CN213039523U - Blade, centrifugal fan and electrical equipment - Google Patents
Blade, centrifugal fan and electrical equipment Download PDFInfo
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- CN213039523U CN213039523U CN202022291754.0U CN202022291754U CN213039523U CN 213039523 U CN213039523 U CN 213039523U CN 202022291754 U CN202022291754 U CN 202022291754U CN 213039523 U CN213039523 U CN 213039523U
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Abstract
The utility model relates to a blade, centrifugal fan and electrical equipment. The thickness of the blade is gradually increased and then gradually reduced from one end of the tail edge 12 of the blade to one end of the front edge 11 of the blade, and the thickness of the tail edge 12 of the blade is larger than 1.5 mm. The centrifugal fan comprises an impeller 3 and a plurality of blades arranged on the impeller 3, wherein the plurality of blades are uniformly distributed along the circumferential direction of the axis of the impeller 3, and the tail edge 12 of each blade is positioned on the outer diameter circle of the impeller 3. The utility model provides a blade, centrifugal fan and electrical equipment have and to compromise large-traffic, low noise and efficient effect, can also improve the intensity of moulding plastics of blade simultaneously, are convenient for mould plastics in batches and produce the blade.
Description
Technical Field
The utility model relates to a centrifugal fan technical field especially relates to a blade, centrifugal fan and electrical equipment.
Background
The front edge, the pressure surface, the tail edge and the suction surface of the blade are sequentially connected end to form an area which forms a fan blade, and the pressure surface is opposite to the suction surface. Most of the blades on the existing centrifugal fan impeller are designed according to airfoil blades so as to improve the performance of the fan, and when the blades are completely designed according to the airfoil blades, the tail edges of the blades are very thin, the strength of the blades is low, the blades are easily broken, the blades are not favorable for injection molding so as to facilitate mass production, and the centrifugal fan is reduced in efficiency and noise and small in flow.
SUMMERY OF THE UTILITY MODEL
The utility model discloses to the not enough problem of current blade intensity, provided a blade, centrifugal fan and electrical equipment, this blade, centrifugal fan and electrical equipment can reach and compromise large-traffic, low noise and efficient technological effect, still are convenient for mass production blade simultaneously.
A vane, the thickness of the vane gradually increases and then gradually decreases from one end of the trailing edge of the vane to one end of the leading edge of the vane, the thickness of the trailing edge of the vane is greater than 1.5 mm.
In one embodiment, the pressure surface of the blade and the suction surface of the blade are both cambered surfaces, and the pressure surface is concave towards the suction surface and the suction surface is convex away from the pressure surface.
The centrifugal fan comprises an impeller and a plurality of blades arranged on the impeller according to any one of the embodiments, the blades are uniformly distributed along the axial direction of the impeller, and the tail edge of each blade is located on the outer diameter circle of the impeller.
In one embodiment, the diameter of the co-tangent circle of the leading edges of the plurality of vanes is the vane inlet diameter D1, and the diameter of the co-tangent circle of the trailing edges of the plurality of vanes is the vane outlet diameter D2;
the vane inlet diameter D1 and the vane outlet diameter D2 satisfy: D1/D2 is 0.8-0.82.
In one embodiment, the length L of the center line of each blade and the width t1 of the blade path of the centrifugal fan satisfy: l/t1 is 2.0-2.2.
In one embodiment, the device further comprises a volute, and the impeller is rotatably arranged inside the volute;
the molded line of the volute is a spiral line and comprises a first bending section, a second bending section, a third bending section and a fourth bending section which are connected in sequence, and the first bending section is connected with a volute tongue of the volute;
the four sequentially connected arc sections obtained based on an equilateral element method comprise a first reference section, a second reference section, a third reference section and a fourth reference section, wherein the first reference section is connected with the volute tongue in a reference manner;
the second, third, and fourth curved segments are configured to coincide with the second, third, and fourth reference segments, respectively, and the first curved segment is configured as a circular arc segment having a curvature less than a curvature of the first reference segment.
In one embodiment, the distance from the connecting point of the first curved section and the volute tongue to the outer diameter circle of the impeller is volute tongue clearance t3, the diameter of the outer diameter circle of the impeller is D2', and the following conditions are met: t 3/D2' is 0.06-0.07.
In one embodiment, the second curved section comprises a first connecting section, a first straight section and a second connecting section which are connected in sequence, the first connecting section is connected with the first curved section, and the second connecting section is connected with the third curved section;
the second reference segment comprises a first reference arc segment, a second reference arc segment and a third reference arc segment which are sequentially connected, the first reference arc segment is connected with the first reference segment, and the third reference arc segment is connected with the third reference segment;
the first and second connection segments are configured to coincide with the first and third reference arc segments, respectively;
the maximum vertical distance from the first straight line segment to the axis of the impeller is smaller than the maximum vertical distance from the second reference segment to the axis of the impeller.
In one embodiment, the fourth bending section comprises a third connecting section, a second straight section and a fourth connecting section which are connected in sequence, and the third connecting section is connected with the third bending section;
the fourth reference segment comprises a fourth reference arc segment, a fifth reference arc segment and a sixth reference arc segment which are connected in sequence, and the fourth reference arc segment is connected to the third reference segment in a reference manner;
the third and fourth connection segments are configured to coincide with the fourth and sixth reference arc segments, respectively;
the maximum vertical distance from the fifth reference section to the axis of the impeller is greater than the maximum vertical distance from the second straight section to the axis of the impeller.
In one embodiment, the first straight line segment and the second straight line segment are both parallel to a tangent of an outer diameter circle of the impeller, a distance from a connection point of the first bent segment and the first connection segment to the outer diameter circle of the impeller is a first distance t7, a distance from the first straight line segment to the outer diameter circle of the impeller is a second distance t6, a distance from a connection point of the third bent segment and the third connection segment to the outer diameter circle of the impeller is a third distance t5, and a distance from the second straight line segment to the outer diameter circle of the impeller is a fourth distance t4, so that:
t6/t7>0.85, and t4/t5> 0.9.
In addition, an electrical apparatus is provided, comprising the centrifugal fan as described in any of the above embodiments.
According to the blade, the thickness of the blade is gradually increased from one end of the tail edge to one end of the front edge and gradually reduced, so that the blade has the characteristics of an airfoil-shaped blade, can effectively reduce the flow resistance, and has the effects of improving the aerodynamic characteristics in the impeller, controlling the separation of blade channels and improving the efficiency of the fan on the premise of increasing the air volume; meanwhile, the thickness of the tail edge of the blade is larger than 1.5mm, so that the strength of the tail edge of the blade is improved, the injection molding strength of the blade is further improved, and the mass production of the blade through injection molding is facilitated; in addition, the strength of the tail edge of the blade is improved, the problems of efficiency reduction, noise increase and flow reduction of the centrifugal fan caused by breakage of the tail edge can be effectively solved, and the technical effects of high flow, low noise and high efficiency can be achieved.
Drawings
Fig. 1 is a schematic structural diagram of a blade according to an embodiment of the present invention;
fig. 2 is a schematic view of a part of a centrifugal fan according to an embodiment of the present invention;
fig. 3 is a schematic view of a part of the centrifugal fan according to another embodiment of the present invention;
fig. 4 is a parameter comparison diagram of the centrifugal fan shown in fig. 3.
Description of reference numerals:
a blade 1; a leading edge 11; a trailing edge 12; a pressure surface 13; a suction surface 14; a volute 2; a volute tongue 21; a first curved section 22; a first reference segment 22'; a second curved section 23; a second reference segment 23'; a third curved section 24; a fourth curved section 25; a fourth reference segment 25'; a first straight line segment 231; a second straight line segment 251; an impeller 3.
Detailed Description
In order to make the above objects, features and advantages of the present invention more comprehensible, embodiments of the present invention are described in detail below with reference to the accompanying drawings. In the following description, numerous specific details are set forth in order to provide a thorough understanding of the present invention. The present invention may, however, be embodied in many different forms and should not be construed as limited to the embodiments set forth herein, as those skilled in the art will be able to make similar modifications without departing from the spirit and scope of the present invention.
In the description of the present invention, it is to be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", "axial", "radial", "circumferential", and the like, indicate the orientation or positional relationship based on the orientation or positional relationship shown in the drawings, and are only for convenience of description and simplicity of description, and do not indicate or imply that the device or element referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be construed as limiting the present invention.
Furthermore, the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include at least one such feature. In the description of the present invention, "a plurality" means at least two, e.g., two, three, etc., unless specifically limited otherwise.
In the present invention, unless otherwise expressly stated or limited, the terms "mounted," "connected," and "fixed" are to be construed broadly and may, for example, be fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; they may be directly connected or indirectly connected through intervening media, or they may be connected internally or in any other suitable relationship, unless expressly stated otherwise. The specific meaning of the above terms in the present invention can be understood according to specific situations by those skilled in the art.
In the present application, unless expressly stated or limited otherwise, the first feature may be directly on or directly under the second feature or indirectly via intermediate members. Also, a first feature "on," "over," and "above" a second feature may be directly or diagonally above the second feature, or may simply indicate that the first feature is at a higher level than the second feature. A first feature being "under," "below," and "beneath" a second feature may be directly under or obliquely under the first feature, or may simply mean that the first feature is at a lesser elevation than the second feature.
It will be understood that when an element is referred to as being "secured to" or "disposed on" another element, it can be directly on the other element or intervening elements may also be present. When an element is referred to as being "connected" to another element, it can be directly connected to the other element or intervening elements may also be present. The terms "vertical," "horizontal," "upper," "lower," "left," "right," and the like as used herein are for illustrative purposes only and do not denote a unique embodiment.
Referring to fig. 1, an embodiment of the present invention provides a blade 1, a thickness of the blade 1 gradually increases from one end of a trailing edge 12 of the blade 1 to one end of a leading edge 11 of the blade 1, and then gradually decreases, the thickness of the leading edge 11 of the blade 1 is not less than the thickness of the trailing edge 12 of the blade 1, and the thickness of the trailing edge 12 of the blade 1 is greater than 1.5 mm.
The thickness of the blade 1 is gradually increased and gradually reduced from one end of the tail edge 12 to one end of the front edge 11, so that the blade 1 has the characteristics of an airfoil-shaped blade, can effectively reduce the flow resistance, and has the effects of improving the aerodynamic characteristics in the impeller 3, controlling the separation of blade channels and improving the efficiency of the fan on the premise of increasing the air volume; meanwhile, the thickness of the tail edge 12 of the blade 1 is larger than 1.5mm, so that the strength of the tail edge 12 of the blade 1 is improved, the injection molding strength of the blade 1 is further improved, and the mass production of the blade 1 through injection molding is facilitated; in addition, the strength of the tail edge 12 of the blade 1 is improved, the problems of efficiency reduction, noise increase and flow reduction of the centrifugal fan caused by breakage of the tail edge 12 can be effectively solved, and the technical effects of high flow, low noise and high efficiency can be achieved.
It should be noted that the thickness of the blade 1 is gradually increased and gradually decreased, so that the lines of the suction surface 14 and the pressure surface 13 can be ensured to be smooth, and the flow resistance of the blade 1 is reduced.
In actual use, the thickness of the trailing edge 12 of the blade 1 may be 1.6mm, 1.7mm, 1.8mm, 2.0mm, etc.
The blade 1 includes a leading edge 11, a pressure surface 13, a trailing edge 12 and a suction surface 14, which are connected in sequence, the leading edge 11 is opposite to the trailing edge 12, the pressure surface 13 is opposite to the suction surface 14, and a region enclosed by the leading edge 11, the pressure surface 13, the trailing edge 12 and the suction surface 14 is the blade 1.
Alternatively, referring to fig. 1, the pressure surface 13 and the suction surface 14 are both cambered surfaces, the pressure surface 13 being concave towards the suction surface 14, the suction surface 14 being convex away from the pressure surface 13. At this time, the pressure surface 13 has a larger curvature than the suction surface 14, so that the purpose of increasing the pressure rise and reducing the boundary layer separation at the time of decreasing the flow rate can be achieved.
Further, referring to fig. 1, the pressure surface 13 is an arc surface, and the suction surface 14 is an arc surface formed when a salient point on the arc surface concentric with the pressure surface 13 at a position of 25% to 45% of the length of the arc surface protrudes in a direction away from the pressure surface 13, and the thickness of the blade 1 at the salient point corresponds to the maximum relative thickness of the blade 1. It will be appreciated that the high points are near the leading edge 11.
Referring to fig. 1, at this time, the radius of the pressure surface 13 is Ra, the radius of the arc segment of the suction surface 14 intersecting the trailing edge 12 and concentric with the pressure surface 13 is Rb, and the thickness t2 of the trailing edge 12 is Rb-Ra.
In other embodiments, the pressure surface 13 and the suction surface 14 may also adopt the existing airfoil structural design, for example, the suction surface 14 and the pressure surface 13 are arranged to be relatively protruded, as long as the thickness of the trailing edge 12 is ensured to be greater than 1.5mm under the condition of having the advantages of effectively reducing the flow resistance of the airfoil blade 1, and the like, so as to ensure the strength of the trailing edge 12.
Further, the front edge 11 is a circular arc surface, and the front edge 11 is smoothly connected with the pressure surface 13 and the suction surface 14, which contributes to reducing the flow resistance.
In addition, referring to fig. 2 to 4, an embodiment of the present invention further provides a centrifugal fan, including an impeller 3 and a plurality of blades 1 disposed on the impeller 3 as described in the above embodiments, wherein the plurality of blades 1 are uniformly arranged along the circumferential direction of the axis of the impeller 3, and the trailing edge 12 of each blade 1 is located on the outer diameter circle of the impeller 3.
It will be appreciated that the leading edge 11 of the blade 1 is disposed closer to the axis of the impeller 3 than the trailing edge 12 of the blade 1.
In actual use, the thickness of the blade 1 is gradually increased and then gradually reduced from one end of the tail edge 12 to one end of the front edge 11, so that the blade 1 has the characteristics of an airfoil-shaped blade 1, can effectively reduce flow resistance, and has the effects of improving aerodynamic characteristics in the impeller 3 on the premise of increasing air volume, controlling blade channel separation and improving the efficiency of a centrifugal fan; meanwhile, the strength of the tail edge 12 of the blade 1 is improved, the problems of efficiency reduction, noise increase and flow reduction of the centrifugal fan caused by breakage of the tail edge 12 can be effectively solved, and the technical effects of high flow rate, low noise and high efficiency can be achieved.
Further, referring to fig. 2, the diameter of the first co-tangent circle of the leading edge 11 of the plurality of blades 1 is the blade 1 inlet diameter D1, the diameter of the second co-tangent circle of the trailing edge 12 of the plurality of blades 1 is the blade 1 outlet diameter D2, and the blade 1 inlet diameter D1 and the blade 1 outlet diameter D2 satisfy: D1/D2 is 0.8-0.82. At this moment, under this proportion, blade 1 can effectively resist high static pressure, guarantees centrifugal fan's gas flow.
In actual use, the design that D1/D2 is 0.81 can be realized.
Wherein the first co-tangential circle is a circle that is tangential to the leading edge 11 of each blade 1 and the second co-tangential circle is a circle that is tangential to the trailing edge 12 of each blade 1. Since the trailing edge 12 is located on the outer diameter circle of the impeller 3, i.e. the trailing edge 12 is tangent to the outer diameter circle of the impeller 3, the diameter of the outer diameter circle of the impeller 3 is equal to the outlet diameter D2 of the blade 1.
It is understood that the first and second co-tangential circles are all concentric with the outer diameter circle of the impeller 3. The circle which is located between the first and second co-tangent circles and has the same distance to the first and second co-tangent circles is the median circle of the blade 1, the diameter of the median circle of the blade 1 is D3, and D3 is (D1+ D2)/2.
When the blade 1 is seen from the cross street surface, the point on the suction surface 14 of the blade 1, which is intersected with the median circle of the blade 1, is the median point of the suction surface 14, and the distance between the median points of the suction surfaces 14 of two adjacent blades 1 is the blade path width t1 of the centrifugal fan; the center line of the blade 1 is the blade profile center line of the blade 1 (also called the chord length of the blade 1), and the length of the center line of the blade 1 is denoted as L. The ratio t1 of the length L of the centre line of the blade 1 to the width of the blade path is the consistency of the blade 1, in general, the greater this value, the greater the resistance to high static pressures and the greater the noise. The number of blades 1 on the impeller 3 can be determined by the satin of the blades 1.
In a preferred embodiment, referring to fig. 2, the length L of the center line of each blade 1 and the width t1 of the blade path of the centrifugal fan satisfy L/t1 (inclusive) 2.0-2.2, that is, the consistency of the blade 1 is 2.0-2.2. Proved by experiments, the centrifugal fan blade channel is not too narrow, the flow can be considered, and the noise is not too large.
In practical use, L/t1 can be 2.1 or 2.15.
In some embodiments, referring to fig. 3 and 4, the centrifugal fan further comprises a volute 2, and the impeller 3 is rotatably disposed inside the volute 2. The molded line of the volute 2 on the cross section perpendicular to the axis of the impeller 3 is a spiral line and comprises a first bending section 22, a second bending section 23, a third bending section 24 and a fourth bending section 25 which are sequentially connected, and the first bending section 22 is connected with a volute tongue 21 of the volute 2; the four sequentially connected arc sections obtained based on the equilateral element method comprise a first reference section 22 ', a second reference section 23', a third reference section and a fourth reference section 25 ', and the first reference section 22' is connected to the volute tongue 21 in a reference manner; the second curved section 23, the third finished section are configured to coincide with the second reference section 23 ', the third reference section and the fourth reference section 25 ', respectively, and the first curved section 22 is configured as a circular arc section having a curvature smaller than that of the first reference section 22 '.
The centrifugal fan volute 2 functions to direct the gas leaving the impeller 3 to the volute 2 outlet and to convert part of the dynamic pressure into static pressure. The structure of the volute 2 is a complex space curved surface body, the molded line of the volute 2 is a spiral line, and because the spiral line structure is complex and difficult to draw, the simplified four-section circular arc is used for approximately replacing the molded line of the volute 2 to form a near Archimedes spiral line. In the present embodiment, the molded line of the scroll casing 2 is generated with reference to four circular arc segments drawn according to the equilateral primitive method.
The four circular arc segments drawn according to the equilateral element method include a first reference segment 22 ', a second reference segment 23', a third reference segment and a fourth reference segment 25 ', and the first reference segment 22' is correspondingly connected to the volute tongue 21. The circumcircle of the base square formed by the circle center of the first reference section 22 ', the circle center of the second reference section 23', the circle center of the third reference section and the circle center of the fourth reference section 25 'is located on the axis of the impeller 3, the radius of the first reference section 22', the radius of the second reference section 23 ', the radius of the third reference section and the radius of the fourth reference section 25' are calculated according to the opening degree of the molded line and are increased in sequence, and the opening degree of the molded line is calculated based on the Archimedes spiral equation.
The second 23, third 24 and fourth 25 curved sections of the profile of the volute 2 are arranged to coincide with the second 23 ', third 25 and fourth reference sections, i.e. the second 23', third 24 and fourth 25 reference sections are respectively the second 23, third 24 and fourth 25 curved sections.
The first bending section 22 of the molded line of the volute 2 is a circular arc section, and the curvature of the first bending section 22 is smaller than that of the first reference section 22 ', at this time, the distance from the connection point of the first bending section 22 and the volute tongue 21 to the outer diameter circle of the impeller 3, that is, the clearance t3 of the volute tongue 21, is greater than the distance from the connection section of the first reference section 22' and the volute tongue 21 to the outer diameter circle of the impeller 3. The bigger the gap of the volute tongue 21 is, the smaller the noise of the centrifugal fan is, and thus, the gap of the volute tongue 21 can be adjusted by flexibly setting the curvature of the first bending section 22 so as to adjust the noise of the centrifugal fan.
When actually drawing the first bending section 22, in order to make the curvature of the first bending section 22 larger than that of the first reference section 22 ', the center of the first bending section 22 is located on the side of the center of the first reference section 22' far away from the volute tongue 21 and located in the area divided by the third reference section.
It will be appreciated that the outlet side of the volute 2 is also provided with a flare to which the fourth curved section 25 is connected.
In fig. 3, the center of the first reference segment 22 ' is a1, the center of the second reference segment 23 ' is a2, the center of the third reference segment is a3, the center of the fourth reference segment 25 ' is a4, and the center of the first curved segment 22 is a 5.
In a preferred embodiment, the distance from the connection point of the first curved section 22 and the volute tongue 21 to the outer diameter circle of the impeller 3 is the volute tongue 21 gap t3, the diameter of the outer diameter circle of the impeller 3 is D2 ', the diameter of the volute tongue 21 gap t3 and the outer diameter circle of the impeller 3 is D2 ', and t3/D2 ' is 0.06-0.07. At this moment, centrifugal fan can reach the effect of compromise high efficiency and low noise.
In practical use, t 3/D2' may be 0.06, 0.065 or 0.07.
It will be appreciated that the diameter D2' of the outer diameter circle of the impeller 3 is equal to the outlet diameter D2 of the vane 1.
In an embodiment, referring to fig. 4, in order to reduce the space occupied by the centrifugal fan so that the centrifugal fan can be placed inside the housing of the electrical apparatus, the volute casing 2 is partially cut away. At this time, the second curved section 23 of the volute 2 includes a first connecting section, a first straight line section 231 and a second connecting section which are connected in sequence, the first connecting section is connected with the first curved section 22, and the second connecting section is connected with the third curved section 24; the second reference arc section 23 'is connected with the first reference arc section 22', and the third reference arc section is connected with the third reference arc section; the first connection section and the second connection section are configured to coincide with the first reference arc section and the third reference arc section, respectively; the maximum perpendicular distance of the first straight line segment 231 to the axis of the impeller 3 is smaller than the maximum perpendicular distance of the second reference segment 23' to the axis of the impeller 3.
At this time, replacing the second reference arc segment with the first straight segment 231 reduces the maximum perpendicular distance of the second curved segment 23 from the axis of the impeller 3, thereby reducing the projection distance and the occupied space of the scroll casing 2 in the corresponding direction.
Further, referring to fig. 3, the fourth curved section 25 of the scroll casing 2 includes a third connecting section, a second straight section 251 and a fourth connecting section which are connected in sequence, the third connecting section connects the third curved section 24; the fourth reference segment 25' comprises a fourth reference arc segment, a fifth reference arc segment and a sixth reference arc segment which are connected in sequence, and the fourth reference arc segment is connected with the third reference segment in a reference manner; the third connecting section and the fourth connecting section are configured to coincide with the fourth reference arc section and the sixth reference section, respectively; the maximum vertical distance of the fifth reference section to the axis of the impeller 3 is greater than the maximum vertical distance of the second straight section 251 to the axis of the impeller 3.
At this time, the fifth reference arc segment is replaced by the second straight line segment 251, the maximum vertical distance of the fourth curved segment 25 from the axis of the impeller 3 is reduced, so that the projection distance and the occupied space of the volute 2 in the corresponding direction are reduced, and the volume of the volute 2 is further reduced.
It will be appreciated that the sixth reference arc segment is connected to the flare and the fourth connection segment is connected to the flare.
In an embodiment, referring to fig. 4, the first straight line segment 231 and the second straight line segment 251 are both parallel to a tangent of an outer diameter circle of the impeller 3, a distance from a connection point of the first curved segment 22 and the first connection segment to the outer diameter circle of the impeller 3 is a first distance t7, a distance from the first straight line segment 231 to the outer diameter circle of the impeller 3 is a second distance t6, a distance from a connection point of the third curved segment 24 and the third connection segment to the outer diameter circle of the impeller 3 is a third distance t5, and a distance from the second straight line segment 251 to the outer diameter circle of the impeller 3 is a fourth distance t4, which satisfies: t6/t7>0.85, and t4/t5> 0.9. In order to ensure that the air quantity and noise of the volute 2 are not greatly influenced after the volume of the volute 2 is reduced.
In practical use, t6/t7 can be 0.9, 0.95, 1.0, 1.1 and the like, and t4/t5 can be 0.9, 0.95, 1.0, 1.05, 1.1, 1.2 and the like.
Optionally, referring to fig. 3 and 4, the first straight line segment 231 and the second straight line segment 251 are parallel to each other, so that the space occupied by the volute 2 can be maximally reduced on the premise that the air volume and the noise of the volute 2 are not greatly influenced.
When designing a centrifugal fan, the flow rate, the efficiency and the noise determine the performance of the fan, however, the parameters are mutually exclusive. The centrifugal fan provided by the embodiment of the utility model can reasonably optimize various fan performance parameters by optimizing the structural parameters of the blade 1 and the volute 2, so that the centrifugal fan can achieve the effects of large flow, high efficiency and low noise; meanwhile, the thickness of the tail edge 12 of the blade 1 is thickened, so that the injection molding of the blade 1 is facilitated, and the mass production of the blade 1 is facilitated.
Additionally, the utility model provides an embodiment still provides an electrical equipment, and this electrical equipment includes the centrifugal fan that provides as in the above-mentioned embodiment. Because this electrical equipment has included above-mentioned centrifugal fan, consequently all beneficial effects of the above-mentioned centrifugal fan of this electrical equipment, do not give unnecessary details here.
Optionally, the electrical device is a fresh air ventilator. Of course, the electrical equipment may also be other equipment such as a dehumidifier, an air conditioner, an air conditioning fan, etc.
The technical features of the embodiments described above may be arbitrarily combined, and for the sake of brevity, all possible combinations of the technical features in the embodiments described above are not described, but should be considered as being within the scope of the present specification as long as there is no contradiction between the combinations of the technical features.
The above-mentioned embodiments only represent some embodiments of the present invention, and the description thereof is specific and detailed, but not to be construed as limiting the scope of the present invention. It should be noted that, for those skilled in the art, without departing from the spirit of the present invention, several variations and modifications can be made, which are within the scope of the present invention. Therefore, the protection scope of the present invention should be subject to the appended claims.
Claims (10)
1. A vane characterized in that the thickness of the vane gradually increases and then gradually decreases from one end of the trailing edge of the vane to one end of the leading edge of the vane, the thickness of the trailing edge of the vane being greater than 1.5 mm;
the pressure surface of the blade and the suction surface of the blade are both arc surfaces, the pressure surface is concave towards the suction surface, the suction surface is convex away from the pressure surface, and the pressure surface is an arc surface.
2. A centrifugal fan comprising an impeller and a plurality of blades as defined in claim 1 provided on said impeller, said plurality of blades being uniformly arranged circumferentially along an axis of said impeller, and a trailing edge of each of said blades being located on an outer diameter circle of said impeller.
3. The centrifugal fan as claimed in claim 2, wherein the diameter of the co-tangent circle of the leading edges of the plurality of blades is a blade inlet diameter D1, and the diameter of the co-tangent circle of the trailing edges of the plurality of blades is a blade outlet diameter D2;
the vane inlet diameter D1 and the vane outlet diameter D2 satisfy: D1/D2 is 0.8-0.82.
4. The centrifugal fan as claimed in claim 3, wherein the length L of the center line of each blade and the width t1 of the centrifugal fan satisfy: l/t1 is 2.0-2.2.
5. The centrifugal fan according to any one of claims 2-4, further comprising a volute, the impeller being rotatably disposed inside the volute;
the molded line of the volute is a spiral line and comprises a first bending section, a second bending section, a third bending section and a fourth bending section which are connected in sequence, and the first bending section is connected with a volute tongue of the volute;
the four sequentially connected arc sections obtained based on an equilateral element method comprise a first reference section, a second reference section, a third reference section and a fourth reference section, wherein the first reference section is connected with the volute tongue in a reference manner;
the second, third, and fourth curved segments are configured to coincide with the second, third, and fourth reference segments, respectively, and the first curved segment is configured as a circular arc segment having a curvature less than a curvature of the first reference segment.
6. The centrifugal fan as claimed in claim 5, wherein a distance from a connection point of the first curved section and the volute tongue to an outer diameter circle of the impeller is a volute tongue gap t3, and a diameter of the outer diameter circle of the impeller is D2', and the following are satisfied: t 3/D2' is 0.06-0.07.
7. The centrifugal fan as claimed in claim 6, wherein the second curved section comprises a first connecting section, a first straight section and a second connecting section which are connected in sequence, the first connecting section is connected with the first curved section, and the second connecting section is connected with the third curved section;
the second reference segment comprises a first reference arc segment, a second reference arc segment and a third reference arc segment which are sequentially connected, the first reference arc segment is connected with the first reference segment, and the third reference arc segment is connected with the third reference segment;
the first and second connection segments are configured to coincide with the first and third reference arc segments, respectively;
the maximum vertical distance from the first straight line segment to the axis of the impeller is smaller than the maximum vertical distance from the second reference segment to the axis of the impeller.
8. The centrifugal fan of claim 7, wherein the fourth curved section comprises a third connecting section, a second straight section and a fourth connecting section connected in sequence, the third connecting section connecting the third curved section;
the fourth reference segment comprises a fourth reference arc segment, a fifth reference arc segment and a sixth reference arc segment which are connected in sequence, and the fourth reference arc segment is connected to the third reference segment in a reference manner;
the third and fourth connection segments are configured to coincide with the fourth and sixth reference arc segments, respectively;
the maximum vertical distance from the fifth reference section to the axis of the impeller is greater than the maximum vertical distance from the second straight section to the axis of the impeller.
9. The centrifugal fan as claimed in claim 8, wherein the first straight line segment and the second straight line segment are both parallel to a tangent of an outer diameter circle of the impeller, a distance from a connection point of the first curved segment and the first connection segment to the outer diameter circle of the impeller is a first distance t7, a distance from the first straight line segment to the outer diameter circle of the impeller is a second distance t6, a distance from a connection point of the third curved segment and the third connection segment to the outer diameter circle of the impeller is a third distance t5, and a distance from the second straight line segment to the outer diameter circle of the impeller is a fourth distance t4, such that:
t6/t7>0.85, and t4/t5> 0.9.
10. Electrical apparatus, characterized in that it comprises a centrifugal fan according to any one of claims 2 to 9.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022291754.0U CN213039523U (en) | 2020-10-14 | 2020-10-14 | Blade, centrifugal fan and electrical equipment |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022291754.0U CN213039523U (en) | 2020-10-14 | 2020-10-14 | Blade, centrifugal fan and electrical equipment |
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| Publication Number | Publication Date |
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| CN213039523U true CN213039523U (en) | 2021-04-23 |
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|---|---|---|---|
| CN202022291754.0U Active CN213039523U (en) | 2020-10-14 | 2020-10-14 | Blade, centrifugal fan and electrical equipment |
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| CN (1) | CN213039523U (en) |
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