WO2014117288A1 - Composite impeller and air supply device thereof - Google Patents

Composite impeller and air supply device thereof Download PDF

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Publication number
WO2014117288A1
WO2014117288A1 PCT/CN2013/000088 CN2013000088W WO2014117288A1 WO 2014117288 A1 WO2014117288 A1 WO 2014117288A1 CN 2013000088 W CN2013000088 W CN 2013000088W WO 2014117288 A1 WO2014117288 A1 WO 2014117288A1
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WO
WIPO (PCT)
Prior art keywords
centrifugal
casing
axial flow
air supply
blades
Prior art date
Application number
PCT/CN2013/000088
Other languages
French (fr)
Chinese (zh)
Inventor
陈耀乾
Original Assignee
Chen Yao-Chien
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.)
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Publication date
Application filed by Chen Yao-Chien filed Critical Chen Yao-Chien
Priority to PCT/CN2013/000088 priority Critical patent/WO2014117288A1/en
Publication of WO2014117288A1 publication Critical patent/WO2014117288A1/en

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D17/00Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
    • F04D17/02Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps having non-centrifugal stages, e.g. centripetal
    • F04D17/025Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps having non-centrifugal stages, e.g. centripetal comprising axial flow and radial flow stages
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D19/00Axial-flow pumps
    • F04D19/002Axial flow fans
    • 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
    • F04D29/32Rotors specially for elastic fluids for axial flow pumps
    • F04D29/325Rotors specially for elastic fluids for axial flow pumps for axial flow fans
    • F04D29/329Details of the hub
    • 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
    • F04D29/32Rotors specially for elastic fluids for axial flow pumps
    • F04D29/34Blade mountings
    • F04D29/36Blade mountings adjustable

Definitions

  • the invention relates to a blowing device, in particular to a composite impeller and an air blowing device thereof. Background technique
  • the blower is roughly divided into a centrifugal blower and an axial flow blower according to the direction in which the airflow passes through the blade.
  • the airflow direction of the centrifugal blower enters along the axial direction of the impeller, and is discharged radially to the outer circumference perpendicular to the axle. It mainly uses the centrifugal effect to pressurize the fluid, so it can generate high pressure and has the characteristics of low air volume and high wind pressure.
  • the airflow of the axial flow fan enters along the axial direction of the impeller and is directly discharged through the blade in the axial direction of the wheel. Therefore, when the blade rotates, the suction surface and the pressure surface are respectively formed on both sides of the blade to drive the airflow, so the pressure is small. However, due to its large area of action, it has a high flow rate and high air volume and low wind pressure.
  • blowers Although the above two types of blowers have the characteristics of "high air volume, low wind pressure” and “low air volume and high wind pressure J, there are actually insurmountable problems.
  • the problem is that the centrifugal blower has airflow.
  • 1361250 discloses that an opening is provided in the low pressure region of the outer casing of the centrifugal blower, so that the inner side of the outer casing is open to the atmosphere, and the air intake area is increased by the aforementioned opening, and the centrifugal blower is increased. The amount of intake air.
  • Taiwan Patent Publication No. 535859, No. 592343, No. M241515, No. M372898, and the like In the case of an axial flow blower, such as the Taiwan Patent Publication No. 535859, No. 592343, No. M241515, No. M372898, and the like.
  • the disclosures of Taiwan Patent Publication Nos. 535859, No. 592343, No. M241515, etc. mainly open an opening through which the airflow can be introduced in the front part of the outer casing of the axial flow blower, so that the inside of the outer casing is open to the atmosphere. With the aforementioned opening The hole increases the intake area and increases the intake air volume of the axial flow fan. According to the disclosure of the patent No.
  • a plurality of baffles fixed on the inner surface of the outer casing are disposed on the air outlet side (rear side) of an impeller disposed in a casing, so that the airflow is sent out through the impeller. And then flowing out along the flow guiding piece, by means of the aforementioned plurality of baffles to increase the flow velocity of the airflow.
  • Taiwan Patent No. 1289630 it combines an impeller for a turbofan and a casing for an axial fan to obtain a high static air by means of an impeller for a turbofan, and is used for an axial flow fan.
  • the housing expands the discharge area.
  • Taiwan Patent No. M262754 the axial flow type and the centrifugal impeller are integrated to improve the flow rate and wind pressure generated by the centrifugal impeller, and the flow passage width is narrowed to increase the Flow rate, the disadvantage of this method is that although the flow velocity of the airflow can be increased, the air intake area cannot be increased to increase the flow rate.
  • Taiwan Patent No. M366881 also has the problem of applicability as described above.
  • Taiwan Patent No. M372898 has a disadvantage in that the provision of the above-mentioned baffle plate can increase the flow velocity of the airflow, but it is not possible to increase the intake air area to increase the flow rate.
  • the diagonal flow impeller has both axial flow and centrifugal characteristics, and is applied to the blower structure.
  • the diagonal flow structure Since a plurality of inclined blades that are radially arranged and extend toward the air outlet and expand outward are used, there is a disadvantage that the volume of the device is increased due to the increase in space.
  • the present invention has been made to solve the above problems of the prior art, and an object thereof is to provide a feature of an axial flow type and a centrifugal type air blower, which can increase the air volume and the wind pressure at the same rotation speed without excessively increasing at the same time.
  • the present invention provides a composite impeller comprising:
  • a casing having an inlet in an axial direction of the center of rotation and a plurality of outlets in a radial direction of the central axis of rotation; a plurality of centrifugal blades uniformly arranged around the central axis of rotation and fixed to an inner surface of the casing, and rotating to generate a centrifugal airflow which is entered by the inlet of the casing and discharged from the plurality of outlets,
  • the range of the rotational motion of the plurality of centrifugal blades is defined to form a centrifugal air supply action zone;
  • a plurality of axial flow vanes centered on the central axis of rotation and radially uniformly disposed around a radial direction of the casing, and rotating to generate an axial flow of air along an axial direction of the rotation center, the plurality of axes
  • the range of the rotational motion of the flow vane defines an axial flow air supply zone
  • a driving unit that drives the casing to rotate around the rotating central axis to synchronously rotate the plurality of centrifugal blades and the plurality of axial flow blades;
  • the outlet of the casing communicates with the centrifugal air supply zone and the axial air supply zone; wherein, when the driving unit drives the plurality of centrifugal blades and the plurality of axial blades to rotate synchronously, the centrifugal is performed
  • the airflow is discharged from the centrifugal blowing action zone through the outlet of the casing such that at least a portion of the centrifugal airflow enters the axial flow air supply zone and is mixed with the axial flow airflow, and the at least a portion of the centrifugal airflow is simultaneously subjected to the
  • the plurality of axial flow blades are rotationally pushed to accelerate the axial direction of the rotation center.
  • the composite impeller wherein the casing has a pair of side plates covering both sides of the plurality of centrifugal blades, and the inlet is provided in one of the pair of side plates, between the pair of side plates And the plurality of outlets are provided on an outer peripheral side of the multi-centrifugal blade.
  • the composite impeller wherein an outlet of the casing communicates with the centrifugal air supply zone and the axial air supply zone.
  • each of the axial flow blades includes a blade portion and a fixing portion, and is fixed to a radial periphery of the casing by a fixing seat
  • the fixing seat includes a first seat body and a first body a two-seat body, wherein the first seat body and the second seat body are interlocked with each other, and the first seat body and the second seat body are respectively provided with corresponding grooves corresponding to each axial flow blade.
  • the cross-sectional shape of the fixing portion of each of the axial flow vanes is circular or polygonal.
  • the composite impeller wherein at least one fastener is further utilized to pass through the machine separately
  • the shell, the first seat body and the second seat body are locked against the locking holes provided by the lock body.
  • the present invention also provides an air supply device, which is provided with a composite impeller in a cylindrical outer casing, wherein the two ends of the tubular outer casing are respectively an air inlet and an air outlet, and The composite impeller rotates to drive air from the air inlet and then from the air outlet.
  • the air blowing device wherein the inside of the cylindrical outer box is further provided with a bracket for supporting the driving unit.
  • the invention has the advantages of: having the characteristics of an axial flow type and a centrifugal type blower, and can increase the air volume and the wind pressure at the same rotation speed without excessively increasing the space of the device.
  • Figure 1 is a perspective view showing the appearance of a composite impeller of the present invention
  • Figure 3 is a longitudinal cross-sectional view of the composite impeller of the present invention including a central axis X;
  • Figure 4 is a plan view of the composite impeller of the present invention as seen from the suction side;
  • Figure 5 is a left side view of Figure 1;
  • Figure 6 is a perspective perspective view of the composite impeller of the present invention and its air blowing device
  • Fig. 7 is a schematic view showing the operation of the composite impeller and the air blowing device thereof according to the present invention.
  • the composite impeller 1 has a plurality of centrifugal blades 20 disposed around the central axis X and fixed to the inside of the casing 10, and is disposed at the periphery of the central axis X and fixed to the radially outer periphery of the casing 10.
  • a plurality of axial flow vanes 30 The so-called centrifugal blade rotates to make the air toward the central axis X (the center of rotation of the impeller)
  • the blade structure of the shaft is discharged in the radial direction.
  • the so-called axial flow vane is rotated to cause the air to be discharged toward the blade structure in a direction parallel to the central axis X (the rotational center axis of the impeller).
  • the composite impeller 1 of the present invention incorporates a centrifugal and axial flow mixed-flow impeller, and the air is sucked from the front side of the composite impeller 1 by centrifugal rotation of the centrifugal vane 20 and the axial flow vane 30 shown in FIG. After the airflow is mixed with the axial flow, it is sent to the rear side to generate a flow in the direction of the central axis X.
  • the central axis X direction described below the front side in Fig. 1 on the suction air side is referred to as the r intake side J, and the rear side in Fig. 1 on the discharge air side is referred to as the "exhaust side".
  • the front side in Fig. 1 on the suction air side is referred to as the r intake side J
  • the rear side in Fig. 1 on the discharge air side is referred to as the "exhaust side”.
  • the composite impeller 1 includes a casing 10, a plurality of centrifugal blades 20, a plurality of axial flow blades 30, and a drive unit 40.
  • the casing 10 is provided with an inlet 1 1 on one side in the direction (axial direction) in which the center axis X extends, and a plurality of outlets 12 are provided around the radial direction of the center axis X.
  • the plurality of centrifugal blades 20 are centered on the central axis X and uniformly arranged around the central axis X in the circumferential direction, and are fixed to the inner surface of the casing 10 by using the plurality of centrifugal blades 20 as the central axis X
  • the center is rotated counterclockwise in FIG. 4 (as in the direction of arrow R1 in FIG. 4), and air is drawn from the inlet 11 of the casing 10 to move air from the plurality of centrifugal blades 20 to each other.
  • the centrifugal airflow is sent out in the centrifugal direction, and the air is discharged from the outlet 12 (i.e., the air is taken in from the front side of the composite impeller 1 in Figs.
  • centrifugal airflow wherein the range of the rotational motion of the plurality of centrifugal blades 20 is defined to form a centrifugal air supply zone 21.
  • the diameter of the inner circumference 11a of the inlet 11 of the casing 10 is larger than the diameter of the inner end 20a of the centrifugal blade 20.
  • the plurality of axial flow vanes 30 are centered around the central axis X and radially uniformly disposed around the radial direction of the casing, by rotating the plurality of axial flow vanes 30 with the central axis X as the center and counterclockwise in FIG. (as in the direction of arrow R1 in Fig. 4), an air flow is generated along the central axis X direction (i.e., from the front side of the composite impeller 1 in Figs. 3, 4, and through the axial flow vanes 30).
  • the axial flow is sent toward the rear side, wherein the range of the rotational motion of the plurality of axial blades 30 defines an axial flow supply zone 31.
  • the driving unit 40 is composed of a motor and is disposed on the opposite side of the casing 10 and disposed on the opposite side of the casing 10, and is connected to the casing 10, and drives the casing 10 counterclockwise with the central axis X as a center ( Rotation in the direction of the arrow R1 in FIG. 4 to rotate the plurality of centrifugal blades 20 and the plurality of axial flow blades 30 in synchronization.
  • the casing 10 has a pair of side plates 13, 14 covering both sides of the plurality of centrifugal blades 20, and the inlet plate 1 is provided in one of the pair of side plates 13, 14 The plurality of outlets are provided between the side plates 13 and 14 and on the outer peripheral side of the plurality of centrifugal blades 20.
  • the outlet 11 of the casing 10 communicates with the centrifugal air supply zone 21 and the axial air supply zone 31.
  • each of the axial flow blades 30 includes a blade portion 32 and a fixing portion 33, and is fixed to a radial periphery of the casing 10 by a fixing base 50.
  • the fixing base 50 includes a first seat.
  • the first base body 51 and the second base body 52 are respectively correspondingly coupled to each other, and the first base body 51 and the second base body 52 are respectively provided with a corresponding one.
  • the grooves 51 1 and 521 are provided for fixing portions 33 of the respective axial flow vanes 30.
  • the cross-sectional shape of the fixing portion 33 of each of the axial flow blades 30 may be circular or polygonal and corresponding to the shapes of the grooves 51 1 and 521 of the first base body 51 and the second base body 52, so that the fixing portion 33 can be The first seat body 51 and the recesses 51 1 and 521 of the second seat body 52 are tightly fitted.
  • the width 30a of the end of each axial blade 30 (that is, the width of the blade portion 32 near the fixed portion 33) is greater than or equal to the width 12a of the outlet 12 of the casing 10 in the axial direction of the central axis X. .
  • each of the axial flow vanes 30 When assembled, the fixing portion 33 of each of the axial flow vanes 30 can be correspondingly inserted into the recesses 51 1 and 521 of the first base body 51 and the second base body 52, and then passed through at least one fastener 60 such as a bolt.
  • the locking holes 61 provided in the corresponding locking members 60 are locked on the casing 10, the first base 51 and the second base 52, so that the axial blades 30 and the casing 10 can be stably locked. Solidified.
  • an indication scale (not shown) may be disposed on the bottom surface of the fixing portion 33 of each of the axial flow vanes 30.
  • the indication scale may be used to identify the installation angle of each axial flow vane 30 when the axial flow vanes 30 are mounted.
  • the axial flow vanes 30 can be easily positioned at the same mounting angle to enhance the efficiency and accuracy of mounting the axial flow vanes 30.
  • the blade 20 rotates and is discharged toward the outlet 12 of the casing 10 (i.e., is sent from the outer peripheral side of the plurality of centrifugal blades 20 toward the central axis X) to form a centrifugal air flow, that is, in the centrifugal air supply.
  • the zone 21 forms a centrifugal gas stream into which at least a portion of the gas stream enters the axial flow supply zone 31, i.e., between the two axial flow vanes 30, and is mixed with the axial flow, and the at least a portion of the centrifugal flow
  • the plurality of axial flow vanes 30 are rotated and pushed, and then the air flow pushed by the rotation is accelerated toward the central axis X direction.
  • the rear side (exhaust side) of the composite impeller 1 in the parallel direction is sent out; and the other part of the air passes through the plurality of axial flow vanes 30 and is rotated out along with the plurality of axial flow vanes 30 to form an axial flow, that is, Forming an axial flow in the axial flow supply zone 31, at least a portion of the axial flow being mixed with at least a portion of the centrifugal flow passing through the outlet 12 of the casing 10, together with the plurality of axial blades 30
  • the composite impeller 1 is sent to the rear side (exhaust side) in a direction parallel to the central axis X direction.
  • the air blowing device 2 of the present invention comprises: a cylindrical outer casing 70, wherein the composite impeller 1 is disposed, wherein the two ends of the cylindrical outer casing 70 are respectively an air inlet. 71 and the air outlet 72, and the composite impeller 1 is rotated to drive air from the air inlet 71, and then through the centrifugal blade 20 and the axial flow blade 30 of the composite impeller 1, and then sent out by the air outlet 72 (as indicated by the arrow in Figure 8).
  • a bracket 73 may be disposed in the cylindrical outer casing 70 for supporting the drive unit 40.
  • the composite impeller and the air blowing device of the present invention can increase the pressure of the air to be sent by combining the blades of the centrifugal and axial flow, and further increase the air flow rate due to the suction side having a wider area. .
  • each of the axial flow vanes 30 is provided on the outer peripheral side of the outlet 12 of the casing 10, whereby the distance of the air sent from the centrifugal vane 20 to the axial flow vanes 30 becomes short, and therefore, the pressure loss of the air can be reduced. , can improve efficiency.
  • the inlet 11 of the casing 10 is disposed on the side of the central axis X of the one side plate 13, and a portion of the side plate 13 other than the inlet 11 covers an outer side of the centrifugal blade 20, whereby It is possible to prevent the air sent out from the outer peripheral side of the centrifugal blade 20 from leaking from the inlet 11 side of the casing 10, and therefore, the efficiency can be improved.

Abstract

A composite impeller and an air supply device thereof. The composite impeller comprises: a casing; multiple centrifugal blades, fixedly arranged in the casing, wherein a rotation stroke range of the centrifugal blades defines a centrifugal air supply action region; multiple axial flow blades, radially and uniformly configured on the radial periphery of the casing, wherein a rotation stroke range of the axial flow blades defines an axial flow air supply action region; and a drive unit, for enabling the centrifugal blades and the axial flow blades to rotate synchronously so as to respectively produce a centrifugal air flow and an axial flow air flow. At least one part of the centrifugal air flow enters the axial flow air supply action region from the centrifugal air supply action region, and is mixed with the axial flow air flow. The mixed air flows are pushed by the axial flow blades in rotation, so that the flowing speed is axially accelerated, and the flow quantity and air pressure can be increased at the same rotation speed.

Description

复合式叶轮及其送风装置 技术领域  Compound impeller and air supply device thereof
本发明涉及一种送风装置, 尤指一种复合式叶轮及其送风装置。 背景技术  The invention relates to a blowing device, in particular to a composite impeller and an air blowing device thereof. Background technique
一般送风机依照气流通过叶片的方向大致分为离心式送风机与轴流式送风 机两种, 其中, 离心式送风机的气流方向沿叶轮的轮轴向方向进入, 再朝垂直 于轮轴的外周围放射线地排出, 其主要系利用离心效应来加压流体, 故可产生 较高的压力, 且具有低风量、 高风压的特性。 轴流式送风机的气流沿叶轮的轮 轴向方向进入, 并直接通过叶片后沿轮轴向方向排出, 因此当叶片转动时, 叶 片的两面分别形成吸入面和压力面来驱动气流流动, 故压力较小, 但因作用面 积大, 具有较高流量, 且具有高风量、 低风压的特性。  Generally, the blower is roughly divided into a centrifugal blower and an axial flow blower according to the direction in which the airflow passes through the blade. The airflow direction of the centrifugal blower enters along the axial direction of the impeller, and is discharged radially to the outer circumference perpendicular to the axle. It mainly uses the centrifugal effect to pressurize the fluid, so it can generate high pressure and has the characteristics of low air volume and high wind pressure. The airflow of the axial flow fan enters along the axial direction of the impeller and is directly discharged through the blade in the axial direction of the wheel. Therefore, when the blade rotates, the suction surface and the pressure surface are respectively formed on both sides of the blade to drive the airflow, so the pressure is small. However, due to its large area of action, it has a high flow rate and high air volume and low wind pressure.
上述两种送风机虽然分别具有 「高风量、 低风压」及 「低风量、 高风压 J 的特性, 但, 实际上却存在有难以克服的问题, 而此问题在于, 离心式送风机 存在有气流流量不足的问题, 轴流式送风机存在有风压低的问题。  Although the above two types of blowers have the characteristics of "high air volume, low wind pressure" and "low air volume and high wind pressure J, there are actually insurmountable problems. The problem is that the centrifugal blower has airflow. The problem of insufficient flow, the axial flow blower has a problem of low wind pressure.
因此, 遂有提出可增加风压或风量的结构, 期待借此一创新设计而可消除 上述缺点。  Therefore, there is a structure for increasing the wind pressure or the amount of wind, and it is expected that the above disadvantages can be eliminated by an innovative design.
以离心式送风机而言, 如中国台湾专利第 M366881号及第 1361250号等专 利案。 其中, 中国台湾专利第 M366881号专利案所揭示内容, 是于其离心叶片 外围环设有多个以涡漩状地间隔配置的导流片, 并使气流经由离心叶片与及多 个导流片而排出, 凭借该多个导流片的导流, 可使令进入导流片的流道中的气 流压力增加, 并使该气流离开速度增加, 借此增加出风速度及风量。 其中, 中 国台湾专利第 1361250号专利案所揭示内容,于离心送风机的外壳的低压区范围 设置开孔, 使外壳内侧与大气相通, 通过前述开孔可使进气面积增加, 而增加 离心式送风机的进气量。  In the case of centrifugal blowers, such as Taiwan Patent No. M366881 and No. 1361250, etc. The disclosure of the Chinese Patent No. M366881 discloses that a plurality of baffles arranged in a swirling manner are arranged on the outer circumference of the centrifugal blade, and the airflow is passed through the centrifugal blade and the plurality of baffles. By discharging, by the diversion of the plurality of baffles, the pressure of the airflow in the flow path entering the baffle can be increased, and the exit velocity of the airflow can be increased, thereby increasing the wind speed and the air volume. Among them, the disclosure of the Chinese Patent No. 1361250 discloses that an opening is provided in the low pressure region of the outer casing of the centrifugal blower, so that the inner side of the outer casing is open to the atmosphere, and the air intake area is increased by the aforementioned opening, and the centrifugal blower is increased. The amount of intake air.
以轴流式送风机而言, 如中国台湾专利公告第 535859号、 第 592343号、 第 M241515号、 第 M372898号等专利案。 其中, 中国台湾专利公告第 535859 号、 第 592343号、 第 M241515号等专利案所揭示内容, 主要是在轴流式送风机 的外壳的前段开设有能导入气流的开孔, 使外壳内侧与大气相通, 凭借前述开 孔可使进气面积增加, 而增加轴流式送风机的进气量。 其中, 第 M372898号专 利案所揭示内容, 在设于一外壳内的一叶轮的出风侧 (后侧) 环设有多个固定 在外壳内表面的导流片, 使气流经叶轮旋转送出后, 再沿着导流片流动而送出 去, 凭借前述多个导流片以增加气流的流动速度。 In the case of an axial flow blower, such as the Taiwan Patent Publication No. 535859, No. 592343, No. M241515, No. M372898, and the like. Among them, the disclosures of Taiwan Patent Publication Nos. 535859, No. 592343, No. M241515, etc., mainly open an opening through which the airflow can be introduced in the front part of the outer casing of the axial flow blower, so that the inside of the outer casing is open to the atmosphere. With the aforementioned opening The hole increases the intake area and increases the intake air volume of the axial flow fan. According to the disclosure of the patent No. M372898, a plurality of baffles fixed on the inner surface of the outer casing are disposed on the air outlet side (rear side) of an impeller disposed in a casing, so that the airflow is sent out through the impeller. And then flowing out along the flow guiding piece, by means of the aforementioned plurality of baffles to increase the flow velocity of the airflow.
如中国台湾专利第 1289630号所揭示内容,其结合涡轮风扇用的叶轮及轴流 式风扇用的壳体, 以凭借涡轮风扇用的叶轮得到高静压的空气, 且凭借轴流式 风扇用的壳体扩大吐出区域。  As disclosed in Taiwan Patent No. 1289630, it combines an impeller for a turbofan and a casing for an axial fan to obtain a high static air by means of an impeller for a turbofan, and is used for an axial flow fan. The housing expands the discharge area.
如中国台湾专利第 M262754号所揭示内容, 其是将轴流式与离心式叶轮作 一整合运用, 来提升离心式叶轮所能产生的流量及风压, 并且利用流道宽窄的 不同来增加其流速, 这种方式的缺点在于, 虽可增加气流的流动速度, 但无法 增加进气面积来使流量增加。  As disclosed in Taiwan Patent No. M262754, the axial flow type and the centrifugal impeller are integrated to improve the flow rate and wind pressure generated by the centrifugal impeller, and the flow passage width is narrowed to increase the Flow rate, the disadvantage of this method is that although the flow velocity of the airflow can be increased, the air intake area cannot be increased to increase the flow rate.
可是, 若依据该以往的技术, 虽然可增加出风速度及风量, 但是通过对送 风机外壳设置能导入气流的开孔的技术而言, 所能提供增加风速及风量比较适 合于小型送风机, 而不适合于大型送风机使用。 因而, 具有产生产品适用性的 问题。 上述中国台湾专利第 M366881号专利案也具有如前述所产生适用性的问 题。 又, 上述中国台湾专利第 M372898号专利案的缺点在于, 设置前述导流片 虽可增加气流的流动速度, 但无法增加进气面积来使流量增加。  However, according to the conventional technique, although the air blowing speed and the air volume can be increased, by providing a technique for introducing the opening of the airflow to the blower casing, it is possible to provide an increase in the wind speed and the air volume, which is suitable for a small blower without Suitable for large blowers. Therefore, there is a problem of producing product suitability. The above-mentioned Taiwan Patent No. M366881 also has the problem of applicability as described above. Further, the above-mentioned Taiwan Patent No. M372898 has a disadvantage in that the provision of the above-mentioned baffle plate can increase the flow velocity of the airflow, but it is not possible to increase the intake air area to increase the flow rate.
再者, 除上述两种传统送风机结构外, 目前市面上已有将斜流式叶轮所兼 具有轴流式与离心式的特性, 而运用在送风机结构上, 然而, 此斜流式的结构 由于使用数片呈放射状排列且朝出风口方向延伸及向外扩张的倾斜扇叶, 因此, 存在有增加装置空间所造成的体积庞大的缺点。  Furthermore, in addition to the above two conventional blower structures, the diagonal flow impeller has both axial flow and centrifugal characteristics, and is applied to the blower structure. However, the diagonal flow structure Since a plurality of inclined blades that are radially arranged and extend toward the air outlet and expand outward are used, there is a disadvantage that the volume of the device is increased due to the increase in space.
因此, 如何提升送风机的整体工作效率, 以产生较大风量、 提高风压, 是 当前重要课题之一。 发明内容  Therefore, how to improve the overall working efficiency of the blower to generate a large amount of air and increase the wind pressure is one of the important issues at present. Summary of the invention
本发明为解决上述现有技术的问题而完成, 其目的在于提供一种兼具有轴 流式及离心式送风机的特点, 而可在相同转速下能增加风量与风压, 且同时不 过度增加装置空间的复合式叶轮及其送风装置。  The present invention has been made to solve the above problems of the prior art, and an object thereof is to provide a feature of an axial flow type and a centrifugal type air blower, which can increase the air volume and the wind pressure at the same rotation speed without excessively increasing at the same time. A composite impeller with a device space and its air supply device.
为达成上述目的, 本发明提供一种复合式叶轮, 其包含:  To achieve the above object, the present invention provides a composite impeller comprising:
一机壳, 具有在旋转中心轴向方向的一进口, 及在该旋转中心轴的径向方 向的多个出口; 多个离心叶片, 均匀地排列在该旋转中心轴周围, 且固接在该机壳的内表 面, 并通过旋转而产生由该机壳的进口进入而由该多个出口排出的离心气流, 该多个离心叶片的旋转动程的范围界定形成一离心送风作用区; a casing having an inlet in an axial direction of the center of rotation and a plurality of outlets in a radial direction of the central axis of rotation; a plurality of centrifugal blades uniformly arranged around the central axis of rotation and fixed to an inner surface of the casing, and rotating to generate a centrifugal airflow which is entered by the inlet of the casing and discharged from the plurality of outlets, The range of the rotational motion of the plurality of centrifugal blades is defined to form a centrifugal air supply action zone;
多个轴流叶片, 以该旋转中心轴为中心且放射线状地均匀配置在该机壳的 径向周围, 并通过旋转而产生沿着该旋转中心轴向方向的轴流气流, 该多个轴 流叶片的旋转动程的范围界定形成一轴流送风作用区; 以及  a plurality of axial flow vanes centered on the central axis of rotation and radially uniformly disposed around a radial direction of the casing, and rotating to generate an axial flow of air along an axial direction of the rotation center, the plurality of axes The range of the rotational motion of the flow vane defines an axial flow air supply zone;
一驱动单元, 以该旋转中心轴为中心驱动该机壳旋转, 以使该多个离心叶 片及该多个轴流叶片同步旋转;  a driving unit that drives the casing to rotate around the rotating central axis to synchronously rotate the plurality of centrifugal blades and the plurality of axial flow blades;
其中, 前述径向方向是垂直于该旋转中心轴;  Wherein the aforementioned radial direction is perpendicular to the central axis of rotation;
其中, 该机壳的出口连通于该离心送风作用区与该轴流送风作用区; 其中, 当该驱动单元驱使该多个离心叶片及该多个轴流叶片同步旋转时, 使该离心气流由该离心送风作用区通过该机壳的出口排出, 使其至少一部分的 离心气流进入该轴流送风作用区, 而与该轴流气流混合, 且该至少一部分的离 心气流同时受到该多个轴流叶片转动推挤而能加速地朝该旋转中心轴向方向流 动。  The outlet of the casing communicates with the centrifugal air supply zone and the axial air supply zone; wherein, when the driving unit drives the plurality of centrifugal blades and the plurality of axial blades to rotate synchronously, the centrifugal is performed The airflow is discharged from the centrifugal blowing action zone through the outlet of the casing such that at least a portion of the centrifugal airflow enters the axial flow air supply zone and is mixed with the axial flow airflow, and the at least a portion of the centrifugal airflow is simultaneously subjected to the The plurality of axial flow blades are rotationally pushed to accelerate the axial direction of the rotation center.
所述的复合式叶轮, 其中, 该机壳具有覆盖该多个离心叶片的两侧的一对 侧板, 并且于该对侧板中的一侧板设有该进口, 于该对侧板间且位于该多离心 叶片的外周侧设有该多个出口。  The composite impeller, wherein the casing has a pair of side plates covering both sides of the plurality of centrifugal blades, and the inlet is provided in one of the pair of side plates, between the pair of side plates And the plurality of outlets are provided on an outer peripheral side of the multi-centrifugal blade.
所述的复合式叶轮, 其中, 该机壳的出口连通于该离心送风作用区及该轴 流送风作用区。  The composite impeller, wherein an outlet of the casing communicates with the centrifugal air supply zone and the axial air supply zone.
所述的复合式叶轮, 其中, 各轴流叶片末端的宽度大于或等于该机壳的出 口在该旋转中心轴的轴向方向上的宽度。  The composite impeller, wherein the width of the end of each axial flow blade is greater than or equal to the width of the outlet of the casing in the axial direction of the central axis of rotation.
所述的复合式叶轮, 其中, 该机壳的进口的内周缘的直径大于该离心叶片 的内端的直径。  The composite impeller, wherein an inner circumference of the inlet of the casing has a diameter larger than a diameter of an inner end of the centrifugal blade.
所述的复合式叶轮, 其中, 各轴流叶片包含一叶片部及一固定部, 并且利 用一固定座固定于该机壳的径向周围上, 该固定座包含一第一座体及一第二座 体, 且该第一座体与该第二座体相互对应锁合, 该第一座体与该第二座体内部 分别设有一相互对应的凹槽, 供夹设各轴流叶片的固定部。  The composite impeller, wherein each of the axial flow blades includes a blade portion and a fixing portion, and is fixed to a radial periphery of the casing by a fixing seat, the fixing seat includes a first seat body and a first body a two-seat body, wherein the first seat body and the second seat body are interlocked with each other, and the first seat body and the second seat body are respectively provided with corresponding grooves corresponding to each axial flow blade. Fixed part.
所述的复合式叶轮, 其中, 各轴流叶片的固定部的截面形状为圆形或多边 形。  In the composite impeller, the cross-sectional shape of the fixing portion of each of the axial flow vanes is circular or polygonal.
所述的复合式叶轮, 其中, 进一步利用至少一锁固件, 以分别穿设过该机 壳、 该第一座体及该第二座体上对应该锁固件设置的锁固孔而锁固。 本发明还提供一种送风装置, 其是于一筒型外箱内设有所述的复合式叶轮, 其特征在于, 该筒型外箱的两端分别为一入风口及出风口, 并通过该复合式叶 轮转动, 以驱使空气由该入风口进入再由该出风口送出。 The composite impeller, wherein at least one fastener is further utilized to pass through the machine separately The shell, the first seat body and the second seat body are locked against the locking holes provided by the lock body. The present invention also provides an air supply device, which is provided with a composite impeller in a cylindrical outer casing, wherein the two ends of the tubular outer casing are respectively an air inlet and an air outlet, and The composite impeller rotates to drive air from the air inlet and then from the air outlet.
所述的送风装置, 其中, 该筒型外箱的内部进一步设置一支承该驱动单元 的支架。  The air blowing device, wherein the inside of the cylindrical outer box is further provided with a bracket for supporting the driving unit.
本发明的有益效果是: 兼具有轴流式及离心式送风机的特点, 而可在相同 转速下能增加风量与风压, 且同时不过度增加装置空间。 附图说明  The invention has the advantages of: having the characteristics of an axial flow type and a centrifugal type blower, and can increase the air volume and the wind pressure at the same rotation speed without excessively increasing the space of the device. DRAWINGS
图 1为本发明的复合式叶轮的外观立体图;  Figure 1 is a perspective view showing the appearance of a composite impeller of the present invention;
图 2为本发明的复合式叶轮的分解示意图;  2 is an exploded perspective view of the composite impeller of the present invention;
图 3为本发明的复合式叶轮以包含中心轴 X的纵向截面图;  Figure 3 is a longitudinal cross-sectional view of the composite impeller of the present invention including a central axis X;
图 4为本发明的复合式叶轮从吸气侧所见的平面图;  Figure 4 is a plan view of the composite impeller of the present invention as seen from the suction side;
图 5为图 1的左侧视图;  Figure 5 is a left side view of Figure 1;
图 6为本发明的复合式叶轮及其送风装置的立体透视图;  Figure 6 is a perspective perspective view of the composite impeller of the present invention and its air blowing device;
图 7为本发明的复合式叶轮及其送风装置的动作说明示意图。  Fig. 7 is a schematic view showing the operation of the composite impeller and the air blowing device thereof according to the present invention.
附图标记说明: 复合式叶轮 1 ; 机壳 10; 进口 1 1 ; 内周缘 1 1a; 出口 12; 宽度 12a; 侧板 13、 14; 离心叶片 20; 内端 20a; 离心送风作用区 21 ; 轴流叶 片 30; 宽度 30a; 轴流送风作用区 31 ; 叶片部 32; 固定部 33 ; 驱动单元 40; 固定座 50; 第一座体 51 ; 第二座体 52; 凹槽 51 1、 521 ; 锁固件 60; 锁固孔 61 ; 筒型外箱 70; 入风口 71 ; 出风口 72; 支架 73。 具体实施方式  DESCRIPTION OF REFERENCE NUMERALS: composite impeller 1; casing 10; inlet 1 1; inner circumference 1 1a; outlet 12; width 12a; side plates 13, 14; centrifugal blade 20; inner end 20a; centrifugal air supply zone 21; Axial flow blade 30; width 30a; axial flow air supply zone 31; blade portion 32; fixing portion 33; drive unit 40; fixing base 50; first body 51; second base 52; groove 51 1 , 521 ; lock 60; locking hole 61; cylindrical outer case 70; air inlet 71; air outlet 72; bracket 73. detailed description
为使本发明更加明确详实, 兹列举较佳实施例并配合下列附图, 将本发明 的结构及其技术特征详述如后:  In order to make the present invention clearer and more detailed, the structure of the present invention and its technical features are detailed as follows with reference to the following drawings:
参考图 1至图 7 ,详细说明本发明的较佳实施内容。在本发明的说明中,「轴 向方向」 是平行旋转轴的方向, 「径向方向」 是垂直旋转轴的方向。  DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS Referring to Figures 1 through 7, a preferred embodiment of the present invention will be described in detail. In the description of the present invention, the "axial direction" is the direction of the parallel rotation axis, and the "radial direction" is the direction of the vertical rotation axis.
如图 1所示,复合式叶轮 1具有配置在中心轴 X周围且固接在机壳 10内侧 的多个离心叶片 20及配置在中心轴 X外围且固接在机壳 10径向外周围的多个 轴流叶片 30。 所谓的离心叶片通过旋转而使空气朝中心轴 X (叶轮的旋转中心 轴) 的放射方向排出的叶片结构。 此外, 所谓的轴流叶片通过旋转而使空气朝 与中心轴 X (叶轮的旋转中心轴)相平行的方向排出的叶片结构。 As shown in FIG. 1, the composite impeller 1 has a plurality of centrifugal blades 20 disposed around the central axis X and fixed to the inside of the casing 10, and is disposed at the periphery of the central axis X and fixed to the radially outer periphery of the casing 10. A plurality of axial flow vanes 30. The so-called centrifugal blade rotates to make the air toward the central axis X (the center of rotation of the impeller) The blade structure of the shaft is discharged in the radial direction. Further, the so-called axial flow vane is rotated to cause the air to be discharged toward the blade structure in a direction parallel to the central axis X (the rotational center axis of the impeller).
有关本发明的复合式叶轮 1结合离心及轴流的混流式叶轮, 通过图 1所示 的离心叶片 20与轴流叶片 30的同步旋转, 从复合式叶轮 1的前侧吸入空气, 并经离心气流与轴流气流的混合后,再朝后侧送出而产生中心轴 X方向的气流。 在以下说明的中心轴 X方向中 , 吸入空气侧的图 1中的前侧称为 r吸气侧 J , 排出空气侧的图 1 中的后侧称为 「排气侧」 。 相较于现有技术内容, 可实现在 相同的转速下提供更加的风量、 风压。  The composite impeller 1 of the present invention incorporates a centrifugal and axial flow mixed-flow impeller, and the air is sucked from the front side of the composite impeller 1 by centrifugal rotation of the centrifugal vane 20 and the axial flow vane 30 shown in FIG. After the airflow is mixed with the axial flow, it is sent to the rear side to generate a flow in the direction of the central axis X. In the central axis X direction described below, the front side in Fig. 1 on the suction air side is referred to as the r intake side J, and the rear side in Fig. 1 on the discharge air side is referred to as the "exhaust side". Compared with the prior art, it is possible to provide more air volume and wind pressure at the same rotational speed.
如图 1至图 4所示, 复合式叶轮 1 包含一机壳 10、 多个离心叶片 20、 多个 轴流叶片 30以及一驱动单元 40。  As shown in Figs. 1 to 4, the composite impeller 1 includes a casing 10, a plurality of centrifugal blades 20, a plurality of axial flow blades 30, and a drive unit 40.
该机壳 10在中心轴 X延伸的方向(轴向方向)的一侧, 设有一进口 1 1 , 而在 中心轴 X的径向方向周围, 设有多个出口 12。  The casing 10 is provided with an inlet 1 1 on one side in the direction (axial direction) in which the center axis X extends, and a plurality of outlets 12 are provided around the radial direction of the center axis X.
多个离心叶片 20以中心轴 X作为中心并于圓周方向以均匀地排列在中心轴 X周围, 且固接在该机壳 10的内表面, 通过使该多个离心叶片 20以中心轴 X 作为中心并于图 4中的逆时针旋转 (如图 4中的箭头 R1的方向), 而产生将空气 由该机壳 10的进口 1 1吸入而从该多个离心叶片 20彼此之间将空气往离心方向 送出, 而从该出口 12将空气排出的离心气流(亦即自图 3、 4中的由该复合式叶 轮 1的前侧吸入空气,并经离心叶片 20再朝中心轴 X放射状地送出离心气流), 其中, 该多个离心叶片 20的旋转动程的范围界定形成一离心送风作用区 21。 于 本实施例中, 该机壳 10的进口 1 1的内周缘 1 1a的直径大于该离心叶片 20的内 端 20a的直径。  The plurality of centrifugal blades 20 are centered on the central axis X and uniformly arranged around the central axis X in the circumferential direction, and are fixed to the inner surface of the casing 10 by using the plurality of centrifugal blades 20 as the central axis X The center is rotated counterclockwise in FIG. 4 (as in the direction of arrow R1 in FIG. 4), and air is drawn from the inlet 11 of the casing 10 to move air from the plurality of centrifugal blades 20 to each other. The centrifugal airflow is sent out in the centrifugal direction, and the air is discharged from the outlet 12 (i.e., the air is taken in from the front side of the composite impeller 1 in Figs. 3 and 4, and is radially sent out through the centrifugal blade 20 toward the central axis X. The centrifugal airflow), wherein the range of the rotational motion of the plurality of centrifugal blades 20 is defined to form a centrifugal air supply zone 21. In the present embodiment, the diameter of the inner circumference 11a of the inlet 11 of the casing 10 is larger than the diameter of the inner end 20a of the centrifugal blade 20.
多个轴流叶片 30以中心轴 X作为中心且放射线状地均匀配置在该机壳的径 向周围,通过使多个轴流叶片 30以中心轴 X作为中心并于图 4中的逆时针旋转 (如图 4中的箭头 R1的方向), 而产生沿着中心轴 X方向的气流(亦即自图 3、 4 中的由该复合式叶轮 1的前侧吸入空气, 并经轴流叶片 30再朝向后侧送出轴流 气流) , 其中, 该多个轴流叶片 30的旋转动程的范围界定形成一轴流送风作用 区 31。  The plurality of axial flow vanes 30 are centered around the central axis X and radially uniformly disposed around the radial direction of the casing, by rotating the plurality of axial flow vanes 30 with the central axis X as the center and counterclockwise in FIG. (as in the direction of arrow R1 in Fig. 4), an air flow is generated along the central axis X direction (i.e., from the front side of the composite impeller 1 in Figs. 3, 4, and through the axial flow vanes 30). The axial flow is sent toward the rear side, wherein the range of the rotational motion of the plurality of axial blades 30 defines an axial flow supply zone 31.
该驱动单元 40由马达构成, 并配至于该机壳 10设进口 1 1的相对另一侧, 且与该机壳 10连接, 并且以中心轴 X作为中心驱动该机壳 10往逆时针方向(如 图 4中的箭头 R1的方向)旋转, 以使该多个离心叶片 20及该多个轴流叶片 30 同步旋转。 此外, 该机壳 10具有覆盖该多个离心叶片 20的两侧的一对侧板 13、 14, 并且于该对侧板 13、 14中的一侧板 13设有该进口 1 1, 于该对侧板 13、 14间的 且位于该多个离心叶片 20外周侧设有该多个出口。 The driving unit 40 is composed of a motor and is disposed on the opposite side of the casing 10 and disposed on the opposite side of the casing 10, and is connected to the casing 10, and drives the casing 10 counterclockwise with the central axis X as a center ( Rotation in the direction of the arrow R1 in FIG. 4 to rotate the plurality of centrifugal blades 20 and the plurality of axial flow blades 30 in synchronization. Further, the casing 10 has a pair of side plates 13, 14 covering both sides of the plurality of centrifugal blades 20, and the inlet plate 1 is provided in one of the pair of side plates 13, 14 The plurality of outlets are provided between the side plates 13 and 14 and on the outer peripheral side of the plurality of centrifugal blades 20.
如图 3所示, 该机壳 10的出口 1 1连通于该离心送风作用区 21及该轴流送 风作用区 31。  As shown in Fig. 3, the outlet 11 of the casing 10 communicates with the centrifugal air supply zone 21 and the axial air supply zone 31.
如图 2所示, 各轴流叶片 30包含一叶片部 32及一固定部 33 , 并且利用一 固定座 50固定于该机壳 10的径向周围上, 该固定座 50包含一第一座体 51及 一第二座体 52 , 且该第一座体 51与该第二座体 52可相互对应锁合, 又该第一 座体 51与该第二座体 52内部分别设有一相互对应的凹槽 51 1、 521 , 供可夹设 各轴流叶片 30的固定部 33。其中各轴流叶片 30的固定部 33的截面形状可为圆 形或多边形且对应于该第一座体 51与该第二座体 52的凹槽 51 1、 521形状, 使 该固定部 33可紧密嵌合在该第一座体 51与该第二座体 52的凹槽 51 1、521中。 如图 5所示, 各轴流叶片 30末端的宽度 30a (亦即叶片部 32近固定部 33处的 宽度) 大于或等于该机壳 10的出口 12在中心轴 X轴向方向上的宽度 12a。  As shown in FIG. 2, each of the axial flow blades 30 includes a blade portion 32 and a fixing portion 33, and is fixed to a radial periphery of the casing 10 by a fixing base 50. The fixing base 50 includes a first seat. The first base body 51 and the second base body 52 are respectively correspondingly coupled to each other, and the first base body 51 and the second base body 52 are respectively provided with a corresponding one. The grooves 51 1 and 521 are provided for fixing portions 33 of the respective axial flow vanes 30. The cross-sectional shape of the fixing portion 33 of each of the axial flow blades 30 may be circular or polygonal and corresponding to the shapes of the grooves 51 1 and 521 of the first base body 51 and the second base body 52, so that the fixing portion 33 can be The first seat body 51 and the recesses 51 1 and 521 of the second seat body 52 are tightly fitted. As shown in FIG. 5, the width 30a of the end of each axial blade 30 (that is, the width of the blade portion 32 near the fixed portion 33) is greater than or equal to the width 12a of the outlet 12 of the casing 10 in the axial direction of the central axis X. .
组装时, 可将各轴流叶片 30的固定部 33对应置入该第一座体 51与该第二 座体 52的凹槽 51 1、 521中, 再通过至少一锁固件 60如螺栓, 以分别穿设过机 壳 10、第一座体 51及第二座体 52上对应锁固件 60所设置的锁固孔 61而锁固, 使各轴流叶片 30与该机壳 10可稳固地锁固成一体。  When assembled, the fixing portion 33 of each of the axial flow vanes 30 can be correspondingly inserted into the recesses 51 1 and 521 of the first base body 51 and the second base body 52, and then passed through at least one fastener 60 such as a bolt. The locking holes 61 provided in the corresponding locking members 60 are locked on the casing 10, the first base 51 and the second base 52, so that the axial blades 30 and the casing 10 can be stably locked. Solidified.
此外, 各轴流叶片 30的固定部 33的底面上可设置一指示刻度(图未示), 供在安装各轴流叶片 30时可藉该指示刻度以辨识各轴流叶片 30的安装角度, 俾使各轴流叶片 30可简易定位于同一安装角度, 以增进安装轴流叶片 30的效 率及准确性。  In addition, an indication scale (not shown) may be disposed on the bottom surface of the fixing portion 33 of each of the axial flow vanes 30. The indication scale may be used to identify the installation angle of each axial flow vane 30 when the axial flow vanes 30 are mounted. The axial flow vanes 30 can be easily positioned at the same mounting angle to enhance the efficiency and accuracy of mounting the axial flow vanes 30.
如图 3及图 4所示, 当使该驱动单元 40逆时钟旋转时(如图 4中的箭头 R1 的方向旋转), 机壳 10、 多个离心叶片 20及多个轴流叶片 30形成一体而逆时钟 旋转, 借此, 可从复合式叶轮 1的前侧 (吸气侧) 吸入空气, 以使一部分空气 由该机壳 10的入口 1 1进入机壳 10内, 再随该多个离心叶片 20旋转, 而朝机 壳 10的出口 12排出(亦即而由多个离心叶片 20的外周側朝中心轴 X的放射方 向送出),而形成一离心气流,也就是在该离心送风作用区 21形成一离心气流, 此离心气流中至少一部分气流进入该轴流送风作用区 31, 也就是进入两轴流叶 片 30之间, 而与该轴流气流混合, 且该至少一部分的离心气流同时受到该多个 轴流叶片 30转动推挤, 然后, 此受转动推挤的气流被加速地朝与中心轴 X方向 平行的方向的该复合式叶轮 1后侧 (排气侧) 送出; 而另一部分空气通过多个 轴流叶片 30且随该多个轴流叶片 30旋转排出, 而形成一轴流气流, 也就是在 该轴流送风作用区 31形成一轴流气流, 此轴流气流中至少一部分气流会与前述 通过机壳 10出口 12的至少一部分离心气流混合, 而一起被该多个轴流叶片 30 以朝与中心轴 X方向平行的方向的该复合式叶轮 1后侧 (排气側) 送出。 As shown in FIG. 3 and FIG. 4, when the driving unit 40 is rotated counterclockwise (rotating in the direction of the arrow R1 in FIG. 4), the casing 10, the plurality of centrifugal blades 20, and the plurality of axial flow blades 30 are integrated. And rotating counterclockwise, whereby air can be taken in from the front side (suction side) of the composite impeller 1 so that a part of the air enters the casing 10 from the inlet 11 of the casing 10, and then with the plurality of centrifugations. The blade 20 rotates and is discharged toward the outlet 12 of the casing 10 (i.e., is sent from the outer peripheral side of the plurality of centrifugal blades 20 toward the central axis X) to form a centrifugal air flow, that is, in the centrifugal air supply. The zone 21 forms a centrifugal gas stream into which at least a portion of the gas stream enters the axial flow supply zone 31, i.e., between the two axial flow vanes 30, and is mixed with the axial flow, and the at least a portion of the centrifugal flow At the same time, the plurality of axial flow vanes 30 are rotated and pushed, and then the air flow pushed by the rotation is accelerated toward the central axis X direction. The rear side (exhaust side) of the composite impeller 1 in the parallel direction is sent out; and the other part of the air passes through the plurality of axial flow vanes 30 and is rotated out along with the plurality of axial flow vanes 30 to form an axial flow, that is, Forming an axial flow in the axial flow supply zone 31, at least a portion of the axial flow being mixed with at least a portion of the centrifugal flow passing through the outlet 12 of the casing 10, together with the plurality of axial blades 30 The composite impeller 1 is sent to the rear side (exhaust side) in a direction parallel to the central axis X direction.
如图 6及图 7所示, 本发明的送风装置 2包含: 一筒型外箱 70 , 其内设有 该复合式叶轮 1, 其中该筒型外箱 70的两端分别为一入风口 71及出风口 72 , 并通过该复合式叶轮 1转动, 以驱使空气由该入风口 71进入, 再经由该复合式 叶轮 1的离心叶片 20及轴流叶片 30后, 再由该出风口 72送出 (如图 8中的箭 头所示) 。 此外, 该筒型外箱 70内可设置支架 73以供支承该驱动单元 40。  As shown in FIG. 6 and FIG. 7, the air blowing device 2 of the present invention comprises: a cylindrical outer casing 70, wherein the composite impeller 1 is disposed, wherein the two ends of the cylindrical outer casing 70 are respectively an air inlet. 71 and the air outlet 72, and the composite impeller 1 is rotated to drive air from the air inlet 71, and then through the centrifugal blade 20 and the axial flow blade 30 of the composite impeller 1, and then sent out by the air outlet 72 (as indicated by the arrow in Figure 8). Further, a bracket 73 may be disposed in the cylindrical outer casing 70 for supporting the drive unit 40.
借此, 本发明的复合式叶轮及其送风装置, 因为结合离心及轴流的叶片, 故, 故可提高送出的空气压力, 更由于具有较广面积的吸入侧, 因此, 可提高 气流量。  Therefore, the composite impeller and the air blowing device of the present invention can increase the pressure of the air to be sent by combining the blades of the centrifugal and axial flow, and further increase the air flow rate due to the suction side having a wider area. .
此外, 各轴流叶片 30设置于机壳 10的出口 12的外周侧, 借此, 由离心叶 片 20送出的空气, 流动至轴流叶片 30的距离变短, 因此, 因为可缩小空气的 压力损失, 可提高效率。  Further, each of the axial flow vanes 30 is provided on the outer peripheral side of the outlet 12 of the casing 10, whereby the distance of the air sent from the centrifugal vane 20 to the axial flow vanes 30 becomes short, and therefore, the pressure loss of the air can be reduced. , can improve efficiency.
此外, 该机壳 10的进口 1 1设置于其中一侧板 13中的中心轴 X側, 该侧板 13中除了进口 1 1以外的部份覆盖离心叶片 20的一外侧边, 借此, 可防止由离 心叶片 20的外周侧送出的空气由机壳 10的进口 11侧泄漏,因此,可提高效率。  Further, the inlet 11 of the casing 10 is disposed on the side of the central axis X of the one side plate 13, and a portion of the side plate 13 other than the inlet 11 covers an outer side of the centrifugal blade 20, whereby It is possible to prevent the air sent out from the outer peripheral side of the centrifugal blade 20 from leaking from the inlet 11 side of the casing 10, and therefore, the efficiency can be improved.
以上所述仅为本发明的优选实施例, 对本发明而言仅是说明性的, 而非限 制性的; 本领域普通技术人员理解, 在本发明权利要求所限定的精神和范围内 可对其进行许多改变, 修改, 甚至等效变更, 但都将落入本发明的保护范围内。  The above are only the preferred embodiments of the present invention, and are intended to be illustrative, and not restrictive, and those of ordinary skill in the art will understand that within the spirit and scope defined by the appended claims Many changes, modifications, and even equivalents may be made without departing from the scope of the invention.

Claims

权 利 要 求 Rights request
1、 一种复合式叶轮, 其特征在于, 包含: 1. A compound impeller, characterized in that it includes:
一机壳, 具有在旋转中心轴向方向的一进口, 及在该旋转中心轴的径向方 向的多个出口; A casing having an inlet in the axial direction of the rotation center and a plurality of outlets in the radial direction of the rotation center axis;
多个离心叶片, 均匀地排列在该旋转中心轴周围, 且固接在该机壳的内表 面, 并通过旋转而产生由该机壳的进口进入而由该多个出口排出的离心气流, 该多个离心叶片的旋转动程的范围界定形成一离心送风作用区; A plurality of centrifugal blades are evenly arranged around the central axis of rotation and fixed on the inner surface of the casing, and rotate to generate centrifugal airflow that enters from the inlet of the casing and is discharged from the plurality of outlets. The range of the rotational strokes of the plurality of centrifugal blades is defined to form a centrifugal air supply area;
多个轴流叶片, 以该旋转中心轴为中心且放射线状地均匀配置在该机壳的 径向周围, 并通过旋转而产生沿着该旋转中心轴向方向的轴流气流, 该多个轴 流叶片的旋转动程的范围界定形成一轴流送风作用区; 以及 A plurality of axial flow blades are evenly arranged around the casing in a radial direction with the rotation center axis as the center and radially, and rotate to generate an axial flow airflow along the axial direction of the rotation center. The plurality of axes The range of the rotational motion of the flow blade is defined to form an axial flow air supply area; and
一驱动单元, 以该旋转中心轴为中心驱动该机壳旋转, 以使该多个离心叶 片及该多个轴流叶片同步旋转; A driving unit drives the casing to rotate with the rotation central axis as the center, so as to cause the plurality of centrifugal blades and the plurality of axial flow blades to rotate synchronously;
其中, 前述径向方向是垂直于该旋转中心轴; Wherein, the aforementioned radial direction is perpendicular to the central axis of rotation;
其中, 该机壳的出口连通于该离心送风作用区与该轴流送风作用区; 其中, 当该驱动单元驱使该多个离心叶片及该多个轴流叶片同步旋转时, 使该离心气流由该离心送风作用区通过该机壳的出口排出, 使其至少一部分的 离心气流进入该轴流送风作用区, 而与该轴流气流混合, 且该至少一部分的离 心气流同时受到该多个轴流叶片转动推挤而能加速地朝该旋转中心轴向方向流 动。 Wherein, the outlet of the casing is connected to the centrifugal air supply area and the axial flow air supply area; wherein, when the driving unit drives the plurality of centrifugal blades and the plurality of axial flow blades to rotate synchronously, the centrifugal air supply area is The airflow is discharged from the centrifugal air supply area through the outlet of the casing, so that at least a part of the centrifugal airflow enters the axial air supply area and mixes with the axial airflow, and at least a part of the centrifugal airflow is simultaneously affected by the The plurality of axial flow blades rotate and push to accelerate the flow in the axial direction of the rotation center.
2、 如权利要求 1所述的复合式叶轮, 其特征在于, 该机壳具有覆盖该多个 离心叶片的两侧的一对侧板, 并且于该对侧板中的一侧板设有该进口, 于该对 侧板间且位于该多离心叶片的外周侧设有该多个出口。 2. The compound impeller according to claim 1, wherein the casing has a pair of side plates covering both sides of the plurality of centrifugal blades, and one side plate of the pair of side plates is provided with the The inlet is provided with the plurality of outlets between the pair of side plates and located on the outer peripheral side of the multi-centrifugal blade.
3、 如权利要求 1所述的复合式叶轮, 其特征在于, 该机壳的出口连通于该 离心送风作用区及该轴流送风作用区。 3. The compound impeller according to claim 1, characterized in that the outlet of the casing is connected to the centrifugal air supply area and the axial air supply area.
4、 如权利要求 1所述的复合式叶轮, 其特征在于, 各轴流叶片末端的宽度 大于或等于该机壳的出口在该旋转中心轴的轴向方向上的宽度。 4. The compound impeller according to claim 1, wherein the width of each axial flow blade end is greater than or equal to the width of the outlet of the casing in the axial direction of the rotation central axis.
5、 如权利要求 1所述的复合式叶轮, 其特征在于, 该机壳的进口的内周缘 的直径大于该离心叶片的内端的直径。 5. The compound impeller according to claim 1, wherein the diameter of the inner peripheral edge of the inlet of the casing is larger than the diameter of the inner end of the centrifugal blade.
6、 如权利要求 1所述的复合式叶轮, 其特征在于, 各轴流叶片包含一叶片 部及一固定部, 并且利用一固定座固定于该机壳的径向周围上, 该固定座包含 一第一座体及一第二座体, 且该第一座体与该第二座体相互对应锁合, 该第一 座体与该第二座体内部分别设有一相互对应的凹槽, 供夹设各轴流叶片的固定 部。 6. The compound impeller according to claim 1, wherein each axial flow blade includes a blade part and a fixed part, and is fixed on the radial periphery of the casing using a fixed base, the fixed base includes A first base body and a second base body, and the first base body and the second base body are correspondingly locked with each other, the first base body A corresponding groove is provided inside the base body and the second base body respectively, for sandwiching the fixing portion of each axial flow blade.
7、 如权利要求 6所述的复合式叶轮, 其特征在于, 各轴流叶片的固定部的 截面形状为圆形或多边形。 7. The compound impeller according to claim 6, wherein the cross-sectional shape of the fixed portion of each axial flow blade is circular or polygonal.
8、 如权利要求 6所述的复合式叶轮, 其特征在于, 进一步利用至少一锁固 件, 以分别穿设过该机壳、 该第一座体及该第二座体上对应该锁固件设置的锁 固孔而锁固。 8. The composite impeller according to claim 6, further utilizing at least one locking member to pass through the casing, the first base body and the second base body respectively and set corresponding to the locking member. locking holes.
9、 一种送风装置, 其是于一筒型外箱内设有如权利要求 1至 8中任一项所 述的复合式叶轮, 其特征在于, 该筒型外箱的两端分别为一入风口及出风口, 并通过该复合式叶轮转动, 以驱使空气由该入风口进入再由该出风口送出。 9. An air supply device, which is provided with a composite impeller as claimed in any one of claims 1 to 8 in a cylindrical outer box, characterized in that the two ends of the cylindrical outer box are respectively The air inlet and the air outlet are rotated by the compound impeller to drive the air to enter from the air inlet and then be sent out from the air outlet.
10、 如权利要求 9所述的送风装置, 其特征在于, 该筒型外箱的内部进一 步设置一支承该驱动单元的支架。 10. The air supply device according to claim 9, characterized in that a bracket supporting the driving unit is further provided inside the cylindrical outer box.
PCT/CN2013/000088 2013-01-29 2013-01-29 Composite impeller and air supply device thereof WO2014117288A1 (en)

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