces some new viewpoints. The flexibility of the design structure, the wind adaptability, the efficiency of space utilization and performance improves and is the relative independence of current wind conditions reached. The corresponding wind turbines can not only for one moderate to a strong wind, but also for a weak wind and a storm wind can be used effectively. Thanks to the special flexibility of the design structure Designers and architects are given a lot of freedom, which is a variety of concrete designs could accomplish.

today one uses almost exclusively the horizontal axis wind turbines, they have a high technological Mature and there is a widespread opinion that this way the only right way is. That's why the big modern horizontal axis wind turbines drawn primarily for comparison. Their main disadvantages are connected with the specifics of wind energy. When the wind weak, they generate almost no electricity. Actually the area the leaves for one moderate and calculated a strong wind. Adjusting by turning the rotor blades, what is called the pitch control or the pitch control is for the Use of weak wind insufficient because the area of leaves in the conventional one Wind turbines for the weak wind not big enough is. The justification by a possible hurricane and the third Potency of wind speed shows that the horizontal axis wind turbines can not use a very strong wind and not flexible enough are. The blade angle control is no protection against gusts of wind the current blade angle does not correspond, and therefore the Slip control in the electric generator and the hydraulic brake used in the transmission, which has certain limits and offers no great flexibility. The transmission must even for a moderate wind have a weighty, typically 1/50 to 1/100, gear ratio, which is also a disadvantage. The aerodynamically perfectly calculated rotor blades do not use the space productively, what not with them, but with the entire construction and the operating principles of the conventional Wind turbines connected. The essential part of wind power, which acts on each rotor blade, can not for the rotation of the rotor blades be exploited and directed to the front, i. after the gondola and after the tower. The tower must be strong enough to handle this To resist power. Because the tower has to be high at the same time, does that for the main effort. The reasonable maximum sizes for this class are already reached. If you want 3MW plants than the 5MW plants does not mean you do not need big equipment. That means only that power 5MW to 10MW for the horizontal axis wind turbines the limit power is and the closer To this limit one comes, the more it technological and economic There are problems and there are no attractive super-wind turbines. If you want 20, 30, 50MW and more, would be that not the right way. Furthermore fit the constructions of the horizontal axis wind turbines ever not to a possible one Wind energy storage buffers that save the abundance of wind energy could. In order to is meant a storage before the conversion into the electric energy. Thanks to such storage could you use the energy of a storm wind and at the same time with Save electric generators.

Nice More than a hudret of years one reinvents different ones again and again Vertical-axis wind turbines. The realizations of these inventions but have not proven very good. One has partially not everything well thought out, partly not the right manufacturing technology chosen and sometimes there are no bold radical solutions.

The closest of my inventions in this field is the invention of the patent US 4684817 , The rotor blade supports, which the inventor has named all the frame wings (e., Framework vane), have many rotor blades with local vertical or horizontal axes. The inner faces of the rotor blade carriers are secured together in the center of the wind turbine by a vertical mast or cylinder. In some variants, supporting wheels are provided on or under a neck ring. The electric generators get the movement from the supporting wheels or from a neck ring or from a neck ring by a rubber transmission belt that performs the function of a damper or a short-term wind energy storage buffer.

The main claims of this conventional invention include, among other things, the characteristics of the rotor blades. The axis of each rotor blade is arranged along one of its four end faces, each rotor blade having thin resilient crossbars and resilient blades or sails therebetween. In most embodiments, an overlap between the red leaves is provided. This makes it possible to completely start the corresponding wind, but makes a direct damping of the gusts of wind impossible. The features of the rotor blades in the main claims limit the scope and at the same time sollche rotor blades are not the best. The supporting wheels and the rolling bearings have received little attention, although the importance of friction for vertical axis wind turbines is important. The wind energy storage buffer is just a damper. But you do not need energy storage for seconds, but for hours, days and more. There are also other features and missing features that indicate inadequate maturity of this invention, eg, the use of weak winds and storm winds is poorly thought out. At the same time, the invention is according to the patent US 4684817 the first step in the right direction and therefore this invention has a great importance. My previous inventions according to the references 10310227.2-15, 10332678.2-15, 102004001573.2-15, 102004024752.8-15, 102004042205.2-15, 102004061369.9-15, 102005011501.2-15 are the last and the most important steps which have fundamentally prepared the present invention.

All mentioned and some not mentioned disadvantages the conventional one Horizontal axis and vertical axis wind turbines are characterized by proposed type of wind turbines partially and sometimes completely eliminated. The advantages of the proposed invention and some new points of view are detailed and explained below in the description.

The Inventor's task, which is primarily the flexibility of the design structure, the wind adaptability, the efficiency of space use, performance and relative independence from present Wind conditions is considered by a flexible hierarchy of technical solutions solved.

1st solution. For example, 1 . 4 . 7 . 8th . 9 . 10 . 15 . 19 . 23 . 24 . 25 . 34 . 94 . 100 ,

The wind turbine has such a wind rotor with the vertical axis ( 2 ), such as a ring rotor mentioned below, and such a wind rotor carrier, such as a space tower ( 28 ), a circular row of room columns ( 29 ), a base ring ( 66 ), a base ring with supports, a base disc, a base disc with supports or a combination thereof ( 128 ) with / without intermediates ( 111 . 461 ), on. The space tower is usually wide and has little difference from the base discus.

The ring rotor has at least one macro ring ( 12 . 16 . 116 ) and at least three rotor blade carriers ( 11 ), which have firm connections with the macro rings. Each rotor blade carrier usually has many rotor blades ( 1 . 1K ) with the horizontal and / or vertical and / or oblique local axes and is here as a macro grid ( 11 ) designated. The macro ring has a main ring ( 36 . 161 ), usually also an inner central ring ( 162 ), which is connected to the main ring by spokes ( 163 ) or ropes, in the many cases also an inner intermediate ring ( 236 ) and sometimes additional inner ( 206 ) and / or outer ( 306 ) Rings on. The main ring goes under the macrogates or through the macrogitter opposite its equilibrium vertical lines or against its direct wind vertical lines.

The room supports ( 29 ) have supporting wheels or super wheels ( 169 ) over which the ring rotor rotates. In this case, the ring rotor has no own supporting wheels and is supported by the main ring or intermediate ring of the single or the lower macro ring. The super wheel has a super rolling bearing instead of a conventional rolling bearing ( 697 ), which corresponds to the above-mentioned fixing super repository ( 970 ) is substantially similar.

The base ring, the base disk or the space tower has the supporting wheels or super wheels or at least one supporting super rolling bearing ( 960 ) for supporting the rotating ring rotor. In this case, the ring rotor is supported by the main ring, intermediate ring or the inner central ring of the single or the lower macro ring. The supporting super-rolling bearing has two concentric rings ( 961 . 962 ) without / with intermediate bars ( 965 ) and horizontal axis smooth load wheels ( 96 ) or load balls with relatively small fixing rolling bearings ( 966 ) or magnetic holders, which are fastened between these rings. The magnet holder ( 968 / 969 ) has a magnet ( 969 ) on the side of the Load wheel or the load ball and a magnet ( 968 ) on the side of one of said concentric rings and the poles of the same name of the magnets are arranged against each other and the cone concavity of a magnet corresponds to the cone convexity of other magnet, the magnets on the side of the load wheel or the load ball or the load roller normally directly arranged in front of each other or replaced by a single double inner magnet.

The ring rotor is fixed relative to the center of the wind turbine thanks to a concentric neck ring of the wind rotor carrier or a fixed approximately cylindrical or polygonal construction which stands alone or is part of the wind rotor carrier. In this case, the ring rotor by a circle of fixed vertical axes wheels or super wheels, a fixing Superwälzläger ( 970 ) and / or other roller means arranged along a concentric circular line, eg the gears in the electric generators, which are arranged on the wind rotor carrier or on another stationary base fixed.

The fixing super-rolling bearing has two parallel rings ( 971 . 972 ) with / without intermediate beam, vertical axis smooth load wheels ( 97 ) or load balls or load rollers with the relatively small fixing rolling bearings ( 976 ) or magnetic holders ( 978 / 979 ), which are fastened between these rings, and relatively small supporting wheels ( 974 ) with relatively small bearings, which are located on the lower side of the lower ring ( 972 ) by devices ( 973 ) or supporting parallel magnetic rings ( 972 . 982 ), whose poles of the same name are arranged against each other, or a relatively small supporting super rolling bearing. The magnets, which are located on the side of the load wheel or the load ball or the load roller, are normally arranged directly in front of each other or replaced by a single double inner magnet.

Comment on the solution 1.

On the first look could it seems that the supportive Wheels because of the friction one inadmissible huge To offer resistance. That would but a false bias. The ring rotor with its macro guides, the a large ratio area / weight have, and its macro rings, which have a large diameter / weight ratio, is much more powerful as the wind rotors of the horizontal axis wind turbines and the usual Vertical Achsenen wind turbines and the electric generators, which are usually along one Boundary ring of the ring rotor far from the central vertical axis are able to afford much greater resistance as the supporting wheels. If The relationship From the wheel diameter to the diameter of the wheel bearing is large, the inner part of the rolling friction be relatively low and smooth Tires of the supporting wheels could be the outer part reduce the rolling friction. Thanks to the supportive Wheels will be the demands on the strength of the wind rotor eased and she are unlike the central bearing, which normally in the conventional Vertical axis wind turbines is used, easily replaceable.

The supportive Super Rolling has opposite a rolling bearing and opposite the supporting one wheels lower friction losses, because the Wälzläger its load wheels or Loadballs are relatively small, do not share the main load and protect the load wheels or load balls before friction with each other and with the guide rail, which in this case has a low concavity and small sidewalls or at all is missing. When using the magnet holder it works even better.

The supportive Super wheels based on the inner super rolling bearings, the opposite the conventional one Wälzlägern the have described benefits. The supporting super wheels make the rolling friction lower and the supportive Superwälzläger make the rolling friction even lower, because part of the friction at they lack. The supporting ones Super wheels but have opposite the supporting one Super Rolling an advantage described in the commentary on solution 9.

The Superwälläläger and the super wheels can Withstand huge loads, what the super size of vertical axis wind turbines allows. The fixing super rolling bearing and the fixing super wheels have opposite a fixing rolling bearing and opposite similar to the fixing wheels Advantages.

Because the speed of the wind and the number of revolutions of the wind turbine do not change, no matter how far you measure them from the center of the wind turbine the rotor blades with different distances differently loaded from the center of the wind turbine and the reduces the effectiveness. Therefore, it is important that the macro rings with a relatively lower Effort a big one Distance between the macrographs and the center of the wind turbine enable. Furthermore to disturb the macrogates less each other when the distance to the center of the Wind turbine is larger.

There is an opinion that the horizontal axis wind turbine is higher and have better wind conditions at altitude. But that's easy with the size of the wind turbine and the Ge country conditions. If the vertical axis wind turbine is erected on a hill or has a sufficient size, the horizontal axis wind turbine on this side have no advantages. For the proposed invention, it is possible to orient about 50 m, the height of the wind rotor about 200 m, the width of each macrogitter about 100 m and the diameter of the wind rotor about 400 m, depending on the height of the wind rotor carrier. In addition, the offshore sector is essentially meant. It is difficult to imagine a horizontal axis wind turbine with the 400m wind rotor.

Of the Diameter of a wind turbine according to the proposed invention is preferably 4 times as big as the width of a macrogitter. A large diameter reduced under the same latitudes the macrographs the mutual interference of the Macrogitter and / or makes use of 6 to 8 macrogrids per Windrotor '' and the corresponding increase the power possible.

2nd solution, which is connected to the solution 1. For example, 4 . 9 . 10 . 34 . 42 . 74 . 80 . 94 . 95 . 97 ,

Each macro grid ( 11 ) has at least one rotor blade ( 1 . 1K ) per cell ( 57 ), which is not cut off and is not used for other purposes. Each rotor blade is equipped with 2 barrier dampers ( 500 ) connected. Each damper performs the blocking function and the damping function, is located in the cell or between the adjacent cells and, in some embodiments, simultaneously serves two rotor blades from the adjacent cells.

Comment on the solution 2.

Under the name rotor blade ( 1 . 1K ) is a rotor blade ( 1 ) or a complementary rotor blade ( 1K ), which is a special variant of the rotor blade. The use of the complementary rotor blades together with the normal rotor blades eliminates the asymmetric stresses that a strong wind generates in the wind rotor. In the vertical axis wind turbines must be the rotor blades in the specific positions for a portion of the rotation period lock and at the same time dampen the wind gusts. These functions correspond to the damper. The damping of the gusts of wind allows the construction of large and at the same time light macroroids, which is important for the use of the weak wind. It is more important to have a larger area with the damping of the gusts of wind than to intercept the entire corresponding wind within a small area without damping the gusts of wind. The different versions of the rotor blades and the silencer in the solutions 41 to 79 and 34 to 99 provide a sufficient basis for the successful implementation of the proposed wind energy system.

ever smaller the rotor blades are, the more of them the macro grid has. The more rotor blades in a macro grid are installed, the smaller their sizes are compared to the size of the whole wind turbine, the further away they are from the center of the wind turbine and the lower the line speed of its ends compared to Macrogitter, what the aerodynamic properties and functionality the wind turbine improves. A similar role also plays the absolute size of the wind turbine. The bigger the Wind turbine is, the less the rotor blades make vibrations per minute, the less friction and the less is the unproductive resistance of the air. That's why even one has to test piece be relatively large. This is also in connection with the wind rotor carrier effort important. At the small size can one to fallacies come.

3. Solution connected to solution 1 or 2. For example, 1 . 4 . 8th . 10 . 19 . 20 . 21 . 22 ,

The wind turbine has a central approximately cylindrical or polygonal tower ( 14 ) standing alone or part of the Winrotor carrier. A circle of fixed vertical axes wheels or super wheels or a fixing super rolling stock ( 970 ) is arranged on the central tower thanks to appropriate devices.

Comment on the solutions 3 and 1.

Even though the ones mentioned below Transmission at the below mentioned Electric generators, air pumps and valve air turbines in essence fix the wind rotor (ring rotor), is the circle row of fixing wheels or super wheels or a fixing Superwälzläger preferred. This provides more safety and a reduction in friction through the Uncoupling of time-unused transmission.

thanks the macro rings, which are fixed by the central tower, become The demands on the strength of the macro grid are relaxed. If the central tower used intensively in the construction of the wind turbine and then simultaneously for Different purposes is used, the effort is compensated.

4. Solution, which is connected to one of the solutions 1 to 3. 1 . 4 . 5 . 6 . 23 . 24 . 25 ,

The inner central rings ( 162 ) the MA kerrings ( 12 . 16 . 116 ) use intermediate parts to create a cylinder ( 114 ) on supporting wheels or super wheels or on a supporting super rolling bearing ( 960 ) and ^normally by a series of fixed vertical axis wheels or super wheels or a fixed super rolling bearing ( 970 ) and through the central tower ( 14 ) fixed.

Comment on the solution 4.

A Variant in which the mentioned Cylinder alone supports the whole ring rotor is possible. Whether such a variant would be useful but depends on the materials and technologies used. Expected is this variant (... alone the ...) not suitable for the largest wind turbines.

5. Solution, which is connected to one of the solutions 1 to 4. 7 . 8th . 9 . 10 . 23 . 24 . 25 ,

If the ring rotor only a single macro ring ( 16 ), the ring rotor is supported on supporting wheels or super wheels or on a supporting super rolling bearing ( 960 ) through the inner central ring ( 162 ) or by an intermediate ring ( 236 ), which belongs to the macro ring and is located between the macro grid ( 11 ) and the inner central ring, or, if the macro grid has a corresponding cutout, through the main ring ( 161 ), which in any case passes through the equilibrium or wind power center of the macro grid.

6. Solution, which is connected to one of the solutions 1 to 5. 1 . 4 ,

Each main ring ( 36 . 161 ) of each macro ring ( 12 . 16 . 161 ) has a tube structure or a more complicated carcass structure having 3 to 9 sub-rings and bars therebetween. The beams are usually arranged at approximately 60 ° angle to each other. The beams and sub-rings normally each have aerodynamically calculated shells or a common aerodynamically calculated sheath.

Comment on the solution 6.

The Structure of the macro ring is the structure of the wheel of the bicycle essentially similar. The relationship · Great strength / weight is for the wheels the bike very well. Thanks to the solution 4, this ratio is for the macro ring even better. In the manufacture of the subrings and the beams can one or the same Technology, as in the production of the propellers of modern Horizontal axis wind turbines, use.

7. Solution connected to one of solutions 1 to 6. 1 . 4 . 7 . 8th . 23 . 24 . 25 ,

The Superrad ( 169 ) has an inner cylinder 880 , an outer ring 660 and two super rolling bearings in between. Each super rolling bearing ( 697 ) has two parallel rings ( 691 . 692 ) with / without intermediate connections, horizontal-axis smooth load wheels ( 197 ) or load balls or load rollers with the relatively small fixing rolling bearings ( 696 ) or magnetic holders ( 698 / 699 ), which are fastened between these rings, and relatively small fixing wheels ( 694 ) with relatively small rolling bearings located on the outer side of the inner ring ( 692 ) by holder ( 693 ) and between a neck ring ( 882 ) of the inner cylinder and a neck ring ( 661 ) of the outer ring, or fixing parallel magnetic rings ( 691 . 791 ) and fixing parallel magnetic rings ( 692 . 792 ), whose eponymous poles are arranged against each other, wherein the magnetic ring ( 791 ) on the attachment ring ( 661 ) or integrated with it and the magnetic ring ( 792 ) on the attachment ring ( 882 ) or integrated with it.

8. Solution, which is connected to one of the solutions 1 to 7. 1 . 4 . 7 . 8th . 23 . 24 . 25 ,

For each supporting wheel or superad ( 169 ) are holders ( 688 ), which support this wheel or super wheel, and screw supports ( 168 ), usually by a ramp ( 680 ) are interconnected.

Each screw support has a threaded part ( 681 ), a four- or six-sided grip part ( 682 ) and a smooth round foot part ( 683 ) on. The threaded part of the screw support corresponds to a threaded opening of the holder or the ramp corresponds, the / there a cylinder ( 687 ) having. If the super wheels are used, the brackets support the inner cylinder ( 880 ) of the super wheel directly or by means of a central inner cylinder ( 888 ) without turning.

Comment on the solution 8.

thanks the screw supports You can see inaccuracies of the construction and the instability of the reason compensate and thanks to the wheels or super wheels you can use the room supports without base ring use.

9. Solution connected to one of solutions 1 to 8. 1 . 4 . 7 . 8th . 9 . 10 ,

Within each macrogitter ( 11 ) takes the durability of its cells ( 57 ), the durability of the rotor blades ( 1 . 1K ) and the resilient resistance of Catch damper ( 500 ) from its outer edges to its attachment site. If the cells, rotor blades and barrier dampers are located relatively far from the attachment site of the macrogrid, they have lightweight materials and / or lightweight construction structure, which allows the use of low wind and partial use of fresh wind, and leave the Rotor blades thanks to the weak resilient resistance of the damper the strong and stormy wind through.

If the cells, rotor blades and damper not too far from the attachment site of the macrogitter they have medium and / or medium design features on, what the use of the fresh wind and partly the use the weak wind allows and leave the rotor blades thanks to the moderate springy resistance the barrier damper the storm wind through. If the cells, rotor blades and damper are relative near the fortification site Makrohitters, they have particularly durable fabrics and / or particularly durable construction structure on what the use of the strong and stormy wind and partly allows the use of the fresh wind, and leave the rotor blades thanks to the strong resistance of the damper only the strong gusts of wind through.

Comment on the solution 9.

These solution and damping allow the gusts of wind the construction of huge and at the same time light macrogrids. Thereby Use the faint wind almost as effectively as the fresh one and the strong wind. The variation of the thicknesses of lines in the Drawings is not a printer error, this illustrates the idea.

10. Solution, which is connected to one of the solutions 1 to 9. For example, 1 . 4 . 8th . 9 . 10 ,

Each macro grid ( 11 ) has the shape of a rectangle up to a circle, and if the macrogitter does not have a right circular shape, the height of the macrogitter is preferably larger than its width.

Comment on the solution 10.

The prefers larger ratio of Height too the width reduces the differences between the distances of the rotor blades up to the center of the wind turbine, what are the differences between reduced the line speeds of the various rotor blades. Furthermore reduces this ratio under the same diameter of the wind turbine the reciprocal Disorders of Macrogitter and / or makes use of 6 to 8 macrogrids per Wind rotor and the corresponding increase in power possible.

11. Solution associated with any of solutions 1 to 10. 7 . 8th . 9 ,

Each macro grid ( 11 ) has vertical ( 536 ) and usually horizontal ( 736 ) Stiffening ribs, which extend over the whole of its height or width. The strength and / or thickness of these stiffening ribs normally increases from the outer edges of the macrogitter to its attachment site.

12th solution, which is connected to one of the solutions 1 to 11. 9 ,

Each macro grid has a frame ( 33 ), which usually has 4 main parts. According to the shape of the macrogitter, this frame is in the form of a rectangle up to a ring.

13. Solution associated with any of solutions 1 to 12. 34 . 42 . 74 . 80 ,

Each macro grid ( 11 ) has horizontal bars ( 310 ), vertical bars ( 320 ) and cross pieces ( 300 ) corresponding to the sides and corners of its cells.

The crosspieces each have 2 parts ( 300L . 300R ), which are inserted in the adjacent bars.

Comment on the solution 13.

The Division of the cross pieces facilitates the construction of the macrogitter. In the production of the beams can one or the same Technology, as in the production of the propellers of modern Horizontal-axis wind turbines, use.

14. Solution associated with one of solutions 1 to 13. For example, 34 ,

Each macro grid ( 11 ) has at the edges of its horizontal and vertical bars perforations, recesses, elevations or railways ( 789 ), which are necessary for an autonomous Auf / Querzug.

Comment on the solution 14.

The autonomous up / traverse must be a support for an automaton or robot that installs, uninstalls and cleans the rotor blades and could be replaced by friction or gears with motors and additional pneumatic drives or by reciprocating pneumatic means and to move additional pneumatic drives.

15. Solution associated with any of solutions 1 to 14. 10 . 11 . 12 . 13 . 14 ,

Each macro grid has the circular shape and a ring frame ( 733 ) on. The ring frame has a tube structure or a more complicated carcass structure having 3 to 9 sub-rings and bars therebetween. The beams are usually arranged at approximately 60 ° angle to each other. The sub-rings and the beams normally each have aerodynamically calculated sheaths or a common aerodynamically calculated sheath.

16. Solution that is connected to the solution 15. 10 . 11 . 12 . 13 . 14 ,

Each macro grid ( 11 ) has a central base ( 761 ), which is at the same time a part of the main ring of the macrogitter. This base has a simple cylinder structure or a more complicated carcass structure having 3 to 9 tubes along the rotational direction and beams therebetween. The beams are usually arranged at approximately 60 ° angle to each other. The tubes and the beams normally each have aerodynamically calculated shells or a common aerodynamically calculated sheath. The width of the ring frame is greater than the width of a rotor blade. Between the ring frame and the end faces of the central base are spokes ( 763 ) spanned.

17. Solution associated with the solution 16. 11 . 13 . 94 . 95 ,

Rods, ropes or ties ( 920 ) are arranged at 60 ° to 120 °, preferably 90 °, angle to each other, on the ring frame ( 733 ) and fastened together at the common crossings. These bars, ropes or ties constitute the main structure of the macrogitter.

18. Solution connected to the solution 17. 13 . 94 . 95 . 96 . 100 ,

The rods, ropes or bands ( 920 ) are. arranged at 30 ° to 60 °, preferably 45 °, angle relative to the vertical and at the common intersections by the corresponding holder ( 600 ), each with at least one damper ( 500 ), or fastened together in some other way.

19. Solution associated with any of solutions 1 to 18. For example, 1 . 8th . 9 . 10 ,

The wind turbine normally has electric generators on the wind rotor support ( 89 ), through the gears ( 80 ) with the ring rotor and / or by the below-mentioned intermediate gear ( 88 . 988 ) with the lower-mentioned valve air turbines ( 99 ) connected. If the transmission ( 80 ), they have a friction or tooth-ring strip or friction or tooth-approach ring ( 26 ) of the single or lower macro ring, a roller contact, or a rotating or roller contact with the supporting wheels or super wheels.

Comment on the solution 19.

These. Circular structure reduces demands on gear ratios the gearbox and makes it easy, the number of electric generators flexible to vary. In the general case, each gearbox has the gear ratio of 1 / n to m, usually 1, and the number of stages from 1 to k, usually 1, on. To the wind adaptation skills To do even better, however, is a few steps in any case useful. Furthermore you can dynamically control the number of electric generators. ever stronger the wind is, the more the number of electric generators, the more to be used.

20. Solution associated with one of solutions 1 to 19. 1 . 26 . 33 ,

Around the center of the wind turbine is at least one super electric generator ( 890 ) arranged a circle series of windings with the cores ( 891 ) on the wind rotor carrier and a circle series of magnets ( 892 ) on a magnet carrier ring ( 894 ), which is normally a lower attachment ring of the ring rotor.

Comment on the solution 20.

The relationship Performance / effort is for the super electric generator better than for the normal electric generators. The bond of the super electric generator to a wind energy storage buffer is however, more complicated.

21. Solution connected to the solution 20. 1 . 26 . 33 ,

With the super electric generator ( 890 ) is a super-transmission ( 893 ), which determines the distance between the circular row of windings with the cores ( 891 ) and the circle series of magnets ( 892 ) varies. The super gear is connected to the cores in the windings and usually divided according to the number of these cores.

Comment on the solution 21.

Thanks to this solution, the wind adaptability of the super electric generator is better than the wind adaptability of the normal ones Electric generators. It makes sense to use both the super electric generator and the normal electric generators.

22. Solution associated with any of solutions 1 to 21. 27 ,

The wind turbine has compressed air reservoirs ( 100 ), Air pumps ( 79 ) with the gears ( 70 ), which are used for the storage of wind energy by the compression of the air, and the valve air turbines ( 99 ), which are used for the use of compressed air on. The air turbines are connected to the electric generators ( 89 ) through the intermediate gear ( 988 ) connected. The electric generators are not connected to the ring rotor.

Comment on the solutions 22 to 30.

These solutions describe different versions Wind Energy Storage Buffer That the compressed air used. The air pumps or the valve air turbines, which fulfill the function of the air pumps due to time, are used when the electric generators can not exploit all the wind energy. If the wind is too strong, the electric generators and the air pumps work at the same time or the air pumps work alone. You can do that Number of air pumps dynamically steurn. The stronger the wind, the more is the number of air pumes used. When the wind is too weak is, the compressed air enters the valve air turbines and they turn directly or through the intermediate gear, the rotors of the electric generators.

23. Solution associated with any of solutions 1 to 21. 28 ,

The wind turbine has compressed air reservoirs ( 100 ), Air pumps ( 79 ) with the gears ( 70 ), which are used for the storage of wind energy by the compression of the air, and the valve air turbines ( 99 ), which are used for the use of compressed air on. The air turbines are connected to the electric generators ( 89 ) through the intermediate gear ( 988 ) connected. The electric generators are also connected to the ring rotor through the gears ( 80 ) connected.

24. Solution associated with any of solutions 1 to 21. 29 ,

The wind turbine has compressed air reservoirs ( 100 ), Valve air turbines ( 99 ) with the gears ( 98 ), which are used for the storage of wind energy by the compression of the air, and the valve air turbines ( 99 ), which are used for the use of compressed air on. The last air turbines are with the electric generators ( 89 ) by intermediate gear ( 988 ) connected. The electric generators are not connected to the ring rotor.

25th solution, which is connected to one of the solutions 1 to 21. 30 ,

The wind turbine has compressed air reservoirs ( 100 ), Valve air turbines ( 99 ) with the gears ( 98 ), which are used for the storage of wind energy by the compression of the air, and the valve air turbines ( 99 ), which are used for the use of compressed air on. The last air turbines are with the electric generators ( 89 ) by intermediate gear ( 988 ) connected. The electric generators are also connected to the ring rotor through the gears ( 80 ) connected.

26. Solution associated with any of solutions 1 to 21. 31 ,

The wind turbine has compressed air reservoirs ( 100 ) and valve air turbines ( 99 ) with the gears ( 98 ), which are used for the storage of wind energy by the compression of the air and also for the use of compressed air on. The air turbines are connected to the electric generators ( 89 ) through the intermediate gear ( 988 ) connected. The electric generators are not connected to the ring rotor.

27. Solution associated with any of solutions 1 to 21. 32 ,

The wind turbine has compressed air reservoirs ( 100 ) and valve air turbines ( 99 ) with the gears ( 98 ), which are used for the storage of wind energy by the compression of the air and also for the use of compressed air on. The air turbines are connected to the electric generators ( 89 ) through the intermediate gear ( 88 ) connected between the gears ( 98 ) and gears ( 80 ) are arranged.

28. Solution connected to one of the solutions 22 to 27. For example, 1 . 7 . 8th . 9 . 10 ,

The gears ( 70 ) and gearboxes ( 98 ) are provided with a friction or tooth-ring strip or friction or tooth-approach ring ( 26 ) of the single or lower macro ring connected by a roller contact or with the supporting wheels or super wheels by a rotary or roller contact.

29. Solution associated with any of solutions 1 to 21. 33 ,

The wind turbine has compressed air reservoirs ( 100 ), Air pumps ( 79 ) with the gears ( 70 ) or valve air turbines ( 99 ) with the gears ( 98 ), which are used for the storage of wind energy by the compression of the air, and the valve air turbines ( 99 ) with the gears ( 98 ), which for the Use of compressed air can be used. The gears ( 70 . 98 ) are fitted with a friction or tooth strip of the magnet carrier ring ( 894 ) of the super electric generator ( 890 ) is connected by a controllable roller contact and in this case the super-electric generator also has a roller / coupling device ( 895 ), the magnet-carrier ring ( 894 ) with a neck ring ( 896 ) of the ring rotor controllably binds. If the wind turbine does not have air pumps, normally the same valve air turbines are used for both the compression of the air and the use of the compressed air and the change of function through the valves, gears ( 98 ) and the roller / coupling device.

30. Solution connected to one of the solutions 22 to 29. For example, 1 . 9 ,

Each valve air turbine ( 99 ) actually has an air turbine ( 991 ) and an air valve ( 992 ), which controls the connection to a compressed air reservoir.

Comment on the solution 30.

The common name ( 99 ) for the air turbine ( 991 ) and the air valve ( 992 ) is used because of lack of space on some drawings sheets and also for simplification of the text.

31. Solution associated with one of solutions 22 to 30. For example, 1 . 7 . 8th . 9 . 10 ,

Each compressed air reservoir ( 100 ) has the shape of a vertical cylinder with round end faces and is normally equipped with a room support ( 29 ) integrated.

32. Solution associated with one of solutions 22 to 30. 2 ,

All compressed air reservoirs are connected to each other and constitute a compressed air reservoir system, which has at least one compressed air line ( 109 ), which goes to an external compressed air network.

Comment on the solution 32.

The Compressed air network can be used as a power network. If the compressed air network big enough Wind energy is independent of the current wind conditions. Besides, you could the compressed air network for the Use compressed air supplies from some factories. Some productions, who need the compressed air and / or the electric power, could directly in the open spaces These huge wind turbines are set in motion.

33. Solution associated with one of solutions 1 to 32. 1 . 2 . 8th . 9 . 10 ,

The wind turbine has at least one room ( 1010 ) with the electrochemical plants for hydrogen production.

34. Solution that is connected to the solution 33. For example, 1 . 2 . 3 . 8th . 9 . 10 ,

The wind turbine has at least one pressurized hydrogen reservoir ( 1100 ), which normally has the shape of a vertical cylinder with round end faces.

35. Solution connected to solution 33 or 34. 1 . 2 . 3 ,

The wind turbine has at least one reservoir ( 1000 ) with the liquid hydrogen.

36. Solution connected to one of solutions 3 to 35. 8th . 9 . 10 ,

The central tower of the wind turbine is equipped with a compressed air reservoir ( 100 ) or a pressurized hydrogen reservoir ( 1100 ) integrated.

37. Solution connected to one of solutions 1 to 36. 1 . 3 . 8th . 9 . 10 ,

The wind turbine has at least one maintenance room ( 1011 ) on.

Comment on the solution 37.

If security measures in terms of hydrogen does not completely eliminate the risk of explosion, the wind turbine must be serviced by maintenance robots or have to the hydrogen reservoirs are stationed in the tank.

The Concern for maintenance does not necessarily mean that the proposed Wind turbines more maintenance per 1 MW than the conventional wind turbines need. However, a good design must be in any case of maintenance be adjusted. This has a huge wind turbine one Advantage, because the super size of the maintenance without a significant percentage of effort.

38. Solution connected to one of solutions 1 to 37. 1 ,

The wind turbine has at least one coupling vehicle ( 860 ), which has no engine and is placed on a ring track of the wind rotor carrier or on a circular path of a ring ramp of the central tower. The coupling vehicle has upper coupling wheels connected to the ring rotor can be coupled by pneumatic drives and by a flexieblen roller-brake contact. The coupling vehicle also has lower coupling wheels which can couple with the rings of the ring track by means of pneumatic drives and by a flexible roller-brake contact. The coupling wheels usually have vertical axes of rotation.

Comment on the solution 38.

The proposed wind turbine is a complicated system and the coupling vehicle is only one element of this system. Although the coupling vehicle not easy, could it will be detailed by a normal proctection task.

39. Solution connected to one of solutions 1 to 38. 1 ,

The central tower ( 14 ) has an inner elevator tube or an inner elevator shaft with an elevator ( 77 ), which moves through gears with a drive.

40. Solution connected to one of the solutions 2 to 39. 1 . 4 ,

On the central tower ( 14 ) is an upper ramp ( 800 ) dedicated to the discharge of helicopters, arranged directly or by a turn-coupling device. This turn-coupling device couples the ramp to the central tower or ring rotor as needed.

Comment on the solutions 38, 39, 40.

These solutions provide a maintenance traffic.

41. Solution connected to one of the solutions 2 to 40. 34 . 94 ,

Each rotor blade ( 1 . 1K ) is equipped with two barrier dampers ( 500 ), which allow the rotor blade to rotate about a local horizontal axis by 90 ° and are secured to the opposite faces of the rotor blade, usually in the cutouts of the rotor blade. The local horizontal axis of rotation divides the rotor blade into a small part ( 41 ) and a large part ( 42 ) under. The difference between the area of the small part and the area of the big part is so essential and the difference between the weight of the small part and the weight of the big part is so small that normally the wind can turn the rotor blade around the local horizontal axis of rotation. The big part does not necessarily have to be the heaviest and every rotor blade ( 1 ) with the heaviest part normally corresponds to a complementary rotor blade ( 1K ) with the heaviest small part.

42. Solution connected to the solution 41. 35 . 36 . 43 . 44 . 96 . 99 ,

The damper ( 500 ) has a mechanism ( 501 ) for the main functions and handle wings ( 503 ) for the attachment of the rotor blade ( 1 . 1K ) on.

The silencer is connected to the macro grid ( 11 ) or by a holder ( 502 . 600 ) attached to it and has a bearing connection with the holder. The holders are on the vertical bars ( 310 ), Rods, ropes ( 920 ) or bands of the macrogitter or at the intersections of the bars, rods, ropes or bands of the macrogitter. If the ropes, bands or relatively thin rods are used, each holder has at least one groove or fold ( 651 . 652 ) for a staff; a rope or a band and, if it is not directly connected to an adjacent holder, two parts ( 601 . 602 ) on.

43. Solution connected to solution 42. 35 . 36 . 38 . 40 . 41 ,

The mechanism ( 501 ) has a jacket ( 551 ), which holds the handle ( 503 ) and with the holder ( 502 . 600 ) directly or indirectly has a roller bearing connection, an open base cylinder ( 552 ), which is attached to the holder and is located substantially inside the mechanism, a cylinder cover ( 553 ) and a strong winding spring ( 550 ) located in the base cylinder.

The winding spring is attached on the one hand to the bottom of the base cylinder or to the holder and on the other hand to the cylinder cover. The cylindrical part of the cylinder cover has a section within the approximately 90 ° -Winckels and within this section are a Sperrwarze ( 555 ) of the jacket and usually a locking wart ( 554 ) of the base cylinder.

Comment on the solution 43.

The cutout of the cylinder cover releases the rotation of the rotor blade by 90 °. The locking wart ( 555 ) encounters when rotating the rotors by more than 90 ° on the one hand to a limit of the cutout of the cylinder cover and on the other hand to the other limit of the cutout of the cylinder cover and the winding spring attenuated by their expansion or collapse resistance, the effect of the gusts. The locking wart ( 554 ) and one of the boundaries of the cutout of the cylinder cover Ensure an initial tension of the winding spring and the determination of the initial resistance position of the barrier damper.

The operation is similar to the operation of a flat variant of the 39 , which is presented as an illustration of how it works.

44. Solution connected to the solution 43. 38 ,

Between the coat ( 551 ) and the base cylinder ( 552 ) are rolling bearings ( 558 ) arranged.

45. Solution that is connected to the solution 43. 40 . 41 ,

In the inner space of the winding spring ( 550 ) is an inner cylinder ( 556 ) coaxially arranged and on the one hand at the bottom of the base cylinder ( 552 ) or on the holder ( 502 . 600 ) attached. A second inner cylinder ( 559 ) is coaxial with the first inner cylinder ( 556 ), on the one hand on the jacket ( 551 ) and passes through a circular window of the cylinder cover ( 553 ). The first inner cylinder ( 556 ) usually has the larger diameter than the second inner cylinder ( 559 ). Between the two coaxial inner cylinders ( 556 . 559 ) are rolling bearings ( 558 ) arranged.

46. Solution connected to solution 42. 43 . 44 . 96 . 99 . 46 to 57 ,

The mechanism ( 501 ) has a jacket ( 551 ), which holds the handle ( 503 ) and with the holder ( 502 . 600 ) directly or indirectly has a roller bearing connection, an open base cylinder ( 552 ), which is attached to the holder and is located substantially within the mechanism, and at least one sub-damper. The sub damper has a strong bow wave spring or bow coil spring ( 550 ), a one-sided open bow steering cylinder ( 557 ) and a one-sided open bow push cylinder ( 553 ) on.

The bow steering cylinder is on the base cylinder or on a neck ring ( 579 ) of the base cylinder concentrically arranged and fixed. The approach ring of the base cylinder has an everted extension of the base cylinder or a ring with / without spokes ( 5792 ) on. The aforementioned spring, the bow-push cylinder and the bow-steering cylinder of the sub-damper are arranged coaxially around each other. The bow push cylinder is partially in the bow steering cylinder. The mentioned spring is located entirely within this arc cylinder ( 553 . 557 ).

47. Solution connected to the solution 46. 46 . 47 . 48 . 49 ,

The bow wave spring or bow coil spring ( 550 ) is on the one hand at the bottom of the sheet steering cylinder ( 557 ) and on the other hand at the bottom of the bow-thrust cylinder ( 553 ), which allows the expansion of this spring.

The waves or windings of the mentioned spring are arranged along a geometric approximately 270 ° circular arc. The bow steering cylinder ( 557 ) is about 180 °. The bow push cylinder ( 553 ) is more than 180 °, preferably about 270 °. The bow push cylinder has at its bottom a Sperrwarze ( 561 ) on. The coat ( 551 ) indicates outside its free space ( 560 ) between the locking wart ( 561 ) of the sheet-impact cylinder and the open end face of the sheet-impact cylinder, a locking cam ( 555 ) on.

The bow-push cylinder usually has at its bottom nor a backbone ( 562 ), which lies just below its first 561 ), and the base cylinder ( 552 ) or its approach ring ( 579 ) usually has a locking wart ( 554 ), which are opposite the sperm wart ( 562 ) is located.

Comment on the solution 47.

The locking wart ( 555 ) encounters when rotating the rotors by more than 90 ° on the one hand to the front side of the sheet steering cylinder and on the other hand to the locking lug ( 561 ) and the bow corrugated spring or bow coil spring dampens the effect of the gusts of wind through its expansion resistance. The warts ( 554 . 562 ) ensure an initial tension of the mentioned spring and the determination of the initial resistance position of the damper.

48. Solution connected to the solution 46. 50 . 51 . 52 . 53 ,

The waves or turns of the bow wave spring or bow turn spring ( 550 ) are arranged along a geometric approximately 270 ° circular arc. The bow steering cylinder ( 557 ) is about 180 °. The bow push cylinder ( 553 ) is more than 90 °, preferably about 180 °.

The coat ( 551 ) shows in its free space ( 560 ) between the bottom of the sheet steering cylinder and the bottom of the sheet-impact cylinder, a locking wart ( 555 ) on. The base cylinder ( 552 ) normally has in the free space of the shell opposite the bottom of the sheet-piercing cylinder a locking teat ( 554 ) on.

Comment on the solution 48.

The locking wart ( 555 When the rotors are rotated by more than 90 °, on the one hand, they hit the bottom of the bow-steering cylinder and, on the other hand, the bottom of the bow-thrust cylinder and the bow-corrugated spring or bow-coil spring dampens the effect of the gusts of wind through their compression resistance. The locking wart ( 554 ) ensures an initial tension of the mentioned spring and the determination of the initial resistance position of the damper.

49. Solution connected to the solution 46. 54 . 55 . 56 . 57 ,

The undulations or turns of this spring of the bow wave spring or bow coil spring ( 550 ) are arranged along a geometric approximately 360 ° circular arc. The bow steering cylinder ( 557 ) is about 180 °. The bow push cylinder ( 553 ) is more than 180 °, preferably about 270 °.

The bow push cylinder has a locking teat ( 565 ), which is 90 ° in front of its floor. The coat ( 551 ) points between the locking wart ( 565 ) and the bottom of the bow steering cylinder ( 557 ) a locking wart ( 555 ) on.

The bow push cylinder usually still has a backbone ( 564 ), which is just below its first rump. The base cylinder ( 552 ) or its approach ring ( 579 ) normally faces the locking wart ( 564 ) a locking wart ( 554 ) on.

Comment on the solution 49.

The locking wart ( 555 ) encounters when rotating the rotors by more than 90 ° on the one hand to the bottom of the bow-steering cylinder and on the other hand to the locking teat ( 565 ) and the bow-wave spring or bow-coil spring dampens the effect of gusts of wind by their crowding resistance. The locking warts ( 554 . 564 ) ensure an initial tension of the mentioned spring and the determination of the initial resistance position of the damper.

50. Solution connected to solution 42. 43 . 44 . 96 . 99 . 58 to 65 ,

The mechanism ( 501 ) has a jacket ( 551 ), which holds the handle ( 503 ) and with the holder ( 502 . 600 ) directly or indirectly has a roller bearing connection, a base cylinder open on one side ( 552 ), which is attached to the holder and is located substantially within the mechanism, and at least one sub-damper. The sub-damper has a compressed gas space ( 400 ), a one-sided open bow steering cylinder ( 557 ) or compressed gas cylinder and a preferably on one side open bow-push cylinder ( 553 ) or a piston.

The bow steering cylinder is on the base cylinder or on a neck ring ( 579 ) of the base cylinder concentrically arranged and fixed. The approach ring of the base cylinder has an everted extension of the base cylinder or a ring with / without spokes ( 5792 ) on. The bow push cylinder and the bow steering cylinder of the sub-damper are coaxially arranged around each other. The bow push cylinder is partially in the bow steering cylinder. The compressed gas space is limited by the bow steering cylinder and the bow push cylinder.

Comment on the solution 50.

The Helium is preferred as a gas. But you can also air to use.

51. Solution connected to solution 50. 58 . 59 . 60 . 61 ,

The compressed gas devices are arranged along a geometric approximately 270 ° circular arc. The bow steering cylinder ( 557 ) is about 180 °. The bow push cylinder ( 553 ) or piston is more than 90 °, preferably 130 ° to 170 °.

The coat ( 551 ) shows in its free space ( 560 ) between the bottom of the sheet steering cylinder and the bottom of the sheet-impact cylinder, a locking wart ( 555 ) on. The base cylinder ( 552 ) or its approach ring ( 579 ) normally indicates in free space ( 560 ) of the jacket relative to the bottom of the bow-thrust cylinder a Sperrwarze ( 554 ) on.

Comment on the solution 51.

The locking wart ( 555 ) encounters when turning the rotors by more than 90 ° on the one hand to the bottom of the bow-steering cylinder and on the other hand to the bottom of the arc-shock cylinder and the compressed gas damps by its compression resistance, the effect of the gusts. The locking wart ( 554 ) ensures an initial compression of the compressed gas and the determination of the initial resistance position of the damper.

52. Solution connected to solution 50. 62 . 63 . 64 . 65 ,

The compressed gas devices are arranged along a geometric approximately 360 ° circular arc. The bow steering cylinder ( 557 ) is about 180 °. The bow push cylinder ( 553 ) or piston before zugt is more than 180 °, preferably 220 ° to 260 °.

The bow push cylinder has a locking teat ( 565 ), which is 90 ° in front of its floor. The coat ( 551 ) points between the locking wart ( 565 ) and the bottom of the floor steering cylinder a locking wart ( 555 ) on.

The bow push cylinder usually still has a backbone ( 564 ), which lies just below its first 565 ) is located. The base cylinder ( 552 ) or its approach ring ( 579 ) normally faces the locking wart ( 564 ) a locking wart ( 554 ) on.

Comment on the solution 52.

The locking wart ( 555 ) encounters when rotating the rotors by more than 90 ° on the one hand to the bottom of the bow-steering cylinder and on the other hand to the locking teat ( 565 ) and the compressed gas dampens the effect of the gusts of wind by its compression resistance. The locking warts ( 554 . 564 ) ensure an initial compression of the compressed gas and the determination of the initial resistance position of the damper.

53. Solution with one of the solutions 50 to 52 is connected.

The compressed gas space ( 400 ) is with an input ( 454 ) of a compressed gas system of the macrogitter ( 11 ) on the vertical bar ( 320 ) by compressed gas lines ( 450 ) of the barrier damper ( 500 ), a compressed gas coupling device ( 451 ) on the holder ( 502 ) and a complementary compressed gas coupling device ( 452 ) connected to the vertical bar.

Comment on the solution 53.

The Connection with a big one Compressed gas system provides the relative independence of the current productivity of the wind turbine from the wind force.

54. Solution with one of the solutions 50 to 52 is connected.

The compressed gas space ( 400 ) is equipped with a valve or nipple ( 452 ) on the base cylinder ( 452 ) or on the holder ( 502 . 600 ) by compressed gas lines ( 450 ) of the barrier damper ( 500 ) connected.

Comment on the solution 54.

These Variant allows even for the ropes structure of the macrograph take place the use of pressurized gas the springs, which could be heavy. you but must the outflow take the compressed gas into account.

55. Solution with one of the solutions 50 to 52 is connected.

The compressed gas space ( 400 ) is not directly with the compressed gas, but filled with the resilient balls, which have the compressed gas inside. The diameter of such a ball is preferably almost as large as the inner diameter of the arc-impact cylinder.

Comment on the solution 55.

In this case, normally no outgassing of the compressed gas takes place. However, the demands on the wear resistance of these balls are high. A possible execution could, for example, the execution of the 62 be similar to. In the 62 only the balls are missing.

56. Solution connected to solution 42. 43 . 44 . 96 . 99 . 66 to 69 ,

The mechanism ( 501 ) has a jacket ( 551 ), which holds the handle ( 503 ) and with the holder ( 502 . 600 ) directly or indirectly has a roller bearing connection, an open base cylinder ( 552 ), which is attached to the holder and is located substantially within the mechanism, and at least one sub-damper. The sub damper has a strong bow wave spring or bow coil spring ( 550 ) along a 360 ° circular arc.

The mentioned spring is on the base cylinder or on a neck ring ( 579 ) of the base cylinder concentrically arranged and at a fixing point ( 571 ) by the two their ends and usually attached an intermediate part. The approach ring of the base cylinder has an everted extension of the base cylinder or a ring with / without spokes ( 5792 ) on.

The mentioned spring or, if it is split, one of its intermediate parts has a locking wart ( 575 ), which is about 180 ° after the attachment point ( 571 is on. The mentioned spring or, if it is divided, one of its intermediate parts, the second locking wart ( 573 ), which is about 90 ° after the first, on. The coat ( 551 ) has a locking wart ( 555 ), which are located between the above-mentioned locking warts ( 573 . 575 ) is located.

The mentioned spring or, when split, one of its intermediate parts usually has the third locking lug ( 574 ), which are among the first ( 575 ), and the base cylinder ( 552 ) or its approach ring ( 579 ) usually also has a locking wart ( 554 ), which opposite to the locking wart ( 574 ) located.

Comment on the solution 56.

The locking wart ( 555 ) encounters the turning of the rotors by more than 90 ° on the one hand to the 575 ) and on the other hand to the locking wart ( 573 ). The locking warts ( 554 . 574 ) ensure an initial tension of the bow wave spring or bow coil spring and the determination of the initial resistance position.

57. Solution connected to the solution 56. 43 . 44 . 96 . 99 . 70 to 73 ,

The mechanism ( 501 ) has a jacket ( 551 ), which holds the handle ( 503 ) and with the holder ( 502 . 600 ) directly or indirectly has a roller bearing connection, an open base cylinder ( 552 ), which is attached to the holder and is located substantially within the mechanism, and at least one sub-damper. The sub damper has a strong bow wave spring or bow coil spring ( 550 ) along a 360 ° circular arc within a concentrically divided hollow steering ring ( 566 . 567 ) with an inner part ( 566 ) and an external part ( 567 ) on.

The inner part ( 566 ) of the hollow steering ring is on the base cylinder or on a neck ring ( 579 ) of the base cylinder concentrically arranged and fixed. The approach ring of the base cylinder has an everted extension of the base cylinder or a ring with / without spokes ( 5792 ) on.

The mentioned spring is at a fixing point ( 571 ) of the inner part ( 566 ) of the hollow steering ring secured by the two ends and usually an intermediate part. The outer part ( 567 ) of the hollow steering ring has a fixed connection ( 572 ) with the changed spring or, if split, with one of its intermediate parts, and no firm connection with the inner part ( 566 ) of the hollow steering ring. The second fixed connection ( 572 ) is located about 180 ° after the fixing point ( 571 ).

The outer part ( 567 ) of the hollow steering ring has two locking lugs ( 565 . 563 ), which are about 90 ° behind each other. The coat ( 551 ) has a locking wart ( 555 ), which are located between the above-mentioned locking warts ( 563 . 565 ) is located.

The outer part ( 567 ) of the hollow steering ring usually has the third retaining lug ( 564 ), which is below the first block ( 565 ), and the base cylinder ( 552 ) or its approach ring ( 579 ) usually also has a locking wart ( 554 ), which opposite to the locking wart ( 564 ) is located.

Comment on the solution 57.

The locking wart ( 555 ) encounters the turning of the rotors by more than 90 ° on the one hand to the 565 ) and on the other hand to the locking wart ( 563 ). The locking warts ( 554 . 564 ) ensure an initial tension of the bow wave spring or bow coil spring and the determination of the initial resistance position. 58. Solution connected to the solution 57. 70 . 71 . 72 , The coat ( 551 ) has inside guide rails ( 568 ), which from the outside the movement of the outer part ( 567 ) of the hollow steering ring and steer.

59. Solution connected to the solution 57. 73 ,

The inner part ( 566 ) of the hollow steering ring and the outer part ( 567 ) of the hollow steering ring have mutually complementary guide rails ( 569 ), which couple the two parts together and allow only the turning against each other.

60. Solution connected to one of solutions 46 to 59. For example, 50 . 51 . 52 . 53 ,

The rolling bearings ( 558 ) are between the base cylinder ( 552 ) and the coat ( 551 ) or between the base cylinder and an inner central cylinder ( 559 ) attached to the mantle or to the handle wing ( 503 ), or between an inner everted extension or an attachment ring ( 549 ) of the base cylinder and the inner central cylinder.

61. Solution associated with one of solutions 2 to 40. 74 . 80 . 95 . 100 ,

Each rotor blade ( 1 ) is equipped with two barrier dampers ( 500 ), which leaves the rotation of the rotor blade about a local vertical or oblique axis by 90 ° to 180 °, preferably about 135 ° for the vertical and preferably about 110 ° for the oblique, and at the opposite end sides of the rotor blade, normally in the cutouts of the rotor blade. The local vertical or oblique axis of rotation divides the rotor blade into a small part ( 41 ) and a large part ( 42 ) under. The difference between the area of the small part and the area of the large part is so essential that the wind around the local vertical or oblique axis of rotation can turn the rotor blade.

Comment on the solution 61.

Opposite the horizontal axis rotor blade ter have the vertical axis and oblique axis rotor blades advantages and disadvantages.

Advantages. It is not necessary, to pick them up. They are within the greater part of the rotation period active.

Disadvantage. They cause asimmetric stresses in the wind rotor. The vertical axis rotor blades strike to once per Rotatio period to the damper.

Conclusion. You need to rather not too far from the attachment site of the Makrogitter be installed. The occupation of the whole area of the macrogitter is but at the moderate resilient Resistance of the damper for the Bent axis rotor blades useful, especially in the oblique Macro lattice structure.

62. Solution that is connected to the solution 61. 75 . 76 . 81 . 82 . 96 . 99 . 100 ,

The damper ( 500 ) has a mechanism ( 501 ) for the main function and handle-wing ( 503 ) for the attachment of the rotor blade ( 1 . 1K ) on.

The silencer is connected to the macro grid ( 11 ) or by a holder ( 502 . 600 ) attached to it and has a bearing connection with the holder. The holders are on the horizontal or sloping bars ( 310 ), Rods, ropes ( 920 ) or tapes of the macrogitter or attached at their crossings. If the ropes, bands or relatively thin rods are used, each holder has at least one groove or fold ( 651 . 652 ) for a rod, a rope or a band and, if it is not directly connected to an adjacent holder, two parts ( 601 . 602 ) on.

63. Solution connected to the solution 62. 75 . 76 . 78 ,

The mechanism ( 501 ) has a jacket ( 551 ), which holds the handle ( 503 ) and with the holder ( 502 . 600 ) directly or indirectly has a roller bearing connection, an open base cylinder ( 552 ), which is attached to the holder and is located substantially inside the mechanism, a cylinder cover ( 553 ), itself a unilaterally opened cylinder with a larger diameter, and a strong winding spring ( 550 ) located in the base cylinder. The winding spring is attached on the one hand to the bottom of the central cylinder and on the other hand to the cylinder cover. The cylindrical part of the cylinder cover has within 90 ° to 180 °, preferably about 135 ° or 110 °, a cutout and within this section there is an inner locking wart ( 555 ) of the coat.

Comment on the solution 63.

The cutout of the cylinder cover releases the rotation of the rotor blade by 90 ° to 180 °, preferably approximately 135 ° or 110 °. The locking wart ( 555 When the rotors are rotated by more than this angle, on the one hand, it encounters a boundary of the section of the cylinder cover and, on the other hand, the other boundary of the section of the cylinder cover, and the winding spring dampens the effect of the wind gusts by its expansion or compression resistance. The locking wart ( 554 ) and one of the boundaries of the section of the cylinder deck ensure an initial tension of the coil spring and the determination of the initial resistance position of the barrier damper. The operation is similar to the operation of a flat variant of the 79 , which is presented as an illustration of how it works.

64. Solution with the solution 63 connected is.

Between the coat ( 551 ) and the base cylinder ( 553 ) are rolling bearings ( 558 ) arranged. If the damper ( 500 ) for the lower position in the vertical axis rotor blade or for the two positions in the oblique axis rotor blade, it has between the shell and the holder ( 502 . 600 ) a supporting or blocking rolling bearing ( 578 ) on.

65. Solution connected to the solution 63. 78 ,

In the inner space of the winding spring ( 550 ) is an inner cylinder ( 556 ) coaxially arranged and on the one hand at the bottom of the base cylinder ( 552 ) or on the holder ( 502 . 600 ) attached. A second inner cylinder ( 559 ) is coaxial with the first inner cylinder ( 556 ), on the one hand on the jacket ( 551 ) and passes through a circular window of the cylinder cover ( 553 ). The first inner cylinder ( 556 ) usually has the larger diameter than the second inner cylinder ( 559 ). Between the two coaxial inner cylinders ( 556 . 559 ) are rolling bearings ( 558 ) arranged.

If the damper ( 500 ) for the lower position in the vertical axis rotor blade or for the two positions in the oblique axis rotor blade is predetermined, it has between the second inner cylinder ( 559 ) and the holder a supporting or blocking rolling bearing ( 578 ) on.

Comment on the solutions 66 to 71.

These solutions can be used for the horizontal axis, vertical axis and oblique axes Ro use torble blades.

66. Solution connected to solution 42 or 62. 43 . 44 . 80 . 81 . 82 . 96 . 99 . 84 ,

The mechanism ( 501 ) has a jacket ( 551 ), which holds the handle ( 503 ) and with the holder ( 502 . 600 ) directly or indirectly has a roller bearing connection, an open base cylinder ( 552 ), which is attached to the holder and is located substantially within the mechanism, and at least one sub-damper. The sub damper has a strong bow wave spring or bow coil spring ( 550 ), a one-sided open bow steering cylinder ( 557 ), a one-sided open bow push cylinder ( 553 ) and a bow-locking device ( 586 ) on. The bow-locking device extends between the shell and the bow-steering cylinder over a 90 ° to 180 °, preferably 90 ° for the horizontal axis rotor blades and preferably 135 ° for the vertical axis rotor blades, arc. The bow-locking device has at its ends locking warts ( 585 . 583 ) and has a firm connection with the bottom of the arch-push cylinder ( 581 ).

The bow steering cylinder is on the base cylinder or on a neck ring ( 579 ) of the base cylinder concentrically arranged and fixed. The approach ring of the base cylinder has an everted extension of the base cylinder or a ring with / without spokes ( 5792 ) on.

The mentioned Pen, the bow push cylinder and the bow steering cylinder of the sub-damper are coaxially arranged around each other. The bow push cylinder is partially in the bow steering cylinder. The mentioned spring is on the one hand at the bottom of the bow-steering cylinder and on the other hand at the bottom of the bow push cylinder attached and located entirely within this arc cylinder.

The bow steering cylinder ( 557 ) is 210 ° to 260 °, preferably about 250 ° for the horizontal axis rotor blades and preferably about 225 ° for the vertical axis rotor blades. The bow push cylinder ( 553 ) is 135 ° to 225 °, preferably about 180 ° for the horizontal axis rotor blades and preferably about 210 ° for the vertical axis rotor blades. The coat ( 551 ) points between the locking warts ( 583 . 585 ) of the bow-locking device a locking wart ( 555 ) on.

Comment on the solution 66.

The locking wart ( 555 ) encounters when rotating the rotors by more than about 90 ° for the horizontal axis rotor blades and more than about 135 ° for the vertical axis rotor blades on the one hand to the locking lug ( 585 ) and on the other hand to the locking wart ( 583 ) and thereby brings the bow-locking device in the movement. The last pushes in its movement in the direction of compression of the spring by the fixed connection ( 581 ) to the open end face of the bow-steering cylinder and during its movement in the direction of expansion of the spring by the fixed connection ( 581 ) and the bottom of the bow-push cylinder to the bottom of the bow-steering cylinder.

67. Solution with the solution 42 or 62 connected is. 43 . 44 . 80 . 81 . 82 . 96 . 99 . 85 ,

The mechanism ( 501 ) has a jacket ( 551 ), which holds the handle ( 503 ) and with the holder ( 502 . 600 ) directly or indirectly has a roller bearing connection, an open base cylinder ( 552 ), which is attached to the holder and is located substantially within the mechanism, and at least one sub-damper. The sub damper has a strong bow wave spring or bow coil spring ( 550 ), a two-sided open bow steering cylinder ( 557 ), two arched push cylinders ( 553 . 588 ) and two bow-locking devices ( 586 . 589 ) on. The bow-locking devices extend between the shell and the bow-steering cylinder over a 90 ° to 180 °, preferably 90 ° for the horizontal axis rotor blades and 135 ° for the vertical axis rotor blades, arc together.

The bow steering cylinder is on the base cylinder or on a neck ring ( 579 ) of the base cylinder concentrically arranged and fixed. The approach ring of the base cylinder has an everted extension of the base cylinder or a ring with / without spokes ( 5792 ) on. The aforementioned spring, the bow-push cylinder and the bow-steering cylinder of the sub-damper are arranged coaxially around each other. The bow push cylinders are partially in the bow steering cylinder. The mentioned spring is located entirely within this arc cylinder.

The first bow-locking device has with the bottom of the first sheet-thrust cylinder ( 553 ) has a fixed connection and has at its end a locking lug ( 585 ) on. The second bow-locking device has with the bottom of the second sheet-thrust cylinder ( 588 ) a fixed connection and has at its end a Sperrwarze ( 583 ) on.

Between the bottom of the first arc collision cylinder and the bottom of the second arc collision cylinder, the base cylinder or its approach ring has a locking cam ( 587 ) on. This Sperrwarze is located about 90 ° after the first open end of the sheet steering cylinder and 10 ° to 60 °, preferably 20 ° for the horizontal axis Rotorblät ter and preferably 45 ° for the vertical axis rotor blades, in front of the second open end of the sheet steering cylinder.

The bow steering cylinder ( 557 ) is 210 ° to 260 °, preferably about 250 ° for the horizontal axis rotor blades and preferably about 225 ° for the vertical axis rotor blades.

The first bow push cylinder ( 553 ) is more than 90 °, preferably about 180 °. The second bow push cylinder ( 588 ) is more than 20 °, preferably about 45 °, for the horizontal axis rotor blades and more than 45 °, preferably about 90 °, for the vertical axis rotor blades.

The coat ( 551 ) points between the locking warts ( 583 . 585 ) the bow-locking devices a locking wart ( 555 ) on.

Comment on the solution 67.

The locking wart ( 555 ) encounters when rotating the rotors by more than about 90 ° for the horizontal axis rotor blades and more than about 135 ° for the vertical axis rotor blades on the one hand to the locking lug ( 585 ) and on the other hand to the locking wart ( 583 ) and thereby brings one of the bow-locking devices in the movement. The first, as it moves in the direction of collapse of the spring, abuts against the first open end of the sheet steering cylinder through the fixed connection with the bottom of the first arc collet cylinder. The second, as it moves in the direction of compression of the spring, abuts against the second open end of the arc steering cylinder through the fixed connection with the bottom of the second sheet-thrust cylinder. The locking wart ( 587 ) ensures an initial tension of the bow wave spring or bow coil spring and the setting of the initial resistance position of the barrier damper.

68. Solution connected to solution 42 or 62. 43 . 44 . 80 . 81 . 82 . 96 . 99 . 86 ,

The mechanism ( 501 ) has a jacket ( 551 ), which holds the handle ( 503 ) and with the holder ( 502 . 600 ) directly or indirectly has a roller bearing connection, an open base cylinder ( 552 ), which is attached to the holder and is located substantially within the mechanism, and at least one sub-damper. The sub-damper has a compressed gas space ( 400 ), a two-sided open bow steering cylinder ( 557 ), two arched push cylinders ( 553 . 588 ) and two bow-locking devices ( 586 . 589 ) on. The bow-locking devices extend between the shell and the bow-steering cylinder over a 90 ° to 180 °, preferably 90 ° for the horizontal axis rotor blades and preferably 135 ° for the vertical axis rotor blades, -Kreisbogen together.

The bow steering cylinder is on the base cylinder or on a neck ring ( 579 ) of the base cylinder concentrically arranged and fixed. The approach ring of the base cylinder has an everted extension of the base cylinder or a ring with / without spokes ( 5792 ) on. The bow push cylinders are partially in the bow steering cylinder. Each sheet push cylinder is arranged coaxially with respect to the sheet steering cylinder. The compressed gas space is located substantially within these arc cylinders.

The first bow-locking device has with the bottom of the first sheet-thrust cylinder ( 553 ) has a fixed connection and has at its end a locking lug ( 585 ) on. The second bow-locking device has with the bottom of the second sheet-thrust cylinder ( 588 ) a fixed connection and has at its end a Sperrwarze ( 583 ) on.

Between the bottom of the first arc collision cylinder and the bottom of the second arc collision cylinder, the base cylinder or its approach ring has a locking cam ( 587 ) on. This Sperrwarze is located about 90 ° after the first open end of the sheet steering cylinder and 10 ° to 60 °, preferably 20 ° for the horizontal axis rotor blades and preferably 45 ° for the vertical axis rotor blades, before the second open end of the sheet steering cylinder.

The bow steering cylinder ( 557 ) is 210 ° to 260 °, preferably about 250 ° for the horizontal axis rotor blades and preferably about 225 ° for the vertical axis rotor blades.

The first bow push cylinder ( 553 ) is more than 90 °, preferably about 180 °. The second bow push cylinder ( 588 ) is more than 20 °, preferably about 45 °, for the horizontal axis rotor blades and more than 45 °, preferably about 90 °, for the vertical axis rotor blades.

The coat ( 551 ) points between the locking warts ( 583 . 585 ) the bow-locking devices a locking wart ( 555 ) on.

Comment on the solution 68.

The locking wart ( 555 ) encounters when rotating the rotors by more than about 90 ° for the horizontal axis rotor blades and more than about 135 ° for the vertical axis rotor blades on the one hand to the locking lug ( 585 ) and on the other hand to the locking wart ( 583 ) and thereby brings one of the bow-locking devices in the movement. The first bumps in the direction of compression as it moves of the pressurized gas through the fixed connection with the bottom of the first arc collision cylinder to the first open end of the sheet steering cylinder. The second, as it moves in the direction of compression of the pressurized gas through the fixed connection with the bottom of the second sheet-thrust cylinder, abuts against the second open end of the sheet steering cylinder. The locking wart ( 587 ) ensures an initial compression of the compressed gas and the determination of the initial resistance position of the barrier damper.

69. Solution with the solution 68 connected is.

The compressed gas space ( 400 ) is with an input ( 454 ) of a compressed gas system of the macrogitter ( 11 ) on the vertical bar ( 320 ) by compressed gas lines ( 450 ) of the barrier damper ( 500 ), a compressed gas coupling device ( 451 ) on the holder ( 502 ) and a complementary compressed gas coupling device ( 453 ) connected to the vertical bar.

Comment on the solution 69.

The part of the execution can be found in the 59 . 60 . 61 Find. The connection with a large compressed gas system provides the relative independence of the current productivity of the wind turbine from the wind force.

70. Solution with the solution 68 connected is.

The compressed gas space ( 400 ) is equipped with a valve or nipple ( 452 ) on the base cylinder ( 452 ) or on the holder ( 502 . 600 ) by compressed gas lines ( 450 ) of the barrier damper ( 500 ) connected.

Comment on the solution 70.

The part of the execution can be found in the 63 . 64 . 65 Find. This variant allows even for the rope structure of the macrogrid the use of compressed gas instead of the springs, which could be heavy. But you have to take the outflow of the compressed gas into consideration.

71. Solution with the solution 68 connected is.

The compressed gas space ( 400 ) is not directly with the compressed gas, but filled with the resilient balls, which have the compressed gas inside. The diameter of such a ball is preferably almost as large as the inner diameter of the arc-impact cylinder.

Comment on the solution 71.

In this case, normally no outgassing of the compressed gas takes place. However, the demands on the wear resistance of these balls are high. One possible embodiment could be the execution of the 86 be similar to. In the 86 only the balls are missing.

72. Solution connected to the solution 62. 80 . 81 . 82 . 96 . 99 . 87 ,

The mechanism ( 501 ) has a jacket ( 551 ), which holds the handle ( 503 ) and with the holder ( 502 . 600 ) directly or indirectly has a roller bearing connection, an open base cylinder ( 552 ), which is attached to the holder and is located substantially within the mechanism, and at least one sub-damper. The sub-damper has along a 360 ° arc a strong arc wave spring or bow coil spring ( 550 ) on.

The mentioned spring is on the base cylinder or on a neck ring ( 579 ) of the base cylinder concentrically arranged and at a fixing point ( 571 ) by the two their ends and usually attached an intermediate part. The approach ring of the base cylinder has an everted extension of the base cylinder or a ring with / without spokes ( 5792 ) on.

The mentioned spring or, if it is split, one of its intermediate parts has a locking wart ( 575 ), which is 90 ° to 180 °, preferably 150 °, after the attachment point ( 571 ) is located. The mentioned spring or, if it is split, one of its intermediate parts still has a (second) locking wart ( 573 ), which is 90 ° to 180 °, preferably 135 °, after the first bump ( 575 ) is located. The coat ( 551 ) has a locking wart ( 555 ), which are located between the above-mentioned locking warts ( 573 . 575 ) is located.

The mentioned spring or, if it is split, one of its intermediate parts normally still has a (third) blocking wart ( 574 ), which are under their first bulge ( 575 ), and the base cylinder ( 552 ) or its approach ring ( 579 ) usually also has a locking wart ( 554 ), which opposite to the locking wart ( 574 ) is located.

Comment on the solution 72.

The locking wart ( 555 ) encounters on turning of the rotors by more than about 135 ° on the one hand to the locking teat ( 575 ) and on the other hand to the locking wart ( 573 ) and the bow wave spring or bow coil spring dampens the effect of the gusts of wind. The locking warts ( 554 . 574 ), which one in the 67 . 68 . 69 ensure an initial tension of the mentioned spring and the determination of the initial resistance position.

73. Solution connected to solution 62. 80 . 81 . 82 . 96 . 99 . 88 . 89 ,

The mechanism ( 501 ) has a jacket ( 551 ), which holds the handle ( 503 ) and with the holder ( 502 . 600 ) directly or indirectly has a roller bearing connection, an open base cylinder ( 552 ), which is attached to the holder and is located substantially within the mechanism, and at least one sub-damper. The sub-damper points along a 360 ° arc inside a concentric split hollow steering ring ( 566 . 567 ) a strong arc wave spring or bow coil spring ( 550 ) on. The concentrically divided hollow steering ring has an inner part ( 566 ) and an external part ( 567 ), which have a freedom of rotation against each other.

The inner part ( 566 ) of the hollow steering ring is on the base cylinder or on a neck ring ( 579 ) of the base cylinder concentrically arranged and fixed. The approach ring of the base cylinder has an everted extension of the base cylinder or a ring with / without spokes ( 5792 ) on.

The mentioned spring is at a fixing point ( 571 ) of the inner part ( 566 ) of the hollow steering ring fixed by its two ends and usually an intermediate part. The outer part ( 567 ) of the hollow steering ring has a fixed connection ( 572 ) with the changed spring or, if split, with one of its intermediate parts, and no firm connection with the inner part ( 566 ) of the hollow steering ring. The fixed connection ( 572 ) is located about 180 ° after the fixing point ( 571 ).

The outer part ( 567 ) of the hollow steering ring has two locking lugs ( 565 . 563 ), which are 90 ° to 180 °, preferably 135 °, nacheiander. The coat ( 551 ) has a locking wart ( 555 ), which are located between the above-mentioned locking warts ( 563 . 565 ) is located.

The outer part ( 567 ) of the hollow steering ring usually still has a (third) retaining lug ( 564 ), which are under their first rump ( 565 ) is located.

The base cylinder ( 552 ) or its approach ring ( 579 ) usually also has a locking wart ( 554 ), which opposite to the locking wart ( 564 ) is located.

Comment on the solution 73.

The locking wart ( 555 ) encounters on turning of the rotors by more than about 135 ° on the one hand to the locking teat ( 565 ) and on the other hand to the locking wart ( 563 ) and the bow wave spring or bow coil spring dampens the effect of the gusts of wind. The locking warts ( 554 . 564 ), which one in the 71 . 72 . 73 ensure an initial tension of the mentioned spring and the determination of the initial resistance position.

74. Solution with the solution 73 connected is.

The coat ( 551 ) has inside guide rails ( 568 ), which from the outside the movement of the outer part ( 567 ) of the hollow steering ring and steer.

Comment on the solution 74.

Such guide rails can be found in the 71 . 72 Find.

75. Solution connected to the solution 73. 89 ,

The inner part ( 566 ) of the hollow steering ring and the outer part ( 567 ) of the hollow steering ring, the mutually komlementären guide rails ( 569 ), which couple the two parts together and allow only the turning against each other.

76. Solution associated with one of solutions 66-75. 89 ,

Rolling bearings ( 558 ) are between the base cylinder ( 552 ) and the coat ( 551 ) or between the base cylinder ( 552 ) or its inner approach ring ( 549 ) and an inner central cylinder ( 559 ) attached to the mantle or to the handle wing ( 503 ) is attached, arranged.

If the damper ( 500 ) is predetermined for the lower position in the vertical axis rotor blade or for the two positions in the oblique axis rotor blade, it has between the holder ( 502 . 600 ) and the jacket or between the holder and the inner central cylinder and a supporting or blocking rolling bearing ( 578 ) on.

77. Solution associated with one of solutions 41 to 76. 93 ,

The complementary rotor blade ( 1K ) has the same construction as the rotor blade ( 1 ), but in its small part ( 41 ) a burden ( 911 ).

78. Solution associated with one of solutions 41 to 77. 90 . 92 . 93 ,

Each rotor blade ( 1 . 1K ) has a carcass structure inside. This carcass structure is between the barrier dampers ( 500 ) especially dense and / or fixed and the further from the axis of rotation are their elements, the thinner and / or thinner they are.

79. Solution associated with one of solutions 42 to 78. 90 ,

Each rotor blade ( 1 . 1K ) has coupling devices ( 902 ), which have a carcass structure inside and the handle wings ( 503 ) correspond.

80. Solution connected to one of solutions 41 to 79. 90 ,

Each rotor blade ( 1 . 1K ) has a base part inside the axis of rotation ( 901 ) extending from one damper to the other damper and having an inner carcass structure.

Comment on the solution 80.

The base part ( 901 ) can be made by the same or a similar technology as the propellers of modern horizontal axis wind turbines.

Explanations to the drawings

• Remark 1. Almost all averages and cross sections are polyhedral.
• Note 2. Not all corresponding solutions are usually stated.

1 - wind turbine. Vertical section. Solutions (L) 1, 2, 3, 4.

2 - wind turbine. Cross section 1. L 1, 2, 3, 4.

3 - wind turbine. Cross section 2. L 1, 2, 3, 4.

4 - wind turbine. View. Big distance. L 1, 2, 3, 4.

5 - Wind turbine with 4 macrogrids. At sight. L 1, 2, 3, 4.

6 - Wind turbine with 6 macrogrids. At sight. L 1, 2, 3, 4.

7 - WKA with a macro ring and without a tower. Vertical section (V). L 1, 2, 5.

8th - WKA with a macro ring (MR) and the super wheels. V. L 1, 2, 3, 5, 11.

9 - WKA with an MR and a supporting super rolling bearing. L 1, 2, 3, 5, 10.

10 - WKA with an MR, circle macro gate and a space tower. L 1, 2, 3, 5, 15.

11 - Circle macro grid with a vertical structure. View A). L 15, 16, 17.

12 - Circle macro grid with a vertical structure. Average. L 15, 16, 17.

13 - Circular macro grid with a barrier-running structure. A. L 15, 16, 17, 18.

14 - Circular macro grid with a barrier-running structure. By. L 16, 17, 18.

15 - Supports super rolling bearing (USWL). L 1.

16 - Load wheel or load ball (LR) of the USWL. Side view. L 1.

17 - LR of the USWL with the fixing bearings. Average. L 1.

18 - LR of the USWL with the magnet holders. Average. L 1.

19 - Fixing super rolling bearing (FSWL). L 1.

20 - Load wheel or load ball (LR) of the FSWL. Side view. L 1.

21 - LR of the FSWL with the fixed rolling bearings. Average. L 1.

22 - LR of the FSWL with the fixing magnet holders. Average. L 1.

23 - Super wheel with the screw supports (SS). Page view. L 7,8.

24 - Super wheel with the SS and the fixed wheels in the SWL. By. L 7, 8.

25 - Super wheel with the SS and the magnet holders in the SWL. Average. L 7, 8.

26 - Superelektrogenerator. Unrolled circular arc view (EKBS). L 20, 21.

27 - Wind energy storage buffers and electric generators. DIB. L 22.

28 - Wind energy storage buffers and electric generators. DIB. L 23.

29 - Wind energy storage buffers and Electric generators. DIB. L 24.

30 - Wind energy storage buffers and electric generators. DIB. L 25.

31 - Wind energy storage buffers and electric generators. DIB. L 26.

32 - Wind energy storage buffers and electric generators. DIB. L 27.

33 - Wind energy storage buffer and superelectrogenerator. DIB. L 29.

34 - cell ( 57 ) of the macrogitter with 2 horizontal axis rotor blades. L 41.

35 - Barrier damper with the cylindrical mechanism (ZM). View 1. L 42.

36 - Barrier damper with the cylindrical mechanism (ZM). View 2. L 42.

37 - Rotor blade with the cutouts for the damper (SD). View 1. L 41.

38 - SD with the ZM and the outer rolling bearings. Average. L 43, 44.

39 - Illustration of the working method of the SD with the ZM. L 43.

40 - SD with the ZM and the inner bearings. Average. L 43, 45.

41 - SD with the ZM and the inner bearings. Average. L 43, 45.

42 - Macrogitter cell with 2 horizontal axis rotor blades. L 41, 42, 46.

43 - SD with the wheel mechanism. View 1. L 42, 46.

44 - SD with the wheel mechanism. View 2. L 42, 46.

45 - Rotor blade with the cutouts for the damper. View. L 41, 46.

46 - SD for the horizontal axis rotor blade (HARB). Average. L 46, 47, 60.

47 - Shock absorber (SD) for the HARB. Cross-section. L 46, 47, 60.

48 SD with the attachment ring ( 579 ) for the HARB. Cross-section. L 46, 47, 60.

49 - SD with 2 sub-dampers for the HARB. Cross-section. L 46, 47, 60.

50 - SD for the horizontal axis rotor blade (HARB). Average. L 46, 48, 60.

51 - Shock absorber (SD) for the HARB. Cross-section. L 46, 48, 60.

52 SD with the attachment ring ( 579 ) for the HARB. Cross-section. L 46, 48, 60.

53 - SD with 2 sub-dampers for the HARB. Cross-section. L 46, 48, 60.

54 - SD for the horizontal axis rotor blade (HARB). Average. L 46, 49, 60.

55 - Shock absorber (SD) for the HARB. Cross-section. L 46, 49, 60.

56 SD with the attachment ring ( 579 ) for the HARB. Cross-section. L 46, 49, 60.

57 - SD with 2 sub-dampers for the HARB. Cross-section. L 46, 49, 60.

58 - SD for the horizontal axis rotor blade (HARB). Average. L 50, 51, 53, 60.

59 - Shock absorber (SD) for the HARB. Cross-section. L 50, 51, 53, 60.

60 SD with the attachment ring ( 579 ) for the HARB. Cross-section. L 50, 51, 53, 60.

61 - SD with 2 sub-dampers for the HARB. Cross-section. L 50, 51, 53, 60.

62 - SD for the horizontal axis rotor blade (HARB). Average. L 50, 52, 54, 60.

63 - Shock absorber (SD) for the HARB. Cross-section. L 50, 52, 54, 60.

64 SD with the attachment ring ( 579 ) for the HARB. Cross-section. L 50, 52, 54, 60.

65 - SD with 2 sub-dampers for the HARB. Cross-section. L 50, 52, 54, 60.

66 - SD for the horizontal axis rotor blade (HARB). Average. L 56, 60.

67 - Shock absorber (SD) for the HARB. Cross-section. L 56.

68 SD with the attachment ring ( 579 ) for the HARB. Cross-section. L 56, 60.

69 - SD with 2 Subdämpfern for the Harb. Cross-section. L 56, 60.

70 - SD for the horizontal axis rotor blade (HARB). Average. L 57, 58, 60.

71 - Shock absorber (SD) for the HARB. Cross-section. L 57, 58, 60.

72 - SD with 2 sub-dampers for the HARB. Cross-section. L 57, 58, 60.

73 - SD with the guide rails ( 569 ) for the HARB. Quersch. L 57, 59, 60.

74 - cell ( 57 ) of the macrogitter with 2 vertical axis rotor blades (VARB). L 61.

75 - SD with the cylindrical mechanism (ZM). View 3. L 62.

76 - SD with the cylindrical mechanism (ZM). View 4. L 62.

77 - Rotor blade with the cutouts for the damper (SD). View 2. L 61.

78 - SD with the ZM and a supporting rolling bearing. Through. L 63, 76.

79 - Illustration of the working method of the SD with the ZM for VARB. L 63.

80 - Cell of the macrogitter with 2 vertical axis rotor blades (VARB). L 61, 66.

81 - SD with the wheel mechanism. View 3. L 62, 66.

82 - SD with the wheel mechanism. View 4. L 62, 66.

83 - Rotor blade with the cutouts for the damper. View. L 61, 66.

84 - SD with a push cylinder for the VARB. Average. L 66.

85 - SD with 2 shock cylinders (SZ) for the VARB. Average. L 67.

86 - SD with 2 bedrooms and one pressurized gas room for the VARB. Average. L 68.

87 - SD with a spring for the VARB. Average. L 72.

88 - SD with a spring and split steering cylinder (TLZ) for VARB. L 73.

89 - SD with a spring and a TLZ for the VARB. Cross-section. L 73, 75, 76.

90 - Rotor blade. Average along the main area. L 78, 79, 80.

91 - Rotor blade. Longitudinal section. L 78.

92 - Rotor blade. Cross-section. L 78, 80.

93 - Complementary rotor blade. Cross-section. L 78, 80.

94 - Slanting macrogitter with horizontal axis rotor blades. L 18, 41.

95 - Slanting macrogitter with vertical axis rotor blades. L 18, 61, 62.

96 - Radial double damper with a split holder. L 42, 62.

97 . 98 . 99 - Rotor blade with the damper. The neck ring ( 579 ) with the spokes ( 5792 ) can be seen. View, forehead view, side view. Eg solution 46.

100 - Slanting macrogitter with the bent axis rotor blades. L 18, 61.

Abbreviations in the explanations

• L

  - Solutions

  MR

  - macro ring

  SD

  - Barrier damper

  SWL

  - Super rolling bearing

  USWL

  - Supports super rolling bearing

  FSWL

  - Fixing super rolling bearing

  LR

  - Load wheel or load ball of the Super roller bearing

  SS

  - Screw support

  EKB

  - Unrolled arc view

  ZM

  - Cylindrical mechanism

  Harb

  - Horizontal axis rotor blade

  VARB

  - Vertical axis-rotor blade

SZ - shock cylinders

TLZ - split hollow steering cylinder

Explanations to the reference number

1

rotor blade of the multi-rotor blade module

1K

Complementary rotor blade of the multi-rotor blade module

2

headquarters vertical axis

11

Rotor blade carrier or Macro grid

12

lower Macroring similar to a red discus

14

central tower

16

central Macro ring

26

neck ring of the bottom macro ring connected to gears

29

Space support, which is normally a compressed air reservoir ( 100 )

33

frame of the macro ring

36

main ring of the bottom macro ring

41

Smaller Part of the rotor blade

42

Big part of the rotor blade

57

cell of the macrogitter who in my previous inventions used a multirotor blade module and here 2 relatively big Includes rotor blades

70

transmission for the air pump

77

elevator

79

air pump

80

transmission of the electric generator

88

intermediate gear

89

electric generator

 96

load wheel or load ball of the supporting one Super roller bearing

97

load wheel, Load ball or load rollers of the fixing super-rolling bearing

98

transmission at the air turbine

99

Valve-air turbine, i.e. an air turbine with a valve

100

Compressed air reservoir

109

External compressed air connection

111

wall between the space columns

114

central cylinder

115

Lid part of the central cylinder

116

Upper macro ring, which has the same structure as the central one ( 16 ) having

128

wide Room tower, broad base disc or a combination

161

main ring of the central or upper macro ring

162

central Ring of the central, upper or lower macro ring

163

spoke of the central, upper or lower macro ring

168

Screw Support

169

Super Rad

197

Load wheel of Superwheel Bearing of Super Wheel ( 169 )

206

additional inner ring of the macro ring

236

inner Intermediate ring of macro ring

281

Oberer Ring adapter for the supportive Super Rolling

282

lower Ring adapter for the supportive Super Rolling

300

Crosspiece of the macrogitter

300L

left part of the cross piece of the macrogitter

300R

right part of the cross piece of the macrogitter

306

Additional outer ring of the macro ring

310

horizontal Beams of the macrogitter

314

Flattened part of the horizontal resilient rod ( 333 )

320

vertical Beams of the macrogitter

381

Outer ring spacer for the fixing Super Rolling

382

inner Ring adapter for the fixing super rolling bearings

400

Pressure gas chamber

450

Pressure gas line

451

Compressed gas coupling device on the side of the barrier damper

452

Pressure gas valve or compressed gas nipples

453

Compressed gas coupling device on the side of the macrogitter

454

Compressed gas input of the compressed gas system of the macrogitter

461

bar between the space columns and the central tower

500

locking damper

501

mechanism the Sperrdämpfers

502

holder for the locking damper (SD)

503

Handle-wing of the SDs for the rotor blade

536

vertical Stiffening Rib of the Macrogitter

549

Inner inverted renewal of the base cylinder or an inner ring

550

feather of the SD

551

coat of the SD

552

base barrel of the SD

553

Cylinder cover or push cylinder of the SD

554

gate button for the Determine the initial resistance position of the SD

555

gate button for the Limitation of the angle of rotation of the rotor blade

556

inner Cylinder attached to the holder for attached to the SD

557

Arch-steering cylinder of the SD

558

Roller bearing of the SD

559

inner Cylinder attached to the mantle or handle wings

560

suitor Space of the coat of the SD

561

gate button 1 at the bottom of the bow-push cylinder of the SD

562

gate button 2 at the bottom of the bow-push cylinder of the SD

564

Warp 1 at the bow impact cylinder ( 557 ) or the part ( 567 )

565

Warp 2 on the bow impact cylinder ( 557 ) or the part ( 567 )

566

lower concentric part of the split bow steering cylinder

567

Outer concentric Part of the split bow steering cylinder

568

Steering rail of the shell for the part ( 567 )

569

guiding Split Bow Steering Cylinder Coupling Devices

570

ground the bow push cylinder of the SD

571

Mounting place the spring of the SD

572

Fastening point of the part ( 567 ) on the spring

573

Outer barrier wart the spring opposite the second angle limit

574

Inner Buttress of the spring against the first angle limit

575

Outer barrier wart the spring opposite the first angle limit

578

Supporting roller bearing of the lower barrier damper

579

Inverted extension of the base cylinder ( 552 ) or a ring

5792

Spokes of the ring ( 579 ) attached to the base cylinder of the SD

580

ground the bow steering cylinder of the SD

581

firm Connection between the bow-lock device and the bottom of the bow-push cylinder

583

gate button the bow-locking device opposite the second angle limit

585

gate button the bow-locking device opposite the first angle limit

586

Arch-locking device

587

Starting gate button on the base cylinder

588

second Arches shock cylinder

589

Second Arch-locking device

600

holder for a Pair of barrier dampers at the barrier-running structure

651

Groove or fold of the barrier damper ( 500 ) or the corresponding holder ( 600 )

652

Groove or fold of the barrier damper ( 500 ) or the corresponding holder ( 600 )

660

Outer Ring of the Super Wheel ( 169 )

661

Neck ring of the outer ring ( 660 ) of the super wheel ( 169 )

669

Shaft for the load wheel ( 96 ) of the supporting super-rolling bearing

679

Shaft for the load wheel ( 97 ) of the fixing super-rolling bearing

680

Supporting ramp for the super wheel ( 169 )

681

Screw part of the screw support for the super wheel ( 169 )

682

Handle part of the screw support for the super wheel ( 169 )

683

Foot part of the screw support for the super wheel ( 169 )

687

Cylinder of the supporting ramp for the super wheel ( 169 )

688

Holder of the Superwheel ( 169 )

691

Outer ring of Superwheel Super Wheel ( 169 )

692

Inner ring of Superwheel Super Wheel ( 169 )

693

holder for the Fixing wheel of super rolling bearing of the super wheel

694

Superwheel bearing superwheel fixing wheel ( 169 )

696

Fixing roller bearing of the loadwheel of the Superwheel bearing of the superwheel ( 169 )

697

Super rolling bearing of the Superrad ( 169 )

698

Outer magnet of the magnet holder for the load wheel ( 197 )

699

Inner magnet of the magnet holder for the load wheel ( 197 )

733

circle frame of the Circle Makrogitter

736

horizontal Stiffening Rib of the Macrogitter

761

Basic part of the Circle Makrogitter

763

spoke of the Circle Makrogitter

760

Zwischenverker vehicle

789

Vertiefungen-, Erhöhungen- or railroad track for a cross / elevator

792

Inside Superwheel Bearing Super Magnetic Ring Fixing Ring ( 169 )

800

platform for the Loading and unloading of the helicopter

808

Elevator shaft or elevator shaft cover

880

Inner cylinder of the super wheel ( 169 )

882

Neck ring of the inner cylinder ( 880 ) of the super wheel ( 169 )

888

Central inner cylinder of the super wheel ( 169 )

890

Super-electric generator

891

winding with a core of the super electric generator

892

magnet of the super electric generator

893

lower Ring adapter of the super electric generator

894

Magnetic carrier ring of the super electric generator

895

Roller / Coupling Devices for the Magnet Carrier Ring ( 894 )

896

lower Neck ring of the ring rotor

901

Basic part of the rotor blade

902

holder of the rotor blade

911

load of the complementary rotor blade

920

Schränklaufende bars, Ropes or ribbons of the Macro grid

960

Unterstüttzendes Super Rolling (USWL)

961

Outer concentric Ring of the USWL

962

inner concentric ring of the USWL

965

between joists of the USWL

966

Fixing rolling bearing for the load wheel ( 96 ) of the USWL

968

Outer magnet of the magnet holder for the load wheel ( 96 ) of the USWL

969

inner Magnet of the magnet holder for the loadwheel (96) of the USWL

970

bandage Super Rolling (FSWL)

971

RAISED Ring of the FSWL

972

lower Ring of the FSWL

973

holder for the supportive Wheel of the FSWL

974

Supporting Wheel of the FSWL

976

Fixing rolling bearing for the load wheel ( 97 ) of the FSWL

978

Outer magnet of the magnet holder for the load wheel ( 97 ) of the USWL

979

Inner magnet of the magnet holder for the load wheel ( 97 ) of the USWL

982

supporting Magnetic ring of the FSWL

988

intermediate gear

991

air turbine

992

Valve at the air turbine

1000

reservoir with the liquid hydrogen

1010

room with electrochemical plants (electrolysis → hydrogen)

1011

maintenance room

1100

reservoir with the pressure hydrogen

5792

Spokes of the ring ( 579 ) attached to the base cylinder of the SD

Claims (80)

Wind turbine, characterized in that it has such a wind rotor with the vertical axis ( 2 ), such as a ring rotor mentioned below and such a wind rotor carrier, such as a space tower ( 28 ), a circular row of room columns ( 29 ), a base ring ( 66 ), a base ring with supports, a base disc, a base disc with supports or a combination thereof ( 128 ) with / without intermediates ( 111 . 461 ) and the space tower is normally wide and has little difference from the base disk, and the ring rotor has at least one macro ring ( 12 . 16 . 116 ) and at least three rotor blade carriers ( 11 ), which have fixed connections with the macro rings, and each rotor blade carrier normally has a large number of rotor blades ( 1 . 1K ) with the horizontal and / or vertical and / or oblique local axes and here as macro grid ( 11 ) and each macro ring has a main ring ( 36 . 161 ), usually also an inner central ring ( 162 ), which is connected to the main ring by spokes ( 163 ) or ropes, in the many cases also an inner intermediate ring ( 236 ) and sometimes additional inner ( 206 ) and / or outer ( 306 ) Has rings and the main ring under the macrographs or by the macrogitter goes opposite to its equilibrium vertical lines or to its direct wind power vertical lines and the space supports ( 29 ) supporting wheels or super wheels ( 169 ), over which the ring rotor rotates, and the ring rotor does not have its own supporting wheels and is supported by the main ring or intermediate ring of the single or lower macro ring and the superrad instead of a conventional rolling bearing a super rolling bearing ( 697 ), which corresponds to the above-mentioned fixing roller bearing ( 970 ) is substantially similar, and the base ring, the base disk or the space tower, the supporting wheels or super wheels or at least one supporting super rolling bearing ( 960 ) for supporting the rotating ring rotor and the ring rotor is supported by the main ring, intermediate ring or the inner central ring of the single or the lower macro ring and the supporting super rolling bearing two concentric rings ( 961 . 962 ) without / with intermediate bars ( 965 ) and horizontal axis smooth load wheels ( 96 ) or load balls with relatively small fixing rolling bearings ( 966 ) or magnetic holders, which are fastened between these rings, and the magnet holder ( 968 / 969 ) a magnet ( 969 ) on the side of the load wheel or the load ball and a magnet ( 968 ) on the side of one of said concentric rings and the poles of the same name of the magnets are arranged against each other and the cone concavity of a magnet of the cone convexity of another magnet and the magnets on the side of the load wheel or the load ball or the load roller normally directly in front of each other are arranged or replaced by a single double inner magnet and the ring rotor with respect to the center of the wind turbine thanks to a concentric approach ring of the wind rotor carrier or a fixed approximately cylindrical or polygonal construction, which stands alone or part of the wind rotor carrier fixed and the ring rotor is characterized by a series of fixed vertical axis wheels or super wheels, a superposition roller bearing ( 970 ) and / or other roller means arranged along a concentric circle line, eg the gearboxes in the electric generators, which are arranged on the wind rotor carrier or on another stationary base, and the fixing super rolling bearing has two parallel rings ( 971 . 972 ) with / without intermediate beams, vertical axis smooth load wheels ( 97 ) or load balls or load rollers with the relatively small fixing rolling bearings ( 976 ) or magnetic holders ( 978 / 979 ), which are fastened between these rings, and relatively small supporting wheels ( 974 ) with relatively small bearings, which are located on the lower side of the lower ring ( 972 ) by holder ( 973 ) or supporting parallel magnetic rings ( 972 . 982 ), whose like poles are arranged against each other, or has a relatively small supporting super rolling bearing and the magnets, which are located on the side of the load wheel or the load ball or the load roller, normally placed directly in front of each other or replaced by a single double as large inner magnet , Wind power plant according to claim 1, characterized in that each macro grid ( 11 ) at least one rotor blade ( 1 . 1K ) per cell ( 57 ), which is not cut off and is not used for any other purpose, and each rotor blade with 2 stopper dampers ( 500 ) is connected and each damper the blocking function and the damping function meets, in the cell or between the be adjacent cells is located and served in some versions simultaneously two rotor blades from the adjacent cells. Wind power plant according to claim 1 or 2, characterized in that it has a central approximately cylindrical or polygonal tower ( 14 ), which stands alone or is part of the Winrotor carrier, and a circle row of fixing vertical axes wheels or super wheels or a fixing super rolling bearing ( 970 ) is arranged on the central tower thanks to appropriate devices. Wind turbine according to one of claims 1 to 3, characterized in that the inner central rings ( 162 ) of the macro rings ( 12 . 16 . 116 ) by means of intermediate parts a cylinder ( 114 ), focusing on the supporting wheels or super wheels ( 169 ) or on the supporting super rolling bearing ( 960 ) and normally by a series of fixed vertical axis wheels or super wheels or a fixed super rolling bearing ( 970 ) and through the central tower ( 14 ) fixed. Wind turbine according to one of claims 1 to 4, characterized in that if the ring rotor only a single macro ring ( 16 ), the ring rotor on supporting wheels or super wheels or on a supporting super rolling bearing ( 960 ) through the inner central ring ( 162 ) or by an intermediate ring ( 236 ), which belongs to the macro ring and is located between the macro grid ( 11 ) and the inner central ring, or, if the macro grid has a corresponding cutout, through the main ring ( 161 ), which in any case goes through the equilibrium or direct wind power center of the macro grid. Wind turbine according to one of claims 1 to 5, characterized in that each main ring ( 36 . 161 ) of each macro ring ( 12 . 16 . 161 ) a pipe structure or a more complicated carcass structure, the 3 to. 9 sub-rings and beams between them has, and the beams are usually arranged at approximately 60 ° angle to each other and the beams and the sub-rings usually ever aerodynamically calculated shells or have a common aerodynamically calculated coat. Wind turbine according to one of claims 1 to 6, characterized in that the superrad ( 169 ) an inner cylinder 880 , an outer ring 660 and has two super-rolling bearings in between and each super-rolling bearing ( 697 ) two parallel rings ( 691 . 692 ) with / without intermediate connections, horizontal-axis smooth load wheels ( 197 ) or load balls or load rollers with the relatively small fixing rolling bearings ( 696 ) or magnetic holders ( 698 / 699 ), which are fastened between these rings, and relatively small fixing wheels ( 694 ) with relatively small rolling bearings located on the outer side of the inner ring ( 692 ) by holder ( 693 ) and between a neck ring ( 882 ) of the inner cylinder and a neck ring ( 661 ) of the outer ring, or fixing parallel magnetic rings ( 691 . 791 ) and fixing parallel magnetic rings ( 692 . 792 ), whose eponymous poles are arranged against each other and the magnetic ring ( 791 ) on the attachment ring ( 661 ) or integrated with it and the magnetic ring ( 792 ) on the attachment ring ( 882 ) or integrated with it. Wind turbine according to one of claims 1 to 7, characterized in that it is at each udstützenden wheel or Superad ( 169 ) Holder ( 688 ), which support this wheel or super wheel, and screw supports ( 168 ), usually by a ramp ( 680 ) and each screw post has a threaded portion ( 681 ), a four- or six-sided grip part ( 682 ) and a smooth round foot part ( 683 ) and the threaded part of each screw support corresponds to a threaded opening of the holder or the ramp, which there is a cylinder ( 687 ), and if the super wheels are used, the brackets support the inner cylinder ( 880 ) of the super wheel directly or by means of a central inner cylinder ( 888 ) of the super wheel without turning firmly support. Wind power plant according to one of claims 1 to 8, characterized in that the durability of the cells ( 57 ), the durability of the rotor blades ( 1 . 1K ) and the resilient resistance of the damper ( 500 ) within each macrogitter ( 11 ) increases from its outer edges to its attachment location, and if the cells, rotor blades, and damper dampers are relatively far from the attachment site of the macrogitter, they have lightweight materials and / or lightweight construction structure, allowing the use of the faint wind and partially allows the use of the fresh wind, and the rotor blades let through the strong and stormy wind thanks to the weak resilient resistance of the damper and if the cells, rotor blades and damper are not too far from the attachment point of the macrogitter, they middle materials and / or medium design structure, which includes the use of fresh wind and partial use of the weak wind, and thanks to the moderate resilience of the damper, the blades allow the wind to pass through and, if the cells, rotor blades and damper are relatively close to the macrograph's attachment, they have particularly durable materials and / or structurally durable construction; which allows the use of the strong and stormy wind and partly the use of fresh wind, and the rotor blades thanks to the strong resilient resistance of the damper only the strong wind gusts pass. Wind power plant according to one of claims 1 to 9, characterized in that each macro grid ( 11 ) has the shape of a rectangle to a circle, and if the macrogitter does not have a right circular shape, the height of the macrograph is preferably larger than its width. Wind power plant according to one of claims 1 to 10, characterized in that each macro grid ( 11 ) vertical ( 536 ) and usually horizontal ( 736 ) Has stiffening ribs that extend throughout its height or width, and the strength and / or thickness of these stiffening ribs normally increases from the outer edges of the macrostructure to its attachment location. Wind power plant according to one of claims 1 to 11, characterized in that each macro grid has a frame ( 33 ), which normally has 4 main parts, and this frame has the shape of a rectangle up to a ring corresponding to the shape of the macrogitter. Wind power plant according to one of claims 1 to 12, characterized in that each macro grid ( 11 ) horizontal bars ( 310 ), vertical bars ( 320 ) and cross pieces ( 300 ), which correspond to the sides and the corners of its cells, and the cross pieces each 2 parts ( 300L . 300R ) which are inserted in the adjacent beams. Wind power plant according to one of claims 1 to 13, characterized in that each macro grid ( 11 ) at the edges of its horizontal and vertical bars perforations, depressions, elevations or railways ( 789 ), which are necessary for an autonomous up / cross train. Wind power plant according to one of claims 1 to 14, characterized in that each macro grid has the circular shape and a ring frame ( 733 ) and the ring frame has a tube structure or a more complex carcass structure having 3 to 9 sub-rings and beams therebetween, and the beams are usually disposed at approximately 60 ° to each other and the sub-rings and the beams normally each have aerodynamically calculated mantles or a common aerodynamically calculated coat. Wind power plant according to one of claims 1 to 15, characterized in that each macro grid ( 11 ) a central base ( 761 ), which is at the same time a part of the main ring of the macrogitter, and this base has a simple cylinder structure or a more complex carcass structure having 3 to 9 tubes along the rotation direction and beams therebetween, and the beams mostly in ca 60 ° angles are arranged against each other and the tubes and the beams normally have aerodynamically calculated shells or a common aerodynamically calculated sheath and the width of the ring frame is greater than the width of a rotor blade and between the ring frame and the end faces of the central base spokes ( 763 ) are spanned. Wind turbine according to one of claims 1 to 16, characterized in that rods, cables or gang ( 920 ) in the 60 ° to 120 °, preferably 90 °, angle to each other, on the ring frame ( 733 ) and are attached to each other at the common intersections and these rods, ropes or ties put together the main structure of the macrogitter. Wind power plant according to claim 17, characterized in that the bars, ropes or bands ( 920 ) in the 30 ° to 60 °, preferably 45 °, angle to the vertical and arranged at the common intersections by the corresponding holder ( 600 ), each with at least one damper ( 500 ), or fastened together in some other way. Wind power plant according to one of claims 1 to 18, characterized in that it is normally mounted on the wind rotor carrier electric generators ( 89 ) provided by the transmission ( 80 ) with the ring rotor and / or by the below-mentioned intermediate gear ( 88 . 988 ) with the lower-mentioned valve air turbines ( 99 ) and if the transmissions ( 80 ) with a friction or tooth-ring strip or friction or tooth attachment ring ( 26 ) of the single or lower macro ring a roller contact or with the supporting wheels or super wheels Have turn or roll contact. Wind power plant according to one of claims 1 to 19, characterized in that at least one super-electric generator ( 890 ) is arranged around the center of the wind turbine and this super-electric generator a circle series of windings with the cores ( 891 ) on the wind rotor carrier and a circle series of magnets ( 892 ) on a magnet carrier ring ( 894 ), which is normally a lower attachment ring of the ring rotor. Wind power plant according to claim 20, characterized in that a super-transmission ( 893 ), which determines the distance between the circle series of the windings with the cores ( 891 ) and the circle series of magnets ( 892 ), with the super electric generator ( 890 ) and this super gear is connected to the cores at the windings and normally divided according to the number of these cores. Wind power plant according to one of claims 1 to 21, characterized in that it comprises compressed air reservoirs ( 100 ), Air pumps ( 79 ) with the gears ( 70 ), which are used for the storage of wind energy by the compression of the air, and the valve air turbines ( 99 ), which are used for the use of compressed air, and the air turbines with the electric generators ( 89 ) through the intermediate gear ( 988 ) are connected and the electric generators are not connected to the ring rotor. Wind power plant according to one of claims 1 to 21, characterized in that it comprises compressed air reservoirs ( 100 ), Air pumps ( 79 ) with the gears ( 70 ), which are used for the storage of wind energy by the compression of the air, and the valve air turbines ( 99 ), which are used for the use of compressed air, and the air turbines with the electric generators ( 89 ) through the intermediate gear ( 988 ) and the electric generators are also connected to the ring rotor through the gears ( 80 ) are connected. Wind power plant according to one of claims 1 to 21, characterized in that it comprises compressed air reservoirs ( 100 ), Valve air turbines ( 99 ) with the gears ( 98 ), which are used for the storage of wind energy by the compression of the air, and the valve air turbines ( 99 ), which are used for the use of compressed air, and the last air turbines with the electric generators ( 89 ) by intermediate gear ( 988 ) are connected and the electric generators are not connected to the ring rotor. Wind power plant according to one of claims 1 to 21, characterized in that the wind turbine compressed air reservoirs ( 100 ), Valve air turbines ( 99 ) with the gears ( 98 ), which are used for the storage of wind energy by the compression of the air, and the valve air turbines ( 99 ), which are used for the use of compressed air, and the last air turbines with the electric generators ( 89 ) by intermediate gear ( 988 ) and the electric generators are also connected to the ring rotor through the gears ( 80 ) are connected. Wind turbine according to one of claims 1 to 21, characterized in that it compressed air reservoirs ( 100 ) and valve air turbines ( 99 ) with the gears ( 98 ), which are used for the storage of wind energy by the compression of the air and also for the use of compressed air, and the air turbines with the electric generators ( 89 ) through the intermediate gear ( 988 ) are connected and the electric generators are not connected to the ring rotor. Wind power plant according to one of claims 1 to 21, characterized in that it comprises compressed air reservoirs ( 100 ) and valve air turbines ( 99 ) with the gears ( 98 ), which are used for the storage of wind energy by the compression of the air and also for the use of compressed air, and the air turbines with the electric generators ( 89 ) through the intermediate gear ( 88 ) connected between the gears ( 98 ) and gears ( 80 ) are arranged. Wind power plant according to one of claims 22 to 27, characterized in that the transmission ( 70 ) and gearboxes ( 98 ) with a friction or tooth-ring strip or friction or tooth attachment ring ( 26 ) of the single or lower macro ring are connected by a roller contact or to the supporting wheels or super wheels by a rotary or roller contact. Wind power plant according to one of claims 1 to 21, characterized in that it comprises compressed air reservoirs ( 100 ), Air pumps ( 79 ) with the gears ( 70 ) or valve air turbines ( 99 ) with the gears ( 98 ), which are responsible for the storage of wind energy by compressing the air be used, and the valve air turbines ( 99 ) with the gears ( 98 ), which are used for the use of compressed air, and the transmission ( 70 . 98 ) with a friction or tooth strip of the magnet carrier ring ( 894 ) of the super electric generator ( 890 ) are connected by a controllable roller contact and in this case the super-electric generator along its entire circle also a roller / coupling device ( 895 ), the magnet-carrier ring ( 894 ) with a neck ring ( 896 ) of the annular rotor controllably binds, and if the wind turbine has no air pumps, normally the same valve air turbines are used both for the compression of the air, as well as for the use of compressed air and the function change through the valves, gearboxes ( 98 ) and the roller / coupling device is controlled. Wind power plant according to one of claims 22 to 29, characterized in that each valve air turbine ( 99 ) actually an air turbine ( 991 ) and an air valve ( 992 ), by means of which the connection to a compressed air reservoir is controlled. Wind power plant according to one of claims 22 to 30, characterized in that each compressed air reservoir ( 100 ) has the shape of a hollow vertical cylinder with round end faces and normally with a room support ( 29 ) is integrated. Wind power plant according to one of claims 22 to 30, characterized in that all compressed air reservoirs are connected to each other and assemble a compressed air reservoir system, which is an external compressed air line ( 109 ), which goes to an external compressed air network. Wind power plant according to one of claims 1 to 32, characterized in that it has at least one space ( 1010 ) with the electrochemical plants for the production of hydrogen. Wind turbine according to claim 33, characterized in that it comprises at least one pressurized hydrogen reservoir ( 1100 ), which normally has the shape of a hollow vertical cylinder with round end faces. Wind power plant according to claim 33 or 34, characterized in that it comprises at least one reservoir ( 1000 ) with the liquid hydrogen. Wind power plant according to one of claims 3 to 35, characterized in that the central tower with a compressed air reservoir ( 100 ) or a pressurized hydrogen reservoir ( 1100 ) is integrated. Wind power plant according to one of claims 1 to 36, characterized in that it has at least one maintenance room ( 1011 ) having. Wind power plant according to one of claims 1 to 37, characterized in that it comprises at least one coupling vehicle ( 860 ), which has no motor and is mounted on an annular path of the wind rotor carrier or on an annular path of a ring ramp of the central tower, and the coupling vehicle has upper coupling wheels connected to the ring rotor by means of pneumatic drives and by a flexieblen roles -Bremse contact, and the coupling vehicle also has lower coupling wheels which can couple with the rings of the ring track by means of pneumatic drives and by a flexieblen roller-brake contact, and the coupling wheels have normally vertical axes of rotation. Wind power plant according to one of claims 1 to 38, characterized in that the central tower ( 14 ) an inner elevator tube or an inner elevator shaft with a lift ( 77 ), which moves through gears with a drive. Wind power plant according to one of claims 2 to 39, characterized in that on the central tower ( 14 ) an upper ramp ( 800 ) dedicated to the discharge of helicopters, is arranged directly or by a turn-coupling device and the turn-coupling device couples the ramp as needed to the central tower or to the ring rotor. Wind turbine according to one of claims 2 to 40, characterized in that each rotor blade ( 1 . 1K ) with two barrier dampers ( 500 ), which allow the rotor blade to rotate 90 ° about a local horizontal axis and are secured to the opposite faces of the rotor blade, usually in the cut-outs of the rotor blade, and the local horizontal axis of rotation separates the rotor blade into a small portion (Fig. 41 ) and a large part ( 42 ) and the difference between the area of the small part and the area of the large part is so substantial and the difference between the weight of the small part and the weight of the big part is so small that normally the wind winds the rotor blade about the local horizontal axis of rotation and the big part does not necessarily have to be the heaviest and every rotor blade ( 1 ) with the heaviest major part usually a complementary ro Torblatt ( 1K ) corresponds to the heaviest small part. Wind power plant according to claim 41, characterized in that the barrier damper ( 500 ) a mechanism ( 501 ) for the main functions and handle wings ( 503 ) for the attachment of the rotor blade ( 1 . 1K ) and with the macrogitter ( 11 ) or by a holder ( 502 . 600 ) is attached to it and with the holder has a roller bearing connection and the holders on the vertical bar ( 310 ), Rods, ropes ( 920 ) or bands of the macrogrid or at the intersections of the beams ( 310 ), Rods, ropes ( 920 ) or bands of the macrogrid, and if the ropes, bands or relatively thin rods are used, each holder has at least one groove or fold ( 651 . 652 ) for a rod, rope or band and, if not directly connected to a neighboring holder, 2 parts ( 601 . 602 ) having. Wind turbine according to claim 42, characterized in that the mechanism ( 501 ) a coat ( 551 ), which holds the handle ( 503 ) and with the holder ( 502 . 600 ) directly or indirectly has a roller bearing connection, an open base cylinder ( 552 ), which is attached to the holder and is located substantially inside the mechanism, a cylinder cover ( 553 ) and a strong winding spring ( 550 ), which is located in the base cylinder, and the winding spring is attached on the one hand to the bottom of the base cylinder or on the holder and on the other hand to the cylinder cover and the cylindrical portion of the cylinder cover within the approximately 90 ° -Winckels a section has and a Sperrwarze ( 555 ) of the jacket and usually a locking wart ( 554 ) of the base cylinder are within this cutout. Wind turbine according to claim 43, characterized in that Wälzläger ( 558 ) between the jacket ( 551 ) and the base cylinder ( 552 ) are arranged. Wind turbine according to claim 43, characterized in that an inner cylinder ( 556 ) in the inner space of the winding spring ( 550 ) coaxially arranged and on the one hand at the bottom of the base cylinder ( 552 ) or on the holder ( 502 . 600 ) and a second inner cylinder ( 559 ) coaxial with the first inner cylinder ( 556 ), on the one hand on the jacket ( 551 ) and by a circular window of the cylinder cover ( 553 ) and the first inner cylinder ( 556 ) normally the larger diameter than the second inner cylinder ( 559 ) and Wälzläger ( 558 ) between the two coaxial inner cylinders ( 556 . 559 ) are arranged. Wind power plant according to claim 42, characterized in that the mechanism ( 501 ) a coat ( 551 ), which holds the handle ( 503 ) and with the holder ( 502 . 600 ) directly or indirectly has a roller bearing connection, an open base cylinder ( 552 ), which is fixed to the holder and is located substantially within the mechanism, and has at least one sub-damper, and the sub-damper has a strong arc wave spring or bow coil spring ( 550 ), a one-sided open bow steering cylinder ( 557 ) and a one-sided open bow push cylinder ( 553 ) and the bow steering cylinder, on the base cylinder or on a neck ring ( 579 ) of the base cylinder is concentrically arranged and fixed, and the neck ring of the base cylinder has an everted extension of the base cylinder or a ring with / without spokes ( 5792 ) and said spring, the bow-push cylinder and the bow-steering cylinder of the sub-damper are coaxially arranged around each other and the bow-stroke cylinder is partially in the bow steering cylinder and the said spring entirely within these arc cylinder ( 553 . 557 ) is located. Wind power plant according to claim 46, characterized in that the arc wave spring or bow coil spring ( 550 ) on the one hand at the bottom of the sheet steering cylinder ( 557 ) and on the other hand at the bottom of the bow-thrust cylinder ( 553 ) and the waves or windings of said spring along a geometric approximately 270 ° circular arc are arranged and the bow steering cylinder ( 557 ) is about 180 ° and the bow push cylinder ( 553 ) more than 180 °, preferably about 270 °, and the bow-push cylinder at its bottom a Sperrwarze ( 561 ) and the jacket ( 551 ) outside his free space ( 560 ) between the locking wart ( 561 ) of the sheet-impact cylinder and the open end face of the sheet-impact cylinder, a locking cam ( 555 ) and the bow-push cylinder normally at its bottom nor a locking wart ( 562 ), which lies just below its first bump ( 561 ), and the base cylinder ( 552 ) or its approach ring ( 579 ) usually a locking wart ( 554 ), which opposite to the sperm wart ( 562 ) is located. Wind turbine according to claim 46, characterized in that the waves or windings of the bow wave spring or bow coil spring ( 550 ) along a ge 270 ° circular arc are arranged and the bow steering cylinder ( 557 ) is about 180 ° and the bow push cylinder ( 553 ) is more than 90 °, preferably about 180 °, and the jacket ( 551 ) in his free space ( 560 ) between the bottom of the sheet steering cylinder and the bottom of the sheet-impact cylinder, a locking wart ( 555 ) and the base cylinder ( 552 ) is normally in the free space of the shell opposite the bottom of the bow-thrust cylinder a locking wart ( 554 ) having. Wind turbine according to claim 46, characterized in that the waves or windings of this spring of the bow wave spring or bow coil spring ( 550 ) are arranged along a geometric approximately 360 ° circular arc and the bow steering cylinder ( 557 ) is about 180 ° and the bow push cylinder ( 553 ) is more than 180 °, preferably about 270 °, and the bow-push cylinder is a locking teat ( 565 ), which is 90 ° in front of its bottom, and the jacket ( 551 ) between the locking wart ( 565 ) and the bottom of the bow steering cylinder ( 557 ) a locking wart ( 555 ) and the bow-thrust cylinder normally still a Sperrwarze ( 564 ), which is just below its first bump, and the base cylinder ( 552 ) or its approach ring ( 579 ) normally opposite the locking wart ( 564 ) a locking wart ( 554 ) having. Wind turbine according to claim 42, characterized in that the mechanism ( 501 ) a coat ( 551 ), which holds the handle ( 503 ) and with the holder ( 502 . 600 ) directly or indirectly has a roller bearing connection, a base cylinder open on one side ( 552 ), which is attached to the holder and is located substantially inside the mechanism, and has at least one sub-damper and the sub-damper a compressed gas space ( 400 ), a one-sided open bow steering cylinder ( 557 ) or compressed gas cylinder and a preferably on one side open bow-push cylinder ( 553 ) or a piston and the bow steering cylinder on the base cylinder or on a neck ring ( 579 ) of the base cylinder is concentrically arranged and fixed, and the neck ring of the base cylinder has an everted extension of the base cylinder or a ring with / without spokes ( 5792 ) and the sheet collision cylinder and the sheet steering cylinder of the sub-damper are coaxially arranged around each other and the sheet collision cylinder is partially in the sheet steering cylinder and the compressed gas space is limited by the sheet steering cylinder and the arc collision cylinder. Wind power plant according to claim 50, characterized in that the compressed gas devices are arranged along a geometric approximately 270 ° circular arc and the bow steering cylinder ( 557 ) is about 180 ° and the bow push cylinder ( 553 ) or piston more than 90 °, preferably 130 ° to 170 °, and the shell ( 551 ) in his free space ( 560 ) between the bottom of the sheet steering cylinder and the bottom of the sheet-impact cylinder, a locking wart ( 555 ) and the base cylinder ( 552 ) or its approach ring ( 579 ) normally in free space ( 560 ) of the jacket relative to the bottom of the bow-thrust cylinder a Sperrwarze ( 554 ) having. Wind power plant according to claim 50, characterized in that the compressed gas devices are arranged along a geometric approximately 360 ° circular arc and the bow steering cylinder ( 557 ) is about 180 ° and the bow push cylinder ( 553 ) or piston is preferably more than 180 °, preferably 220 ° to 260 °, and the bow-thrust cylinder is a locking wart ( 565 ), which is 90 ° in front of its bottom, and the jacket ( 551 ) between the locking wart ( 565 ) and the bottom of the floor steering cylinder a locking wart ( 555 ) and the bow-thrust cylinder normally still a Sperrwarze ( 564 ), which lies just below its first bump ( 565 ), and the base cylinder ( 552 ) or its approach ring ( 579 ) normally opposite the locking wart ( 564 ) a locking wart ( 554 ) having. Wind power plant according to one of claims 50 to 52, characterized in that the compressed gas space ( 400 ) with an input ( 454 ) of a compressed gas system of the macrogitter ( 11 ) on the vertical bar ( 320 ) by compressed gas lines ( 450 ) of the barrier damper ( 500 ), a compressed gas coupling device ( 451 ) on the holder ( 502 ) and a complementary compressed gas coupling device ( 452 ) is connected to the vertical bar. Wind power plant according to one of claims 50 to 52, characterized in that the compressed gas space ( 400 ) with a valve or nipple ( 452 ) on the base cylinder ( 452 ) or on the holder ( 502 . 600 ) by compressed gas lines ( 450 ) of the barrier damper ( 500 ) connected is. Wind power plant according to one of claims 50 to 52, characterized in that the compressed gas space ( 400 ) not directly with the compressed gas, but with the resilient balls in the interior ren have the compressed gas, is filled and the diameter of such a sphere is preferably almost as large as the inner. Diameter of the arc push cylinder is. Wind turbine according to claim 42, characterized in that the mechanism ( 501 ) a coat ( 551 ), which holds the handle ( 503 ) and with the holder ( 502 . 600 ) directly or indirectly has a roller bearing connection, an open base cylinder ( 552 ), which is fixed to the holder and is located substantially within the mechanism, and has at least one sub-damper, and the sub-damper has a strong arc wave spring or bow coil spring ( 550 ) along a 360 ° circular arc and said spring on the base cylinder or on a neck ring ( 579 ) of the base cylinder concentrically arranged and at a fixing point ( 571 ) is attached by the two ends thereof and usually an intermediate part and the approach ring of the base cylinder has an everted extension of the base cylinder or a ring with / without spokes ( 5792 ) and the said spring or, if split, one of its intermediate parts is a backbone ( 575 ), which is about 180 ° after the attachment point ( 571 ), and the mentioned spring or, when split, one of its intermediate parts, the second locking lug ( 573 ), which is located about 90 ° after the first, and the jacket ( 551 ) a locking wart ( 555 ), which is located between the above-mentioned locking warts ( 573 . 575 ), and the mentioned spring or, if split, one of its intermediate parts normally the third locking cam ( 574 ), which are among the first ( 575 ) and the base cylinder ( 552 ) or its approach ring ( 579 ) usually also a Sperrwarze ( 554 ), which opposite to the locking wart ( 574 ) is located. Wind turbine according to claim 56, characterized in that the mechanism ( 501 ) a coat ( 551 ), which holds the handle ( 503 ) and with the holder ( 502 . 600 ) directly or indirectly has a roller bearing connection, an open base cylinder ( 552 ), which is fixed to the holder and is located substantially within the mechanism, and has at least one sub-damper, and the sub-damper has a strong arc wave spring or bow coil spring ( 550 ) along a 360 ° circular arc within a concentrically divided hollow steering ring ( 566 . 567 ) with an inner part ( 566 ) and an external part ( 567 ) and the inner part ( 566 ) of the hollow steering ring on the base cylinder or on a neck ring ( 579 ) of the base cylinder is concentrically arranged and fixed, and the neck ring of the base cylinder has an everted extension of the base cylinder or a ring with / without spokes ( 5792 ) and the said spring at a fixing point ( 571 ) of the inner part ( 566 ) of the hollow steering ring is secured by the two ends thereof and normally an intermediate part and the outer part ( 567 ) of the hollow steering ring a fixed connection ( 572 ) with the changed spring or, if split, with one of its intermediate parts, and no firm connection with the inner part ( 566 ) of the hollow steering ring and the second fixed connection ( 572 ) about 180 ° after the fixing point ( 571 ) and The outer part ( 567 ) of the hollow steering ring has two locking lugs ( 565 . 563 ), which are located about 90 ° behind each other, and the jacket ( 551 ) a locking wart ( 555 ), which is located between the above-mentioned locking warts ( 563 . 565 ), and the outer part ( 567 ) of the hollow steering ring normally the third locking lug ( 564 ), which extends below the first block ( 565 ), and the base cylinder ( 552 ) or its approach ring ( 579 ) usually also a Sperrwarze ( 554 ), which opposite to the locking wart ( 564 ) is located. Wind turbine according to claim 57, characterized in that the jacket ( 551 ) inside guide rails ( 568 ), which from the outside the movement of the outer part ( 567 ) of the hollow steering ring and steer. Wind turbine according to claim 57, characterized in that the inner part ( 566 ) of the hollow steering ring and the outer part ( 567 ) of the hollow steering ring against each other komlementäre guide rails ( 569 ), which couple the two parts together and allow only the rotation against each other. Wind turbine according to one of claims 46 to 59, characterized in that the rolling bearings ( 558 ) between the base cylinder ( 552 ) and the coat ( 551 ) or between the base cylinder and an inner central cylinder ( 559 ) attached to the mantle or to the handle wing ( 503 ), or between an inner everted extension or an attachment ring ( 549 ) of the base cylinder and the inner central cylinder are arranged. Wind turbine according to one of claims 2 to 40, characterized in that each rotor blade ( 1 ) with two barrier dampers ( 500 ), which allow the rotation of the rotor blade about a local vertical or oblique axis by 90 ° to 180 °, preferably about 135 ° for the vertical and preferably about 110 ° for the oblique, and to the has opposite end faces of the rotor blade, normally in the cutouts of the rotor blade, attached, and the local vertical axis of rotation, the rotor blade in a small part ( 41 ) and a large part ( 42 ) and the difference between the area of the small part and the area of the large part is so substantial that the wind can turn the rotor blade about the local vertical or oblique axis of rotation. Wind power plant according to claim 61, the damper ( 500 ) a mechanism ( 501 ) for the main functions and handle wings ( 503 ) for the attachment of the rotor blade ( 1 . 1K ) and with the macrogitter ( 11 ) or by a holder ( 502 . 600 ) is attached to it and with the holder has a rolling bearing connection and the holders on the horizontal or oblique beams ( 310 ), Rods, ropes ( 920 ) or bands of the macrogitter or at their intersections and if the ropes, bands or relatively thin rods are used, each holder has at least one groove or fold ( 651 . 652 ) for a rod, a rope or a band and, if it is not directly connected to an adjacent holder, two parts ( 601 . 602 ) having. Wind turbine according to claim 62, characterized in that the mechanism ( 501 ) a coat ( 551 ), which holds the handle ( 503 ) and with the holder ( 502 . 600 ) directly or indirectly has a roller bearing connection, an open base cylinder ( 552 ), which is attached to the holder and is located substantially inside the mechanism, a cylinder cover ( 553 ), itself a unilaterally opened cylinder with a larger diameter, and a strong winding spring ( 550 ), which is located in the base cylinder, and the winding spring is attached on the one hand to the bottom of the central cylinder and on the other hand to the cylinder cover and the cylindrical portion of the cylinder cover within 90 ° to 180 °, preferably about 135 ° for the vertical axis rotor blades, and preferably 110 ° for the oblique axis rotor blades, has a cutout and an inner locking wart ( 555 ) is located within this section of the jacket. Wind turbine according to claim 63, characterized in that Wälzläger ( 558 ) between the jacket ( 551 ) and the base cylinder ( 553 ) are arranged and if the damper ( 500 ) for the lower position in the vertical axis rotor blade or for the two positions in the oblique axis rotor blade, it is predetermined between the jacket and the holder ( 502 . 600 ) a supporting or blocking rolling bearing ( 578 ) having. Wind turbine according to claim 63, characterized in that an inner cylinder ( 556 ) in the inner space of the winding spring ( 550 ) coaxially arranged and on the one hand at the bottom of the base cylinder ( 552 ) or on the holder ( 502 . 600 ) and a second inner cylinder ( 559 ) coaxial with the first inner cylinder ( 556 ), on the one hand on the jacket ( 551 ) and by a circular window of the cylinder cover ( 553 ) and the first inner cylinder ( 556 ) normally the larger diameter than the second inner cylinder ( 559 ) and Wälzläger ( 558 ) between the two coaxial inner cylinders ( 556 . 559 ) are arranged and if the damper ( 500 ) for the lower position in the vertical axis rotor blade or for the two positions in the oblique axis rotor blade is predetermined, he between the second inner cylinder ( 559 ) and the holder a supporting or blocking rolling bearing ( 578 ) having. Wind turbine according to claim 42 or 62, characterized in that the mechanism ( 501 ) a coat ( 551 ), which holds the handle ( 503 ) and with the holder ( 502 . 600 ) directly or indirectly has a roller bearing connection, an open base cylinder ( 552 ), which is fixed to the holder and is located substantially within the mechanism, and has at least one sub-damper, and the sub-damper has a strong arc wave spring or bow coil spring ( 550 ), a one-sided open bow steering cylinder ( 557 ), a one-sided open bow push cylinder ( 553 ) and a bow-locking device ( 586 ) and the sheet-locking device between the shell and the bow-steering cylinder over a 90 ° to 180 °, preferably 90 ° for the horizontal axis rotor blades and preferably 135 ° for the vertical axis rotor blades, arc extends and the bow-locking device at their ends, warts ( 585 . 583 ) and with the bottom of the arc-impact cylinder a firm connection ( 581 ) and the bow steering cylinder on the base cylinder or on a neck ring ( 579 ) of the base cylinder is concentrically arranged and fixed, and the neck ring of the base cylinder has an everted extension of the base cylinder or a ring with / without spokes ( 5792 ) and the mentioned spring, the bow-push cylinder and the bow-steering cylinder of the sub-damper are coaxially arranged around each other and the bow-push cylinder is partially in the bow steering cylinder and said spring on the one hand to the bottom of the bow steering cylinder and on the other hand is attached to the bottom of the bow-push cylinder and is located entirely within this arc cylinder and the bow steering cylinder ( 557 ) 210 ° to 260 °, preferably about 250 ° for the horizontal axis rotor blades and preferably about 225 ° for the vertical axis rotor blades, is and the bow-thrust cylinder ( 553 ) 135 ° to 225 °, preferably about 180 ° for the horizontal axis rotor blades and preferably about 210 ° for the vertical axis rotor blades, is and the sheath ( 551 ) between the locking warts ( 583 . 585 ) of the bow-locking device a locking wart ( 555 ) having. Wind turbine according to claim 42 or 62, characterized in that the mechanism ( 501 ) a coat ( 551 ), which holds the handle ( 503 ) and with the holder ( 502 . 600 ) directly or indirectly has a roller bearing connection, an open base cylinder ( 552 ), which is fixed to the holder and is located substantially within the mechanism, and has at least one sub-damper, and the sub-damper has a strong arc wave spring or bow coil spring ( 550 ), a two-sided open bow steering cylinder ( 557 ), two arched push cylinders ( 553 . 588 ) and two bow-locking devices ( 586 . 589 ) and the bow-locking devices between the shell and the bow-steering cylinder over a 90 ° to 180 °, preferably 90 ° for the horizontal axis rotor blades and preferably 135 ° for the vertical axis rotor blades, -Kreisbogen extend together and the bow Steering cylinder on the base cylinder or on a shoulder ring ( 579 ) of the base cylinder is concentrically arranged and fixed, and the neck ring of the base cylinder has an everted extension of the base cylinder or a ring with / without spokes ( 5792 ) And the mentioned spring, the bow-push cylinder and the bow-steering cylinder of the sub-damper are arranged coaxially around each other and the bow-stroke cylinder are partially in the bow steering cylinder and said spring is located entirely within these arc cylinder and the first Bow-locking device with the bottom of the first bow-thrust cylinder ( 553 ) has a fixed connection and at its end a Sperrwarze ( 585 ) and the second sheet-locking device with the bottom of the second sheet-thrust cylinder ( 588 ) has a fixed connection and at its end a locking wart ( 583 ) and the base cylinder or its neck ring between the bottom of the first sheet-piercing cylinder and the bottom of the second sheet-piercing cylinder, a locking projection ( 587 ) and this Sperrwarze ( 587 ) About 90 ° after the first open end of the sheet steering cylinder and 10 ° to 60 °, preferably 20 ° for the horizontal axis rotor blades and preferably 45 ° for the vertical axis rotor blades, located in front of the second open end face of the sheet steering cylinder and the bow steering cylinder ( 557 ) 210 ° to 260 °, preferably about 250 ° for the horizontal axis rotor blades and preferably about 225 ° for the vertical axis rotor blades, is and the first arc collision cylinder ( 553 ) is more than 90 °, preferably about 180 °, and the second arc collision cylinder ( 588 ) is more than 20 °, preferably about 45 °, for the horizontal axis rotor blades and more than 45 °, preferably about 90 °, for the vertical axis rotor blades and the shell ( 551 ) between the locking warts ( 583 . 585 ) the bow-locking devices a locking wart ( 555 ) having. Wind turbine according to claim 42 or 62, characterized in that the mechanism ( 501 ) a coat ( 551 ), which holds the handle ( 503 ) and with the holder ( 502 . 600 ) directly or indirectly has a roller bearing connection, an open base cylinder ( 552 ), which is attached to the holder and is located substantially inside the mechanism, and has at least one sub-damper and the sub-damper a compressed gas space ( 400 ), a two-sided open bow steering cylinder ( 557 ), two arched push cylinders ( 553 . 588 ) and two bow-locking devices ( 586 . 589 ) and the bow-locking devices extend between the shell and the bow-steering cylinder over a 90 ° to 180 °, preferably 90 ° for the horizontal axis rotor blades and preferably 135 ° for the vertical axis rotor blades, -Kreisbogen together and the bow Steering cylinder on the base cylinder or on a shoulder ring ( 579 ) of the base cylinder is concentrically arranged and fixed, and the neck ring of the base cylinder has an everted extension of the base cylinder or a ring with / without spokes ( 5792 ) and the sheet push cylinders are partially in the sheet steering cylinder and each sheet collision cylinder is arranged coaxially relative to the sheet steering cylinder and the compressed gas space is located substantially within these arc cylinder and the first arc-locking device to the bottom of the first bow impact cylinder ( 553 ) has a fixed connection and at its end a Sperrwarze ( 585 ) and the second sheet-locking device with the bottom of the second sheet-thrust cylinder ( 588 ) has a fixed connection and at its end a locking wart ( 583 ) and the base cylinder or its approach ring between the bottom of the first sheet-piercing cylinder and the bottom of the second sheet-piercing cylinder a Sperrwarze ( 587 ) and this Sperrwarze ( 587 ) About 90 ° after the first open end of the sheet steering cylinder and 10 ° to 60 °, preferably 20 ° for the horizontal axis rotor blades and preferably 45 ° for the vertical axis rotor blades, located in front of the second open end face of the sheet steering cylinder and the bow steering cylinder ( 557 ) Is preferably 210 ° to 260 °, preferably about 250 ° for the horizontal axis rotor blades and preferably about 225 ° for the vertical axis rotor blades and the first arc collision cylinder ( 553 ) is more than 90 °, preferably about 180 °, and the second arc collision cylinder ( 588 ) is more than 20 °, preferably about 45 °, for the horizontal axis rotor blades and more than 45 °, preferably about 90 °, for the vertical axis rotor blades and the shell ( 551 ) between the locking warts ( 583 . 585 ) the bow-locking devices a locking wart ( 555 ) having. Wind power plant according to claim 68, characterized in that the compressed gas space ( 400 ) with an input ( 454 ) of a compressed gas system of the macrogitter ( 11 ) on the vertical bar ( 320 ) by compressed gas lines ( 450 ) of the barrier damper ( 500 ), a compressed gas coupling device ( 451 ) on the holder ( 502 ) and a complementary compressed gas coupling device ( 453 ) is connected to the vertical bar. Wind power plant according to claim 68, characterized in that the compressed gas space ( 400 ) with a valve or nipple ( 452 ) on the base cylinder ( 452 ) or on the holder ( 502 . 600 ) by compressed gas lines ( 450 ) of the barrier damper ( 500 ) connected is. Wind power plant according to claim 68, characterized in that the compressed gas space ( 400 ) is not directly filled with the pressurized gas, but with the resilient balls, which have the compressed gas inside, and the diameter of such a ball is preferably almost as large as the inner diameter of the arc-impact cylinder. Wind turbine according to claim 62, characterized in that the mechanism ( 501 ) a coat ( 551 ), which holds the handle ( 503 ) and with the holder ( 502 . 600 ) directly or indirectly has a roller bearing connection, an open base cylinder ( 552 ), which is attached to the holder and is located substantially within the mechanism, and has at least one sub-damper and the sub-damper along a 360 ° circular arc a strong arc wave spring or bow coil spring ( 550 ) and the mentioned spring on the base cylinder or on a neck ring ( 579 ) of the base cylinder concentrically arranged and at a fixing point ( 571 ) is attached by its two ends and normally an intermediate part and the approach ring of the base cylinder has an everted extension of the base cylinder or a ring with / without spokes ( 5792 ) and the said spring or, if split, one of its intermediate parts is a backbone ( 575 ), which is 90 ° to 180 °, preferably 150 °, after the attachment point ( 571 ) and the mentioned spring or, if it is split, one of its intermediate parts still a Sperrwarze ( 573 ), which is 90 ° to 180 °, preferably 135 °, after the first first bump ( 575 ) and the jacket ( 551 ) a locking wart ( 555 ), which is located between the above-mentioned locking warts ( 573 . 575 ) and the mentioned spring or, if split, one of its intermediate parts normally still a (second) locking wart ( 574 ), which extends below its first block ( 575 ), and the base cylinder ( 552 ) or its approach ring ( 579 ) usually also a Sperrwarze ( 554 ), which opposite to the locking wart ( 574 ) is located. Wind turbine according to claim 62, characterized in that the mechanism ( 501 ) a coat ( 551 ), which holds the handle ( 503 ) and with the holder ( 502 . 600 ) directly or indirectly has a roller bearing connection, an open base cylinder ( 552 ), which is fixed to the holder and is located substantially within the mechanism, and having at least one sub-damper, and the sub-damper along a 360 ° arc within a concentrically divided hollow steering ring ( 566 . 567 ) a strong arc wave spring or bow coil spring ( 550 ) and the concentrically divided hollow steering ring has an inner part ( 566 ) and an external part ( 567 ), which have a freedom of rotation against each other, and the inner part ( 566 ) of the hollow steering ring on the base cylinder or on a neck ring ( 579 ) of the base cylinder is concentrically arranged and fixed, and the neck ring of the base cylinder has an everted extension of the base cylinder or a ring with / without spokes ( 5792 ) and the said spring at a fixing point ( 571 ) of the inner part ( 566 ) of the hollow steering ring is fixed by its two ends and normally an intermediate part and the outer part ( 567 ) of the hollow steering ring a fixed connection ( 572 ) with the changed spring or, if split, with one of its intermediate parts, and no firm connection with the inner part ( 566 ) of the hollow steering ring and the fixed connection ( 572 ) about 180 ° after the fixing point ( 571 ) and the outer part ( 567 ) of the hollow steering ring two locking wart ( 565 . 563 ), which are 90 ° to 180 °, preferably 135 °, nacheiander, and the jacket ( 551 ) a locking wart ( 555 ), which is located between the above-mentioned locking warts ( 563 . 565 ), and the outer part ( 567 ) of the hollow steering ring normally still a (third) locking wart ( 564 ), which extends below its first block ( 565 ), and the base cylinder ( 552 ) or its approach ring ( 579 ) usually also a Sperrwarze ( 554 ), which opposite to the locking wart ( 564 ) is located. Wind turbine according to claim 73, characterized in that the jacket ( 551 ) inside guide rails ( 568 ), which from the outside the movement of the outer part ( 567 ) of the hollow steering ring and steer. Wind turbine according to claim 73, characterized in that the inner part ( 566 ) of the hollow steering ring and the outer part ( 567 ) of the hollow steering ring the against each other komlementären guide rails ( 569 ), which couple the two parts together and allow only the rotation against each other. Wind turbine according to one of claims 66 to 75, characterized in that Wälzläger ( 558 ) between the base cylinder ( 552 ) and the coat ( 551 ) or between the base cylinder ( 552 ) or its inner approach ring ( 549 ) and an inner central cylinder ( 559 ) attached to the mantle or to the handle wing ( 503 ), are arranged, and if the damper ( 500 ) for the lower position in the vertical axis rotor blade or for the two positions in the oblique axis rotor blade is predetermined, he between the holder ( 502 . 600 ) and the jacket or between the holder and the inner central cylinder and a supporting or blocking rolling bearing ( 578 ) having. Wind power plant according to one of claims 41 to 76, characterized in that the complementary rotor blade ( 1K ) the same construction as the rotor blade ( 1 ), but in its small part ( 41 ) a burden ( 911 ) having. Wind turbine according to one of claims 41 to 77, characterized in that each rotor blade ( 1 . 1K ) has inside a carcass structure and this carcass structure between the barrier dampers ( 500 ) is particularly dense and / or solid and the further from the axis of rotation are their elements, the thinner and / or thinner they are. Wind turbine according to one of claims 42 to 78, characterized in that each rotor blade ( 1 . 1K ) Coupling devices ( 902 ) having inside a carcass structure and the handle wings ( 503 ) correspond. Wind turbine according to one of claims 41 to 79, characterized in that each rotor blade ( 1 . 1K ) inside the axis of rotation a base part ( 901 ) extending from one damper to the other damper and having an inner carcass structure.