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JPS5993971A - Turbine for collecting kinetic fluid energy, particularly, wind force energy - Google Patents

Turbine for collecting kinetic fluid energy, particularly, wind force energy

Info

Publication number
JPS5993971A
JPS5993971A JP58201850A JP20185083A JPS5993971A JP S5993971 A JPS5993971 A JP S5993971A JP 58201850 A JP58201850 A JP 58201850A JP 20185083 A JP20185083 A JP 20185083A JP S5993971 A JPS5993971 A JP S5993971A
Authority
JP
Japan
Prior art keywords
turbine
wing
energy
blades
section
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
JP58201850A
Other languages
Japanese (ja)
Inventor
ルイ・エル・ルポワ
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of JPS5993971A publication Critical patent/JPS5993971A/en
Pending legal-status Critical Current

Links

Classifications

    • 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
    • F03D7/00Controlling wind motors 
    • F03D7/06Controlling wind motors  the wind motors having rotation axis substantially perpendicular to the air flow entering the rotor
    • 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
    • F03D3/061Rotors characterised by their aerodynamic shape, e.g. aerofoil profiles
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00Components
    • F05B2240/20Rotors
    • F05B2240/21Rotors for wind turbines
    • F05B2240/211Rotors for wind turbines with vertical axis
    • F05B2240/212Rotors for wind turbines with vertical axis of the Darrieus type
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00Components
    • F05B2240/20Rotors
    • F05B2240/21Rotors for wind turbines
    • F05B2240/211Rotors for wind turbines with vertical axis
    • F05B2240/213Rotors for wind turbines with vertical axis of the Savonius type
    • 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
    • Y02E10/72Wind turbines with rotation axis in wind direction
    • 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

Landscapes

  • Engineering & Computer Science (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)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Wind Motors (AREA)

Abstract

(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。
(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

【発明の詳細な説明】 本発明はエネルギー収集装置、特に風力タービンの分野
に係り、運動流体エネルギー、特に風力エネルギーの収
集用タービンを目的とする。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to the field of energy harvesting devices, particularly wind turbines, and is directed to turbines for harvesting kinetic fluid energy, especially wind energy.

実際に様々のタイプの風力エネルギー収集装置が存在し
ているが、これらの装置は翼を備えるタービンとして構
成され、前記翼は軸に取付けられ空気通路を介して相互
に連結されるか或いは連結されない。
Various types of wind energy harvesting devices exist in practice, which are constructed as turbines with blades, which are either mounted on a shaft and interconnected via air passages, or not. .

これらの公知のタービンによりある程度の結果が得られ
ているが、その形状のために効率が低い。
Although some results have been obtained with these known turbines, their efficiency is low due to their geometry.

実際、これらのタービンの翼は一般に、該翼内への流体
入口断面に対応するように偏位させて組合わせられ回転
軸に取付けられた半円筒形表面によって構成されるので
、翼の有効容積は所与の翼断面に対して比較的大きく、
その抵抗係数は大きい。
In fact, the blades of these turbines are generally constituted by semi-cylindrical surfaces mounted on a rotating shaft and offset to correspond to the fluid inlet cross-section into the blade, so that the effective volume of the blade is is relatively large for a given wing cross section,
Its drag coefficient is large.

本発明の目的は上記の欠点を解消することである。The aim of the invention is to overcome the above-mentioned drawbacks.

実際に本発明の目的は運動流体エネルギー、特に風力エ
ネルギーの収集用タナビンを提供することであり、この
タービンは主に回転軸に固着された2枚組の翼から構成
、され、これらの翼は前記回転軸について対称を成し、
それぞれ好ましくは180°よりやや小さい中心角度に
伸びた双曲線状水平断面と、投影面がほぼ楕円形状の鉛
直断面とを有し、これらの翼は、2個の三日月形開口部
を形成するように接合面のレベルで偏位させて相互に組
合わせられており、該開口部の端部は断面間の各接合点
で半円形断面の通路を形成すべく狭窄している。
In fact, the object of the invention is to provide a turbine for the collection of kinetic fluid energy, in particular wind energy, which turbine consists mainly of two sets of blades fixed to a rotating shaft, these blades being symmetrical about the axis of rotation,
Each wing has a hyperbolic horizontal section extending at a central angle of preferably slightly less than 180° and a vertical section whose projection plane is approximately elliptical, the wings being shaped so as to form two crescent-shaped openings. They are offset from one another at the level of the joint surfaces, and the ends of the openings are constricted at each junction between the sections to form a passageway of semi-circular cross section.

本発明は、添附図面について以下に述べられる非限定的
な好ましい具体例に関する記載によって、更に理解され
よう。
The invention will be further understood by the description of preferred non-limiting embodiments set forth below with reference to the accompanying drawings, in which: FIG.

本発明に従うと、例示として特に第1図及び第2図に示
すように、運動流体エネルギー、特に風力エネルギーの
収集用タービンは、主に回転軸2に固着され該軸2につ
いて対称形を成す2枚組の翼1から構成される。
According to the invention, as shown by way of example and in particular in FIGS. 1 and 2, a turbine for the collection of kinetic fluid energy, in particular wind energy, is primarily attached to a rotating shaft 2 and having a symmetrical shape about said axis 2. It is composed of a set of blades 1.

各界1は、好ましくは180°よりやや小さい中心角度
に伸びた双曲線状水平断面(第2図)と、投影面がほぼ
楕円形状である鉛直断面とを有する。
Each field 1 preferably has a hyperbolic horizontal section (FIG. 2) extending at a central angle of slightly less than 180° and a vertical section whose projection plane is approximately elliptical.

これらの翼1は、2個の三日月形開口部3を形成するよ
うに接合面のレベルで偏位させて相互に組合わせられて
おり、該開口部の各々の端部はそれぞれ断面半円形状の
通路を形成する狭窄部4を有し、この通路は翼1により
画成される容積の内部に開口する。
These wings 1 are assembled to each other offset at the level of the joint surfaces so as to form two crescent-shaped openings 3, each end of which has a semicircular cross-section. It has a constriction 4 forming a passageway which opens into the interior of the volume defined by the wings 1.

このようにして得られるタービンは、数学的曲線、即ち
円形または楕円形のアセンブリによって構成され、従っ
て非常に空気力学的な形状の翼が得られ、効率も向上す
る。
The turbines obtained in this way are constructed by mathematical curves, i.e. circular or elliptical assemblies, thus resulting in highly aerodynamically shaped blades and also increased efficiency.

本発明の特徴に従うと、各界1の内側表面は、タービン
内の運動流体の速度を増加すべく、内側に向って連続的
に狭窄している。
According to a feature of the invention, the inner surface of each field 1 is continuously constricted inwardly to increase the velocity of the moving fluid within the turbine.

各界1は、好ましくは1806よりやや小さい中心角度
の表面部分に伸びた水平断面を有する双曲線状の螺旋部
分によって構成されるので、タービンの内部に収容され
た流体は正確に排出され得る。
Each field 1 is preferably constituted by a hyperbolic helical section with a horizontal section extending to a surface section with a central angle slightly smaller than 1806, so that the fluid contained inside the turbine can be evacuated precisely.

更に第3図に示すように、翼1は18o°の角度まで伸
びていないので、一方の翼1の軸2がら遠い端部を通る
面と他方の翼1の軸2の側の端部この間の角が鋭角を成
し、従ってタービンの流体出口内に於ける空気の流通が
促進される。
Further, as shown in FIG. 3, since the blades 1 do not extend to an angle of 18°, there is a gap between the plane passing through the end of one blade 1 far from the axis 2 and the end of the other blade 1 on the side of the axis 2. The corners are acute, thus promoting air flow within the fluid outlet of the turbine.

本発明の変形具体例(図示せず)に従うと、180’の
中心角度で伸びる翼を有するタービンを形成することも
可能である。
According to a variant embodiment of the invention (not shown), it is also possible to form a turbine with blades extending at a center angle of 180'.

更に本発明に従うターどンは、同じ寸法で同じ型の既存
のタービンに比べて著しく広い流体通路5を形成し、そ
の直径は対応する正方形または長方形の鉛直断面を有す
るタービンよりも大きいので駆動トルクはより大きい。
Furthermore, the turret according to the invention forms a significantly wider fluid passage 5 compared to existing turbines of the same size and type, and its diameter is larger than that of turbines with a corresponding square or rectangular vertical section, so that the driving torque is reduced. is larger.

更に、翼1の回転によって形成される立体が非常に好ま
しい空気力学的形状、即ち小さい抵抗係数を有するので
、タービンの効率は同じ型の既存のタービンに比べて著
しく改良される。
Furthermore, since the volume formed by the rotation of the blades 1 has a very favorable aerodynamic shape, ie a low drag coefficient, the efficiency of the turbine is significantly improved compared to existing turbines of the same type.

本発明に従うタービンは以下のように作動する。The turbine according to the invention operates as follows.

空気は2個の翼1間の開口部3に入り、該当する翼の内
側面に圧力を加える。空気は前記面に当って乱れを生じ
、こうしてタービン容積の内部で得られる速度により、
他、方の翼の開口部3がら空気が排出されるより以前に
、対向する内側面に抗力が生じる。タービン内の空気の
この運動は前記他方の翼を軸の回りに回転させ、翼の形
状により抗力とトルク増加の効果があるため効率が改良
される。
Air enters the opening 3 between the two wings 1 and exerts pressure on the inner surface of the respective wing. The air hits said surface and creates turbulence, and the velocity thus obtained inside the turbine volume causes
On the other hand, before the air is discharged from the opening 3 of the other wing, a drag force is created on the opposing inner surface. This movement of air within the turbine causes the other blade to rotate about its axis, and the shape of the blade has the effect of increasing drag and torque, thereby improving efficiency.

本発明の他の特徴に従うと、タービンはその内部容積中
に於いて、縁部で連合する翼1の間の接合部のレベルに
7または複数の回転軸受、発電機または他の機械的、電
気的或いは電子的要素を備え得る。
According to another feature of the invention, the turbine has in its internal volume seven or more rotary bearings, generators or other mechanical, electrical It may include physical or electronic elements.

更に、タービンはその内部容積中に信号またはランプ形
状の発光要素を備え得る。このような具体例により、信
号用または好ましくは美的あるいは装飾的用途の空気タ
ービンが得られる。
Furthermore, the turbine may be equipped with signal or lamp-shaped light emitting elements in its internal volume. Such an embodiment provides an air turbine for signaling purposes or preferably for aesthetic or decorative purposes.

本発明の他の特徴に従うと、第4図に示すように翼1の
表面は光起電力電池6を備え、これらの電池は翼の外部
及び部分的に内部に分配され、好ましピは翼と一体的に
形成され、補助電気エネルギーを供給する。
According to another characteristic of the invention, the surface of the wing 1 is provided with photovoltaic cells 6, as shown in FIG. It is integrally formed with and supplies auxiliary electrical energy.

当然のことながら、本発明は夙カタービンとして記載さ
れた。しかし乍ら、このタービンは同様に他の流体、特
に水を用いても作動し得る。
As will be appreciated, the invention has been described as a turf turbine. However, the turbine can also be operated with other fluids, especially water.

当然のことながら、本発明は上記記載の具体例及び添附
図面に限定されない。特に各種要素の構成の観点から、
或いは同等の技術を代替することにより、同様に本発明
の保護の領域を逸することなしに変形が可能である。
Naturally, the invention is not limited to the specific examples described above and the accompanying drawings. Especially from the perspective of the composition of various elements,
Alternatively, modifications are possible by substituting equivalent techniques without likewise leaving the scope of protection of the invention.

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

第1図は本発明に従うタービンの正面図、第2図は第1
図に従うタービンの水平断面図、第3図は前記タービン
の拡大斜視図及び第4図は本発明の変形具体例を示す第
1図と同様の図である。 1・・・・・・翼、2・・・・・・回転軸、3・・・・
・・開口部、4・・・・・・狭窄部、5・・・・・・通
路、6・・・・・・光起電力電池。 −鼾
FIG. 1 is a front view of a turbine according to the present invention, and FIG.
3 is an enlarged perspective view of said turbine, and FIG. 4 is a view similar to FIG. 1 showing a modified embodiment of the invention. 1... Wings, 2... Rotating shaft, 3...
... opening, 4 ... constriction, 5 ... passage, 6 ... photovoltaic cell. −Snoring

Claims (6)

【特許請求の範囲】[Claims] (1) 運動流体エネルギー、特に風力エネルギーの収
集用タービンであり、前記タービンは基本的に回転軸に
固着された2枚組の翼から構成されており、前記翼は前
記回転軸について対称を成し、それぞれ好ましくは18
0°よりやや小さい中心角度に伸びた双曲線状の水平断
面と、投影面がほぼ楕円形状の鉛直断面とを有しており
、前記翼は、三日月形の2個の開口部を形成するように
接合面のレベルで偏位させて相互り組合わせられており
、前記開口部の端部は断面間の各接合点で半円形断面の
通路を形成するように狭窄している運動流体エネルギー
、特に風力エネルギーの収集用タービン。
(1) A turbine for collecting kinetic fluid energy, especially wind energy, said turbine basically consisting of a set of two blades fixed to a rotating shaft, said blades being symmetrical about said rotating shaft. and each preferably 18
The wing has a hyperbolic horizontal cross section extending to a central angle slightly smaller than 0° and a vertical cross section whose projection plane is approximately elliptical, and the wing is configured to form two crescent-shaped openings. The kinetic fluid energy, in particular, is offset from one another at the level of the joint surfaces, and the ends of said openings are constricted to form a passage of semi-circular cross section at each joint point between the cross sections. Turbines for collecting wind energy.
(2) タービン内の運動流体の速度を増加すべく、各
翼の内側表面は内側に向って連続的に狭窄している特許
請求の範囲第1項に記載のタービン。
2. The turbine of claim 1, wherein the inner surface of each blade is continuously narrowed inwardly to increase the velocity of the moving fluid within the turbine.
(3) 内部容積内に於いて、福部で連合する翼の間の
接合部のレベルに1または複数の回転軸受、発電機また
は他の機械的、電気的もしくは電子的要素を備えている
特許請求の範囲第1項または第2項に記載のタービン。
(3) Patents comprising one or more rotating bearings, generators or other mechanical, electrical or electronic elements in the interior volume at the level of the joint between the blades that combine in the wing. A turbine according to claim 1 or 2.
(4) 内部容積内に於いて、信号またはランプ形状の
発光要素を備えている、特許請求の範囲第1項乃至第3
項のいずれかに記載のタービン。
(4) Claims 1 to 3, comprising a light-emitting element in the shape of a signal or lamp in the internal volume.
The turbine according to any of paragraphs.
(5) 翼の外側表面は、好ましくは翼と一体的 −6
に形成されており補助電気エネルギーを供給する光起電
力電池を備え得る特許請求の範囲第1項乃至第4項のい
ずれかに記載のタービン。
(5) The outer surface of the wing is preferably integral with the wing -6
5. A turbine according to any one of claims 1 to 4, which may be provided with a photovoltaic cell formed in a cylindrical shape and supplying supplementary electrical energy.
(6) 翼が180°の中心角度に伸延するように構成
されている特許請求の範囲第1項に記載のタービン。
6. The turbine of claim 1, wherein the blades are configured to extend at a center angle of 180°.
JP58201850A 1982-10-28 1983-10-27 Turbine for collecting kinetic fluid energy, particularly, wind force energy Pending JPS5993971A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR8218300A FR2535406B1 (en) 1982-10-28 1982-10-28 TURBINE FOR CAPTURING THE ENERGY OF MOVING FLUIDS, ESPECIALLY FOR WIND ENERGY
FR8218300 1982-10-28

Publications (1)

Publication Number Publication Date
JPS5993971A true JPS5993971A (en) 1984-05-30

Family

ID=9278801

Family Applications (1)

Application Number Title Priority Date Filing Date
JP58201850A Pending JPS5993971A (en) 1982-10-28 1983-10-27 Turbine for collecting kinetic fluid energy, particularly, wind force energy

Country Status (2)

Country Link
JP (1) JPS5993971A (en)
FR (1) FR2535406B1 (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2583823B2 (en) * 1982-10-28 1988-11-25 Lepoix Louis TURBINE FOR CAPTURING THE ENERGY OF MOVING FLUIDS, ESPECIALLY FOR WIND ENERGY
FR2574490B2 (en) * 1982-10-28 1988-12-30 Lepoix Louis TURBINE FOR CAPTURING THE ENERGY OF MOVING FLUIDS, ESPECIALLY FOR WIND ENERGY
DE3574760D1 (en) * 1984-12-07 1990-01-18 Louis L Lepoix TURBINE TO RECEIVE FLUIDUM ENERGY, ESPECIALLY WIND ENERGY.
AT403401B (en) * 1996-04-02 1998-02-25 Kita Firooz DEVICE FOR GENERATING ELECTRIC ENERGY FROM WIND POWER
US7453167B2 (en) * 2006-07-19 2008-11-18 Micah Gilbert Solar windmill

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR430879A (en) * 1911-06-10 1911-10-26 Louis Andre Lefrancois Rotating illuminated sign
US3941504A (en) * 1974-08-28 1976-03-02 Snarbach Henry C Wind powered rotating device
US4005947A (en) * 1975-02-10 1977-02-01 Norton Joseph R Fluid operated rotor
CA1119961A (en) * 1977-02-21 1982-03-16 Colin C. Kerr Vertical axis windmill rotor
DE2734938A1 (en) * 1977-08-03 1979-02-22 Rudolf Cammann Wind turbine generator with horizontal axis - uses solar radiation and anemometer-type blades to turn rotors on army to use Magnus effect

Also Published As

Publication number Publication date
FR2535406B1 (en) 1986-10-03
FR2535406A1 (en) 1984-05-04

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