JPS61500926A - Wind rotating body parts - Google Patents
Wind rotating body partsInfo
- Publication number
- JPS61500926A JPS61500926A JP60500353A JP50035385A JPS61500926A JP S61500926 A JPS61500926 A JP S61500926A JP 60500353 A JP60500353 A JP 60500353A JP 50035385 A JP50035385 A JP 50035385A JP S61500926 A JPS61500926 A JP S61500926A
- Authority
- JP
- Japan
- Prior art keywords
- rotating body
- body member
- wind
- hub portion
- degrees
- 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
Links
- 230000004323 axial length Effects 0.000 claims description 4
- 230000015572 biosynthetic process Effects 0.000 description 3
- 238000005096 rolling process Methods 0.000 description 3
- 241000282994 Cervidae Species 0.000 description 1
- 241000238631 Hexapoda Species 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000005461 lubrication Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000010248 power generation Methods 0.000 description 1
- 210000002784 stomach Anatomy 0.000 description 1
Classifications
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- 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
- F03D1/00—Wind motors with rotation axis substantially parallel to the air flow entering the rotor
- F03D1/06—Rotors
- F03D1/0608—Rotors characterised by their aerodynamic shape
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- 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
- F05B2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
- F05B2240/301—Cross-section characteristics
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- 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
- Y02E10/72—Wind turbines with rotation axis in 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
(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】 用回転体部材 この発明は用回転体部材、すなわち風によって駆動されることを企図した回転体 部材に関する。その上特に、この発明は回転体部材がほぼ水平軸輪周りに回転運 動をするために取付けられた中央ハブ部分と、ハブ部分に相対的に固定された位 置で前記ハブ部分に固定され、ハブ部分からほぼ半径方向の外部方向へ延びる多 数の回転体羽根とを有するこの種類の用回転体部材に関する。[Detailed description of the invention] Rotating body parts This invention relates to a rotating body member, that is, a rotating body intended to be driven by wind. Regarding parts. Moreover, in particular, the present invention provides a method in which the rotating body member is rotated about a substantially horizontal shaft ring. A central hub section attached for movement and a position fixed relative to the hub section. a polygon secured to said hub portion at a location and extending generally radially outwardly from said hub portion; The present invention relates to a rotating body member of this type having several rotating body blades.
このような回転体部材は電気風力発電所のための駆動VtMとして最初に用いら れている。しかしながら、これ先行技術の風力発電所の重大な欠点は発電所の配 置で風速の大きさが比較的制限された範囲内にあるときだけ風力発電所から電力 を得ることができることである。これは風速が比較的低い上限値を越えて、既知 の風力発電所の全てでどの操作でも容易にするために風速が比較的高い下限値を 越えなければならず、過度に高い薇械的歪の結果としてml傷を受けることから 発電所を防ぐために発電所を操作から除くことが必要である事実による。許すこ とのできない高い風速で操作から発電所を除くことを可能にするために、発電所 は可動の羽根、すなわち発電所が操作中長手方向の軸線の周りにハブ部分を相対 的に回転する羽根を有する用回転体部材によって通常駆動される。Such rotating body members were first used as drive VtM for electric wind power plants. It is. However, a significant drawback of this prior art wind farm is that the power plant layout is Electricity is drawn from the wind farm only when the magnitude of the wind speed at the site is within a relatively limited range. It is possible to obtain the following. This means that the wind speed exceeds a relatively low upper limit and In order to facilitate any operation in all wind power plants, wind speeds have a relatively high lower limit. must be exceeded and from sustaining ml scratches as a result of excessively high mechanical strains. Due to the fact that in order to prevent power plants it is necessary to remove them from operation. Forgive me In order to make it possible to exclude the power plant from operation at high wind speeds where it is not possible to is a movable vane, i.e. the power plant is relative to the hub part around the longitudinal axis during operation It is usually driven by a rotating body member having blades that rotate.
この発明は先行技術の用回転体部材に比較して操作の相当改良された安全を同時 に提供して実在する風速ノ実實的に増加した範囲の変化内で操作する最初にvG 述したこの種類の改良された用回転体部材を提供することをその目的のために有 する。The invention simultaneously provides considerably improved safety of operation compared to prior art rotary members. The first vG to operate within a practically increased range of changes in existing wind speeds by providing For that purpose it is an object of the present invention to provide an improved rotating body member of the kind described above. do.
この発明により、各回転体羽根がその内方端部よりその外方端部でより大きい羽 根角度を有することを最初に特徴とする前記種類の用回転体部材を、前記目的の ために、提案する。このような状況において、用コ羽根角度は回転体羽根が、そ の長さに沿うどの位置においても、その回転平面で、すなわち回転体部材の0転 軸線に垂直な平面で形成される角度として理解されるように企図する。The invention provides that each rotor blade has a larger blade at its outer end than at its inner end. A rotating body member of the type described above, which is initially characterized in that it has a root angle, is used for the purpose described above. I would like to make a suggestion. In this situation, the blade angle of the rotor blade is at any point along its length, i.e. at the zero rotation of the rotating member. It is intended to be understood as an angle formed in a plane perpendicular to an axis.
本発咀により提案された回転体羽根の装置は低い風速で風によって回転体部材に 加えられたトルクが従来知られた回転体部材より相当高くなり、羽根が飛行機の プロペラ、すなわちその外方端部よりその内方端部でより大きい羽根角度を有す る、場合と同様な方法でl!成されることに帰着する。結果として、本発明の回 転体部材は以前に可能であるよりも、実質的に低い!a速で操作を始めることが できる。The rotating body vane device proposed by Honhaktsui is a device that can be used for rotating body members caused by wind at low wind speeds. The applied torque is considerably higher than previously known rotating components, and the blades of the aircraft a propeller, i.e. having a larger blade angle at its inner end than at its outer end In the same way as in case l! It comes down to what gets done. As a result, the rotation of the present invention The rolling element is substantially lower than previously possible! It is possible to start operations at speed A. can.
回転体羽根、すなわちその内方端部からその外方端部の方の方向へ増加する羽根 角度を有する、′a案された形状、さらに、操作中、円錐渦が回転体部材の前方 の空気中に生じることによる。前記渦が回転体部材の半径方向の内部部分で負圧 帯または真空帯を形成して、回転体羽根の半径方向の外部部分の方へ到来する空 気流をまげるようにさせる0円錐渦のM径は増加する風速で及び回転体部材の増 加する回転速度で増加する。この結果、回転体部材は高い風速で、すなわち回転 体部材に制限された駆動作用のみ用いるために到来する空気流をもたらすように 、その回転速度を自動的にTI4整する自動調整式になる。従って、本発明の回 転体部0は無限に高い風速で操作される。a rotor vane, i.e. a vane increasing in the direction from its inner end towards its outer end In addition, during operation, a conical vortex is formed in front of the rotating body member. This is due to the fact that it occurs in the air. The vortex creates a negative pressure in the radially internal portion of the rotating body member. Air arriving towards the radially outer part of the rotor blades forming a band or vacuum band. The M diameter of the zero conical vortex that causes the airflow to bend increases with increasing wind speed and the number of rotating body members. increases with increasing rotational speed. As a result, the rotating body parts are rotated at high wind speeds, i.e. so as to bring the incoming airflow to use only a limited driving action on the body member. , it becomes an automatic adjustment type that automatically adjusts the rotation speed to TI4. Therefore, the rotation of the present invention Rolling element 0 is operated at an infinitely high wind speed.
各回転体羽根の羽根角度は回転体羽根の内方端部からその外方端部の方へ次第に 増加する方がよい、各回転体羽根の内方端部で羽根角度が約01からv910度 まで適切であり、一方各回転体羽根の外方端部で羽根角度が約20度から約50 度までの方がよく、約30度から約401[までの方がよい。The blade angle of each rotor blade gradually increases from the inner end of the rotor blade toward its outer end. It is better to increase the vane angle from about 01 to v910 degrees at the inner end of each rotor vane while the blade angle at the outer end of each rotor blade is approximately 20 degrees to approximately 50 degrees. It is better to go up to about 30 degrees to about 401 degrees.
上記渦形成及びそれによって生じた回転体部材の自動5uit能を促進するため に、回転体部材のハブ部分がほぼ円錐状前部部分を有する方がよい。To promote the above-mentioned vortex formation and the automatic 5uit ability of the rotating body member caused by it. Furthermore, it is preferred that the hub portion of the rotating body member has a generally conical front portion.
各回転体羽根の長さはその最も広い部分でハブ部分の直径と同程度の大きさが適 切である。各回転体部材の長さは前記直径の約0.5から約3@まである方がよ い。The length of each rotor blade should be approximately the same size as the diameter of the hub at its widest point. It's urgent. It is preferable that the length of each rotating body member is from about 0.5 to about 3 of the diameter. stomach.
ハブ部分の上記の円錐状前部部分はハブ部分の最も広い部分の、それぞれ、半径 または直径と同程度の大きさの適切な相当な軸線方向長さを好適に有すべきであ る。The above conical front section of the hub section is the radius of the widest part of the hub section, respectively. or should preferably have a suitable substantial axial length of the same order of magnitude as the diameter. Ru.
以下本発明が添付概略図面を参照してさらに詳細に記載される。The invention will now be described in more detail with reference to the accompanying schematic drawings, in which: FIG.
第1図は実例によって選択された本発明の実施例の用回転体部材からなる駆13 装冨を有する電気風力タービンの透視図、第2A図、第2B図及び第2C図は前 記回転体部材の回転体羽根を通る3つの異なる拡大断面図、第3図は優か変更し た構造の電気風力タービンの一部断面正面図、第4A図、第4B図及び第4C図 は第3図の夕 ′−−ピンの用回転体部材の回転体羽根を通る、それぞれ、第2 A図、第2B図及び第2C図と同様な3つの異なる拡大断面図、第5図は回転体 羽根と回転体部材の中央ハブ部分との間の連結の好適な型の一部断面因を示す。FIG. 1 shows a drive 13 consisting of a rotary member according to an embodiment of the present invention selected by way of example. A perspective view of an electric wind turbine with loading, Figures 2A, 2B and 2C are front Three different enlarged cross-sectional views through the rotor blades of the rotor member, FIG. 4A, 4B, and 4C are partial cross-sectional front views of an electric wind turbine having a similar structure; 3' in FIG. 3, respectively, passing through the rotating body blades of the rotating body member for the pin. Three different enlarged cross-sectional views similar to Figures A, 2B and 2C; Figure 5 is a rotating body; Figure 3 shows a partial cross-section of a preferred type of connection between a vane and a central hub portion of a rotating body member;
第1図に示す風力タービンは一般に10に指定された、用回転体部材を有する。The wind turbine shown in FIG. 1 has a rotating body member generally designated 10. The wind turbine shown in FIG.
この回転体部材は円筒状ハウジング11内に取付けられた電力発電機(図示せず )のために駆動装置として役立つ、前記ハウジング11は回転体部材10と発電 機との間の適当な駆り連結を設けるために歯車及び伝S装置はもちろん、はぼ水 平な軸線周りを回転するために回転体部材10を支持する軸受装置(第1因に図 示せず)をまた囲む。This rotary member is connected to a power generator (not shown) installed in the cylindrical housing 11. ), said housing 11 serves as a drive device for the rotating body member 10 and the power generation In order to establish an appropriate drive connection between the machine and the A bearing device that supports the rotating body member 10 in order to rotate around a flat axis (the first factor is the (not shown) is also enclosed.
回転体部材10.ハウジング11から遠いその端部でロッド13によって前記ハ ウジングに堅固に連結された風作動舵取羽根12を有する。参@数字17はほぼ 垂直軸線周りに自由に回転できるハウジング11を支持する8118を有するマ ストの上部部分を示す。舵取羽根12及び回転自在な支持Hiif18の設備は ハウジング11が回転体部材10を風に対して回転するようにさせる位置を連続 的にとることに帰着する。Rotating body member 10. At its end remote from the housing 11 the rod 13 It has a wind-operated steering vane 12 rigidly connected to the housing. Reference@Number 17 is almost 8118 supporting housing 11 that is freely rotatable about a vertical axis; The upper part of the strike is shown. The equipment for the steering blade 12 and rotatable support Hiif 18 is Continuously adjust the positions where the housing 11 allows the rotating body member 10 to rotate with respect to the wind. It comes down to hitting the target.
回転体部材10はほぼ円錐状前部部分14及び多数の回転体羽根16が等しい間 隔を置いてほぼ半径方向へ延びる(よは円筒状@部部分15からなる中央ハブ部 分を有する。第1図に示す場合には、回転体部材が3゛つの羽根を有する。しか しながら、前記数は好適に3または3の倍数、例えば6であるべきであるけれど も、どのような他の数の回転体羽根でも選ばれる。The rotor member 10 has a generally conical front portion 14 and a number of equal rotor vanes 16. A central hub section consisting of generally radially spaced (also cylindrical) sections 15; have a minute. In the case shown in FIG. 1, the rotating body member has three blades. deer However, said number should preferably be 3 or a multiple of 3, such as 6. or any other number of rotor blades.
回転体羽根16はその相対的に固゛定した位置で後部ハブ部材15に固定される 。しかしながら、回転体羽根と前記ハブ部分との間の連結は前記羽根をハブに固 定するとき、各据付は位置で部分的な円周が適切に合うようにこれら角度位置を 配置することを可能にさせるようになる。このような連結の1つの適切な型が第 5図に示される。The rotor vane 16 is fixed to the rear hub member 15 in its relatively fixed position. . However, the connection between the rotor blades and the hub portion is such that the blades are fixed to the hub. When setting up each installation, adjust these angular positions so that the partial circumferences fit properly in position. It will now be possible to place them. One suitable type of such concatenation is This is shown in Figure 5.
回転体羽根の特性のあるV8黴は第2A図、第2B図及び第2C図に示される。V8 mold with characteristics of rotor blades is shown in FIGS. 2A, 2B, and 2C.
これら図面は第1図の、それぞれ、一点!ll1lASB及びCに沿って取られ た回転体羽根を通る断面を示す、前記断面図から示されるように、回転体羽根1 6の羽根角度が、各羽根の内方端部からその外方端部の方へ次第に増加する。前 記角度は回転体部材10の水平回転軸線に垂直に延びる羽根16の回転平面Rと 、問題の羽根部分の弦との間の、それぞれの角度■ 、■8及びvoとして示さ れる。第2A図、第2B図及び第2C図から示されるように羽根16の内方端部 に近い断面Aで角度vAは単に約2度であり、一方羽根16の中央に近い断面B で角度V、は実質的により広い、約20度であり、羽根16の外方端部に近い断 面Cで角度V。はなお広く、約40度である。Each of these drawings is one piece from Figure 1! taken along ll1lASB and C As shown in the cross-sectional view showing the cross section through the rotor blade 1, the rotor blade 1 The vane angle of 6 increases progressively from the inner end of each vane towards its outer end. Before The angle is the rotation plane R of the blade 16 extending perpendicularly to the horizontal rotation axis of the rotating body member 10. , the respective angles between the chord of the blade part in question, shown as ■, ■8 and vo. It will be done. The inner end of the vane 16 as shown in FIGS. 2A, 2B, and 2C. At section A near the center of the blade 16 the angle vA is only about 2 degrees, while at section B near the center of the blade 16 The angle V, is substantially wider, about 20 degrees, and the section near the outer end of the vane 16 Angle V on plane C. is still wide, about 40 degrees.
812の操作中、示された形状及び回転体羽根゛16の装置の結果として、円錐 渦は回転体部材1oの前方の空気中に形成される。この渦形成はほぼ円錐状前部 ハブ部分14によって高められ、その軸線方向の長さは、入れかわって、回転体 羽根16の長さとほぼ同程度であるハブ部分の最も広い直径と同程度である。During operation of 812, as a result of the shape shown and the arrangement of the rotor vanes 16, a conical A vortex is formed in the air in front of the rotating body member 1o. This vortex formation has an almost conical front increased by the hub portion 14, the axial length of which is alternately It is of the same order of magnitude as the widest diameter of the hub portion, which is of the same order of magnitude as the length of the vane 16.
前記渦形成の結果として、到来空気は回転体部材10の回転する間口転体羽根1 6によって一掃された環状面の外部円r@部分の方で半径方向外部方向へまげら れるようになる。到来空気のこの曲げの大きさ及び同時に生じる真空帯の直径は 実在する風速及び回転体部材10の回転速度による。高い風速で、回転体部材は 自動m制式になり、それにより非常に高い大きさの風速を生じるときでも、許容 最大速度以下でその回転速度を絶えず維持する。As a result of said vortex formation, the incoming air flows through the rotating frontage rolling blades 1 of the rotating body member 10. The outer circle r@ part of the annular surface swept by 6 is radially outward. You will be able to do it. The magnitude of this bending of the incoming air and the diameter of the vacuum band created at the same time are It depends on the actual wind speed and the rotational speed of the rotating body member 10. At high wind speeds, rotating parts automatic m-control system, which allows for maximum tolerance even when wind speeds of very high magnitude occur. Continuously maintain its rotational speed below the maximum speed.
第3図、第4A図、第4B図及び第4C図に示す変更した構造は小さな個所にお いてのみ第1図、第2A図、第2B図及び第2C図の装置と異なる。第3図にお いて、前部ハブ部分14は第1図より短く、回転体羽根の数は3の代りに2だけ である。更に、ハウジング11は回転体部材1oのハブ部分の最大直径にほぼ等 しい直径を有するように示されている。その上、ハウジング11の左端部が後部 ハブ部分15に堅固に連結され、軸受21によって2つの環状支持板2o内に回 転自在に取付けられた中央水平軸19を部分的に覆いのない断面で示されている 。ハウジング11内の板20の間に限定さ°れた至22は軸受21のための潤滑 油で充されるように示されている。The modified structure shown in Figures 3, 4A, 4B, and 4C is suitable for use in small areas. 1, 2A, 2B, and 2C. In Figure 3 1, the front hub section 14 is shorter than in FIG. 1, and the number of rotor blades is only two instead of three. It is. Furthermore, the housing 11 has a diameter approximately equal to the maximum diameter of the hub portion of the rotating body member 1o. shown with a new diameter. Moreover, the left end of the housing 11 is located at the rear. It is rigidly connected to the hub part 15 and rotated by bearings 21 into two annular support plates 2o. A rotatably mounted central horizontal shaft 19 is shown in partially uncovered section. . A shaft 22 defined between plates 20 in the housing 11 provides lubrication for the bearing 21. Shown as being filled with oil.
第4B図及び第4C図に示される断面図は第2B図及び第2C図に示された対応 図にほぼ等しい。しかしながら、第4A図は羽根角度vAが2度の代りに約10 度であり、羽根16が第2A図より薄いことが第2A図と異なる。The cross-sectional views shown in Figures 4B and 4C correspond to those shown in Figures 2B and 2C. Approximately equal to the figure. However, FIG. 4A shows that the vane angle vA is approximately 10 degrees instead of 2 degrees. 2A in that the blade 16 is thinner than that in FIG. 2A.
第5図に示す回転体羽根16とハブ部分15との間の連結は回転体部材の羽根を そのハブ部分に固定するとき、前記回転体部材のための適切に羽根角度を定める ことができるようにするのに役立つ、示された連結は後部ハブ部分15に堅固に 固定された取付は基部23、分割上部締付はリング24、及び締付はポルト25 を有する。その内方端部に、羽根16が適当にgl製された位置で堅くmsさせ ることができるようにリング24の対応する面取り表面と基部23との間で締付 けられるように用いられた面取り端部表面を備えた頭部26を有する。The connection between the rotor blades 16 and the hub portion 15 shown in FIG. Determine the blade angle appropriately for the rotating body member when fixing it to its hub part The connection shown is firmly attached to the rear hub portion 15, which serves to make it possible to Fixed mounting is at the base 23, split upper tightening is at the ring 24, and tightening is at the port 25. has. At its inner end, the vane 16 is firmly attached at a suitably glazed position. between the corresponding chamfered surface of the ring 24 and the base 23 so that the It has a head 26 with a chamfered end surface used to allow it to be cut.
第1図に示されたタービンとほぼ同様な虫カタービンは約400cmの全回転体 直径を有し、約100cmの最大ハブ直径が4ケ月の期間中絶えず試験された。The insect turbine, which is almost similar to the turbine shown in Figure 1, has a total rotating body of about 400 cm. A maximum hub diameter of approximately 100 cm was tested continuously over a four month period.
この期間中、風速が零から約30m/Sまで変化された0回転体は約2〜3m/ Sの風速で回転し初め、最大゛速度が約1500rp■に設定されることがわか る。に設定されることがわかる。During this period, the zero rotating body, whose wind speed was changed from zero to approximately 30 m/s, was approximately 2 to 3 m/s. It can be seen that it starts rotating at a wind speed of S, and the maximum speed is set to about 1500 rpm. Ru. You can see that it is set to .
本発明は上記した、図面に示された実施例に制限されない0代りに、多くの他の 実施例が本発明の範囲内で寅施できる。The present invention is not limited to the embodiments described above and shown in the drawings, but can also include many other embodiments. Embodiments can be implemented within the scope of the invention.
FIG、 1 閂 倚 t1! 専 謡 牛FIG. 1 Bolt t1! Special song cow
Claims (8)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SE8400157A SE442659B (en) | 1984-01-13 | 1984-01-13 | WIND rotor element |
| SE8400157-7 | 1984-01-13 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS61500926A true JPS61500926A (en) | 1986-05-08 |
Family
ID=20354299
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP60500353A Pending JPS61500926A (en) | 1984-01-13 | 1985-01-14 | Wind rotating body parts |
Country Status (6)
| Country | Link |
|---|---|
| EP (1) | EP0168465A1 (en) |
| JP (1) | JPS61500926A (en) |
| DE (1) | DE3590007T1 (en) |
| DK (1) | DK414885D0 (en) |
| SE (1) | SE442659B (en) |
| WO (1) | WO1985003110A1 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2013515901A (en) * | 2009-12-24 | 2013-05-09 | タイダル ジェネレーション リミテッド | Turbine assembly |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DK164925B (en) * | 1990-07-11 | 1992-09-07 | Danregn Vindkraft As | WINGS TO A WINDMILL |
| US5562420A (en) * | 1994-03-14 | 1996-10-08 | Midwest Research Institute | Airfoils for wind turbine |
| US6068446A (en) * | 1997-11-20 | 2000-05-30 | Midwest Research Institute | Airfoils for wind turbine |
| TW200726908A (en) * | 2005-10-04 | 2007-07-16 | Arthur Benjamin O Connor | Wind turbine |
| GB2459453B (en) * | 2008-04-21 | 2011-06-08 | Barry Robert Marshall | Energy output limiter for wind turbine rotor(s) |
-
1984
- 1984-01-13 SE SE8400157A patent/SE442659B/en not_active IP Right Cessation
-
1985
- 1985-01-14 DE DE19853590007 patent/DE3590007T1/en not_active Withdrawn
- 1985-01-14 JP JP60500353A patent/JPS61500926A/en active Pending
- 1985-01-14 WO PCT/SE1985/000012 patent/WO1985003110A1/en not_active Ceased
- 1985-01-14 EP EP85900791A patent/EP0168465A1/en not_active Withdrawn
- 1985-09-12 DK DK414885A patent/DK414885D0/en not_active Application Discontinuation
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2013515901A (en) * | 2009-12-24 | 2013-05-09 | タイダル ジェネレーション リミテッド | Turbine assembly |
Also Published As
| Publication number | Publication date |
|---|---|
| SE8400157L (en) | 1985-07-14 |
| EP0168465A1 (en) | 1986-01-22 |
| SE442659B (en) | 1986-01-20 |
| DE3590007T1 (en) | 1986-02-20 |
| DK414885A (en) | 1985-09-12 |
| DK414885D0 (en) | 1985-09-12 |
| WO1985003110A1 (en) | 1985-07-18 |
| SE8400157D0 (en) | 1984-01-13 |
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