CN1056672C - Centrifugal blower - Google Patents
Centrifugal blower Download PDFInfo
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- CN1056672C CN1056672C CN95115116A CN95115116A CN1056672C CN 1056672 C CN1056672 C CN 1056672C CN 95115116 A CN95115116 A CN 95115116A CN 95115116 A CN95115116 A CN 95115116A CN 1056672 C CN1056672 C CN 1056672C
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- 230000004323 axial length Effects 0.000 claims description 9
- 238000009423 ventilation Methods 0.000 claims description 6
- 230000001629 suppression Effects 0.000 abstract description 2
- 230000003068 static effect Effects 0.000 description 19
- 238000010586 diagram Methods 0.000 description 18
- 230000000694 effects Effects 0.000 description 5
- 238000009792 diffusion process Methods 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 238000007664 blowing Methods 0.000 description 1
- 239000012141 concentrate Substances 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 238000013139 quantization Methods 0.000 description 1
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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
- F04D17/00—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
- F04D17/08—Centrifugal pumps
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Abstract
一种离心式送风机,其外壳沿离心式叶轮轴向的纵剖面为大致长圆形,其轴向宽度从鼻状起向离心式叶轮的旋转方向渐渐扩大,最大宽度部分处于至排出口之间,故可扩大壳体的轴向扩散率,以弥补对于径向扩散率的抑制,确保实质性的扩散率。本发明没有传统壳体拐角部的二维流、即涡流等。不需增大体积即可实现大风量、低噪音,即使使用细管道,也不会降低风量、增大噪音。
A centrifugal blower, the longitudinal section of the casing along the axial direction of the centrifugal impeller is roughly oblong, its axial width gradually expands from the nose shape to the direction of rotation of the centrifugal impeller, and the maximum width part is between the discharge port , so the axial diffusivity of the shell can be expanded to compensate for the suppression of the radial diffusivity and ensure a substantial diffusivity. The present invention does not have the two-dimensional flow, ie, eddy current, etc. of the corners of the conventional casing. Large air volume and low noise can be achieved without increasing the volume. Even if thin ducts are used, the air volume will not be reduced and the noise will not be increased.
Description
本发明涉及对壳体进行改良的离心式送风机。The invention relates to a centrifugal blower with an improved casing.
传统的这类离心式送风机如图37所示,具有离心式叶轮1、围住该叶轮1的壳体2,通过用马达3对该离心式叶轮1进行旋转驱动,离心式叶轮1从轴方向吸入空气后向圆周方向排出,壳体2将该被排出的空气集中后引向排出口4,并按顺序通过管道接口部5及管道6后送出。As shown in FIG. 37, a conventional centrifugal fan of this type has a
上述的离心式送风机,在用于例如安装于天花板背面的管道用换气扇时,由于天花板背面的空间有限,故要求其体积不大,送风量大,且噪音低。然而,要在体积不大的条件下实现这样的大风量和低噪音是非常困难的。When the above-mentioned centrifugal blower is used, for example, as a ventilating fan for ducts installed on the back of the ceiling, due to the limited space on the back of the ceiling, it is required to have a small volume, a large air supply volume, and low noise. However, it is very difficult to achieve such a large air volume and low noise in a small volume.
又,当在房屋的狭小的天花板背面空间施工时,或是为了降低成本,要使用更细的管道。然而,如果使用细管道,由此造成的压力损失会增大,从而降低风量,增大噪音。Also, when constructing in a narrow space behind the ceiling of a house, or to reduce costs, it is necessary to use thinner pipes. However, if thin pipes are used, the resulting pressure loss will increase, thereby reducing the air volume and increasing the noise.
鉴于上述实情,本发明的目的在于提供一种离心式送风机,它可在整体体积不大的条件下实现大风量化和低噪音化,且即使使用细管道也不会导致风量降低、噪音增大。In view of the above facts, the object of the present invention is to provide a centrifugal blower that can achieve high wind volume and low noise with a small overall volume, and even if thin ducts are used, the air volume will not decrease and the noise will increase.
为了实现上述目的,本发明的离心式送风机的特征在于,按下述构造形成壳体,即沿离心式送风机轴方向的纵向剖面为大致长圆形状,其轴方向的宽度从鼻状部向离心式送风机的旋转方向渐渐扩大,且其最宽部分处于至排出口之间。In order to achieve the above object, the centrifugal blower of the present invention is characterized in that the casing is formed in such a structure that the longitudinal section along the axial direction of the centrifugal blower is approximately oblong, and the width in the axial direction extends from the nose portion to the centrifugal blower. The direction of rotation of the blower gradually expands, and its widest part is between the discharge port.
在这种场合,如设离心式叶轮的轴方向长度为b,外径为d2,壳体的轴方向最大宽度为Bmax,则可定为:In this case, if the axial length of the centrifugal impeller is b, the outer diameter is d2, and the maximum axial width of the casing is Bmax, it can be determined as:
b/d2=0.45~0.70b/d2=0.45~0.70
b/Bmax=0.55~0.75b/Bmax=0.55~0.75
又,壳体的轴方向的最大宽度部分形成的位置最好从鼻状部向离心式送风机的旋转方向呈200~310°角度。In addition, it is preferable that the position where the maximum width portion in the axial direction of the casing is formed forms an angle of 200 to 310° from the nose portion to the rotation direction of the centrifugal blower.
而且,壳体的轴方向的最小宽度部分形成的长度最好处于从鼻状部向离心式送风机的旋转方向至鼻状部附近的范围内,尤其是处于从鼻状部起呈45°角以下的范围。Furthermore, the length formed by the smallest width portion in the axial direction of the casing is preferably within a range from the nose portion to the rotation direction of the centrifugal blower to the vicinity of the nose portion, especially at an angle of 45° or less from the nose portion. range.
离心式送风机的性能受壳体尺寸影响很大。这种影响比叶轮外径和轴向长度的影响还大。The performance of centrifugal blowers is greatly influenced by the size of the housing. This effect is greater than that of the impeller outer diameter and axial length.
离心式送风机一般是在径向形成具有一定扩散率的涡旋状,其扩散率越大,越能获得大风量和高静压。然而,一旦把使用离心式送风机的例如管道用换气扇装于天花板背面,则由于空间有限,而不得不使壳体的径向扩散率受到某种程度的抑制。Centrifugal blowers generally form a vortex with a certain diffusion rate in the radial direction. The larger the diffusion rate, the greater the air volume and high static pressure can be obtained. However, if a ventilating fan for a duct using a centrifugal blower, for example, is mounted on the back of the ceiling, the radial diffusivity of the casing has to be suppressed to some extent due to limited space.
针对这一点,如上所述,如采用下述构造形成壳体,即沿离心式叶轮轴方向的纵向剖面为大致长圆形状,其轴方向的宽度从鼻状部向离心式送风机的旋转方向渐渐扩大,且其最宽部分处于至排出口之间,则通过增大壳体的轴向扩散率,可弥补对径向扩散率的抑制,确保壳体的实质性扩散率。Regarding this point, as mentioned above, if the casing is formed by adopting the following structure, that is, the longitudinal section along the axial direction of the centrifugal impeller has an approximately oblong shape, and the width in the axial direction gradually expands from the nose portion to the rotational direction of the centrifugal blower. , and its widest part is between the discharge port, by increasing the axial diffusivity of the shell, the suppression of the radial diffusivity can be compensated to ensure the substantial diffusivity of the shell.
又,沿离心式叶轮轴向的纵向剖面为大致长圆形的壳体可消除在传统的剖面为矩形的壳体拐角部发生的二维流即所渭涡流等现象,从而可实质上扩大风路,由此可实现离心式送风机的大风量化、低噪音化,还可实现高静压化。In addition, the substantially oblong casing along the longitudinal section of the axial direction of the centrifugal impeller can eliminate the two-dimensional flow, that is, the so-called vortex, which occurs at the corner of the conventional rectangular casing, thereby substantially expanding the wind flow. As a result, the centrifugal blower can achieve large air volume, low noise, and high static pressure.
又,在这种场合,设离心式叶轮的轴方向长度为b,外径为d2,壳体的轴方向最大宽度为Bmax,若定为:Also, in this case, assume that the axial length of the centrifugal impeller is b, the outer diameter is d2, and the maximum axial width of the casing is Bmax, if it is set as:
b/d2=0.45~0.70b/d2=0.45~0.70
b/Bmax=0.55~0.75时,则根据实际测试结果,可比其他数值获得更理想的数据。When b/Bmax=0.55~0.75, according to the actual test results, more ideal data can be obtained than other values.
此外,若壳体的轴方向的最大宽度部分形成的位置从鼻状部向离心式送风机的旋转方向呈200~310°角度,则根据实际测试结果,也可比其他数值获得更理想的数据。In addition, if the maximum width in the axial direction of the casing is formed at an angle of 200° to 310° from the nose portion to the rotation direction of the centrifugal blower, more ideal data than other values can be obtained according to actual test results.
而且,若壳体的轴方向的最小宽度部分形成的长度处于从鼻状部向离心式送风机的旋转方向至鼻状部附近的范围内,则可减少通过鼻状部间隙而返回的风,可取得更好的结果。其中,若是该壳体的最小部分形成的长度处于从鼻状部起呈45°角以下的范围,则根据实际测试结果,可比其他数值获得更理想的数据。Moreover, if the length formed by the minimum width portion in the axial direction of the housing is within the range from the nose to the rotation direction of the centrifugal blower to the vicinity of the nose, the wind returning through the gap of the nose can be reduced, and achieve better results. Wherein, if the length formed by the smallest part of the housing is within the range of an angle of less than 45° from the nose, more ideal data can be obtained than other values according to actual test results.
以下是对附图的简单说明。The following is a brief description of the accompanying drawings.
图1是沿图2(表示本发明第1实施例)中I-I线的剖面展开图。Fig. 1 is a sectional development view along line I-I in Fig. 2 (showing the first embodiment of the present invention).
图2是整体的纵剖视图。Fig. 2 is an overall longitudinal sectional view.
图3是横剖视图。Fig. 3 is a cross-sectional view.
图4是主视图。Fig. 4 is a front view.
图5是传统离心式送风机壳体部的局部纵剖视图。Fig. 5 is a partial longitudinal sectional view of a casing portion of a conventional centrifugal blower.
图6本发明的离心式送风机壳体部的局部纵剖视图。Fig. 6 is a partial longitudinal sectional view of the casing of the centrifugal blower according to the present invention.
图7是离心式叶轮的局部放大剖视图。Fig. 7 is a partially enlarged sectional view of a centrifugal impeller.
图8是离心式叶轮的叶片部分的放大剖视图。Fig. 8 is an enlarged sectional view of a blade portion of a centrifugal impeller.
图9是特性图之1。Fig. 9 is characteristic diagram 1.
图10是特性图之2。Figure 10 is the second characteristic diagram.
图11是特性图之3。Figure 11 is the third characteristic diagram.
图12是特性图之4。Figure 12 is the fourth characteristic diagram.
图13是特性图之5。Figure 13 is the fifth characteristic diagram.
图14是特性图之6。Fig. 14 is characteristic diagram No. 6.
图15是特性图之7。Fig. 15 is characteristic diagram No. 7.
图16是特性图之8。Figure 16 is the eighth characteristic diagram.
图17是特性图之9。Fig. 17 is characteristic diagram No. 9.
图18是表示本发明第2实施例的图1的相当图。Fig. 18 is a view corresponding to Fig. 1 showing a second embodiment of the present invention.
图19是特性图之10。Figure 19 is the tenth characteristic diagram.
图20是特性图之11。Figure 20 is characteristic diagram 11.
图21是特性图之12。Figure 21 is characteristic diagram 12.
图22是表示本发明第3实施例的侧视图。Fig. 22 is a side view showing a third embodiment of the present invention.
图23是表示本发明第4实施例的横剖视图。Fig. 23 is a cross-sectional view showing a fourth embodiment of the present invention.
图24是沿图23II-II线的剖视图。Fig. 24 is a sectional view along line II-II of Fig. 23 .
图25是沿图23III-III线的剖视图。Fig. 25 is a sectional view along line III-III of Fig. 23 .
图26是沿图23IV-IV线的剖视图。Fig. 26 is a sectional view taken along line IV-IV of Fig. 23 .
图27是沿图23V-V线的剖视图。Fig. 27 is a sectional view taken along line V-V of Fig. 23 .
图28是表示本发明第5实施例的连接口体部分的放大纵剖视图。Fig. 28 is an enlarged vertical cross-sectional view showing a connection port body portion of a fifth embodiment of the present invention.
图29是挡风板单体的放大立体图。Fig. 29 is an enlarged perspective view of a windshield alone.
图30是连接口体部分的放大纵剖视图。Fig. 30 is an enlarged longitudinal sectional view of the connecting port body.
图31是表示本发明第6实施例的图30的相当图。Fig. 31 is a diagram corresponding to Fig. 30 showing a sixth embodiment of the present invention.
图32是表示本发明第7实施例的整体的半纵剖视图。Fig. 32 is a half vertical sectional view showing the whole of a seventh embodiment of the present invention.
图33是图1的相当图。FIG. 33 is a diagram corresponding to FIG. 1 .
图34是表示本发明第8实施例的图2的相当图。Fig. 34 is a view corresponding to Fig. 2 showing an eighth embodiment of the present invention.
图35是表示本发明第9实施例的图2的相当图。Fig. 35 is a view corresponding to Fig. 2 showing a ninth embodiment of the present invention.
图36是表示本发明第10实施例的图2的相当图。Fig. 36 is a view corresponding to Fig. 2 showing a tenth embodiment of the present invention.
图37是表示传统示例的图2的相当图。Fig. 37 is a diagram equivalent to Fig. 2 showing a conventional example.
以下结合附图说明本发明的实施例。Embodiments of the present invention are described below in conjunction with the accompanying drawings.
首先结合图1至图17说明用于管道用换气扇的本发明第1实施例。First, a first embodiment of the present invention for a ventilation fan for ducts will be described with reference to Figs. 1 to 17 .
图2中示出了外框11,其下面呈开放式箱形,其上壁部11a的大致中央部装有马达12,在位于外框11内的马达12的旋转轴12a上装有离心式叶轮13。Shown in Fig. 2 is the
上述离心式叶轮13是把弯曲的多片叶片14(见图8)在圆形底板15的周围部排列成圆筒状,各前端部用端环16围绕而成,而其整体再用壳体17围住。The above-mentioned
上述壳体17由所述外框11的上壁部11a为主的上部和设于外框11内的上下中间部的盖子18构成,其沿离心式叶轮13轴的纵向剖面形状为大致长圆形,且如图3所示,具有与离心式叶轮13接近的鼻状部19,并具有从该鼻状部19到离心式叶轮13间的距离渐渐扩大的涡旋状通风路20。还有如图1中Bmin及Bmax所示,该壳体17的轴向(图2中上下方向)的宽度B从上述鼻状部19向着离心式叶轮13的旋转方向(用箭头R表示)渐渐扩大,其最大宽度Bmax部分处于到排出口21(见图3)之间,再从该处向着排出口21渐渐缩小。The
这里若对所述壳体17的轴方向最大宽度Bmax,设所述离心式叶轮13的轴方向长度为b,外径为d2(见图2),则可定为:Here if the maximum axial width Bmax of the
b/d2=0.45~0.70b/d2=0.45~0.70
b/Bmax=0.55~0.75b/Bmax=0.55~0.75
又,壳体17的轴向最大宽度Bmax部分形成的位置从所述鼻状部19向着离心式叶轮13的旋转方向呈200~310°角度。In addition, the position where the axially maximum width Bmax of the
另外,所述盖子18在面对离心式叶轮13的大致中央部具有喇叭口22。又,外框11安装于房屋的天花板23上,设于天花板背面,其下面的开放部用装饰框24复盖。而天花板23上装有图4所示的安装板25,使与该安装板25形成一体的连接口体26与所述排出口21连通,且在连接口体26的剖面为圆形的前端部连接着比传统所用管道27的额定直径细的剖面为圆形的管道28。In addition, the
以下说明上述构造的离心式送风机的作用。The operation of the centrifugal blower constructed as described above will be described below.
在采用上述构造时,一旦用马达12使离心式叶轮13旋转,离心式叶轮13即将外框11所面对的下方室内的空气从轴方向通过装饰框24及盖子18的喇叭口22吸入,并向圆周方向排出,壳体1′将该排出的空气集中后引向排出口21,并从连接口体26经过管道28而排出室外。When the above-mentioned structure is adopted, once the
然而,离心式送风机的性能受壳体17的尺寸影响很大。这种影响比离心式叶轮13的外径d2或轴向的长度b的影响还要大。However, the performance of the centrifugal blower is greatly affected by the size of the
离心式送风机的壳体17一般形成为径向有某种扩散率的涡旋状,其扩散率越大,越能获得大风量、高静压。即,如图3所示,如果对离心式叶轮13的外径d2,设与排出口21的面平行且通过离心式叶轮13中心的壳体17的内径为D0,则D0/d2越大,越能获得高性能。然而,现在的实际情况是,如果将使用离心式送风机的例如管道用换气扇装于天花板背面,则会因为空间有限而不得不在某种程度缩小壳体17径向的扩散率,D0/d2一般只能在1.4~1.6左右,即必须控制在2.0以下。The
针对这一点,如上所述,如采用下述构造形成壳体17,即沿离心式叶轮13轴的纵向剖面为大致长圆形状,其轴方向的宽度B从鼻状部19向离心式叶轮13的旋转方向渐渐扩大,且其最大宽度Bmax部分处于至排出口21之间,则通过增大壳体17的轴向扩散率,可弥补上述那种不得不对径向扩散率进行的抑制,确保壳体的实质性扩散率。Regarding this point, as described above, if the
又,沿离心式叶轮13轴的纵向剖面为大致长圆形的壳体17如图6所示,可消除在传统的剖面为矩形的壳体2拐角部发生的图5箭头所示的二维流即所渭涡流s,从而可实质上扩大风路,由此可实现离心式送风机的大风量化、低噪音化,还可实现高静压化。Again, the longitudinal section along the axis of the
因而,不必增大体积即可实现大风量化和低噪音化,还可实现高静压化,由此即使使用细管道,也不会导致风量降低和噪音增大。Therefore, large air volume and low noise can be realized without increasing the volume, and high static pressure can also be realized, so even if thin ducts are used, the air volume will not decrease and the noise will not increase.
此外,在采用上述构造时,如下所示,还进一步找出了离心式叶轮13的最佳尺寸和壳体17的最佳尺寸。In addition, when adopting the above configuration, as shown below, the optimal size of the
(1)b/d2(离心式叶轮13的轴向长度/外径)(1) b/d2 (axial length/outer diameter of the centrifugal impeller 13)
离心式叶轮13的吸入面积和排出有效面积最好相等。所谓离心式叶轮13的有效面积,是指从离心式叶轮13的排出风(空气)的圆周侧部的面积中除去叶片14和底板15、端环16各自的壁厚度,并且再除去在离心式叶轮13的吸入端发生的死水区(由于气流的方向不会急剧变化,而在离心式叶轮13的吸入端发生的吹不到风的部分…见图7)、以及在从鼻状部19向着旋转方向约2成之处的离心式叶轮13的几乎吹不到风的圆周侧部(由于从壳体17的排出部通过鼻状部19的间隙后返回的风的缘故而不从离心式叶轮13圆周侧部吹出风的部分…见图3)的面积。由此来求离心式叶轮13的吸入面积与有效排出面积相等的轴向长度b和外径d2之比,则:The suction area and discharge effective area of the
离心式叶轮13的吸入面积S1=π×(d1/2)2 Suction area S1 of the
离心式叶轮13的圆周侧部的面积S2=π×d2×bArea S2 of the circumferential side of the
离心式叶轮13的有效圆周侧部面积S2’=S2×A×C×EThe effective circumferential side area S2'=S2×A×C×E of the
d1:离心式叶轮13的内径(见图7)d1: inner diameter of the centrifugal impeller 13 (see Figure 7)
A:离心式叶轮13的圆周侧部面积减少率=0.40~0.65A: The reduction rate of the circumferential side area of the
所谓离心式叶轮13的圆周侧部面积减少率A,实际上是风吹出的有效面积Se和圆周侧部面积S2之比,有效面积Se是叶片14间距离p(见图8)与有效长度b’(见图7)及叶片14的片数Z的积。The circumference side area reduction rate A of the so-called
从而,thereby,
A=Se/S2=(p×b’×Z)/(π×d2×b)通常,塑料制的离心式叶轮13为A=0.40~0.55,而金属制的离心式叶轮13则为A=0.50~0.65。A=Se/S2=(p×b′×Z)/(π×d2×b) Usually, the
C:离心式叶轮13因死水区而造成的有效圆周侧部面积减少率=约0.8C: The reduction rate of the effective peripheral side area of the
E:离心式叶轮13因鼻状部19的几乎吹不到风的部分造成的面积减少率=约0.8E: The area reduction rate of the
由此可得出:From this it can be concluded that:
S1=S2’=S2×A×C×ES1=S2'=S2×A×C×E
π=(d1/2)2=(π×d2×b)×(0.40~0.65)×0.8×0.8π=(d1/2) 2 =(π×d2×b)×(0.40~0.65)×0.8×0.8
且离心式叶轮13的内外径比(d1/d2)通常设计为0.82,故d1=0.82×d2,把它代入上述式子,则,And the inner and outer diameter ratio (d1/d2) of the
π×(0.82×d2/2)2=(π×d2×b)×(0.40~0.65)×0.8×0.8π×(0.82×d2/2) 2 =(π×d2×b)×(0.40~0.65)×0.8×0.8
(0.82/2)2×d2=b×(0.40~0.65)×0.8×0.8(0.82/2) 2 ×d2=b×(0.40~0.65)×0.8×0.8
b/d2=0.40~0.56b/d2=0.40~0.56
图9至图11是根据实际测得的结果制作的特性图。它们分别根据离心式叶轮13的外径d2为10〔cm〕、18〔cm〕、23〔cm〕时测得的结果制成的。从图9至图11可知,存在一个风量及静压最大、噪音最小的范围b/d2,即0.45~0.70。此范围略微偏离从上述理论求出的数值,这是因为在叶片14背面发生的气流剥离使实际的吹风有效圆周侧部面积更加缩小(可以认为圆周侧部面积减少率A实际上比前述的数值小)的缘故。Figures 9 to 11 are characteristic diagrams made based on actual measured results. They are respectively made according to the results measured when the outer diameter d2 of the
从而,本发明根据实际测试结果而将b/d2定为可取得高性能的0.45~0.70。Therefore, the present invention sets b/d2 as 0.45-0.70, which can achieve high performance, according to the actual test results.
(2)b/Bmax(离心式叶轮13的轴方向长度/壳体17的最大宽度)(2) b/Bmax (axial length of the
图12至图14是使用上述各性能中接近最小噪音值b/d2的尺寸的离心式叶轮13,并分别变化壳体17的最大宽度Bmax后进行测试,根据所测结果制成的特性图。从图12至图14可知,存在一个风量及静压为最大值,噪音为最小值的范围b/Bmax,即0.55~0.75。在这种场合,人们往往容易认为壳体17的最大宽度Bmax越大,性能越佳,其实不然,由于壳体17的排出部尺寸有限,其最大宽度Bmax越大,排出部的缩小率就越大,并且气流缩小引起的损失越大,结果反而使性能劣化。因而,必定存在一个能取得平衡的最佳的壳体最大宽度Bmax。Figures 12 to 14 are characteristic diagrams made according to the test results after using the
从而,本发明根据实际测得的结果,将b/Bmax也定为可获得高性能的0.55~0.75。Therefore, the present invention also sets b/Bmax to 0.55 to 0.75, which can obtain high performance, based on the actual measured results.
图15至图17是使用接近上述最小噪音值b/d2的尺寸的离心式叶轮13,并分别变化壳体17的最大宽度Bmax部分的位置后进行测试,根据所测结果制成的特性图。从图15至图17可知,存在一个风量及静压为最大值,噪音为最小值的壳体17的最大宽度Bmax部分的位置,即从鼻状部19向着离心式叶轮13的旋转方向呈200~310°角的位置。Figures 15 to 17 are characteristic diagrams made according to the test results after using the
从而,本发明根据实际测得的结果,将壳体17的轴方向最大宽度Bmax部分的位置也定在可获得高性能的上述200~310°角的位置上。Therefore, according to the actual measured results, the present invention sets the position of the portion of the maximum width Bmax in the axial direction of the
这样一来,与尺寸相同的本公司传统机种相比,风量可增加4~8〔%〕,静压增加5~10〔%〕,噪音减少0.8~1.3〔dB〕,有效地提高了性能。In this way, compared with our traditional models of the same size, the air volume can be increased by 4-8〔%〕, the static pressure can be increased by 5-10〔%〕, and the noise can be reduced by 0.8-1.3〔dB〕, effectively improving the performance .
图18至图21表示本发明的第2实施例,表示壳体17的轴方向最小宽度Bmin部分形成的长度是在从鼻状部19向着离心式叶轮13的旋转方向至鼻状部19附近的范围内,尤其处在从鼻状部19起45°角以下的长度范围。18 to 21 show the second embodiment of the present invention, showing that the length of the minimum width Bmin in the axial direction of the
一旦壳体17的轴方向最小宽度Bmin部分形成的长度是在从鼻状部19向离心式叶轮13的旋转方向至鼻状部19附近的范围内,则可减少通过鼻状部19的间隙而返回的风,可在大风量化、低噪音化、高静压化方面获得更好的结果。Once the minimum width Bmin in the axial direction of the
特别是,在这种场合,如果壳体17的轴方向最小宽度Bmin部分形成的长度从鼻状部19起超出45°角的范围,则从离心式叶轮13吹出的风的通路会变窄,且如图19至图21的实际测试结果所示,性能会降低,而将其长度定在45°角以下的范围,则能可靠地获得高性能,尤其可在保持大风量、低噪音的情况下增大静压。Particularly, in this case, if the length formed by the minimum width Bmin in the axial direction of the
图22为本发明的第3实施例,鼻状部19形成弯曲状,离心式叶轮13的吸入端(端环16一侧)部分19a及吸入的对置端(底板15一侧)部分19b从排出口21看延长至离心式叶轮13的圆周侧部或圆周侧部附近,这样一来,在鼻状部19附近,分别通过喇叭口22与离心式叶轮13间的间隙、及与其对置的外框上壁部11a与离心式叶轮13间的间隙而在壳体17内循环的风量便可减少,因此可在大风量化、低噪音化、高静压化方面取得更好的结果。Fig. 22 is the 3rd embodiment of the present invention, nose-shaped
图23至图27是本发明的第4实施例,上述的弯曲状鼻状部19的延长部19a19b的各自通风路20的侧剖面形状为弧状,而且,处于其鼻状部19之延长部19a、19b部分的壳体17的形状为向着排出口21,其剖面渐渐由长圆形变成近似圆形。这样一来,风流可以顺利地从壳体17流入前端部剖面为圆形的连接口体26,继而流入剖面为圆形的管道28,从而可进一步增大风量和静压,减少噪音。Fig. 23 to Fig. 27 are the 4th embodiment of the present invention, the side cross-sectional shape of each
图28至图30是本发明的第5实施例,设于连接口体26内的防逆流用挡风板29成弯曲形状,当该挡风板29由于从排出口21吹出的风的压力而开放时,处在沿着连接口体26的圆弧状内上面。又,在这种场合,挡风板29的枢支部30设于与连接口体26前端部的上缘位置基本相同的位置,因此,从壳体17进入连接口体26内,继而进入管道28内的风流可不受挡风板29及其枢支部30的影响顺利地流入,故可进一步增大风量和静压,减少噪音。还可防止这种场合因挡风板29的枢支部30而容易发生的涡流声。28 to 30 are the fifth embodiment of the present invention. The
图31是本发明的第6实施例,挡风板29的枢支部31设在比连接口体26的前端部上缘更高的位置,从而从壳体17进入连接口体26内及管道28内的风流可更不受挡风板29及其枢支部31的影响而顺利流入,并可更有效地防止因挡风板29的枢支部31而容易发生的涡流声。Fig. 31 is the sixth embodiment of the present invention, the
图32及图33是本发明第7实施例,系按照离心式叶轮13与连接口体26间的中心位置的偏差下来将壳体17的鼻状部19的位置与排出部的位置错开,且壳体17的鼻状部19一侧的扩大形状与排出部一侧的缩小形状不同,以分别作出对应。Fig. 32 and Fig. 33 are the 7th embodiment of the present invention, and the position of the nose-shaped
在这种场合,由于采用这种离心式送风机的管道用换气扇装于狭窄的天花板背面,故对产品高度有限制,因而,如图33所示,马达12的最高位置(尺寸H)受到限制。其中,在用金属制成外框11的上壁部11a时,由于加工(例如深冲)方面的问题,壳体17的深度G不能太大,随之而来的是离心式叶轮13的位置也必然受限制。In this case, since the duct adopting this centrifugal fan is mounted on the back of the narrow ceiling, the height of the product is limited. Therefore, as shown in FIG. 33, the highest position (dimension H) of the
另外,外框11具体是被固定在天花板23上所装的木框32上的。又,为了把连接口体26与管道28加以连接,需要进行攻螺纹作业,而为了提高作业性,要求木框32与连接口体26之间有充分的空间。为此,连接口26的安装位置必须升高。In addition, the
从性能方面看,离心式叶轮13与连接口体26各自上下方向的中心位置最好相等,然而,由于受上述的市场要求及加工性方面的限制,只能将离心式叶轮13与连接口体26的中心位置错开。为此,要在壳体17的最大宽度Bmax部分至排出部之间将这一错位加以弥补,按上述方法制成不同的壳体17的形状,由此可以使从壳体17进入连接口体26和管道28内的风流仍然顺利流动。From the performance point of view, the vertical center positions of the
图34至图36是本发明的第8至第10实施例,其中图34的外框33由外框主体34与另外的上壁35连接而成,盖子36则被嵌至该连接部。又,图35的外框37由比上述外框主体34的高度低的外框主体38与比上述上壁35的深度深的上壁39连接而成,盖子40则被嵌至该连接部。图36中的盖子41因部件的厚度,形成了喇叭口42从外框11的下面开放部起渐渐变窄的状态,从而提高了空气的吸入性。34 to 36 are eighth to tenth embodiments of the present invention, wherein the
此外,本发明并不限于上述及附图所示的实施例,还可在不脱离本发明要点的范围内作适当变更后实施之。In addition, the present invention is not limited to the embodiments described above and shown in the drawings, and can be implemented with appropriate changes within the scope not departing from the gist of the present invention.
以上说明的本发明的离心式风机具有下述效果。The centrifugal fan of the present invention described above has the following effects.
第1,这种离心式送风机具有通过旋转而将空气从轴方向吸入后向圆周方向排出的离心式叶轮、及具有与该离心式叶轮接近的鼻状部且将离心式叶轮排出的空气集中于涡旋状的通风路并引向排出口部的壳体,且该壳体沿离心式叶轮的轴方向的纵向剖面为大致长圆形状,其轴方向的宽度从上述鼻状部起向着离心式叶轮的旋转方向渐渐扩大,其最大部分处于至上述排出口之间,从而不必增大整体的体积即可实现大风量、低噪音,并可实现高静压,故即使使用细管道,也不会导致风量降低和噪音增大。First, this type of centrifugal blower has a centrifugal impeller that sucks air from the axial direction and discharges it to the circumferential direction by rotation, and has a nose portion close to the centrifugal impeller and concentrates the air discharged from the centrifugal impeller. The vortex-shaped ventilation path leads to the casing of the discharge port, and the longitudinal section of the casing along the axial direction of the centrifugal impeller is approximately oblong, and the width of the axial direction extends from the nose-shaped part to the centrifugal impeller. The rotation direction of the pipe gradually expands, and its largest part is between the above-mentioned discharge port, so that large air volume, low noise, and high static pressure can be realized without increasing the overall volume, so even if a thin pipe is used, it will not cause damage. Reduced air volume and increased noise.
第2,当设上述离心式叶轮的轴方向长度为b,外径为d2,壳体的轴方向最大宽度为Bmax时,通过如下设定,即Second, assuming that the axial length of the above-mentioned centrifugal impeller is b, the outer diameter is d2, and the maximum axial width of the casing is Bmax, it is set as follows, namely
b/d2=0.45~0.70b/d2=0.45~0.70
b,Bmax=0.55~0.75可在实际中取得更为理想的大风量、低噪音、高静压效果。b, Bmax=0.55~0.75 can achieve more ideal effects of large air volume, low noise and high static pressure in practice.
第3,由于上述壳体的轴方向最大宽度部分形成的位置是在从鼻状部向离心式叶轮13旋转方向呈200~310°角,故同样可在实际中取得理想的大风量、低噪音、和高静压效果。Third, since the position of the maximum width in the axial direction of the casing is formed at an angle of 200° to 310° from the nose portion to the direction of rotation of the
第4,由于上述壳体的轴方向最小部分形成的长度是在从鼻状部向离心式叶轮旋转方向至鼻状部附近为止的范围内,故可减少通过鼻状部的间隙而返回的风量,可在增大风量、降低噪音、提高静压方面获得更好效果。Fourth, since the length of the minimum axial portion of the housing is within the range from the nose to the direction of rotation of the centrifugal impeller to the vicinity of the nose, the amount of air returning through the gap in the nose can be reduced. , can achieve better results in terms of increasing air volume, reducing noise, and increasing static pressure.
第5,由于上述壳体的轴方向最小宽度部分形成的长度是在从鼻状部起处在45°角以下的范围内,故在实际中也可取得理想的大风量、低噪音、高静压效果。Fifth, since the length of the minimum width in the axial direction of the above-mentioned housing is within the range of 45° from the nose, ideal large air volume, low noise, and high static pressure can also be obtained in practice. pressure effect.
Claims (5)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP94316509 | 1994-12-20 | ||
| JP31650994A JP3442885B2 (en) | 1994-12-20 | 1994-12-20 | Centrifugal blower |
| JP316509/94 | 1994-12-20 |
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| Publication Number | Publication Date |
|---|---|
| CN1129777A CN1129777A (en) | 1996-08-28 |
| CN1056672C true CN1056672C (en) | 2000-09-20 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN95115116A Expired - Fee Related CN1056672C (en) | 1994-12-20 | 1995-08-18 | Centrifugal blower |
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| Country | Link |
|---|---|
| JP (1) | JP3442885B2 (en) |
| KR (1) | KR960023830A (en) |
| CN (1) | CN1056672C (en) |
| TW (1) | TW272251B (en) |
Families Citing this family (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2001182692A (en) * | 1999-12-28 | 2001-07-06 | Osaka Gas Co Ltd | Centrifugal air blower |
| CN200941495Y (en) | 2006-08-18 | 2007-08-29 | 富士康(昆山)电脑接插件有限公司 | electrical connector |
| JP5439423B2 (en) * | 2011-03-25 | 2014-03-12 | 三菱重工業株式会社 | Scroll shape of centrifugal compressor |
| JP5432295B2 (en) * | 2012-01-10 | 2014-03-05 | 富士工業株式会社 | Belmouth and range hood for blower |
| CN105332939B (en) * | 2014-08-15 | 2018-04-17 | 珠海格力电器股份有限公司 | Net cover ring and fan with same |
| CN204553343U (en) * | 2014-12-19 | 2015-08-12 | 特灵空调系统(中国)有限公司 | Flow blower casing |
| JP6758520B2 (en) * | 2017-10-27 | 2020-09-23 | 三菱電機株式会社 | Centrifugal blower and blower |
| WO2019082392A1 (en) * | 2017-10-27 | 2019-05-02 | 三菱電機株式会社 | Centrifugal blower, air blower device, air conditioning device, and refrigeration cycle device |
| JP7161654B2 (en) * | 2018-02-28 | 2022-10-27 | サンデン株式会社 | Blower |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6295785B1 (en) * | 1999-03-22 | 2001-10-02 | Robert M. Herrmann | Geodesic dome and method of constructing same |
| US9295785B2 (en) * | 2010-12-21 | 2016-03-29 | Sanofi-Aventis Deutschland Gmbh | Front end for an auto-injector |
-
1994
- 1994-12-20 JP JP31650994A patent/JP3442885B2/en not_active Expired - Fee Related
-
1995
- 1995-07-29 TW TW084107867A patent/TW272251B/en active
- 1995-08-18 CN CN95115116A patent/CN1056672C/en not_active Expired - Fee Related
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6295785B1 (en) * | 1999-03-22 | 2001-10-02 | Robert M. Herrmann | Geodesic dome and method of constructing same |
| US9295785B2 (en) * | 2010-12-21 | 2016-03-29 | Sanofi-Aventis Deutschland Gmbh | Front end for an auto-injector |
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| Publication number | Publication date |
|---|---|
| KR960023830A (en) | 1996-07-20 |
| JPH08177795A (en) | 1996-07-12 |
| TW272251B (en) | 1996-03-11 |
| JP3442885B2 (en) | 2003-09-02 |
| CN1129777A (en) | 1996-08-28 |
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