TW201706497A - Turbine rotor and natural energy generator system having same - Google Patents

Abstract

The turbine rotor (18) includes a main shaft (22) rotatable about an axis thereof, and blades (24) which are fixed to the main shaft (22) and rotate about the axis by being driven by wind power or water power. Each of the blades (24) includes a straight portion (28) extending in a parallel direction or in a vertical direction with respect to the main shaft (22) and a blade tip portion (29) extending from an end portion from the straight portion. The blade tip portion (29) is so formed as to have a cross-section, which is cut along a plane containing the axis of the main shaft (22), of a shape inclined away from the straight portion (28) in plural steps from its base end toward a tip, or of a shape curved away from the straight portion (28) from its base end toward a tip.

Description

Impeller and natural energy power generation device with impeller

The present invention relates to an impeller and a natural energy power generation device, which relates to a technique for improving conversion efficiency of converting wind, hydraulic or tidal energy received by a blade into rotational energy, and improving blade strength.

The windmills or waterwheels of natural energy power generation devices are roughly classified into two types: horizontal axis type and vertical axis type. Vertical axis type is used for smaller windmills or waterwheels because it does not need to control wind direction, water flow direction and power flow direction.

In a wind turbine or a waterwheel for vertical axis power generation, the shape of the tip end portion of the blade is designed in order to improve the conversion efficiency of converting wind, hydraulic power or tidal energy into rotational energy. For example, by tilting the tip end portion of the blade toward the vertical main axis, energy received from wind, water, or tidal current can be efficiently converted into rotational energy. This inclined blade front end portion is referred to as an aileron. By providing this aileron, the wing tip vortex from the tip end of the blade can be reduced to become a highly efficient blade (Patent Document 1). [Prior Technical Literature] [Patent Literature]

Patent Document 1: Patent No. 4173727

[Problem to be Solved by the Invention] In a natural energy power generation device, how to efficiently convert the energy received by the blade into rotational energy is an extremely important factor. This conversion efficiency (power factor) is theoretically limited to 16/27 (Bez limit). Relative to this limit value, the current blade conversion efficiency is about 0.3 to 0.45, and in order to improve the conversion efficiency, it is necessary to further improve the blade.

Fig. 18A is a front view of a blade 50 of a vertical shaft type power generation wind turbine or a waterwheel according to a conventional example, and Fig. 18B is a sectional view taken along line XVIIIB-XVIIIB of Fig. 18A. In the blade 50, when the angle θ formed by the straight portion 51 and the aileron 52 is equal to or smaller than a predetermined angle, there may be a fear that stress is concentrated on the joint portion 53 connecting the flat portion 51 and the aileron 52. . In this case, problems arise in the strength of the blade.

When only the angle θ of the joint portion 53 is increased, since the entire length La of the blade is defined by the size of the windmill or the waterwheel, the length Lv of the straight portion 51 is shortened. In this case, the conversion efficiency is lowered due to a substantial decrease in the wind receiving area or the water receiving area.

It is also possible to increase the angle θ of the joint portion 53 below the length Lv of the straight portion 51. In this case as well, since the full length La of the blade 50 is defined, the horizontal direction length Lh of the aileron 52 is made shorter. As a result, the effect of reducing the tip vortex is deteriorated.

The invention aims to provide an impeller and a natural energy power generation device provided with an impeller, which can improve the conversion efficiency of converting the energy received by the blade into rotational energy in the impeller, and can improve the blade strength. [Method of solving the problem]

The impeller of the present invention comprises: a main shaft disposed to rotate freely about an axis; and a vane fixed to the main shaft and driven to rotate around the shaft by wind or hydraulic force, wherein: the vane has: a straight portion extending in a direction parallel or perpendicular to the main axis; and a blade leading end portion extending from an end portion of the straight portion, the blade leading end portion cutting the blade leading end portion in a plane including the spindle axis The cross-sectional shape is formed such that the shape is inclined to a plurality of segments as it goes away from the straight portion from the base end to the front end, or is further away from the straight line as it goes from the base end to the front end The shape of the part is curved. The impeller is a windmill or a waterwheel.

According to this configuration, the cross-sectional shape of the spindle axis including the tip end portion of the blade is formed so as to be inclined in a plurality of stages so as to be away from the straight portion from the base end toward the tip end, or The shape that is curved from the base end to the front end and away from the flat portion can reduce the wrap vortex from the tip end of the blade.

In particular, when the tip end portion of the blade is inclined to a plurality of stages, the entire tip end portion of the blade can be largely inclined even if the bending angle of the tip end portion of the blade is slowed down compared with the case where the blade is inclined at a plurality of stages. Therefore, when the entire length of the blade is fixed, it is ensured that the horizontal length of the tip end portion of the blade is a desired length, and the length of the straight portion is ensured to be long.

Further, in particular, when the tip end portion of the blade is curved, a portion of the tip end portion of the blade is not inclined as much as possible, and the entire tip end portion of the blade is largely inclined as compared with the case where the blade is formed to be inclined. Therefore, when the entire length of the blade is fixed, it is ensured that the horizontal length of the tip end portion of the blade is a desired length, and the length of the straight portion is ensured to be long.

In this way, since the length of the long flat portion can be obtained, the conversion efficiency of the wind, hydraulic or tidal energy (referred to collectively as "natural energy" or simply "energy") to the rotational energy can be improved. . Further, by ensuring that the horizontal length of the tip end portion of the blade is a desired length, the tip vortex generated from the tip end of the blade can be surely reduced. Further, when the tip end portion of the blade is inclined in a plurality of stages, since the bending angle of each joint portion can be alleviated, the stress acting on the bent portion can be reduced, and the strength of the blade can be improved. When the tip end portion of the blade is curved, since the local bending angle of the tip end portion of the blade can be reduced, the stress acting on the bending portion of the tip end portion of the blade can be dispersed, and the strength of the blade can be improved.

In one embodiment of the present invention, the flat portion of the blade may extend in parallel with the main axis, and the blade may be coupled to the main shaft by the support at a position away from the main shaft in a radial direction. That is, the impeller may also be a vertical axis type impeller having a vertical main shaft (spindle) that is freely rotatable about an axis; a support body integrally provided on the vertical main shaft; and a blade connected by the support body The vertical spindle is rotated about the axis by wind or hydraulic drive.

In an embodiment of the present invention, the impeller may be a vertical wind turbine for wind power generation, and the plurality of blades extending in the vertical direction are disposed away from the vertical main axis and are disposed around the vertical main axis. When the wind turbine is installed in the northern hemisphere of the earth, the cross-sectional shape of each of the blades is a shape in which the wind force is rotated in a counterclockwise direction in a plan view.

During the development of small wind turbines, it was learned that by defining the direction of rotation of the blades as a specific direction, the blades can be rotated even with the energy of the breeze. Specifically, in Japan, which is located in the northern hemisphere, the direction of the blade extending in the vertical direction of the vertical-axis windmill is reversed and attached to the main shaft to confirm, and it is found that the left-handed rotation is the same under the same condition as the right-handed rotation. Rotation is preferred. In the northern hemisphere, due to the Earth's rotation, the vortex from the typhoon, vortex, and even the drain is all left-handed (counterclockwise). This is generally believed to be due to the Coriolis force produced by the Earth's rotation. On the other hand, due to the cross-sectional shape of the blade, when the blade is subjected to wind, the direction of rotation of the windmill can be determined according to the lift generated by the difference in air velocity flowing through both sides of the blade. According to the wind turbine having such a configuration, when the wind turbine is disposed in the northern hemisphere, the shape of the cross-sectional shape of each blade is a shape of a rotational force that rotates counterclockwise in a plan view by the wind force, so that the blade has a clockwise rotation relative to the conventional one. The vertical axis wind power generation windmill can effectively utilize the effect of the earth's rotation, and reduce the rotational impedance, and can rotate most of the blades under the same conditions. Therefore, by using a wind turbine for power generation having a vertical main shaft, power generation can be performed with a smaller wind energy.

In an embodiment of the invention, the straight portion of the blade may extend outward in a radial direction with respect to the main axis. That is, the impeller can also be a horizontal axis impeller.

In an embodiment of the present invention, the tip end portion of the blade may be formed in a tapered shape whose width is narrowed from the base end to the tip end. In this case, the wing tip vortex can be further reduced as compared with the case where the blade tip end is set to a flat shape. Therefore, the conversion efficiency of converting the energy received by the blade into rotational energy can be further improved.

A natural energy power generation device according to the present invention includes: the impeller according to any one of the embodiments of the present invention; and a generator driven by the impeller. According to this configuration, the conversion efficiency of converting the energy received by the blade into the rotational energy can be improved more than the conventional product. Therefore, in particular, in the vertical axis type, the natural energy power generation device can be installed in a place that cannot be installed in the past. Moreover, since the blade strength can be further improved by the conventional product, for example, the blade material can be reduced or the maintainability can be improved.

In the natural energy power generation device according to the embodiment of the present invention, the generator may be a self-excited generator including: an output core wound around an output winding; and a magnetic field core wound around a main magnetic field winding and a secondary magnetic field winding, one of the output iron core and the magnetic field iron core is a stator, and the other is a rotor, wherein the magnetic field windings are connected to a rectifying mechanism, and the rotation of the vanes causes the stator and the rotor to rotate relative to each other The generated electric power is further provided, and the generator further includes an initial excitation mechanism that generates a magnetic force required for the excitation at the initial stage of power generation.

In the case of this configuration, since the generator is self-excited, it does not need to be powered by him, so the configuration is simple, and there is no need to apply a permanent magnet to the magnetic field, and the torque is not problematic. Since the torque is small, the torque can be started with a small torque. A magnetic field is required to start the operation. If there is residual magnetic flux, it can start to operate. However, due to long-term placement or maintenance, the residual magnetic flux may disappear. If the residual magnetic flux disappears, the operation cannot be started. However, since the initial excitation mechanism is provided, it is possible to surely start the operation. Since the magnetic flux that becomes the magnetic field increases with the rotation, the magnetic flux required for the initial excitation is only a small amount, and the influence on the torque is small, and the rotation can be started with a small torque to generate electricity.

As described above, the self-excited generator including the initial excitation mechanism has an advantage that it can be rotated with a small amount of torque and can reliably generate power. On the other hand, the impeller having the inclined tip end portion of the blade can improve the conversion efficiency. In particular, by combining a vertical spindle type impeller having the inclined blade tip end portion with a self-excited generator having the initial excitation mechanism, even in a conventional natural energy power generation device, the power generation efficiency is poor. It can also carry out the necessary power generation. Further, the impeller having the inclined tip end portion of the blade and the impeller having the curved blade tip end portion have an advantage that the water can be rotated even by the breeze or the low flow rate. Therefore, by combining the vertical spindle type impeller having the blade tip end portion having such a shape with the motor having the self-excited type and the initial excitation mechanism, it is possible to rotate even with water by a breeze or a low flow rate. The advantages of the impeller are effectively combined with the characteristics of a generator that can be generated by a small torque rotation, and it is possible to generate electricity in a conventional natural energy power generation device that cannot generate electricity with a slight breeze or a low flow rate of water.

Any combination of at least two configurations disclosed in the scope of the patent application and/or the specification and/or the drawings is also included in the present invention. In particular, any combination of two or more of the claims of the patent application scope is also included in the present invention.

An impeller and a natural energy power generation device according to an embodiment of the present invention will be described with reference to Figs. 1 to 5 . Fig. 1 is a cross-sectional plan view of the impeller 18 of this embodiment. Figure 2 is a front view of the impeller 18 for this purpose. This impeller 18 is a so-called linear wing vertical axis type impeller (vertical axis type impeller) in which the blades 24 are extended in the vertical direction. As shown in FIGS. 1 and 2, the natural energy power generation device 19 includes an impeller 18 and a generator 26 (described later) driven by the impeller 18. The impeller 18 has a rotor Rt as a rotating body and a fixed base Kd as a fixed body. The fixed base Kd has: a support plate 20; a frame 21; and a base 25. The support plate 20 is a flat plate body placed on the ground contact surface, and a base 25 is disposed on the top surface of the support plate body 20. Inside the base 25, a generator 26, which will be described later, is provided.

The casing 21 has a plurality of (four in this example) pillars 21a extending upward from the support plate body 20, and a plurality of connecting members 21b that connect the pillars 21a in the horizontal direction and a plurality of bridge members 21c. The plurality of connecting members 21b include a plurality of upper connecting members 21b that connect the upper end portions of the adjacent pillars 21a to each other, and a plurality of lower connecting members 21b that connect the vicinity of the lower ends of the adjacent pillars 21a to each other. A bridge member 21c is placed between the connecting member 21b defined in the connecting member 21b of the upper stage (upper side in FIG. 2) and the connecting member 21b opposed to the connecting member 21b. Further, a bridge member 21c is placed between the connecting member 21b defined in the connecting member 21b of the lower stage (lower side in FIG. 2) and the connecting member 21b opposed to the connecting member 21b.

The rotor Rt has a vertical main shaft (spindle) 22, a support 23, and a vane 24. The vertical main shaft 22 is rotatably supported by the bearings 27 and 27 in the intermediate portion in the longitudinal direction of each of the erecting members 21c and 21c. The vertical main shaft 22 extends in the up and down direction, and the lower end portion of the vertical main shaft 22 extends to the inside of the base 25. The plurality of supports 23 are provided so as to extend outward in the radial direction from the vicinity of the middle portion in the longitudinal direction of the vertical main shaft 22. The supports 23 are, for example, arranged parallel to the front view of the impeller 18 and in phase in the top view of the impeller.

Blades 24 are provided on the front end portions of both sides of the plurality of supports 23, respectively. In this example, one blade 24 is connected to one end of the upper and lower supports 23 and 23, and the other blade 24 is connected to the other end of the upper and lower supports 23 and 23. The blades 24 and 24 are disposed at a position with a phase difference of 180 degrees centering on the vertical main axis 22. Each of the vanes 24 extends in the vertical direction, and is disposed in the same casing 21 so as not to interfere with the casing 21. Each of the vanes 24 receives wind or water from all directions and rotates about the axis L1 of the vertical main shaft 22.

Fig. 3A is a front view of the blade 24 of the impeller; Fig. 3B is a sectional view taken along line IIIB-IIIB of Fig. 3A. As shown in FIGS. 3A and 3B, the blade 24 has a flat portion 28 and blade end portions 29 and 29 extending from both ends in the longitudinal direction of the straight portion 28. The straight portion 28 and the blade tip end portions 29, 29 are integrally formed of the same material. The straight portion 28 extends parallel to the vertical main axis 22 (Fig. 2) and is the same width in any of the up and down directions in the front view of Fig. 3A. Further, as shown in FIG. 3B, the straight portion 28 is formed to have the same thickness in any of the up and down directions.

Figure 4 is a cross-sectional view taken along line IV-IV of Figure 3B. As shown in FIGS. 1 and 4, the plurality of (two in this example) blades 24 are each cut transversely to a plane perpendicular to the axis L1 (FIG. 2) of the vertical main axis 22, relative to the rotation of the blades 24. The direction is asymmetrical, and the portion which becomes the thicker side of the same cross section (the upper side portion of Fig. 4) is set as the front end of each blade 24 in the rotational direction. Further, the outer surface 28a of the flat portion 28 of each blade 24 is a curved surface that protrudes outward in the radial direction; and most of the inner side surface 28b of the flat portion 28 is a flat surface 28ba.

Further, the inner side surface 28b may not have a curved surface having a larger radius of curvature than the outer side surface 28a, without setting the majority of the inner side surface 28b to the flat surface 28ba. Among the inner side faces 28b of the straight portion 28, the joint portion with one end of the outer side surface 28a in the circumferential direction (upper side in Fig. 4) is an arcuate surface 28bb. The joint portion between the circular arc surface 28bb and the flat surface 28ba is formed to be smoothly continuous without a step.

The joint portion between the inner side surface 28b of the straight portion 28 and the other end (the lower side in Fig. 4) of the outer side surface 28a in the circumferential direction is formed into a corner portion at an acute angle. The front end portion of the support body 23 is joined to a portion of the flat surface 28ba of the inner side surface 28b of the straight portion 28 near the circular arc surface 28bb. The flat surface 28ba is a plane perpendicular to the longitudinal direction of the support 23, and the vertical plane extends in the up and down direction.

As shown in Fig. 2 and Figs. 3A and 3B, the blade leading end portions 29, 29 are used to reduce so-called ailerons from the tip vortex of the tip end of each blade. The blade tip end portion 29 is formed by cutting the blade tip end portion 29 in a plane shape including the axis L1, and is formed so as to be inclined in plural as it goes closer to the vertical main axis L1 from the base end toward the tip end. The segment (in this case, the second segment) (in other words, the shape of the plurality of segments inclined away from the straight portion 28). The upper and lower blade tip end portions 29 and 29 are formed in the same shape in line symmetry with respect to the center line L2 of the intermediate portion in the longitudinal direction of the straight portion 28.

Fig. 5 is an enlarged view of the V portion of Fig. 3B, that is, the blade leading end portion 29 on the upper side. Further, as described above, since the upper and lower blade tip end portions 29 and 29 have the same shape in line symmetry, only the upper blade tip end portion 29 is attached with a reference numeral, and the lower blade tip end portion 29 is given. The blade tip end portion 29 on the upper side in Fig. 3B is denoted by the same reference numeral, and detailed description thereof will be omitted. As shown in FIG. 3B and FIG. 5, the blade leading end portion 29 has a first-stage inclined portion 29a joined to the front end in the longitudinal direction of the straight portion 28, and a second-stage inclined portion 29b which is continued from the first-stage inclined portion 29a. .

The first-stage inclined portion 29a is at an angle θ1 with respect to the straight portion 28 in the cross section, and is inclined toward the vertical main shaft side. The first inclined portion 29a is formed to have the same thickness t1 in any of the up and down directions. At the upper end of the first inclined portion 29a, the second inclined portion 29b is joined. This second-stage inclined portion 29b is at an angle θ2 with respect to the first-stage inclined portion 29a in this cross section, and is inclined toward the vertical main shaft side. The second-stage inclined portion 29b is formed in a cross-sectional shape in which the thickness t2 in the cross section becomes thinner as it goes to the upper end. Further, each of the angles θ1 and θ2 is defined as an angle formed by the center line in each width direction of the straight portion 28, the first-stage inclined portion 29a, and the second-stage inclined portion 29b defining the angle. The angles θ1 and θ2 are set to be larger than the angle θ of the joint portion 53 of the conventional example (Fig. 18B). Further, in this example, the angles θ1 and θ2 are set to be the same angle. However, the angles θ1 and θ2 are not limited to the same angle.

According to the blade 24 of the impeller 18 described above, the cross section of the spindle axis center including the blade tip end portion 29 is inclined so as to be inclined toward the vertical spindle side from the base end toward the tip end. Therefore, the wing tip vortex from the front end of the blade can be reduced. In particular, since the blade tip end portion 29 is inclined in a plurality of stages, the blade tip end can be made even if the bending angles θ1 and θ2 of the joint portions 30 and 31 of the blade tip end portion 29 are gentle as compared with the case where the blade tip end portion 29 is inclined. The portion 29 is tilted as a whole. Therefore, when the entire length of the blade is fixed, it is possible to ensure that the horizontal length Lh of the blade leading end portion 29 is below the desired length while ensuring that the length Lv of the straight portion 28 is long. As described above, in addition to the fact that the wing tip vortex from the tip end of the blade can be surely reduced, and the desired wind receiving area or water receiving area can be secured, even a small amount of breeze or a low flow rate of water can be rotated.

Thus, since the length Lv of the long straight portion 28 can be obtained, the conversion efficiency of converting the energy received by the blade 24 into the rotational energy can be improved. Further, by ensuring that the horizontal direction length Lh of the blade tip end portion 29 is a desired length, the tip vortex generated from the tip end of the blade can be surely reduced, and the bending angle of each joint portion can be reduced, so that the action on the bent portion can be reduced. Stress increases the strength of the blade 24.

Since the tip end portion 29 of the blade is formed into a tapered shape which becomes narrower toward the tip end from the base end, the tip vortex can be further reduced as compared with the case where the blade tip end is formed into a flat shape. Therefore, the conversion efficiency of converting the energy received by the blade 24 into rotational energy can be further improved.

Further, the blade tip end portion 29 of the vertical axis type impeller 18 cuts the cross section seen by the blade tip end portion 29 in a plane including the axis L1, and may be further away from the base end toward the front end. The cross-sectional shape of the plurality of segments is inclined in such a manner that the opposite side of the vertical spindle L1 side. A plurality of blades 24 may be disposed in the up and down direction with respect to a vertical main shaft 22. In this case, the wind receiving area of the blade 24 with respect to the set area of the impeller can be increased. Further, the number of blades is not limited to two for each segment, and may be three or more.

Next, a second embodiment of the present invention will be described. In the following description, the same reference numerals will be given to the parts of the above-described aspects in the respective aspects, and the overlapping description will be omitted. In the case where only the components are described, the other components of the configuration are the same as those described above unless otherwise specified. The same effect can be obtained from the same composition. It is not intended to be a combination of the specific portions described in the respective embodiments, and the embodiments may be combined with each other if the combination does not cause a problem.

Fig. 6A is a front view of the blade 24A of the impeller according to the second embodiment; Fig. 6B is a sectional view taken along line VIB-VIB of Fig. 6A. This impeller is a horizontal-axis impeller in which the straight portion 28A of the blade 24A extends outward in the radial direction with respect to the main shaft 22. That is, the main shaft 22 is disposed to be rotatable about the axis L1, and the outer circumference of the main shaft 22 is fixed at a fixed interval in the circumferential direction (for example, about 2 to 5 pieces: only one piece is shown in FIG. 6A) Blade 24A. From the front view shown in Fig. 6A, the flat portion 28A of the blade 24A is formed to gradually widen from the base end toward the front end. Others have the same configuration as the first embodiment described above. The farther the blade 24A is from the rotational axis of the main shaft 22, the greater the torque can be ensured. Further, the direction in which the blade tip end portion 29 is inclined may be set toward the proximal end side of the main shaft 22 or may be directed toward the front end side of the main shaft 22. According to this configuration, the flat portion 28A is formed such that the wider the width from the base end toward the front end, that is, the larger the area, the higher the conversion efficiency of the front end of the straight portion 28A of the torque can be further ensured. Further, since the blade tip end portion 29 is formed into a cross-sectional shape of a plurality of stages as described above, the conversion efficiency of converting the energy received by the blade 24A into the rotational energy can be improved, and the strength of the blade 24A can be improved.

An impeller and a natural energy power generation device according to a third embodiment of the present invention will be described with reference to Figs. 7 to 11 . Figure 7 is a cross-sectional plan view of the impeller 18 of this embodiment. Figure 8 is a front view of the impeller 18. In the following description, the same reference numerals will be given to the parts of the above-described aspects in the respective aspects, and the overlapping description will be omitted. In the case where only the components are described, the other components of the configuration are the same as those described above unless otherwise specified. The same effect can be obtained from the same composition. It is not intended to be a combination of the specific portions described in the respective embodiments, and the embodiments may be combined with each other if the combination does not cause a problem.

Fig. 9A is a front view of the blade 24 of the impeller; Fig. 9B is a sectional view taken along line IXB-IXB of Fig. 9A. As shown in FIGS. 9A and 9B, the blade 24 has a flat portion 28 and blade end portions 29 and 29 extending from both ends in the longitudinal direction of the straight portion 28. The straight portion 28 and the blade tip end portions 29, 29 are integrally formed of the same material. The straight portion 28 extends parallel to the vertical main shaft 22 (Fig. 8), and in the front view of Fig. 9A, is the same width in any of the up and down directions. Further, as shown in FIG. 9B, the straight portion 28 is formed to have the same thickness in any of the up and down directions.

Figure 10 is a cross-sectional view taken along line X-X of Figure 9B. As shown in FIGS. 7 and 10, the plurality of (two in this example) blades 24 are each cut in a transverse plane perpendicular to the axis L1 (FIG. 8) of the vertical main axis 22, relative to the rotation of the blades 24. The direction is asymmetrical, and the portion which becomes the thicker side of the same cross section (the upper side portion of Fig. 10) is set as the front end of each blade 24 in the rotational direction. Further, the outer side surface 28a of the straight portion 28 of each blade 24 is a curved surface which is convex outward in the radial direction, and most of the inner side surface 28b of the flat portion 28 is a flat surface 28ba.

Further, the inner side surface 28b may not be formed as a flat surface 28ba, and the inner side surface 28b may have a curved surface having a larger radius of curvature than the outer side surface 28a. Among the inner side faces 28b of the straight portion 28, the joint portion with one end of the outer side surface 28a in the circumferential direction (upper side in Fig. 10) is an arcuate surface 28bb. The joint portion between the circular arc surface 28bb and the flat surface 28ba is formed to be smoothly continuous without a step.

The joint portion between the inner side surface 28b of the straight portion 28 and the other end (the lower side in Fig. 10) of the outer side surface 28a in the circumferential direction is formed into a corner portion at an acute angle. The front end portion of the support body 23 is joined to a portion of the flat surface 28ba of the inner side surface 28b of the straight portion 28 near the circular arc surface 28bb. The flat surface 28ba is a plane perpendicular to the longitudinal direction of the support 23, and the vertical plane extends in the up and down direction.

As shown in Fig. 8 and Figs. 9A and 9B, the blade leading end portions 29 and 29 are used to reduce so-called ailerons from the tip vortex of the tip end of each blade. The shape of the cross section (spindle cross section) of the blade tip end portion 29 cut along the plane containing the axis L1 is formed so as to be closer to the vertical main axis L1 side from the base end to the front end (in other words, The shape that is curved away from the straight portion 28). The upper and lower blade tip end portions 29 and 29 are formed in the same shape in line symmetry with respect to the center line L2 of the intermediate portion in the longitudinal direction of the straight portion 28.

Fig. 11 is an enlarged view of the y portion of Fig. 9B, that is, the blade leading end portion 29 on the upper side. Further, as described above, since the upper and lower blade tip end portions 29 and 29 have the same shape in line symmetry, only the upper blade tip end portion 29 is attached with a reference numeral, and the lower blade tip end portion 29 is given. The blade tip end portion 29 on the upper side in Fig. 9B is denoted by the same reference numeral, and detailed description thereof will be omitted. As shown in FIG. 9B and FIG. 11, the blade tip end portion 29 is constituted by a curved portion 29c that is joined to the longitudinal end 32 of the straight portion 28.

This curved portion 29c is formed so as to gradually bend toward the front end toward the vertical main shaft side. The main shaft section of the curved portion 29c includes an inner surface side portion 29aa on the vertical main shaft side and an outer surface side portion 29ab on the opposite side to the inner surface side portion 29aa. The inner side portion 29aa is smoothly joined to the inner side surface 28b of the straight portion 28 without a step; the outer side portion 29ab is smoothly joined to the outer side surface 28a of the straight portion 28 without any step. The inner surface side portion 29aa and the outer surface side portion 29ab are each formed by predetermined curvature radii Ra, Rb. The center of curvature C1, C2 of the inner side portion 29aa and the outer side portion 29ab is, for example, located near the middle of the straight portion 28 and the vertical main shaft 22 (Fig. 8), and the front end 32 of the flat portion 28 in the longitudinal direction. At roughly the same height. The curvature centers C1 and C2 of the inner surface side portion 29aa and the outer surface side portion 29ab are set at different positions. Further, the curved portion 29c is formed in a cross-sectional shape in which the thickness t1 of the main shaft section becomes thinner as it goes to the upper end. Further, the curvature radii Ra and Rb are appropriately set, for example, by a result such as an experiment or a simulation.

According to the blade 24 of the impeller 18 described above, since the main shaft section of the blade tip end portion 29 is formed to have a cross-sectional shape closer to the vertical main shaft side from the base end to the front end, the wing tip vortex from the blade tip end can be reduced. Spin. In particular, the shape in which the blade tip end portion 29 is closer to the vertical main axis side toward the front end is curved, so that a partial sharp bending portion is not generated at the blade leading end portion 29 as compared with the case where the blade tip end portion 29 is inclined. Further, the entire blade tip end portion 29 can be largely inclined. Therefore, when the entire length of the blade is fixed, it is possible to ensure that the horizontal length Lh of the blade leading end portion 29 is below the desired length while ensuring that the length Lv of the straight portion 28 is long. As described above, in addition to the fact that the wing tip vortex from the tip end of the blade can be surely reduced, and the desired wind receiving area or water receiving area can be secured, even a small amount of breeze or a low flow rate of water can be rotated.

Thus, since the length Lv of the long straight portion 28 can be obtained, the conversion efficiency of converting the energy received by the blade 24 into the rotational energy can be improved. Further, by ensuring that the horizontal length Lh of the blade tip end portion 29 is a desired length, the wing tip vortex generated from the tip end of the blade can be surely reduced, and the local bending angle of the blade tip end portion 29 can be alleviated, so that the blade can be dispersed The stress of the curved portion of the front end portion 29 can increase the strength of the blade 24.

Since the blade tip end portion 29 is formed into a tapered shape that becomes narrower from the base end toward the tip end, the blade tip vortex can be further reduced as compared with the case where the blade tip end is formed into a flat shape. Therefore, the conversion efficiency of converting the energy received by the blade 24 into rotational energy can be further improved.

Further, the inner surface side portion 29aa and the outer surface side portion 29ab of the curved portion 29c may be formed by the same radius of curvature, and the thickness t1 of the main shaft section of the curved portion 29c may be set to any position in the up and down direction. All are the same wall thickness. The inner surface side portion 29aa and the outer surface side portion 29ab of the curved portion 29c may be formed by a predetermined radius of curvature from the base end to a certain fixed position, and a quadratic curve from the fixed position to the front end. A parabolic curve is formed. The relationship between this radius of curvature and the parabolic curve can also be reversed. Other curvature radius and parabolic curve can also be combined.

Hereinafter, a fourth embodiment of the present invention will be described. In the following description, the same reference numerals will be given to the parts of the above-described aspects in the respective aspects, and the overlapping description will be omitted. In the case where only the components are described, the other components of the configuration are the same as those described above unless otherwise specified. The same effect can be obtained from the same composition. It is not intended to be a combination of the specific portions described in the respective embodiments, and the embodiments may be combined with each other if the combination does not cause a problem.

Fig. 12A is a front view of the blade 24A of the impeller according to the fourth embodiment; Fig. 12B is a sectional view taken along line XIIB-XIIB of Fig. 12A. This impeller is a horizontal axis type in which the straight portion 28A of the blade 24A extends outward in the radial direction with respect to the main shaft 22. That is, the main shaft 22 is rotatable about the axis L1, and the outer circumference of the main shaft 22 is fixed at a fixed interval in the circumferential direction (for example, about 2 to 5 pieces: only one piece is shown in FIG. 12A). . In the front view of Fig. 12A, the flat portion 28A of the blade 24A is formed to be wider as it goes from the base end to the front end. The configuration is the same as that of the other embodiments described above. The farther the blade 24A is from the rotational axis of the main shaft 22, the greater the torque can be ensured. Further, the direction in which the blade tip end portion 29 is inclined may be set toward the proximal end side of the main shaft 22 or may be directed toward the front end side of the main shaft 22. According to this configuration, the flat portion 28A is formed such that the wider the width from the base end toward the front end, that is, the larger the area, the higher the conversion efficiency of the front end of the straight portion 28A of the torque can be further ensured. Further, since the cross-sectional shape of the blade tip end portion 29 is closer to the vertical spindle side as it goes from the base end to the tip end, the conversion efficiency of converting the energy received by the blade 24A into the rotational energy can be improved, and Increase the strength of the blade 24A.

An impeller (that is, a wind turbine for wind power generation) according to a fifth embodiment of the present invention and a natural energy power generation device (that is, a wind power generator) will be described with reference to FIG. 13 and FIG. Fig. 13 is a cross-sectional plan view showing an impeller (windmill) 18 for wind power generation of the embodiment. This windmill 18 is a so-called linear wing vertical axis type windmill in which the blades 24 are extended in the vertical direction. This windmill 18 is placed in the northern hemisphere. In the following description, the same reference numerals will be given to the parts of the above-described aspects in the respective aspects, and the overlapping description will be omitted. In the case where only the components are described, the other components of the configuration are the same as those described above unless otherwise specified. The same effect can be obtained from the same composition. It is not intended to be a combination of the specific portions described in the respective embodiments, and the embodiments may be combined with each other if the combination does not cause a problem.

Further, the shape of the blade 24 of the impeller (windmill) 18 of the present embodiment may be any one of the blade of the vertical axis type impeller 18 (that is, the impeller 18 of the first embodiment and the impeller 18 of the third embodiment). In the following description, the blade 24 of the third embodiment in which the front end portion 29 of the blade 24 is formed in a curved shape will be described as a representative example.

Fig. 14 is a cross-sectional view showing a cross section of the blade 24 of the embodiment shown in Fig. 13 at the same position as the cross section shown in Fig. 10 of the third embodiment. As shown in FIGS. 13 and 14, the cross section of the plurality of blades (two in this example) is formed so as to be independent of the wind direction and define the direction of rotation as a specific direction (counterclockwise rotation as indicated by an arrow R1 in FIG. 13). The shape. That is, each of the plurality of blades 24 cuts a cross section as seen in a plane perpendicular to the axis L1 of the vertical main axis 22, is asymmetrical with respect to the direction of rotation of the blade 24, and will be a portion of the thicker side of the same section. (the lower side portion in Fig. 14) is the front end of each blade 24 in the rotational direction. Further, the outer side surface 28a of the flat portion 28 of each blade 24 is a curved surface which is convex outward in the radial direction; and most of the inner side surface 28b of the flat portion 28 of each blade 24 is set as a flat surface 28ba. .

Further, in addition to the fact that most of the inner side surface 28b is the flat surface 28ba, the inner side surface 28b may have a curved surface having a larger radius of curvature than the outer side surface 28a. In the inner side surface 28b of the straight portion 28, the joint portion with one end of the outer side surface 28a in the circumferential direction (the lower side in Fig. 14) is an arcuate surface 28bb. The joint portion between the circular arc surface 28bb and the flat surface 28ba is formed to be smoothly continuous without a step.

The joint portion between the inner side surface 28b of the straight portion 28 and the other end (the upper side in Fig. 14) of the outer side surface 28a in the circumferential direction is formed into a corner portion at an acute angle. The front end portion of the support body 23 is joined to a portion of the flat surface 28ba of the inner side surface 28b of the straight portion 28 near the circular arc surface 28bb. The flat surface 28ba is a plane perpendicular to the longitudinal direction of the support 23, and the vertical plane extends in the up and down direction.

When the blade 24 is subjected to wind, the flow velocity along the outer side surface 28a is faster than the flow velocity along the inner side surface 28b, and the pressure distribution around the blade increases the negative pressure of the outer side surface 28a. Therefore, the blade as a whole generates the lift force L from the inner side surface side to the outer side surface side. As shown in Fig. 14, here, the lift generated in the blade by the relative wind speed v generated by the rotation of the blade 24 and the combined wind speed w of the wind speed u is set to L. As a result, the combined component (Lt-Dt) of the lift L and the direction of the resistance D in the t direction becomes the force of the rotation direction of the blade 24.

When the windmill 18 having the plurality of blades 24 that rotates in a counterclockwise direction regardless of the wind direction is installed in the northern hemisphere, the wind turbine for vertical axis wind power generation having a conventional clockwise rotation blade can be effectively utilized. The Coriolis force generated by the Earth's rotation reduces the rotational impedance and rotates the majority of the blades 24 under the same conditions. Therefore, by using the wind turbine 18 for power generation having the vertical main shaft 22, power generation can be performed with less wind energy. Since the windmill 18 is a linear-axis vertical axis type windmill, the ratio of the lift force to the resistance acting on the blade 24 can be increased. In addition, a large torque can be obtained at a high peripheral speed ratio.

Next, the generator 26 will be collectively explained using Figs. 15 to 17 . Inside the base 25 (FIG. 2), a generator 26 that generates electric power by rotating the rotor 5, which will be described later, by the rotation of the vertical main shaft 22 (FIG. 2) is provided. Fig. 15 is a cross-sectional front view and a combined explanatory view of a circuit diagram of the generator body 1 of the generator 26. In Fig. 15, the generator body 1 of the generator 26 has an annular stator 4, and a rotor 5 which is rotatably provided inside the stator 4 around the center of the stator 4. For example, the rotor 5 is coupled coaxially with the aforementioned vertical main shaft (Fig. 2). The stator 4 has an output core 6 and an output winding 7. In this embodiment, in the case of a two-pole generator, the output core 6 is formed at two places in the circumferential direction of the annular yoke portion 6A, and a toothed magnetic pole portion 6b that protrudes inward is formed. The output winding 7 is wound around each of the magnetic pole portions 6b.

As shown in Fig. 16, the output windings 7 of the respective magnetic pole portions 6b are connected in series so that the magnetic pole faces of the adjacent magnetic pole portions 6b of the output iron core 6 are opposite to each other on the magnetic pole faces. Both ends of the output winding 7 serve as terminals 7a and 7b. As shown in Fig. 15, the external load 3 is connected to the terminals 7a and 7b, and the current is taken out from the generator to the outside.

As shown in FIGS. 15 and 16, the rotor 5 includes a magnetic field core 8 and a main field winding 9 and a sub-field winding 10 wound around the magnetic field core 8. The magnetic field core 8 is provided on the outer circumference of the core body 8a having the center hole, and a plurality of tooth-shaped magnetic pole portions 8b projecting toward the outer diameter side are arranged side by side in the circumferential direction. Three magnetic pole portions 8b are provided for each of the magnetic pole portions 6b of the output iron core 6.

The main magnetic field winding 9 is wound across the adjacent two magnetic pole portions 8b, 8b, which spans the main magnetic field windings 9 wound around the two magnetic pole portions 8b, 8b, for two groups of adjacent magnetic pole groups. The magnetic pole faces of each other are connected in series in a manner different from each other. The sub-field winding 10 and the field winding 9 are displaced by only one phase of the magnetic pole portion 8b, and are wound around the adjacent two magnetic pole portions 8b and 8b in the same manner as the main magnetic field winding 9. The sub-field windings 10 wound around the two magnetic pole portions 8b and 8b are connected in series so that the magnetic pole faces of the two adjacent magnetic pole groups are different from each other. The terminals at both ends of each of the series connection bodies of the main field winding 9 and the sub field winding 10 are shown in Fig. 16 by reference numerals 9a, 9b, 10a, and 10b, respectively.

As shown in FIG. 17, a rectifying element (rectifying means) 11 is connected in parallel to the main field winding 9 to flow a current in a direction in which the rectifying element 11 can flow in the main field winding 9. The secondary magnetic field winding 10 is connected in series with the main magnetic field winding 9, and a rectifying element (rectifying means) 12 is connected in series, and only the current in the same direction as the main magnetic field winding 9 flows through the sub magnetic field winding 10. The arrows in the figure indicate the direction in which current flows.

In the self-excited generator including the sub-field winding 10, the generator 26 has an initial excitation mechanism 2 that generates a magnetic force required for the initial stage of power generation. As shown in FIG. 15, in the output winding 7, the magnetizing power source 14 is connected in parallel to the external load 3 via the switching mechanism 13. The magnetization power source 14 and the switching mechanism 13 constitute the initial excitation mechanism 2. The switching mechanism 13 uses a semiconductor switching element or a switch having a contact. The magnetizing power source 14 is a power storage mechanism such as a secondary battery or a capacitor. When the external load 3 is a secondary battery, it can also be used as a power source for magnetization.

In order to perform magnetization, it is only necessary to cause a current of a predetermined magnitude to flow in a very short time. The degree of magnetization may be set to the extent of the current and the start-up time of the switching mechanism 13 as long as the degree of remanence required for the initial excitation to start power generation is obtained. The switching operation of the switching mechanism 13 is performed by the switch control mechanism 15. The switch control mechanism 15, for example, monitors the detection signal of the rotation detecting mechanism 16 for detecting the rotation of the rotor 5, and detects that the switching mechanism 13 only starts the set time required for magnetization when the rotor 5 is rotated from the stationary state. .

Further, when the stop time of the rotation of the rotor 5 is short, since the residual magnetization is sufficiently left, the switch control mechanism 15 can also activate the switch mechanism 13 in accordance with the set condition (for example, the rotor 5 is stopped only for the set time or longer. When the rotation starts later, the switching mechanism 13 is activated to perform control. Further, the magnetization may be performed only when the power generation is not started even if the number of rotations is not established, and the magnetization may be performed when the generator rotation is stopped every predetermined time.

In this embodiment, the output winding 7 is connected to the magnetizing power source 14. However, as shown in FIG. 17, the field windings 9 and 10 may be connected to the magnetizing power source 14 via the switching mechanism 13. In this case, the magnetizing power source 14 may be a secondary battery or a capacitor. In order to perform magnetization, it is only necessary to cause a current of a predetermined magnitude to flow in a very short time. As in the embodiment of Fig. 15, the switching mechanism 13 is switched and controlled by the switch control unit 15.

Hereinafter, an operation when the rotor 5 rotates to generate electricity will be described. As shown in Fig. 17, the rectifying element 11 is connected in parallel to the main field winding 9, so that the main field winding 9 flows a current in a direction through which the rectifying element 11 can flow. Therefore, a magnetic flux is generated in a direction determined by the current that can flow through the main field winding 9. Further, by electromagnetic induction, a current is prevented from flowing in a direction in which the magnetic flux in the same direction as the magnetic flux generating current is reduced, and no current flows in a direction in which the magnetic flux is prevented from increasing. Therefore, the reduction of the magnetic flux can be prevented, but the increase of the magnetic flux is not prevented. In the secondary field winding 10, the rectifying element 12 is connected in series, and only the current in the same direction as the main field winding 9 flows.

As shown in FIGS. 15 to 17, current is caused to flow through the main field winding 9 by the residual magnetism of the output core 6 or the magnetic field core 8. With this current, the magnetic flux generated by the main field winding 9 is caused to change the magnetic flux which is interlinked to the sub-field winding 10, and the secondary field winding 10 generates a voltage. With this voltage, the secondary field winding 10 supplies current through the main field winding 9 so that the current flowing through the main field winding 9 increases. When the secondary field winding 10 does not induce a voltage and does not supply a current, the return current flows to the main field winding 9 via the commutator 11 to maintain the magnetic flux of the main field winding 9.

When a current is supplied to the main field winding 9, the magnetic flux generated by the main field winding 9 becomes large, so that the magnetic flux which is interlinked to the sub-field winding 10 also becomes large, and a larger current is supplied to the main field winding 9. Thus, the current of the main field winding 9 is gradually increased to generate the magnetic flux required for power generation. With the relative movement of the output core 6 and the magnetic field core 8, the flux linkage of the output winding 7 changes to generate a voltage.

As described above, power generation is performed while the rotor 5 is rotating. However, if the rotor 5 is stopped for a certain period of time, the output core 6 and the magnetic field core 8 are not remanent, or the residual magnetization is insufficient, and power generation cannot be started. Therefore, in this embodiment, when the rotation of the rotor 5 is started, the switching mechanism 13 of the initial excitation mechanism 2 is activated, and the magnetization current is supplied from the magnetization power supply 14 to the output winding 7, and the output core 6 is magnetized. As described above, since the magnetic flux gradually increases as the rotation continues, the degree of magnetization can be obtained as long as the remanence required for the initial excitation for starting the power generation can be obtained. Therefore, the magnetization only needs to flow a current of a predetermined magnitude in a very short time. By this magnetization, even after the rotor 5 is stopped for a long time, it is possible to surely start power generation by re-rotation.

In the case of the embodiment in which the switch mechanism 13 is provided, the switching mechanism 13 of the initial excitation mechanism 2 is activated when the rotation of the rotor 5 is stopped, and the magnetizing current flows from the magnetizing power source 14 to the main field winding 8 to make the magnetic field. The core 8 is magnetized. When the magnetic field core 8 is magnetized in this manner, power generation can be started even after the rotor 5 is stopped for a long time.

According to the generator 26 of the present embodiment, the following advantages can be obtained. Since the generator 26 is a self-excited generator, it does not need to be powered by him, so the configuration is simple, and there is no need to apply a permanent magnet to the magnetic field, and the torque is not a problem. Since the torque is small, the torque can be started with a small torque. A magnetic field is required to start the operation. If there is residual magnetic flux, it can start to operate. However, due to long-term placement or maintenance, the residual magnetic flux may disappear. If the residual magnetic flux disappears, the operation cannot be started. However, since the initial excitation mechanism 2 is provided, it is possible to surely start the operation. Since the magnetic flux that becomes the magnetic field increases with the rotation, the magnetic flux required for the initial excitation is only a small amount, and the influence on the torque is small, and the rotation can be started with a small torque to generate electricity.

As described above, the self-excited generator 26 provided with the initial excitation mechanism 2 has an advantage that it can be rotated with a small amount of torque and can reliably generate power. On the other hand, the impeller 18 having the inclined blade leading end portion 29 can improve the conversion efficiency. In particular, by combining the vertical spindle type impeller 18 having the inclined blade tip end portion 29 with the self-excited generator 26 provided with the initial excitation mechanism 2, even in a conventional natural energy power generation device In an environment with poor efficiency, sufficient power generation can be performed as needed. Further, the impeller 18 having the inclined blade tip end portion 29 and the impeller 18 having the curved blade tip end portion 29 have an advantage that the water can be rotated even by the breeze or the low flow rate. Therefore, by combining the vertical spindle type impeller 18 having the blade tip end portion 29 having such a shape with the self-excited motor 26 provided with the initial excitation mechanism 2, it is possible to use water even by a breeze or a low flow rate. The advantage of the rotatable impeller 18 is that it can be effectively combined with the characteristics of the generator 26 that can be rotated with a small amount of torque to generate power, which makes it possible to generate electricity in a conventional natural energy power generation device with a little breeze or a low flow rate of water.

Although it is a self-excited generator, it is provided with an initial excitation mechanism 2 that can magnetize any of the cores of the generator during the initial stage of power generation, so even after the rotation is stopped, after disassembly and maintenance, or at a low speed. It is also possible to start generating electricity. Although the initial excitation mechanism 2 is required, the initial excitation mechanism 2 can be magnetized so as to generate magnetic force required for excitation at the initial stage of power generation, and therefore can be relatively small compared to the external power supply of the other generator. Achieved.

Further, in the above-described embodiment, the stator core 4 side is the output iron core 6, and the rotor 5 side is the magnetic field iron core 8, but the stator 4 side may be the magnetic field iron core 9, 10 instead. The rotor 5 side is set as the output core 6. Further, in the above embodiment, the two-pole generator is used, but a multi-pole generator such as four poles, eight poles, or six poles may be used. Moreover, the generator is not limited to a self-excited generator, but may be a generator or other various forms of generators.

The generator 26 can also use a synchronous generator that generates a magnetic field with a permanent magnet. A plurality of generators 26 may be provided for one vertical main shaft 22, and each of the generators 26 may be individually powered by the rotation of the one vertical main shaft 22.

The embodiments of the present invention have been described above based on the embodiments, but the embodiments disclosed herein are illustrative in all aspects and are not intended to be limiting. The scope of the present invention is defined by the scope of the claims and the scope of the claims and the scope of the claims.

2‧‧‧Initial excitation mechanism
3‧‧‧External load
4‧‧‧ Stator
5‧‧‧Rotor
6‧‧‧Output core
6a‧‧‧ yoke
6b‧‧‧Magnetic pole
7‧‧‧Output winding
7a, 7b‧‧‧ terminals
8‧‧‧ magnetic field core
8a‧‧‧core body
8b‧‧‧Magnetic pole
9‧‧‧Main field winding
9a, 9b‧‧‧ terminals
10‧‧‧Sub-field winding
10a, 10b‧‧‧ terminals
11, 12‧‧‧Rectifying components (rectifying mechanism)
13‧‧‧Switching mechanism
14‧‧‧Power supply for magnetization
15‧‧‧Switch control mechanism
16‧‧‧Rotating inspection agency
18‧‧‧ Impeller
19‧‧‧Natural energy power generation unit
20‧‧‧Support plate
21‧‧‧ frame
21a‧‧‧ pillar
21b‧‧‧Connected components
21c‧‧‧ erecting components
22‧‧‧Vertical spindle (spindle)
23‧‧‧Support
24, 24A‧‧‧ leaves
25‧‧‧Abutment
26‧‧‧Generator
27‧‧‧ bearing
28, 28A‧‧‧ Straight Department
28a‧‧‧Outside
28b‧‧‧ inside side
28ba‧‧‧flat surface
28bb‧‧‧ arc surface
29‧‧‧Front end of the blade
29a‧‧‧The first section of the slope
29b‧‧‧The second section of the slope
29c‧‧‧Bend section
29aa‧‧‧ inside side part
29ab‧‧‧Outside part
30, 31‧‧‧ joints
32‧‧‧Long-side direction front end
50‧‧‧ leaves
51‧‧‧ Straight
52‧‧‧Aileron
53‧‧‧ joints
C1, C2‧‧‧ Curvature Center
D‧‧‧ resistance
Resistance in the direction of Dt‧‧‧t
Kd‧‧‧ fixed abutment
L‧‧‧ Lift
Lift in the direction of Lt‧‧‧t
L1‧‧‧ Axis
L2‧‧‧ center line
La, Lv‧‧‧ length
Lh‧‧‧ horizontal length
R1‧‧‧ arrow
Radius of Ra, Rb‧‧‧
Rt‧‧‧ rotor
T‧‧‧direction
T1, t2‧‧‧ thickness
u‧‧‧Wind speed
V‧‧‧relative wind speed
w‧‧‧Combined wind speed θ, θ1, θ2‧‧‧ angle

The invention will be better understood from the following description of the preferred embodiments of the appended drawings. However, the embodiments and the drawings are intended to be illustrative only and not to limit the scope of the invention. The scope of the invention is defined by the scope of the appended claims. In the figures, the same reference numerals in the plural figures are the same or equivalent parts. Fig. 1 is a cross-sectional plan view of an impeller according to a first embodiment of the present invention. [Fig. 2] Front view of the same impeller. [Fig. 3A] Front view of the blade of the same impeller. Fig. 3B is a cross-sectional view taken along line IIIB-IIIB of Fig. 3A. Fig. 4 is a sectional view taken along line IV-IV of Fig. 3B. Fig. 5 is an enlarged view of a portion V of Fig. 3B. Fig. 6A is a front view of a blade of an impeller according to a second embodiment of the present invention. Fig. 6B is a cross-sectional view taken along line VIB-VIB of Fig. 6A. Fig. 7 is a cross-sectional plan view showing an impeller according to a third embodiment of the present invention. [Fig. 8] A front view of the same impeller. [Fig. 9A] Front view of the blade of the same impeller. Fig. 9B is a cross-sectional view taken along line IXB-IXB of Fig. 9A. Fig. 10 is a sectional view taken along line X-X of Fig. 9B. Fig. 11 is an enlarged view of a portion XI of Fig. 9B. Fig. 12A is a front view of a blade of an impeller according to a fourth embodiment of the present invention. Fig. 12B is a cross-sectional view taken along line XIIB-XIIB of Fig. 12A. Fig. 13 is a cross-sectional plan view showing a wind turbine for wind power generation according to an embodiment of the present invention. Fig. 14 is a cross-sectional view showing a cross section of the blade shown in Fig. 13 at the same position as the cross section shown in Fig. 10. Fig. 15 is an explanatory view showing a cross-sectional front view of a generator body of a generator according to an embodiment of the present invention in combination with a circuit diagram. Fig. 16 is an explanatory view showing a linear shape of the generator body. Fig. 17 is a circuit diagram showing the configuration of an electric circuit of the generator body. Fig. 18A is a front view of a blade of an impeller of a conventional example. Fig. 18B is a cross-sectional view taken along line XVIIIB-XVIIIB of Fig. 18A.

24‧‧‧ leaves

28‧‧‧ Straight

29‧‧‧Front end of the blade

29a‧‧‧The first section of the slope

29b‧‧‧The second section of the slope

30, 31‧‧‧ joints

L2‧‧‧ center line

Lh‧‧‧ length

Θ1, θ2‧‧‧ angle

Claims (7)

An impeller having a main shaft disposed to rotate freely about an axis; and a vane fixed to the main shaft and rotating around the shaft by wind or hydraulic driving, characterized in that: the blade has: a flat portion And extending in a direction parallel or perpendicular to the main axis; and a tip end portion of the blade extending from an end portion of the straight portion, and cutting a tip end portion of the blade into a plane shape including a plane of the spindle axis, The front end portion of the blade is inclined in a plurality of shapes so as to be away from the straight portion from the base end toward the front end, or the front end portion of the blade is farther away from the straight portion from the base end toward the front end. The shape of the part is curved. The impeller according to claim 1, wherein the straight portion of the blade extends in parallel with respect to the main shaft, and the blade is coupled to the main shaft by the support at a position away from the main shaft in a radial direction. The impeller according to claim 2, wherein the impeller is a wind turbine for wind power generation, and the plurality of blades extending in the vertical direction are disposed away from the vertical main axis and are disposed around the vertical main shaft, and the wind turbine is disposed on the wind turbine. In the case of the northern hemisphere of the earth, the cross-sectional shape of each of the blades is a shape in which the wind generates a rotational force that rotates counterclockwise in a plan view. The impeller according to claim 1, wherein the straight portion of the blade extends outward in a radial direction with respect to the main shaft. The impeller according to any one of claims 1 to 4, wherein the tip end portion of the blade is formed in a tapered shape in which the twist is narrowed from the base end to the front end. A natural energy power generation device comprising: the impeller according to any one of claims 1 to 5; and a generator driven by the impeller. The natural energy power generation device of claim 6, wherein the generator is a self-excited generator, comprising: an output core wound around an output winding; and a magnetic field core wound with a main magnetic field winding and a pair a field winding, one of the output core and the magnetic field core is a stator, and the other is a rotor, wherein the field windings are connected to a rectifying mechanism, and the stator is rotated relative to the rotor to generate electric power. The generator further includes: an initial excitation mechanism that generates a magnetic force required for the initial excitation of the power generation.