TWI299769B - Magnus type wind power generation system - Google Patents
Magnus type wind power generation system Download PDFInfo
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- TWI299769B TWI299769B TW094124318A TW94124318A TWI299769B TW I299769 B TWI299769 B TW I299769B TW 094124318 A TW094124318 A TW 094124318A TW 94124318 A TW94124318 A TW 94124318A TW I299769 B TWI299769 B TW I299769B
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1299769 九、發明說明: 【發明所屬之技術销織】 技術領域 % 5 本發明係有關於一種藉著各旋轉圓柱的旋轉與風力的 相互作用所產生的馬格_升力使水平旋轉減轉驅動 發電機構件之馬格納斯(Magnus)型風力發電裝置。 t先前技系餘】 背景技術 作為效率型的風力發電裝置雖然已有使用薩伏紐斯 1〇 (S_mUS)風車者被實雜,但薩伏_風車的葉片由於無 έ:疋轉至風速以上,發電能力亦小,故不適合大電力發電, 另方面雖然有使用螺旋槳型風車之較高發電能力的實 用里風力务電裝置,但有無法於較低風速域提高風車效率 之問題。 —示了這~方式外,使相對於水平旋轉軸成放射狀配置 、 勺疑轉圓柱產生馬格納斯升力,使水平旋轉軸旋 轉m 1的馬袼納斯型風力發電裝置亦為周知(例如參 照專利文獻1、2)。 〔專利文獻丨〕美國專利第4366386號說明書 〔專利文獻2〕俄羅斯聯邦專利第2189494C2號說明書 【發明内容】 發明揭示 發明欲解決之問題 於專利文獻1所示的馬格納斯型風力發電裝置由於藉 1299769 者使旋轉圓柱旋轅立 51299769 IX. Description of the invention: [Technical sales of the invention] Technical field % 5 The present invention relates to a horse-to-lift force generated by the interaction of the rotation of each rotating cylinder with the wind force, which causes the horizontal rotation to reduce the driving power generation Magnus type wind power generator for machine components. BACKGROUND OF THE INVENTION As an efficient wind power generator, although a sailor using a Savonius 1 (S_mUS) windmill has been used, the blade of the Savoy_windmill is innocent: the wind is turned to above the wind speed. The power generation capacity is also small, so it is not suitable for large-scale power generation. In addition, although there is a practical wind power supply device using a higher power generation capability of a propeller type windmill, there is a problem that the windmill efficiency cannot be improved in a lower wind speed range. - In addition to this, it is known that the Marunus wind power generation device is arranged radially with respect to the horizontal rotation axis, and the Magnus lift is generated by the scooping rotation cylinder, and the horizontal rotation axis is rotated m 1 (for example). Refer to Patent Documents 1, 2). [Patent Document 美国] US Patent No. 4366386 (Patent Document 2) Russian Patent No. 2189494C2 [Invention] The present invention discloses a problem to be solved by the Magnus type wind power generator shown in Patent Document 1. 1299769 The rotating cylinder is erected 5
轉進行發電,故為了斯升力,使水平旋轉轴旋 轉速度,加強馬4、斯:發電里’必須提高旋轉圓柱的旋 、#_ 升力。但是,為了使旋轉圓柱以高 速=,會她過多的能量,使發電效率變差。 二於專利文獻2所示的馬格納斯型風力發電裝置因為 使用藉著風力旋轉的薩伏紐斯轉子使旋轉圓柱旋轉,故可 省略旋轉圓㈣傳動機構且不f要設置用以使旋轉圓柱旋 轉的驅動馬料,城伏紐㈣子由於無法旋轉至風速以 上’無法提高旋轉圓柱的旋轉速度,故無法產生大的馬格 納斯升力,不適合有效率的發電。 本發明係提供一種可同時解決上述問題,可於低風速 域至較高風速域有效率地發電之馬格納斯型風力發電裝 置。 解決問題之方法 15 為了解決上述問題,本發明之申請專利範圍第1項之馬 格納斯型風力發電裝置係具有用以傳達旋轉力矩至發電機 構件之水平旋轉軸、由該水平旋轉軸成放射狀配置預定數 量之旋轉圓柱及用以驅動前述各旋轉圓柱以該等旋轉圓柱 的軸為中心旋轉之驅動馬達,用以藉著前述各旋轉圓柱的 20旋轉與風力的相互作用所產生的馬格納斯升力使前述水平 旋轉轴旋轉,驅動發電機構件者,於預定位置設置有用以 使前述旋轉圓柱的外周表面產生空氣流動,使馬格納斯升 力增大的空氣流動機構。 本發明係基於發明者發現的新的原理、即,與自然風 1299769 =伴心者旋轉圓柱而旋轉的旋轉圓麵層 同,藉著使旋轉圓柱的外周表面產生*:、工氣的流動不 各旋轉圓枝的旋轉與風力的相互作用::流動,可使藉著 力增大,藉此,成功地使用以驅動發^馬格納斯升 ^至較1^風速域㈣地上升。 〜率於低風速Turning to power generation, in order to increase the speed of the horizontal rotating shaft for the lift, strengthen the horse 4, Si: power generation must increase the rotation of the rotating cylinder, #_ lift. However, in order to make the rotating cylinder at a high speed =, she will have too much energy to deteriorate the power generation efficiency. 2. The Magnus-type wind power generator shown in Patent Document 2 rotates the rotating cylinder by using a Savonius rotor that is rotated by the wind, so that the rotating circle (four) transmission mechanism can be omitted and the rotating cylinder is not provided. Rotating drive horse material, the city Volt (4) can not be rotated above the wind speed 'can not improve the rotation speed of the rotating cylinder, so it can not produce large Magnus lift, not suitable for efficient power generation. SUMMARY OF THE INVENTION The present invention provides a Magnus type wind power generation apparatus which can simultaneously solve the above problems and efficiently generate power in a low wind speed range to a high wind speed range. Solution to Problem 15 In order to solve the above problem, the Magnus type wind power generation device of claim 1 of the present invention has a horizontal rotation axis for transmitting a rotational torque to a generator member, and is radiated from the horizontal rotation axis. a predetermined number of rotating cylinders and a driving motor for driving the rotating cylinders to rotate around the axes of the rotating cylinders for generating a Magna by the interaction of the rotation of the rotating cylinders and the wind The lifter rotates the horizontal rotary shaft to drive the generator member, and an air flow mechanism is provided at a predetermined position to generate air flow on the outer peripheral surface of the rotating cylinder to increase the Magnus lift. The present invention is based on the new principle discovered by the inventors, that is, the same as the rotating circular surface layer rotated by the natural wind 1299769 = the rotating cylinder of the accompaniment, by causing the outer peripheral surface of the rotating cylinder to produce *:, the flow of the working gas is not The interaction between the rotation of each rotating branch and the wind:: The flow can be increased by the force, thereby being successfully used to drive the launch of the Magnus to the wind speed (4). ~ rate at low wind speed
裝置係士 1之申叫專利祀圍第2項之馬格納斯型風力發電 衣置係如巾請專利範圍第 η風力U 置,其中前述空氣流動機構係用 二及伴隨著旋轉一 進卡予鱼^的〜動而形成的馬格納斯升力, 15可形二與旋轉圓柱的轴相平行的空氣流的分量,因此 _::::=rr認’馬_斯升力、 轉轉圓::不須全部與旋轉圓柱平行,只要有至少 的向量分量即具有足夠的效果。 2〇妒置射由之申明專利乾圍第3項之馬格納斯型風力發電 利範圍第1項或第2項之馬格納斯型風力發 _矣 巾Μ 4空氣流動機構係用以使前述旋轉 圓柱的 依該特徵’藉著以空氣流動 方==生與該旋轉圓_&平行且朝遠離前述水平 方疋轉軸的方向的空氣流動分量者。 機構於旋轉圓柱的外周表 7 1299769 面產生朝遠離水平旋轉軸的方向的空氣流動,可增大於旋 轉圓柱產生的馬格納斯升力。 . 本赉明之申請專利範圍第4項之馬格納斯型風力發電 • 裝置係如申請專利範圍第1項或第2項之馬格納斯型風力發 5電農置,其中前述空氣流動機構係用以使前述旋轉圓柱的 外周表面產生與該旋轉圓柱的軸相平行且朝向前述水平旋 轉軸的空氣流動分量者。 依該特徵,藉著以空氣流動機構於旋轉圓柱的外周表 • 减生朝向水平旋轉軸的空氣流動,可增大於旋轉圓柱產 10 生的馬格納斯升力。 本發明之申請專利範圍第5項之馬格納斯型風力發電 .I置係Μ料職®第如奴馬格、_获力發電農 • 4,其中前述空氣流動機構係設置於前述旋轉圓柱的外周 表面之翼元件。 15 20 合因置元件 轉時,旋轉圓柱周圍的空氣 2件而流動,可增大於旋轉圓杈產生的馬格納斯升 本發明之申請專利範圍第6 裝置係如申請專利範圍第5項之二斯型風力發電 置,其中•作為空氣流動機構的風力發Μ 轉圓柱的外周表面的螺旋狀的突條 设置於前述旋 依該特徵,於旋轉圓柱旋轉 使_勻且安定地流動於旋轉 馬格納斯升力,„可減域切音。4表面’可增大 8 1299769 本發明之申請專利範圍苐7項之馬格納斯型風力發電 裝置係如中#專利㈣第丨或2項之馬格納斯型風力發電装 置其中於刖迷旋轉圓柱的前端設置有直經比該旋轉圓挺 大的端蓋。 依該特徵 ;、〇月】述空氧流時’依實驗註明安裝端 蓋可提高馬格納斯效應,又,實驗可明白,設㈣蓋時, 麻平旋轉軸方向流動空氣的方式會比相反地朝放射方向 w動空氣的方錢驗‘—植應增大。 10 15 20 本發明之中請專利範圍第8項之馬格納斯型風力發電 tr專利範㈣6項或第7項之馬格納斯型風力發 屯衣置’其中别述突條以多條螺旋構成。 ^特徵’藉著設置多條螺旋’即使不擴大螺旋的直 ^ =更多的空氣圓滑地流動於旋轉圓柱的表面,提 同馬格納斯效應。 事置係專利耗圍第9項之馬格納斯型風力發電 裝置係如申晴專利範圍第 置,其中於前述旋轉圓納斯型風力發電裝 饮兮壯 口柱的外周表面形成複數的凹凸件。 特徵,旋轉圓柱以軸為 件可攪亂旌鳇^ ^^疋轉日可,複數的凹凸 環,使 二使:轉圓柱產生的馬格納斯升 皆可。Hu以《亂表層流的凹凸,為任何形狀 1299769 置’其中於前述突條的前端外表面設置凹凸件或突起。依該特徵,凹凸件或突起可授亂突條的前端外表面的層流(交界層),抑制剝離並增加循環,使馬格納斯升力進 一步增大。 5 ^月之巾Μ專利圍第u項之馬格納斯型風力發電 ^系如申明專利|巳圍第域2項之馬格納斯型風力發電裝“中⑴述㈣圓柱被支持成可相對於水平旋轉軸於徑 万向自由伸縮。The Magnus type wind power clothing set of the second section of the device is called the patent scope η wind power U, wherein the air flow mechanism is used twice and the card is rotated The Magnus lift formed by the movement of the fish ^, 15 the shape of the air flow parallel to the axis of the rotating cylinder, so _::::=rr recognizes the horse's lift, the turn circle:: It is not necessary to be all parallel to the rotating cylinder, as long as there is at least a vector component that has sufficient effect. 2 〇妒 〇妒 〇妒 申 申 申 专利 专利 马 马 马 马 马 马 马 马 马 马 空气 空气 空气 空气 空气 空气 空气 空气 空气 空气 空气 空气 空气 空气 空气 空气 空气 空气 空气 空气 空气 空气 空气 空气 空气 空气 空气 空气 空气The characteristic of the rotating cylinder is by the air flow side == the air flow component parallel to the rotating circle _& and facing away from the aforementioned horizontal square axis of rotation. The mechanism produces a flow of air in a direction away from the horizontal axis of rotation on the outer surface of the rotating cylinder 7 1299769, which increases the Magnus lift generated by the rotating cylinder. The Magnus-type wind power generation device according to item 4 of the patent application scope of the present invention is the Magnus-type wind power generator 5 of the patent application scope 1 or 2, wherein the aforementioned air flow mechanism is used. The outer peripheral surface of the aforementioned rotating cylinder is caused to generate a component of air flow parallel to the axis of the rotating cylinder and toward the aforementioned horizontal rotating shaft. According to this feature, by the air flow mechanism on the outer circumference of the rotating cylinder, the air flow toward the horizontal rotating shaft is reduced, and the Magnus lift of the rotating cylinder can be increased. The Magnus-type wind power generation of the fifth application of the present invention is in the form of a 旋转 职 ® 第 第 奴 奴 奴 第 第 第 第 、 、 , , , , , , , , , , , , , , , , , , Wing element of the outer peripheral surface. 15 20 When the component is turned, the air around the rotating cylinder flows, and the Magnus can be increased in the rotating circle. The sixth device of the invention is as claimed in the fifth paragraph of the patent application. Wind power generation, wherein: the wind swell as the air flow mechanism, the spiral ridge of the outer peripheral surface of the rotating cylinder is arranged in the above-mentioned rotation, and rotates in the rotating cylinder to make the _ even and stable flow to the rotating Magnus Lifting force, „can reduce the cut-off sound. 4 surface' can be increased 8 1299769 The patent application scope of the invention 苐 7 items of the Magnus type wind power generation device such as the # patent (4) the third or the second Magnus type The wind power generating device is provided with an end cover which is straighter than the rotating circle at the front end of the rotating cylinder. According to the feature, when the oxygen flow is described, the installation of the end cover according to the experiment can improve the Magnus. The effect, in addition, the experiment can understand that when the (four) cover is set, the way of flowing air in the direction of the rotation axis of the Maping will be increased compared with the opposite direction of moving the air in the radial direction w. The plant should be increased. 10 15 20 In the present invention please The Magnus-type wind power tr patent of the 8th item of the benefit range (4) The Magnus-type wind-fighting clothing set of 6 or 7 'The spurs are composed of multiple spirals. ^Characteristics by setting more The spiral "even if the air is not enlarged" = more air flows smoothly on the surface of the rotating cylinder, which is accompanied by the Magnus effect. The Magnus-type wind power generation device of the patent item 9 is Shen Qing's patent scope is set, in which a plurality of concave and convex parts are formed on the outer peripheral surface of the rotating circular Nass type wind power generation and drinking sturdy column. Features, the rotating cylinder can be disturbed by the axis. ^^^疋日Yes, the plurality of embossed rings can be used to make the Magnus swells produced by the rotating cylinders. Hu is provided with the concave and convex of the laminar flow, for any shape 1299769, in which the outer surface of the front end of the aforementioned ridge is provided with a concave or convex piece or According to this feature, the concavo-convex or protrusion can disturb the laminar flow (boundary layer) of the outer surface of the front end of the ridge, suppress the peeling and increase the circulation, and further increase the Magnus lift. 5 ^月的巾Μ专利围The U of the u Si ^ wind power system as stated in Patent | Pat circumference of the Magnus type wind power domain 2 of the apparatus "described in (iv) ⑴ cylinder is supported so as to be horizontal with respect to the diameter of the rotary shaft joint free to expand.
10 1510 15
20 依5亥特徵’因為旋轉圓柱可自由伸縮,故可依照自然 L風向錢速使旋侧柱伸縮、發電,於—般情形時, 的難伸展,錢風_成為最大,增大旋轉圓柱 ’且於強風時射藉__侧柱,使受風 —止支持台的倒塌或旋轉圓柱的破損。 、 裝置專利範圍第12項之馬格納《風力發電 置圍第1或2奴馬油斯型風力發電裝 置’其中係使用數I卜命 述驅動馬達同時_動 轉圓柱的所需定數量少的前 依該特徵= 二各旋轉圓柱旋轉。 π -h^\ 、 p、勺用以驅動驅動馬達的電力,故 可^風力發電裝置的發電效率。 圖式簡單說明 弟1圖係顯 裝置之正視圖c第2圖係馬格納斯升力的說明圖 弟3圖係顯示第1圖中的旋轉 丁本^日月之實施例1之馬格納斯型風力發 電 圓柱之A-A截面圖。 10 1299769 第4圖係顯示經設置突條 疋轉圓桂之正相图。 第5圖係顯示實施例2中經 回 視圖 硬合體的旋轉圓柱之正 第6圖係顯示實施例3中 5 件的旋轉圓柱之正視圖。 於複合體巾的突條設置凹凸 圖 第7圖係顯示實施例4中經設置 四條的旋轉圓柱之正視 第8圖係顯示實施例5中绫今番 工°又置2條突條的旋轉圓柱之 正視圖。 10第9圖係顯示經設置2條突條的旋轉圓柱之立體圖。 第10圖係顯示實施例6中的旋轉圓柱之正視圖。 第11圖係顯示實施例7中的端蓋之立體圖。 第12圖係顯示實施例8中的馬格納斯型風力發電裝置 之正視圖。 15 第13圖係顯示實施例9中的馬格納斯型風力發電裝置 之旋轉體之縱截面側視圖。 _ 帛14圖係顯示第圖中的旋轉體之B-B縱截面背視圖。 I:實方包方式】 發明之較佳實施形態 20 、 以下’說明本發明之實施例。 〔實施例1〕 以圖不說明本發明之實施例之馬格納斯型風力發電裝 置’首先,第1圖係顯示本發明之實施例丨之馬格納斯型風 力發電裝置之正視圖,第2圖係馬格納斯升力的說明圖,第 11 1299769 3圖係顯示第1圖中的旋轉圓柱之A韻面圖,第4圖係顯示 經設置突條的旋轉圓柱之正視圖。 虎明般的馬格納斯升力的產生機制,如第2圖所示, 於第2圖的旋轉圓柱c的旋轉方向與空氣流的方向下,碰到 5旋轉圓柱C的正面側的空氣流動係與旋轉圓柱^的旋轉〆 起流動於上方,此時,流動於旋轉圓柱c的上方側的空氣的 流速因為比流動於旋轉圓柱c的下方側的空氣快,故因旋轉 圓柱C的上方側的負壓與下方側的正壓,於空氣壓上產生差 異、即產生馬格納斯效應,於旋轉圓柱C上,於與空氣的流 10動成直角的方向上產生馬格納斯升力γ〇。 第1圖的標號Α係適用本發明的馬袼納斯型風力發電裝 該馬格納斯型風力發電裝置八於直立設置於地面的支持 台1的上部配置有發電機構件2,該發電機構件2係以垂直馬 達(圖不省略)為中心,於水平方向可自由旋轉地被軸支,該 15發電機構件2具有被軸支成可自由旋轉於垂直方向的水平 ^轉軸3,該水顿雜3的—端與發電韻件⑽部配置的 =電機(圖示省略)相連結,同時水平旋轉轴3的另_端被固 定於旋轉體4。 2〇 如第1圖所示,於旋轉體4的内部被配置有6個驅動馬達 〇 15,同時於旋轉體4的外周成放射狀配置有6根旋轉圓柱5, 各旋轉圓柱5的基部與配設於旋轉體4内部的各驅動馬達15 相連結,各旋轉圓柱5被軸支成可藉著各驅動馬達的驅動 而旋轉。又,於旋轉圓柱5的前端面被安裝有直徑比旋轉圓 的直徑大的圓盤狀的端蓋16。 12 1299769 於灰轉1]柱5的軸外周面,被—體地捲繞設 ,構的翼元件、即螺旋狀的突條6,該 大’/、1合成樹脂等材質或耐候性輕量合金等材 =針對該突條6進行說明,如第4圖所示,預定寬声= 5定高度W條突條6,由旋轉圓柱5的前端面看時成右^狀 地被固定。 系方疋狀 使用弟1圖所示的馬格納斯型風力發電裝置a Γ先’以風向計(圖示省略)檢測出風向’以控制電路(二 名略)驅動垂直馬達(圖示省略),如同由旋轉體4的正面側: )’配合風向使發電機構件2旋轉。 = 轉體4内部的各軸馬扣,使各旋㈣讀動方疋 圖及第圓柱:旋轉方向與突條6的捲繞方式,如第1 15 20 柱5的„^1^讀圓柱5的前端部方向看時,旋轉ϋ 級狀的犬條6的捲繞方式成右螺旋狀時,旋 的方疋轉方向成向左轉。 杈5 圓柱5的旋轉方向成相反r 方向與旋轉 X的:氣—側流動。又,於突條6的螺二 :方向與旋轉圓柱5的旋轉方向為同 方疋轉圓柱5的外周矣品从 J便,瓜動於 (放射方向)流動^,空氣朝由水平旋轉軸3遠離的方向 於旋著於輯圓柱5設置螺旋狀的突條6, 動^此時著螺旋狀的突條6會產生空氣的流 著碇轉圓柱周表面,除了自Μ及伴隨 疋轉的旋轉圓柱5表層的空氣的動向外,另外 13 5 可產生與旋轉圓柱5的財 士昝 卜 的流動分IV。 圖及弟4圖所示,藉著 即於旋軸聊卜㈣產rtr卜周的空氣流、 然風及伴隨著旋轉圓柱5旋動F心成以自 向所形成的三次元的空氣轉圓柱5表層的空氣的動 於後述的實驗可確認蕤 ;:相州組__2=::==力 10 部與旋轉圓㈣:行氣的餘叹不須全 分 /、要有至少與旋轉圓柱5平行的向量 被提高的原^的絲。雖然仍财核,但馬格納斯升力Y 正壓:差广忍為是因為產生施加於旋轉圓柱5的負壓與 15 現象及升力產生面被擴大之現象等。 又湘、盖16時,可提高馬格納斯效應之點亦經實 :月gP,藉著於旋轉圓柱5的前端面設置端蓋Μ,該端 盖16會對空氣流F帶來正面影響,提高馬格納斯升力γ。又, 如後所述,由實驗可知,設置端蓋16時,使空氣朝水平旋 轉軸方向流動的方式會比使线相反地減射方向流動的 方式更能使馬格納斯效應增大。 20 如第1圖所示,藉著於各旋轉圓柱5產生的馬袼納斯升 力γ ’方疋轉圓柱5及旋轉體4以水平旋轉軸3為中心旋轉,被 連結於水平旋轉轴3的_端的發電機(圖示省略)被驅動,可 進盯發電。然後,藉著於旋轉圓柱5設置螺旋狀的突條6, 可增大用以驅動發電機(圖示省略)的水平旋轉軸3的力矩值 (旋轉力矩)’可提高馬格納斯型風力發電裝置A的發電效 14 1299769 藉著發電機⑽料略则發電時,可臟 的—部份供給至用以使旋轉圓柱5_的驅動馬 ^ • 補助電力利用。 作為 y…下將本貫施例所使用的旋轉1]柱5於風洞實絡〜 〜证貫驗。關於本實施例中的馬格納斯型風力 的旋轉圓柱5與其他發明中的旋轉圓柱及理想流體 1比0及升力係數Cy兹以表说明,表】係顯示周迷比㊀用 升力係數Cy的關係之圖,以旋轉圓柱的直徑⑽為己,旋^ • 圓柱每秒的旋轉數_為η,風速(m/s)細時,旋轉圓^的 ⑺周速比Θ以0=7Z;dn/U表示,升力係數Cy係升力γ除以每單 位體積的風的動能(1/2)pu2與旋轉圓柱的投影面積沿(1係 旋轉圓柱的長度)的乘積之值,於理想流體中以C y=2 π Θ表 • 示。周速比0係用以儘可能地使實驗結果不因直徑d、旋轉 數η、風速u的不同而改變者,升力係數(^亦被使用於用以 15使貫驗結果儘可能地不因風速u、旋轉圓柱的尺寸d、1或流 體密度p而改變者。 • 【表1】 15 129976920 According to the characteristics of 5H's because the rotating cylinder can be freely stretched and retracted, the rotating side column can be expanded and generated according to the natural L wind direction. In the general case, it is difficult to stretch, and the money wind becomes the largest, and the rotating cylinder is enlarged. In the case of strong winds, the __ side column is taken to make the wind-stop the collapse of the support table or the damage of the rotating cylinder. , Magna, the 12th item of the device patent scope, "Wind power generation, 1st or 2nd horse oil-type wind power generation device", which uses the number I to describe the drive motor and the number of required to rotate the cylinder According to this feature = two rotations of each rotating cylinder. π -h^\, p, and spoon are used to drive the power of the drive motor, so the power generation efficiency of the wind power generation device can be improved. The drawing shows a simple view of the front view of the brother 1 display device. The second picture shows the Magnus lift. The figure 3 shows the Magnus type of the embodiment 1 of the rotating Ding in the first picture. AA cross-section of a wind power cylinder. 10 1299769 Fig. 4 shows the normal phase diagram of the set ridges. Fig. 5 is a front view showing the rotating cylinder of the fifth embodiment in the back view of the second embodiment. Fig. 6 is a front view showing the rotating cylinder of the fifth member in the third embodiment. Fig. 7 shows a embossing of the ridge of the composite body. Fig. 7 shows a front view of the rotating cylinder provided with four in the embodiment 4. Fig. 8 shows a rotating cylinder in which the 绫 番 工The front view. Fig. 9 is a perspective view showing a rotating cylinder provided with two ridges. Fig. 10 is a front view showing the rotating cylinder in the embodiment 6. Fig. 11 is a perspective view showing the end cap in the seventh embodiment. Fig. 12 is a front elevational view showing the Magnus type wind power generator in the eighth embodiment. 15 Fig. 13 is a longitudinal sectional side view showing a rotating body of the Magnus type wind power generator in the ninth embodiment. The _ 帛 14 diagram shows the B-B longitudinal section back view of the rotating body in the figure. I: Solid package method] BEST MODE FOR CARRYING OUT THE INVENTION 20, Hereinafter, an embodiment of the present invention will be described. [Embodiment 1] A Magnus type wind power generation apparatus according to an embodiment of the present invention is not illustrated. First, FIG. 1 is a front view showing a Magnus type wind power generation apparatus according to an embodiment of the present invention, and a second view. Fig. 11 1299769 3 shows the A rhyme of the rotating cylinder in Fig. 1, and Fig. 4 shows the front view of the rotating cylinder with the ribs set. The mechanism for generating the lift of the Magnus-like Magnus, as shown in Fig. 2, hits the air flow system on the front side of the rotating cylinder C in the direction of rotation of the rotating cylinder c and the direction of the air flow in Fig. 2 The rotation of the rotating cylinder ^ flows upward, and at this time, the flow velocity of the air flowing on the upper side of the rotating cylinder c is faster than the air flowing on the lower side of the rotating cylinder c, so the upper side of the rotating cylinder C The negative pressure and the positive pressure on the lower side cause a difference in the air pressure, that is, a Magnus effect, and on the rotating cylinder C, a Magnus lift γ 产生 is generated in a direction perpendicular to the flow 10 of the air. The figure Α of the first drawing is applied to the Marvinas-type wind power generation apparatus of the present invention. The Magnus type wind power generation apparatus 8 is provided with a generator member 2 on the upper portion of the support table 1 which is erected on the ground, and the generator member 2 is a shaft that is rotatably supported in a horizontal direction centering on a vertical motor (not shown), and the 15 generator member 2 has a horizontal shaft 3 that is pivotally rotatably rotatable in a vertical direction. The end of the miscellaneous 3 is coupled to the = motor (not shown) disposed in the power generating component (10), and the other end of the horizontal rotating shaft 3 is fixed to the rotating body 4. 2, as shown in Fig. 1, six drive motors 15 are disposed inside the rotary body 4, and six rotating cylinders 5 are radially arranged on the outer circumference of the rotary body 4, and the bases of the respective rotary cylinders 5 are The drive motors 15 disposed inside the rotary body 4 are coupled to each other, and each of the rotary cylinders 5 is pivotally supported to be rotatable by driving of the drive motors. Further, a disk-shaped end cap 16 having a diameter larger than the diameter of the rotating circle is attached to the front end surface of the rotating cylinder 5. 12 1299769 The outer peripheral surface of the shaft of the ash turn 1] column 5 is wound around the body, and the wing element, that is, the spiral ridge 6 is formed, and the material of the large '/, 1 synthetic resin or the weather resistance is light. Alloy or the like = The ridge 6 is described. As shown in Fig. 4, the predetermined wide sound = 5 fixed height W ribs 6 are fixed in the right shape when viewed from the front end surface of the rotating cylinder 5. The Magnus-type wind power generator a shown in the figure 1 is used to detect the wind direction by a wind direction meter (not shown). The control circuit (two omitted) drives the vertical motor (not shown). As with the front side of the rotating body 4: ) 'The wind direction causes the generator member 2 to rotate. = Each of the shafts inside the swivel 4 is buckled so that each of the swivel (four) read squares and the first cylinder: the direction of rotation and the winding of the ridges 6, such as the 1 15 20 column 5 of the „^1^ reading cylinder 5 When the front end portion is viewed in the direction of rotation, when the winding method of the dog bar 6 is rotated to the right, the direction of rotation of the dog is turned to the left. 杈5 The direction of rotation of the cylinder 5 is opposite to the direction of the r and the rotation X The gas-side flow. In addition, the snail 2 in the spur 6: the direction of rotation and the rotation direction of the rotating cylinder 5 are the same as the outer circumference of the slewing cylinder 5 from the J, the melon moves in the (radiation direction) ^, air In a direction away from the horizontal rotation axis 3, a spiral protrusion 6 is provided on the cylinder 5, and the spiral protrusion 6 generates air to circulate the circumferential surface of the cylinder, except for the self-deflection. And the moving outward of the air of the surface of the rotating cylinder 5 with the twisting, and the other 13 5 can generate the flow division IV of the financialian with the rotating cylinder 5. As shown in the figure and the brother 4, by the spine (4) The air flow, the wind, and the three-dimensional air-rotating cylinder formed by the self-direction of the air flow with the rotating cylinder 5 The movement of the layer of air can be confirmed by the experiment described later;: phase group __2=::== force 10 and rotation circle (four): the sigh of the gas does not need to be fully divided, and at least parallel to the rotating cylinder 5 The vector is raised by the original wire. Although it is still nuclear, the Magnus lifts Y positive pressure: the difference is due to the negative pressure applied to the rotating cylinder 5 and the 15 phenomenon and the phenomenon that the lift surface is enlarged. In addition, when Xiang and cover 16, the point that can improve the Magnus effect is also true: month gP, by providing the end cover 于 on the front end surface of the rotating cylinder 5, the end cover 16 will have a positive influence on the air flow F. In addition, as will be described later, it can be seen from the experiment that when the end cap 16 is provided, the manner in which the air flows in the horizontal rotation axis direction is more efficient than the manner in which the line flows in the opposite direction. The Magnus effect is increased. 20 As shown in Fig. 1, the horse's turbulence γ' square turn 5 and the rotator 4 which are generated by the respective rotating cylinders 5 are rotated around the horizontal rotating shaft 3, and are The generator (not shown) connected to the _ end of the horizontal rotating shaft 3 is driven to be able to enter the power generation Then, by providing the spiral protrusion 6 to the rotating cylinder 5, the torque value (rotational moment) of the horizontal rotating shaft 3 for driving the generator (not shown) can be increased to improve the Magnus type wind power generation. The power generation efficiency of the device A 14 1299769 is slightly generated by the generator (10), and the dirt can be partially supplied to the drive horse for the rotating cylinder 5_ to use the auxiliary power. As a y... The rotation 1] column 5 used in the example is in the wind tunnel. The rotation cylinder 5 of the Magnus type wind in this embodiment is compared with the rotating cylinder of the invention and the ideal fluid 1 to 0 and the lift coefficient. Cyz shows in the table that the table shows the relationship between the weekly fan and the lift coefficient Cy, with the diameter of the rotating cylinder (10) as its own, and the number of rotations per second of the cylinder _ is η, the wind speed (m/s When fine, the (7) cycle speed ratio 旋转 of the circle ^ is 0=7Z; dn/U, the lift coefficient Cy is the lift γ divided by the kinetic energy of the wind per unit volume (1/2) pu2 and the projected area of the rotating cylinder. The value of the product along the length of the 1 series rotating cylinder is C y = 2 π 理想 in the ideal fluid. Show. The circumferential speed ratio 0 is used to make the experimental results not change due to the difference of the diameter d, the number of revolutions η, and the wind speed u. The lift coefficient (^ is also used to 15 to make the results of the inspection as unobtrusive as possible. The wind speed u, the size of the rotating cylinder d, 1 or the fluid density p change. • [Table 1] 15 1299769
周速比0 如表1所示,曲線⑷係顯示本發明的馬格納斯型周 發電裝置A的旋轉圓柱5的周軌Θ與升力係數Cy_ 5 10 曲線(口)係顯示ITAM(俄羅斯)的馬格納斯型風力發電裝 的旋轉圓柱的周速比Θ與升力係數Cy的關係,曲線 顯示多被採用於螺旋紫風車型的風力發電裝置 NACA4415葉片(_2度的螺旋槳葉請周速比θ (對 於旋轉圓柱的周速比Θ的換算值)與升力係數〇的關係£ mTAM的旋轉圓柱的曲線(口)及naca44i5葉片的 與本發明的旋轉圓柱5的曲線⑷相比較時,本發 及車τ圓柱5的曲線⑷係近似於理想流體(不須考慮摩 趣’理想上不會產生流_失的流體)的曲線。 ^特別是比較本發明的旋轉圓柱5的曲線⑷與叮歲 衿圓柱的曲線(口)時,於周速比Θ較低的狀態与L5 16 1299769 下)下’本發明的旋轉圓柱5的曲線(〇的升力係數Cy比 ITAM的旋轉圓柱的曲線(口)的升力係數Cy高。 此係顯示於旋轉圓柱的旋轉數η較低的狀態下,本發明 的馬格納斯型風力發電裝置Α的旋轉圓柱5可最有效率地產 生馬格納斯升力γ,本發明的馬格納斯型風力發電裝置A因 為旋轉圓柱5即使於較低的旋轉數n,亦可以高的馬格納斯 升力Y使水平疑轉軸3旋轉,故可節約用以旋轉驅動旋轉圓 柱5的驅動馬達15的消耗電力,可有效率地發電。 10 15 20 接著以表2及表3說明本實施例中的馬格納斯型風力 赉電裝置A的端蓋16與發電機構件2中的水平旋轉轴^的力 矩值(方疋轉力矩)與周速比0的關係。以下,於本實施例 中,將使流動於旋轉圓柱5的外周表面的空氣朝水平旋轉軸 3流動的旋轉圓柱5的旋轉方向稱為正旋轉,將使流動於旋 轉因柱5的外周表面的空氣朝遠離水平旋轉軸3的方向流動 的旋轉圓柱5的旋轉方向稱為逆旋轉。 表2係顯示使直㈣Φ的旋轉ϋ柱5正旋轉時的周速比 ⑽矩伽的關係之圖,曲線嶋^ 突條6及端蓋16的旋轉 置累旋狀的 周速比”力矩健的關係 5設置螺旋狀的突條6的旋轉圓柱5的周 速二:矩值Ν的關係之圖,曲線 旋狀的突條6的旋_柱财直徑Μ 〗時= 速比”力矩健的_# Δ ^ 係之圖,曲線W)係顯示於餘今詈嫘 6的旋轉圓柱5安裝直經2獅的端蓋^士的周 速比Θ與力矩值N的關係之圖。 17 1299769 2 表 15 里联:«The peripheral speed ratio 0 is as shown in Table 1, and the curve (4) shows the circumferential trajectory of the rotating cylinder 5 of the Magnus type peripheral power generating apparatus A of the present invention and the lift coefficient Cy_ 5 10 curve (port) showing the ITAM (Russia) The relationship between the circumferential speed ratio Θ and the lift coefficient Cy of the rotating cylinder of the Magnus type wind power installation is shown in the spiral windmill type wind power generator NACA4415 blade (the ratio of the propeller blade of the 2 degree degree is θ ( When the relationship between the peripheral speed ratio Θ of the rotating cylinder and the lift coefficient £ is the curve of the rotating cylinder of the mTAM (port) and the curve of the naca44i5 blade with the rotating cylinder 5 of the present invention (4), The curve (4) of the car τ cylinder 5 is similar to the ideal fluid (without considering the curve of the fluid that is ideally not generating flow_loss). ^ In particular, comparing the curve (4) of the rotating cylinder 5 of the present invention with the 叮 衿When the curve of the cylinder (port) is lower, the curve of the rotating cylinder 5 of the present invention is lower than the state of L5 16 1299769. The lift coefficient Cy is high. In the state in which the number of rotations η of the rotating cylinder is low, the rotating cylinder 5 of the Magnus type wind power generator of the present invention can generate the Magnus lift γ most efficiently, and the Magnus type wind power generation of the present invention Since the rotating cylinder 5 can rotate the horizontal suspect shaft 3 by the high Magnus lift Y even if the rotating cylinder 5 has a low rotation number n, the power consumption of the driving motor 15 for rotationally driving the rotating cylinder 5 can be saved. Power generation is efficient. 10 15 20 Next, the torque values of the horizontal rotation axis ^ of the end cap 16 of the Magnus type wind power generation device A and the generator member 2 in the present embodiment will be described with reference to Table 2 and Table 3. In the present embodiment, the rotation direction of the rotating cylinder 5 in which the air flowing on the outer peripheral surface of the rotating cylinder 5 flows toward the horizontal rotating shaft 3 is referred to as a positive rotation. The direction of rotation of the rotating cylinder 5 flowing in the direction away from the horizontal rotating shaft 3 by the air flowing on the outer peripheral surface of the column 5 is referred to as reverse rotation. Table 2 shows the case where the rotating column 5 of the straight (four) Φ is rotated. Weekly speed ratio The graph of the relationship of the moments of gamma, the curve 嶋^ The rotation of the ridges 6 and the end caps 16 is arranged in a swirling circumferential speed ratio. The relationship between the moments and the moments 5 sets the circumferential speed of the spiral cylinder 5 of the spiral ridges 6: the moment The graph of the relationship of the value Ν, the rotation of the curved ridge 6 of the curve _ 财 财 〗 〖 = speed ratio "torque robust _# Δ ^ system diagram, curve W) is shown in the future 詈嫘 6 The relationship between the circumferential speed ratio Θ and the torque value N of the end cap of the 2 lions is installed in the rotating cylinder 5 . 17 1299769 2 Table 15 Lilian: «
⑹有突條正旋轉 有端塞(200Φ ) .(c)有突條正旋轉 有端塞 ⑻有突條正旋轉 無端塞 %無突條 無端塞(6) There is a positive rotation of the ridge. There is an end plug (200Φ). (c) There is a positive rotation of the ridge. There is an end plug. (8) There is a positive rotation of the ridge. No end plug. No protrusion. No end plug.
冰f螺,未。又置螺知狀的突條6的旋轉圓柱5的曲線⑷及經 狀的突條6的旋轉圓柱5的正旋轉的曲線⑻,藉著 突條6由於可增大於旋轉圓柱5產生的馬格納斯升力Y,故經 設置突條6的旋轉圓柱5的曲線⑻的力矩值N比未設置突條 6的旋轉圓柱5的曲線(a)的力矩值n高。 又,於經設置螺旋狀的突條6的旋轉圓柱5的正旋轉的 曲線(b)及曲線(c)中,比較未設置端蓋16的旋轉圓柱5的曲 線(b)及經於旋轉圓柱5安裝直徑140Φ的端蓋16時的曲線( 18 10 !299769 4,设置端蓋16可提高於旋轉圓柱5的端蓋16附近產生的馬 袼納斯效應所產生的力矩值N,藉著設置端蓋16,於旋轉圓 杈5的前端面附近產生大的馬格納斯升力丫。即,經設置端 $ |16的旋轉圓柱5的曲線(c)的力矩值n比未設置端蓋16的 5旋轉圓柱5的曲線(b)的力矩值N高。Ice f screw, no. The curve (4) of the rotating cylinder 5 of the ridge 6 and the curve (8) of the rotation of the rotating cylinder 5 of the warp ridge 6 are formed by the ridges 6 which can be enlarged by the rotating cylinder 5 Since the lift force Y is set, the torque value N of the curve (8) of the rotating cylinder 5 through which the ridge 6 is disposed is higher than the torque value n of the curve (a) of the rotating cylinder 5 where the ridge 6 is not provided. Further, in the curve (b) and the curve (c) of the positive rotation of the rotating cylinder 5 in which the spiral ridges 6 are provided, the curve (b) of the rotating cylinder 5 in which the end cover 16 is not provided is compared and the rotating cylinder is rotated. 5 Curve when installing the end cap 16 with a diameter of 140Φ (18 10 !299769 4, the end cap 16 can be raised to increase the torque value N generated by the Martinas effect generated near the end cap 16 of the rotating cylinder 5, by setting The end cap 16 generates a large Magnus lift 附近 near the front end face of the rotating turn 5. That is, the torque value n of the curve (c) of the rotating cylinder 5 via the set end $ | 16 is smaller than the end value of the end cap 16 5 The torque value N of the curve (b) of the rotating cylinder 5 is high.
10 1510 15
2020
於正%轉日守,比較於叙轉圓柱5安裳直徑①的端蓋 16時的曲線⑷與於旋轉圓柱5安農直徑如⑽的端蓋16時的 線(d)安裝直控較大的端蓋16的旋轉圓柱5的曲線⑷的 力矩值N比安裝直徑較小的端蓋16的旋轉圓柱㈣曲線⑷ 的缝值N高。如表2所示,可明白藉著於經設置突條6的旋 專圓柱5安裝端蓋16,可產生較大的馬格納斯升力γ。 表3係顯示使旋轉圓柱5逆旋轉時的周速比θ與力矩值 顯示未設置螺旋狀的突條 16的旋轉圓柱5的周速比0盘 现 。力矩值N的關係之圖,曲線⑷ 員不5又置螺旋狀的突條6的旋轉圓柱5的周速比”力矩 值N的關係之圖,曲绫係 - r艟鬥a 於經設置螺旋狀的突條6的 _圓柱5安裝直徑聊的端蓋16_ N的關係之圖,曲線⑻係顯示細 ”力矩值 轉圓柱5安裝直徑2獅的群禮的突條6的旋 的關係之圖。 而」6時的周速比Θ與力矩值N 【表3】 19 1299769 (f) @有突條逆旋轉 有端塞(200 f) 汀)有突條逆旋轉 有端塞〇40必〉 _ (e)有突條逆旋轉 無端塞 •(幻無突條 無端塞 (e) (ay^ γ\λ η 9η λ αγ\ —-—」』 周速比β 20 比較未設置螺旋狀的突條⑽ 的曲線 設置螺旋狀的突條6的旋 /的曲線⑻及,‘ 於蕤荽”㈤、, Q柱5的心疋轉的曲線⑷時,由 、曰大1本可冒大於旋轉圓柱5產生的馬格納斯升力γ,故 料置突胸__的蝴e)的力矩拠未設置突 ίτ、6的方疋轉圓柱5的曲線⑷的力矩值n高。 於…又置螺凝狀的突條6的旋轉圓柱5的逆旋轉的曲線 ⑷及曲線(f)巾,比較未設置端蓋16的旋轉圓柱5的曲線(e) 及經於旋轉圓杈5安裝直徑14⑽的端蓋16時的曲線⑴時, 設置端蓋16可提高於旋轉圓柱5的端蓋16附近產生的馬格 20 10 1299769 納斯效應所產生的力矩值N,藉著設置端蓋16,於旋轉圓柱 5的前端面附近產生大的馬格納斯升力Y。即,經設置端蓋 16的旋轉圓柱5的曲線(f)的力矩值N比未設置端蓋16的旋轉 圓柱5的曲線(e)的力矩值N高。 5In the case of Yu Zhengyin, the curve (4) when compared with the end cover 16 of the diameter of the cylinder 5 is compared with the line (d) of the end cap 16 of the diameter of the rotating cylinder 5 (10). The torque value N of the curve (4) of the rotating cylinder 5 of the end cap 16 is higher than the slit value N of the rotating cylinder (four) curve (4) of the end cap 16 having a smaller mounting diameter. As shown in Table 2, it can be understood that a larger Magnus lift γ can be produced by attaching the end cap 16 to the spin-on cylinder 5 through which the ridges 6 are provided. Table 3 shows the peripheral speed ratio θ and the torque value when the rotating cylinder 5 is reversely rotated. The peripheral speed ratio 0 of the rotating cylinder 5 in which the spiral 16 is not provided is shown. A diagram showing the relationship between the torque value N and the curve (4): the relationship between the circumferential speed ratio of the rotating cylinder 5 of the spiral ridge 6 and the torque value N, the curve of the curve --r 艟 a Figure 7 shows the relationship between the diameter of the end cap 16_N of the diameter of the ribs 5, and the curve (8) shows the relationship of the rotation of the ridges 6 of the group of the lions with a diameter of 2 . And the circumferential speed ratio 力矩 and torque value N at 6 o'clock [Table 3] 19 1299769 (f) @There is a reverse rotation of the spurs with end plugs (200 f) Ting) There is a reverse rotation of the spurs and the end plugs 40 must> _ (e) There is a reverse rotation of the ridge without a tip plug. (The illusion is without a tip plug (e) (ay^ γ\λ η 9η λ αγ\ —-—”” The circumferential speed ratio β 20 is compared with no spiral protrusion. The curve of (10) sets the curve of the spiral protrusion 6 (8) and the curve of the heart of the Q column 5 (5), and the curve of the heart column of the Q column 5 (4). The generated Magnus lift γ, so the torque of the butterfly __ 的 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ The reverse rotation curve (4) and the curve (f) of the rotating cylinder 5 of the ridge 6 compare the curve (e) of the rotating cylinder 5 in which the end cover 16 is not provided and the end cover 16 through which the diameter 14 (10) is attached to the rotating circle 5 In the case of the curve (1), the end cap 16 is provided to increase the torque value N generated by the Mars 20 10 1299769 Nas effect generated near the end cap 16 of the rotating cylinder 5, by providing the end cap 16 in the rotating cylinder 5 Front end face A large Magnus lift Y is generated in the vicinity. That is, the torque value N of the curve (f) of the rotating cylinder 5 through which the end cover 16 is disposed is higher than the torque value N of the curve (e) of the rotating cylinder 5 in which the end cover 16 is not provided. 5
10 1510 15
20 於逆旋轉時,比較於旋轉圓柱5安裝直徑14〇φ的端蓋 16時的曲線(f)與於旋轉圓柱5安裝直徑2獅的端_時的 曲線(g),安裝直徑較大的端蓋16的旋轉圓柱5的曲線⑻的 力矩值安裝直錄小的端蓋16的旋轉圓柱5的曲線_ 力矩值N高。如表3所示,可明白藉著於經設置突條6的旋轉 圓柱5安裝端蓋16,可產生較大的馬格納斯升力γ。 又,如表2及表3所示,可明白經設置突條6等的空氣产 動機構的旋轉圓柱5的曲線(b〜g)的力矩值N比切置^ 流動機構的旋轉圓柱5的曲線⑻的力矩值N大,由此實驗姓 果可發現新的原理,即,與自然風或伴隨著旋轉圓柱5旋轉 的旋轉圓柱5表層的空氣的流動不同’藉著使於旋轉圓柱5 的外周表面產生空氣流動,可使藉著各旋轉圓柱㈣旋轉愈 風力的相互作用所產生的馬格納斯升力γ增大,於本實施例 中的馬格_型風力發㈣置財,成功地使肋驅動發電 機構件2的水平旋轉軸3的力矩似增大,使馬格納斯型風力 發電裝置Α的發電效率由低風速域跨較高風速域大幅地上 ^又^予空氣流時,安裝端蓋16者可提高馬格納斯效 應亦經貫驗證明。 21 1299769 圓柱5的外周表面的空氣朝水平旋轉軸3流動地正旋轉旋轉 圓柱5可更增大力矩值n,依此實驗結果可知,設置端蓋16 日寸,朝水平旋轉軸3的方向流動空氣的方式會比相反地朝遠 離水平旋轉軸3的方向(放射方向)流動空氣的方式更能增大 5 馬格納斯效應。 以下,以表4說明本實施例中的馬袼納斯型風力發電裝 置A的突條6及發電機構件2中的水平旋轉軸3的力矩值N (旋轉力矩)與風速u的關係。表4係顯示使旋轉圓柱5以旋 轉數1080〔mirf1〕旋轉時的風速u與力矩值N的關係之圖, 10曲線(h)係顯示未設置螺旋狀的突條6的旋轉圓柱5的風速u 與力矩值N的關係之圖,曲線⑴係顯示經設置螺旋狀的突條 6的旋轉圓柱5的風速u與力矩值n的關係之圖。 1 〇 -1 2 £ T/ 6 5 4 3 〔Z1 Masq: —---— 圓柱旋轉數 1080 [m i η *J] ζιζιζί -_— : ~ 一 _l_ ,- (h)夔塞(200W ;... :— 0 5 10 卜 風速 u [m/s] ° 25 即,比較未設置作為沿著旋轉圓柱5附加空氣流 15件的突條6的旋轉圓柱5的曲線⑻與經設置突條㈣ 圓 22 1299769 柱5的曲線⑴時,可明白未設置突條6的旋轉圓柱㈣曲線⑻ 的力矩值N無關於風速u幾乎成一定,相對於此,經設置突 • 條6的旋轉圓柱5的曲線⑴的力矩值N則伴隨著風速u成高^ 而增大,風力有效率地被轉換成馬袼納斯升力γ。 5 此係顯示由自然風中一般的風速為低速時至風速為高 速的強風時,本發明的馬格納斯型風力發電裝置八的旋轉: 柱5可最有效率地產生馬格納斯升力γ,因此,顯示可使水 平旋轉軸3的旋轉效率提高,可製錢量損失少的馬格納斯 # 型風力發電裝U,同時由自然風中的低速域至高速域都可 10 發電。 15 20 如录4所不,於未設置突條6的旋轉圓柱5的曲線⑻ 中,於風速讀施時,產生逆馬格㈣效應,力矩值_ 不負值,但於曲線⑴所示的經設置突條6的旋轉圓柱5中, 則顯示不易受到逆馬格納斯效應的影響力矩似增大。 休、本實施例中的馬格_型風力發電ΜΑ於屋 二:::貫驗’基於該實驗結果’以表5說明本實施例中 的馬格納斯型風力發電裝置A與螺旋樂型風 的《輪_之關係。㈣顯 2_本貫施例中的馬_斯魏力發職置 :力發電裝置的風速與發電輪斷圖,曲線二= =的螺旋槳型風力發衫置的風速與發電輸出圖, 雜)係喊不本貫施例中的馬格納斯型風力發電裝置 輸出w” ’曲線(1)係顯示年平均風速 的風速的雷利(啊)分佈之圖(觀職 23 1299769 【表5】 2500 200020 In the case of reverse rotation, the curve (f) when the end cap 16 of the diameter 14 〇φ is mounted on the rotating cylinder 5 is compared with the curve (g) when the end of the lion is mounted on the rotating cylinder 5, and the mounting diameter is large. The torque value of the curve (8) of the rotating cylinder 5 of the end cap 16 is mounted to the curve _ the torque value N of the rotating cylinder 5 of the directly recorded small end cap 16. As shown in Table 3, it can be understood that a larger Magnus lift γ can be produced by mounting the end cap 16 on the rotating cylinder 5 through which the ridges 6 are provided. Moreover, as shown in Table 2 and Table 3, it can be understood that the torque value N of the curve (b to g) of the rotating cylinder 5 of the air-producing mechanism provided with the ridges 6 and the like is smaller than that of the rotating cylinder 5 of the flow mechanism The torque value N of the curve (8) is large, and thus the experimental surname can find a new principle, that is, different from the flow of the natural wind or the surface of the rotating cylinder 5 which is rotated with the rotating cylinder 5, by making the rotating cylinder 5 The outer peripheral surface generates air flow, which can increase the Magnus lift γ generated by the interaction of the rotating winds of the respective rotating cylinders (four), and in the present embodiment, the horse-type wind power (four) is wealthy, successfully making The moment of the horizontal rotating shaft 3 of the rib drive generator member 2 is increased, so that the power generation efficiency of the Magnus type wind power generation device is greatly increased from the low wind speed region to the upper wind speed region, and the air is installed. The cover 16 can improve the Magnus effect and pass the test. 21 1299769 The air of the outer peripheral surface of the cylinder 5 flows toward the horizontal rotating shaft 3 and rotates the rotating cylinder 5 to increase the torque value n. According to the experimental results, the end cap is set to 16 inches and flows in the direction of the horizontal rotating shaft 3. The way of air increases the 5 Magnus effect more than the way of flowing air away from the horizontal axis of rotation 3 (radiation direction). In the following, the relationship between the torque value N (rotational moment) of the horizontal rotating shaft 3 and the wind speed u in the ridge 6 of the Martinas-type wind power generator A and the generator member 2 in the present embodiment will be described with reference to Table 4. Table 4 is a graph showing the relationship between the wind speed u and the moment value N when the rotating cylinder 5 is rotated by the number of revolutions 1080 [mirf1], and the curve (h) shows the wind speed of the rotating cylinder 5 in which the spiral protrusion 6 is not provided. u is a graph showing the relationship between the wind speed u and the torque value n of the rotating cylinder 5 in which the spiral ridge 6 is provided. 1 〇-1 2 £ T/ 6 5 4 3 [Z1 Masq: —---— Cylinder rotation number 1080 [mi η *J] ζιζιζί -_- : ~ a _l_ ,- (h) sputum (200W; ... : - 0 5 10 Bu wind speed u [m/s] ° 25 That is, the curve (8) of the rotating cylinder 5 which is not provided as the ridge 6 of the additional air flow 15 along the rotating cylinder 5 is compared with the set ridge (4) For the curve (1) of the circle 22 1299769 column 5, it can be understood that the torque value N of the rotating cylinder (4) curve (8) without the protrusion 6 is almost constant with respect to the wind speed u, whereas the rotating cylinder 5 of the protrusion 6 is provided. The torque value N of the curve (1) increases with the wind speed u becoming high, and the wind is efficiently converted into the horsepower γ. 5 This system shows that the natural wind speed is low speed to wind speed. At high speed and strong wind, the rotation of the Magnus type wind power generator 8 of the present invention: the column 5 can generate the Magnus lift γ most efficiently, so that the display can improve the rotation efficiency of the horizontal rotary shaft 3, and can make money. The Magnus # type wind power installation with less loss of quantity can be used from the low speed range to the high speed range in the natural wind. 10 Power generation 15 20 If the number is not 4, in the curve (8) of the rotating cylinder 5 where the ridge 6 is not set, the inverse Markov (four) effect occurs when the wind speed is applied, and the torque value _ is not negative, but the curve (1) In the illustrated rotating cylinder 5 of the set ridge 6, it is shown that the torque is less susceptible to the influence of the inverse Magnus effect. Hugh, the Marg-type wind power generation in the present embodiment is in the second house::: According to the results of the experiment, the relationship between the Magnus-type wind power generator A and the spiral-type wind in the present embodiment is described in Table 5. (4) Displaying the horse in the present embodiment Wei Lifa's position: the wind speed and power wheel break diagram of the power generation device, the wind speed and power generation output map of the propeller-type wind-powered shirt with curve 2 = =, the miscellaneous) is the Magnus-type wind power generation Device output w" 'curve (1) is a map showing the distribution of the wind speed of the annual average wind speed (observation 23 1299769 [Table 5] 2500 2000
ο ο ο ο 5 ο f . 1霉ο ο ο ο 5 ο f . 1 mildew
親«:S5:S«M 風速[m/s] 於年平均風速的制分佈的㈣⑴巾的風速相對度數 (%)的最高風速5m附近中,比較過去型的螺旋槳型風力發電 5裝置的曲線⑴的發電輪出w與本實施射的馬格納斯型風 力發電裝置A的曲線⑻的發電輸出W時,馬格納斯型風力 發電裝置A的曲線⑻的發電輸出贱螺旋槳型風力發電裝 置的曲線⑴的發電輸出W高。 又 " 其係顯示於全年平均產生最多的風速之 10下)之自然風中,本實施例中的馬格納斯型風力發電裳1 可以比螺㈣型風力發電裝置高的效率發電,若使用、本實 施例之馬格納斯型風力發電裝置A,相較於過去的螺旋樂^ 風力發電裝置,可確保較多的全年發電量。 〔實施例2〕 15 以下,參照第5圖說明實施例2之旋轉圓柱%的空 24 1299769 動機構。又,省略與前述構造相_造的重複說明。 第5圖係顯示實施例2中經設置複合體9b的旋轉圓柱5b 之正視圖’於旋轉圓柱5b的轴外周面—體被覆有複合體 ^ ’該複合體%係由被覆材8域作為本實施例中的空氣流 5動機構的翼元件、即螺旋狀的突條处組合而成於以合成 樹脂製或耐候性輕量合金製等構成的被覆⑽表面被凹凸 设置有多數的凹凸件7b,該螺旋狀的突條6b則以預定的引 導一體捲繞於該被覆材肋的表面。 1〇 如第5圖所示,藉著於旋轉圓柱%的表面設置凹凸件 :可增加旋轉圓柱5b的表面積,同時可以複數的凹凸件 表層流(交界層),使空氣的流域著螺旋狀的突祕 白卜月地流動於旋轉圓柱5b的表面,藉著產生於旋轉圓柱外 的相表面所產生的空氣流動蹄空氣流動分量V,可抑制 剝離並增加循環,使於旋轉圓柱513產生的馬格納斯 15 增大。 又,不使用被覆材8b,於旋轉圓柱5b的表面直接凹凸 叹置多數的凹凸件7b,於經凹凸設置凹凸件7b的旋轉圓柱 勺表面捲繞突條价亦可。又,於此所謂的凹凸件几係。 要是用以攪亂表層流的凹凸,為任何形狀皆可。 20 〔實施例3〕 以下,參照第6圖說明實施例3之旋轉圓柱父的空氣流 動機構。又,省略與前述構造相同構造的重複說明。 第6圖係顯示實施例3中經於複合體9c中的突條&設置 凹凸件7c的旋轉圓柱5c之正視圖,於旋轉圓柱5〇的軸外周 25 1299769 面/體被覆有複合體9C,該複合體9C係由經凹凸設置多數 的四凸件7c的被覆材以、被設置於該被覆材訃的表面的作 為本貫施例中的空氣流動機構的翼元件、即螺旋狀的突條 6c及被凹凸°又置於作為螺旋狀的突條6c的本實施例中的前 5端外表面的頂面1的多數凹凸件7c組合而成。 如第6圖所示,除了被凹凸設置於被覆材〜的多數的凹 凸件九外,藉著於螺旋狀的突條6c的頂面l〇c設置多數的凹 凸件7C,由於可以複數的凹凸件7c攪亂表層流(交界層),故 • 可使於旋轉圓柱5c產生的馬格納斯升力Y增加。又,藉著突 1〇條邰可使空氣圓滑地流動於旋轉圓柱5c的表面,可產生於 • %轉®柱5e的外周表面所產生的空氣流動F的空氣流動分 量V 〇 又’於遠作為複合體9c的突條6c中的前端外表面的頂 15 1〇<:中,除了凹凸件7c外,亦可突設半球狀的突起,凹凸 件或突起可攪亂突條6c的前端外表面的表層流,同時可 • 抑制剝離使循環增加,使於旋轉圓柱5c產生的馬格納斯升 力Y進一步增大。 〔貫施例4〕 2〇 以下’參照第7圖說明實施例4之旋轉圓柱5d的空氣流 動機構。又’省略與前述構造相同構造的重複說明。 第了圖係顯示實施例4中經設置凹條17d的旋轉圓柱5d 正視圖’於旋轉圓柱5d的軸外周面凹設有作為本實施例 中的空氣流動機構之螺旋狀的凹條17d,該凹條17d由旋轉 圓杈5d的前端面看時成右螺旋狀 ,同時於旋轉圓柱5d的前 26 1299769 10 15 端面被安裝有端蓋16d。 :’於使旋轉圓柱5d旋轉時’由旋轉圓柱_前端部 =看旋轉圓柱5d的凹細成右螺旋狀時,旋轉圓柱_ 二方向成左旋轉,凹條17d的螺旋捲繞方向與旋轉圓柱% 的旋轉方向相反。 因此,由於可使流動於旋轉圓柱5d的外周表面的空氣 朝水平旋轉軸側流動,故可於旋轉·_外周表面產生 空氣流動F’產生與旋轉圓㈣的軸平行的空氣流動分量 V’使於旋轉圓柱5d產生的馬格納斯升力γ增大且藉著咬 置,旋轉圓㈣的前端面的料16d,謂端蓋16^近= 空氣的流動造成影響,使於旋轉圓㈣的端蓋m附近產生 大的馬格納斯升力γ。 〔實施例5〕 以下,參照第8圖及第9圖說明實施例5之旋轉圓柱^ 的空氣流動機構。X,省略與前述構造相同構造的重複說 明 20 第8圖係顯示實施例5中經設置2條的突條㈣旋轉圓 柱5e之正視圖,第9圖係顯示經設置2條的突條⑽旋轉圓 柱5e之立體圖,於旋轉圓柱5e的軸外周面安裝有作為本每 施例中的空氣流動機構的翼元件、即2條螺旋狀的突條心, 該呈雙層螺旋的突條6e由旋轉圓柱5e的前端面看時被固定 成右螺旋狀,同時於旋轉圓柱5e的前端面被安裝有端笔 16e 又 ’被設置於旋轉圓柱5e的突條6e不限於2條螺旋, 以 27 1299769 3條、4條或其以上的多條的螺旋構成亦可,藉著設置多數 的突條6e,因為即使不增大螺旋的直徑,亦可使更多的空 氣藉突條6e圓滑地流動於旋轉圓柱5e的表面,故可於旋轉 圓柱5e的外周表面產生空氣流動F,產生與旋轉圓桎弘的軸 5平行的空氣流動分量V,使於旋轉圓柱5e產生的馬袼納斯效 應增大,增大馬格納斯升力γ。 〔實施例6〕 以下’蒼照第10圖說明實施例6之旋轉圓柱分的空氣流 動機構。又,省略與前述構造相同構造的重複說明。 10 第10圖係顯示實施例6中的旋轉圓柱5f之正視圖,於旋 轉圓柱5f的前端部附近的軸外周面被安裝有作為本實施例 中的空氣流動機構的翼元件、即2條突條6f。於旋轉圓柱5f 的前端部被設置有端蓋16f,同時藉著於_圓柱5f的前端 部附近被設置端蓋16f,可將於旋轉圓柱⑽前端部產生的 15 馬格納斯升力Y增大。 〔實施例7〕 以下,蒼照第11圖說明實施例7之旋轉圓柱々的空氣流 動機構。又,省略與前述構造相同構造的重複說明。 第11圖係顯示實施例7中的端蓋16g之立體圖,於旋轉 2〇圓柱5g的前端面被安裝有圓盤狀的端蓋16g,於該端蓋16g 面向疑轉圓柱5g的内面被設置有作為本實施例中的空氣流 動機構的複數的翼6g。該翼6g被安裝成朝外側成放射狀擴 展狀,同日^考曲地形成,以使旋轉圓柱城近的空氣流動。 使第11圖所示的旋轉圓柱5§正旋轉時,端蓋I6g附近的 28 1299769 工氣因為藉著設置於端蓋16g的翼知會被朝旋轉圓柱化側 拉進’故可於旋轉圓柱5g表面產生空氣流動,使於旋轉圓 產㈣馬格納斯升力丫增大。又,逆旋轉旋轉圓柱巧 4,因為會使端蓋l6g附近的空氣朝外側放出,故可於旋轉 圓板5g表面產生空氣流動,使於旋轉圓吻產生的馬格納 斯升力Y增大。 〔實施例8〕 以下,參知、苐12圖說明貫施例8之馬格納斯型風力發電 裝置A。又,省略與前述構造相同構造的重複說明。 10 第12圖係顯示實施例8中的馬格納斯型風力發電裝置a 的正視圖,馬格納斯型風力發電裝置A的旋轉圓柱25以相對 於旋轉體24被固定的内筒39及可自由滑動地被安裝於該内 筒39的外周的外筒40構成,外筒40藉著依照控制電路(圖示 省略)的控制被驅動的伸縮馬達(圖示省略),而可相對於水 15 平旋轉轴23於徑方向滑動。 於外筒40的軸外周面被固定有第4圖所示的實施例1中 的作為空氣流動機構的翼元件、即突條26,同時於被固定 於旋轉體24的内筒39的軸外周面被凹凸設置有第5圖所示 的實施例2中的多數的凹凸件7b。又,亦可將第6圖至第11 20圖所示的其他實施例3〜7中的空氣流動機構設置於内筒19 或外筒20。 如第12圖所示,藉著旋轉圓柱25呈可自由伸縮,可依 照自然風的風向或風速使旋轉圓柱25伸縮,於風速為低速 的一般情形時,可使旋轉圓柱25的外筒朝外側滑動,藉著 29 1299769 伸展旋轉圓柱25,可使旋轉圓柱25的受風面積成為最大, 使於旋轉圓柱25產生的馬格納斯升力γ增大,因此,可使馬 格納斯型風力發電裝置A有效率地發電。 又,於風速為尚速的強風時,可使旋轉圓柱25的外筒 5朝内側滑動,藉著縮短旋轉圓柱25,可使旋轉圓柱25的受 風面積變小,防止支持台21的倒塌或旋轉圓柱μ的破損。 於進一步的強風時,藉著停止驅動使旋轉圓柱25旋轉的驅 動馬達35,可使於旋轉圓柱25產生的馬格納斯升力γ消失, 分止旋轉體24的旋轉,防止破壞馬格納斯型風力發電裝置 10 A。特別是於本實施例中,由於具備突條%的外筒4〇存在於 方疋轉圓柱25的前端側,故可獲得最大限度的力矩。 〔實施例9〕 以下,參照第13圖及第14圖說明實施例9之馬格納斯型 風力务裝置。又,省略與前述構造相同構造的重複說明。 15 第13圖係顯示實施例9中的馬格納斯型風力發電裝置 之旋轉體41之縱截面侧視圖。第14圖係顯示第13圖中的旋 轉體41之縱截面背視圖。如第13圖所示,於與發電機構 件連、纟"的水平旋轉軸4 2的正面側的旋轉體41的外周被配置 有6根的旋轉圓柱43,於旋轉體41的内部被配置用以使旋轉 20圓柱43旋轉的1個驅動馬達44。 驅動馬達44與大直徑的傘狀齒輪45相連結,如第14圖 所不,該傘狀齒輪45被配置於旋轉體41的中心,同時與被 設置於6根的旋轉圓柱43的小直徑的傘狀齒輪牝相連結。使 驅動馬達44驅動時,可使6根的旋轉圓柱43旋轉,由於可使 30 1299769 用比旋轉圓桂43的根數少的驅動馬達44使各旋轉圓柱概 轉’故可節約用以驅動驅動馬達44的電力,可提高馬格納 斯型風力發電裝置的發電效率。 以上係以圖示說明本發明之實施例,但具體的構造並 5不限於該等實施例,於不脫離本發明的要旨之範圍内的變 更或追加亦包含於本發明中。 例如,於上述實施例中雖然係設置螺旋狀的突條作為 設置於旋轉圓柱的空氣流動機構,但本發明並不限定於 此,/、要形成可於旋轉圓柱的表面產生升力的面,以任何 10 方向賦予空氣流動皆可。 進而,於上述實施例中雖然於旋轉圓柱的前端面設置 圓盤狀的端蓋,但本發明並不限於此,只要能維持正壓側 與負壓側的壓力差,為任何形狀皆可。 又,於上述實施例中雖然於旋轉體設置6根的旋轉圓 I5柱,但本發明並不限於此,設置2根、3根或其以上的預定 根數的旋轉圓柱亦可。 產業之可利用性 依本發明之馬格納斯型風力發電裝置,可活用於大型 風力發電乃至於家庭用的小型風力發電,對風力發電業界 20有彳艮大的貢獻。進而,若將本發明之馬格納斯型的升力產 生機制利用於旋筒式風力推進船、旋筒式風力推進運栽工 具等,亦可提高交通工具的運動效率。 【圖式簡單說明3 第1圖係顯示本發明之實施例丨之馬格納斯型風力發電 31 12^769 裝置之正視圖。 第2圖係馬格納斯升力的說明圖。 第3圖係顯示第1圖中的旋轉圓柱之A-A截面圖。 5 第4圖係顯示經設置突條的旋轉圓柱之正視圖。 第5圖係顯示實施例2中經設置複合體的旋轉圓柱之正 視圖。 第6圖係顯示實施例3中經於複合體中的突條設置凹凸 件的旋轉圓柱之正視圖。 χ 第7圖係顯示實施例4中經設置凹條的旋轉圓柱之正視 υ圖。 第8圖係顯示實施例5中經設置2條突條的旋轉圓杈之 正视圖。 第9圖係顯示經設置2條突條的旋轉圓柱之立體圖。 第10圖係顯示實施例6中的旋轉圓柱之正視圖。 第11圖係顯示實施例7中的端蓋之立體圖。 第12圖係顯示實施例8中的馬袼納斯型風力發電裝置 之正視圖。 第13圖係顯示實施例9中的馬格納斯型風力發電裝置 之旋轉體之縱截面側視圖。 20 第14圖係顯示第13圖中的旋轉體之Β-Β縱截面背視圖。 【主要元件符號說明】 Α…馬格納斯型風力發電裝置 3···水平旋轉轴 L··支持台 4 #紅4 4···%轉體 2···發電機構件 5 H疋轉圓柱 32 1299769Pro «:S5:S«M wind speed [m/s] In the vicinity of the annual wind speed 5 (m) (1) wind speed relative degree (%) of the highest wind speed 5m, compare the curve of the past type propeller wind power 5 When the power generation output w of (1) and the power generation output W of the curve (8) of the Magnus type wind power generation apparatus A that is being launched are the output of the curve (8) of the Magnus type wind power generation apparatus A, the curve of the propeller type wind power generation apparatus (1) The power generation output W is high. In addition, the "the system is shown in the natural wind that produces the most wind speed in the whole year; the Magnus type wind power generator 1 in this embodiment can generate electricity at a higher efficiency than the screw (four) type wind power generation device, if With the use of the Magnus-type wind power generator A of the present embodiment, it is possible to secure a large amount of annual power generation compared to the conventional spiral wind power generation device. [Embodiment 2] 15 Hereinafter, a moving mechanism of the rotating cylinder % of the second embodiment will be described with reference to Fig. 5 . Further, overlapping descriptions of the above-described configurations are omitted. Fig. 5 is a front view showing the rotating cylinder 5b of the composite body 9b in the second embodiment. The outer peripheral surface of the rotating cylinder 5b is covered with a composite body. The composite body % is based on the domain of the covering material 8 In the embodiment, the wing element of the air flow mechanism, that is, the spiral ridge, is formed by a combination of a synthetic resin or a weather-resistant lightweight alloy, and the surface of the coating (10) is provided with a plurality of uneven portions 7b. The spiral protrusion 6b is integrally wound around the surface of the covering rib with a predetermined guide. 1 As shown in Fig. 5, a concave-convex member is provided by the surface of the rotating cylinder: the surface area of the rotating cylinder 5b can be increased, and at the same time, the surface flow (boundary layer) of the plurality of concave-convex portions can be made to make the air flow spiral The sudden flow of the white moon on the surface of the rotating cylinder 5b, by the air flow component V generated by the air generated from the surface of the rotating cylinder, can suppress the peeling and increase the circulation, so that the horse generated by the rotating cylinder 513 The Gunas 15 increased. Further, without using the covering material 8b, a large number of uneven portions 7b are directly slanted on the surface of the rotating cylinder 5b, and the ridges may be wound around the surface of the rotating cylindrical spoon provided with the uneven portion 7b. Moreover, here, the so-called unevenness is several. If it is used to disturb the unevenness of the surface flow, it can be any shape. [Embodiment 3] Hereinafter, an air flow mechanism of a rotating cylinder parent of Embodiment 3 will be described with reference to Fig. 6. Further, a repetitive description of the same configuration as the above configuration is omitted. Fig. 6 is a front view showing the rotating cylinder 5c of the ridges and the embossing member 7c provided in the composite body 9c in the embodiment 3, and the surface of the outer circumference of the rotating cylinder 5 25 25 1299769 is covered with the composite 9C. The composite body 9C is a wing member which is provided on the surface of the covering material by the covering material of the four convex members 7c which are provided with a large number of irregularities, and which is provided on the surface of the covering material, that is, a spiral protrusion The strip 6c and a plurality of concavo-convex members 7c which are placed on the top surface 1 of the outer surface of the front end 5 of the present embodiment as the spiral projection 6c are combined. As shown in Fig. 6, in addition to the plurality of uneven portions 9 provided with the unevenness of the covering material, a plurality of uneven portions 7C are provided by the top surface 10c of the spiral protruding strip 6c, and the plurality of concave and convex portions 7C can be used. The piece 7c disturbs the surface stream (junction layer), so that the Magnus lift Y generated in the rotating cylinder 5c can be increased. Further, the air can smoothly flow on the surface of the rotating cylinder 5c by the protrusion, and the air flow component V of the air flow F generated on the outer peripheral surface of the column 5e can be generated. In the top 15 1〇<: of the front end outer surface of the protrusion 6c of the composite body 9c, in addition to the unevenness piece 7c, a hemispherical protrusion may be protruded, and the uneven piece or protrusion may disturb the front end of the protrusion 6c. The surface flow of the surface, at the same time, can suppress the peeling and increase the circulation, so that the Magnus lift Y generated in the rotating cylinder 5c is further increased. [Example 4] 2 〇 Hereinafter, the air flow mechanism of the rotating cylinder 5d of the fourth embodiment will be described with reference to Fig. 7. Further, a repetitive description of the same configuration as the above configuration is omitted. The first drawing shows a rotating cylinder 5d in which the concave strip 17d is provided in the embodiment 4, and a spiral concave strip 17d which is an air flow mechanism in the present embodiment is recessed in the outer peripheral surface of the shaft of the rotating cylinder 5d. The concave strip 17d is formed in a right-handed spiral shape when viewed from the front end surface of the rotating round cymbal 5d, and an end cap 16d is attached to the front surface of the front 26 1299769 10 15 of the rotating cylinder 5d. : 'When the rotating cylinder 5d is rotated' is rotated by the rotating cylinder _ front end portion = when the concave portion of the rotating cylinder 5d is turned into a right spiral shape, the rotating cylinder _ two directions are rotated to the left, and the spiral winding direction of the concave strip 17d is rotated and the rotating cylinder % rotates in the opposite direction. Therefore, since the air flowing on the outer peripheral surface of the rotating cylinder 5d can flow toward the horizontal rotating shaft side, the air flow F' can be generated on the outer surface of the rotating outer surface to generate an air flow component V' parallel to the axis of the rotating circle (four). The Magnus lift γ generated in the rotating cylinder 5d is increased and by the biting, the material 16d of the front end surface of the circle (4) is rotated, that is, the end cover 16^n=the flow of the air is affected, so that the end cover of the rotating circle (4) A large Magnus lift γ is generated near m. [Embodiment 5] Hereinafter, an air flow mechanism of a rotating cylinder of Embodiment 5 will be described with reference to Figs. 8 and 9. X, a repetitive description of the same configuration as the foregoing structure is omitted. Fig. 8 shows a front view of the ridge (4) rotating cylinder 5e provided with two in the embodiment 5, and the ninth figure shows the ridge (10) which is set by two. A perspective view of the cylinder 5e is attached to the outer peripheral surface of the shaft of the rotating cylinder 5e with a wing element as an air flow mechanism in each of the embodiments, that is, two spiral-shaped ridges, and the double-spiral ridge 6e is rotated. The front end surface of the cylinder 5e is fixed in a right spiral shape, and the end pen 16e is attached to the front end surface of the rotating cylinder 5e. The ridge 6e provided on the rotating cylinder 5e is not limited to two spirals, to 27 1299769 3 A plurality of spirals of strips, four or more may be formed by providing a plurality of ridges 6e, because even if the diameter of the spiral is not increased, more air can be smoothly flowed by the ridges 6e. The surface of the cylinder 5e is such that an air flow F is generated on the outer circumferential surface of the rotating cylinder 5e, and an air flow component V which is parallel to the axis 5 of the rotating circular cymbal 5 is generated, so that the effect of the Martinus generated by the rotating cylinder 5e is increased. Increase the Magnus lift γ. [Embodiment 6] The air flow mechanism of the rotating cylinder of Embodiment 6 will be described below with reference to Fig. 10. Further, a repetitive description of the same configuration as the above configuration is omitted. 10 is a front view showing the rotating cylinder 5f in the embodiment 6, and the outer peripheral surface of the shaft near the front end portion of the rotating cylinder 5f is attached with a wing member as an air flow mechanism in the present embodiment, that is, two projections. Article 6f. The end cap 16f is provided at the front end portion of the rotating cylinder 5f, and the end cap 16f is provided near the front end portion of the cylinder 5f, so that the 15 Magnus lift Y generated at the front end portion of the rotating cylinder (10) can be increased. [Embodiment 7] Hereinafter, the air flow mechanism of the rotating cylindrical crucible of the seventh embodiment will be described with reference to Fig. 11. Further, a repetitive description of the same configuration as the above configuration is omitted. Fig. 11 is a perspective view showing the end cap 16g of the seventh embodiment, in which a disc-shaped end cap 16g is attached to the front end surface of the rotating 2〇 cylinder 5g, and the inner surface of the end cap 16g facing the suspected rotating cylinder 5g is set. There are a plurality of wings 6g as the air flow mechanism in the present embodiment. The wing 6g is installed to be radially expanded toward the outside, and is formed on the same day to flow the air near the cylindrical city. When the rotating cylinder 5 shown in Fig. 11 is rotated positively, the 28 1299769 process gas near the end cover I6g is pulled into the cylindrical side by the wing provided by the end cover 16g, so that the rotating cylinder 5g can be rotated. The surface generates air flow, which increases the lift of the Magnus. Further, by rotating the rotary cylinder 4 in the reverse direction, since the air in the vicinity of the end cover l6g is discharged to the outside, air flow can be generated on the surface of the rotating circular plate 5g, and the Magnas lift force Y generated by the rotating round kiss is increased. [Embodiment 8] Hereinafter, a Magnus type wind power generator A according to Embodiment 8 will be described with reference to FIG. Further, a repetitive description of the same configuration as the above configuration is omitted. 10 is a front view showing the Magnus type wind power generator a in the eighth embodiment, and the rotating cylinder 25 of the Magnus type wind power generator A is freely fixed to the inner cylinder 39 with respect to the rotating body 24 The outer cylinder 40 is slidably attached to the outer circumference of the inner cylinder 39, and the outer cylinder 40 is horizontally fixed with respect to the water by a telescopic motor (not shown) that is driven in accordance with control of a control circuit (not shown). The rotating shaft 23 slides in the radial direction. The outer peripheral surface of the outer cylinder 40 is fixed with the wing member 26 as the air flow mechanism in the first embodiment shown in Fig. 4, that is, the ridge 26, and is fixed to the outer circumference of the inner cylinder 39 of the rotary body 24. The uneven portion 7b of the plurality of the second embodiment shown in Fig. 5 is provided on the surface. Further, the air flow mechanisms of the other embodiments 3 to 7 shown in Figs. 6 to 11 may be provided in the inner cylinder 19 or the outer cylinder 20. As shown in Fig. 12, the rotating cylinder 25 is freely expandable and contractible, and the rotating cylinder 25 can be expanded and contracted according to the wind direction or wind speed of the natural wind. When the wind speed is low, the outer cylinder of the rotating cylinder 25 can be made to the outside. By sliding, by rotating the rotating cylinder 25 by 29 1299769, the wind receiving area of the rotating cylinder 25 is maximized, and the Magnus lift γ generated in the rotating cylinder 25 is increased, so that the Magnus type wind power generation device A can be Generate electricity efficiently. Further, when the wind speed is a strong wind at a constant speed, the outer cylinder 5 of the rotating cylinder 25 can be slid inward, and by shortening the rotating cylinder 25, the wind receiving area of the rotating cylinder 25 can be made small, and the support table 21 can be prevented from collapsing or Breaking of the rotating cylinder μ. In the case of further strong wind, by stopping the driving of the drive motor 35 that rotates the rotating cylinder 25, the Magnus lift γ generated in the rotating cylinder 25 can be eliminated, and the rotation of the rotating body 24 can be stopped to prevent damage to the Magnus type wind. Power generation device 10 A. In particular, in the present embodiment, since the outer cylinder 4 having the ridges % is present on the front end side of the square turn cylinder 25, the maximum torque can be obtained. [Embodiment 9] Hereinafter, a Magnus type wind power installation according to a ninth embodiment will be described with reference to Figs. 13 and 14. Further, a repetitive description of the same configuration as the above configuration is omitted. Fig. 13 is a longitudinal sectional side view showing the rotary body 41 of the Magnus type wind power generator in the ninth embodiment. Fig. 14 is a longitudinal sectional rear view showing the rotary body 41 in Fig. 13. As shown in Fig. 13, six rotating cylinders 43 are disposed on the outer circumference of the rotating body 41 on the front side of the horizontal rotating shaft 42 that is connected to the generator member, and are disposed inside the rotating body 41. A drive motor 44 for rotating the rotation 20 cylinder 43. The drive motor 44 is coupled to the large-diameter bevel gear 45. As shown in FIG. 14, the bevel gear 45 is disposed at the center of the rotating body 41 while being small-diameter with the rotating cylinders 43 disposed at six. The umbrella gears are connected to each other. When the drive motor 44 is driven, six rotating cylinders 43 can be rotated, and since 30 1299769 can be used to drive the rotating cylinders by a drive motor 44 having a smaller number than the rotating cylinder 43, the driving can be saved. The electric power of the motor 44 can increase the power generation efficiency of the Magnus type wind power generation device. The embodiments of the present invention are illustrated by the above description, but the specific configuration is not limited to the embodiments, and variations or additions within the scope of the gist of the invention are also included in the invention. For example, in the above embodiment, although a spiral protrusion is provided as the air flow mechanism provided in the rotating cylinder, the present invention is not limited thereto, and/or a surface capable of generating lift on the surface of the rotating cylinder is formed. Any 10 directions can be used to impart air flow. Further, in the above embodiment, the disk-shaped end cap is provided on the front end surface of the rotating cylinder. However, the present invention is not limited thereto, and any shape may be used as long as the pressure difference between the positive pressure side and the negative pressure side can be maintained. Further, in the above embodiment, six rotating circle I5 columns are provided in the rotating body, but the present invention is not limited thereto, and two or three or more rotating cylinders of a predetermined number may be provided. INDUSTRIAL APPLICABILITY The Magnus-type wind power generation device according to the present invention can be used for large-scale wind power generation or small-scale wind power generation for home use, and contributes greatly to the wind power generation industry 20. Further, the use of the Magnus type lift generating mechanism of the present invention can be utilized for a rotary wind propulsion ship or a rotary wind propulsion planting tool, and the moving efficiency of the vehicle can be improved. BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a front elevational view showing a device of the Magnus type wind power generation 31 12 769 of the embodiment of the present invention. Figure 2 is an explanatory diagram of the Magnus lift. Fig. 3 is a cross-sectional view showing the A-A of the rotating cylinder in Fig. 1. 5 Figure 4 shows a front view of the rotating cylinder with the ridges set. Fig. 5 is a front view showing the rotating cylinder of the composite body set in Embodiment 2. Fig. 6 is a front view showing the rotating cylinder in which the concavo-convex members are provided by the ridges in the composite body in the embodiment 3. χ Fig. 7 is a front elevational view showing the rotating cylinder in which the concave strip is set in Embodiment 4. Fig. 8 is a front view showing a rotary circle in which two ridges are provided in the embodiment 5. Fig. 9 is a perspective view showing a rotating cylinder provided with two ridges. Fig. 10 is a front view showing the rotating cylinder in the embodiment 6. Fig. 11 is a perspective view showing the end cap in the seventh embodiment. Fig. 12 is a front elevational view showing the Macinas type wind power generator in the eighth embodiment. Fig. 13 is a longitudinal sectional side view showing a rotating body of the Magnus type wind power generator in the ninth embodiment. 20 Fig. 14 shows a top view of the Β-anastole of the rotating body in Fig. 13. [Description of main component symbols] Α...Magnus type wind turbine 3···Horizontal rotation axis L··Support table 4 #红4 4···% Swiveling 2···Generator component 5 H疋Rotary cylinder 32 1299769
5b...旋轉圓柱 5c...旋轉圓柱 5d...旋轉圓柱 5e...旋轉圓柱 5f...旋轉圓柱 5g...旋轉圓柱 6...突條(空氣流動機構、翼元 件) 6b···突條(空氣流動機構、翼元 件) 6c...突條(空氣流動機構、翼元 件) 6e...突條(空氣流動機構、翼元 件) 6f...突條(空氣流動機構、翼元 件) 6g···翼(空氣流動機構) 7b...凹凸件 7c...凹凸件 8b...被覆材 8c...被覆材 9b...複合體 9c...複合體 10c···頂面(前端外表面) 15.. .驅動馬達 16.. .端蓋 16d...端蓋 16e···端蓋 16f...端蓋 16g...端蓋 17d···凹條(空氣流動機構) 19.. .内筒 20…外筒 21.. .支持台 23.. .水平旋轉軸 24.. .旋轉體 25.. .旋轉圓柱 26…突條(空氣流動機構、翼元 件) 35.. .驅動馬達 39.. .内筒 40.··外筒 41.. .旋轉體 42.. .水平旋轉軸 43.. .旋轉圓柱 44.. .驅動馬達 45.. .傘狀齒輪 46··.傘狀齒輪 335b...Rotating cylinder 5c...Rotating cylinder 5d...Rotating cylinder 5e...Rotating cylinder 5f...Rotating cylinder 5g...Rotating cylinder 6...Stroke (air flow mechanism, wing element) 6b··· truss (air flow mechanism, wing element) 6c... ridge (air flow mechanism, wing element) 6e... ridge (air flow mechanism, wing element) 6f... ridge (air Flow mechanism, wing element) 6g···wing (air flow mechanism) 7b...concave-convex 7c...concave-convex 8b...cladding material 8c...cladding material 9b...composite 9c... Composite body 10c··· top surface (front end outer surface) 15.. drive motor 16... end cover 16d... end cover 16e···end cover 16f... end cover 16g... end cover 17d ···Recessed strip (air flow mechanism) 19.. .Inner cylinder 20...outer cylinder 21.. Supporting table 23.. Horizontal rotating shaft 24.. Rotating body 25.. Rotating cylinder 26... protruding strip ( Air flow mechanism, wing element) 35.. Drive motor 39.. Inner cylinder 40.·. Outer cylinder 41.. Rotating body 42.. Horizontal rotating shaft 43.. Rotating cylinder 44.. Drive motor 45.. .Umbrella gear 46··.Umbrella gear 33
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TWI710501B (en) * | 2019-06-27 | 2020-11-21 | 周中奇 | Magnus rotor |
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CN112141308A (en) * | 2019-06-27 | 2020-12-29 | 周中奇 | Magnus Rotor |
US11143159B2 (en) | 2019-06-27 | 2021-10-12 | Chung-Chi Chou | Magnus rotor |
CN112141308B (en) * | 2019-06-27 | 2022-02-01 | 周中奇 | Magnus rotor |
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