JPS6090992A - Spiral blade type vertical shaft windmill - Google Patents

Spiral blade type vertical shaft windmill

Info

Publication number
JPS6090992A
JPS6090992A JP19904783A JP19904783A JPS6090992A JP S6090992 A JPS6090992 A JP S6090992A JP 19904783 A JP19904783 A JP 19904783A JP 19904783 A JP19904783 A JP 19904783A JP S6090992 A JPS6090992 A JP S6090992A
Authority
JP
Japan
Prior art keywords
wind turbine
windmill
spiral
rotor
blade
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
JP19904783A
Other languages
Japanese (ja)
Inventor
Moriaki Tsukamoto
守昭 塚本
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hitachi Ltd
Original Assignee
Hitachi Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Hitachi Ltd filed Critical Hitachi Ltd
Priority to JP19904783A priority Critical patent/JPS6090992A/en
Publication of JPS6090992A publication Critical patent/JPS6090992A/en
Pending legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03D—WIND MOTORS
    • F03D3/00—Wind motors with rotation axis substantially perpendicular to the air flow entering the rotor 
    • F03D3/06—Rotors
    • F03D3/061—Rotors characterised by their aerodynamic shape, e.g. aerofoil profiles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00—Components
    • F05B2240/20—Rotors
    • F05B2240/21—Rotors for wind turbines
    • F05B2240/211—Rotors for wind turbines with vertical axis
    • F05B2240/213—Rotors for wind turbines with vertical axis of the Savonius type
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00—Components
    • F05B2240/20—Rotors
    • F05B2240/24—Rotors for turbines
    • F05B2240/243—Rotors for turbines of the Archimedes screw type
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2250/00—Geometry
    • F05B2250/10—Geometry two-dimensional
    • F05B2250/15—Geometry two-dimensional spiral
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2250/00—Geometry
    • F05B2250/20—Geometry three-dimensional
    • F05B2250/25—Geometry three-dimensional helical
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00—Energy generation through renewable energy sources
    • Y02E10/70—Wind energy
    • Y02E10/74—Wind turbines with rotation axis perpendicular to the wind direction

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Sustainable Energy (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Wind Motors (AREA)

Abstract

PURPOSE:To reduce torque fluctuation and drag fluctuation by forming rotor blades integrally with and spiral about the rotary shaft of the windmill. CONSTITUTION:The spiral rotor blades 11, 12 are arranged about the rotary shaft of the windmill, which connects the rotary shafts 16, 17, so as to be symmetrical to the shaft and so as to have the angles of twist of 180 deg.. The spiral rotor blades 11, 12 are fixed to respective end plates 13, 15 at the uppermost and lowermost section thereof. The ratio of areas of dynamic blade, receiving torque in a direction to rotate the windmill, and brake blade, receiving torque into the direction of braking, becomes constant independently from a rotating angle theta, therefore, there is little torque fluctuation. The area of projection of the windmill is also constant independently from the rotary angle theta and, therefore, the drag force, effecting on the whole of the windmill, will never be fluctuated substantially.

Description

【発明の詳細な説明】 〔発明の利用分野〕 本発明は垂直軸風車に係り%特に小形の風力発′亀装置
や風力ポンプ等に使用するに好適な垂直軸風車に関する
。
DETAILED DESCRIPTION OF THE INVENTION [Field of Application of the Invention] The present invention relates to a vertical axis wind turbine, and more particularly to a vertical axis wind turbine suitable for use in small wind turbine generators, wind pumps, and the like.

〔発明の背景〕[Background of the invention]

従来の垂直軸風車の代表的なものとして2枚または3枚
のロータ興奮もつサポニウス風車がある。
A typical example of a conventional vertical axis wind turbine is a Saponius wind turbine with two or three rotor excitations.

サポニウス風車は構造が簡単で起動性がよく、かつ風向
変化の影響が少ないなどの利点を有しているが、風車の
回転角θによりロータ真に対する風の作用程度が異なる
。そのため風車の回転角θによシ回転トルクが変動する
とともに、風車全体に作用する風の抗力も変動するので
風車の撮動が大きく、安定な運転が困難であるという欠
点金有していた。この欠点全改善する目的でなされた従
来の方法として、第1図に示すサボニウス風車(日本機
械学会、精機学会共催1日立地方講演会論文集、昭和5
3年9月]がある。この風車は第1図に示すようにサポ
ニウス風車全上下2段重ねとし、上段ロータR1と下段
ロータ翼2金回転角θ方向に90°ずらして配置したも
のである。なお、第1図の3,4及び5は端板、6及び
7は回転軸である。第2図には、第1図の風車の回転角
θに対する靜トルク係数Cmk放射方向にとった靜トル
ク分布を示す。同図よう、サボニウス風単金2段重ねと
しても静トルク係数Csの最大と最小は4個所に生じ、
かつ静トルク係1’l Csの最大値C6nと最小値C
st、の比Cgn/ C[ILは2以−ヒと大きく、回
転トルクの変動は十分小さくなっていない。この回転ト
ルクの変動を十分小さくするためには、さらに風車全1
0段以上の多段に重ねることが考えられるが、第1図の
構造では、多段化に際して以下の欠点を有している。(
1)各段を接続するために中間の端板4が必要であシ、
風車重量の増加とともに回転時の抵抗となり、コスト會
増加させるとともに風車効率を低下させる。(2)各段
の接続に際して、各段間の回転中心がくるいやすく、振
動の原因となる。(3)各段接続部の中間の端板4によ
り、各段間の空気の流れが防げられ、風車効率が低下す
る。
Saponius wind turbines have advantages such as a simple structure, good startup performance, and little influence from changes in wind direction, but the degree of wind action on the rotor stem differs depending on the rotation angle θ of the wind turbine. For this reason, the rotational torque varies depending on the rotation angle θ of the windmill, and the drag force of the wind acting on the entire windmill also varies, so the windmill has to be photographed extensively, making stable operation difficult. As a conventional method aimed at alleviating this drawback, the Savonius windmill shown in Fig.
September 3rd]. As shown in FIG. 1, this wind turbine has two upper and lower Saponius wind turbines stacked one on top of the other, and the upper rotor R1 and the lower rotor blades are arranged 90 degrees apart in the gold rotation angle θ direction. In addition, 3, 4 and 5 in FIG. 1 are end plates, and 6 and 7 are rotating shafts. FIG. 2 shows the quiet torque distribution taken in the radial direction of the quiet torque coefficient Cmk with respect to the rotation angle θ of the wind turbine shown in FIG. As shown in the figure, the maximum and minimum of the static torque coefficient Cs occur at four locations even when two layers of Savonius-style single metal are stacked,
and the maximum value C6n and minimum value C of static torque coefficient 1'l Cs
The ratio Cgn/C[IL of st, is as large as 2 or more, and the variation in rotational torque is not sufficiently small. In order to sufficiently reduce this variation in rotational torque, it is necessary to
It is conceivable to stack them in 0 or more stages, but the structure shown in FIG. 1 has the following drawbacks when multi-staged. (
1) An intermediate end plate 4 is required to connect each stage,
As the weight of the wind turbine increases, it becomes a resistance during rotation, increasing costs and reducing the efficiency of the wind turbine. (2) When connecting each stage, the center of rotation between each stage is likely to be twisted, causing vibration. (3) The end plate 4 in the middle of each stage connection part prevents air flow between each stage, reducing wind turbine efficiency.

〔発明の目的〕 本発明の目的は、上記した従来技術の欠点をなくシ、垂
直軸風車?多段に構成することなくトルク変動及び抗力
変動が小さく、かつ風車効率の高い垂直軸風車を提供す
ることにある。
[Object of the Invention] An object of the present invention is to eliminate the above-mentioned drawbacks of the prior art and to create a vertical axis wind turbine. It is an object of the present invention to provide a vertical axis wind turbine that has small torque fluctuations and drag fluctuations without having to be constructed in multiple stages, and has high wind turbine efficiency.

〔発明の概要〕[Summary of the invention]

上記の目的全達成するため本発明では、ロータ翼を風車
回転軸まわりに螺旋状に一体成形したロータ野としてい
る。このとき、この螺旋状ロータ翼のひねり角αは、風
車ロータ翼枚数をNとしたとき。
In order to achieve all of the above objects, the present invention employs a rotor field in which the rotor blades are integrally molded in a spiral shape around the rotation axis of the wind turbine. At this time, the twist angle α of this spiral rotor blade is when the number of wind turbine rotor blades is N.

ただし、nは正の整数 としている。このことよシ、風車の回転角θによらず、
N枚の螺旋状ロータ翼に作用する回転トルク及び風車全
体に作用する抗力は一定となり、振動の少ない安定な運
転が可能となる。また螺旋状ロータ興に入射後の風は、
その一部が螺旋状ロータ諷に沿って流れ、風車の回転を
助ける方向に作用す、るので、風車効率金高めることが
できる。
However, n is a positive integer. This means that regardless of the rotation angle θ of the wind turbine,
The rotational torque acting on the N helical rotor blades and the drag force acting on the entire wind turbine are constant, allowing stable operation with less vibration. In addition, the wind after entering the spiral rotor is
A part of it flows along the helical rotor and acts in a direction that helps the rotation of the windmill, thereby increasing the efficiency of the windmill.

〔発明の実施例〕[Embodiments of the invention]

以下本発明全実施例により詳細に説明する。第3図は本
発明の螺旋翼式垂直軸風車の一実施例を示す構造図であ
る。また、第4図は、第3図のA−A断面、B−B断面
、C−C断面、D−D断面。
The present invention will be explained in detail below with reference to all embodiments. FIG. 3 is a structural diagram showing an embodiment of the spiral blade type vertical axis wind turbine of the present invention. Moreover, FIG. 4 is an AA cross section, a B-B cross section, a C-C cross section, and a D-D cross section of FIG.

及びE−E断面を示す断面図である。第3図において、
11.12は一対の螺旋状ロータ其、13゜15はそれ
ぞれ上部及び下部端板、16.17は回転軸である。2
枚の螺旋状ロータ翼11,12は回転軸16.l’l結
ぶ風車回転軸まわりにそれぞれ180°のひねシ角α金
持ち、かつその風車回転軸に軸対称に配置されている。
FIG. In Figure 3,
Reference numerals 11 and 12 indicate a pair of helical rotors, 13° and 15 indicate upper and lower end plates, respectively, and 16 and 17 indicate a rotating shaft. 2
The spiral rotor blades 11 and 12 are connected to a rotating shaft 16. They each have a twist angle α of 180° around the wind turbine rotation axis, and are arranged axially symmetrically to the wind turbine rotation axis.

この2枚の螺旋状ロータ翼11,12は上部及び下部で
それぞれ端板13,15に固定されている。回転軸16
゜17はそれぞれ端板13,15に固定されている。
The two helical rotor blades 11 and 12 are fixed to end plates 13 and 15 at the upper and lower parts, respectively. Rotating shaft 16
17 are fixed to the end plates 13 and 15, respectively.

第1図の風車の軸方向各点の断面は、第4図に示すよう
に、最上部のA−A断面形状が1800回転して最下部
のE−E断面形状となる。
As shown in FIG. 4, the cross section at each point in the axial direction of the wind turbine in FIG. 1 is such that the top A-A cross section is rotated 1800 times to become the bottom E-E cross section.

螺旋状ロータ翼の材質は、軽量でかつ強度の高いERP
′fr:使用しているが、アルミ合金等でも可能である
。
The material of the spiral rotor blades is ERP, which is lightweight and has high strength.
'fr: Although used, aluminum alloy etc. can also be used.

以下1本発明の螺旋翼垂直軸風車の動作特性を説明する
。第5図は第3図の風車の回転角θに対する靜トルク係
数C111に放射方向にとった静トルク分布の測定値で
ある。ここで静トルク係数Csは、次式で表わされる。
The operating characteristics of the helical blade vertical axis wind turbine of the present invention will be explained below. FIG. 5 shows measured values of the static torque distribution taken in the radial direction of the quiet torque coefficient C111 with respect to the rotation angle θ of the wind turbine in FIG. Here, the static torque coefficient Cs is expressed by the following equation.

ただし、 Os =静トルク係数 TB=静トルク ρ=空気密度 U=風速 As =風車投影面積(Asが回転角θによって変わる
場合は、その最大値をと る) R=風車回転半径 第5図よシ、静トルク係数C−は回転角θによらず、1
1は一定となる。これは、風を受けて風車を回転させる
方向にトルク受ける動力具21(第5図)と逆に、制動
する方向にトルクを受ける制動翼22(第5図)の面積
の割合が、本発明の螺旋翼式垂直軸風車では回転角θに
よらず一定となるlめでちゃ、トルク変動のほとんどな
い安定な運転が可能である。また、本風車では風車の投
影面積もjQ1転角θによらず一定であり、風速がほぼ
一定であれば風車全体に作用する抗力もほとんど変動せ
ず安定な運転が可能である。さらに、靜トルクが回転角
θによらないことから、風車停止時にどららの方向から
風が吹いてもすみやかに起動可能である。
However, Os = Static torque coefficient TB = Static torque ρ = Air density U = Wind speed As = Wind turbine projected area (if As changes depending on the rotation angle θ, take its maximum value) R = Wind turbine rotation radius , the static torque coefficient C- is 1 regardless of the rotation angle θ.
1 is constant. This means that the proportion of the area of the brake vane 22 (Fig. 5), which receives torque in the direction of braking, as opposed to the power tool 21 (Fig. 5), which receives torque in the direction of rotating the wind turbine due to the wind, is In the spiral blade type vertical axis wind turbine, the torque is constant regardless of the rotation angle θ, and stable operation with almost no torque fluctuation is possible. In addition, in this windmill, the projected area of the windmill is also constant regardless of the jQ1 rotation angle θ, and if the wind speed is approximately constant, the drag force acting on the entire windmill hardly changes and stable operation is possible. Furthermore, since the quiet torque does not depend on the rotation angle θ, the wind turbine can be started quickly even if the wind blows from any direction when the wind turbine is stopped.

通常、自然風はたえずその風向が変動する。この風向変
動時、従来の第1図に示す風車では風向に対する相対的
な回転角が変動するこ七により、トルク及び抗力が変動
し、風向の変動も振動の原因となる。一方1本発明の第
3図の風車では、風向が変動してもトルク及び抗力il
:変動しないので、風向変動に対しても安定に運転でき
る。
Normally, natural wind constantly changes its direction. When the wind direction fluctuates, in the conventional wind turbine shown in FIG. 1, the rotation angle relative to the wind direction fluctuates, causing torque and drag to fluctuate, and the wind direction fluctuation also causes vibration. On the other hand, in the wind turbine of the present invention shown in FIG. 3, even if the wind direction changes, the torque and drag force
: Since it does not fluctuate, it can operate stably even when the wind direction fluctuates.

第6図は本発明の第3図に示した風車の出力特性を第1
図の従来の風車に比較して示したものである。第6図に
おいて縦軸は風車出力係数CP。
Figure 6 shows the output characteristics of the wind turbine shown in Figure 3 of the present invention.
This is a comparison with the conventional wind turbine shown in the figure. In Fig. 6, the vertical axis is the wind turbine output coefficient CP.

横軸は周速比φである。ここで、風車出力係数Cpと周
速比φは次式で定義される量である。
The horizontal axis is the peripheral speed ratio φ. Here, the wind turbine output coefficient Cp and the circumferential speed ratio φ are quantities defined by the following equation.

ただし、 Cp”風車出力係数 P=風車出力 ρ=空気密度 U=風速 AR−風車投影面積 φ=周速比 R=風車回転半径 W=風車回転角速度 第6図において、黒丸で示した31は第1図の従来の風
車の出力特性、白丸で示した32は第3図の本発明の風
車の出力特性の代表例である。第6図よシ2本発明の風
車の出力特性31は、従来の風車の出力特性32に比較
して最大出力係数Cpは10%以上大きくなシ、かつ出
力係数CPの大きい周速比範囲も広くなっている。この
理由は、第1図の従来の風車と第3図の本発明の風車の
ロータ翼形状の差異によるものである。すなわち、第1
図の従来の風車のロータ翼1及び2は長さ方向に直線状
であり、かつ上段ロータ翼1と下段ロータ翼2は端板4
で仕切られている。そのため、動力翼、例えばロータ翼
2の腹部に入射した風は、その一部はロータ興2の後縁
部を通って制御翼(ロータ翼2と対をなすもう1枚のロ
ータ翼)の腹部へ逃げ、他の一部の風は動力翼の前縁部
から逃けるが、上下方向へはロータ翼が垂直であること
や端板4等によシ逃げに<<、制動翼に負のトルク全付
加するように作用する。そのため風車の出力係数が低下
する。
However, Cp'' Wind turbine output coefficient P = Wind turbine output ρ = Air density U = Wind speed AR - Wind turbine projected area φ = Circumferential speed ratio R = Wind turbine rotation radius W = Wind turbine rotation angular speed In Fig. 6, 31 indicated by a black circle is The output characteristics of the conventional wind turbine in Figure 1 and 32 indicated by white circles are representative examples of the output characteristics of the wind turbine of the present invention in Figure 3.The output characteristics 31 of the wind turbine of the present invention in Figure 6 Compared to the output characteristic 32 of the wind turbine shown in Fig. 1, the maximum output coefficient Cp is larger by more than 10%, and the circumferential speed ratio range in which the output coefficient CP is large is also wider. This is due to the difference in the shape of the rotor blades of the wind turbine of the present invention shown in FIG.
The rotor blades 1 and 2 of the conventional wind turbine shown in the figure are straight in the length direction, and the upper rotor blade 1 and the lower rotor blade 2 have an end plate 4.
It is separated by Therefore, a part of the wind that enters the abdomen of the power blade, for example, the rotor blade 2, passes through the trailing edge of the rotor blade 2 and passes through the abdomen of the control blade (another rotor blade paired with the rotor blade 2). Some of the other wind escapes from the leading edge of the power blade, but in the vertical direction, the rotor blade is vertical, the end plate 4, etc. causes a negative flow to the brake blade. Acts to add full torque. Therefore, the output coefficient of the wind turbine decreases.

一方、本発明の風車では第3図に示すように、ロータ翼
11,12がなめらかな螺旋状に構成されている。その
ため、本発明では1枚のロータ翼の中に動力翼として働
く部分と制動翼として働く部分があり、動力興と制動翼
の明確な区別は困難であるが、風車軸方向のおる断面で
見れば、ロータ翼11が動力翼として働く場合には、も
う一枚のロータ翼12は制動翼として働くことになる。
On the other hand, in the wind turbine of the present invention, as shown in FIG. 3, the rotor blades 11 and 12 are configured in a smooth spiral shape. Therefore, in the present invention, one rotor blade has a part that works as a power blade and a part that works as a brake blade, and although it is difficult to clearly distinguish between the power blade and the brake blade, it is difficult to clearly distinguish between the power blade and the brake blade. For example, when the rotor blade 11 works as a power blade, the other rotor blade 12 works as a brake blade.

したがって本発明の風車の動力翼部分に入射した風は、
従来の風車の場合と同様に、その一部の風は動力翼の後
縁部を通って制動翼の膜部へ逃げ、他の一部の風は動力
翼の前縁部から逃げる。さらに本発明の風車ではロータ
翼がなめらかな螺旋状に構成されていることにより、動
力翼部分に入射した風のかなシの部分が、螺旋状のロー
タ翼に沿って逃げることになり、この逃げる風も風車に
回転トルクを与える方向に作用する。
Therefore, the wind incident on the power blade portion of the wind turbine of the present invention is
As in conventional wind turbines, some of the wind escapes through the trailing edge of the power vane to the brake blade membrane, and some of the wind escapes through the leading edge of the power vane. Furthermore, in the wind turbine of the present invention, since the rotor blades are configured in a smooth spiral shape, a portion of the wind that is incident on the power blade portion escapes along the spiral rotor blade. Wind also acts in a direction that provides rotational torque to the windmill.

さらに、制動翼部背部にある風もロータ翼の螺旋に沿っ
て逃げ、動力翼部の腹部に入射して風車に回転トルクを
与える方向に作用する風が従来の直線状のロータ翼をも
つ風車に比較して多くなる。
Furthermore, the wind at the back of the brake blade also escapes along the spiral of the rotor blade, enters the abdomen of the power blade, and acts in the direction of giving rotational torque to the wind turbine. It becomes more compared to .

これらの効果によシ、本発明の風車の出力係数Cse高
くすることができる。
Due to these effects, the output coefficient Cse of the wind turbine of the present invention can be increased.

第7図は本発明の他の実施例を示すもので、第3図と異
なるのは、螺旋状ロータ興奮41のみの1枚としたこと
である。このときは螺旋のひねシ角αは360°として
いる。この実施例では、ロータ翼の枚数が少ないことに
よシ回転トルクは小さくなるが、高速回転可能となシ、
発電等の用途に適するという効果がある。
FIG. 7 shows another embodiment of the present invention, which differs from FIG. 3 in that only one helical rotor excitation 41 is used. At this time, the twist angle α of the spiral is 360°. In this embodiment, the rotational torque is small due to the small number of rotor blades, but the rotor can rotate at high speed.
It has the effect of being suitable for uses such as power generation.

第8図は、本発明の他の実施例を示すもので、第3図と
異なるのはジャイロミル形風車に螺旋状ロータ翼を取9
つけだことである。第8図において、51及び52は螺
旋状ロータ翼であシ、それぞれのロータ翼51及び52
のひねり角αは1800である。この1対のロータ翼5
1,52は回転軸53に54.55,56,57,58
゜59.60.61の各支持棒により固定されている。
FIG. 8 shows another embodiment of the present invention, which differs from FIG.
That's a given. In FIG. 8, 51 and 52 are spiral rotor blades.
The twist angle α is 1800. This pair of rotor blades 5
1, 52 are 54, 55, 56, 57, 58 on the rotating shaft 53
It is fixed by support rods of 59, 60 and 61 degrees.

第8図のF−F断面を第9図に示す。ロータ翼51,5
2の断面形状は、第9図に示すように翼形をしておシ、
この翼形としてはNACAOO12形などが適当である
。
FIG. 9 shows a cross section taken along line FF in FIG. 8. Rotor blades 51,5
The cross-sectional shape of No. 2 is airfoil-shaped as shown in Fig. 9.
A suitable airfoil shape is NACAOO12 type.

ジャイロミル形風車は前に説明したサポニウス風車とは
異なった空力作用によシ回転する。すなわち、サボニウ
ス風車ではロータ翼の動力翼部と制動翼部にそれぞれ作
用する風の抗力の差によシトルクを得て回転する。一方
、ジャイロミル形風車では断面が翼形全したロータ典に
作用する揚力によってトルクを得て回転する。しかし、
ジャイロミル形風車においても風車の回転角θによりロ
ータ翼に作用する揚力の大きさ及び方向が変化し、トル
ク変動を避けることができない。第9図でロータ翼の位
置が回転角θ=90°、270°のとき最小揚力を受け
、θ=0°、180°のとき最大揚力を受ける。しかし
、第8図に示した本実施例のごとく、ロータJ!l!!
を螺旋状とすることによ勺ロータ翼に作用するトルク変
動の位置を分散させることにより風車全体に作用するト
ルク変動を小さくすることができ、振動の少ない安定し
た運転が可能となる。
Gyromill type windmills rotate by aerodynamic forces that are different from the Saponius windmills described previously. In other words, the Savonius wind turbine rotates by obtaining a torque due to the difference in wind drag acting on the power vane and brake vane of the rotor blade. On the other hand, a gyro mill type wind turbine rotates by obtaining torque from the lift force acting on the rotor, which has an airfoil-shaped cross section. but,
Even in a gyro mill type wind turbine, the magnitude and direction of lift acting on the rotor blades change depending on the rotation angle θ of the wind turbine, and torque fluctuations cannot be avoided. In FIG. 9, the rotor blade receives minimum lift when the rotation angle θ=90° and 270°, and receives maximum lift when θ=0° and 180°. However, as in this embodiment shown in FIG. 8, the rotor J! l! !
By making the wind turbine spiral, the positions of torque fluctuations acting on the rotor blades are dispersed, thereby making it possible to reduce torque fluctuations acting on the entire wind turbine, allowing stable operation with less vibration.

なお1以上説明した実施例では、螺旋状ロータ翼のひね
シ角αは、ロータ翼枚数が1枚のときにはα=360°
、ロータ翼枚数が2枚のときはα=180°としたが、
一般にロータ具枚数ff:N、正の整数fnとしたとき
1次式で表わされるひね9角αとすれば、同様の効果が
得られる。
In the embodiment described above, the twist angle α of the helical rotor blade is α=360° when the number of rotor blades is one.
, when the number of rotor blades is two, α = 180°, but
Generally, when the number of rotor members ff is N and a positive integer fn, the same effect can be obtained by setting the twist angle α to be expressed by a linear equation.

また、螺旋の方向は右ねじ方向でも、左ねじ方向でもよ
い。
Further, the direction of the spiral may be a right-handed thread direction or a left-handed thread direction.

〔発明の効果〕〔Effect of the invention〕

以上説明したごとく、本発明によれば、風車のロータ興
奮回転軸まわりに螺旋状に構成することによシ、トルク
変動及び抗力変動がほとんどなくなシ、振動の少ない安
定した運転が可能となるとともに風車の効率を高めるこ
とができる。
As explained above, according to the present invention, by configuring the rotor of a wind turbine in a spiral around the excited rotation axis, torque fluctuations and drag fluctuations are almost eliminated, and stable operation with less vibration is possible. At the same time, the efficiency of the wind turbine can be increased.

【図面の簡単な説明】[Brief explanation of drawings]

第1図は従来の2段式すポニウス風車の構造図、第2図
は第1図の風車の静トルク特性を示す説明図、第3図は
本発明の風車の一実施例を示す構造図、第4図は第3図
の風車の軸方同各位置のロータ翼形状金示す断面図%第
5図は第3図に示した本発明の風車の靜トルク特性を示
す説明図、第6図は第1図の風車と第3図の風車の出力
特性を示す説明図、第7図社本発明の風車の変形例を示
す構造図、第8図は本発明の風車の他の変形例を示す構
造図、第9図は第8図の風車のF−15断面図である。 1・・・上段ロータ翼、2・・・下段ロータ翼、3,4
゜5・・・端板、6,7・・・回転軸、11.12・・
・螺旋状ロータ翼、13.15・・・端板、16.17
・・・回転軸、41・・・螺旋状ロータ翼% 42.4
3・・・端板、44.45・・・回転軸%5’l、52
・・・螺旋状ロータR153・・・回転軸% 54,5
5,56,57゜58.59,60.61・・・支持棒
、α・・・螺旋状ロータ翼のO・ねシ角、θ・・・風車
の回転角408・・・靜トルク係数、Cp・・・風車出
力係数、N・・・ロータ翼270゜ p(、!Ty−) 茅7霞
Fig. 1 is a structural diagram of a conventional two-stage Sponius wind turbine, Fig. 2 is an explanatory diagram showing the static torque characteristics of the wind turbine in Fig. 1, and Fig. 3 is a structural diagram showing an embodiment of the wind turbine of the present invention. , FIG. 4 is a cross-sectional view showing the shape of the rotor blade at each axial position of the wind turbine shown in FIG. 3, FIG. The figures are an explanatory diagram showing the output characteristics of the wind turbine in Fig. 1 and the wind turbine in Fig. 3, Fig. 7 is a structural diagram showing a modification of the wind turbine of the present invention, and Fig. 8 is another modification of the wind turbine of the invention. FIG. 9 is a cross-sectional view taken along F-15 of the wind turbine shown in FIG. 8. 1... Upper rotor blade, 2... Lower rotor blade, 3, 4
゜5... End plate, 6, 7... Rotating shaft, 11.12...
・Spiral rotor blade, 13.15... End plate, 16.17
... Rotating shaft, 41 ... Spiral rotor blade % 42.4
3... End plate, 44.45... Rotating axis %5'l, 52
...Spiral rotor R153...Rotating axis% 54,5
5,56,57゜58.59,60.61...Support rod, α...O-helix angle of spiral rotor blade, θ...Rotation angle of wind turbine 408...Silent torque coefficient, Cp... Wind turbine output coefficient, N... Rotor blade 270゜p (,!Ty-) Chi7 Haze

Claims (1)

【特許請求の範囲】 1、垂直に配置された回転軸と%該回転軸に、脱絖され
た1枚以上のロータ翼とより成る垂直軸風車において、
該ロータJKを該回転軸重わりに螺旋状にひねった螺旋
状ロータ翼としたこと’41徴とする螺旋具式垂直軸風
車。 2、特許請求の範囲第1項において、該ロータ翼枚数を
N1正の整数をnで表わしたとき、該螺旋状ロータ翼の
ひねシ角αを、 360゜ としたことを特徴とする螺旋具式垂直軸風車。
[Claims] 1. A vertical axis wind turbine comprising a vertically arranged rotating shaft and one or more unscrewed rotor blades on the rotating shaft,
A spiral gear type vertical axis wind turbine characterized in that the rotor JK is a spiral rotor blade twisted spirally around the rotating shaft. 2. A spiral tool according to claim 1, characterized in that the helical rotor blade has a twist angle α of 360°, where N1 is a positive integer representing the number of rotor blades. vertical axis windmill.
JP19904783A 1983-10-26 1983-10-26 Spiral blade type vertical shaft windmill Pending JPS6090992A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP19904783A JPS6090992A (en) 1983-10-26 1983-10-26 Spiral blade type vertical shaft windmill

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP19904783A JPS6090992A (en) 1983-10-26 1983-10-26 Spiral blade type vertical shaft windmill

Publications (1)

Publication Number Publication Date
JPS6090992A true JPS6090992A (en) 1985-05-22

Family

ID=16401225

Family Applications (1)

Application Number Title Priority Date Filing Date
JP19904783A Pending JPS6090992A (en) 1983-10-26 1983-10-26 Spiral blade type vertical shaft windmill

Country Status (1)

Country Link
JP (1) JPS6090992A (en)

Cited By (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4718821A (en) * 1986-06-04 1988-01-12 Clancy Brian D Windmill blade
JPH06156702A (en) * 1992-11-20 1994-06-03 Ichikoo:Kk Vertical carrying device
US6428275B1 (en) 1997-06-30 2002-08-06 Shield Oy Helical wind rotor and a method for manufacturing the same
DE10227404A1 (en) * 2002-06-20 2004-01-15 Krüger, Wolfgang Drive rotor for vertical motion wind power systems has blade with flat wave profile that is twisted in longitudinal direction with flat pitch angle with zigzag or sinusoidal normal function profile
WO2004067957A1 (en) * 2003-01-30 2004-08-12 Flucon As A screw turbine device
EP1519011A1 (en) * 2003-09-24 2005-03-30 Roll Power LLC Electric power generator driven by the draft of passing vehicles
US7132760B2 (en) 2002-07-31 2006-11-07 Becker William S Wind turbine device
WO2007079974A1 (en) * 2005-12-29 2007-07-19 Georg Hamann Device and system for producing regenerative and renewable energy from wind
JP2008019762A (en) * 2006-07-12 2008-01-31 Matsushita Electric Ind Co Ltd Savonius windmill
US7362004B2 (en) 2003-07-29 2008-04-22 Becker William S Wind turbine device
WO2008157174A1 (en) * 2007-06-13 2008-12-24 Skyron Systems, Inc. Wind turbine blade
WO2009099683A3 (en) * 2008-02-01 2009-10-08 Windside America Fluid rotor
ITCO20090026A1 (en) * 2009-07-28 2011-01-28 Windesign S R L "HYBRID TURBINE WITH VERTICAL TREE FOR ELECTRIC ENERGY GENERATORS"
WO2011033348A3 (en) * 2009-09-18 2011-08-04 Urban Green Energy, Inc. Vertical axis wind turbine and its wind rotor
EP2464859A4 (en) * 2009-08-20 2013-04-17 Windworks Engineering Ltd A blade assembly for a wind turbine
ITPD20120126A1 (en) * 2012-04-23 2013-10-24 Vortex Energy S R L PERFECT STRUCTURE OF WIND OR HYDRAULIC TURBINE WITH VERTICAL AXIS
CN106545466A (en) * 2016-12-07 2017-03-29 上海理工大学 A kind of resistance-type vertical axis wind turbine

Cited By (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4718821A (en) * 1986-06-04 1988-01-12 Clancy Brian D Windmill blade
JPH06156702A (en) * 1992-11-20 1994-06-03 Ichikoo:Kk Vertical carrying device
US6428275B1 (en) 1997-06-30 2002-08-06 Shield Oy Helical wind rotor and a method for manufacturing the same
DE10227404A1 (en) * 2002-06-20 2004-01-15 Krüger, Wolfgang Drive rotor for vertical motion wind power systems has blade with flat wave profile that is twisted in longitudinal direction with flat pitch angle with zigzag or sinusoidal normal function profile
DE10227404B4 (en) * 2002-06-20 2008-05-21 Krüger, Wolfgang Drive rotor for vertically running wind turbines
US7132760B2 (en) 2002-07-31 2006-11-07 Becker William S Wind turbine device
WO2004067957A1 (en) * 2003-01-30 2004-08-12 Flucon As A screw turbine device
US7362004B2 (en) 2003-07-29 2008-04-22 Becker William S Wind turbine device
EP1519011A1 (en) * 2003-09-24 2005-03-30 Roll Power LLC Electric power generator driven by the draft of passing vehicles
WO2007079974A1 (en) * 2005-12-29 2007-07-19 Georg Hamann Device and system for producing regenerative and renewable energy from wind
JP2008019762A (en) * 2006-07-12 2008-01-31 Matsushita Electric Ind Co Ltd Savonius windmill
WO2008157174A1 (en) * 2007-06-13 2008-12-24 Skyron Systems, Inc. Wind turbine blade
WO2009099683A3 (en) * 2008-02-01 2009-10-08 Windside America Fluid rotor
US8087897B2 (en) 2008-02-01 2012-01-03 Windside America Fluid rotor
ITCO20090026A1 (en) * 2009-07-28 2011-01-28 Windesign S R L "HYBRID TURBINE WITH VERTICAL TREE FOR ELECTRIC ENERGY GENERATORS"
WO2011012970A1 (en) * 2009-07-28 2011-02-03 Windesign S.R.L. Hybrid type vertical shaft turbine for wind power generating devices
EP2464859A4 (en) * 2009-08-20 2013-04-17 Windworks Engineering Ltd A blade assembly for a wind turbine
WO2011033348A3 (en) * 2009-09-18 2011-08-04 Urban Green Energy, Inc. Vertical axis wind turbine and its wind rotor
US9243611B2 (en) 2009-09-18 2016-01-26 Hanjun Song Vertical axis wind turbine blade and its wind rotor
ITPD20120126A1 (en) * 2012-04-23 2013-10-24 Vortex Energy S R L PERFECT STRUCTURE OF WIND OR HYDRAULIC TURBINE WITH VERTICAL AXIS
CN106545466A (en) * 2016-12-07 2017-03-29 上海理工大学 A kind of resistance-type vertical axis wind turbine

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