TW200419076A - High efficiency ceiling fan - Google Patents

High efficiency ceiling fan Download PDF

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TW200419076A
TW200419076A TW92122108A TW92122108A TW200419076A TW 200419076 A TW200419076 A TW 200419076A TW 92122108 A TW92122108 A TW 92122108A TW 92122108 A TW92122108 A TW 92122108A TW 200419076 A TW200419076 A TW 200419076A
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Taiwan
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fan
blade
angle
attack
ceiling fan
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TW92122108A
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Chinese (zh)
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TWI309695B (en
Inventor
Gregory Michael Bird
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Hunter Fan Co
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Priority claimed from US10/223,333 external-priority patent/US6719533B2/en
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Publication of TWI309695B publication Critical patent/TWI309695B/en

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Abstract

Ceiling fan energy consumption efficiency is enhanced with fan blades that have an angle attack that decreases from root end to tip end at higher rates of decrease nearer their tip ends than at their root ends. Air flow distribution is enhanced with at least a portion of the blades having a dihedral that continuously increases. Efficiency on downdraft is also achieved with the blades having concave top and bottom surfaces.

Description

200419076 玖、發明說明: 【發明所屬之技術領域】 凊序號之 本案為2002年7月30日錄案第綠申 邵分接續申請案。 本發明關於吊扇,特別是電動吊扇及其效率。 【先前技術】 多年來由電動馬達所驅動之吊扇已運用於空氣循環,其 通常具有-位於罩框内且安裝至直桿之馬達,使風扇葉^ 以直桿之軸線旋轉。傳統之風扇葉片為扁平狀,且其傾斜 方:或斜度在轉動時提供空氣一攻角,使空氣向下流動。 當自其旋轉軸徑向伸展之風扇葉片轉動時’,葉片尖端之 移動路徑在任何時間皆係遠大祕部端之移動路徑,因此 葉片尖端移動之速度遠快於根部端。為平衡沿著葉片及其 移動所產生氣流之風阻負載,風扇葉片係設計具有一朝向 尖端縮小之攻角,此設計特徵常見於其他旋轉葉片之設計 中’例如船隻螺旋槳葉及飛機螺旋槳葉。200419076 发明 Description of the invention: [Technical field to which the invention belongs] The serial number of this case is the green application filed on July 30, 2002. The invention relates to ceiling fans, in particular electric ceiling fans and their efficiency. [Prior art] For many years, ceiling fans driven by electric motors have been used for air circulation. They usually have a motor located in the hood and mounted to a straight rod, so that the fan blade ^ rotates on the axis of the straight rod. The traditional fan blades are flat and have an oblique side: or the inclination provides an angle of attack of the air when rotating, so that the air flows downward. When a fan blade extending radially from its axis of rotation rotates, 'the movement path of the blade tip is at any time the path of the great secretion end, so the blade tip moves much faster than the root end. In order to balance the wind resistance load along the airflow generated by the blades and their movements, the fan blades are designed with a reduced angle of attack towards the tip. This design feature is common in the design of other rotating blades, such as boat propeller blades and aircraft propeller blades.

Flonda Solar Energy Center在 1997年中執行一有關數個 市場可購得吊扇之效率研究,此測試報告發表在美國第 M39,54m專财’財卿所有者發現風扇葉片之設計 可&升此量效率,即每功率消耗(waUs)之氣流量(cfM), 該葉片在根部端漸次的彎曲而向下均勻的窄縮為較小之彎 曲或為尖端之攻角,例如20英吋長之葉片(含窄縮之弦狀部 )根部具有26.7。之-曲,在尖端具有69。之彎曲。 另-與吊扇有關JL長期存在之問題是氣流之分佈。葉片Flonda Solar Energy Center carried out a study on the efficiency of commercially available ceiling fans in mid-1997. This test report was published in the U.S. M39,54m Financial Specialist's owner found that the design of fan blades can be increased. Efficiency, which is the air flow rate (cfM) per power consumption (waUs), the blade gradually bends at the root end and narrows down evenly to a smaller bend or an angle of attack, such as a 20 inch blade (Including the narrowed string-shaped part) The root has 26.7. Zhi-qu has 69 at the tip. Of the bend. Another-The long-standing problem with ceiling fans related to JL is the distribution of airflow. blade

87191.DOC 200419076 具有一攻角之方位,惟大部分吊扇之葉片係在一水平面中 轉動’此迫使芝氣向下而在風扇下方提供氣流,因氣流並 非直接自風扇處流動,故周遭之氣流不足。由於風扇葉片 之結構為雙曲面的,此可減輕該問題之影響,惟其需考量 風扇下方氣流之不足。 【發明内容】 吾人已知攻角或扭角以均一之速率縮小對吊扇而言並非 最有效率的。二呎長之葉片或螺旋槳葉尖端所移動一圈之 圓周為2 Π (2),因此其一呎中點或長度一半移動之距離為2 Π(1),此線性關係對飛機螺旋槳葉係洽當的,因其移動之 軌道路徑通常落在垂直於飛行路徑之平面中。然而吊扇轉 動之軌道路徑平行且位於氣流下方,故葉片並非均勻的撞 擊空氣,其與飛機不同,此現象之原因為吊扇葉片尖端處,, 且換空氣之效益大於葉片尖端内側。旋轉軸線附近之空氣 須自周遭環境移動經過天花板面與風扇葉片之間的空間而 到達其i部端。 由於上述事項,吾人已認知具有攻角之葉片可提昇吊扇 效率,孩攻角自根部端非均勻的擴大至尖端,特別是葉片 尖端處攻角或斜度之改變速率大於根部處改變之速率。這 點可迫使天花板下方風扇葉片向内置換空氣,故葉片根部 端附近之艾氣較易置換。但無論此理論是否正確,其已譁 明效率之提昇。因葉片尖端處攻角之變化大於根部處之攻 角變化,其表示風扇效率將明顯的提昇。 具有向上曲線之吊扇葉片亦可改善氣流分佈,該葉片形87191.DOC 200419076 has an angle of attack, but the blades of most ceiling fans are rotated in a horizontal plane. This forces the chi gas downward and provides airflow under the fan. Because the airflow does not flow directly from the fan, the surrounding airflow insufficient. Because the fan blades are hyperbolic, this can reduce the impact of this problem, but it needs to consider the lack of airflow under the fan. [Summary of the Invention] We know that reducing the angle of attack or twisting angle at a uniform rate is not the most efficient for ceiling fans. The circumference of a two-foot blade or the tip of a propeller blade is 2 Π (2), so the distance of one-foot midpoint or half of the length is 2 Π (1). This linear relationship is consistent with the aircraft propeller blade system. When it does, the path of its orbit usually falls in a plane perpendicular to the flight path. However, the orbital path of the ceiling fan is parallel and located below the airflow, so the blades do not hit the air uniformly, which is different from the aircraft. The reason for this phenomenon is that the tip of the ceiling fan blade, and the benefit of air exchange is greater than the inside of the blade tip. The air near the axis of rotation must move from the surrounding environment through the space between the ceiling surface and the fan blades to the end of the i-section. Due to the above matters, we have realized that blades with angle of attack can increase the efficiency of ceiling fans. The angle of attack increases non-uniformly from the root end to the tip, especially the rate of change of the angle of attack or slope at the tip of the blade is greater than the rate of change at the root. This can force the fan blades below the ceiling to displace air inward, so the moxa gas near the root end of the blade is easier to replace. But whether this theory is correct or not, it has made clear the improvement in efficiency. Since the change in the angle of attack at the blade tip is greater than the change in the angle of attack at the root, it means that the fan efficiency will be significantly improved. Ceiling fan blades with upward curves can also improve airflow distribution.

87191.DOC 20041907687191.DOC 200419076

之成果不僅是效率提昇, 成果不僅是效率提昇,氣流分佈亦較佳。 成漸次之雙曲面,其係自根部端延續至尖端 可配合所述攻角或扭角非均勻之縮減加以The result is not only an increase in efficiency. The result is not only an increase in efficiency, but also a better air distribution. Into a progressive hyperbola, which extends from the root end to the tip, and can be matched with the non-uniform reduction of the angle of attack or twist

度約小於沿著兩側邊厚度之25% 。 【實施方式】 風扇葉片技術揭示於美國第6,039,541號專利,其假設流 入風扇葉片之空氣皆來自垂直於葉片旋轉平面之方向。此 外,當運用於飛機螺旋槳葉理論時,其假設氣流以固定速 度自葉片根部流至尖端。藉由此假設,葉片自根部至尖端 具有一定之扭速。 葉片之扭轉欲使相對於葉片表面之氣流方向相對攻角最 佳化,此可確保葉片由根部至尖端在最佳之攻角下操作。 攻角係變化以符合葉片尖端移動之速度大於葉片根部移動 之速度’該速度之提昇使葉片上風的方向改變。 此假设對吊扇而言係無效的。吊扇為空氣循環裝置,其 未如同飛機螺旋槳葉一般使空氣移動,空氣自葉片根部端 至尖端並未以相同之向量或速度移動。 圖1顯示傳統構造之吊扇,除了其葉片之輪廓外。風扇利 用一向下直桿安裝在天花板下方,該直桿自天花板伸展至 電動馬達及開關盒外框,且風扇在底端處具有一套輕裝置 。電力供應至馬達導體驅動葉片,導體經由該向下直桿伸The degree is less than about 25% of the thickness along both sides. [Embodiment] The fan blade technology is disclosed in U.S. Patent No. 6,039,541, which assumes that the air flowing into the fan blades comes from a direction perpendicular to the plane of rotation of the blades. In addition, when applied to aircraft propeller blade theory, it assumes that airflow flows from the blade root to the tip at a fixed speed. Based on this assumption, the blade has a certain twisting speed from the root to the tip. The twisting of the blade is to optimize the relative angle of attack with respect to the direction of the airflow relative to the blade surface. This ensures that the blade operates from the root to the tip at the optimal angle of attack. The angle of attack changes to match the speed at which the blade tip moves faster than the speed at which the blade root moves'. The increase in this speed changes the direction of the blade upwind. This assumption is invalid for ceiling fans. Ceiling fan is an air circulation device. It does not move air like the propeller blade of an airplane. The air does not move at the same vector or speed from the blade root to the tip. Figure 1 shows a conventional ceiling fan, except for the outline of its blades. The fan is installed under the ceiling by a straight down bar, which extends from the ceiling to the electric motor and the outer frame of the switch box, and the fan has a light device at the bottom end. Electricity is supplied to the motor conductor driving blades through which the conductor extends

87191.DOC 200419076 展至一局部電源。 螺旋狀之風扇葉片優於平坦狀之風扇葉片、且具有漸次 之雙曲面。到達及離開風扇葉片之氣流以多條箭頭線顯示 ,藉此可理解為何風扇葉片並非如飛機螺旋槳葉一般衝擊 艾氣,且葉片上方限定之空間使進入風扇之氣流向量改變 ’其與飛機螺旋槳葉相反。 如圖2所示,風扇葉片隨著其寬度及弦窄縮,其自底部或 根部端至尖端窄縮,故尖端之尺寸較小。此外,葉片皆具 有圖1所示之雙曲面,惟其並非能具體實施本發明之優點。 雙曲面在風扇下方提供較大之空氣分佈。 參見圖2及3,雖然葉片為單一之構造,圖式顯示葉片具 有三個部位。24英对長之葉片具有三個長度相同之部位, 即8英忖,其皆以圖β式扭轉,惟自根部扭轉至尖端之速 率不同。扭角或攻角自根部端縮小為尖端之1〇。,如圖丨所 示’此縮小以三種不同之速率進卜與根部端相鄰之第一 個8英叶-部位中扭轉之速率變化為〇4〇/英叶,中間部位之 速率為〇.7。/英叶’與尖端相鄰之第三個部位中扭轉之速率 變化為i.O。/料^ #然’相鄰部位之間存有些許之轉換。 因此’圖3中自外侧部位-端至另—端之攻角差異為⑼。/ 英忖X8H)’中間部位之差異約為6。,内側部位 約為3°。 〃 圖5至7詳示圖i風扇之葉片1〇,其根部端u安裝至風扇 達轉子如,尖端13位讀之末^如圖丨所示,較以天 板垂直向下直桿之軸線旋轉’最清楚的係以葉片中心綠87191.DOC 200419076 to a local power source. Spiral fan blades are superior to flat fan blades and have a progressive hyperboloid. The airflow reaching and leaving the fan blades is shown with multiple arrow lines, so that you can understand why the fan blades do not impact the moxa like the propeller blades of an aircraft, and the space defined above the blades changes the vector of the airflow entering the fan. in contrast. As shown in Fig. 2, the fan blade narrows with its width and chord. It narrows from the bottom or root to the tip, so the tip size is smaller. In addition, the blades all have the hyperboloid shown in FIG. 1, but they are not the advantages of the present invention. The hyperboloid provides a larger air distribution under the fan. Referring to Figs. 2 and 3, although the blade has a single structure, the figure shows that the blade has three parts. A blade with a length of 24 inches has three parts of the same length, namely 8 inches, which are all twisted in the form of β, but the rate of rotation from the root to the tip is different. The twist angle or angle of attack is reduced from the root end to 10 of the tip. , As shown in Figure 丨 'This reduction at three different rates into the first 8-inch leaf adjacent to the root end-the rate of change in the twist in the site is 0/40, the rate of the middle part is 0. 7. The change rate of torsion in the third part adjacent to the tip is i.O. / 料 ^ # 然 ’There is a slight conversion between adjacent parts. Therefore, the difference in the angle of attack from the outer side to the other side in FIG. 3 is ⑼. / 英 忖 X8H) 'The difference in the middle part is about 6. , The inner part is about 3 °. 〃 Figures 5 to 7 show the blade 10 of the fan i in detail. The root end u is mounted to the fan and the rotor. Rotate 'the clearest line with the center of the leaf green

87191.DOC 200419076 顯示,葉片在根部端U具有0。之雙曲面,在尖端13且有i〇c 之雙曲面d、風扇葉片兩端之間呈連續的弧形或彎曲,故 其雙曲面在兩端之間係連續的變化。如圖㈤線所示之氣流 分佈,艾氣直接分佈在風扇下方以及其周遭之空間中。相 反的,先前技藝之風扇主要將空氣導至其下方,故周遭空 間中之氣流非直接流動且較弱。雖然沿著長度以固定之雙 曲面傾斜之風扇葉片可解決此問豸,惟其需考量風扇下; 較弱之氣流。 、葉片雙曲面可在兩端之間持續的變化,惟靠近根部端及/ 或尖端時為固定的,其餘部位為弧形或曲線狀。事實上, 參見轉鳥之設計’最有效率之設計為自根部端至尖端之中 間處之雙曲面為G。’之後持續增加到達尖端為1()。。在較佳 具體實施例中,葉片根部端具有G。之雙曲面,尖端具有1〇。 之雙曲面,惟根部端之雙曲面可小於或大於〇。,尖端之雙 曲面可小於或大於心風扇尺寸、功率、高度及應用皆= 選取特定雙曲面之考量因素。 吊扇能夠以傳統方式反向操作,如圖8A所示,由下方觀 視時葉片係順時針轉動,在此方向中及其攻角,葉片以箭 頭所示方向使空氣向上,這點為空調中常見之例子,其向 下抽離風扇上方之熱空氣。如圖8β所示,葉片亦可逆時針 旋轉,其在較熱之環境下將空氣吹至人們使其冷卻。吾人 發現厚度不一之葉片可提昇效率,其顯示於圖8C,葉片自 側邊窄縮至側邊。葉片1 Q之頂端如底端一般略微的凹陷, 故中空凹陷處位於其根部與尖端之間。可產生最佳效率之87191.DOC 200419076 shows that the blade has 0 at the root end U. The hyperbola has a continuous arc or curve between the two ends of the fan blade at the tip 13 and ioc. The hyperbola has a continuous change between the two ends. As shown in the line ㈤, the airflow is distributed directly below the fan and in the surrounding space. In contrast, the fans of the previous technology mainly guided the air below it, so the air flow in the surrounding space was indirect and weak. Although fan blades inclined with a fixed hyperboloid along the length can solve this problem, they need to consider the fan; weaker airflow. The blade hyperbola can be continuously changed between the two ends, but it is fixed near the root end and / or the tip, and the rest is arc or curved. In fact, see the design of Zhuan Niao ’, the most efficient design is that the hyperboloid from the root to the middle of the tip is G. After that, it continues to increase to 1 (). . In a preferred embodiment, the root end of the blade has G. The hyperboloid has 10 at the tip. Hyperboloid, but the hyperboloid at the root can be less than or greater than 0. The tip hyperboloid can be smaller or larger than the core fan size, power, height, and application = considerations for selecting a particular hyperboloid. The ceiling fan can be operated in the traditional reverse direction, as shown in Figure 8A. When viewed from below, the blades rotate clockwise. In this direction and its angle of attack, the blades make the air upward in the direction shown by the arrow. A common example is to pull down the hot air above the fan. As shown in Figure 8β, the blades can also rotate counterclockwise, which blows air to people to cool them in a hot environment. I have found that blades of different thicknesses can increase efficiency, which is shown in Figure 8C, where the blades narrow from the side to the side. The top of the blade 1 Q is slightly depressed like the bottom, so the hollow depression is located between its root and tip. Which produces the best efficiency

87191.DOC -9- 200419076 葉片係沿著中心部位之厚度小於兩側邊部位厚度約25%, 且頂面及底面宜具有相同之輪廓。吾人尚不瞭解這點優於 一平坦表面、縮小攻角及雙曲面變化之原因。為便於說明 及澄清,圖8 C僅顯示沿著平面8 - 8之風扇葉片。 當葉片以圖8B所示方式旋轉形成向下氣流時,葉片側邊 之間厚度的改變使效率提昇3%至4%,若以圖8A方向轉動 時,效率之變化不明顯,吾人已完全瞭解其成因,特別是 僅一表面凹陷時效率之提昇較少。 風扇在Hunter Fan Company之實驗室測試,其通過環保 機關之認證執行Energy StarC〇mpHance測試。除了空氣速 度偵測器仍安裝在葉片頂端上方及附近之外,風扇根據 Energy Star測試規定加以測試,這點可量測風扇葉片附近 之空氣速度。測試過程中測得葉片根部端至尖端 不同位置 處之不同空氣速度,圖4顯示測試參數,實際之測試結果揭 示於表1。 偵測器 平均速度 空氣速度 FPM FPS 0 283 4.7 1 303 5.1 2 320 5.3 3 325 5.4 4 320 5.3 5 313 5.2 31.487191.DOC -9- 200419076 The thickness of the blade along the center is less than about 25% of the thickness on both sides, and the top and bottom surfaces should have the same profile. I do not yet understand why this is better than a flat surface, reduced angle of attack, and hyperbolic variation. For ease of illustration and clarification, FIG. 8C shows only the fan blades along plane 8-8. When the blade is rotated in the manner shown in FIG. 8B to form a downward airflow, the change in thickness between the sides of the blade increases the efficiency by 3% to 4%. If it is rotated in the direction of FIG. 8A, the efficiency change is not obvious. The reason for this, especially when only one surface is recessed, the efficiency improvement is small. The fan is tested in the Hunter Fan Company's laboratory and it is certified by the Environmental Protection Agency to perform the Energy Star CompHance test. Except that the air speed detector is still installed above and near the top of the blade, the fan is tested according to the Energy Star test regulations, which measures the air speed near the fan blade. During the test, different air velocities were measured at different positions from the root to the tip of the blade. Figure 4 shows the test parameters. The actual test results are shown in Table 1. Detector Average Speed Air Speed FPM FPS 0 283 4.7 1 303 5.1 2 320 5.3 3 325 5.4 4 320 5.3 5 313 5.2 31.4

合成 合成 角度/ 速度 角度 英乞 23.2 11.7 24.9 11.7 0.07 26.7- 11.5 0.16 28.4 11.0 0.54 30.1 10.2 0.79 31.8 9.4 0.76 ^ 87191.DOC -10- 200419076 6 308 5.1 33.1 33.5 · 8.8 0.63 7 305 5.1 34.9 35.3 8.3 0.51 8 290 4.8 36.6 37.0 7.5 0.77 9 275 4.6 38.4 38.7 6.8 0.71 10 262 4.4 40.1 40.4 6.2 0.60 11 235 3.9 41.9 42.0 5.3 0.87 12 174 2.9 43.6 43.7 3.8 1.54 13 132 2.2 45.4 45.5 2.8 1.03 比較性之測試結果顯示於表2,其中葉片1具有前述之10° 固定雙曲面,葉片2為第6,039,541號專利所示設計之 Hampton Bay Gossomer Wind/Windward葉片,葉片 3為具有 1 5。固定攻角之平坦葉片。如前文所界定,表列為能源效率 之改良。 表2 葉片 馬達 含圓柱 體 優於 Hampton Bay之改 良 優於標 準之改 良 無圓 柱體 優於 Hampton Bay之改 良 外側4英 呎之改 良 1 172 X 18 AM 12,878 21% 29% 37,327 24% 27% 2 188X15 10,639 NA 6% 30,034 NA NA 3 172X 18 AM 10,018 -6% NA 28,000 -7% -7% 87191.DOC -11 - 200419076 ^此’所示吊扇強化氣流分佈使能源效率優於先前技藝 :當然,風扇亦可應用於例如桌頂之其他糾。雖然本文 ^車乂佳具體實施例加以揭示,惟其他變更、改良或刪除事 項皆在本發明申請專利範圍之精神及範疇中。 【圖式簡單說明】 圖1為吊扇之側視圖,其為本發明一較佳具體實施例。 圖2為圖1風扇葉片之輪廓,其以假設之平面以利說明。 圖3為圖2葉片之輪廓,其顯示葉片沿著長度在不同位置 的螺旋。 圖4為氣流測試參數之圖形。 圖5為圖1風扇一葉片之側視圖。 圖6為圖1風扇一葉片之上視圖。 圖7為圖1風扇一葉片之端視圖。 圖8 A及8 B為圖1風扇一葉片之其他側視圖,其以剖面顯 示’圖8C為葉片沿著平面8-8之剖視圖。 【圖式代表符號說明】 10 11 12 13 15 葉片 根部端 軟 尖端 中心線Synthetic composition angle / speed angle 23.2 11.7 24.9 11.7 0.07 26.7- 11.5 0.16 28.4 11.0 0.54 30.1 10.2 0.79 31.8 9.4 0.76 ^ 87191.DOC -10- 200419076 6 308 5.1 33.1 33.5 · 8.8 0.63 7 305 5.1 34.9 35.3 8.3 0.51 8 290 4.8 36.6 37.0 7.5 0.77 9 275 4.6 38.4 38.7 6.8 0.71 10 262 4.4 40.1 40.4 6.2 0.60 11 235 3.9 41.9 42.0 5.3 0.87 12 174 2.9 43.6 43.7 3.8 1.54 13 132 2.2 45.4 45.5 2.8 1.03 Comparative test results are shown in Table 2 Among them, the blade 1 has the aforementioned 10 ° fixed hyperboloid, the blade 2 is a Hampton Bay Gossomer Wind / Windward blade of the design shown in the 6,039,541 patent, and the blade 3 has 15. Flat blade with fixed angle of attack. As defined earlier, the table lists improvements in energy efficiency. Table 2 Blade motors with cylinders are better than Hampton Bay, better than standard modified, no cylinder is better than Hampton Bay, modified 4 feet outside, improved 1 172 X 18 AM 12,878 21% 29% 37,327 24% 27% 2 188X15 10,639 NA 6% 30,034 NA NA 3 172X 18 AM 10,018 -6% NA 28,000 -7% -7% 87191.DOC -11-200419076 ^ The ceiling fan's enhanced airflow distribution shown here makes energy efficiency better than previous technologies: Of course, fans It can also be applied to other corrections such as table tops. Although the specific embodiments of the present invention are disclosed herein, other changes, improvements, or deletions are within the spirit and scope of the scope of patent application of the present invention. [Brief description of the drawings] FIG. 1 is a side view of a ceiling fan, which is a preferred embodiment of the present invention. FIG. 2 is the outline of the fan blade of FIG. 1, which is illustrated by a hypothetical plane. Figure 3 is the outline of the blade of Figure 2, showing the spiral of the blade at different locations along its length. Figure 4 is a graph of airflow test parameters. 5 is a side view of a blade of the fan of FIG. 1. 6 is a top view of a fan blade of FIG. 1. FIG. 7 is an end view of a blade of the fan of FIG. 1. FIG. Figs. 8A and 8B are other side views of a fan blade of Fig. 1, which are shown in section. Fig. 8C is a sectional view of the blade along plane 8-8. [Illustration of Symbols] 10 11 12 13 15 Blade Root End Soft Tip Center Line

87191.DOC87191.DOC

Claims (1)

200419076 拾、申請專利範圍: 1. :種《複數個風扇葉片之吊扇,該等葉片被安裝成以 葉片旋轉之直立風扇軸線轉動,各風扇葉片之兩加長侧 邊部位位於-加長中央部位之外側,且其中各風扇葉片 <薇中央部位厚度小於兩側邊部位之厚度。 2. 減中請專利_第1項之吊扇,其中沿著其中心線之各 葉片厚度小於該側邊部位最大厚度約25%。 3. 根據申請專利範圍第巧之吊扇,其中各葉片之該兩例邊 部位及該中央部位皆大致自各葉片之根部端伸展至尖端。 4. 根據申請專利範圍第卜頁之吊扇,其中各葉片具有一凹陷 之頂面及底面。 5·根據申請專利範圍第1項之吊扇,其中各該風扇葉片朝向 其尖端向上彎曲而具有連續漸次之雙曲面·。 6·根據申請專利範圍第5項之吊扇,其中各葉片纟根部端之 雙曲面約為0。,在尖端之雙曲面約為1〇。。 7·根據中請專利範圍第巧之吊扇,其中各葉片靠近 軸線之攻角大於該風扇軸線末端之攻角,且其間=角之 變化率不一致。 8·根據申請專利範圍第7項之吊扇,其中各葉片在尖端之雙 曲面約為10。,攻角約為1〇。。 9·根據令請專利範圍第5項之吊扇,其中各葉片靠近該風扇 軸線之攻角大於該風扇軸線末端之攻角,且其間攻角之 變化率不一致。 中各葉片在根部端之 1 〇 ·根據申請專利範圍第9項之吊扇,其 87191.DOC 200419076 雙曲面約為0。,在尖端之雙曲面約為10。。 11. 12. 13. 14. 15. -種具有複數個風扇葉片之吊扇,其葉片具有凹陷之頂 面及展面,被安裝成以葉片旋轉之直立風扇轴線在兩方 向中轉動。 根據申請專利範圍第11項之吊扇,其中該葉片頂面及底 面具有相同之輪廓。 根據申請專利範圍第12項之吊扇,其中各葉片朝向其尖 端向上彎曲而具有連續漸次之雙曲面。 根據申請專利範圍第12項之吊扇,其中各葉片靠近該風 扇軸線之攻角大於該風扇軸線末端之攻角’且其間攻角 之變化率不一致。 根據申請專利範圍第13項之吊扇,其中各葉片靠近該風 扇轴線之攻角大於該風扇軸線末端之攻角,且其間攻角 之變化率不一致。 87191.DOC200419076 The scope of patent application: 1. A type of "ceiling fan of a plurality of fan blades, which are installed to rotate with the vertical axis of the fan rotating blades, and the two extended side parts of each fan blade are located outside the extended central part And the thickness of each fan blade < Wei central part is smaller than the thickness of the two side parts. 2. Minus patents_ ceiling fan of item 1, wherein the thickness of each blade along its centerline is less than about 25% of the maximum thickness of the side portion. 3. The ceiling fan according to the scope of the patent application, wherein the two edge portions and the central portion of each blade extend approximately from the root end to the tip of each blade. 4. According to the ceiling fan of the scope of patent application, each blade has a concave top surface and a bottom surface. 5. The ceiling fan according to item 1 of the scope of the patent application, wherein each of the fan blades is curved upward toward its tip to have a continuous progressive hyperbola. 6. The ceiling fan according to item 5 of the patent application, wherein the hyperbola at the root end of each blade is approximately zero. , The hyperbola at the tip is about 10. . 7. According to the patent application of the ceiling fan, the angle of attack of each blade near the axis is greater than the angle of attack at the end of the axis of the fan, and the change rate of the angle = angle is inconsistent. 8. The ceiling fan according to item 7 of the scope of patent application, wherein the hyperbola of each blade at the tip is about 10. , The angle of attack is about 10. . 9. The ceiling fan according to item 5 of the patent, wherein the angle of attack of each blade near the axis of the fan is greater than the angle of attack at the end of the axis of the fan, and the rate of change of the angle of attack is inconsistent. 10 of the blades at the root end of the blade. According to the ceiling fan of item 9 of the patent application scope, its 87191.DOC 200419076 hyperboloid is about 0. , The hyperbola at the tip is about 10. . 11. 12. 13. 14. 15.-A ceiling fan having a plurality of fan blades, the blades of which have recessed top surfaces and spreading surfaces, are mounted to rotate in two directions with the vertical fan axis of the blade rotation. The ceiling fan according to item 11 of the patent application, wherein the top and bottom surfaces of the blade have the same contour. A ceiling fan according to item 12 of the patent application, wherein each blade is curved upward toward its pointed end to have a continuous progressive hyperboloid. According to the ceiling fan of claim 12, wherein the angle of attack of each blade near the axis of the fan is greater than the angle of attack at the end of the axis of the fan 'and the rate of change of the angle of attack is inconsistent. According to the ceiling fan of the patent application No. 13, the angle of attack of each blade near the axis of the fan is greater than the angle of attack at the end of the axis of the fan, and the rate of change of the angle of attack is inconsistent. 87191.DOC
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