JP2005188494A5 - - Google Patents

Description

Vertical shaft type impeller device

  The present invention is a vertical shaft type impeller device used in a device using fluid energy such as wind energy or hydraulic energy, and has a plurality of blades which are a kind of Savonius type particularly known as a low wind speed type. The present invention relates to a vertical-shaft impeller device that can be applied to a wind turbine as a matter of course.

A windmill, which is an impeller, has a main part that receives wind energy and a rotating shaft that transmits the energy, even though they are called “wings, feathers, blades, and propellers”.
Furthermore, the rotation axis is divided into a horizontal axis type represented by a propeller type parallel to the wind direction and a vertical axis type upright in the vertical direction.

The former is a windmill that rotates due to the rotational direction component of lift generated on the wings and is called a lift type, but it has the disadvantage that it is very difficult to start in a low-speed wind region.
In this respect, the vertical axis type is called a drag type, and when the wind hits the wing, a force of the rotational force component and a starting torque are generated by the drag, and there is an advantage of rotating regardless of the direction of the wind force. That is, it can be said that it is a very advantageous windmill for low-speed wind regions.

Therefore, it can be seen that the conventional vertical shaft type impeller has been developed mainly for wind power generation when it is used as a device. In fact, it can be said that the development of wind power is required more quickly.
Therefore, explanations in the present invention will be mainly explained for wind turbines using wind power. That is, for the time being, the vertical axis type impeller will be described as a vertical axis type windmill.
Note that wings, wings, blades, and the like are used as the names of the portions that receive the wind of the vertical axis type wind turbine, but in the text, all of them including the explanation of the prior art are expressed as “wings”.

Vertical axis type wind turbines include a battle type, a Savonius type, a gyromill type, and a Darius type.
Conventionally, many types of these wind turbines have been proposed. However, in most cases, the blades of the wind turbines are fixed to the rotating shaft or fixed to the tip of the arm extending from the rotating shaft. is there. Next, some conventional examples are introduced.

  The conventional example using a Savonius type windmill, which is a low-speed wind type, is characterized by the shape of the wing as a wind power generator, and the wing continues to a concave surface that becomes a wind receiving portion of the curved wing with a cross section perpendicular to the rotation axis The name of the invention “wind power generation” is to improve the power generation efficiency by increasing the strength and reducing the resistance to the inflow and outflow of the air by rolling the end of the outflow portion of the straight portion in the opposite direction to the concave surface and forming an S-shape. There is a device "(for example, refer to Patent Document 1).

  In addition, there are circular fixed frames above and below the outer periphery of the wing around the rotation axis of the wing, and a plurality of fixed frames are installed around the fixed frame so as to be directed outward from the fixed frame. The name of the invention “Savonius type windmill and Savonius type windmill using the Savonius type windmill”, which has blades and improves the power generation efficiency by making it easy to introduce the wind outside the blades into the blades due to the presence of this fixed blade (For example, refer to Patent Document 2).

Furthermore, as a crossflow type windmill that looks similar to the present invention, there is an arm that extends radially from a shaft that is a rotation shaft for output at the center, and a longitudinal axis is provided at the tip of each arm. There is a rotating body that can rotate as a center, and a power generator with blades that are erected so that the rotating angle can be freely changed around the support shaft in order to rotate the rotating body by receiving fluid Each of these wings is composed of a front wing, a middle wing, and a rear wing, and is configured to be freely deformable in three portions according to the wind direction so that lift can be generated.
And the name “power generation device” of the invention was proposed in which the attitude of each blade was changed to a predetermined rotation angle position based on the fluid orientation obtained by the detection of another fluid orientation detection means to improve the efficiency. (For example, refer to Patent Document 3).

Furthermore, the wind turbine of a small wind power generator that rotates from a wind speed of 1 m per second is a vertical axis type wind turbine in which five blades are arranged in a cylindrical shape around the rotation axis, and the wind turbine rotates in the horizontal direction. It is introduced as being able to reduce the cost (for example, see Non-Patent Document 1).

Japanese Patent Laid-Open No. 11-343959 ([0016], FIG. 2) Japanese Patent Laid-Open No. 11-062813 ([0019], FIG. 1) Japanese Unexamined Patent Publication No. 2003-155972 ([0006] to [0009], FIGS. 1 and 5)   Nikkei Sangyo Shimbun November 5, 2003 A13 Part 2 Global Environmental Economics Summit Special feature “Winning Change” article on wind power generation.

  However, in the wind turbine generator of Patent Document 1, even if the shape of the blade sandwiching the rotation shaft itself is an S-shape with the concave curved surface facing it, the blade can be used as the rotation shaft. Since it is fixedly provided, when the wing rotates and moves toward the windward side, there remains a problem that a considerable wind pressure resistance is applied to the back side of the wing.

  Further, in the Savonius type windmill of Patent Document 2, there are blades fixed to the rotation shaft, and a plurality of fixed frames are directed outward at an angle of about 45 degrees in the tangential direction in which the blades rotate. It is said that it is possible to reduce the amount of wind hitting the wing on the side moving against the wind, while increasing the amount of wind taken into the wing through the outside of the wing and fixing it at equal intervals When the wing rotates toward the windward side, the decrease in wind pressure resistance to the backside of the wing is not sufficient.

In the appearance similar to the present invention of Patent Document 3, wings are provided at the ends of a plurality of arms extending radially around the rotation axis. Each of the wings is divided into a front wing, a middle wing, and a rear wing, and the wind direction is detected by a separate fluid direction detection means so that lift generation is maximized with respect to the wind direction. In combination with the presence of the deformed circular control rail, the rotation angle is changed so as to be freely deformable, and the main shaft as the rotation shaft is efficiently rotated as a whole.
Therefore, although it can be said to be the most ideal device, it requires a fluid direction detection means, and since the blade itself is divided into three parts, various mechanisms for moving each of them are required, and the configuration is complicated at all. It must be expensive and expensive, and maintenance is also difficult due to the large number of parts.

  The wind turbine of non-patent document 1 has a simple configuration that makes it easy to take in the wind by making the cross section of the blade into a “T” shape, but it is strongest when the back surface of the blade is located on the windward and leeward sides. The problem of receiving wind resistance remains.

Each of these conventional examples has a configuration in which the blade is substantially fixed to the rotating shaft and the arm extending from the rotating shaft. For this reason, there is a drawback that a considerable wind pressure resistance is generated on the back side of the wing when rotating and moving from the leeward to the leeward. Would not have obtained.
An object of the present invention is to provide a vertical shaft type impeller apparatus that can be provided at a low cost with a relatively simple structure, starts rotating with a slight wind from any direction, and can obtain effective rotation even in a low wind speed range.

The basic configuration of the vertical shaft type impeller apparatus of the present invention will be described based on FIG. 1 as an example for easy understanding. In other plan views except FIG. 1 and FIG. 8, center lines and concentric circles are drawn with thin dotted lines so that the configuration of the present invention can be easily understood.
In the vertical shaft type impeller apparatus, the blade rotation shaft support 2 is provided in parallel with an interval between the blade rotation shaft support 2 above and below the vertical rotation shaft 1 so as to be orthogonal to the rotation shaft 1.

Between the upper and lower blade rotating shaft supports 2 and on the peripheral green side portion thereof, a blade rotating shaft 3 and a blade stopper rod 4 that are parallel to the rotating shaft 1 are provided upright. The blade rotating shaft 3 is freely rotated around the blade, and at least a part of the blade rotates to stop against the blade stopper rod 4, and the height is close to the length of the blade rotating shaft 3. It is assumed that rectangular wings 5 are provided.
The blade rotating shaft 3, blade impingement body 4, and blade 5 constitute a basic unit of one impeller. A vertical axis type impeller apparatus is characterized in that a plurality of sets are arranged so as to be all equidistant between the basic unit and the adjacent basic unit to form the whole.

Since the shape of the wing 5 is rectangular as a whole, the short side is the upper and lower sides. The cross-sectional shape of the short side is best a streamlined shape similar to the cross section of an airplane wing as shown in FIG.
In addition, it is set as the vertical axis | shaft type impeller apparatus which the blade rotating shaft 3 of the rotating blade | wing 5 is in the position suitably shifted | deviated from the one end in the short side of the blade | wing 5, and comprises a basic unit.
The position where the blade rotation shaft 3 is displaced in the blade 5 is the position of the blade 5 when the blade rotation shaft 3 is used as a core and the blade tail 8 of the blade 5 is held and rotated 180 degrees from the blade stopper rod body 4. The short wing head 7 is positioned so as to hit the opposite side of the wing stop dedicated body 4.

Further, a vertical shaft type impeller apparatus in which the blade rotation shaft 3 of the rotating blade 5 is located at one end of the short side of the blade 5 and constitutes a basic unit may be used.
At that time, as shown in FIG. 7, the vertical shielding plate 6 is provided along the outer periphery of the blade rotating shaft support 2 from the position in contact with one long side of the blade 5 and over the vertical interval length thereof. It is also possible to.
Furthermore, in each example where the vertical shielding plate 6 is not provided, the blade stopper rods 4 may be provided on both the left and right sides of the blade rotation shaft 3 as shown in FIG.

  Although the above-described blade 5 has been shown in a single state, as shown in FIG. 9, a plurality of blades 5 having blade rotation shafts 3 are arranged in series as a blade row 10, and blade blades 10 are arranged on the left and right sides of the blade row 10. It is good also as a structure which provided the stop rod body 4. FIG.

.
The blade rotating shaft support 2 may be an arm extending radially from the rotating shaft 1, but it is better to prevent the fluid taken in the shape of a disk from flowing out in the vertical direction.

  The position where the blade stopper rod body 4 of each of the above-mentioned examples is erected has an important meaning in the present invention. That is, when the rotating shaft 1 rotates, the blade 5 is positioned so that the short sides of the blade 5 are orthogonal to the direction of arrival of fluid energy so that the blade 5 can receive energy most efficiently. At the same time, the short side of the blade 5 is set in a parallel state in the fluid flow direction so that the loss of fluid energy is minimized. It must be provided at a position that satisfies both.

However, the effect of the present invention cannot be satisfactorily brought out only by this. The reason will be described with reference to FIGS. In both figures, four sets of basic units in which four blades 5 are provided on the both blade rotating shaft support 2 are shown, and the fluid will be described with wind.
A large arrow at the bottom of both figures represents the wind direction. In any of the drawings, the rotation direction of the rotary shaft 1 is assumed to be opposite to the clockwise direction, that is, counterclockwise.

As shown in FIG. 2, if the blade rotation shaft 3 and the blade stopper rod body 4 are all arranged on a line passing through the center of the rotation shaft 1, the blade 5 rotates the blade rotation shaft 3 lightly and freely. Therefore, a part of the wing 5 stops against the wing stop rod 4 and only the wing 5 on the right side of the rotating shaft 1 is perpendicular to the wind direction and receives strong wind, and the other three places. The wing 5 is parallel to the wind direction, so the wind resistance is minimized and seems to be considered most efficient, but it is actually wrong.
In addition, what was represented by a chain line is a state in which the blade 5 is inverted. In this way, even if it is reversed, the direction of each wing 5 does not change, so that there is no significant change in effect.

In FIG. 3, all the wing stop rods 4 are slightly shifted to the right. The posture of the wing 5 on which the wind strikes changes just by slightly shifting in this way. At the same time, the rotation shaft 1 is smoothly rotated.
That is, the right and upper wings 5 stop against the wing stop rod body 4, but the left and lower wings 5 are parallel to the wind direction due to the flow of the wind and are separated from the wing stop rod body 4. It becomes a state.
When the wind enters the apparatus from below, it strikes the right wing 5 to generate a rotational torque, and the wind flows obliquely upward along the right wing 5 and strikes the upper wing 5.
Since the directions of the right wing 5 and the upper wing 5 are orthogonal to each other, the wind that hits the upper wing 5 from the right produces an effect of generating rotational torque even in the upper wing 5.

  The wind hitting the upper wing 5 flows away slightly upward in FIG. What is represented by a chain line is a state in which the blade 5 is inverted. In this way, even if it is reversed, the direction of each wing 5 does not change, so that there is no significant change in effect.

The reason why the rotation is not smooth in the case of FIG. 2 can be considered as the reason why the right wing 5 in FIG. 2 is more sensitive to the wind direction than the right wing 5 in FIG. Since the wings 5 themselves generate a large rotational torque, there is a problem in the subsequent direction of the struck wind.
In other words, the bounced wind hits the lower wing 5 and the left wing 5 and tries to change the direction of both wings 5. It is thought that this is because it is difficult to obtain rotational energy as a result. Therefore, when the impeller of the present invention is used as a windmill, the arrangement of the wings 5 in the posture as shown in FIG. 2 is not adopted.

  These vertical shaft type impeller apparatuses according to the present invention can be applied to both, as described above, as a windmill using wind energy as a power source, and as a turbine using hydraulic energy as a power source. Furthermore, it is natural that the energy can be connected to a mechanism or the like that directly uses the energy as power, or can be connected to a generator.

According to such a vertical shaft type impeller apparatus of the present invention, the following effects can be obtained.
(A) Since a basic unit of one set of impellers is configured assuming that the blades 5 rotate freely around the blade rotation shaft 3 and have one end stopped against the blade stop rod body 4, By selecting the optimum position of the stop rod body 4, the direction of the blade 5 with respect to the rotating shaft 1 can be easily determined. Therefore, the trajectory of the wind flow associated with the arrangement of each blade 5 is taken into consideration. As a result of receiving fluid energy, the most efficient energy exchange can be achieved, and the rotating shaft 1 can smoothly rotate.

(A) Further, the blade rotating shaft 3 has a structure in which the blade 5 is smoothly and freely rotated, so that the blade 5 can start to rotate even if the fluid energy is a slight force. Since the direction of is naturally parallel to the direction of fluid flow at a position where it does not contact the blade stopper rod body 4, there is no need to worry about wind resistance on the back surface of the blade as in the conventional example. The loss of is minimal.

(C) In the case where the blade stopper rods 4 are provided on both the left and right sides of the blade rotation shaft 3, the rotation range of the blade 5 with respect to the blade rotation shaft 3 is limited, so that swinging due to centrifugal force or the like is suppressed. The impact force at the time of impacting with the wing stop dedicated body 4 can be reduced, and the durability can be improved.
Further, although not shown, shock absorber material is provided on the blade 5 and the blade stopper rod body 4 in order to reduce the stopping force.

(D) In the case where the blade rotation shaft support 2 is a disc shape, the blade rotation shaft support 2 is provided parallel to each other so as to be orthogonal to the rotation shaft 1, and the height of the rectangular blade 5 is increased and decreased. By making the length close to between the blade rotation shaft supports 2, the space between the upper and lower blade rotation shaft supports 2 corresponding to the area of the blade 5 is occupied, so that the fluid energy received by the blades 5 is increased and decreased. The efficiency can be increased with the effect of not escaping in the direction.

(E) From the above, although it is for both wind and hydraulic power, it can be manufactured at a low cost with a relatively simple structure, and when the blade 5 rotates from the fluid arrival side to the fluid outflow side, a large amount of fluid energy pressure is generated. When the wing 5 rotates from the fluid outflow side to the fluid arrival side, the fluid energy pressure resistance received by the wing 5 can be reduced as much as possible. In the beginning, it was possible to make effective rotation even in the low wind region.

(F) A structure in which a plurality of blades 5 having blade rotation shafts 3 are arranged in series, and blade stopper rods 3 are provided on the left and right sides thereof, the occupied rotation range of one blade 5 is reduced. The stopping force when 5 stops against the blade stopper rod 4 or the blade rotating shaft 3 can be reduced.

  Considering that the present invention is optimal for wind power use, there is a rotary shaft 1 for taking out rotational power in the center of a horizontal rotation type impeller device, and it is provided at the upper and lower portions so as to be orthogonal to the rotation shaft 1. The blade rotating shaft support 2 is simply a disk. In the vicinity of the outer periphery of the blade rotating shaft support 2 which is this disk, an elongated blade rotating shaft 3 and a similarly elongated round rod impingement rod body 4 are provided in the vicinity of the rotating shaft 1 in the vicinity thereof. 3 is a basic unit of a set of impellers having a rectangular wing 5 that easily rotates about the core 3 and that has one end that stops against the balance rod 4.

  The basic units of the impeller are arranged at equal intervals in the vicinity along the outer periphery of the blade rotating shaft support 2 that is a disk. As shown in FIG. 5 and FIG. 7, at least 4 sets are necessary, and it cannot be said that the expected output and the size of the device is different depending on whether the fluid is wind or water, but 6 sets as shown in FIG. Is the best.

Considering the shape of the wing 5 here, it is rectangular in the length direction, but the cross-sectional shape at the short side is preferably a streamlined type like an airplane wing as shown in FIG. It can be said that the blade rotation shaft 3 is preferably hidden in the blade 5.
In FIG. 8, a certain position of the blade rotation shaft 3 in the blade 5 is approaching the blade head 7 side, and the distance between the blade tail 8 and the blade rotation shaft 3 is 5 as a result of the experiment. A preferable result is obtained in which the distance between the end of the head 7 and the blade rotation shaft 3 is 3.

In FIG. 4, the wing 5 having the shape as shown in FIG. 8 is drawn, but the wings 5 in the other drawings are schematically drawn as black and thin arrows. It explains using.
In order to maintain the best trajectory of the fluid flowing through the blade 5, an auxiliary blade 9 having an appropriate length that is soft and freely flutters may be added on the extension line of the blade tail 8.

  Next, the operation of the present invention will be described with reference to FIG. First, at the beginning of the wind, the wings 8 on the lower side and the left side with respect to the wind direction (downward arrow) are in a position where they do not touch the wing stop rod body 4, so that the wing tail 8 faces the leeward while being parallel to the wind direction. ing. The right and upper wings 5 are pushed by wind pressure, and a part of the wings 5 is stopped by the wing stop rod body 4 so that the wing tail 8 changes its direction as shown in the figure. Acquires wind and stores wind power.

  This wind energy can rotate the rotating shaft 1 counterclockwise together with the blade rotating shaft support 2 via the blade stopper rod 4 to generate rotational torque, and power can be extracted from the rotating shaft 1 as rotating energy. Furthermore, the flow of the wind hitting the right wing 5 hits the upper wing 5 and generates a rotational torque here, and escapes in the upper right direction in FIG. Actually, since the blade rotating shaft support 2 is rotating counterclockwise during the above-described period, the wind path is slightly shifted to the left from the above.

When the rotational speed of the rotary shaft 1 increases, all the blades 5 rotate around the blade rotary shaft 3 as a result of the generation of centrifugal force, and let the blade tail 8 jump out of the blade rotation support 2. And
However, since the centrifugal force is generated by the rotation of the blade rotating shaft support 2 generated by the wind force, the centrifugal force is not generated without the wind force. Therefore, since normal centrifugal lift and this centrifugal force do not reach the wind energy, the direction of the wings 5 when the wind is strong windward, that is, when turning to the left and lower positions, is greater than the wind force. Therefore, the wing tail 8 is always directed to the leeward while maintaining the same direction as that at the time of starting, that is, parallel to the wind direction.

The upper wing 5 located on the leeward side is just below the wind (upper side in FIG. 3), and the wind energy is weakened due to the leeward side. Since it starts to rotate counterclockwise away from the body 4, the wing tail 8 at that time also takes into account the wind flow in combination with the centrifugal force, so the wing 5 suddenly reverses 180 degrees around the wing rotation axis 3. The wing tail 8 of the wing 5 is in the state farthest away from the wing rotating shaft support 2. It is the state shown by the chain line in FIG.
The subsequent operation is the posture of the left and lower blades 5 as described above, parallel to the laminar flow, reducing the wind pressure resistance as much as possible, and reducing the loss of rotational energy. It can be rotated.

  By the way, as described above, it is best to set six basic units of the impeller as shown in FIG. That is, the size of the wing 5 itself is relatively smaller than that of the four sets, but the orientation of each wing 5 and its wing tail 8 is in the posture shown in FIG. 6 with respect to the wind direction from below. In other words, when the blade 5 is brought into contact with the blade stopper rod 4, the blade rotation shaft 3 and the blade stopper rod 4 are moved so that the direction of the blade tail 8 points obliquely with respect to the right adjacent blade 5. It is disposed on the rotary shaft support 2.

In this case, since the number of blades 5 is larger than that of four sets of basic units, the flow of wind becomes smooth, and the rotation balance is improved as a whole, thereby improving the efficiency.
In FIG. 6, as indicated by the chain line, the blade 5 is suddenly reversed when the upper blade 5 passes just below the wind, and the blade tail 8 moves outward from the blade rotating shaft support 2. It becomes a state.

Therefore, the number of basic units of the impeller in the apparatus of the present invention is preferably around six. If it dares to limit, it seems that it is good to compose with 4-8 sets.
Below that, the rotational force is insufficient and the output is too low. Even if the wing 5 is made smaller than that, the wings 5 interfere with each other and obstruct the passage of the wind, disturbing the flow of the wind and improving the efficiency. Will be reduced.

Embodiments of the present invention will be described below with reference to FIGS. Here, in each Example, the component which has the same function attaches | subjects the same code | symbol, and abbreviate | omits or simplifies description.
First, FIG. 1 shows a typical vertical axis type impeller apparatus in which four basic units of the impeller of the present invention are used, and it uses natural wind power. Since the size may be determined according to the target output, all dimensions are omitted, but it is believed that the size of each part can be determined relatively sufficiently from the figure.

The upper and lower blade rotating shaft support 2 is a disk and the blade 5 is rectangular, but the material may be selected according to the usage environment, it is made of titanium for durability, aluminum for light weight, iron or wooden for cost, In the vicinity of the sea, a plastic or the like that is excellent in corrosion resistance may be used.
The blade stopper rod body 4 and the blade rotating shaft 3 will be elongated steel rods, but may be made of a hard synthetic resin. The blade rotating shaft 3 may be either fixed to the upper and lower blade rotating shaft supports 2 or rotatably mounted on both ends of the blade rotating shaft 3 as long as the blade 5 can be rotated as easily as possible.

In FIG. 1, the blade rotation shaft support 2 is rotatably attached to the upper and lower sides of the blade rotation shaft 3, and the entire length is shown as being bonded and welded to one surface of the blade 5.
The position of the blade stopper rod body 4 is a position where both the blade head 7 and the blade tail 8 of the blade 5 can stop, and is provided in FIG. 3 provided inside the vertical shaft 4, that is, closer to the rotating shaft 1. I want you to see it.

The second embodiment will be described with reference to FIG. 4. Since the blade 5 has a cross section as shown in FIG. 8 and the blade rotation shaft 3 is in the blade 5, the streamlined shape of the blade 5 remains unchanged. Since it appears on the outer periphery, disturbance of the wind flow is reduced, which is a preferred embodiment.
However, for comparison, all the basic units other than the shape of the blade 5 are shown as the same as those in FIG. 3, but when the streamlined blade 5 in FIG. In particular, it can be seen that the wing tail 8 direction of the right wing 5 appears significantly different. The dimensions should be determined taking this into consideration.
In addition, although the chain line was drawn imagining the case where the wing | blade 5 reversed at the position, it does not actually reverse.

As shown in FIG. 5 as the third embodiment, the blade stopper rods 4 are provided on the left and right sides of the blade rotation shaft 3 for the purpose of limiting the rotation range of the blade 5.
The position of the rotating shaft 3 in this embodiment is assumed to be the outer peripheral edge of the blade rotating shaft support 2 and the tip of the blade head 7 of the blade 5.
The blade stopper rod body 4 has one side (left side) at the outer peripheral edge of the blade rotating shaft support 2 and the other side (right side) at 120 degrees from the blade stopper rod body 4 on the outer peripheral edge side. The position is set to an angle.
Thus, when the wind blows from below, the wings 5 are each in the posture shown in FIG.

That is, similar to the embodiment of FIG. 3, the wind that hits the right wing 5 continues to hit the upper wing 5. If comprised in this way, the rotation range with respect to the blade rotating shaft 3 of the wing | blade 5 will be restrict | limited, The swinging force of the wing | blade 5 by centrifugal force etc. will be suppressed, and the striking force with the wing | blade stop rod body 4 can be made small. As described above, the durability can be improved.
In FIG. 3, the positions of both blade stopper rods 4 are equidistant from the blade rotation shaft 3.

As shown in FIG. 7, the fourth embodiment is a vertical shaft type impeller apparatus having a vertical shielding plate 6 different from the above-described embodiments.
For ease of comparison, the description will be made in comparison with FIG. That is, except for the blade stopper 4 on the outer peripheral edge of the blade rotation shaft support 2 of FIG. 5, instead, the blade rotation shaft 3 between that position and the upper and lower blade rotation shaft support 2 is replaced. A vertical shielding plate 6 is provided.

Such a configuration is suitable for a water turbine. In other words, unlike the wind current, the water flow has a weight that cannot be compared, and it is easy to obtain it with a large rotational energy.
Also, there is a clear width in the water stream unlike the wind. Therefore, although it is installed in the water, the design will be somewhat different depending on whether it is installed in a half-submerged state, but in short, it is only necessary to catch the water and obtain the rotational torque. Therefore, the inventor made the shape of the wing 5 slightly concave and provided the vertical shielding plate 6 so as not to let inflowing water escape.

Since the vertical shielding plate 6 is provided between the upper and lower blade rotating shaft supports 2, a water receiving packet is formed by these and the blade 5, and the water flow can be surely received.
Although not shown in the drawings, in this vertical shaft type impeller apparatus for hydropower, when installed in a water stream, it is more natural to install it horizontally like a turbine than in a vertical installation in the water stream. .

  Here, as shown in FIG. 9, a plurality of blades 5 having blade rotation shafts 3 are arranged in series, and the blade impacting bodies 4 are provided on the left and right sides. Thus, the range in which the small single blade 5 occupies and rotates is reduced, and the stopping force of the blade 5 to stop against the blade stopping rod body 4 and the blade rotating shaft 3 can be reduced.

  Further, for additional explanation, in FIG. 10, the flow of wind and the isobars of wind are shown by thin lines. As can be seen, the compressed portion and the lean portion of the air can be seen, that is, the air that has entered the impeller Therefore, the air that has entered the impeller from the lower arrow is compressed by the right and upper wings 5, and the wings 5 are dragged. Further, the air released from the inside of the impeller is released from the compression, and a lean air component is formed on the right side and the back side of the upper wing 5 so that the wing 5 is lifted.

In the above-described embodiments, if the fluid may escape in the vertical direction, although not shown in the drawings, the blade rotating shaft support 2 is replaced with a disk, and an arm extending radially from the rotating shaft 1 part to the periphery, The basic unit of the impeller may be provided around the tip of the arm.
Further, the blade 5 fixed to the blade rotation shaft 3 is used as an attachment means between the upper and lower blade rotation shaft supports 2, and the pipe is used as a pipe of the blade rotation shaft 3 itself that rotatably penetrates the mandrel. Various conventional means may be used, such as fixing both ends of the mandrel to the upper and lower blade rotating shaft supports 2, and the present invention is not limited by the adoption of these equivalent means.

  By extracting fluid energy as rotational kinetic energy, it can be used for any device that requires rotational motion. However, if the purpose is changed and the size is reduced and an appropriate picture is drawn on the wing 5, it can be used as an indoor display. It is also possible.

  It is a perspective view which shows the Example of this invention. (Example 1)   It is a top view for description for demonstrating the quality of operation | movement of this invention.   It is a top view for operation | movement explanation which shows the Example of this invention.   It is a top view for description which changed the shape of the wing | blade in FIG. (Example 2)   It is the top view for operation | movement explanation shown as what provided the blade | wing stopper rod body in the both sides of the wing | blade in the other Example of this invention. Example 3   It is a top view for operation | movement description in further another Example of this invention.   It is the top view for operation | movement explanation shown as what provided the vertical shielding board in other Example of this invention. (Example 4)     It is sectional drawing of a short side direction in one Example of the wing | blade of this invention.     (Example 5) which is the top view for description which showed the blade cascade of this invention   It is an illustration of the isobar of air of this invention, and a lean part.

Explanation of symbols

DESCRIPTION OF SYMBOLS 1 Rotating shaft 2 Wing rotating shaft support body 3 Wing rotating shaft 4 Wing stop dedication body 5 Wing 6 Vertical shielding board 7 Wing head 8 Wing tail 9 Auxiliary wing 10 Blade row

Claims (9)

  In the vertical shaft type impeller apparatus, the blade rotation shaft support (2) is provided in parallel with a space between the blade rotation shaft support (2) above and below the rotation shaft (1) so as to be orthogonal to the rotation shaft (1). A blade rotation shaft (3) parallel to the rotation shaft (1) and a blade stopper rod body (4) are erected on the peripheral edge of the space between the two blade rotation shaft supports (2) to rotate the blade. The shaft (3) rotates freely about the core, and at least a part of the shaft rotates to stop against the blade stopper rod (4), and the height is the length of the blade rotating shaft (3). A basic unit of one set of impellers is constituted by the blade rotation shaft (3), blade stopper rod body (4), and blade (5) provided with a rectangular blade (5) that is close to A vertical shaft type impeller apparatus, wherein a plurality of sets are arranged so that a distance between the one set of basic units and the adjacent basic unit is all equal.   The vertical axis type wing according to claim 1, wherein the wing rotation axis (3) of the rotating wing (5) is located at a position appropriately deviated from one end on the short side of the rectangular wing (5) to constitute a basic unit. Car equipment.   The vertical shaft type impeller apparatus according to claim 1, wherein the rotating shaft (3) of the rotating blade (5) is at one end of the short side of the rectangular blade (5) and constitutes a basic unit.   The vertical shaft type impeller apparatus according to any one of claims 1 to 3, wherein the blade stopper rod body (4) is provided at both left and right ends of the blade rotation shaft (3).   The vertical shielding plate (6) is disposed along the outer periphery of the two-blade rotary shaft support (2) from the position in contact with one long side of the blade (5) and over the vertical distance of the two-blade rotary shaft support (2). The vertical axis type impeller apparatus according to claim 3 provided.   The vertical shaft type impeller apparatus according to any one of claims 1 to 5, wherein the blade rotating shaft support (2) has a disk shape.   The vertical shaft type impeller apparatus according to any one of claims 1 to 6, wherein wind energy is used as a driving force and is used as a windmill.   The vertical axis type impeller apparatus according to any one of claims 1 to 6, wherein hydraulic energy is used as a driving force and is used as a turbine.   The vertical axis type impeller apparatus according to any one of claims 1 to 8, wherein a plurality of blades (5) each having a blade rotation shaft (3) are arranged in series.