WO2023045004A1 - Motor fan impeller - Google Patents

Motor fan impeller Download PDF

Info

Publication number
WO2023045004A1
WO2023045004A1 PCT/CN2021/125172 CN2021125172W WO2023045004A1 WO 2023045004 A1 WO2023045004 A1 WO 2023045004A1 CN 2021125172 W CN2021125172 W CN 2021125172W WO 2023045004 A1 WO2023045004 A1 WO 2023045004A1
Authority
WO
WIPO (PCT)
Prior art keywords
plane
outlet
front cover
symmetry
fan impeller
Prior art date
Application number
PCT/CN2021/125172
Other languages
French (fr)
Chinese (zh)
Inventor
崔可
王韬
郑国丽
周茜茜
何维林
Original Assignee
中车株洲电机有限公司
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 中车株洲电机有限公司 filed Critical 中车株洲电机有限公司
Publication of WO2023045004A1 publication Critical patent/WO2023045004A1/en

Links

Images

Classifications

    • 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
    • F04D29/281Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for fans or blowers
    • 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
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K9/00Arrangements for cooling or ventilating
    • H02K9/02Arrangements for cooling or ventilating by ambient air flowing through the machine
    • H02K9/04Arrangements for cooling or ventilating by ambient air flowing through the machine having means for generating a flow of cooling medium
    • H02K9/06Arrangements for cooling or ventilating by ambient air flowing through the machine having means for generating a flow of cooling medium with fans or impellers driven by the machine shaft

Definitions

  • the invention relates to the technical field of motors, in particular to a motor fan impeller.
  • Self-ventilated double-rotating motors usually use a self-ventilating fan that rotates coaxially with the motor to drive the air flow in the frame to enhance the convective heat dissipation effect between the air in the frame and the stator and rotor of the motor, and improve the overall cooling efficiency of the motor.
  • Self-ventilating fans usually have the airflow characteristics of axial air inlet and radial air outlet, mainly relying on the work of fan blades and centrifugal force to achieve the purpose of boosting air and driving air flow, so this kind of fan is a centrifugal fan.
  • a type of fan is mainly relying on the work of fan blades and centrifugal force to achieve the purpose of boosting air and driving air flow.
  • the installation angle of the self-ventilating double-rotation motor centrifugal fan blade is zero, which is to ensure that the ventilation effect of the fan is exactly the same as the motor rotates forward and reverse. Due to the installation angle of zero, the fan blades have a significantly weaker pressurization capacity than a one-way rotating centrifugal fan.
  • the radial arrangement of the fan blades makes the shape of the end surface of the fan flow channel have the obvious characteristics of narrow air inlet and wide air outlet as shown in Figure 1, and the gas flow channel gradually widens from the inlet to the outlet at a constant speed , This also causes the wall adhesion between the gas and the blades to gradually deteriorate with the airflow movement, and a relatively obvious airflow separation and outlet recirculation area will generally be formed near the outlet, causing the outlet to be blocked and affecting the fan's flow efficiency.
  • the object of the present invention is to provide a motor fan impeller with high fan flow efficiency.
  • the present invention provides the following technical solutions:
  • a motor fan impeller comprising a front cover plate and a rear cover plate arranged in sequence along the axial direction, a hub is fixedly arranged between the front cover plate and the rear cover plate, and a plurality of Blades; the center of the front cover is provided with an air inlet, and an air outlet channel is formed between adjacent blades, so that the wind can enter in the axial direction through the air inlet, and then flow out radially through the air outlet channel ;
  • the blades sequentially include an inlet structure and an outlet structure
  • the inlet structure is a plane symmetric structure, and the symmetry plane is the plane where the rotation center line of the hub is located;
  • the outlet structure at least part of the circumferential end surface is a deformed surface, and along the airflow direction, the deformed surface gradually deviates from the corresponding plane of symmetry, wherein the outlet structure is the same as that of the inlet structure in the same blade.
  • the plane of symmetry corresponds.
  • two circumferential end surfaces of the outlet structure are respectively located on two sides of the corresponding plane of symmetry.
  • the two circumferential end faces of the outlet structure are plane-symmetric with respect to the corresponding plane of symmetry.
  • all the blade structures are identical and arranged evenly.
  • the deformation surface is parallel to the axial direction.
  • the distance between the two adjacent inlet structures in the circumferential direction of the air outlet channel gradually increases, and the partial distance between the two adjacent outlet structures in the circumferential direction gradually decreases.
  • the outlet structure includes two tail plates arranged in sequence along the circumferential direction, and the two tail plates are respectively arranged on both sides of the corresponding symmetrical plane, and the deformation surface is arranged on the The tail plate is far away from the circumferential end surface of the other tail plate; along the airflow direction, the two tail plates swing in directions gradually away from the corresponding plane of symmetry, so that the outlet structure forms a bifurcated structure .
  • the outlet structure is a solid plate-like structure.
  • the deformation surface gradually deviates from the corresponding plane of symmetry.
  • the outlet structure in a direction perpendicular to the front cover plate and away from the front cover plate, includes at least two sub-plates in turn; each of the sub-plates gradually moves away from the corresponding plane of symmetry along the airflow direction swing in the same direction, and the adjacent sub-plates in the outlet structure are respectively located on both sides of the corresponding symmetry plane; the deformation surface is provided on the circumferential end surface of the sub-plate away from the corresponding symmetry plane superior.
  • the motor fan impeller provided by the present invention includes a front cover and a rear cover arranged in sequence in the axial direction, a hub is fixedly arranged between the front cover and the rear cover, and a plurality of blades are fixed in turn on the hub along the circumferential direction.
  • An air inlet is arranged in the center of the front cover, and an air outlet channel is formed between adjacent blades, so that the wind can enter in the axial direction through the air inlet, and then flow out in the radial direction through the air outlet channel.
  • the blade comprises in turn an inlet structure and an outlet structure.
  • the inlet structure is a plane symmetrical structure, and the symmetrical plane is the plane where the rotation centerline of the hub is located.
  • the outlet structure at least part of the circumferential end surface is a deformed surface, and along the airflow direction, the deformed surface gradually deviates from the corresponding symmetry plane, wherein the outlet structure corresponds to the symmetry plane of the inlet structure in the same blade.
  • each deformed surface can slow down the circumferential expansion trend of the airflow channel, and can weaken the wall shedding of the airflow at the fan outlet to a certain extent Phenomenon and outlet backflow phenomenon, thereby improving the working ability of the fan and the convection heat dissipation efficiency in the motor frame, and improving the fan flow efficiency.
  • the inlet structure is a plane symmetrical structure, the impact on the bidirectional rotation capability of the impeller can be reduced.
  • Fig. 1 is a schematic diagram of the traditional fan backflow phenomenon in the prior art, X is the rotation direction of the fan, C is the forward airflow, and D is the reverse airflow;
  • Fig. 2 is a schematic diagram of the suppression of the backflow phenomenon by the bifurcated blades in the impeller in Embodiment 1 of the present invention, X is the rotation direction of the fan, and C is the forward airflow;
  • Fig. 3 is an axial view of the impeller in Embodiment 1 of the present invention, and the solid line with arrows indicates the air flow;
  • FIG. 4 is a radial cross-sectional view of the impeller in Embodiment 1 of the present invention, O is the rotation centerline of the hub and the fan, and the arrow on the dotted line indicates the direction perpendicular to the front cover and away from the front cover;
  • Fig. 5 is a structural diagram of blades in the impeller in Embodiment 1 of the present invention.
  • Fig. 6 is a partial structural diagram of the impeller in Embodiment 1 of the present invention.
  • Fig. 7 is a partial structural diagram of the impeller in the second embodiment of the present invention.
  • Fig. 8 is an axial view of the impeller in the second embodiment of the present invention.
  • Fig. 9 is a partial structural view of the impeller in Embodiment 3 of the present invention.
  • Fig. 10 is an axial view of the impeller in Embodiment 3 of the present invention.
  • Fig. 11 is a partial structural diagram of the impeller in Embodiment 4 of the present invention.
  • Fig. 12 is an axial view of the impeller in Embodiment 4 of the present invention.
  • Fig. 13 is a structural diagram of the blades of the impeller in Embodiment 5 of the present invention.
  • Outlet structure 2 deformation surface 21, tail plate 22, sub-plate 23, circumferential end surface 24 of the outlet structure;
  • Blade 3 air outlet channel 31, air inlet side 32, air outlet side 33;
  • Front cover 4 air inlet 41;
  • the core of the present invention is to provide a motor fan impeller with high fan flow efficiency.
  • the first specific embodiment of the motor fan impeller provided by the present invention is used in the field of cooling power components of bidirectional motors in electrical equipment, please refer to Figures 2 to 6, including a front cover 4 and a rear cover 6 arranged in sequence along the axial direction .
  • a wheel hub 5 is fixedly arranged between the front cover plate 4 and the rear cover plate 6, and the rear cover plate 6 and the wheel hub 5 are generally integrated.
  • a plurality of blades 3 are fixedly arranged in turn on the hub 5 along the circumferential direction, and the main function of the blades 3 is to perform work on the airflow to increase the total pressure of the airflow.
  • the front cover plate 4 and the rear cover plate 6 mainly play the role of guiding the flow and supporting the blades 3, and the center of the front cover plate 4 is provided with an air inlet 41 , and an air outlet channel 31 is formed between adjacent blades 3, so that the wind can enter in the axial direction through the air inlet 41 as shown in FIG.
  • the airflow direction Q refers to the direction of the airflow following its flow.
  • the blade 3 comprises an inlet structure 1 and an outlet structure 2 in sequence.
  • the inlet structure 1 is a plane symmetrical structure, and the symmetrical plane S is the plane where the rotation center line of the hub 5 is located.
  • the inlet structure 1 is a straight plate structure, and its two circumferential end surfaces are planes parallel to the symmetry plane S, and may also be other shapes with unequal thickness.
  • the outlet structure 2 At least part of the circumferential end surface is a deformed surface 21 , and along the airflow direction Q, the deformed surface 21 gradually deviates from the symmetry plane S corresponding to the inlet structure 1 in the same blade 3 .
  • both ends of the outlet structure 2 in the circumferential direction are circumferential end faces.
  • deformation surfaces 21 are provided on both circumferential end faces.
  • the outlet structure 2 extends from the middle of the blade 3 to the tail end of the blade 3 , the starting position of the outlet structure 2 can be set according to actual needs, and the tail end is the tail end of the blade 3 .
  • the outlet structure 2 , the inlet structure 1 and the symmetry plane S of the inlet structure 1 on the same blade 3 have a corresponding relationship.
  • the air flow enters from the air inlet 41, first flows in the axial direction, and gradually changes to flow in the radial direction. When passing through the blade 3, it first adheres to the circumferential direction of the inlet structure 1 of the blade 3.
  • each deformed surface 21 can slow down
  • the circumferential expansion trend of the airflow channel as shown in the deformation surface A in Figure 2, can slow down its expansion trend on the right side of the left airflow channel, and can weaken the wall shedding phenomenon and outlet backflow of the airflow at the fan outlet to a certain extent phenomenon, thereby improving the working ability of the fan and the convection heat dissipation efficiency in the motor frame.
  • the inlet structure 1 is a plane symmetrical structure, it can reduce the influence on the two-way rotation ability of the impeller.
  • the two circumferential end surfaces 24 of the outlet structure 2 are located on both sides of the corresponding symmetry plane S, which can improve the structural consistency of the two circumferential end surfaces 24 of the outlet structure 2 and improve the bidirectional rotation capability of the impeller. More preferably, as shown in FIG. 5 , the two circumferential end surfaces 24 of the outlet structure 2 are planarly symmetrical with respect to the symmetry plane S, so as to further ensure that the working performance of the impeller is exactly the same when it is forward and reverse.
  • the deformation surface 21 is parallel to the axial direction, more specifically, it is arranged on a plane parallel to the axial direction, which is convenient for processing.
  • the spacing between the two circumferentially adjacent inlet structures 1 of the air outlet channel 31 gradually increases, and the partial spacing between the circumferentially adjacent two outlet structures 2 Gradual reduction, so that along the airflow direction Q, the circumferential width of the air outlet channel 31 gradually expands and then tapers, which can further avoid the phenomenon of backflow.
  • the partial spacing between two adjacent outlet structures 2 in the circumferential direction can also be gradually increased, but the increase speed is slower than that between two adjacent outlet structures 2 of the air outlet channel 31 in the circumferential direction. The speed at which the spacing between the inlet structures 1 increases.
  • all blades 3 have identical structures and are evenly arranged, which can ensure the working capacity of the impeller and facilitate processing.
  • the outlet structure 2 includes two tail plates 22 sequentially arranged along the circumferential direction, and the two tail plates 22 are respectively arranged on both sides of the corresponding plane S of symmetry.
  • the tail plate 22 may be a straight plate of equal thickness, or may adopt a plate of unequal thickness or a non-straight plate structure.
  • each tail plate 22 its deformation surface 21 is arranged on the circumferential end surface of the tail plate 22 away from the other tail plate 22 in the same outlet structure 2, that is to say, in the outlet structure 2, each tail plate 22 is far away from the other tail plate 22.
  • the circumferential end surface of a tail plate 22 is the circumferential end surface 24 of the outlet structure 2 .
  • the entire circumferential end surface of the outlet structure 2 is the deformation surface 21 .
  • the two tailgates 22 swing in directions gradually away from the corresponding symmetry plane S, so that the outlet structure 2 forms a bifurcated structure. Due to the setting of the bifurcated structure, the outlet structure 2 can have a deformed surface. 21 simultaneously, reduce blade 3 weights.
  • the bifurcation angle between the two tail plates 22 ranges from 0° to 180°.
  • the inlet side 32 and the outlet side 33 are straight or non-linear. In the airflow direction Q, the inlet side 32 is specifically the starting side of the inlet structure 1 , and the outlet side 33 is the trailing side of the outlet structure 2 .
  • the angle ⁇ between the air inlet side 32 and the rotation center line O of the impeller ranges from 0° to 180°, and the angle between the air outlet side 33 and the rotation center line O ranges from 0° to 90°.
  • the impeller of the self-ventilating centrifugal fan of the double-rotating motor with circumferentially bifurcated blades provided in this embodiment, based on the setting of the outlet structure 2, can solve the problem of serious backflow at the outlet of the self-ventilating fan of the traditional double-rotating motor and relatively high secondary flow loss.
  • the symmetrical structure of the blade 3 it can meet the requirements of forward and reverse rotation.
  • the work ability of forward and reverse airflow is consistent Compared with the existing self-ventilating fan, the flow rate and efficiency are higher, and the aerodynamic performance is better.
  • the outlet structure 2 is not limited to be the bifurcated structure in the first embodiment.
  • the outlet structure 2 is a solid plate structure, which is convenient for processing.
  • the deformed surface 21 is not limited to be arranged parallel to the axial direction, and the entire circumferential end surface may not be provided as the deformed surface 21 .
  • the deformation surface 21 gradually deviates from the corresponding symmetry plane S.
  • the direction perpendicular to the front cover plate 4 is consistent everywhere on the airflow direction Q; In different positions, the direction perpendicular to the front cover 4 is specifically the direction perpendicular to the tangent plane of each point of the front cover 4 .
  • the deformed surface 21 of the outlet structure 2 a part of the surface of the circumferential end surface of the outlet structure 2 is the deformed surface 21, which is shown in FIG.
  • These two directions both have a gradual change trend, which can partially improve the backflow problem of the air outlet channel 31 .
  • the two circumferential end faces of the outlet structure 2 may not be plane-symmetrical with respect to the symmetry plane S.
  • the outlet structure 2 sequentially includes at least two sub-boards 23 .
  • Each sub-plate 23 swings along the airflow direction Q toward a direction gradually away from the corresponding symmetry plane S, and adjacent sub-plates 23 in the outlet structure 2 are located on both sides of the corresponding symmetry plane S, respectively.
  • the deformation surface 21 is provided on the circumferential end surface of the sub-plate 23 away from the symmetry plane S.
  • two sub-boards 23 are provided, and in other embodiments, three sub-boards 23 may also be provided or other numbers.
  • each sub-plate 23 can reduce the backflow phenomenon in one of the rotation directions of the impeller.
  • the deformation surface 21 may be provided on only one of the two circumferential end surfaces 24 of the outlet structure 2 .
  • the left circumferential end surface of the outlet structure 2 is a deformation surface 21, and the right circumferential end surface is a surface parallel to the corresponding symmetry plane S, not It has a gradual tendency and is not a deformed surface 21.

Abstract

A motor fan impeller, comprising a front cover plate (4) and a rear cover plate (6) arranged in sequence along an axial direction, wherein a hub (5) is fixedly arranged between the front cover plate (4) and the rear cover plate (6), and a plurality of blades (3) are fixedly arranged on the hub (5) in sequence along a circumferential direction. An air inlet (41) is arranged at the center of the front cover plate (4), and an air outlet channel (31) is formed between adjacent blades (3), so that wind may enter along the axial direction via the air inlet (41), and then flow out radially by means of the air outlet channel (31). In an airflow direction, each blade (3) sequentially comprises an inlet structure (1) and an outlet structure (2). The inlet structure (1) is a plane symmetrical structure, and a symmetrical plane (S) is a plane where the rotational center line of the hub (5) is located. In the outlet structure (2), at least part of a circumferential end surface is a deforming surface (21), and along the airflow direction (Q), the deforming surface (21) gradually deviates from the corresponding symmetrical plane (S). Since the deforming surface (21) is provided on the outlet structure (2), compared to straight blades in the prior art, the circumferential expansion trend of an airflow channel may be mitigated, and the flow efficiency of the fan may be increased.

Description

一种电机风扇叶轮A motor fan impeller
本申请要求于2021年9月26日提交中国专利局、申请号为202111128299.5、发明名称为“一种电机风扇叶轮”的中国专利申请的优先权,其全部内容通过引用结合在本申请中。This application claims the priority of the Chinese patent application with the application number 202111128299.5 and the title of the invention "A Motor Fan Impeller" submitted to the China Patent Office on September 26, 2021, the entire contents of which are incorporated in this application by reference.
技术领域technical field
本发明涉及电机技术领域,特别涉及一种电机风扇叶轮。The invention relates to the technical field of motors, in particular to a motor fan impeller.
背景技术Background technique
自通风型双旋向电机通常采用与电机同轴旋转的自通风风扇来驱动机座内空气流动,以增强机座内空气与电机定转子间的对流散热效果、提升电机整体的冷却效率。自通风风扇通常具有轴向进风、径向出风的气流特点,主要借助于风扇叶片做功以及离心力的作用来达到使空气增压进而达到驱动空气流动的目的,因此这种风扇这是属于离心风扇的一种。Self-ventilated double-rotating motors usually use a self-ventilating fan that rotates coaxially with the motor to drive the air flow in the frame to enhance the convective heat dissipation effect between the air in the frame and the stator and rotor of the motor, and improve the overall cooling efficiency of the motor. Self-ventilating fans usually have the airflow characteristics of axial air inlet and radial air outlet, mainly relying on the work of fan blades and centrifugal force to achieve the purpose of boosting air and driving air flow, so this kind of fan is a centrifugal fan. A type of fan.
与传统离心风扇所不同的是,自通风型双旋向电机离心风扇叶片安装角为零,这是为了保证风扇随电机正反转是通风效果完全一样。由于安装角为零,风扇叶片对气流的增压能力显著弱于单向旋转的离心风扇。同时,风扇叶片的放射状布置,使得风扇流道端面形状具有明显的如图1所示的进气口窄、出气口宽、且气体流道由进口向出口逐渐以不变的速度加宽的特点,这样因此也造成气体与叶片的附壁性随气流运动逐渐变差,出口附近一般会形成比较明显的气流分离和出口回流区,造成出口堵塞,影响风扇通流效率。Different from the traditional centrifugal fan, the installation angle of the self-ventilating double-rotation motor centrifugal fan blade is zero, which is to ensure that the ventilation effect of the fan is exactly the same as the motor rotates forward and reverse. Due to the installation angle of zero, the fan blades have a significantly weaker pressurization capacity than a one-way rotating centrifugal fan. At the same time, the radial arrangement of the fan blades makes the shape of the end surface of the fan flow channel have the obvious characteristics of narrow air inlet and wide air outlet as shown in Figure 1, and the gas flow channel gradually widens from the inlet to the outlet at a constant speed , This also causes the wall adhesion between the gas and the blades to gradually deteriorate with the airflow movement, and a relatively obvious airflow separation and outlet recirculation area will generally be formed near the outlet, causing the outlet to be blocked and affecting the fan's flow efficiency.
因此,如何提高风扇通流效率,是本领域技术人员目前需要解决的技术问题。Therefore, how to improve the ventilation efficiency of the fan is a technical problem to be solved by those skilled in the art.
发明内容Contents of the invention
有鉴于此,本发明的目的是提供一种电机风扇叶轮,其风扇通流效率较高。In view of this, the object of the present invention is to provide a motor fan impeller with high fan flow efficiency.
为实现上述目的,本发明提供如下技术方案:To achieve the above object, the present invention provides the following technical solutions:
一种电机风扇叶轮,包括沿轴向依次设置的前盖板和后盖板,所述前盖板和所述后盖板之间固定设置轮毂,所述轮毂上沿周向依次固定设置多个叶片;所述前盖板的中心设置进风口,相邻所述叶片之间形成出风通道,以使风能够经所述进风口沿轴向进入,再通过所述出风通道沿径向流出;A motor fan impeller, comprising a front cover plate and a rear cover plate arranged in sequence along the axial direction, a hub is fixedly arranged between the front cover plate and the rear cover plate, and a plurality of Blades; the center of the front cover is provided with an air inlet, and an air outlet channel is formed between adjacent blades, so that the wind can enter in the axial direction through the air inlet, and then flow out radially through the air outlet channel ;
在气流方向上,所述叶片依次包括入口结构和出口结构;In the airflow direction, the blades sequentially include an inlet structure and an outlet structure;
所述入口结构为平面对称结构,且对称平面为所述轮毂的旋转中心线所在的平面;The inlet structure is a plane symmetric structure, and the symmetry plane is the plane where the rotation center line of the hub is located;
所述出口结构中,至少部分周向端面为变形面,沿着气流方向,所述变形面逐渐偏离对应的所述对称平面,其中,所述出口结构与同一所述叶片中所述入口结构的所述对称平面相对应。In the outlet structure, at least part of the circumferential end surface is a deformed surface, and along the airflow direction, the deformed surface gradually deviates from the corresponding plane of symmetry, wherein the outlet structure is the same as that of the inlet structure in the same blade. The plane of symmetry corresponds.
优选地,所述出口结构的两个周向端面分别位于对应的所述对称平面的两侧。Preferably, two circumferential end surfaces of the outlet structure are respectively located on two sides of the corresponding plane of symmetry.
优选地,所述出口结构的两个周向端面相对于对应的所述对称平面呈平面对称。Preferably, the two circumferential end faces of the outlet structure are plane-symmetric with respect to the corresponding plane of symmetry.
优选地,所有所述叶片结构完全相同且均匀排布。Preferably, all the blade structures are identical and arranged evenly.
优选地,所述变形面平行于轴向。Preferably, the deformation surface is parallel to the axial direction.
优选地,沿着气流方向,所述出风通道在周向相邻的两个所述入口结构之间的间距逐渐增加,且在在周向相邻的两个所述出口结构之间的部分间距逐渐减小。Preferably, along the airflow direction, the distance between the two adjacent inlet structures in the circumferential direction of the air outlet channel gradually increases, and the partial distance between the two adjacent outlet structures in the circumferential direction gradually decreases. .
优选地,所述出口结构中,包括沿着周向依次设置的两个尾板,且两个所述尾板分别设于对应的所述对称平面的两侧,所述变形面设于所述尾板远离另一所述尾板的周向端面上;沿着气流方向,两个所述尾板分别朝向逐渐远离对应的所述对称平面的方向摆动,以使所述出口结构形成分叉结构。Preferably, the outlet structure includes two tail plates arranged in sequence along the circumferential direction, and the two tail plates are respectively arranged on both sides of the corresponding symmetrical plane, and the deformation surface is arranged on the The tail plate is far away from the circumferential end surface of the other tail plate; along the airflow direction, the two tail plates swing in directions gradually away from the corresponding plane of symmetry, so that the outlet structure forms a bifurcated structure .
优选地,所述出口结构为实心的板状结构。Preferably, the outlet structure is a solid plate-like structure.
优选地,在垂直于所述前盖板且远离所述前盖板的方向上,所述变形面逐渐偏离对应的所述对称平面。Preferably, in a direction perpendicular to the front cover and away from the front cover, the deformation surface gradually deviates from the corresponding plane of symmetry.
优选地,在垂直于所述前盖板且远离所述前盖板的方向上,所述出口 结构依次包括至少两个分板;各所述分板沿着气流方向朝向逐渐远离对应的对称平面的方向摆动,且所述出口结构中相邻所述分板分别位于对应的所述对称平面的两侧;所述变形面设于所述分板上远离对应的所述对称平面的周向端面上。Preferably, in a direction perpendicular to the front cover plate and away from the front cover plate, the outlet structure includes at least two sub-plates in turn; each of the sub-plates gradually moves away from the corresponding plane of symmetry along the airflow direction swing in the same direction, and the adjacent sub-plates in the outlet structure are respectively located on both sides of the corresponding symmetry plane; the deformation surface is provided on the circumferential end surface of the sub-plate away from the corresponding symmetry plane superior.
本发明提供的电机风扇叶轮,包括沿轴向依次设置的前盖板和后盖板,前盖板和后盖板之间固定设置轮毂,轮毂上沿周向依次固定设置多个叶片。前盖板的中心设置进风口,相邻叶片之间形成出风通道,以使风能够经进风口沿轴向进入,再通过出风通道沿径向流出。在气流方向上,叶片依次包括入口结构和出口结构。入口结构为平面对称结构,且对称平面为轮毂的旋转中心线所在的平面。出口结构中,至少部分周向端面为变形面,沿着气流方向,变形面逐渐偏离对应的对称平面,其中,出口结构与同一叶片中入口结构的对称平面相对应。The motor fan impeller provided by the present invention includes a front cover and a rear cover arranged in sequence in the axial direction, a hub is fixedly arranged between the front cover and the rear cover, and a plurality of blades are fixed in turn on the hub along the circumferential direction. An air inlet is arranged in the center of the front cover, and an air outlet channel is formed between adjacent blades, so that the wind can enter in the axial direction through the air inlet, and then flow out in the radial direction through the air outlet channel. In the direction of the airflow, the blade comprises in turn an inlet structure and an outlet structure. The inlet structure is a plane symmetrical structure, and the symmetrical plane is the plane where the rotation centerline of the hub is located. In the outlet structure, at least part of the circumferential end surface is a deformed surface, and along the airflow direction, the deformed surface gradually deviates from the corresponding symmetry plane, wherein the outlet structure corresponds to the symmetry plane of the inlet structure in the same blade.
气流从进风口进入,先轴向流动,逐渐变为沿径向流动,在流经叶片时,先贴着叶片的入口结构的周向端面流动,再贴着叶片的出口结构的周向端面流动,其中,由于出口结构上设置变形面,相比于现有技术平直的叶片,每个变形面可以减缓气流通道的周向扩张趋势,能够在一定程度上减弱气流在风扇出口处的壁面脱落现象和出口回流现象,从而提高风扇的做功能力和电机机座内的对流散热效率,提高风扇通流效率。另外,由于入口结构为平面对称结构,能够降低对叶轮的双向旋转能力的影响。The air flow enters from the air inlet, first flows axially, and gradually changes to radial flow. When passing through the blade, it first flows against the circumferential end surface of the inlet structure of the blade, and then flows close to the circumferential end surface of the outlet structure of the blade. , wherein, since the outlet structure is provided with deformed surfaces, compared with the prior art straight blades, each deformed surface can slow down the circumferential expansion trend of the airflow channel, and can weaken the wall shedding of the airflow at the fan outlet to a certain extent Phenomenon and outlet backflow phenomenon, thereby improving the working ability of the fan and the convection heat dissipation efficiency in the motor frame, and improving the fan flow efficiency. In addition, since the inlet structure is a plane symmetrical structure, the impact on the bidirectional rotation capability of the impeller can be reduced.
附图说明Description of drawings
为了更清楚地说明本发明实施例或现有技术中的技术方案,下面将对实施例或现有技术描述中所需要使用的附图作简单地介绍,显而易见地,下面描述中的附图仅仅是本发明的实施例,对于本领域普通技术人员来讲,在不付出创造性劳动的前提下,还可以根据提供的附图获得其他的附图。In order to more clearly illustrate the technical solutions in the embodiments of the present invention or the prior art, the following will briefly introduce the drawings that need to be used in the description of the embodiments or the prior art. Obviously, the accompanying drawings in the following description are only It is an embodiment of the present invention, and those skilled in the art can also obtain other drawings according to the provided drawings without creative work.
图1为现有技术中传统风扇回流现象示意图,X为风扇旋向,C为顺向气流,D为逆向气流;Fig. 1 is a schematic diagram of the traditional fan backflow phenomenon in the prior art, X is the rotation direction of the fan, C is the forward airflow, and D is the reverse airflow;
图2为本发明具体实施例一中叶轮中分叉叶片对回流现象的抑制示意图,X为风扇旋向,C为顺向气流;Fig. 2 is a schematic diagram of the suppression of the backflow phenomenon by the bifurcated blades in the impeller in Embodiment 1 of the present invention, X is the rotation direction of the fan, and C is the forward airflow;
图3为本发明具体实施例一中叶轮的轴向视图,带箭头的实线指示气流;Fig. 3 is an axial view of the impeller in Embodiment 1 of the present invention, and the solid line with arrows indicates the air flow;
图4为本发明具体实施例一中叶轮的径向剖视图,O为轮毂以及风扇的旋转中心线,虚线上的箭头指示垂直于前盖板且远离前盖板的方向;4 is a radial cross-sectional view of the impeller in Embodiment 1 of the present invention, O is the rotation centerline of the hub and the fan, and the arrow on the dotted line indicates the direction perpendicular to the front cover and away from the front cover;
图5为本发明具体实施例一中叶轮中叶片的结构图;Fig. 5 is a structural diagram of blades in the impeller in Embodiment 1 of the present invention;
图6为本发明具体实施例一中叶轮的局部结构图;Fig. 6 is a partial structural diagram of the impeller in Embodiment 1 of the present invention;
图7为本发明具体实施例二中叶轮的局部结构图;Fig. 7 is a partial structural diagram of the impeller in the second embodiment of the present invention;
图8为本发明具体实施例二中叶轮的轴向视图;Fig. 8 is an axial view of the impeller in the second embodiment of the present invention;
图9为本发明具体实施例三中叶轮的局部结构图;Fig. 9 is a partial structural view of the impeller in Embodiment 3 of the present invention;
图10为本发明具体实施例三中叶轮的轴向视图;Fig. 10 is an axial view of the impeller in Embodiment 3 of the present invention;
图11为本发明具体实施例四中叶轮的局部结构图;Fig. 11 is a partial structural diagram of the impeller in Embodiment 4 of the present invention;
图12为本发明具体实施例四中叶轮的轴向视图;Fig. 12 is an axial view of the impeller in Embodiment 4 of the present invention;
图13为本发明具体实施例五中叶轮的叶片的结构图。Fig. 13 is a structural diagram of the blades of the impeller in Embodiment 5 of the present invention.
附图标记:Reference signs:
对称平面S,气流方向Q;Symmetry plane S, airflow direction Q;
入口结构1; Ingress struct 1;
出口结构2,变形面21,尾板22,分板23,出口结构的周向端面24; Outlet structure 2, deformation surface 21, tail plate 22, sub-plate 23, circumferential end surface 24 of the outlet structure;
叶片3,出风通道31,进气边32,出气边33; Blade 3, air outlet channel 31, air inlet side 32, air outlet side 33;
前盖板4,进风口41; Front cover 4, air inlet 41;
轮毂5; hub 5;
后盖板6。 rear cover 6.
具体实施方式Detailed ways
下面将结合本发明实施例中的附图,对本发明实施例中的技术方案进行清楚、完整地描述,显然,所描述的实施例仅仅是本发明一部分实施例,而不是全部的实施例。基于本发明中的实施例,本领域普通技术人员在没有做出创造性劳动前提下所获得的所有其他实施例,都属于本发明保护的范围。The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.
本发明的核心是提供一种电机风扇叶轮,其风扇通流效率较高。The core of the present invention is to provide a motor fan impeller with high fan flow efficiency.
本发明所提供电机风扇叶轮的具体实施例一,用于电气设备双旋向电机冷却动力部件领域,请参考图2至图6,包括沿轴向依次设置的前盖板4和后盖板6。前盖板4和后盖板6之间固定设置轮毂5,后盖板6与轮毂5通常为一体。轮毂5上沿周向依次固定设置多个叶片3,叶片3主要作用是对气流做功,以提高气流总压。前盖板4、后盖板6两者与叶片3之间均不存在间隙,前盖板4、后盖板6主要起导流及支撑叶片3作用,前盖板4的中心设置进风口41,且相邻叶片3之间形成出风通道31,以使风能够如图4所示,经进风口41沿轴向进入,再通过出风通道31沿径向流出。The first specific embodiment of the motor fan impeller provided by the present invention is used in the field of cooling power components of bidirectional motors in electrical equipment, please refer to Figures 2 to 6, including a front cover 4 and a rear cover 6 arranged in sequence along the axial direction . A wheel hub 5 is fixedly arranged between the front cover plate 4 and the rear cover plate 6, and the rear cover plate 6 and the wheel hub 5 are generally integrated. A plurality of blades 3 are fixedly arranged in turn on the hub 5 along the circumferential direction, and the main function of the blades 3 is to perform work on the airflow to increase the total pressure of the airflow. There is no gap between the front cover plate 4 and the rear cover plate 6 and the blades 3, the front cover plate 4 and the rear cover plate 6 mainly play the role of guiding the flow and supporting the blades 3, and the center of the front cover plate 4 is provided with an air inlet 41 , and an air outlet channel 31 is formed between adjacent blades 3, so that the wind can enter in the axial direction through the air inlet 41 as shown in FIG.
对于每个叶片3,气流方向Q指的是贴合其流动的气流的方向。在气流方向Q上,叶片3依次包括入口结构1和出口结构2。For each vane 3 , the airflow direction Q refers to the direction of the airflow following its flow. In the airflow direction Q, the blade 3 comprises an inlet structure 1 and an outlet structure 2 in sequence.
入口结构1为平面对称结构,且对称平面S为轮毂5的旋转中心线所在的平面。具体地,入口结构1为直板形结构,其两个周向端面均为平行于对称平面S的平面,也可以为其他非等厚度的形状。The inlet structure 1 is a plane symmetrical structure, and the symmetrical plane S is the plane where the rotation center line of the hub 5 is located. Specifically, the inlet structure 1 is a straight plate structure, and its two circumferential end surfaces are planes parallel to the symmetry plane S, and may also be other shapes with unequal thickness.
出口结构2中,至少部分周向端面为变形面21,沿着气流方向Q,变形面21逐渐偏离同一叶片3中入口结构1对应的对称平面S。其中,出口结构2在周向上的两端均为周向端面,如图2所示,两个周向端面上均设置变形面21。具体地,沿着气流方向Q,出口结构2由叶片3的中部延伸至叶片3的尾端,出口结构2的起始位置具体可以根据实际需要进行设置,尾端为叶片3的尾端。In the outlet structure 2 , at least part of the circumferential end surface is a deformed surface 21 , and along the airflow direction Q, the deformed surface 21 gradually deviates from the symmetry plane S corresponding to the inlet structure 1 in the same blade 3 . Wherein, both ends of the outlet structure 2 in the circumferential direction are circumferential end faces. As shown in FIG. 2 , deformation surfaces 21 are provided on both circumferential end faces. Specifically, along the airflow direction Q, the outlet structure 2 extends from the middle of the blade 3 to the tail end of the blade 3 , the starting position of the outlet structure 2 can be set according to actual needs, and the tail end is the tail end of the blade 3 .
其中,本申请中,同一个叶片3上的出口结构2、入口结构1和该入口结构1的对称平面S具有对应关系。Wherein, in the present application, the outlet structure 2 , the inlet structure 1 and the symmetry plane S of the inlet structure 1 on the same blade 3 have a corresponding relationship.
本实施例中,如图4所示,气流从进风口41进入,先轴向流动,逐渐变为沿径向流动,在流经叶片3时,先贴着叶片3的入口结构1的周向端面流动,再贴着叶片3的出口结构2的周向端面24流动,其中,由于出口结构2上设置变形面21,相比于现有技术平直的叶片3,每个变形面21可以减缓气流通道的周向扩张趋势,如图2中的变形面A,可以在其左侧气流通道的右侧减缓其扩张趋势,能够在一定程度上减弱气流在风扇出口处的壁面脱落现象和出口回流现象,从而提高风扇的做功能力和电机机座内的对流散热效率。另外,由于入口结构1为平面对称结构,能够降低对 叶轮的双向旋转能力的影响。In this embodiment, as shown in FIG. 4, the air flow enters from the air inlet 41, first flows in the axial direction, and gradually changes to flow in the radial direction. When passing through the blade 3, it first adheres to the circumferential direction of the inlet structure 1 of the blade 3. The end surface flows, and then flows against the circumferential end surface 24 of the outlet structure 2 of the blade 3, wherein, since the outlet structure 2 is provided with a deformed surface 21, compared with the straight blade 3 of the prior art, each deformed surface 21 can slow down The circumferential expansion trend of the airflow channel, as shown in the deformation surface A in Figure 2, can slow down its expansion trend on the right side of the left airflow channel, and can weaken the wall shedding phenomenon and outlet backflow of the airflow at the fan outlet to a certain extent phenomenon, thereby improving the working ability of the fan and the convection heat dissipation efficiency in the motor frame. In addition, since the inlet structure 1 is a plane symmetrical structure, it can reduce the influence on the two-way rotation ability of the impeller.
进一步地,出口结构2的两个周向端面24位于对应的对称平面S的两侧,可以改善出口结构2两个周向端面24结构的一致性,提高叶轮的双向旋转能力。更优选地,如图5所示,出口结构2的两个周向端面24相对于对称平面S呈平面对称,以进一步保证叶轮正反转时做功能力完全相同。Further, the two circumferential end surfaces 24 of the outlet structure 2 are located on both sides of the corresponding symmetry plane S, which can improve the structural consistency of the two circumferential end surfaces 24 of the outlet structure 2 and improve the bidirectional rotation capability of the impeller. More preferably, as shown in FIG. 5 , the two circumferential end surfaces 24 of the outlet structure 2 are planarly symmetrical with respect to the symmetry plane S, so as to further ensure that the working performance of the impeller is exactly the same when it is forward and reverse.
进一步地,如图3和图5所示,变形面21平行于轴向,更具体设置在平行于轴向的平面上,便于加工。Further, as shown in FIG. 3 and FIG. 5 , the deformation surface 21 is parallel to the axial direction, more specifically, it is arranged on a plane parallel to the axial direction, which is convenient for processing.
进一步地,如图3所示,沿着气流方向Q,出风通道31在周向相邻的两个入口结构1之间的间距逐渐增加,且在周向相邻的两个出口结构2之间的部分间距逐渐减小,使得沿着气流方向Q,出风通道31的周向宽度渐扩再渐缩,能够进一步避免回流现象的出现。当然,在其他实施例中,在气流方向Q上,在周向相邻的两个出口结构2之间的部分间距也可以逐渐增大,但是增大的速度小于出风通道31在周向相邻的两个入口结构1之间的间距增大的速度。Further, as shown in FIG. 3 , along the airflow direction Q, the spacing between the two circumferentially adjacent inlet structures 1 of the air outlet channel 31 gradually increases, and the partial spacing between the circumferentially adjacent two outlet structures 2 Gradual reduction, so that along the airflow direction Q, the circumferential width of the air outlet channel 31 gradually expands and then tapers, which can further avoid the phenomenon of backflow. Of course, in other embodiments, in the airflow direction Q, the partial spacing between two adjacent outlet structures 2 in the circumferential direction can also be gradually increased, but the increase speed is slower than that between two adjacent outlet structures 2 of the air outlet channel 31 in the circumferential direction. The speed at which the spacing between the inlet structures 1 increases.
进一步地,如图3所示,所有叶片3结构完全相同且均匀排布,可以保证叶轮的工作能力,且便于加工。Further, as shown in FIG. 3 , all blades 3 have identical structures and are evenly arranged, which can ensure the working capacity of the impeller and facilitate processing.
进一步地,如图3和图6所示,出口结构2中,包括沿着周向依次设置的两个尾板22,且两个尾板22分别设于对应的对称平面S的两侧。具体地,尾板22可以为等厚度的直板,也可以采取非等厚度板或者非直板结构。对于每个尾板22,其变形面21设置在该尾板22远离同一出口结构2中的另一尾板22的周向端面上,也就是说,出口结构2中,各尾板22远离另一尾板22的周向端面为出口结构2的周向端面24。优选地,出口结构2的整个周向端面均为变形面21。沿着气流方向Q,两个尾板22分别朝向逐渐远离对应的对称平面S的方向摆动,以使出口结构2形成分叉结构,由于分叉结构的设置,能够在使得出口结构2具有变形面21的同时,减轻叶片3重量。Further, as shown in FIG. 3 and FIG. 6 , the outlet structure 2 includes two tail plates 22 sequentially arranged along the circumferential direction, and the two tail plates 22 are respectively arranged on both sides of the corresponding plane S of symmetry. Specifically, the tail plate 22 may be a straight plate of equal thickness, or may adopt a plate of unequal thickness or a non-straight plate structure. For each tail plate 22, its deformation surface 21 is arranged on the circumferential end surface of the tail plate 22 away from the other tail plate 22 in the same outlet structure 2, that is to say, in the outlet structure 2, each tail plate 22 is far away from the other tail plate 22. The circumferential end surface of a tail plate 22 is the circumferential end surface 24 of the outlet structure 2 . Preferably, the entire circumferential end surface of the outlet structure 2 is the deformation surface 21 . Along the airflow direction Q, the two tailgates 22 swing in directions gradually away from the corresponding symmetry plane S, so that the outlet structure 2 forms a bifurcated structure. Due to the setting of the bifurcated structure, the outlet structure 2 can have a deformed surface. 21 simultaneously, reduce blade 3 weights.
另外,如图2所示,出口结构2中,两个尾板22之间的分叉角度的范围为0°-180°。此外,如图4所示,叶片3上,进气边32和出气边33为直线或者非直线。在气流方向Q上,进气边32具体为入口结构1的起始边,出气边33为出口结构2的尾端边线。进气边32与叶轮的旋转中心线O夹角β范围为 0°-180°之间,出气边33与旋转中心线O夹角大小范围为0°-90°。In addition, as shown in FIG. 2 , in the outlet structure 2 , the bifurcation angle between the two tail plates 22 ranges from 0° to 180°. In addition, as shown in FIG. 4 , on the blade 3 , the inlet side 32 and the outlet side 33 are straight or non-linear. In the airflow direction Q, the inlet side 32 is specifically the starting side of the inlet structure 1 , and the outlet side 33 is the trailing side of the outlet structure 2 . The angle β between the air inlet side 32 and the rotation center line O of the impeller ranges from 0° to 180°, and the angle between the air outlet side 33 and the rotation center line O ranges from 0° to 90°.
本实施例中提供的具有周向分叉形式叶片的双旋向电机自通风离心风扇叶轮,基于出口结构2的设置,可以解决传统双旋向电机自通风风扇出口回流严重、二次流损失较大、通流效果差的问题,同时,通过叶片3的对称结构的设置,能够满足正反转要求,为保证正反转情况下冷却散热效果相同,在满足正反转对气流做功能力一致的前提下,与现有自通风风扇相比流量、效率更高,气动性能更好。The impeller of the self-ventilating centrifugal fan of the double-rotating motor with circumferentially bifurcated blades provided in this embodiment, based on the setting of the outlet structure 2, can solve the problem of serious backflow at the outlet of the self-ventilating fan of the traditional double-rotating motor and relatively high secondary flow loss. At the same time, through the setting of the symmetrical structure of the blade 3, it can meet the requirements of forward and reverse rotation. In order to ensure the same cooling and heat dissipation effect under the condition of forward and reverse rotation, the work ability of forward and reverse airflow is consistent Compared with the existing self-ventilating fan, the flow rate and efficiency are higher, and the aerodynamic performance is better.
当然,出口结构2也不限于设置为实施例一中的分叉结构。如具体实施例二中,请参考图7和图8,出口结构2为实心的板状结构,便于加工。Of course, the outlet structure 2 is not limited to be the bifurcated structure in the first embodiment. As in the second embodiment, please refer to FIG. 7 and FIG. 8 , the outlet structure 2 is a solid plate structure, which is convenient for processing.
另外,变形面21也不限于平行于轴向设置,且可以不将整个周向端面均设置成变形面21。如具体实施例三中,参考图9至图10,在垂直于前盖板4且远离前盖板4的方向上,变形面21逐渐偏离对应的对称平面S。In addition, the deformed surface 21 is not limited to be arranged parallel to the axial direction, and the entire circumferential end surface may not be provided as the deformed surface 21 . As in the third embodiment, referring to FIG. 9 to FIG. 10 , in the direction perpendicular to the front cover 4 and away from the front cover 4 , the deformation surface 21 gradually deviates from the corresponding symmetry plane S.
其中,前盖板4为平直结构时,在气流方向Q上各处,垂直于前盖板4的方向是一致的,而在前盖板4具有弧形面时,在前盖板4的不同位置,垂直于前盖板4的方向具体为垂直于前盖板4各点切面的方向。Wherein, when the front cover plate 4 is a straight structure, the direction perpendicular to the front cover plate 4 is consistent everywhere on the airflow direction Q; In different positions, the direction perpendicular to the front cover 4 is specifically the direction perpendicular to the tangent plane of each point of the front cover 4 .
也就是说,本实施例中,出口结构2的变形面21,出口结构2周向端面的一部分表面为变形面21,其如图9所示在气流方向Q、垂直于前盖板4的方向这两个方向上均具有渐变的趋势,能够局部改善出风通道31的回流问题。That is to say, in this embodiment, the deformed surface 21 of the outlet structure 2, a part of the surface of the circumferential end surface of the outlet structure 2 is the deformed surface 21, which is shown in FIG. These two directions both have a gradual change trend, which can partially improve the backflow problem of the air outlet channel 31 .
此外,区别于实施例一,出口结构2的两个周向端面也可以不相对于对称平面S呈平面对称。在具体实施例四中,如图11和图12所示,在垂直于前盖板4且远离前盖板4的方向上,出口结构2依次包括至少两个分板23。各分板23沿着气流方向Q朝向逐渐远离对应的对称平面S的方向摆动,且出口结构2中的相邻分板23分别位于对应的对称平面S的两侧。其中,变形面21设于分板23上远离对称平面S的周向端面上。具体地,本实施例中,分板23设置两个,在其他实施例中,分板23也可以设置三个或者其他数量。本实施例中,各分板23能够在叶轮的其中一个旋转方向上起到减少回流现象的效果。In addition, different from the first embodiment, the two circumferential end faces of the outlet structure 2 may not be plane-symmetrical with respect to the symmetry plane S. In the fourth embodiment, as shown in FIG. 11 and FIG. 12 , in a direction perpendicular to the front cover 4 and away from the front cover 4 , the outlet structure 2 sequentially includes at least two sub-boards 23 . Each sub-plate 23 swings along the airflow direction Q toward a direction gradually away from the corresponding symmetry plane S, and adjacent sub-plates 23 in the outlet structure 2 are located on both sides of the corresponding symmetry plane S, respectively. Wherein, the deformation surface 21 is provided on the circumferential end surface of the sub-plate 23 away from the symmetry plane S. As shown in FIG. Specifically, in this embodiment, two sub-boards 23 are provided, and in other embodiments, three sub-boards 23 may also be provided or other numbers. In this embodiment, each sub-plate 23 can reduce the backflow phenomenon in one of the rotation directions of the impeller.
此外,不同于实施例一,出口结构2的两个周向端面24中,可以仅在 其中一个周向端面上设置变形面21。如图13所示的具体实施例五,对于叶片3,其出口结构2的左侧的周向端面为变形面21,而右侧的周向端面为平行于对应的对称平面S的表面,不具有渐变趋势,不是变形面21。In addition, different from the first embodiment, the deformation surface 21 may be provided on only one of the two circumferential end surfaces 24 of the outlet structure 2 . As shown in Figure 13 in the fifth embodiment, for the blade 3, the left circumferential end surface of the outlet structure 2 is a deformation surface 21, and the right circumferential end surface is a surface parallel to the corresponding symmetry plane S, not It has a gradual tendency and is not a deformed surface 21.
需要说明的是,当元件被称为“固定”另一个元件,它可以直接在另一个元件上或者也可以存在居中的元件。当一个元件被认为是“连接”另一个元件,它可以是直接连接到另一个元件或者可能同时存在居中元件。术语“中心”、“上”、“下”、“左”、“右”、“竖直”、“水平”、“内”、“外”等指示的方位或位置关系为基于附图所示的方位或位置关系,仅是为了便于描述本发明和简化描述,而不是指示或暗示所指的装置或元件必须具有特定的方位、以特定的方位构造和操作,因此不能理解为对本发明的限制。It should be noted that when an element is referred to as "fixing" another element, it may be directly on the other element or there may be an intervening element. 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 orientation or positional relationship indicated by the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer" and the like are based on the The orientation or positional relationship is only for the convenience of describing the present invention and simplifying the description, but does not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be construed as limiting the present invention .
除非另有定义,本文所使用的所有的技术和科学术语与属于本发明的技术领域的技术人员通常理解的含义相同。本文中在本发明的说明书中所使用的术语只是为了描述具体的实施例的目的,不是旨在于限制本发明。Unless otherwise defined, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the technical field of the invention. The terms used herein in the description of the present invention are for the purpose of describing specific embodiments only, and are not intended to limit the present invention.
本说明书中各个实施例采用递进的方式描述,每个实施例重点说明的都是与其他实施例的不同之处,各个实施例之间相同相似部分互相参见即可。Each embodiment in this specification is described in a progressive manner, each embodiment focuses on the difference from other embodiments, and the same and similar parts of each embodiment can be referred to each other.
以上对本发明所提供的双旋向电机离心风扇叶轮进行了详细介绍。本文中应用了具体个例对本发明的原理及实施方式进行了阐述,以上实施例的说明只是用于帮助理解本发明的方法及其核心思想。应当指出,对于本技术领域的普通技术人员来说,在不脱离本发明原理的前提下,还可以对本发明进行若干改进和修饰,这些改进和修饰也落入本发明权利要求的保护范围内。The centrifugal fan impeller provided by the present invention has been introduced in detail above. In this paper, specific examples are used to illustrate the principle and implementation of the present invention, and the descriptions of the above embodiments are only used to help understand the method and core idea of the present invention. It should be pointed out that for those skilled in the art, without departing from the principle of the present invention, some improvements and modifications can be made to the present invention, and these improvements and modifications also fall within the protection scope of the claims of the present invention.

Claims (10)

  1. 一种电机风扇叶轮,其特征在于,包括沿轴向依次设置的前盖板(4)和后盖板(6),所述前盖板(4)和所述后盖板(6)之间固定设置轮毂(5),所述轮毂(5)上沿周向依次固定设置多个叶片(3);所述前盖板(4)的中心设置进风口(41),相邻所述叶片(3)之间形成出风通道(31),以使风能够经所述进风口(41)沿轴向进入,再通过所述出风通道(31)沿径向流出;A motor fan impeller, characterized in that it includes a front cover (4) and a rear cover (6) arranged in sequence along the axial direction, and a gap between the front cover (4) and the rear cover (6) The wheel hub (5) is fixedly arranged, and a plurality of blades (3) are fixedly arranged in turn on the wheel hub (5) along the circumferential direction; the center of the front cover (4) is provided with an air inlet (41), adjacent to the blades ( 3) form an air outlet channel (31) between them, so that the wind can enter axially through the air inlet (41), and then flow out radially through the air outlet channel (31);
    在气流方向上,所述叶片(3)依次包括入口结构(1)和出口结构(2);In the airflow direction, the blade (3) sequentially includes an inlet structure (1) and an outlet structure (2);
    所述入口结构(1)为平面对称结构,且对称平面(S)为所述轮毂(5)的旋转中心线所在的平面;The inlet structure (1) is a plane symmetric structure, and the symmetry plane (S) is the plane where the rotation centerline of the hub (5) is located;
    所述出口结构(2)中,至少部分周向端面(24)为变形面(21),沿着气流方向,所述变形面(21)逐渐偏离对应的所述对称平面(S),其中,所述出口结构(2)与同一所述叶片(3)中所述入口结构(1)的所述对称平面(S)相对应。In the outlet structure (2), at least part of the circumferential end surface (24) is a deformed surface (21), and along the airflow direction, the deformed surface (21) gradually deviates from the corresponding plane of symmetry (S), wherein, Said outlet structure (2) corresponds to said plane of symmetry (S) of said inlet structure (1) in the same said blade (3).
  2. 根据权利要求1所述的电机风扇叶轮,其特征在于,所述出口结构(2)的两个周向端面(24)分别位于对应的所述对称平面(S)的两侧。The motor fan impeller according to claim 1, characterized in that, the two circumferential end surfaces (24) of the outlet structure (2) are respectively located on two sides of the corresponding plane of symmetry (S).
  3. 根据权利要求2所述的电机风扇叶轮,其特征在于,所述出口结构(2)的两个周向端面(24)相对于对应的所述对称平面(S)呈平面对称。The motor fan impeller according to claim 2, characterized in that, the two circumferential end surfaces (24) of the outlet structure (2) are plane-symmetric with respect to the corresponding plane of symmetry (S).
  4. 根据权利要求1所述的电机风扇叶轮,其特征在于,所有所述叶片(3)结构完全相同且均匀排布。The motor fan impeller according to claim 1, characterized in that, all the blades (3) have the same structure and are uniformly arranged.
  5. 根据权利要求1所述的电机风扇叶轮,其特征在于,所述变形面(21)平行于轴向。The motor fan impeller according to claim 1, characterized in that the deformation surface (21) is parallel to the axial direction.
  6. 根据权利要求1所述的电机风扇叶轮,其特征在于,沿着气流方向,所述出风通道(31)在周向相邻的两个所述入口结构(1)之间的间距逐渐增加,且在在周向相邻的两个所述出口结构(2)之间的部分间距逐渐减小。The motor fan impeller according to claim 1, characterized in that, along the airflow direction, the distance between the two adjacent inlet structures (1) in the circumferential direction of the air outlet channel (31) gradually increases, and Partial spacing between two circumferentially adjacent outlet structures (2) decreases gradually.
  7. 根据权利要求1至6任一项所述的电机风扇叶轮,其特征在于,所述出口结构(2)中,包括沿着周向依次设置的两个尾板(22),且两个所述尾板(22)分别设于对应的所述对称平面(S)的两侧,所述变形面(21)设于所述尾板(22)远离另一所述尾板(22)的周向端面上;沿着气流方 向,两个所述尾板(22)分别朝向逐渐远离对应的所述对称平面(S)的方向摆动,以使所述出口结构(2)形成分叉结构。The motor fan impeller according to any one of claims 1 to 6, characterized in that, the outlet structure (2) includes two tail plates (22) sequentially arranged along the circumferential direction, and the two The tail plate (22) is respectively arranged on both sides of the corresponding said symmetry plane (S), and the said deformation surface (21) is arranged on the circumferential direction of the said tail plate (22) away from the other said tail plate (22). On the end surface: along the direction of airflow, the two tail plates (22) respectively swing towards the direction gradually away from the corresponding plane of symmetry (S), so that the outlet structure (2) forms a bifurcated structure.
  8. 根据权利要求1至6任一项所述的电机风扇叶轮,其特征在于,所述出口结构(2)为实心的板状结构。The motor fan impeller according to any one of claims 1 to 6, characterized in that the outlet structure (2) is a solid plate-like structure.
  9. 根据权利要求1至4任一项所述的电机风扇叶轮,其特征在于,在垂直于所述前盖板(4)且远离所述前盖板(4)的方向上,所述变形面(21)逐渐偏离对应的所述对称平面(S)。The motor fan impeller according to any one of claims 1 to 4, characterized in that, in a direction perpendicular to the front cover (4) and away from the front cover (4), the deformation surface ( 21) Gradually deviate from the corresponding said plane of symmetry (S).
  10. 根据权利要求1至5任一项所述的电机风扇叶轮,其特征在于,在垂直于所述前盖板(4)且远离所述前盖板(4)的方向上,所述出口结构(2)依次包括至少两个分板(23);各所述分板(23)沿着气流方向朝向逐渐远离对应的对称平面(S)的方向摆动,且所述出口结构(2)中相邻所述分板(23)分别位于对应的所述对称平面(S)的两侧;所述变形面(21)设于所述分板(23)上远离对应的所述对称平面(S)的周向端面上。The motor fan impeller according to any one of claims 1 to 5, characterized in that, in a direction perpendicular to the front cover (4) and away from the front cover (4), the outlet structure ( 2) including at least two sub-boards (23) in sequence; each of the sub-boards (23) swings along the airflow direction toward a direction gradually away from the corresponding plane of symmetry (S), and the adjacent outlet structures (2) The sub-plates (23) are respectively located on both sides of the corresponding symmetry plane (S); circumferential end face.
PCT/CN2021/125172 2021-09-26 2021-10-21 Motor fan impeller WO2023045004A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CN202111128299.5 2021-09-26
CN202111128299.5A CN113685371A (en) 2021-09-26 2021-09-26 Motor fan impeller

Publications (1)

Publication Number Publication Date
WO2023045004A1 true WO2023045004A1 (en) 2023-03-30

Family

ID=78587149

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/CN2021/125172 WO2023045004A1 (en) 2021-09-26 2021-10-21 Motor fan impeller

Country Status (2)

Country Link
CN (1) CN113685371A (en)
WO (1) WO2023045004A1 (en)

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2007040236A1 (en) * 2005-10-06 2007-04-12 Mitsubishi Electric Corporation Turbo fan and air conditioner
US20090269196A1 (en) * 2008-04-25 2009-10-29 Chia-Ming Hsu Fan and airflow guiding structure thereof
CN109322842A (en) * 2018-11-26 2019-02-12 浙江理工大学 With front shroud blade and notch without spiral case centrifugal fan and working method
CN109779964A (en) * 2019-04-02 2019-05-21 萨震压缩机(上海)有限公司 Energy-saving centrifugal impeller
CN209781249U (en) * 2018-11-16 2019-12-13 依必安派特穆尔芬根有限两合公司 Diagonal fan
CN210509638U (en) * 2019-08-02 2020-05-12 珠海格力电器股份有限公司 Mixed flow fan and air conditioner
CN113048096A (en) * 2021-03-31 2021-06-29 太仓欣华盈电子有限公司 Fan blade and fan module
CN216111447U (en) * 2021-09-26 2022-03-22 中车株洲电机有限公司 Motor fan impeller

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2007040236A1 (en) * 2005-10-06 2007-04-12 Mitsubishi Electric Corporation Turbo fan and air conditioner
US20090269196A1 (en) * 2008-04-25 2009-10-29 Chia-Ming Hsu Fan and airflow guiding structure thereof
CN209781249U (en) * 2018-11-16 2019-12-13 依必安派特穆尔芬根有限两合公司 Diagonal fan
CN109322842A (en) * 2018-11-26 2019-02-12 浙江理工大学 With front shroud blade and notch without spiral case centrifugal fan and working method
CN109779964A (en) * 2019-04-02 2019-05-21 萨震压缩机(上海)有限公司 Energy-saving centrifugal impeller
CN210509638U (en) * 2019-08-02 2020-05-12 珠海格力电器股份有限公司 Mixed flow fan and air conditioner
CN113048096A (en) * 2021-03-31 2021-06-29 太仓欣华盈电子有限公司 Fan blade and fan module
CN216111447U (en) * 2021-09-26 2022-03-22 中车株洲电机有限公司 Motor fan impeller

Also Published As

Publication number Publication date
CN113685371A (en) 2021-11-23

Similar Documents

Publication Publication Date Title
US10052931B2 (en) Outdoor cooling unit in vehicle air-conditioning apparatus
CN106762780B (en) Fan support and fan device comprising same
JP4926843B2 (en) Airflow rectifier and series fan
TW201219657A (en) Fan structure
JP4374897B2 (en) Axial fan
JP2014047775A (en) Diffuser, and centrifugal compressor and blower including the diffuser
WO2008075467A1 (en) Cascade of axial compressor
CN106593952A (en) Axial-flow fan blade, fan with same, and air conditioner outdoor unit
JP2001234893A (en) Axial blower
CN216111447U (en) Motor fan impeller
WO2023045004A1 (en) Motor fan impeller
CN113883098A (en) Stator blade distortion-resistant axial flow compressor and stator blade distortion-resistant method of axial flow compressor
WO2021243969A1 (en) Fan blade, fan, air conditioner outdoor unit and air conditioner system
JP2016524094A (en) Vertical axis wind turbine
JPH09100795A (en) Air conditioner
WO2021169197A1 (en) Centrifugal fan and air conditioning device
CN216343043U (en) Static blade distortion-resistant axial flow compressor
CN108953222B (en) Centrifugal impeller
JP2000130799A (en) Outdoor unit of air conditioner
CN211737550U (en) Backward centrifugal cross-section noise reduction type centrifugal fan blade
CN220227235U (en) Disrotatory fan
CN206449014U (en) Axial-flow leaf and blower fan, air-conditioner outdoor unit with it
US9903206B2 (en) Impeller
JP6330738B2 (en) Centrifugal blower and air conditioner using the same
WO2022191034A1 (en) Propeller fan and refrigeration device

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 21958119

Country of ref document: EP

Kind code of ref document: A1