TW200427930A - Centrifugal blower - Google Patents
Centrifugal blower Download PDFInfo
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- TW200427930A TW200427930A TW93115201A TW93115201A TW200427930A TW 200427930 A TW200427930 A TW 200427930A TW 93115201 A TW93115201 A TW 93115201A TW 93115201 A TW93115201 A TW 93115201A TW 200427930 A TW200427930 A TW 200427930A
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- discharge
- centrifugal blower
- casing
- discharge port
- fluid
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
- F04D29/44—Fluid-guiding means, e.g. diffusers
- F04D29/441—Fluid-guiding means, e.g. diffusers especially adapted for elastic fluid pumps
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
Description
200427930 玫、發明說明: 【發明所屬之技術領域】 ^本發明,係有關使用於空調設備或換氣設備等、具備 灰渴狀之機殼的離心送風機。 【先前技術】 第5圖,係顯示具備習知旋渦狀機殼之離心送風機之 1冓成的縱截面圖。離心送風機2〇〇,係具備機殼1 〇、及内 藏方、A機设丨〇之漩渦室的葉片輪丨1。機殼1 〇之排放口 1〇&之軸向中心線12、與通過葉片輪11之軸線且與排放口 1〇a,之軸向同方向之中心線(以下稱為第1中心線)CU,兩 者平行,相隔既定距離。 該離心送風機200之機殼10之排放口 1Ga中,流過其 ° ^^之机體之流動比流過内周側之流體之流動還快。因 此右連接於排放口 l〇a之配管之彎曲方向與葉片輪u之 轉方向相同,則流體沿配管之彎曲流動,故沒有大的壓 力損失,而當配管之彎曲方向與葉片輪u之旋轉方向相反 1在配管之彎曲部分,流動快之部分之流體導致大的壓 力扣失。因此,有無法獲得既定風量的問題。 對此’以往係如第6A圖及第6β圖所示,在將流體往 同方向(圖巾’上方)送風的情形,與連接於機殼1 0之排 二口 W的配管之f曲方向相對應,分別準備2種旋轉方 °疋或左方疋)不同的葉片輪、及與其對應之機殼10。 該機殼 離心送風機 10,係與驅動葉片輪11之馬達15 —起設置於 200之基台14上。若葉片輪11之旋轉方向相 200427930 同,且僅改變流體之排放方向13,則分別如第Μ圖、第 6C圖及第6E圖所示,將相同之機殼丨〇,以排放口 }仏之 軸向中心線12與各流體之排放方向13(圖中之上方、 及右方)大致-致之方式設置於基台14上。然而,因:裝 於機叙1 0之基台14的部分之形狀互里 <办狀互異,故必須對應流體 之排放方向13準備3種基台。 同樣地,若葉片輪卩之旋轉方向與上述不同,則如第 6B圖、“D圖及“F圖所示,將相同之機㈣,以排放 口心之軸向中心線12與各流體之排放方向13 (圖中之 上方、左方及右方)大致—致之方式設置於基台“上。在 此情形,亦與上述同樣地必須準備3種基台丨4。 【發明内容】 基於上述原因,以往必須準備至少6種有相同性能之 離心送風冑⑽。因此,有離心送風機咖之生產性差、 庫存管理亦繁雜的問題。 子b可如第7A圖所示,將以2點鏈線代表之習知 土 钱冗又1 0 ’以排放口 1 Oa之軸向中心線12 二近上述葉片輪11之第1中心線CL1之方式配置於基台 。接著,於該機殼10之排放口 10a安裝肘接頭16且 使石亥機设1 〇之排放200427930, Description of the invention: [Technical field to which the invention belongs] ^ The present invention relates to a centrifugal blower provided with a gray-like casing for use in air-conditioning equipment or ventilation equipment. [Prior Art] Fig. 5 is a longitudinal sectional view showing a centrifugal blower provided with a conventional vortex-shaped casing. The centrifugal blower 200 is a vane wheel 1 provided with a casing 10 and a vortex chamber with a built-in side and an A machine. The centerline 12 of the axial direction of the discharge opening 10 of the casing 10, and the centerline passing through the axis of the blade wheel 11 and the same direction as the axial direction of the discharge opening 10a (hereinafter referred to as the first centerline) CU, the two are parallel, separated by a predetermined distance. In the discharge port 1Ga of the casing 10 of the centrifugal blower 200, the flow of the body passing through it is faster than the flow of the fluid flowing through the inner peripheral side. Therefore, the bending direction of the pipe connected to the discharge port 10a is the same as the turning direction of the vane wheel u, so the fluid flows along the bending of the pipe, so there is no large pressure loss. Opposite direction 1 In the bent part of the piping, the fluid that flows fast causes a large pressure drop. Therefore, there is a problem that a predetermined air volume cannot be obtained. In this regard, as shown in FIG. 6A and FIG. 6β, in the case where the fluid is sent in the same direction (above the figure), the direction of f-curve is the same as that of the pipe connected to the two ports W of the casing 10 Correspondingly, two kinds of blade wheels with different rotation directions (° 疋 or left 疋) are prepared, and the corresponding casing 10 is prepared. The casing centrifugal blower 10 is arranged on a base 14 of 200 together with a motor 15 driving a blade wheel 11. If the rotation direction of the blade wheel 11 is the same as 200427930, and only the discharge direction 13 of the fluid is changed, as shown in Fig. M, Fig. 6C and Fig. 6E, respectively, the same casing is used as the discharge port. The axial centerline 12 and the discharge direction 13 (upper and right in the figure) of each fluid are arranged on the base 14 in a substantially consistent manner. However, since the shapes of the parts of the abutment 14 mounted on the machine 10 are mutually different, the three types of abutments must be prepared corresponding to the discharge direction 13 of the fluid. Similarly, if the rotation direction of the blade wheel 卩 is different from the above, as shown in Fig. 6B, "D" and "F", the same machine ㈣ is used to discharge the axial centerline 12 of the center of the mouth and the fluid The discharge direction 13 (upper, left, and right in the figure) is set on the abutment "in a uniform manner. In this case, three kinds of abutments must be prepared in the same way as above. [Contents of the invention] Based on For the above reasons, at least 6 kinds of centrifugal fans with the same performance must be prepared in the past. Therefore, there are problems that the centrifugal fans have poor productivity and complicated inventory management. As shown in Figure 7A, sub-b can be linked in two points. The conventional knowledge represented by the line is redundant and is arranged on the abutment in a manner close to the first center line CL1 of the blade wheel 11 in the axial center line 12 of the discharge port 1 Oa. Next, in the casing 10 An elbow joint 16 is installed at the discharge port 10a and the Shihai machine is set to discharge at 10
Wa之軸向中心線12與葉片輪11之 弟1中心線CL1 一致。从, 欠口此’於肘接頭16之端部新形成之 排放口 16a之軸向+、、妗t 中〜線12a與葉片輪11之第1中心線 IL1 一 致。 猎此’上述流動快之流體便靠近上述新的排放口 16a 200427930 之中央部附近,即便將連拯於兮祕4 “ %接於邊排放σ 16a之配管,往與 茱片輪11之方疋轉方向同方向彎曲 ^ 弓曲遇疋彺相反方向彎曲, 在言曲部分亦難以發生流㈣夕 生桃體之剝離等現象。結果,能防止 大的壓力損失發生。 然而,在此情形,因肘接 耵接頭16新安裝於機殼10之排 放口 10 a ’故與習知情飛★曰μ ’有機殼10變大且壓力損失 變大的問題。 貝天 對此’在日本特開平I〗 …门^ U U4393唬公報所揭示之離心 达風機201中,機殼1〇,係 ^ Α 宁如弟7β圖所不,以排放口 1 〇a 之軸向中心線12靠近荤片私 π十二 茱片輪11之第1中心線CL1且朝相 同方向之方式,將機殼1 〇 排放口 10a附近之一部分17The axial centerline 12 of Wa coincides with the centerline CL1 of the younger brother 1 of the blade wheel 11. Therefore, the axial direction of the discharge opening 16a newly formed at the end of the elbow joint 16 is +, and the center line 12a is consistent with the first center line IL1 of the blade wheel 11. The above-mentioned fast-flowing fluid will be near the central part of the new discharge port 16a 200427930. Even if you connect Lian Zhengyu Secret 4 "% to the side discharge σ 16a, go to the side of the round 11 The direction of rotation is the same as the bending direction. ^ The bow is bent in the opposite direction, and it is difficult to cause the peeling of the flowing peach in the song. As a result, large pressure loss can be prevented. However, in this case, because The elbow joint connector 16 is newly installed at the discharge port 10 a of the casing 10. Therefore, it ’s familiar and familiar with flying. Μ μ “The organic casing 10 becomes larger and the pressure loss becomes larger. Beitian responds to this” in Japanese Patent Application Laid-Open I 〗… The door ^ U U4393 disclosed in the centrifugal fan 201, the casing 10, ^ Α Ning Rudi 7β diagram, the axial centerline 12 of the discharge port 10a is close to the cymbal private π The first centerline CL1 of the twelve dog disc wheels 11 faces the same direction as the first center line CL1, and a portion 17 near the discharge port 10a of the casing 17
削掉而形成。藉此,如上沭無τ W 10a._B+4i 这叙,不必於機殼10之排放σ 丄Ua设置肘接頭16便能佶瓿# > 綠19 ▲ 使此使新形成之排放口 l〇b之軸向中心 線12a罪近葉片輪η夕筮ί + U之幻中心線CL1且朝相同方向。 猎此’如上述般,離心送風機2 離心送風機201之擴散写邻Μ” 然而,Shaved to form. With this, as described above, there is no τ W 10a._B + 4i, and it is not necessary to set the elbow joint 16 for the discharge σ 机 Ua of the cabinet 10 to ampoule # > Green 19 ▲ This makes the newly formed discharge port l〇 The axial centerline 12a of b is near the blade wheel η 筮 筮 + U of the magic centerline CL1 and faces the same direction. Hunting this ’as described above, the diffusion write of the centrifugal blower 2 and the centrifugal blower 201” However,
> $ & 〃政态邛18變短,故無法將該部分】S 之流速充分減速,該部分 18 … 1 8之壓力損失增加,而有籬 迗風機201之性能降低之問題。 具體來說,如第8 η 一 _ 所7F ’相對於習知離心送風機之> $ & 〃policy state 18 is shorter, so the flow velocity of this part] S cannot be fully decelerated, the pressure loss of this part 18… 18 is increased, and the performance of the fan 201 is reduced. Specifically, as the 8th η _ 所 7F ′ compared to the conventional centrifugal blower
八里 清塵之曲線L1,裳7D ^ 1第圖所示之離心送風機 —靜壓之曲線L2县分十知m <風置 么士果 同風量下靜壓變小的方向移動。 、、…有在既:之靜遷下無法獲得既定風量之問題。 此藉著加長上述擴散器部1 8來抑制壓力損失 W 口 ’但如上述般有離心送風機變大的問題。 、 200427930 焉示 因此’本發明’係用以解決以上之問題而開發者 :二:提供一種離心送風機,相較於習知離心送風機, b在)±月匕不降低下減少種類。 :發明為一種離心送風機’係於旋渦狀之機殼内藏有 葉片輪,且於機殼具備:排放通路’設置成該通路之排放 口之軸向中心線通過葉片輪之軸 ,、 =通路之排放口附近,其流路向外彎曲且沿流體之排放 方向逐漸擴大,用來使流過其内側之流體高效率地減速。 依據上述構成,在離心送風機之排放通路之排放口, 流動快之流體能接近中央部附近,並且能使在當中流動之 流體高效率地減速。因此,即便將連接於排放通路之配管 在與葉片輪之旋轉方向同方向彎曲或往相反方向彎曲,在 遠背曲部分亦難以發生流體之剝離等,故不發生大的壓力 損失。藉此,能在不降低離心送風機之性能之下,使離心 送風機之葉片輪之旋轉方向,從以往之2種變成}種。 此外’該減速部’亦可分別形成於排放通路之排放口 附近之與葉片輪之軸向同方向之兩側。 一般,離心送風機之;i^ 排放通路之排放口附近之葉片輪 之徑向之兩側之内面,得>VL嬙M a、^ 你^喊之漩渦形狀來形成,故在 這部分不發生大的愿力損失。相對於此,在離心送風機之 排放通路之排放口附近之與葉片輪軸向之兩側之内面,離 心送風機之排放通路之排放口之與葉片輪轴向同方向之寬 度尺寸比機成之與葉片輪轴向同方向之寬度尺寸還大, 200427930 故兩内面之相隔距離往排放口逐漸擴大。因此,有時在該 t放通路内流動之流體從排放通路之内面發生剝離等,而Λ :生大的壓力損失。因& ’本發明,為了防止這現象,而 ::6亥部分設置減速部。藉此,能防止壓力損失之增加,故 能防止離心送風磯之性能之降低。 、此外,上述減速部之f曲部分之曲率半徑最好為排放 通路之排放口之内徑之5〜20%。The curve of Bali dust dust L1, the centrifugal fan shown in figure 7D ^ 1—static pressure curve L2 counties are divided into ten knowledge m < wind set moss fruit and the direction of static pressure becomes smaller under the same air flow. ,, ... There is a problem that the established air volume cannot be obtained under the relocation. This lengthens the diffuser portion 18 to suppress the pressure loss W port ′, but there is a problem that the centrifugal blower becomes large as described above. 200427930 Indications Therefore, the present invention was developed to solve the above problems. Second: Provide a centrifugal blower. Compared with the conventional centrifugal blower, b) reduce the types without reducing the moon dagger. : The invention is a centrifugal blower, which is attached to a vortex-shaped casing with a vane wheel, and the casing is provided with: a discharge passage, which is arranged so that the axial centerline of the discharge port of the passage passes through the axis of the vane wheel, and = passage Near the discharge port, the flow path is curved outward and gradually expanded along the discharge direction of the fluid, which is used to efficiently decelerate the fluid flowing through its inside. According to the above configuration, at the discharge port of the discharge path of the centrifugal blower, a fast-flowing fluid can approach the vicinity of the central portion, and the fluid flowing therein can be efficiently decelerated. Therefore, even if the pipe connected to the discharge passage is bent in the same direction as the direction of rotation of the vane wheel or bent in the opposite direction, the peeling of the fluid is difficult to occur in the far back curved portion, so no large pressure loss occurs. Thereby, the rotation direction of the blade wheel of the centrifugal blower can be changed from the conventional two types to the second type without reducing the performance of the centrifugal blower. In addition, the "deceleration portion" may be formed on both sides of the discharge passage in the same direction as the axial direction of the blade wheel, respectively. Generally, the inner surfaces of both sides of the radial direction of the blade wheel near the discharge opening of the centrifugal blower are formed by> VL 漩涡 M a, ^ you ^ shouting vortex shape, so it does not occur in this part Great loss of will. On the other hand, the inner and outer sides of the discharge path of the centrifugal blower near the two sides of the blade wheel in the axial direction, and the width and size ratio of the discharge port of the centrifugal blower's discharge path in the same direction as the axial direction of the blade wheel are compared The width of the wheel in the same direction is still large. 200427930 Therefore, the distance between the two inner surfaces gradually increases toward the discharge port. Therefore, the fluid flowing in the discharge path may be peeled off from the inner surface of the discharge path, and Λ may cause a large pressure loss. Because of the & ' s present invention, in order to prevent this phenomenon, a :: 6hai portion is provided with a deceleration portion. Thereby, an increase in pressure loss can be prevented, and thus a decrease in performance of the centrifugal fan can be prevented. In addition, it is preferable that the radius of curvature of the f-curved portion of the deceleration portion is 5 to 20% of the inner diameter of the discharge opening of the discharge passage.
_依據上述構成,在離心送風機之排放通路内流動之流 體在減速部高效率地減速。藉此,能防止壓力損失之增加 能防止離心送風機之性能之降低。又,若減速部:彎 曲部分之曲率半徑小於排放通路之排放口之内徑之5%,則 減速部太短而無法使流體高效率地減速。X 彎曲部分之曲率半徑大於排放通路之排放口之内 ’則機殼變大。 【實施方式】 發明之最祛形能 以下’筝照圖式說明本發明之實施形態。 ^第1A圖所[離心、送風機_,係具備㈣狀機殼 、及忒置於該機殼i之璇渦室u内的葉片輪2。於 具備排放通路lb’該通路113之流路從旋涡室1&之出:擴 大。如第1B圖所示,旋渦室la之流路截面大致呈矩形狀 ’该流路截面從璇渦室la經排放通路化漸漸變為圓形, 在排放通路1 b之排放口 1C成為圓形。 其次’該排放口 lc之軸向中心線3,係與通過葉片輪 10 之軸線、且與排放口 lc MAM ^ 心孕由向同方向之中心線(以下, 私為弟I中心線)CU大致一 ,在1 a 亦即,上述軸向中心線〔 係通過葉片輪2之軸線。 藉此,能使流動比較快的户縣 M ^ r, Ί 〕/巩體接近離心送風機100之 卜放口 1 c之中央部附近。社 之^〜本 、、°果,即便將連接於排放口 lc 之配官(未圖示),往與葉月於 μ 4± ± 、 兩 之旋轉方向同方向彎曲, 攻^王相反方向彎曲,在續蠻ώ # , ^ σ弓曲σ卩分亦難以發生流體之剥離 寻,故此防止發生大的壓力損 貝失猎此,能將葉片輪2之 疋轉方向,從以往之2種統一為!種。 示且步詳細說明,該排放通路ib,係如第1。圖所 ,”i “以使流過其内側之流體高效率地減速之減速部4 之路1B之轴向以機殼1之寬度方向(與葉片輪2 :同方向。參照第以圖之符號w。)之擴張角度 大形成之傾斜部C '、 ^ 、及用以連絡該傾斜部位5與減速部4 方以曲率半徑2R彎曲形成之連絡部位 ,傾斜部位5夕姐EE么— 還有 内發生”― 卜係預先設定成避免在部位5 Μ I生Μ體剝離等現象之角度。 忒減速部4,係如第1Β圖所示形成於該離心送風 1〇°之排放通路lb之排放口 lc附近之機殼】寬产方二機 兩側(第1B圖中之斜線部)速部 之 示,由第1B圖夕Λ A 第1C圖所 心 固之A-A線戴面視’相對排放口 ^之輪向中 曲。 工右對稱,且以既定之曲率半徑R往裎向外方彎 其认’ f曲之減速部4之曲率半徑,係如第2a〜 z tf圖 11 200427930 、X3 — Χ3、Χ4 所示,由第1Β圖之XI — Χ1、Χ2〜χ2、Α Χ4線截面視,分別為R1、R2、r、^ 、R4。這些半徑且右 R1>R2>R、及 R4>R3>R 之關係。亦 gp,# 一 ^ ^ Λ 、, 即截面視之位置從排放 口 lc之中心越在左右方(機殼1之掉士 4 <&方向垂直方向)遠 離,對應該位置之減速部4之曲皋主彡 牛牛從便漸大。此外,該 減速部4之左右端’係與排放通路1^ 、峪1b之排放口 lc附近之 減速部4之外的部位7分別連續。 在此,該減速部4之曲率半徑R最好設定成〇 〇5d〜 0· 2D(D為排放通路lb之排放口 lr夕咖"、 丄c之内杈)。理由是,當 減速部4之曲率半徑R小於排放通路lb之排放口 ic之内 徑D之5%時’減速部4太短,無法使流體高效率地減速。 此外,若減速部4之曲率半徑R大於排放口 lc之内徑 20%’則機殼1變大。另外’最好與該減速部4之曲率半徑 R相對應,將減速部4之軸向之高度H2設定成〇 〇5D〜 0· 2D。 還有,減速部4之彎曲曲線,實際上是依據離心送風 機之風量、待送風之流體之種類等預先由實驗等來設定。 上述減速部4,在當中流動之流體高效率地減速,故 能將流體減速所必要的排放通路1 b之軸向之距離設定的比 以往的還小。反過來說,若於排放口 1C附近不設置滅速部 4,則必須加長上述距離。 更具體來說,可將通過葉片輪2之軸線、且與排放口 1 c大致平行的中心線(以下稱為第2中心線)CL2到排放口 1 c之高度Η,例如設定在排放口 1 c之内徑D之1 · 5倍以下 12 200427930 藉上述之方式,本實施形態之離心送風機100之機殼 1能比習知送風機更小型。 此外,亦可使排放口 lc之内徑D,與機殼1之吸入口 8之内役D1相同。藉此,亦可將連接於這些排放口之配管 之種類加以統一。 另外,在此,雖使機殼1之排放通路1 b之排放口 i c 之轴向中心線3,與葉片輪2之第1中心線cli 一致,不 過,也可視連接於該排放口 lc之配管之配置,使該軸向中 心線3與葉片輪2之第2中心線CL2大致一致。 以下’根據實施例來詳述本發明。 實施例 如第1A〜1C圖所示,離心送風機⑽,係具備旋渦狀 機殼i、及設置於該機殼!之旋渦室u内的葉片輪2。機 殼!之排放通路lb之排放口 lc之轴向中心線3與葉片輪 2之垂直方向中心、線CL1大致一致。該排放〇 k附近 減速部4。 此外,有關該離心送風機1〇〇 , 戍UU之设定,相對機殼1之 排放口 lc之内徑D,葉片輪 】々1 心之4 2中心線CL2到排放口 lc之冋度H = 〇· 95D,減速部4 , , ^ ^ I 4之曲率半徑R=0.07D,減 速部4之南度Η2=0·07Ι) 28。 ^放通路lb之擴張角度5 1 = 比較例1 與實施例不同的是 比較例1,如第5圖所示 13 200427930 機殼10之排放口 之軸線且與排放口 1〇a之車由向中心線12、與通過葉片輪11 1 〇 a之車由向同方向之中心線(以下,垂直 方向中心線)CL1相隔既定 部4,三、相對於機殼J 〇 距離平行,二、未具備上述減速 之排放口 l〇a之内徑D2(大約 〇· 85D)葉片輪u之第2中心線⑴到排放口⑽之高度 H3=0.92D2。其他則與實施例相同。 比較例2 比車乂例2 ’如第7B圖所示,與實施例不同的是未具備According to the above configuration, the fluid flowing in the discharge path of the centrifugal blower is efficiently decelerated in the deceleration section. Thereby, an increase in pressure loss can be prevented, and a decrease in performance of the centrifugal blower can be prevented. In addition, if the radius of curvature of the deceleration portion: the curved portion is less than 5% of the inner diameter of the discharge port of the discharge passage, the deceleration portion is too short to decelerate the fluid efficiently. The radius of curvature of the X-curved portion is larger than the inside of the discharge opening of the discharge path ′, the case becomes larger. [Embodiment] The most deformable form of the invention The following embodiment of the present invention will be described with reference to the figure. ^ Figure 1A [Centrifugal, blower_ is a blade-shaped casing and a blade wheel 2 placed in a vortex chamber u of the casing i. The flow path of the path 113 provided with the discharge path lb 'exits from the vortex chamber 1 & As shown in FIG. 1B, the cross section of the flow path of the vortex chamber la is generally rectangular. The cross section of the flow path gradually turns from the vortex chamber la through the discharge passage to a circular shape, and the discharge port 1C of the discharge passage 1 b becomes circular. . Secondly, the axial centerline 3 of the discharge port lc is related to the axis passing through the blade wheel 10 and the discharge port lc MAM ^ The heart is formed by the centerline in the same direction (hereinafter, the centerline of the private I) CU First, at 1 a, that is, the above-mentioned axial center line [passes through the axis of the blade wheel 2. Thereby, the Huxian M ^ r, Ί] / scorpion, which flows relatively quickly, can be brought close to the central part of the opening 1 c of the centrifugal blower 100.果 ~ 本 ,、 °, even if a matching officer (not shown) connected to the discharge port lc is bent in the same direction as the rotation direction of Ye Yue at μ 4 ± ±, and the attacker is bent in the opposite direction, It is also difficult to find the peeling of the fluid in Continued #, ^ σ bow, σ 卩 points, so to prevent the occurrence of large pressure loss. This can unify the turning direction of the blade wheel 2 from the previous two types into !! Species. As shown in detail, the discharge path ib is the first one. As shown in the figure, "i" is the axial direction of the path 1B of the deceleration part 4 for efficiently decelerating the fluid flowing through the inside thereof, and the width direction of the casing 1 (the same direction as the blade wheel 2: see the symbol in the figure). w.) The inclined portion C ′, ^ formed by a large expansion angle, and the contact portion formed by bending the inclined portion 5 and the decelerating portion 4 with a curvature radius 2R, is the inclined portion 5 Xijie EE — and also inside Occurrence "-The angle is set in advance to avoid the phenomenon of 5 MH body peeling at the site. 忒 The deceleration part 4 is a discharge opening formed in the discharge path lb of the centrifugal supply air 10 ° as shown in Fig. 1B. Chassis near lc] The speed parts of the two sides of the wide production side (the oblique line in Fig. 1B) are shown by the AA line shown in Fig. 1B and the AA line. ^ The direction of the wheel is curved. The right side is symmetrical, and the radius of curvature of the deceleration part 4 of the f-curve 4 is curved outward with a predetermined radius of curvature R, as shown in Figure 2a ~ z tf Figure 11 200427930, X3 — X3 and X4 are viewed from the XI-X1, X2 ~ χ2, and AX4 cross-sections in Figure 1B, and are respectively R1, R2, r, ^, and R4. The relationship between these radii and the right R1 > R2 > R, and R4 > R3 > R. Also gp, # 一 ^ ^ Λ, that is, the position of the cross section is more to the left and right from the center of the discharge port lc (Taxi 4 < & direction vertical direction) away, corresponding to the position of the deceleration section 4 of the deflection section 4 main yak cattle gradually increased. In addition, the left and right ends of the deceleration section 4 are connected to the discharge path 1 ^, 峪 1b The parts 7 other than the deceleration part 4 near the discharge port lc are continuous respectively. Here, the radius of curvature R of the deceleration part 4 is preferably set to 0.05d to 0.2D (D is the discharge port lr of the discharge passage lb. ", the inner branch of 丄 c). The reason is that when the radius of curvature R of the deceleration portion 4 is less than 5% of the inner diameter D of the discharge port ic of the discharge passage lb, the 'deceleration portion 4 is too short to make the fluid efficiently In addition, if the radius of curvature R of the deceleration part 4 is larger than the inner diameter of the discharge port lc by 20% ', the casing 1 becomes larger. In addition, it is preferable to correspond to the radius of curvature R of the deceleration part 4 The height H2 in the axial direction is set to 0.05D to 0.2D. In addition, the bending curve of the deceleration section 4 is actually based on the centrifugal blower. The amount and type of the fluid to be blown are set in advance by experiments, etc. The above-mentioned decelerating section 4 efficiently decelerates the fluid flowing therein, so that the axial distance of the discharge path 1 b necessary for decelerating the fluid can be set. It is smaller than before. On the other hand, if the speed-out portion 4 is not provided near the discharge port 1C, the distance must be increased. More specifically, the axis passing through the blade wheel 2 and the discharge port 1 c can be roughly The height Η of the parallel center line (hereinafter referred to as the second center line) CL2 to the discharge port 1 c, for example, is set to be 1 · 5 times or less the inner diameter D of the discharge port 1 c 12 200427930 According to the above method, this embodiment The casing 1 of the centrifugal blower 100 can be smaller than the conventional blower. In addition, the inner diameter D of the discharge port lc can be made the same as the inner service D1 of the suction port 8 of the casing 1. In this way, the types of pipes connected to these discharge ports can be unified. In addition, although the axial centerline 3 of the discharge port ic of the discharge path 1 b of the casing 1 is made the same as the first centerline cli of the blade wheel 2, the piping connected to the discharge port lc may be seen. The arrangement is such that the axial centerline 3 substantially coincides with the second centerline CL2 of the blade wheel 2. Hereinafter, the present invention will be described in detail based on examples. Example As shown in Figs. 1A to 1C, a centrifugal fan ⑽ is provided with a vortex casing i, and is installed in the casing! The vane wheel 2 inside the vortex chamber u. Chassis! The axial center line 3 of the discharge port lc of the discharge path lb is substantially the same as the vertical center and line CL1 of the blade wheel 2. The emission is near 0 k deceleration section 4. In addition, regarding the setting of the centrifugal blower 100, 戍 UU, relative to the inner diameter D of the discharge port lc of the casing 1, the blade wheel] 々1 heart 4 2 center line CL2 to the discharge port lc H = 0.95D, the radius of curvature R of the decelerating section 4,, ^ ^ I 4 R = 0.07D, and the south degree of the decelerating section 4 Η2 = 0.07I) 28. ^ Expansion angle of the release path lb 5 1 = Comparative Example 1 The difference between the example and Comparative Example 1 is shown in Figure 5. 13 200427930 The axis of the discharge port of the casing 10 and the direction of the vehicle from the discharge port 10a The centerline 12 is separated from the center line CL1 in the same direction (hereinafter, the vertical centerline) CL1 by the vehicle passing through the blade wheel 11 1 〇a. The distance is parallel to the case J. The distance is parallel. The inner diameter D2 (approximately 0.85D) of the above-mentioned decelerated discharge port 10a has a height H3 = 0.92D2 from the second center line ⑴ of the blade wheel u to the discharge port ⑽. Others are the same as the embodiment. Comparative Example 2 Comparing Example 2 ′ As shown in FIG. 7B, it is different from the example in that it is not provided
上述減速部4。因此,如以第1C圖之2點鏈線所示,上述 之排放通路1b之擴張角度5 1從28。擴張成30。。其他則 與實施例相同。 特性之 使用上述實施例、比較例丨及比較例2之離心送風機 ,測疋離心送風機之性能,進行了該評估。將其結果顯示 於第3圖。圖中,符號L1、L2、,為分別對應比較例^ 、比較例2、及實施例的性能曲線。The speed reduction unit 4 described above. Therefore, as shown by the two-point chain line in FIG. 1C, the expansion angle 51 of the above-mentioned discharge passage 1b is from 28 to 28. Expansion to 30. . Others are the same as those of the embodiment. Characteristics Using the centrifugal blowers of the above Examples, Comparative Examples, and Comparative Examples 2, the performance of the centrifugal blowers was measured, and the evaluation was performed. The results are shown in Fig. 3. In the figure, symbols L1 and L2 are performance curves corresponding to Comparative Example ^, Comparative Example 2, and Example, respectively.
如第3圖所示,若將比較例丨(性能曲線L1)與實施例 (性能曲線L3)相比,則得知與比較例丨相比實施例之性能 未明顯降低。由此可說實施例與比較例1有相同之性能。 而且’本貫施例之離心送風機,如上述,不必如比較例1 之_心送風機般,與連接於排放口 1 〇a之配管之配置相對 應準備許多種類。具體來說,如第4A〜4c圖所示,能將本 貫施例之離心送風機之完成品之種類,從以往之6種減至 3種。 14 200427930 另一方面,比較例2,與實施例相同,可減少離心送 · 風機之種類,但如第3圖所示,離心送風機之性能降低。 尤其,在離心送風機之高風量域,相對實施例(性能曲線 L3) ’比較例2(性能曲線L2)之靜壓大幅降低,發生大的壓 力損失。理由是,於上述之排放通路lb未設置減速部4, 故在當中流動之流體未充分減速,以及,排放通路ib之擴 張角度51從28。擴張至30。,故在排放通路化之内面易 於發生流體之剝離等。由此可知,於離心送風機丨〇〇之排 放通路lb設置減速部4,對於降低壓力損失是有效的。 _ 此外,上述之實施形態為一個例子,在未超出本發明 之要旨的範圍,可作各種變更,本發明並未限定於上述之 實施形態。 產業上之利用^可能性 依據本發明之離心送風機,相較於習知離心送風機, 可在不降低性能之下減少種類。結果,本發明之離心送風 機’係生產性佳,庫存管理亦容易,為一種有用的離心送 風機。 g 【圖式簡單說明】 (一)圖式部分 第1A圖,係顯示本發明一實施形態之離心送風機之基 本構成例的縱截面圖。 土 第1β圖,係顯示本發明一實施形態之離心送風機之基 本構成例之俯視圖。 土As shown in Fig. 3, if the comparison example (performance curve L1) is compared with the example (performance curve L3), it is understood that the performance of the example is not significantly lower than that of the comparison example. From this, it can be said that the example has the same performance as the comparative example 1. In addition, as described above, the centrifugal blower of the present embodiment does not need to be prepared in many types corresponding to the arrangement of the piping connected to the discharge port 10a as in the heart blower of Comparative Example 1. Specifically, as shown in Figs. 4A to 4c, the type of the finished product of the centrifugal blower in the present embodiment can be reduced from six to three in the past. 14 200427930 On the other hand, Comparative Example 2 can reduce the number of centrifugal blowers and fans similar to the examples, but as shown in Figure 3, the performance of the centrifugal blowers is reduced. In particular, in the high air volume range of the centrifugal blower, the static pressure was significantly lower than that of the embodiment (performance curve L3) 'and comparative example 2 (performance curve L2), and a large pressure loss occurred. The reason is that the deceleration section 4 is not provided in the above-mentioned discharge passage lb, so the fluid flowing therein is not sufficiently decelerated, and the expansion angle 51 of the discharge passage ib is from 28. Expansion to 30. Therefore, the internal surface of the discharge passage is prone to fluid peeling and the like. From this, it can be seen that the provision of the speed reduction section 4 in the discharge passage lb of the centrifugal blower is effective for reducing the pressure loss. _ In addition, the above-mentioned embodiment is an example, and various changes can be made without departing from the scope of the present invention, and the present invention is not limited to the above-mentioned embodiment. Industrial Applicability ^ Possibility The centrifugal blower according to the present invention can reduce the variety without reducing performance compared to the conventional centrifugal blower. As a result, the centrifugal fan according to the present invention has good productivity and easy inventory management, and is a useful centrifugal fan. g [Schematic description] (I) Schematic part Fig. 1A is a longitudinal sectional view showing a basic configuration example of a centrifugal fan according to an embodiment of the present invention. Figure 1β is a plan view showing a basic configuration example of a centrifugal fan according to an embodiment of the present invention. earth
第1C圖,係第1Β圖所示離心送風機之排放通路之A 15 200427930 一 A線局部截面圖。 第 2A 圖 ,係 第 1B 圖 之 XI -XI 線局部戴 面 圖〇 第 2B 圖 ,係 第 1B 圖 之 X2 -X2 線局部截 面 圖。 第 2C 圖 ,係 第 1B 圖 之 A — -A線 局部截面 圖 〇 第 2D 圖 ,係 第 1B 圖 之 X3 -X3 線局部截 面 圖。 第 2E 圖 ,係 第 1B 圖 之 X4 -X4 線局部截 面 圖0 弟3圖’係顯示離心送風機之風量與靜壓之關係的曲 線圖。Figure 1C is a partial cross-sectional view of line A 15 200427930-A of the discharge path of the centrifugal blower shown in Figure 1B. Figure 2A is a partial cross-sectional view taken along line XI-XI in Figure 1B. Figure 2B is a partial cross-sectional view taken along line X2-X2 in Figure 1B. Fig. 2C is a partial cross-sectional view taken along line A- -A in Fig. 1B. 〇 Fig. 2D is a cross-sectional view taken along line X3-X3 in Fig. 1B. Fig. 2E is a partial cross-section of line X4-X4 in Fig. 1B. Fig. 0 and Fig. 3 'are graphs showing the relationship between the air volume and static pressure of the centrifugal blower.
第4A圖,係本發明一實施形態之離心送風機之完成品 之前視圖,顯示在流體之排放方向為鉛直上方之情形下之 構成例。 第4B圖,係本發明一實施形態之離心送風機之完成品 之前視圖,顯示在流體之排放方向為右方之情形下之構成 例。 第4C圖,本發明一實施形態之離心送風機之完成品之 前視圖,顯示在流體之排放方向為左方之情形下之構成例Fig. 4A is a front view of a finished product of a centrifugal blower according to an embodiment of the present invention, and shows a configuration example in a case where the discharge direction of the fluid is vertically above. Fig. 4B is a front view of a finished product of a centrifugal blower according to an embodiment of the present invention, and shows a configuration example in a case where the discharge direction of the fluid is right. Fig. 4C is a front view of a finished product of a centrifugal blower according to an embodiment of the present invention, showing a configuration example in a case where the discharge direction of the fluid is left
成的縱截面圖。 第6A圖’係習知離心送風機之完成品之縱截面圖 示在流體之排放方向為鉛直上方、且葉片輪之旋轉方 往左繞之情形下之構成例。 -第6B圖係、白知離心送風機之完成品之縱截面圖 示在流體之排放方向為鉛直上方、且葉片輪之旋轉方 16 200427930 在右繞之情形下之構成例。 —第6C圖係、白知離心送風機之完成品之縱截面圖 示在流體之排放方向為左方、且葉片輪之旋轉方向為好 繞之情形下之構成例。 工 第6D圖,係習知離心送風機之完成品之縱戴面 示在流體之排放方向為左方、且葉片輪之旋轉方向為往: 繞之情形下之構成例。 第6E圖’係習知離心送風機之完成品之縱戴面圖,領 示在流體之排放方向為右方、且葉片輪之旋轉方向為往左 繞之情形下之構成例。 工 第6F圖’係習知離心送風機之完成品之縱截面圖,顯 不在流體之排放方向為右方、且葉片輪之旋轉方向為往右 繞之情形下之構成例。 、弟7A圖,係將第5圖所示之習知離心送風機之機殼, 以排放口之軸向中心線靠近通過葉片輪之軸線、且與排放 :之軸向同方向之中心線之方式配置於基台,並於排放口 安凌肘接頭來構成之另—離心送風機之縱截面圖。 第7B圖,係將第5圖所示之習知離心送風機之機殼, 以排放口之車由肖中心、線靠近通過葉片輪之輕線、且與排放 口之軸向同方向之中心線之方式配置於基台,纟削掉機殼 之排放口附近之一部分來構成之另一離心送風機之縱截面 圖。 第8圖,係顯示習知離心送風機之風量與靜壓之關係 的曲線圖。 ” 17 200427930 (二)元件代表符號 1 機殼 la 旋满室 lb 排放通路 1 c 排放口 2 葉片輪 3 軸向中心線 4 減速部 5 傾斜部位 6 連絡部位 7 排放通路lb之排放口 lc附近之減速部4之 外的部位 10 機殼 10a 排放口 10b 新形成之排放口 11 葉片輪 12 排放口 1 Oa之軸向中心線 12a 排放口 1 Ob之軸向中心線 13 流體之排放方向 14 基台 15 馬達 16 肘接頭 16a 新形成之排放口 17 機殼1 0之排放口 10a附近之一部分 18 200427930 18 擴 散 器 部 100 離 心 送風 機 200 習 知 離 心 送風 機 201 習 知 離 心 送風 機 CL1 第 1 中 心 線 CL2 第 2 中 心 線Into a longitudinal section. Fig. 6A 'is a longitudinal sectional view of a finished product of a conventional centrifugal blower, showing a configuration example in a case where the discharge direction of the fluid is vertically above, and the rotation direction of the blade wheel is wound to the left. -Figure 6B is a vertical cross-sectional view of the finished product of the Baizhi centrifugal blower. It shows a configuration example of a case where the discharge direction of the fluid is vertically above and the rotation direction of the vane wheel is 2004 right. —Figure 6C is a longitudinal sectional view of the finished product of the Baizhi centrifugal blower, showing a configuration example in a case where the discharge direction of the fluid is left and the rotation direction of the blade wheel is good. Fig. 6D shows the longitudinal wearing surface of the finished product of the conventional centrifugal blower, showing the configuration example in the case where the discharge direction of the fluid is to the left and the rotation direction of the blade wheel is toward. Fig. 6E 'is a longitudinal sectional view of a finished product of a conventional centrifugal blower, and shows a configuration example in a case where the discharge direction of the fluid is right and the rotation direction of the blade wheel is leftward. Fig. 6F is a longitudinal sectional view of a finished product of a conventional centrifugal blower, showing a configuration example in a case where the discharge direction of the fluid is right, and the rotation direction of the blade wheel is rightward. Figure 7A is the method of moving the casing of the conventional centrifugal blower shown in Figure 5 to the axial centerline of the discharge port near the axis line passing through the axis of the blade wheel and in the same direction as the axis of the discharge: Arranged on the abutment and installed at the exhaust port to elbow joints to form another—a longitudinal section view of a centrifugal blower. Fig. 7B is the center line of the conventional centrifugal blower shown in Fig. 5 with the discharge port from the center of Shaw, close to the light line passing through the vane wheel and in the same direction as the axis of the discharge port. The method is arranged on the abutment, and a longitudinal section view of another centrifugal blower formed by cutting out a part near the discharge opening of the casing. Fig. 8 is a graph showing the relationship between the air volume and the static pressure of a conventional centrifugal blower. 17 200427930 (II) Symbols for components 1 Enclosure la Rotating chamber lb Drainage path 1 c Drainage port 2 Vane wheel 3 Axial centerline 4 Deceleration part 5 Inclined part 6 Contact position 7 Near the discharge port lc of the discharge path lb Parts other than the deceleration part 4 10 Case 10a Discharge port 10b Newly formed discharge port 11 Blade wheel 12 Discharge port 1 Axial centerline of Oa 12a Discharge port 1 Axial centerline of Ob 13 Discharge direction of fluid 14 Abutment 15 Motor 16 Elbow joint 16a Newly formed exhaust port 17 Part of the casing 10 near the exhaust port 10a 18 200427930 18 Diffuser section 100 Centrifugal blower 200 Known centrifugal blower 201 Known centrifugal blower CL1 1st centerline CL2 2nd Center line
1919
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JP2003160153A JP4590167B2 (en) | 2003-06-05 | 2003-06-05 | Centrifugal blower |
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CN104420431B (en) * | 2013-08-28 | 2016-08-10 | 苏州宝时得电动工具有限公司 | Blowing device |
CN211082385U (en) * | 2019-10-17 | 2020-07-24 | 中山大洋电机股份有限公司 | Volute component and induced draft fan applying same |
MX2021015112A (en) | 2019-10-17 | 2022-01-24 | Zhongshan Broad Ocean Motor Co | Volute assembly and induced draught fan using same. |
EP4191072A4 (en) * | 2020-07-29 | 2023-09-20 | Mitsubishi Electric Corporation | Scroll casing of centrifugal blower, centrifugal blower provided with scroll casing, air conditioner, and refrigeration circuit device |
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GB733533A (en) * | 1952-08-26 | 1955-07-13 | Establissements Neu Sa Des | Improvements in or relating to centrifugal blowers, compressors, pumps and the like |
US3860360A (en) * | 1973-09-04 | 1975-01-14 | Gen Motors Corp | Diffuser for a centrifugal compressor |
JPS5529381Y2 (en) * | 1976-01-19 | 1980-07-12 | ||
JPS5313610U (en) * | 1976-07-19 | 1978-02-04 | ||
JPS59131799A (en) * | 1983-12-19 | 1984-07-28 | Hitachi Ltd | Casing for centrifugal hydraulic machine |
JPH03217699A (en) * | 1990-01-23 | 1991-09-25 | Nissan Motor Co Ltd | Scroll structure of compressor |
DE50011843D1 (en) * | 1999-06-14 | 2006-01-19 | Waertsilae Schweiz Ag Winterth | Charging group for a large diesel engine |
JP2001193682A (en) * | 2000-01-06 | 2001-07-17 | Ebara Corp | Voltex pump |
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TWI253491B (en) | 2006-04-21 |
CN1788168A (en) | 2006-06-14 |
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