CN111648998A - Blade structure of centrifugal blower - Google Patents

Blade structure of centrifugal blower Download PDF

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CN111648998A
CN111648998A CN201910641193.1A CN201910641193A CN111648998A CN 111648998 A CN111648998 A CN 111648998A CN 201910641193 A CN201910641193 A CN 201910641193A CN 111648998 A CN111648998 A CN 111648998A
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blade
back plate
shape
centrifugal blower
shroud
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CN111648998B (en
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上田和成
日置达也
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Sinko Industries Ltd
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/28Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
    • F04D29/30Vanes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/66Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/661Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
    • F04D29/666Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps by means of rotor construction or layout, e.g. unequal distribution of blades or vanes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/66Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/661Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
    • F04D29/667Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps by influencing the flow pattern, e.g. suppression of turbulence

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

本发明提供一种能够得到鼓风效率、噪音降低效果的离心鼓风机的叶片构造。该离心鼓风机在背板和与所述背板隔开规定间隔地配置的护罩之间竖立设置多个叶片,其中,所述叶片的靠背板侧和护罩侧的叶片旋转方向上的前缘部附近为扭转形状,该扭转形状在所述叶片的靠背板和护罩的附近向外周方向弯曲,所述叶片的与该扭转形状相连的后续部为同一圆柱平面,并且所述前缘部的缘的形状是中央部凹陷的弯曲形状,并且,叶片的宽度方向上的中央部也是自前缘部至后续部为同一圆柱平面。

Figure 201910641193

The present invention provides a blade structure of a centrifugal blower capable of obtaining blowing efficiency and noise reduction effect. In this centrifugal blower, a plurality of vanes are erected between a back plate and a shroud arranged at a predetermined interval from the back plate, wherein the vanes have leading edges in the rotational direction of the vanes on the back plate side and the shroud side. The vicinity of the torsion shape is a twisted shape that is curved in the outer circumferential direction in the vicinity of the backrest plate and the shroud of the blade, the subsequent part of the blade connected to the twisted shape is the same cylindrical plane, and the leading edge of the blade is in the same cylindrical plane. The shape of the edge is a curved shape in which the center portion is recessed, and the center portion in the width direction of the blade is also the same cylindrical plane from the leading edge portion to the subsequent portion.

Figure 201910641193

Description

离心鼓风机的叶片构造Blade structure of centrifugal blower

技术领域technical field

本发明涉及一种空调机等所使用的离心鼓风机的叶片构造。The present invention relates to a blade structure of a centrifugal blower used in an air conditioner or the like.

背景技术Background technique

以往的多叶片风机、离心风机(日文:プラグファン)等离心鼓风机是在空气吸入侧的护罩与马达侧背板之间竖立设置有多个叶片的叶轮的吸入部与风机吸入口组合而成的结构,利用马达的旋转使叶轮旋转而进行鼓风。Centrifugal blowers such as conventional multi-blade fans and centrifugal fans (Japanese: プラグファン) are composed of a combination of a suction part of an impeller with a plurality of blades erected between a shroud on the air suction side and a back plate on the motor side and a fan suction port. The structure uses the rotation of the motor to rotate the impeller to blow air.

所述离心鼓风机如专利文献1所示那样多用于空调设备的鼓风等,将以往的常见的离心风机图示在图1~图4中进行说明。The centrifugal blower is often used for blowing air of an air-conditioning apparatus, etc., as shown in Patent Document 1, and a conventional conventional centrifugal blower is illustrated in FIGS. 1 to 4 .

如图2所示,是图1中的包括护罩a、叶片b、背板c的叶轮d的吸入部e与风机吸入口g组合而成的结构。利用轮毂等(紧固接头)j将马达轴h紧固于叶轮d的背板c,利用马达i的旋转使叶轮d旋转。As shown in FIG. 2 , it is a structure in which the suction part e of the impeller d including the shroud a, the vane b, and the back plate c in FIG. 1 is combined with the fan suction port g. The motor shaft h is fastened to the back plate c of the impeller d by a hub or the like (fastening joint) j, and the impeller d is rotated by the rotation of the motor i.

在此,所述叶片b的形状为图3~图4所示的形状,整体为将图1、图3所示那样的圆柱的一部分被切掉了的形状,在护罩a与背板c之间以自吸入部e(参照图1)朝向外周的排出部f倾斜的方式配置。在图3中,下侧为沿着背板c的直线b1,上侧为沿着护罩a的内侧面的形状,图3中的右侧的吸入部e的附近为隆起的形状b2,与其相连地具有水平缘b3,将风切断的前面缘为直线b4,后面缘也是上下方向上的直线b5。Here, the shape of the blade b is the shape shown in FIGS. 3 to 4 , and the whole is a shape in which a part of the column as shown in FIG. 1 and FIG. 3 is cut away. It is arrange|positioned so that it may incline toward the discharge part f of the outer periphery from the suction part e (refer FIG. 1). In FIG. 3 , the lower side is the straight line b1 along the back plate c, the upper side is the shape along the inner surface of the shroud a, and the vicinity of the suction part e on the right side in FIG. 3 is the bulging shape b2. The horizontal edge b3 is connected to each other, the front edge which cuts off the wind is the straight line b4, and the rear edge is also the straight line b5 in the vertical direction.

图3中的叶片b的沿着剖切线A-A’、B-B’、C-C’的剖视图是图4。The sectional view of the blade b in Fig. 3 along the sectional lines AA', BB', CC' is Fig. 4 .

像这样,在图4中,叶片b的沿着各剖切线A-A’、B-B’、C-C’的截面为同一形状,是相同的叶片截面形状在叶片的宽度方向上连续的叶片形状,容易制作,但在叶片前缘部和叶片之间的流路内会产生气流湍流,而导致风机的鼓风效率降低,还会产生因风噪声导致的噪音。In this way, in FIG. 4 , the cross-sections of the blade b along the cutting lines AA', BB', and CC' have the same shape, and the same blade cross-sectional shape is continuous in the width direction of the blade. The blade shape is easy to manufacture, but the airflow turbulence is generated in the flow path between the blade leading edge and the blade, which reduces the blowing efficiency of the fan and generates noise due to wind noise.

现有技术文献prior art literature

专利文献Patent Literature

专利文献1:日本特开2013-96378号公报Patent Document 1: Japanese Patent Laid-Open No. 2013-96378

发明内容SUMMARY OF THE INVENTION

发明要解决的问题Invention to solve problem

本发明是鉴于上述的问题点而做成的,着眼于即使叶片的上下的宽度方向上的形状变化也能够期待改善鼓风效率的情况,想要提供一种通过使叶片的上下的宽度方向上的形状变化来得到鼓风效率、噪音降低效果的离心鼓风机的叶片构造。The present invention has been made in view of the above-mentioned problems, and, in view of the fact that it is expected to improve the blowing efficiency even if the shape of the upper and lower width directions of the blades is changed, it is intended to provide a method by making the upper and lower width directions of the blades The blade structure of the centrifugal blower can be obtained by changing the shape of the centrifugal blower to obtain the blowing efficiency and noise reduction effect.

用于解决问题的方案solution to the problem

为了解决上述问题,技术方案1的发明是一种离心鼓风机的构造,该离心鼓风机在背板和与所述背板隔开规定间隔地配置的护罩之间竖立设置多个叶片,其中,所述叶片的靠背板侧和护罩侧的叶片旋转方向上的前缘部附近为扭转形状,该扭转形状在所述叶片的靠背板和护罩的附近向外周方向弯曲,所述叶片的与该扭转形状相连的后续部为同一圆柱平面,并且所述前缘部的缘的形状是中央部凹陷的弯曲形状。In order to solve the above-mentioned problems, the invention of claim 1 is a centrifugal blower in which a plurality of blades are erected between a back plate and a shroud arranged at a predetermined interval from the back plate, wherein the The vicinity of the front edge portion in the rotation direction of the blade on the back plate side and the shroud side of the blade has a twisted shape, and the torsion shape is curved in the outer peripheral direction in the vicinity of the back plate and the shroud of the blade. The subsequent parts connected in the twisted shape are the same cylindrical plane, and the shape of the edge of the front edge part is a curved shape with a concave central part.

技术方案2的发明是一种离心鼓风机的叶片构造,其特征在于,叶片的宽度方向上的中央部自前缘部至后续部为同一圆柱平面。The invention of claim 2 is a blade structure for a centrifugal blower, characterized in that the central part in the width direction of the blade is the same cylindrical plane from the leading edge part to the subsequent part.

在技术方案1或2所述的离心鼓风机的叶片构造的基础上,技术方案3的发明的特征在于,所述叶片的前缘部和背板的连接部的附近呈缓坡状延伸。In addition to the blade structure of the centrifugal blower according to claim 1 or 2, the invention of claim 3 is characterized in that the vicinity of the connecting portion between the front edge portion and the back plate of the blade extends in a gentle slope.

发明的效果effect of invention

采用技术方案1的离心鼓风机的叶片构造,利用叶片前缘部的扭转形状,使叶片入口角自叶片宽度方向上的中央部到背板和护罩连续地变小,从而叶片前缘部的气流的流入状态得到改善,不仅能够抑制因叶片与气流的碰撞产生的湍流,还能够抑制整个流路的湍流,能够实现高效率化、低噪音化。With the blade structure of the centrifugal blower of claim 1, the torsional shape of the leading edge of the blade is used to continuously reduce the inlet angle of the blade from the center in the width direction of the blade to the back plate and the shroud, so that the airflow at the leading edge of the blade is reduced. The inflow state of the air flow is improved, and not only the turbulent flow caused by the collision between the blades and the airflow can be suppressed, but also the turbulent flow of the entire flow path can be suppressed, and high efficiency and low noise can be achieved.

并且,采用技术方案2的离心鼓风机的叶片构造,除技术方案1的效果之外,还能够通过使叶片宽度方向上的中央部在叶片的宽度方向上呈圆柱状平行地延长,从而能够维持对高效率化、低噪音化有效的叶片扭转形状部,并且能够使叶片宽度可变,由此能够非常容易地制作能维持效率并且为同一叶轮直径且风量不同的风机。Furthermore, according to the blade structure of the centrifugal blower according to claim 2, in addition to the effect of claim 1, by extending the central portion in the width direction of the blade in a columnar shape in parallel with the width direction of the blade, it is possible to maintain the accuracy of the blade. The blade twist-shaped portion is effective for high efficiency and low noise, and the blade width can be changed, thereby making it possible to very easily manufacture a fan having the same impeller diameter and different air volumes while maintaining efficiency.

而且,采用技术方案3的离心鼓风机的叶片构造,除技术方案1或2的效果之外,还能够通过使叶片的前缘部和背板的连接部的附近呈缓坡状延伸,来进一步改善叶片前缘的背板附近部的气流的流入状态,实现进一步高效率化、低杂音化。Furthermore, according to the blade structure of the centrifugal blower of claim 3, in addition to the effects of claim 1 or 2, the blade can be further improved by extending the vicinity of the connecting portion between the leading edge portion of the blade and the back plate in a gentle slope shape. The inflow state of the airflow in the vicinity of the back plate of the leading edge achieves further improvement in efficiency and reduction in noise.

附图说明Description of drawings

图1是以往的离心鼓风机的叶轮构造的立体说明图。FIG. 1 is an explanatory perspective view of an impeller structure of a conventional centrifugal blower.

图2是以往的离心鼓风机组装于空调设备的状态的侧视图。2 is a side view of a state in which a conventional centrifugal blower is assembled in an air conditioner.

图3是图1中的以往的叶片单体的侧视图。FIG. 3 is a side view of the conventional blade in FIG. 1 .

图4是图3中的叶片的沿着切断线的剖视图。FIG. 4 is a cross-sectional view of the blade of FIG. 3 along a cutting line.

图5是本发明的实施例1的离心鼓风机的叶轮构造的立体说明图。5 is an explanatory perspective view of the impeller structure of the centrifugal blower according to the first embodiment of the present invention.

图6是图示在实施例1的叶片单体中叶片的剖断线的部位的侧视图。6 is a side view illustrating a portion of a section line of the blade in the blade unit of Example 1. FIG.

图7是图6中的实施例1的叶片的沿着各剖切线的剖视图。FIG. 7 is a cross-sectional view of the blade of Example 1 in FIG. 6 along each cutting line.

图8是叶片的入口角α的说明图。FIG. 8 is an explanatory diagram of the inlet angle α of the blade.

图9是本发明的实施例2的离心鼓风机的叶轮构造的立体说明图。9 is an explanatory perspective view of the impeller structure of the centrifugal blower according to the second embodiment of the present invention.

图10是图9中的实施例2的叶片的侧视图。FIG. 10 is a side view of the blade of Example 2 in FIG. 9 .

附图标记说明Description of reference numerals

1、背板;2、护罩;3、叶片;31、叶片下侧;312、背板侧前缘部附近(Y1);313、背板侧缓坡状部(X1);32、叶片前缘部;321、弯曲部(X2);33、叶片上侧;331、护罩侧前缘部附近(Y2);332、凸形状部;34、叶片后缘部;4、叶轮;5、吸入部;6、排出部;7、风机吸入口1. Back plate; 2. Shroud; 3. Blade; 31. Lower side of blade; 312. Near the front edge of the back plate (Y1); 313. The gentle slope of the back plate side (X1); 32. The leading edge of the blade part; 321, curved part (X2); 33, the upper side of the blade; 331, the vicinity of the front edge of the shroud side (Y2); 332, the convex part; 34, the rear edge part of the blade; 4, the impeller; 5, the suction part ; 6. Discharge part; 7. Fan suction port

具体实施方式Detailed ways

参照附图说明本发明的离心鼓风机的叶片构造的实施例,参照图5~图8说明实施例1,参照图9、图10说明实施例2。Embodiments of the blade structure of the centrifugal blower of the present invention will be described with reference to the drawings, Embodiment 1 will be described with reference to FIGS. 5 to 8 , and Embodiment 2 will be described with reference to FIGS. 9 and 10 .

[实施例1][Example 1]

对本发明的离心鼓风机的叶片构造的优选的实施例1进行说明,图5的离心鼓风机的叶轮4与以往同样地以图2所示那样的结构,配置于空调设备内的鼓风室。Preferred Embodiment 1 of the blade structure of the centrifugal blower of the present invention will be described. The impeller 4 of the centrifugal blower of FIG. 5 is arranged in the blower chamber in the air conditioner with the same structure as shown in FIG. 2 as in the related art.

首先,从组装于图5中的实施例1的叶轮4的叶片3开始进行说明,该叶轮4与风机吸入口7相组合。First, the vane 3 assembled to the impeller 4 of the first embodiment in FIG. 5 , which is combined with the fan suction port 7 , will be described.

叶轮4的叶片3以等间隔自吸入部5朝向外周的排出部6倾斜地配置在背板1与护罩2之间。The blades 3 of the impeller 4 are disposed at equal intervals between the back plate 1 and the shroud 2 so as to be inclined from the suction portion 5 toward the outer peripheral discharge portion 6 .

叶片3的叶片下侧31为沿着背板1的形状,叶片上侧33为沿着护罩2的内侧面的形状,叶片上侧33的将空气切断的吸入部5的附近具有隆起的凸形状部332。The blade lower side 31 of the blade 3 is shaped along the back plate 1, the blade upper side 33 is shaped along the inner surface of the shroud 2, and the blade upper side 33 has a raised protrusion near the suction part 5 that cuts off the air. Shape portion 332 .

并且,将空气切开的叶片前缘部32具有弯曲部321(X2),该弯曲部321(X2)具有稍微向内侧凹陷的曲线,缓坡状部313(X1)设在叶片3的叶片前缘部32和背板1的背板吸入部5的附近,向前方延伸。利用该缓坡状部31(X1),不仅能够抑制因叶片和气流产生的湍流,还能够抑制整个流路的湍流,能够实现高效率化、低噪音化。同样地,所述弯曲部321(X2)也是抑制空气湍流的形状。另外,本实施例的叶片后缘部34是上下方向上的直线,但也可以是其他形状。In addition, the leading edge portion 32 of the blade in which the air is cut has a curved portion 321 ( X2 ) having a curve slightly concave inward, and a gently sloped portion 313 ( X1 ) is provided on the leading edge of the blade 3 The part 32 and the vicinity of the back panel suction part 5 of the back panel 1 extend forward. This gentle slope-shaped portion 31 ( X1 ) can suppress not only the turbulent flow due to the vanes and the airflow, but also the turbulent flow of the entire flow path, thereby achieving high efficiency and low noise. Likewise, the curved portion 321 (X2) is also shaped to suppress air turbulence. In addition, although the blade trailing edge portion 34 of the present embodiment is a straight line in the vertical direction, other shapes may be used.

另外,如图7所示,背板1侧的叶片旋转方向上的前缘部附近312为扭转形状Y1(实线),扭转方向在背板1的附近向外周外侧弯曲,即:A-A’截面形状相比中央的C-C’(虚线)截面形状而言弯曲平缓且向外周外侧扭转。同样地,叶片3的护罩2侧的叶片旋转方向上的前缘部附近331也为扭转形状Y2(实线),扭转方向在护罩2的附近向外周外侧弯曲。在以实施例1的数值进行表示时,例如叶片3的上下高度为140mm,在图7中,如果将作为基准的C-C’截面形状中的前缘部处的曲率半径R3设为313.2mm,则A-A’截面形状中的前缘部处的曲率半径R1为333.2mm,距离a1为4.9mm左右。并且,E-E’截面形状中的前缘部处的曲率半径R2为318.3mm,距离a2为1.7mm左右。In addition, as shown in FIG. 7 , the vicinity of the leading edge portion 312 in the rotation direction of the blade on the side of the backing plate 1 is a twisted shape Y1 (solid line), and the twisting direction is bent to the outer peripheral outer side in the vicinity of the backing plate 1, that is: AA 'Cross-sectional shape is curved more gently than the central CC' (broken line) cross-sectional shape, and is twisted to the outside of the outer periphery. Similarly, the vicinity of the leading edge portion 331 of the blade 3 in the blade rotation direction on the side of the shroud 2 also has a twisted shape Y2 (solid line), and the twist direction is curved to the outer peripheral outer side in the vicinity of the shroud 2 . When expressed by the numerical values of Example 1, for example, the vertical height of the blade 3 is 140 mm, and in FIG. 7 , the radius of curvature R3 at the leading edge of the CC' cross-sectional shape serving as a reference is set to 313.2 mm , the radius of curvature R1 at the front edge in the AA' cross-sectional shape is 333.2 mm, and the distance a1 is about 4.9 mm. In addition, the curvature radius R2 of the front edge portion in the EE' cross-sectional shape is 318.3 mm, and the distance a2 is about 1.7 mm.

利用前缘部附近312、331的扭转形状Y1、Y2,使叶片入口角α自叶片3的上下宽度中央部(C-C')到背板1和护罩2连续地变小。在利用图8说明该入口角α时,叶片3(图8)的中央部的由点划线所示的切线与叶片内切圆R所成的角度、即入口角为α1,但通过使前缘部附近设为扭转形状Y1、Y2,入口角为α2的叶片前缘部(32)整体都接近于空气的流入角度,因此叶片3的前缘部附近312、331的气流的流入状态得到改善,不仅能够抑制因叶片与气流的碰撞产生的湍流,还能够抑制整个流路的湍流,能够实现高效率化、低噪音化。By the twisted shapes Y1 and Y2 of the vicinity of the leading edge portions 312 and 331 , the blade inlet angle α is continuously reduced from the vertical width center portion (CC′) of the blade 3 to the back plate 1 and the shroud 2 . When this inlet angle α is described with reference to FIG. 8 , the angle formed by the tangent line at the center of the vane 3 ( FIG. 8 ) indicated by the dashed-dotted line and the vane inscribed circle R, that is, the inlet angle is α1, but by setting the front The vicinity of the edge is made into twisted shapes Y1 and Y2, and the entire blade leading edge (32) with the inlet angle α2 is close to the inflow angle of the air, so the inflow state of the airflow in the vicinity of the leading edge 312 and 331 of the blade 3 is improved. , not only can suppress the turbulent flow caused by the collision between the blade and the airflow, but also can suppress the turbulent flow of the entire flow path, and can achieve high efficiency and low noise.

[实施例2][Example 2]

在本发明中,通过调节离心鼓风机的叶轮4内的叶片3的上下宽度中央部的带的宽度,能够使前缘部附近的扭转形状Y1、Y2保持原样,从而能够维持高效率化、低噪音化,并且能够容易地变更叶片宽度(Z)。因而,能够设计、制造与设计风量相对应的离心风机。In the present invention, by adjusting the width of the belt at the center of the vertical width of the blade 3 in the impeller 4 of the centrifugal blower, the twisted shapes Y1 and Y2 near the leading edge portion can be kept as they are, and high efficiency and low noise can be maintained. , and the blade width (Z) can be easily changed. Therefore, the centrifugal fan corresponding to the designed air volume can be designed and manufactured.

在此,参照图9和图10说明使叶轮4’的上下宽度变化并且为与鼓风量相对应的叶片宽度的实施例2。Here, a second embodiment in which the vertical width of the impeller 4' is changed to have the blade width corresponding to the blowing volume will be described with reference to Figs. 9 and 10 .

图9是实施例2的叶轮4’的立体图,如图10所示,叶片3的前缘部附近的扭转形状Y1、Y2与实施例1的相同,与以往的一部分圆柱状的叶片相比,鼓风效率得到提高,并且噪音也得到降低。即,只要在使叶片3的上下宽度变化时使叶片3的中央部的带状部分(单点划线C-C’D-D’)的上下宽度z伸缩而使整体的上下宽度Z伸长或者缩短,并且将存在于背板1侧和护罩2侧的扭转形状Y1、Y2保持原样即可。9 is a perspective view of the impeller 4 ′ according to the second embodiment. As shown in FIG. 10 , the torsional shapes Y1 and Y2 near the leading edge portion of the blade 3 are the same as those of the first embodiment, and compared with the conventional partially cylindrical blades, The blowing efficiency is improved and the noise is also reduced. That is, when the vertical width of the blade 3 is changed, the vertical width z of the belt-shaped portion (the one-dot chain line CC'DD') in the central part of the blade 3 is expanded and contracted, and the overall vertical width Z can be extended. Alternatively, it may be shortened, and the twisted shapes Y1 and Y2 existing on the back plate 1 side and the shield 2 side may be kept as they are.

像这样,能够维持对高效率化、低噪音化有效的叶片扭转形状部并且容易改变叶片宽度,能够容易地形成同一叶轮直径且风量不同的风机。In this way, the blade width can be easily changed while maintaining the blade twist shape portion effective for high efficiency and noise reduction, and a fan having the same impeller diameter and different air volumes can be easily formed.

由于是以上那样的结构,因此,采用各实施例的离心鼓风机的叶片构造,利用叶片前缘部的扭转形状,使叶片入口角自叶片宽度方向上的中央部到背板和护罩连续地变小,从而叶片前缘部的气流的流入状态得到改善,不仅能够抑制因叶片与气流的碰撞产生的湍流,还能够抑制整个流路的湍流,能够实现高效率化、低噪音化。Because of the above structure, the blade structure of the centrifugal blower of each embodiment is adopted, and the blade inlet angle is continuously changed from the center in the blade width direction to the back plate and the shroud by utilizing the twisted shape of the blade leading edge. When the blade is small, the inflow state of the airflow at the leading edge of the blade is improved, and turbulence caused by the collision between the blade and the airflow can be suppressed, and the turbulent flow of the entire flow path can be suppressed, and high efficiency and low noise can be achieved.

并且,通过使叶片宽度方向上的中央部在叶片的宽度方向上呈圆柱状平行地延长,能够维持对高效率化、低噪音化有效的叶片扭转形状部,并且即使叶片宽度可变也能取得鼓风效率、降低噪音的效果。由此,能够非常容易地制作维持效率并且为同一叶轮直径且风量不同的风机。In addition, by extending the central portion in the width direction of the blade in a columnar shape in parallel with the width direction of the blade, it is possible to maintain the blade twist shape portion effective for high efficiency and noise reduction, and even if the blade width is variable. The effect of blowing efficiency and noise reduction. Thereby, it is possible to very easily manufacture a fan having the same impeller diameter and different air volumes while maintaining efficiency.

而且,叶片的前缘部和背板的连接部的附近呈缓坡状延伸,因此能够进一步改善叶片前缘的背板附近部的气流的流入状态,实现进一步高效率化、低杂音化。Furthermore, since the vicinity of the connection between the leading edge of the blade and the back plate extends in a gentle slope, it is possible to further improve the inflow state of the airflow in the vicinity of the back plate of the leading edge of the blade, and achieve further higher efficiency and lower noise.

另外,不言而喻,只要不破坏本发明的特征即可,并不限定于上述的实施例,在实施例中,应用于空调设备的鼓风机,但例如,也可以用作鼓风机单体。In addition, it goes without saying that the present invention is not limited to the above-described embodiments as long as the characteristics of the present invention are not destroyed. In the embodiments, the embodiment is applied to a blower of an air conditioner, but it can be used as a blower alone, for example.

Claims (3)

1. A blade structure of a centrifugal blower in which a plurality of blades are erected between a back plate and a shroud disposed at a predetermined interval from the back plate,
the blade has a twisted shape in the vicinity of the leading edge in the direction of rotation of the blade on the back plate side and the shroud side, the twisted shape being curved in the peripheral direction in the vicinity of the back plate and the shroud of the blade, the trailing portion of the blade connected to the twisted shape being the same cylindrical plane, and the edge of the leading edge having a curved shape in which the central portion is recessed.
2. The centrifugal blower vane construction of claim 1,
the central part of the blade in the width direction is the same cylindrical plane from the front edge part to the subsequent part.
3. The vane structure of a centrifugal blower according to claim 1 or 2,
the blade has a front edge portion and a back plate, and a portion near a connecting portion between the front edge portion and the back plate extends in a gentle slope.
CN201910641193.1A 2019-03-04 2019-07-16 Blade structure of centrifugal blower Active CN111648998B (en)

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