WO2012073321A1 - Vertical shaft windmill - Google Patents

Vertical shaft windmill Download PDF

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Publication number
WO2012073321A1
WO2012073321A1 PCT/JP2010/071336 JP2010071336W WO2012073321A1 WO 2012073321 A1 WO2012073321 A1 WO 2012073321A1 JP 2010071336 W JP2010071336 W JP 2010071336W WO 2012073321 A1 WO2012073321 A1 WO 2012073321A1
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WO
WIPO (PCT)
Prior art keywords
blade
rotating shaft
wing
cylindrical rotating
vertical axis
Prior art date
Application number
PCT/JP2010/071336
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French (fr)
Japanese (ja)
Inventor
健 杉崎
Original Assignee
株式会社Cno
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Priority to JP2012546603A priority Critical patent/JPWO2012073321A1/en
Priority to PCT/JP2010/071336 priority patent/WO2012073321A1/en
Publication of WO2012073321A1 publication Critical patent/WO2012073321A1/en

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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D3/00Wind motors with rotation axis substantially perpendicular to the air flow entering the rotor 
    • F03D3/06Rotors
    • F03D3/062Rotors characterised by their construction elements
    • F03D3/064Fixing wind engaging parts to rest of rotor
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/70Wind energy
    • Y02E10/74Wind turbines with rotation axis perpendicular to the wind direction

Definitions

  • the present invention relates to a vertical axis type windmill used for wind power generation and the like.
  • a horizontal axis type windmill having a horizontal rotation axis and a vertical axis type windmill having a vertical rotation axis are known.
  • the vertical axis type wind turbine has an advantage that it can be used as a rotational drive source for wind from either direction of 360 degrees and can be arranged in a compact space.
  • Patent Document 1 discloses a technique for improving the aerodynamic characteristics of a blade by adjusting the blade thickness of a vertical axis wind turbine to improve the rotation efficiency.
  • an object of the present invention is to propose a vertical axis type windmill that can be efficiently rotated even in a low wind speed region.
  • the present invention is a vertical axis wind turbine comprising a cylindrical rotating shaft and a plurality of blades supported by a blade rotating arm on the cylindrical rotating shaft.
  • a vertical axis wind turbine is proposed in which the interval between the cylindrical rotating shafts is substantially the same as the diameter of the cylindrical rotating shaft.
  • the blade since the force (inductive drag) that drags the blade toward the trailing edge is weakened and the ratio of lift to the drag is increased, the blade can be efficiently rotated even in the low wind speed region.
  • the front view which shows an example of the shape of the vertical axis type windmill of Embodiment 1. 1 is a side view showing an example of the structure of a vertical axis wind turbine according to a first embodiment.
  • the figure which shows the mode of the induction drag which acts on the blade of the conventional vertical axis type windmill The figure which shows the mode of the induced drag which acts on the blade
  • the front view which shows an example of the shape of the vertical axis type windmill of Embodiment 2.
  • the side view which shows an example of the structure of the vertical axis type windmill of Embodiment 2.
  • the side view which shows an example of the structure of the vertical axis type windmill of Embodiment 3.
  • the vertical axis wind turbine according to the present embodiment is characterized in that the distance between the blade and the cylindrical rotating shaft is equal to or less than the length of the blade in the vertical direction.
  • ⁇ Configuration> 1 and 2 are a plan view and a front view showing an example of the shape of the vertical axis wind turbine according to the present embodiment.
  • the “vertical shaft type windmill” of the present embodiment is supported by the “cylindrical rotating shaft” 1 and the “cylindrical rotating shaft” by the “wing support arm” 2.
  • wing support arm 2.
  • the “cylindrical rotating shaft” 1 has a function as a rotating shaft of the wing and a function of receiving air blowing from the horizontal direction on its side surface to form an airflow around the shaft. Furthermore, it plays a role as a surface facing the “lower surface of the blade” 31 and has a function of increasing the pressure of the airflow between the blade and the cylindrical rotating shaft.
  • the diameter of the cylindrical rotating shaft is substantially the same as the “chord chord length” 32 in order to sufficiently fulfill the role of the surface facing the cylindrical rotating shaft. If the diameter of the cylindrical rotating shaft is made smaller than the chord length, the function as the surface facing the lower surface of the wing will be reduced, and if it is made too large, the size and weight of the cylindrical rotating shaft will become larger than necessary. turn into. In the present specification, “substantially the same” means that the difference between the values of one and the other is within ⁇ 20% of the magnitude of the smaller one or the other.
  • the vertical length of the cylindrical rotating shaft and the vertical length of the blade are substantially the same in order for the cylindrical rotating shaft to sufficiently fulfill the role of the surface facing the lower surface of the blade.
  • the vertical length of the cylindrical rotating shaft is shortened compared to the vertical length of the wing, the function as the facing surface is reduced, and the vertical length of the cylindrical rotating shaft is reduced to the vertical length of the wing. If it is longer than that, the size and weight of the cylindrical rotating shaft will be larger than necessary.
  • the “cylindrical rotating shaft” includes a “post member” 11, a “connecting member” 12 that connects the post member and the wing support arm member, and a “cylindrical cover” for covering the post member and the like.
  • the structure which consists of "member” 13 etc. can be considered.
  • the cylindrical cover member is provided with an “arm extraction hole” 14 through which the member of the wing support arm passes.
  • high strength materials such as stainless steel and carbon fiber are used for the strut members
  • durable and lightweight materials such as metal such as aluminum, carbon fiber, and plastic resin are used for the connecting member and the cylindrical cover member.
  • metal such as aluminum, carbon fiber, and plastic resin
  • the “wing support arm” 2 has a function of connecting the blade and the cylindrical rotating shaft and transmitting the rotational force of the blade to the cylindrical rotating shaft.
  • the “wing support arm” includes two “arm members” 21 ⁇ / b> A and 21 ⁇ / b> B connected to a cylindrical rotating shaft, and a pair of “arm cover members” covering the arm members.
  • a configuration including 22A, 22B, and the like is conceivable.
  • a highly durable and lightweight material such as aluminum or carbon fiber for the arm member.
  • a lightweight plastic material that is easy to process, such as acrylic resin or ABS resin.
  • the “interval between the blade and the cylindrical rotating shaft” 41 is “the length of the blade in the vertical direction” 33 or less, as described below, the force (inductive drag) that drags the blade toward the trailing edge is reduced. It becomes possible.
  • FIG. 5 is a diagram showing a state of induced drag acting on the blades in a conventional general vertical axis type wind turbine.
  • the “interval between the blade and the rotary shaft” 40 is made relatively large, and the diameter of the rotary shaft is made as small as the strength allows.
  • the pressure at the distance between the blade and the rotating shaft is slightly higher than the upper surface of the blade, but not so high.
  • the “inclination of airflow (down angle)” 26 increases from the upper surface side to the lower surface side of the blade at the trailing edge of the blade.
  • a relatively large “induced drag” 27 is generated on the wing.
  • FIG. 6 is a diagram showing a state of induced drag acting on the wing when the distance between the wing and the cylindrical rotating shaft is equal to or less than the vertical length of the wing.
  • the “interval between the blade and the cylindrical rotating shaft” 41 is equal to or less than the length in the vertical direction, the pressure at the interval between the blade and the cylindrical rotating shaft is higher than that of the conventional vertical axis type wind turbine. Therefore, the “airflow inclination (down angle)” 26 from the upper surface side to the lower surface side of the blade at the trailing edge of the blade is relatively small. Since the induced drag acting on the wing becomes weaker as the blow-down angle is smaller, the “induced drag” 27 acting on the wing decreases as the blow-down angle decreases. That is, it is possible to reduce the induced drag acting on the blade by making the rotation shaft cylindrical and setting the distance between the blade and the cylindrical rotation shaft to be equal to or less than the vertical length of the blade.
  • the distance between the blade and the cylindrical rotating shaft is not more than half the vertical length of the blade, it is preferable in that the induced drag acting on the blade is particularly reduced. However, if the distance between the blade and the cylindrical rotating shaft is too narrow, the rotational torque will be reduced. Therefore, the distance between the blade and the cylindrical rotating shaft is about 25 to 35% of the vertical length of the blade. It is preferable.
  • the “average horizontal width of the wing support arm” 42 is preferably 30% or more of the diameter of the cylindrical rotating shaft from the viewpoint of rectifying the air flowing on the side surface of the wing support arm in the horizontal direction. From the viewpoint of lightness, the blade support arm is preferably less than 50% of the diameter of the cylindrical rotating shaft. Further, by making the arm cover member a curved surface as shown in FIGS. 2 and 3, the flow of the airflow can be made smooth.
  • FIGS. 2 and 3 show the configuration in which the wing is supported by the wing support arm at one central position in the vertical direction.
  • the wing support arm may be configured to support the wing at two upper and lower positions.
  • the support is provided at more points.
  • Various support points are also conceivable.
  • “Wings” 3 has a function of generating torque in the rotational direction by lift.
  • a lightweight and high-strength material such as fiber reinforced plastic or carbon fiber for the wing.
  • blade is supported at equal intervals in a rotation direction from a viewpoint of generating a torque equally irrespective of the direction where the wind of a horizontal direction blows.
  • the “wing upper surface” 30 is gently curved from the leading edge to the trailing edge, and the “wing lower surface” 31 is planar from the leading edge to the trailing edge.
  • the leading edge portion of the wing has a rounded shape, and the trailing edge portion has a sharp shape.
  • FIG. 7 is a diagram showing the force acting on the wing when a horizontal wind blows.
  • the “wing” 3 generates “lift” 52 by receiving “wind from the horizontal direction” 51.
  • the lift acts in a direction perpendicular to “drag” 53 acting on the wing, and has a component of “rotation direction” 54.
  • the blade rotates using the component in the rotation direction as a drive source.
  • the “force for dragging the blade toward the trailing edge (inductive drag)” 27 is reduced by setting the distance between the blade and the cylindrical rotating shaft to be equal to or less than the vertical length of the blade as described above. For this reason, in the vertical axis type windmill of this embodiment, the ratio of the lift to the drag is increased, and a larger rotational force can be obtained.
  • the vertical axis wind turbine supports the wings at two upper and lower positions so that the rectification surrounded by the wing support arms, the cylindrical rotating shaft, and the wings A window is formed. Since the air that has entered the inside of the wing's circumferential trajectory is compressed by the rectifying window, the induced drag acting on the wing is further reduced, and the ratio of lift to drag is increased. It becomes possible to do.
  • FIG. 8 is a front view showing an example of the shape of the vertical axis wind turbine of the present embodiment.
  • the basic configuration is the same as that of the first embodiment, but the vertical axis type wind turbine of the present embodiment supports the “wings” 3 by the “wing support arms” 2A and 2B at two upper and lower positions.
  • a “rectifying window” 4 surrounded by the “wing support arms” 2A and 2B, the “cylindrical rotating shaft” 1 and the “wing” 3 is formed.
  • the “rectifying window” has a function of adjusting the flow velocity and direction of the air flowing into the space between the blade support arm, the cylindrical rotating shaft, and the blade. Since the air flowing into the rectifying window is compressed, the induced drag acting on the wing is further reduced. Therefore, in the vertical axis type windmill of this embodiment, the ratio of lift to drag is further increased, and higher rotational efficiency can be obtained even in the slight wind speed region.
  • FIG. 9 is a side view showing an example of the structure of the vertical axis wind turbine of the present embodiment.
  • the arm cover member Is a hyperboloid, and when the rectifying window is viewed from the front, it may be substantially zero-shaped.
  • the arm cover member may have a curved shape such as a truncated cone or a hemispherical surface.
  • the horizontal width of the blade support arm is preferably 30% or more of the length of the blade in the rotation direction. Note that even if it is 50% or more, the effect of rectification is not greatly affected, so 30 to 50% is preferable from the viewpoint of weight reduction.
  • the distance between the upper and lower wing support arms is preferably 50% or more of the vertical length of the wing.
  • the distance between the blade and the cylindrical rotating shaft is approximately half of the distance between the upper and lower blade support arms. Since the distance is less than half the vertical length of the wing, the force acting on the trailing edge of the wing (inductive drag) can be reduced sufficiently, and between the wing and the cylindrical rotating shaft. Since there is a certain interval, a relatively large rotational torque can be generated.
  • the vertical axis wind turbine according to the present embodiment is characterized in that in addition to the configuration of the first or second embodiment, a generator sharing a shaft with a cylindrical rotating shaft is provided. With this configuration, the rotation of the cylindrical rotation shaft can be directly transmitted to the generator, and power generation can be performed efficiently.
  • FIG. 10 is a diagram illustrating an example of the structure of the vertical axis wind turbine according to the present embodiment.
  • the basic configuration is the same as in the first or second embodiment, but the vertical axis wind turbine of the present embodiment has a “generator” 5 that shares a “cylindrical rotating shaft” 1 and an “axis” 11. It is characterized by.
  • The“ generator ” has a function of converting the rotation of the cylindrical rotating shaft into electric power. Since the generator of this embodiment shares a shaft with the cylindrical rotating shaft, the rotating force of the cylindrical rotating shaft can be directly used, and power generation can be performed efficiently. As a specific example of the generator, for example, a permanent magnet type AC generator may be used. The electric power generated by the generator is taken out by wiring not shown. It is conceivable that the electric power is consumed by an electric device such as a lighting fixture or a battery is charged.
  • FIG. 11 is a diagram showing another example of the structure of the vertical axis wind turbine of the present embodiment.
  • the generator can be arranged inside the cylindrical rotating shaft as shown in FIG. 10.
  • FIG. 10 it is possible to adopt a configuration in which it is arranged below the cylindrical rotating shaft.
  • positions a generator above a cylindrical rotating shaft is also possible.
  • the vertical axis wind turbine of the present embodiment can directly transmit the rotation of the cylindrical rotary shaft to the generator, so that it is possible to efficiently generate power.
  • the vertical axis wind turbine of the present embodiment includes a cylindrical rotating shaft, a blade supporting arm that supports the blade at two upper and lower positions, three blades supported at equal intervals in the rotation direction, and a cylindrical rotating shaft. And a generator that shares the shaft and is arranged inside the cylindrical rotating shaft.
  • the shape of the vertical axis wind turbine of this embodiment is the same as the example shown in FIGS. 7 and 8, and the structure is the same as the example shown in FIG.
  • the cylindrical rotating shaft is composed of a support member, a connecting member that connects the support member and the wing support arm, and a hollow cylindrical cover member that covers the support member and the like.
  • the support member is made of stainless steel
  • the connecting member and the cylindrical cover member are made of aluminum.
  • the upper and lower portions of the cylindrical cover member are acrylic resin dome.
  • the diameter of the cylindrical cover member is the same as the chord length of the wing, and the vertical length of the cylindrical cover member including the dome is 115% of the vertical length of the wing.
  • the chord length is 0.30 [m]
  • the vertical length of the wing is 1 [m].
  • each wing support arm is composed of two arm members arranged with a gap and a pair of arm cover members.
  • the arm member is an aluminum material
  • the arm cover member is an acrylic resin material.
  • the distance from the cylindrical cover member to the wing is 30% of the vertical length of the wing.
  • the average horizontal width of the wing support arms is 40% of the diameter of the cylindrical cover member.
  • the arm cover member is a hyperboloid, and the rectifying window surrounded by the arm cover member, the cylindrical cover member, and the wings has a substantially zero shape when viewed from the horizontal direction.
  • the upper surface of the wing has a gently curved shape from the leading edge to the trailing edge, and the lower surface of the wing has a planar shape from the leading edge to the trailing edge.
  • the leading edge portion of the wing has a rounded shape, and the trailing edge portion has a sharp shape.
  • the diameter of the circumferential trajectory of the wing is the same as the vertical length of the wing.
  • the thickest part of the wing is 5% of the vertical length of the wing.
  • the weight of each wing is 3 [kg].
  • the generator is a permanent magnet type three-phase AC generator, which is arranged inside a cylindrical rotating shaft.
  • the body of the generator and the wing support arm are connected by an aluminum connecting member.
  • FIG. 12 is a diagram showing the relationship between the power generation amount and the wind speed of the vertical axis wind turbine of this example.
  • the vertical axis wind turbine of this example generates 11 [W] of power at a wind speed of 4 [m / s] and 305 [W] of power at a wind speed of 12 [m / s]. It is possible to generate electricity. In other words, it was possible to efficiently generate power even in the low wind speed region.

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  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
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  • Chemical & Material Sciences (AREA)
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Abstract

[Problem] Conventional vertical shaft windmills struggled to obtain good rotation starting properties, because drag operated more strongly than lift force in low wind regions. The purpose of the present invention is to provide a vertical shaft windmill capable of efficient rotation even in low wind regions. [Solution] In order to solve said issue, the present invention provides a vertical shaft windmill comprising a cylindrical rotating shaft and a plurality of blades supported by the cylindrical rotating shaft via a blade supporting arm. The interval between the blades and the cylindrical rotating shaft is at or below the length of the blades in the vertical direction.

Description

垂直軸型風車Vertical axis windmill
 本発明は、風力発電などに用いられる垂直軸型風車に関する。 The present invention relates to a vertical axis type windmill used for wind power generation and the like.
 風車としては、回転軸が水平方向の水平軸型風車と、回転軸が垂直方向の垂直軸型風車が知られている。垂直軸型風車は、水平軸型風車と異なり、360度どちらの方向からの風についても回転駆動源とすることが可能であり、かつ、コンパクトなスペースに配置することができるという利点を有する。 As a windmill, a horizontal axis type windmill having a horizontal rotation axis and a vertical axis type windmill having a vertical rotation axis are known. Unlike the horizontal axis type wind turbine, the vertical axis type wind turbine has an advantage that it can be used as a rotational drive source for wind from either direction of 360 degrees and can be arranged in a compact space.
 垂直軸型風車としては、細い回転軸を中心とした円周上に複数の翼を設置する構造のものが一般的に知られている。例えば、特許文献1では、垂直軸型風車の翼厚を調整することによって翼の空力特性を改善し、回転効率を向上させる技術が開示されている。 As a vertical axis type wind turbine, one having a structure in which a plurality of blades are installed on a circumference around a thin rotating shaft is generally known. For example, Patent Document 1 discloses a technique for improving the aerodynamic characteristics of a blade by adjusting the blade thickness of a vertical axis wind turbine to improve the rotation efficiency.
特開2009-191744JP 2009-191744 A
 しかしながら、従来の垂直軸型風車では微風速域において揚力よりも抗力が強く作用するため、高い回転起動性を得ることが難しかった。そこで、本発明は、微風速域においても効率的に回転させることが可能な垂直軸型風車を提案することを目的とする。 However, in the conventional vertical axis type windmill, the drag acts more strongly than the lift force in the slight wind speed region, so it is difficult to obtain high rotational startability. Therefore, an object of the present invention is to propose a vertical axis type windmill that can be efficiently rotated even in a low wind speed region.
 以上の課題を解決するために、本発明は、円筒状回転軸と、円筒状回転軸に翼支持腕にて複数支持される翼と、からなる垂直軸型風車であって、前記翼と前記円筒状回転軸の間隔は、前記円筒状回転軸の直径と略同一である垂直軸型風車を提案する。 In order to solve the above-mentioned problems, the present invention is a vertical axis wind turbine comprising a cylindrical rotating shaft and a plurality of blades supported by a blade rotating arm on the cylindrical rotating shaft. A vertical axis wind turbine is proposed in which the interval between the cylindrical rotating shafts is substantially the same as the diameter of the cylindrical rotating shaft.
 本発明では、翼を後縁側に引きずる力(誘導抗力)が弱くなり、抗力に対する揚力の比率が大きくなるため、微風速域であっても効率的に翼を回転させることが可能になる。 In the present invention, since the force (inductive drag) that drags the blade toward the trailing edge is weakened and the ratio of lift to the drag is increased, the blade can be efficiently rotated even in the low wind speed region.
実施形態1の垂直軸型風車の形状の一例を示す平面図The top view which shows an example of the shape of the vertical axis type windmill of Embodiment 1. 実施形態1の垂直軸型風車の形状の一例を示す正面図The front view which shows an example of the shape of the vertical axis type windmill of Embodiment 1. 実施形態1の垂直軸型風車の構造の一例を示す側面図1 is a side view showing an example of the structure of a vertical axis wind turbine according to a first embodiment. 実施形態1の垂直軸型風車の構造の一例を示す平面図The top view which shows an example of the structure of the vertical axis type windmill of Embodiment 1. 従来の垂直軸型風車の翼に作用する誘導抗力の様子を示す図The figure which shows the mode of the induction drag which acts on the blade of the conventional vertical axis type windmill 実施形態1の垂直軸型風車の翼に作用する誘導抗力の様子を示す図The figure which shows the mode of the induced drag which acts on the blade | wing of the vertical axis type windmill of Embodiment 1. 実施形態1の垂直軸型風車の翼に作用する揚力と抗力を示す図The figure which shows the lift and the drag which act on the wing | blade of the vertical axis type windmill of Embodiment 1. 実施形態2の垂直軸型風車の形状の一例を示す正面図The front view which shows an example of the shape of the vertical axis type windmill of Embodiment 2. 実施形態2の垂直軸型風車の構造の一例を示す側面図The side view which shows an example of the structure of the vertical axis type windmill of Embodiment 2. 実施形態3の垂直軸型風車の構造の一例を示す側面図The side view which shows an example of the structure of the vertical axis type windmill of Embodiment 3. 実施形態3の垂直軸型風車の構造の他の例を示す側面図The side view which shows the other example of the structure of the vertical axis type windmill of Embodiment 3. 実施例1の垂直軸型風車の発電量と風速の関係を示す図The figure which shows the relationship between the electric power generation amount of the vertical axis type windmill of Example 1, and a wind speed.
 以下、本発明の実施形態について説明する。請求項と実施形態の対応関係は以下のとおりである。実施形態1は主に請求項1から請求項5に関し、実施形態2は主に請求項6と請求項7に関し、実施形態3は主に請求項9に関する。なお、本件発明は以下の実施形態の例に限定されるものではなく、種々なる態様で実施することが可能である。 Hereinafter, embodiments of the present invention will be described. The correspondence between the claims and the embodiment is as follows. The first embodiment mainly relates to claims 1 to 5, the second embodiment mainly relates to claims 6 and 7, and the third embodiment mainly relates to claim 9. In addition, this invention is not limited to the example of the following embodiment, It is possible to implement in various aspects.
<<実施形態1>> << Embodiment 1 >>
<概要>
 本実施形態の垂直軸型風車は、翼と円筒状回転軸の間隔が、翼の鉛直方向の長さ以下であることを特徴とする。当該構成とすることにより、翼を後縁側に引きずる力(誘導抗力)が減少し、抗力に対する揚力の比率が大きくなるため、翼の回転起動性が高くなる。
<Overview>
The vertical axis wind turbine according to the present embodiment is characterized in that the distance between the blade and the cylindrical rotating shaft is equal to or less than the length of the blade in the vertical direction. With this configuration, the force that drags the wing toward the trailing edge (inductive drag) decreases, and the ratio of lift to drag increases, so that the rotational startability of the wing increases.
<構成>
 図1と図2は、本実施形態の垂直軸型風車の形状の一例を示す平面図と正面図である。これらの図に示されているように、本実施形態の「垂直軸型風車」は、「円筒状回転軸」1と、「円筒状回転軸」に「翼支持腕」2にて支持される複数の「翼」3と、からなる。
<Configuration>
1 and 2 are a plan view and a front view showing an example of the shape of the vertical axis wind turbine according to the present embodiment. As shown in these drawings, the “vertical shaft type windmill” of the present embodiment is supported by the “cylindrical rotating shaft” 1 and the “cylindrical rotating shaft” by the “wing support arm” 2. And a plurality of “wings” 3.
 「円筒状回転軸」1は、翼の回転軸としての機能と、水平方向から吹いてくる風をその側面で受け止めて、軸周りの気流を形成する機能を有する。さらに、「翼の下面」31に対向する面としての役割を担い、翼と円筒状回転軸の間の気流の圧力を高める機能を有する。 The “cylindrical rotating shaft” 1 has a function as a rotating shaft of the wing and a function of receiving air blowing from the horizontal direction on its side surface to form an airflow around the shaft. Furthermore, it plays a role as a surface facing the “lower surface of the blade” 31 and has a function of increasing the pressure of the airflow between the blade and the cylindrical rotating shaft.
 円筒状回転軸が対向する面としての役割を十分に果たすために、円筒状回転軸の直径は「翼弦長」32と略同一とすることが好ましい。円筒状回転軸の直径を翼弦長よりも小さくすると翼の下面に対向する面としての機能が低下し、翼弦長よりも大きくし過ぎると必要以上に円筒状回転軸のサイズや重量が大きくなってしまう。なお、本明細書において、略同一であるとは、一方と他方の値の差が、一方又は他方のいずれか絶対値が小さい方の大きさの±20%以内であることを意味する。 It is preferable that the diameter of the cylindrical rotating shaft is substantially the same as the “chord chord length” 32 in order to sufficiently fulfill the role of the surface facing the cylindrical rotating shaft. If the diameter of the cylindrical rotating shaft is made smaller than the chord length, the function as the surface facing the lower surface of the wing will be reduced, and if it is made too large, the size and weight of the cylindrical rotating shaft will become larger than necessary. turn into. In the present specification, “substantially the same” means that the difference between the values of one and the other is within ± 20% of the magnitude of the smaller one or the other.
 同様に、円筒状回転軸が翼の下面に対向する面の役割を十分に果たすために、円筒状回転軸の鉛直方向の長さと翼の鉛直方向の長さを略同一とすることが好ましい。円筒状回転軸の鉛直方向の長さを翼の鉛直方向の長さと比較して短くすると対向する面としての機能が低下し、円筒状回転軸の鉛直方向の長さを翼の鉛直方向の長さと比較して長くすると必要以上に円筒状回転軸のサイズや重量が大きくなってしまう。 Similarly, it is preferable that the vertical length of the cylindrical rotating shaft and the vertical length of the blade are substantially the same in order for the cylindrical rotating shaft to sufficiently fulfill the role of the surface facing the lower surface of the blade. When the vertical length of the cylindrical rotating shaft is shortened compared to the vertical length of the wing, the function as the facing surface is reduced, and the vertical length of the cylindrical rotating shaft is reduced to the vertical length of the wing. If it is longer than that, the size and weight of the cylindrical rotating shaft will be larger than necessary.
 図3と図4は、本実施形態の垂直軸型風車の内部構造の一例を示す側面図と平面図である。図3に示すように、「円筒状回転軸」は、「支柱部材」11と、支柱部材と翼支持腕の部材を連結する「連結部材」12と、支柱部材などを覆うための「円筒カバー部材」13などからなる構成が考えられる。また、円筒カバー部材には翼支持腕の部材を通すための「アーム取出孔」14が設けられている。 3 and 4 are a side view and a plan view showing an example of the internal structure of the vertical axis wind turbine according to the present embodiment. As shown in FIG. 3, the “cylindrical rotating shaft” includes a “post member” 11, a “connecting member” 12 that connects the post member and the wing support arm member, and a “cylindrical cover” for covering the post member and the like. The structure which consists of "member" 13 etc. can be considered. The cylindrical cover member is provided with an “arm extraction hole” 14 through which the member of the wing support arm passes.
 ここで、支柱部材についてはステンレス等の金属やカーボンファイバーなどの強度の高い素材を用い、連結部材や円筒カバー部材についてはアルミニウム等の金属やカーボンファイバー、プラスチック樹脂などの耐久性が高く軽量な素材を用いることが好ましい。なお、円筒カバー部材において強度が要求されない部分については、アクリル樹脂、ABS樹脂等の加工しやすく軽量なプラスチック素材を用いることも考えられる。 Here, high strength materials such as stainless steel and carbon fiber are used for the strut members, and durable and lightweight materials such as metal such as aluminum, carbon fiber, and plastic resin are used for the connecting member and the cylindrical cover member. Is preferably used. In addition, it is also conceivable to use a lightweight plastic material that is easy to process, such as an acrylic resin or an ABS resin, for a portion of the cylindrical cover member that does not require strength.
 「翼支持腕」2は、翼と円筒状回転軸をつなぎ、翼による回転力を円筒状回転軸に伝達する機能を有する。「翼支持腕」は、例えば図3及び図4に示すように、円筒状回転軸に連結される二本の「アーム部材」21A・21Bと、アーム部材を覆う一組の「アームカバー部材」22A・22Bなどからなる構成が考えられる。 The “wing support arm” 2 has a function of connecting the blade and the cylindrical rotating shaft and transmitting the rotational force of the blade to the cylindrical rotating shaft. For example, as shown in FIGS. 3 and 4, the “wing support arm” includes two “arm members” 21 </ b> A and 21 </ b> B connected to a cylindrical rotating shaft, and a pair of “arm cover members” covering the arm members. A configuration including 22A, 22B, and the like is conceivable.
 ここで、アーム部材についてはアルミニウム、カーボンファイバー等の耐久性が高く軽量な素材を用いることが好ましい。また、アームカバー部材についてはアクリル樹脂、ABS樹脂等の加工しやすく軽量なプラスチック素材を用いることが好ましい。 Here, it is preferable to use a highly durable and lightweight material such as aluminum or carbon fiber for the arm member. For the arm cover member, it is preferable to use a lightweight plastic material that is easy to process, such as acrylic resin or ABS resin.
 また、「翼と円筒状回転軸の間隔」41を「翼の鉛直方向の長さ」33以下とすることによって、以下に述べるように、翼を後縁側に引きずる力(誘導抗力)を減少させることが可能になる。 Further, by setting the “interval between the blade and the cylindrical rotating shaft” 41 to be “the length of the blade in the vertical direction” 33 or less, as described below, the force (inductive drag) that drags the blade toward the trailing edge is reduced. It becomes possible.
 図5は、従来の一般的な垂直軸型風車において翼に作用する誘導抗力の様子を示した図である。従来の垂直軸型風車では、回転力を大きくする観点から「翼と回転軸の間隔」40を比較的大きくし、強度が許す限りにおいて回転軸の直径を小さくしている。このような場合、翼と回転軸の間隔における圧力は翼の上面より少し高くなるものの、それ程高くはならない。このため、翼の後縁にて翼の上面側から下面側に向かう「気流の傾き(吹き下ろし角)」26が大きくなる。ここで、吹き下ろし角が大きいほど翼に作用する誘導抗力が大きくなるため、翼に対して比較的大きな「誘導抗力」27が発生する。 FIG. 5 is a diagram showing a state of induced drag acting on the blades in a conventional general vertical axis type wind turbine. In the conventional vertical axis type wind turbine, from the viewpoint of increasing the rotational force, the “interval between the blade and the rotary shaft” 40 is made relatively large, and the diameter of the rotary shaft is made as small as the strength allows. In such a case, the pressure at the distance between the blade and the rotating shaft is slightly higher than the upper surface of the blade, but not so high. For this reason, the “inclination of airflow (down angle)” 26 increases from the upper surface side to the lower surface side of the blade at the trailing edge of the blade. Here, since the induced drag acting on the wing increases as the blowing angle increases, a relatively large “induced drag” 27 is generated on the wing.
 図6は、翼と円筒状回転軸の間隔が前記翼の鉛直方向の長さ以下である場合に、翼に作用する誘導抗力の様子を示した図である。「翼と円筒状回転軸の間隔」41が鉛直方向の長さ以下である場合、翼と円筒状回転軸の間隔における圧力が従来の垂直軸型風車よりも高くなる。このため、翼の後縁にて翼の上面側から下面側に向かう「気流の傾き(吹き下ろし角)」26が比較的小さくなる。吹き降ろし角が小さいほど翼に作用する誘導抗力が弱くなるため、吹き降ろし角の減少に伴って翼に作用する「誘導抗力」27が減少する。つまり、回転軸を円筒状にして、かつ、翼と円筒状回転軸との間隔を翼の鉛直方向の長さ以下とすることにより、翼に作用する誘導抗力を減らすことが可能になる。 FIG. 6 is a diagram showing a state of induced drag acting on the wing when the distance between the wing and the cylindrical rotating shaft is equal to or less than the vertical length of the wing. When the “interval between the blade and the cylindrical rotating shaft” 41 is equal to or less than the length in the vertical direction, the pressure at the interval between the blade and the cylindrical rotating shaft is higher than that of the conventional vertical axis type wind turbine. Therefore, the “airflow inclination (down angle)” 26 from the upper surface side to the lower surface side of the blade at the trailing edge of the blade is relatively small. Since the induced drag acting on the wing becomes weaker as the blow-down angle is smaller, the “induced drag” 27 acting on the wing decreases as the blow-down angle decreases. That is, it is possible to reduce the induced drag acting on the blade by making the rotation shaft cylindrical and setting the distance between the blade and the cylindrical rotation shaft to be equal to or less than the vertical length of the blade.
 なお、翼と円筒状回転軸の間隔が、翼の鉛直方向の長さの半分以下である場合は、翼に作用する誘導抗力が特に減少する点で好ましい。ただし、翼と円筒状回転軸の間隔を狭くし過ぎると逆に回転トルクが小さくなってしまうため、翼と円筒状回転軸の間隔は翼の鉛直方向の長さの25~35%程度とすることが好ましい。 It should be noted that when the distance between the blade and the cylindrical rotating shaft is not more than half the vertical length of the blade, it is preferable in that the induced drag acting on the blade is particularly reduced. However, if the distance between the blade and the cylindrical rotating shaft is too narrow, the rotational torque will be reduced. Therefore, the distance between the blade and the cylindrical rotating shaft is about 25 to 35% of the vertical length of the blade. It is preferable.
 また、「翼支持腕の平均水平幅」42は、翼支持腕の側面を流れる空気を水平方向に整流する観点から、円筒状回転軸の直径の30%以上とすることが好ましい。なお、軽量性の観点から、翼支持腕は円筒状回転軸の直径の50%未満とすることが好ましい。また、図2や図3に示すようにアームカバー部材を曲面状にすることによって、気流の流れをスムーズにすることが可能である。 Also, the “average horizontal width of the wing support arm” 42 is preferably 30% or more of the diameter of the cylindrical rotating shaft from the viewpoint of rectifying the air flowing on the side surface of the wing support arm in the horizontal direction. From the viewpoint of lightness, the blade support arm is preferably less than 50% of the diameter of the cylindrical rotating shaft. Further, by making the arm cover member a curved surface as shown in FIGS. 2 and 3, the flow of the airflow can be made smooth.
 また、翼支持腕のいずれかの位置に穴部を設けて、鉛直方向の流路を確保することが好ましい。当該構成とすることにより、翼支持腕が回転した状態においても鉛直方向に流路が確保されるため、翼の円周軌跡の内側に対する空気の出入りがスムーズになる。具体的には、図4に示すように、二本の「アーム部材」21A・21Bを所定の間隔をあけて配置し、翼から円筒状回転軸までの領域の略中央では「アーム部材」を「アームカバー部材」22A・22Bで覆わない構成とすることが考えられる。これにより、翼から円筒状回転軸までの領域の略中央に鉛直方向の流路となる「穴部」23が形成される。 It is also preferable to provide a hole in any position of the blade support arm to ensure a vertical flow path. With this configuration, since the flow path is secured in the vertical direction even when the blade support arm is rotated, air can smoothly enter and exit from the inside of the circumferential locus of the blade. Specifically, as shown in FIG. 4, two “arm members” 21 </ b> A and 21 </ b> B are arranged at a predetermined interval, and the “arm member” is arranged at the approximate center of the region from the wing to the cylindrical rotating shaft. It is conceivable that the arm cover members 22A and 22B are not covered. As a result, a “hole” 23 serving as a vertical flow path is formed in the approximate center of the region from the blade to the cylindrical rotation axis.
 なお、図2と図3では翼支持腕により鉛直方向の略中央の位置一か所で翼を支持する構成を示したが、翼支持腕により上下二か所で翼を支持する構成も可能であるし、それ以上の箇所で支持する構成も可能である。また、支持点についても種々考えられる。 2 and 3 show the configuration in which the wing is supported by the wing support arm at one central position in the vertical direction. However, the wing support arm may be configured to support the wing at two upper and lower positions. There is also a configuration in which the support is provided at more points. Various support points are also conceivable.
 「翼」3は、揚力により回転方向にトルクを発生させる機能を有する。ここで、翼は、繊維強化プラスチック、カーボンファイバー等の軽量で強度の高い素材を用いることが好ましい。また、複数の翼は、水平方向の風が吹いてくる方向に関係なく均等にトルクを発生させる観点から、回転方向にて等間隔に支持されることが好ましい。 “Wings” 3 has a function of generating torque in the rotational direction by lift. Here, it is preferable to use a lightweight and high-strength material such as fiber reinforced plastic or carbon fiber for the wing. Moreover, it is preferable that a some wing | blade is supported at equal intervals in a rotation direction from a viewpoint of generating a torque equally irrespective of the direction where the wind of a horizontal direction blows.
 図4に示すように、「翼の上面」30は前縁から後縁にかけて緩やかに湾曲し、「翼の下面」31は前縁から後縁にかけて平面的になっている。また、翼の前縁部分は丸みを帯びた形状であり、後縁部分はとがった形状となっている。これらの特徴は飛行機の主翼と同様である。翼厚は、高い揚力を発生させる観点から、もっとも厚い部分で円筒状回転軸の直径の5~30%とすることが好ましい。 As shown in FIG. 4, the “wing upper surface” 30 is gently curved from the leading edge to the trailing edge, and the “wing lower surface” 31 is planar from the leading edge to the trailing edge. The leading edge portion of the wing has a rounded shape, and the trailing edge portion has a sharp shape. These features are similar to the main wing of an airplane. The blade thickness is preferably 5 to 30% of the diameter of the cylindrical rotating shaft at the thickest portion from the viewpoint of generating high lift.
 図7は、水平方向の風が吹いたときに翼に作用する力を示す図である。この図に示すように、「翼」3は、「水平方向からの風」51を受けることによって「揚力」52を発生させる。当該揚力は翼に作用する「抗力」53と垂直な方向に作用し、「回転方向」54の成分を有する。当該回転方向の成分を駆動源として翼は回転する。ここで、「翼を後縁側に引きずる力(誘導抗力)」27は、上述のように、翼と円筒状回転軸の間隔を翼の鉛直方向の長さ以下とすることによって小さくなっている。このため、本実施形態の垂直軸型風車において、抗力に対する揚力の比率が大きくなり、より大きな回転力を得ることが可能になる。 FIG. 7 is a diagram showing the force acting on the wing when a horizontal wind blows. As shown in this figure, the “wing” 3 generates “lift” 52 by receiving “wind from the horizontal direction” 51. The lift acts in a direction perpendicular to “drag” 53 acting on the wing, and has a component of “rotation direction” 54. The blade rotates using the component in the rotation direction as a drive source. Here, the “force for dragging the blade toward the trailing edge (inductive drag)” 27 is reduced by setting the distance between the blade and the cylindrical rotating shaft to be equal to or less than the vertical length of the blade as described above. For this reason, in the vertical axis type windmill of this embodiment, the ratio of the lift to the drag is increased, and a larger rotational force can be obtained.
<効果>
 本実施形態の垂直軸型風車においては、翼を後縁側に引きずる力(誘導抗力)が小さくなり、抗力に対する揚力の比率が大きくなるため、微風速域であっても効率的に翼を回転させることが可能になる。
<Effect>
In the vertical axis wind turbine of the present embodiment, the force (inductive drag) that drags the blade toward the trailing edge is reduced, and the ratio of lift to the drag is increased. Therefore, the blade can be efficiently rotated even in the low wind speed region. It becomes possible.
<<実施形態2>> << Embodiment 2 >>
<概要>
 本実施形態の垂直軸型風車は、実施形態1の特徴に加えて、翼支持腕が上下二か所で翼を支持することで、翼支持腕と円筒状回転軸と翼とによって囲まれる整流窓が形成されることを特徴とする。翼の円周軌跡の内側に入り込んだ空気は整流窓によって圧縮されるため、翼に作用する誘導抗力はさらに減少し、抗力に対する揚力の比率が大きくなるため、微風速域における回転効率をさらに高くすることが可能になる。
<Overview>
In addition to the features of the first embodiment, the vertical axis wind turbine according to the present embodiment supports the wings at two upper and lower positions so that the rectification surrounded by the wing support arms, the cylindrical rotating shaft, and the wings A window is formed. Since the air that has entered the inside of the wing's circumferential trajectory is compressed by the rectifying window, the induced drag acting on the wing is further reduced, and the ratio of lift to drag is increased. It becomes possible to do.
<構成>
 図8は、本実施形態の垂直軸型風車の形状の一例を示す正面図である。基本的な構成は、実施形態1と同様であるが、本実施形態の垂直軸型風車は、「翼支持腕」2A・2Bが上下二か所で「翼」3を支持することで、「翼支持腕」2A・2Bと「円筒状回転軸」1と「翼」3とによって囲まれる「整流窓」4が形成されることを特徴とする。
<Configuration>
FIG. 8 is a front view showing an example of the shape of the vertical axis wind turbine of the present embodiment. The basic configuration is the same as that of the first embodiment, but the vertical axis type wind turbine of the present embodiment supports the “wings” 3 by the “wing support arms” 2A and 2B at two upper and lower positions. A “rectifying window” 4 surrounded by the “wing support arms” 2A and 2B, the “cylindrical rotating shaft” 1 and the “wing” 3 is formed.
 「整流窓」は、翼支持腕と円筒状回転軸と翼の間の空間に流れ込む空気の流速や方向を整える機能を有する。整流窓に流れ込む空気は圧縮されるため、翼に作用する誘導抗力がさらに減少する。よって、本実施形態の垂直軸型風車では、抗力に対する揚力の比率がさらに高くなり、微風速域であってもより高い回転効率を得ることが可能になる。 The “rectifying window” has a function of adjusting the flow velocity and direction of the air flowing into the space between the blade support arm, the cylindrical rotating shaft, and the blade. Since the air flowing into the rectifying window is compressed, the induced drag acting on the wing is further reduced. Therefore, in the vertical axis type windmill of this embodiment, the ratio of lift to drag is further increased, and higher rotational efficiency can be obtained even in the slight wind speed region.
 図9は本実施形態の垂直軸型風車の構造の一例を示す側面図である。この図に示すように、「翼支持腕」が二本の「アーム部材」21A・21B(21C・21D)と「アームカバー部材」22A・22B(22C・22D)とからなる場合、アームカバー部材を双曲面として、整流窓を正面から見た場合に略0字型になるようにすることが考えられる。なお、アームカバー部材は、円錐台や、半球面などの曲面形状とすることも可能である。 FIG. 9 is a side view showing an example of the structure of the vertical axis wind turbine of the present embodiment. As shown in this figure, when the “wing support arm” is composed of two “arm members” 21A and 21B (21C and 21D) and “arm cover members” 22A and 22B (22C and 22D), the arm cover member Is a hyperboloid, and when the rectifying window is viewed from the front, it may be substantially zero-shaped. Note that the arm cover member may have a curved shape such as a truncated cone or a hemispherical surface.
 整流の効果を高くするために、翼支持腕の水平幅は翼の回転方向の長さの30%以上とすることが好ましい。なお、50%以上としても整流の効果に大きく影響を与えないため、軽量化の観点において30~50%とすることが好ましい。 In order to increase the effect of rectification, the horizontal width of the blade support arm is preferably 30% or more of the length of the blade in the rotation direction. Note that even if it is 50% or more, the effect of rectification is not greatly affected, so 30 to 50% is preferable from the viewpoint of weight reduction.
 また、上下二か所の翼支持腕の間隔は、翼の鉛直方向の長さの50%以上とすることが好ましい。整流窓の領域をある程度大きくすることによって、所定量以上の空気を水平方向に整流(圧縮)することが可能になる。 Also, the distance between the upper and lower wing support arms is preferably 50% or more of the vertical length of the wing. By enlarging the area of the rectifying window to some extent, it becomes possible to rectify (compress) a predetermined amount or more of air in the horizontal direction.
 また、翼と円筒状回転軸の間隔は、上下二か所の翼支持腕の間隔の略半分とすることが特に好ましい。当該間隔は、翼の鉛直方向の長さの半分以下であるため、翼の後縁側に作用する力(誘導抗力)を十分減少させることが可能であり、かつ、翼と円筒状回転軸の間に一定の間隔が存在するため、比較的大きな回転トルクを発生させることが可能である。 In addition, it is particularly preferable that the distance between the blade and the cylindrical rotating shaft is approximately half of the distance between the upper and lower blade support arms. Since the distance is less than half the vertical length of the wing, the force acting on the trailing edge of the wing (inductive drag) can be reduced sufficiently, and between the wing and the cylindrical rotating shaft. Since there is a certain interval, a relatively large rotational torque can be generated.
<効果>
 本実施形態の垂直軸型風車においては、実施形態1の垂直軸型風車と比較して、さらに誘導抗力が減少するため、微風速域であってもより高い回転効率を得ることが可能になる。
<Effect>
In the vertical axis wind turbine of the present embodiment, since the induction drag is further reduced as compared with the vertical axis wind turbine of the first embodiment, it is possible to obtain higher rotational efficiency even in the low wind speed region. .
<<実施形態3>> << Embodiment 3 >>
<概要> <Overview>
 本実施形態の垂直軸型風車は、実施形態1又は2の構成に加えて、円筒状回転軸と軸を共有する発電機を有することを特徴とする。当該構成により、円筒状回転軸の回転をダイレクトに発電機に伝達することが可能になり、効率的に発電を行うことが可能になる。 The vertical axis wind turbine according to the present embodiment is characterized in that in addition to the configuration of the first or second embodiment, a generator sharing a shaft with a cylindrical rotating shaft is provided. With this configuration, the rotation of the cylindrical rotation shaft can be directly transmitted to the generator, and power generation can be performed efficiently.
<構成>
 図10は、本実施形態の垂直軸型風車の構造の一例を示す図である。基本的な構成は、実施形態1又は2と同様であるが、本実施形態の垂直軸型風車は、「円筒状回転軸」1と「軸」11を共有する「発電機」5を有することを特徴とする。
<Configuration>
FIG. 10 is a diagram illustrating an example of the structure of the vertical axis wind turbine according to the present embodiment. The basic configuration is the same as in the first or second embodiment, but the vertical axis wind turbine of the present embodiment has a “generator” 5 that shares a “cylindrical rotating shaft” 1 and an “axis” 11. It is characterized by.
 「発電機」は、円筒状回転軸の軸回転を電力に変換する機能を有する。本実施形態の発電機は円筒状回転軸と軸を共有しているため、円筒状回転軸の回転力を直接的に利用することができ、効率的に発電を行うことが可能になる。発電機の具体例としては、例えば永久磁石式の交流発電機などを用いることが考えられる。発電機により発電された電力は図示しない配線によって取り出される。当該電力は、照明器具などの電気機器にて消費されたり、バッテリーに充電されたりすることが考えられる。 “The“ generator ”has a function of converting the rotation of the cylindrical rotating shaft into electric power. Since the generator of this embodiment shares a shaft with the cylindrical rotating shaft, the rotating force of the cylindrical rotating shaft can be directly used, and power generation can be performed efficiently. As a specific example of the generator, for example, a permanent magnet type AC generator may be used. The electric power generated by the generator is taken out by wiring not shown. It is conceivable that the electric power is consumed by an electric device such as a lighting fixture or a battery is charged.
 図11は、本実施形態の垂直軸型風車の構造の他の例を示す図である。発電機は図10に示したように円筒状回転軸の内部に配置することも可能であるが、例えば発電機の形状が大きく、円筒状回転軸の内部に配置できない場合などは、図11に示すように円筒状回転軸の下方に配置する構成も可能である。また、発電機を円筒状回転軸の上方に配置する構成も同様に可能である。 FIG. 11 is a diagram showing another example of the structure of the vertical axis wind turbine of the present embodiment. The generator can be arranged inside the cylindrical rotating shaft as shown in FIG. 10. However, for example, when the shape of the generator is large and cannot be arranged inside the cylindrical rotating shaft, FIG. As shown, it is possible to adopt a configuration in which it is arranged below the cylindrical rotating shaft. Moreover, the structure which arrange | positions a generator above a cylindrical rotating shaft is also possible.
 なお、円筒状回転軸と軸を共有するギア、プーリーなどの変速機を配置し、当該変速機と連結される発電機を設けることによって、低回転高出力風力発電機を構成することも可能である。 It is also possible to configure a low-rotation high-output wind power generator by disposing a gear, pulley, etc. that share the shaft with the cylindrical rotation shaft and providing a generator that is connected to the transmission. is there.
 また、上記発電機を垂直軸型風車の内部又は外部に設置される制御コントローラによって制御する構成も可能である。例えば、回転速度を一定速度域に制御したい場合は発電機に接続されるバッテリーの電力を利用して電気ブレーキをかけたり、加速させたりすることが考えられる。 Also, a configuration in which the generator is controlled by a controller installed inside or outside the vertical axis wind turbine is possible. For example, when it is desired to control the rotation speed within a constant speed range, it is conceivable to apply an electric brake or accelerate using the power of a battery connected to the generator.
<効果>
 本実施形態の垂直軸型風車により、実施形態1の効果に加えて、円筒状回転軸の回転をダイレクトに発電機に伝達することができるため、効率的に発電を行うことが可能になる。
<Effect>
In addition to the effects of the first embodiment, the vertical axis wind turbine of the present embodiment can directly transmit the rotation of the cylindrical rotary shaft to the generator, so that it is possible to efficiently generate power.
 本実施例の垂直軸型風車は、円筒状回転軸と、翼を上下二か所で支持する翼支持腕と、回転方向にて等間隔に支持される三枚翼と、円筒状回転軸と軸を共有し円筒状回転軸の内部に配置される発電機と、から構成される。本実施形態の垂直軸型風車の形状は、図7及び図8に示す例と同様であり、構造は図10に示す例と同様である。 The vertical axis wind turbine of the present embodiment includes a cylindrical rotating shaft, a blade supporting arm that supports the blade at two upper and lower positions, three blades supported at equal intervals in the rotation direction, and a cylindrical rotating shaft. And a generator that shares the shaft and is arranged inside the cylindrical rotating shaft. The shape of the vertical axis wind turbine of this embodiment is the same as the example shown in FIGS. 7 and 8, and the structure is the same as the example shown in FIG.
 円筒状回転軸は、支柱部材と、支柱部材と翼支持腕を連結する連結部材と、支柱部材などを覆う中空の円筒カバー部材と、から構成される。ここで、支柱部材はステンレス素材であり、連結部材や円筒カバー部材はアルミニウム素材である。なお、円筒カバー部材の上部及び下部はアクリル樹脂素材のドームとなっている。円筒カバー部材の直径は、翼の翼弦長と同一であり、ドームを含めた円筒カバー部材の鉛直方向の長さは、翼の鉛直方向の長さの115%となっている。なお、翼弦長は0.30[m]であり、翼の鉛直方向の長さは1[m]となっている。 The cylindrical rotating shaft is composed of a support member, a connecting member that connects the support member and the wing support arm, and a hollow cylindrical cover member that covers the support member and the like. Here, the support member is made of stainless steel, and the connecting member and the cylindrical cover member are made of aluminum. The upper and lower portions of the cylindrical cover member are acrylic resin dome. The diameter of the cylindrical cover member is the same as the chord length of the wing, and the vertical length of the cylindrical cover member including the dome is 115% of the vertical length of the wing. The chord length is 0.30 [m], and the vertical length of the wing is 1 [m].
 本実施例の垂直軸型風車においては、三枚翼を上下二か所で支持するため、全部で6つの翼支持腕が存在する。各翼支持腕は、隙間を開けて配置される二本のアーム部材と、一組のアームカバー部材と、から構成される。アーム部材はアルミニウム素材であり、アームカバー部材はアクリル樹脂素材である。円筒カバー部材から翼までの間隔は、翼の鉛直方向の長さの30%となっている。また、翼支持腕の平均水平幅(アームカバー部材の平均水平幅)は、円筒状カバー部材の直径の40%となっている。また、アームカバー部材は双曲面となっており、アームカバー部材と円筒カバー部材と翼とによって囲まれる整流窓は水平方向から見て略0字形状となっている。 In the vertical axis wind turbine according to the present embodiment, there are six blade support arms in total because the three blades are supported at two locations, upper and lower. Each wing support arm is composed of two arm members arranged with a gap and a pair of arm cover members. The arm member is an aluminum material, and the arm cover member is an acrylic resin material. The distance from the cylindrical cover member to the wing is 30% of the vertical length of the wing. Further, the average horizontal width of the wing support arms (average horizontal width of the arm cover member) is 40% of the diameter of the cylindrical cover member. Further, the arm cover member is a hyperboloid, and the rectifying window surrounded by the arm cover member, the cylindrical cover member, and the wings has a substantially zero shape when viewed from the horizontal direction.
 翼の上面は前縁から後縁にかけて緩やかに湾曲した形状となっており、翼の下面は前縁から後縁にかけて平面的な形状となっている。また、翼の前縁部分は丸みを帯びた形状であり、後縁部分はとがった形状となっている。翼の円周軌跡の直径は、翼の鉛直方向の長さと同一になっている。また、翼のもっとも厚い部分は翼の鉛直方向の長さの5%となっている。なお、各翼の重さは3[kg]となっている。 The upper surface of the wing has a gently curved shape from the leading edge to the trailing edge, and the lower surface of the wing has a planar shape from the leading edge to the trailing edge. The leading edge portion of the wing has a rounded shape, and the trailing edge portion has a sharp shape. The diameter of the circumferential trajectory of the wing is the same as the vertical length of the wing. The thickest part of the wing is 5% of the vertical length of the wing. The weight of each wing is 3 [kg].
 発電機は永久磁石式の三相交流発電機であり、円筒状回転軸の内部に配置されている。ここで、発電機のボディと翼支持腕はアルミニウムの連結部材で連結されている。 The generator is a permanent magnet type three-phase AC generator, which is arranged inside a cylindrical rotating shaft. Here, the body of the generator and the wing support arm are connected by an aluminum connecting member.
 図12は、本実施例の垂直軸型風車の発電量と風速の関係を示した図である。この図に示すように、本実施例の垂直軸型風車は、風速4[m/s]において11[W]の電力を発電し、風速12[m/s]において305[W]の電力を発電することが可能である。つまり、微風速域においても効率的に発電を行うことが可能であった。 FIG. 12 is a diagram showing the relationship between the power generation amount and the wind speed of the vertical axis wind turbine of this example. As shown in this figure, the vertical axis wind turbine of this example generates 11 [W] of power at a wind speed of 4 [m / s] and 305 [W] of power at a wind speed of 12 [m / s]. It is possible to generate electricity. In other words, it was possible to efficiently generate power even in the low wind speed region.
1…円筒状回転軸、2…翼支持腕、3…翼、4…整流窓、5…発電機、11…支柱部材、12…連結部材、13…円筒カバー部材、14…アーム取出孔、21A~D…アーム部材、22A~D…アームカバー部材、23…穴部、26…吹き降ろし角、27…誘導抗力、30…翼の上面、31…翼の下面、32…翼弦長、33…翼の鉛直方向の長さ、40…翼と回転軸の間隔(従来技術)、41…翼と円筒状回転軸の間隔、42…翼支持腕の水平幅、51…水平方向の風、52…翼に作用する揚力、53…翼に作用する抗力、54…翼の回転方向 DESCRIPTION OF SYMBOLS 1 ... Cylindrical rotating shaft, 2 ... Blade support arm, 3 ... Blade, 4 ... Rectification window, 5 ... Generator, 11 ... Strut member, 12 ... Connecting member, 13 ... Cylindrical cover member, 14 ... Arm extraction hole, 21A D: Arm member, 22A to D: Arm cover member, 23: Hole, 26: Blow down angle, 27: Inductive drag, 30 ... Upper surface of wing, 31 ... Lower surface of wing, 32 ... Length of chord, 33 ... Vertical length of the wing, 40 ... spacing between the wing and the rotating shaft (conventional technology), 41 ... spacing between the wing and the cylindrical rotating shaft, 42 ... horizontal width of the wing support arm, 51 ... horizontal wind, 52 ... Lift acting on the wing, 53 ... Drag acting on the wing, 54 ... Direction of rotation of the wing

Claims (8)

  1.  円筒状回転軸と、
     円筒状回転軸に翼支持腕にて複数支持される翼と、
     からなる垂直軸型風車であって、
     前記翼と前記円筒状回転軸の間隔は、前記翼の鉛直方向の長さ以下である垂直軸型風車。
    A cylindrical rotation axis;
    A plurality of wings supported by a wing support arm on a cylindrical rotating shaft;
    A vertical axis type windmill consisting of
    A vertical axis wind turbine in which a distance between the blade and the cylindrical rotating shaft is equal to or less than a length in a vertical direction of the blade.
  2.  前記翼と前記円筒状回転軸の間隔は、前記翼の鉛直方向の長さの半分以下である請求項1に記載の垂直軸型風車。 The vertical axis wind turbine according to claim 1, wherein a distance between the blade and the cylindrical rotating shaft is equal to or less than a half of a vertical length of the blade.
  3.  前記円筒状回転軸の直径は、前記翼の翼弦長と略同一である請求項1又は2に記載の垂直軸型風車。 The vertical axis wind turbine according to claim 1 or 2, wherein a diameter of the cylindrical rotating shaft is substantially the same as a chord length of the blade.
  4.  前記円筒状回転軸の鉛直方向の長さは、前記翼の鉛直方向の長さと略同一である請求項1から3のいずれか一に記載の垂直軸型風車。 The vertical axis wind turbine according to any one of claims 1 to 3, wherein a vertical length of the cylindrical rotating shaft is substantially the same as a vertical length of the blade.
  5.  前記翼支持腕の水平幅は、前記翼の回転方向の長さの30~50%である請求項1から4のいずれか一に記載の垂直軸型風車。 The vertical axis wind turbine according to any one of claims 1 to 4, wherein a horizontal width of the blade support arm is 30 to 50% of a length in a rotation direction of the blade.
  6.  前記翼支持腕が上下二か所で翼を支持することで、翼支持腕と円筒状回転軸と翼とによって囲まれる整流窓が形成される請求項1から5のいずれか一に記載の垂直軸型風車。 The vertical direction according to any one of claims 1 to 5, wherein a rectifying window surrounded by the wing support arm, the cylindrical rotating shaft, and the wing is formed by the wing support arm supporting the wing at two upper and lower positions. Axial wind turbine.
  7.  前記翼と前記円筒状回転軸の間隔は、前記上下二か所の翼支持腕の間隔の略半分である請求項6に記載の垂直軸型風車。 The vertical axis wind turbine according to claim 6, wherein a distance between the blade and the cylindrical rotating shaft is substantially half of a distance between the blade support arms at the two upper and lower portions.
  8.  前記円筒状回転軸と軸を共有する発電機をさらに有する請求項1から7のいずれか一に記載の垂直軸型風車。 The vertical axis wind turbine according to any one of claims 1 to 7, further comprising a generator sharing an axis with the cylindrical rotating shaft.
PCT/JP2010/071336 2010-11-30 2010-11-30 Vertical shaft windmill WO2012073321A1 (en)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11927174B1 (en) * 2023-04-03 2024-03-12 Wind Harvest International Inc Vertical axis wind turbine blade-arm connection member

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Publication number Priority date Publication date Assignee Title
JP2003206848A (en) * 2001-11-09 2003-07-25 Tokai Univ Integrated wind and water turbine, and manufacturing method thereof
JP2006070761A (en) * 2004-08-31 2006-03-16 Daiwa House Ind Co Ltd Wind power generator
JP2006283713A (en) * 2005-04-04 2006-10-19 Daiwa House Ind Co Ltd Lift/drag combined type vertical shaft windmill
JP2009150319A (en) * 2007-12-20 2009-07-09 Sinfonia Technology Co Ltd Wind turbine vibration damping device, and wind turbine device

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2003206848A (en) * 2001-11-09 2003-07-25 Tokai Univ Integrated wind and water turbine, and manufacturing method thereof
JP2006070761A (en) * 2004-08-31 2006-03-16 Daiwa House Ind Co Ltd Wind power generator
JP2006283713A (en) * 2005-04-04 2006-10-19 Daiwa House Ind Co Ltd Lift/drag combined type vertical shaft windmill
JP2009150319A (en) * 2007-12-20 2009-07-09 Sinfonia Technology Co Ltd Wind turbine vibration damping device, and wind turbine device

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11927174B1 (en) * 2023-04-03 2024-03-12 Wind Harvest International Inc Vertical axis wind turbine blade-arm connection member

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