JP4658768B2 - Rotor blade and power generator using the rotor blade - Google Patents

Description

  The present invention relates to a rotor blade that can be used as a power source in wind power generation, for example, and further relates to a power generator using the rotor blade.

  As a rotor blade that can be used as a power source in wind power generation, for example, there is one described in Patent Document 1 below. Such a rotor blade can rotate by receiving wind force. This rotational force can be used as a power source such as wind power generation.

By the way, when using a rotor blade as a power source for wind power generation or the like, it is necessary to efficiently convert wind power into power. In this regard, there is room for further improvement in the conventional rotor blade.
JP-A-11-141453

  The present invention has been made in view of such circumstances, and intends to provide a rotor blade that can be used as an efficient power source.

The rotary blade according to claim 1 of the present invention includes a first rotary shaft, a first link, a plate-like blade member, a second rotary shaft, and a second link. The first link extends outward from the first rotation shaft and is connected to one side of the plate-like wing member, and the plate-like wing member rotates with respect to the first link. The second rotating shaft is eccentric from the first rotating shaft, and the second link is extended from the first rotating shaft in the outer direction so that the second rotating shaft is attached to the second rotating shaft. The rotary shaft is connected to the other side of the plate-like wing member, and the separation distance between the second rotary shaft and the wing member is kept constant. The adjustment mechanism further includes an adjustment mechanism, and the adjustment mechanism adjusts the position of the first rotation shaft to a predetermined position according to the flow of the fluid . Without this adjustment mechanism, even if it initially rotates, it will be necessary to stop the rotation. Furthermore, the rotational direction of the first rotating shaft is reversed by reversing the positional relationship between the first rotating shaft and the second rotating shaft in the fluid flow direction.

According to a second aspect of the present invention, the rotating blade is configured so that the second rotating shaft is moved relative to the first rotating shaft in the fluid flow direction by the adjustment mechanism and the configuration in which the rotating direction of the first rotating shaft is reversed . It is characterized by being arranged at a position where the highest rotational speed is obtained approximately near the downstream side or near the flow side.

According to a third aspect of the present invention, the rotary blade includes a single rotary shaft, a first link, a plate-like blade member, a second link, and an eccentric bearing mechanism. The first link is extended outward from the rotating shaft and connected to one side of the wing member, and the plate-like wing member is attached to be rotatable with respect to the first link. The second link is extended outward from the eccentric bearing mechanism portion and connected to the eccentric bearing mechanism portion attached to the rotary shaft and the other side of the plate-like wing member , and the rotation The distance between the eccentric bearing mechanism attached to the shaft and the wing member is kept constant, and the eccentric bearing mechanism is located at a position eccentric from the center of the rotating shaft. The second link is attached with an eccentric rotation mechanism that eccentrically rotates the outer periphery of the rotation shaft. And the adjusting mechanism which controls the direction of the said eccentric bearing mechanism part according to the flow of the said fluid is provided. Without this adjustment mechanism, even if it initially rotates, it will be necessary to stop the rotation. Furthermore, the rotational direction of the rotating shaft is reversed by reversing the positional relationship between the rotating shaft and the eccentric bearing mechanism portion in the fluid flow direction.

According to a fourth aspect of the present invention, the rotation center of the eccentric bearing mechanism is substantially downstream with respect to the rotation shaft in the fluid flow direction by the configuration in which the adjustment mechanism and the rotation direction of the rotation shaft are reversed. It is preferable to arrange at the position where the highest rotational speed is obtained in the vicinity or near the upstream.

The power generator according to claim 5 is configured to generate power by the rotational force of the rotor blade according to any one of claims 1 to 4 .

  According to the rotor blade of the present invention, it is possible to efficiently extract the rotational force from the fluid flow.

  Hereinafter, a rotor blade according to an embodiment of the present invention will be described with reference to the accompanying drawings.

(Configuration of the first embodiment)
The rotary blade includes a first rotary shaft 1, a first link 2, a blade member 3, a second rotary shaft 4, a second link 5, a base 6, an adjustment mechanism 7, a connector 8, As a main element (see FIG. 1).

  The lower end of the first rotating shaft 1 is attached to a bearing 61 of the base 6 so as to be rotatable with respect to the base 6. The first rotating shaft 1 includes two attachments 11 for attaching the first link 2.

  A connecting tool 8 is rotatably attached to the upper end of the first rotating shaft 1 via a bearing 81.

  The number of the first links 2 is eight in the example shown in FIG. These first links 2 are substantially rigid, although some deformation is allowed.

  The four first links 2 are attached to the lower fixture 11. The remaining four first links 2 are attached to the upper fixture 11. These first links 2 are extended from the first rotating shaft 1 in the outward direction. More specifically, each first link 2 is arranged in a direction extending radially from the first rotation shaft 1. Furthermore, the first links 2 are of equal length. The first links 2 in the same plane are equally spaced. The first link 2 is attached by a fixture 11 so as to rotate as the first rotating shaft 1 rotates.

  In this embodiment, the wing member 3 has a simple rectangular plate shape. The wing member 3 is attached to the tip of each first link 2. Here, the wing member 3 is attached to each first link 2 so as to be rotatable (in this specification, it can be rotated in the forward and reverse directions at least within a certain angular range). Yes. The wing member 3 may be an airplane wing shape or a propeller shape. The cross-sectional shape of the wing member 3 is not limited to a rectangle, and an appropriate shape such as an ellipse or a circle can be selected.

  The lower end of the second rotating shaft 4 is attached so as not to rotate in the hole 82 of the connector 8 attached to the upper end of the first rotating shaft 1. Thereby, the second rotating shaft 4 is arranged at a position eccentric from the first rotating shaft 1. The second rotating shaft 4 is arranged so as to be at a position where the highest rotational speed is obtained, for example, on the downstream side or the upstream side of the first rotating shaft 1 in the fluid flow direction for applying a rotational force to the rotary blades. Is done.

  In this example, there are four second links 5. The second link 5 connects the second rotating shaft 4 and the wing member 3. Specifically, each second link 5 has the same length and extends radially from the second rotation center 4. In this example, a substantially rigid body is used as the second link 5. The second link 5 does not substantially extend, and thus the second link 5 can maintain a constant separation distance between the second rotating shaft 4 and the blade member 3. ing. One end of each second link 5 is attached to a bearing 41 of the second rotating shaft 4. Thereby, the second link 5 is rotatable with respect to the second rotation shaft 4. With this configuration, the second link 5 is configured to change the angle of attack of the wing member 3 that rotates about the first rotation shaft 1. The other end of the second link 5 is attached to the wing member 3 so as to be rotatable.

  The connector 8 includes a plurality of holes 82 so that the eccentric distance and the positional relationship between the first rotating shaft 1 and the second rotating shaft 2 can be adjusted.

  The adjustment mechanism 7 includes a rod-like base 71, a blade part 72 attached near the rear end of the base 71, and a balancer 73 attached to the tip of the base 71. An intermediate portion of the base portion 71 is attached to the upper end of the second rotation shaft 4 so as not to rotate. The blade | wing part 72 is formed in plate shape, and is arrange | positioned so that the surface may become substantially parallel to the 1st or 2nd rotating shaft.

(Operation of the embodiment)
Next, the operation of the rotor blade according to the present embodiment configured as described above will be described. First, wind is sent from a certain direction to the rotor blades. Of course, this wind may be generated by natural force. In the present embodiment, the direction of the wind relative to the rotor blade is not particularly limited in the initial state. If the wind has a velocity component that intersects the first and second rotation axes of the rotor blades, it is possible to obtain the rotational force by the rotor blades of the present embodiment by the operation described later. However, when using natural wind, the wind often blows in a direction parallel to the ground surface, so the first and second rotating shafts of the rotor blades are generally in a direction substantially perpendicular to the ground surface. Preferably they are arranged.

  When the rotor blades receive wind, the blade portion 72 of the adjustment mechanism 7 moves to the leeward side by wind power. Thereby, a rotational force is applied to the second rotating shaft 4. Then, the 2nd rotating shaft 4 rotates centering on the 1st rotating shaft 1, and is arrange | positioned in the leeward side (downstream side) rather than the 1st rotating shaft 1 (refer FIG.1, FIG.2 and FIG.4). In FIG. 2, it is assumed that the wind is blowing from the left to the right in the figure.

  On the other hand, a rotational force is generated in the wing member 3 by the wind force, and the rotational force is rotated about the first rotation shaft 1. Then, the second link 5 rotates about the second rotation shaft 4 via the wing member 3. Here, the wing member 3 is held at a constant distance from the second rotating shaft 4 by the second link 5 and is rotatable with respect to the first link 2. For this reason, the angle of attack of the wing member 3 with respect to the air flow changes according to the rotation angle of the first link 2. FIG. 5 shows a change in the angle of attack of the wing member 3 according to the rotation angle. Furthermore, the locus | trajectory of the front-end | tip of a 1st and 2nd link is shown with the dashed-dotted line in FIG.

  Here, if the angle of attack of the wing member 3 is constant regardless of the rotation angle of the first link 2, the rotational force obtained while the wing member 3 makes one round is canceled out, and the first rotating shaft 1. It cannot produce a rotational force.

  However, in the rotary blade of this embodiment, as described above, the angle of attack of the wing member 3 varies depending on the rotation angle, so the rotational force in the wing member 3 varies depending on the rotation angle. Then, as a whole rotor blade, a rotational force in a fixed direction (counterclockwise in the drawing in the example of FIG. 5) can be applied to the rotor blade.

  In the rotary blade of this embodiment, since the angle of attack of each blade member 3 is controlled by the second link 5, the mechanism can be simplified compared to the case where the angle of attack is controlled by an actuator. There are advantages.

  In addition, this rotary blade has an advantage that it does not require power for operating an actuator for controlling the angle of attack. If the prime mover itself for wind power generation consumes energy, the energy efficiency of the entire wind power generation decreases, but if the rotor blade of this embodiment is used, the energy efficiency of the entire wind power generation can be improved. It becomes.

  Moreover, according to the rotor blade of this embodiment, the electric power generating apparatus which generates electric power with the rotational force can be comprised.

  Furthermore, according to the rotor blade of the present embodiment, even if the blade member 3 has a simple plate shape, there is almost no decrease in the efficiency of extracting the rotational force from the wind force, so the manufacturing cost of the rotor blade can be kept low. There is also an advantage.

(Example)
Under the following conditions, the relationship between the position of the first rotating shaft 1 and the second rotating shaft 4 and the rotational speed was measured. In addition, how to take the dimension was shown in FIG.
Eccentricity e = 15cm
First link length lr = 150 cm
Second link length le = 147cm
Distance c = 35 cm between the first link and the second link at the attachment position to the wing member
The speed of the wind given to the rotor blades is three stages, about 8 m / s in the strong case, about 5.0 m / s in the middle case, and about 2 m / s in the weak case.

  The results are shown in FIG. In FIG. 6, “eccentric angle” indicates an eccentric angle of the second rotating shaft 4 with respect to the first rotating shaft 1. As for the method of taking the angle, in the wind direction, the state where the second rotation shaft 4 is located just behind the first rotation shaft 1 (just the leeward side) is 0 ° (or 360 °), and the opposite side (just The state where the second rotating shaft 4 is on the windward side is 180 °. Further, the data when the wind power is strong is represented by a square, the data when the wind is medium is represented by a triangle (Δ), and the data when the wind is weak is represented by a diamond.

As is clear from FIG. 6, the high rotational speed of the wing member 3 can be obtained in a state in which the second rotating shaft 4 is disposed approximately near the leeward side or approximately near the leeward side of the first rotating shaft 1. It was. When the second rotating shaft 4 is in the range of about 160 ° to about 210 ° and about 320 ° to about 10 °, particularly in the range of about 180 ° to about 200 ° and about 340 ° to about 0 °, the second rotational axis 4 has a particularly high rotational speed. I was able to get it. In FIG. 6, the range of about 180 ° to about 200 ° is described as “clockwise high eccentricity angle”, and the range of about 340 ° to about 0 ° is “counterclockwise high eccentricity angle”. " On the other hand, when the second rotating shaft 4 is on the side of the first rotating shaft 1 (in the vicinity of + 90 ° or −90 °), the rotational force of the blade member 3 could hardly be obtained. . In FIG. 6, the range of about 75 ° to about 95 ° is described as “an eccentric angle whose rotation direction is unstable (both rotate)”, and the range of about 250 ° to about 270 ° is “restraining rotation”. The eccentric angle ", that is, the fact that the wing member 3 is difficult to rotate is described. Note that the wing member 3 is difficult to rotate, and can be forcibly stopped at this position for maintenance, or used for safety improvement measures in strong winds.

  Therefore, it can be understood that the wind power can be converted into the rotational force with high efficiency by arranging the second rotating shaft 4 in the vicinity of the first rotating shaft 1 or the substantially upstream side of the first rotating shaft 1 by the adjusting mechanism 7. In addition, experiments with and without the adjusting mechanism 7 were also conducted. As a result, in the case where the adjusting mechanism 7 is not provided, the rotational force can be extracted at first, but the rotation stops and the rotational force cannot be extracted. Therefore, in the present embodiment, it is an essential requirement to provide the adjusting mechanism 7, and the adjusting mechanism 7 causes the second rotating shaft 4 to move to the first rotating shaft 1 in the fluid flow direction as described above. On the other hand, it can be arranged at a position where the highest rotational speed is obtained approximately near the downstream side or near the upstream side.

  In this embodiment, when the second rotary shaft 4 is on the windward side of the first rotary shaft 1, the rotational direction of the rotary blade, that is, the first rotary shaft 1, compared to the case on the leeward side. Was reversed. Therefore, the direction of rotation of the first rotary shaft 1 can be controlled by changing the position of the second rotary shaft 4. In the present embodiment, when the positional relationship between the blade portion 72 and the balancer 73 in the adjustment mechanism 7 is reversed, the positional relationship between the first rotating shaft 1 and the second rotating shaft 4 when receiving wind is reversed. be able to. For this purpose, for example, the base 71 may be temporarily detached from the second rotating shaft 4, the base 71 may be rotated 180 ° in the horizontal direction, and then the base 71 may be attached to the second rotating shaft 4 again. Thereby, the positional relationship of the blade | wing part 72 and the balancer 73 becomes reverse, and the rotation direction of the 1st rotating shaft 1 can be controlled. When the balancer 73 is not used, the position of the blade portion 72 may be changed to the opposite side with the second rotating shaft 4 interposed therebetween.

  The rotor blade according to the present invention is not limited to the above-described embodiment, and it is needless to say that various changes can be made without departing from the gist of the present invention.

  For example, in the above-described embodiment, the number of the first links 2 is four, but it is natural that the number is not limited to this. The number of the first links 2 may be even or odd.

  In this embodiment, the first links 2 have the same length and the same interval. However, the present invention is not limited to this, and the first links 2 may have different lengths or different intervals.

  Furthermore, in this embodiment, the wing member 3 is plate-shaped and attached to each first link 2 so as to be rotatable. For example, the wing member 3 is made of a material that can be elastically deformed, and this is the first link. 2 may be fixed. In short, the wing member 3 may be any member that can change the angle of attack by the second link 5.

  In this embodiment, a substantially rigid body is used as the second link 5, but a deformable material such as a string can be used for the second link 5. However, in this case, the wing member 3 needs to be provided with a restoring force capable of returning to the original position. Examples of the restoring force applying method include a method of attaching a spring to the wing member 3 and a method of using the wing member 3 itself as an elastic member. In short, the characteristic required for the second link 5 itself is that the separation distance between the second rotating shaft 4 and the blade member 3 can be kept constant.

  Furthermore, although the example which gives wind force to a rotary blade was demonstrated in the said embodiment, it is also possible to obtain rotational force not only by a wind but by giving other fluids, such as water.

  Moreover, in the said embodiment, although the blade | wing part 72 was formed in plate shape and the surface was arrange | positioned substantially parallel to the 1st or 2nd rotating shaft, the shape and arrangement | positioning state of the blade | wing part 72 are not restricted to these. . As the blade portion 72, when receiving wind, the second rotating shaft 4 gives a rotational force to the second rotating shaft 4 such that the second rotating shaft 4 moves leeward or upwind with respect to the first rotating shaft 1. Any configuration can be used. The blade portion 72 and the base portion 71 may be integrated.

  Furthermore, in the said embodiment, although the adjustment mechanism 7 was comprised by the base 71, the blade | wing part 72, and the balancer 73, as the adjustment mechanism 7, in short, according to the flow of the fluid, the 2nd rotating shaft 4 is made into the 1st. What is necessary is just to be located in the vicinity of the substantially downstream side or the substantially upstream side of the one rotating shaft 1. In particular, as the adjusting mechanism 7, the second rotating shaft 4 is positioned near the downstream side or the upstream side of the first rotating shaft 1 by using the force of the fluid itself without using another power source. Is preferred.

(Configuration of Second Embodiment)
The rotary blade includes a single rotary shaft 21, a first link R 1, a blade member 3, a second link R 2, a base 6, an adjustment mechanism 17, an eccentric bearing mechanism portion J, and a fixture 22. As a main element (see FIG. 7). Note that there is nothing corresponding to the connector 8 of the first embodiment.

  One rotating shaft 21 is provided with two upper and lower fixtures 22 for attaching the first link R1. The lower end of one rotating shaft 21 is attached to a bearing 61 of the base 6 so as to be rotatable with respect to the base 6.

  In the example shown in FIGS. 7 to 10, there are eight first links R1. The four first links R <b> 1 are attached to the lower fixture 22, and the remaining four first links R <b> 1 are attached to the upper fixture 22. These first links R1 are extended from the rotary shaft 21 in the outer direction. More specifically, each first link R1 is arranged in a direction extending radially from the rotation shaft 21. Further, the first links R1 are equal in length. The first links R1 in the same plane are equally spaced. The first link R <b> 1 is attached by the fixture 22 so as to rotate as the rotary shaft 21 rotates. These first links R1 are substantially rigid, although some deformation is allowed.

  In this embodiment, the wing member 3 has a simple rectangular plate shape. The wing member 3 is attached to the tip of each first link R1 via a connecting plate r. Here, the wing member 3 is attached to each first link R1 in a state of being rotatable (in this specification, it can be rotated in the forward and reverse directions at least within a certain angular range). Yes. The wing member 3 may be an airplane wing shape or a propeller shape. The cross-sectional shape of the wing member 3 is not limited to a rectangle, and an appropriate shape such as an ellipse or a circle can be selected.

  In this example, there are four second links R2. The second link R <b> 2 connects the one rotating shaft 21 and the wing member 3 via an eccentric bearing mechanism J. Each of the second links R2 has the same length, extends radially from the eccentric bearing mechanism portion J, and is connected to the tip end side of the second link R2 via the connecting member r. That is, the other end of the second link R <b> 2 is attached so as to be rotatable with respect to the wing member 3. In this example, a substantially rigid body is used as the second link R2. As for 2nd link R2, 1st member Ra and 2nd member Rb are connected, The length can be changed. That is, a bolt hole Ba and a positioning hole are formed in the connecting direction of the first member Ra and the second member Rb, and are connected by bolting with the bolt B at a position of a predetermined length. One end of the second link R2 is rotatably attached to the eccentric bearing mechanism J.

  The eccentric bearing mechanism portion J rotates eccentrically around the outer periphery of the rotating shaft 21 at a position that is eccentric from the center of the rotating shaft 21, and the eccentric bearing mechanism portion J is connected to the rotating shaft 21. And an outer peripheral portion Jb disposed on the outer periphery of the inner peripheral portion Ja, and a bearing Br is disposed between the inner peripheral portion Ja and the outer peripheral portion Jb. That is, the eccentric bearing mechanism portion J has a long portion and a short portion at the center of one rotating shaft 21, and the outer peripheral portion Jb is eccentric to the center of the rotating shaft 21. The outer periphery of the inner peripheral portion Ja is eccentrically rotated through the bearing Br at the position. With this configuration, the second link R2 is configured to change the angle of attack of the wing member 3 that rotates about the rotation shaft 2 as in the first embodiment.

  The adjustment mechanism 17 includes a rod-like base portion 17a and a blade portion 17b attached near the rear end of the base portion 17a. The base portion 17a is attached via a connecting portion 27 that is integrally connected to the eccentric bearing mechanism portion J. The blade portion 17b is formed in a plate shape. The eccentric bearing mechanism part J and the adjusting mechanism 17 can be mounted above the rotary shaft 21, but in order to ensure the stability of the vertically arranged rotor blades, It is attached to the lower side on the near side.

(Operation of the embodiment)
Therefore, when the blade portion 17b of the adjusting mechanism 17 receives wind in the rotor blade having the above-described configuration, the connecting portion 27 integral with the eccentric bearing mechanism portion J immediately rotates around the rotating shaft 21. That is, when the wing member 3 receives wind, the blade portion 17b of the adjustment mechanism 17 moves to the leeward side by wind force. Thereby, a rotational force is applied to the eccentric bearing mechanism portion J, and the eccentric bearing mechanism portion J rotates about the rotation shaft 21. Since the adjustment mechanism 17 is attached integrally with the eccentric bearing mechanism portion J, the eccentric bearing mechanism portion J immediately rotates around the rotation shaft 21. In FIGS. 9 and 10, the direction of the wind is indicated by an arrow.

  On the other hand, a rotational force is generated in the wing member 3 by wind force, and the rotational member 21 rotates around the rotational shaft 21 by this rotational force. Then, the second link R <b> 2 rotates about the eccentric bearing mechanism J through the wing member 3. When the wing member 3 receives wind, the first link R1 rotates about the rotation axis. Here, the wing member 3 is held at a constant distance from the eccentric bearing mechanism portion J by the second link R2, and is rotatable with respect to the first link R1. For this reason, the angle of attack of the wing member 3 with respect to the air flow changes according to the rotation angle of the first link R1 (FIGS. 9 and 10). The change in the angle of attack of the wing member 3 according to the rotation angle is the same as that in FIG. 5 described in the first embodiment. In addition, the operation and effect of the present embodiment are the same as those of the first embodiment, and the experimental example obtained almost the same results as those of the first embodiment. In other words, the adjusting mechanism 17 causes the rotation center (eccentric position) of the eccentric bearing mechanism portion J to have the highest rotational speed near the downstream side or the upstream side with respect to the rotary shaft 1 in the fluid flow direction. Here, the rotation center (eccentric position) of the eccentric bearing mechanism portion J refers to the eccentric position of the second rotating shaft 4 of the first embodiment corresponding to this ( (See FIG. 6).

  However, according to the present embodiment, since there is one rotating shaft 21, the number of parts can be reduced as compared with the first embodiment that requires the first rotating shaft 1 and the second rotating shaft 4. At the same time, since one rotating shaft 21 is connected to the base 6, the stability of the rotating shaft 21 is enhanced. In addition, if it rotates so that the upper end of a rotating shaft may be supported, the stability of a rotating shaft will be acquired further.

  Note that the rotor blades of the present embodiment are not limited to the above-described embodiment, like the rotor blades of the first embodiment, and the first blade is within the scope not departing from the gist of the present invention. Various modifications can be made in the same manner as the rotor blades of the embodiment. For example, as shown in FIG. 11, the number of the first links R1 and the second links R1 is three, and the wing member 3 is also composed of three, but the other configurations are the same as in the second embodiment. It is.

It is a perspective view which shows the schematic structure of the rotary blade which concerns on the 1st Embodiment of this invention. It is a front view of the rotary blade shown in FIG. FIG. 3 is a right side view of FIG. 2. FIG. 3 is a plan view of FIG. 2. It is explanatory drawing for demonstrating the change of the elevation angle accompanying rotation of a wing | blade member. It is a graph which shows the measurement result of the rotation speed in the rotary blade of an Example. It is a perspective view which shows schematic structure of the rotary blade which concerns on the 2nd Embodiment of this invention. It is sectional drawing of the rotary blade shown in FIG. FIG. 8 is a plan view of FIG. 7. It is explanatory drawing for demonstrating the change of the elevation angle accompanying rotation of a wing | blade member. It is a perspective view which shows the schematic structure of the other rotary blade which concerns on the said 2nd Embodiment.

Explanation of symbols

DESCRIPTION OF SYMBOLS 1,21 1st rotating shaft 11,22 Attachment 2, R1 1st link 3 Wing member 4 2nd rotating shaft 41 Bearing 5, R2 2nd link 6 Base 21 One rotating shaft 61 Bearing 7,17 Adjustment mechanism 71 , 17a Base portion 72, 17b Blade portion 73 Balancer 8 Coupling device 81 Bearing 82 Hole J Eccentric bearing mechanism portion Ja Inner peripheral portion Jb Outer peripheral portion Br Bearing

Claims (5)

A first rotating shaft, a first link, a plate-like wing member, a second rotating shaft, and a second link;
The first link extends from the first rotating shaft in the outer direction and is connected to one side of the plate-like wing member,
The plate-like wing member is attached in a rotatable state with respect to the first link ,
The second rotating shaft is connected to the first rotating shaft so that the second rotating shaft can be rotated eccentrically from the first rotating shaft ,
The second link extends from the first rotating shaft in the outer direction, and is connected to the second rotating shaft and the other side of the plate-like wing member ,
It is configured to keep a separation distance between the second rotating shaft and the wing member constant,
In addition, an adjustment mechanism that adjusts the position of the first rotation shaft to a predetermined position according to the flow of the fluid , and a position between the first rotation shaft and the second rotation shaft is provided. A rotating blade having a configuration in which the rotation direction of the first rotating shaft is reversed by reversing the relationship substantially in the fluid flow direction . Due to the configuration in which the adjustment mechanism and the rotation direction of the first rotation shaft are reversed , the second rotation shaft is arranged in the vicinity of the downstream side or the upstream side in the fluid flow direction. The rotor blade according to claim 1, wherein the rotor blade is disposed at a position where the highest rotational speed is obtained. One rotating shaft, a first link, a plate-like wing member, a second link, and an eccentric bearing mechanism,
The first link extends from the rotating shaft in the outer direction and is connected to one side of the plate-like wing member,
The plate-like wing member is attached in a rotatable state with respect to the first link ,
The second link is extended from the eccentric bearing mechanism portion in the outer direction, and is connected to the eccentric bearing mechanism portion attached to the rotating shaft and the other side of the plate-like wing member ,
It is configured to maintain a constant separation distance between the eccentric bearing mechanism portion attached to the rotating shaft and the wing member,
The eccentric bearing mechanism portion has an eccentric rotation mechanism that eccentrically rotates the outer periphery of the rotation shaft at a position eccentric from the center of the rotation shaft, and the second link is attached thereto.
Furthermore, an adjustment mechanism that adjusts the direction of the eccentric bearing mechanism portion according to the flow of the fluid is provided , and the positional relationship between the rotating shaft and the eccentric bearing mechanism portion is substantially reversed in the fluid flow direction. Thus, the rotating blade is configured to reverse the rotation direction of the rotating shaft . With the configuration in which the adjustment mechanism and the rotation direction of the rotating shaft are reversed , the rotation center of the eccentric bearing mechanism portion is the most in the vicinity of the downstream side or the most upstream side with respect to the rotating shaft in the fluid flow direction. The rotor blade according to claim 3, wherein the rotor blade is disposed at a position to obtain a high speed rotation speed.   The power generator which generates electric power with the rotational force by the rotary blade of any one of Claims 1-4.

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