JPH07145798A - Impeller of axial blower - Google Patents
Impeller of axial blowerInfo
- Publication number
- JPH07145798A JPH07145798A JP29516493A JP29516493A JPH07145798A JP H07145798 A JPH07145798 A JP H07145798A JP 29516493 A JP29516493 A JP 29516493A JP 29516493 A JP29516493 A JP 29516493A JP H07145798 A JPH07145798 A JP H07145798A
- Authority
- JP
- Japan
- Prior art keywords
- blade
- impeller
- surface side
- blades
- negative pressure
- Prior art date
- Legal status (The legal status 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 status listed.)
- Pending
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/38—Blades
- F04D29/384—Blades characterised by form
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Air-Conditioning Room Units, And Self-Contained Units In General (AREA)
Abstract
Description
【0001】[0001]
【産業上の利用分野】本発明は、空気調和機などの送風
機に用いる軸流送風機の羽根車に関するものである。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an impeller of an axial blower used for a blower such as an air conditioner.
【0002】[0002]
【従来の技術】近年、空気調和機などの送風機は高性能
化・低騒音化への要求が高まり、羽根板の表面形状、羽
根板の断面形状の改良など、種々の羽根車の性能向上方
法が提案されている。2. Description of the Related Art In recent years, blowers such as air conditioners have been required to have higher performance and lower noise, and various methods for improving the performance of impellers such as improving the surface shape of the vane and the cross-sectional shape of the vane. Is proposed.
【0003】従来の送風機に用いる軸流送風機の羽根車
としては、実開昭63−160400号公報に示される
ているものがある。An impeller of an axial blower used for a conventional blower is disclosed in Japanese Utility Model Laid-Open No. 63-160400.
【0004】以下、図面を参照しながら、上述した従来
の軸流送風機の羽根車について説明する。Hereinafter, the impeller of the conventional axial flow fan described above will be described with reference to the drawings.
【0005】図8は従来の軸流送風機の羽根車の構造
を、図9は図8の軸流送風機の羽根車のA−A’線要部
断面図を、図10は従来の軸流送風機羽根車の羽根負圧
面側要部拡大図を示すものである。図において1は羽根
車であり、羽根車1はハブ2とハブ2の周囲に設けられ
た複数の羽根3とからなり、羽根3の負圧面側3aに
は、気流Fの流れ方向に対して上流側部分に気流の境界
層を乱流境界層に遷移させる凹凸状の剥離防止部4を、
気流Fの流れ方向と直行する方向に沿って凹凸状に形成
している。FIG. 8 shows the structure of an impeller of a conventional axial flow fan, FIG. 9 is a sectional view of the main part of the impeller of the axial flow fan of FIG. 8 taken along the line AA ', and FIG. 10 is a conventional axial flow fan. It is a figure which shows the blade negative pressure surface side main part enlarged view of an impeller. In the figure, 1 is an impeller, and the impeller 1 is composed of a hub 2 and a plurality of blades 3 provided around the hub 2, and a suction surface side 3 a of the blade 3 has a direction of flow of an air flow F. An uneven separation preventing portion 4 for transitioning the boundary layer of the airflow to a turbulent boundary layer is provided on the upstream side portion,
It is formed in an uneven shape along a direction orthogonal to the flow direction of the air flow F.
【0006】以上のように構成された軸流型の送風機に
ついて以下その動作を説明する。まず、モータ(図示せ
ず)の駆動力によって羽根車1が所定の回転方向に回転
すると、空気が羽根車1内に流入され、複数の羽根3の
間を通過する際に静圧と動圧を付加され羽根車1から外
に吐出され送風作用を為す。The operation of the axial-flow type blower configured as described above will be described below. First, when the impeller 1 is rotated in a predetermined rotation direction by the driving force of a motor (not shown), air is introduced into the impeller 1 and static pressure and dynamic pressure are applied when passing between the plurality of blades 3. Is added and is discharged to the outside from the impeller 1 to perform an air blowing action.
【0007】このとき、羽根3の負圧面側3aには気流
Fの流れ方向に対して上流側部分の凹凸状の剥離防止部
4によって羽根3の負圧面側3aに沿って流れる気流F
の境界層を乱流境界層に遷移させるとともに、剥離防止
部4を気流Fの流れ方向と直行する方向に沿って凹凸状
に形成することにより、気流Fの流れ方向と直行する方
向で各気流間に位相差を設け、羽根3の負圧面側3aに
沿って流れる気流Fを効果的に乱流境界層に遷移させ、
羽根3の負圧面側3aにおける気流Fの流れ方向に対し
て下流側部分で気流Fの境界層に剥離流が形成されるこ
とを効果的に防止し、送風能力の低下と乱流騒音の増加
を抑えることができる。At this time, on the suction surface side 3a of the blade 3, the air flow F flowing along the suction surface side 3a of the blade 3 by the uneven separation preventing portion 4 on the upstream side with respect to the flow direction of the air flow F.
The boundary layer is changed to a turbulent boundary layer, and the separation preventing portion 4 is formed in an uneven shape along the direction orthogonal to the flow direction of the air flow F, so that each air flow in the direction orthogonal to the flow direction of the air flow F. By providing a phase difference therebetween, the airflow F flowing along the suction surface side 3a of the blade 3 is effectively transitioned to the turbulent boundary layer,
Effectively preventing the separation flow from being formed in the boundary layer of the airflow F in the downstream side with respect to the flow direction of the airflow F on the negative pressure surface side 3a of the blade 3, lowering the blowing capacity and increasing turbulent noise. Can be suppressed.
【0008】[0008]
【発明が解決しようとする課題】しかしながら、上記の
ような構成では、羽根3の負圧面側に剥離防止部4を設
けることによる羽根3の負圧面側3aを流れる気流Fの
剥離を抑制する効果は、羽根3の負圧面側3aに沿って
を流れる気流Fが剥離防止部4まで剥離することなく流
れる必要があり、設計条件よりも静圧付加が大きい場合
には、羽根3の負圧面側3aに沿って流れる気流Fが剥
離防止部4までに剥離してしまい、非常に限定された使
用範囲内でしか狙いとする効果が得られないという課題
を有していた。However, in the above structure, the effect of suppressing the separation of the air flow F flowing on the suction surface side 3a of the blade 3 by providing the separation prevention portion 4 on the suction surface side of the blade 3. Requires that the air flow F flowing along the suction surface side 3a of the blade 3 flows to the separation preventing portion 4 without separation, and when the static pressure addition is larger than the design condition, the suction surface side of the blade 3 is There was a problem that the airflow F flowing along 3a was separated up to the separation prevention part 4, and the desired effect could be obtained only within a very limited use range.
【0009】本発明は上記課題に鑑み、高静圧条件下で
使用される場合などに、羽根負圧面側を沿って流れる気
流が剥離することを抑制し、送風能力の低下と乱流騒音
の増加を抑えることができる軸流送風機の羽根車を提供
するものである。In view of the above problems, the present invention suppresses separation of the airflow flowing along the blade negative pressure surface side when used under a high static pressure condition, thereby lowering the blowing capacity and reducing turbulent noise. An impeller of an axial blower capable of suppressing the increase is provided.
【0010】[0010]
【課題を解決するための手段】この課題を解決するため
に、本発明の軸流送風機の羽根車は、モータと、前記モ
ータに取り付けられたハブと、前記ハブの周囲に設けら
れた複数の第1の羽根と、前記ハブの周囲に設けられ、
前記第1の羽根の気流の流れ方向上流側に位置し、前記
第1の羽根の翼弦長より短い複数の第2の羽根とで羽根
車を構成し、前記第2の羽根の後縁を前記第1の羽根の
負圧面側前縁近傍に設け、近接した前記第1の羽根と前
記第2の羽根とが1つの翼を形成しているものである。In order to solve this problem, an impeller of an axial blower according to the present invention comprises a motor, a hub attached to the motor, and a plurality of hubs provided around the hub. A first vane and is provided around the hub,
A plurality of second blades, which are located on the upstream side in the flow direction of the air flow of the first blades and are shorter than the chord length of the first blades, constitute an impeller, and a trailing edge of the second blades is formed. It is provided in the vicinity of the front edge of the first blade on the suction surface side, and the first blade and the second blade which are adjacent to each other form one blade.
【0011】さらに、他の発明の軸流送風機の羽根車
は、略同心円上に位置し、第1の羽根と第2の羽根とを
連結する複数の連結板を設けたものである。Further, an impeller of an axial blower according to another invention is provided with a plurality of connecting plates which are located on substantially concentric circles and which connect the first blade and the second blade.
【0012】[0012]
【作用】本発明の軸流送風機の羽根車では、第1の羽根
の負圧面側の気流の流れ方向上流側に第2の羽根を配置
し、第2の羽根の後縁を第1の羽根の負圧面側前縁近傍
に設けて、第1の羽根と第2の羽根とが1つの翼を形成
しているので、第2の羽根により偏向された気流は第1
の羽根の負圧面側の気流境界層の安定的な成長に役立
ち、第1の羽根の前縁部から後縁部まで気流が剥離する
ことなく流れるため、送風能力の低下と乱流騒音の増加
を抑える。In the impeller of the axial blower according to the present invention, the second blade is arranged on the suction side of the first blade on the upstream side in the flow direction of the air flow, and the trailing edge of the second blade is the first blade. Since the first blade and the second blade form one blade provided near the front edge of the negative pressure surface side, the airflow deflected by the second blade is
This helps the stable growth of the airflow boundary layer on the suction surface side of the blade, and the airflow flows from the leading edge to the trailing edge of the first blade without separation, resulting in a reduction in the blowing capacity and an increase in turbulent noise. Suppress.
【0013】さらに、他の発明の軸流送風機の羽根車で
は、略同心円上に位置し、第1の羽根と第2の羽根とを
連結する複数の連結板を設けているので、羽根車内に流
入した気流が羽根車外周側に向かって流れるのを羽根吐
出側への流れに偏向させるため、送風能力の向上と乱流
騒音の増加を抑え、さらに、羽根車の一体成型がしやす
くなり、羽根車の強度も増加する。Further, in the impeller of the axial blower according to another invention, since a plurality of connecting plates are provided which are located on substantially concentric circles and connect the first blade and the second blade, the impeller is provided in the impeller. Since the inflowing airflow is deflected toward the outer peripheral side of the impeller to the flow toward the discharge side of the impeller, it improves the blowing capacity and suppresses the increase of turbulent noise, and further, the impeller can be easily integrally molded, The strength of the impeller also increases.
【0014】[0014]
【実施例】以下、本発明による軸流送風機の羽根車の第
1の実施例について図面を参照しながら説明する。尚、
従来例と同一構成の部分については重複を避ける為、同
一の符号を付けて説明を省略する。DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS A first embodiment of an impeller of an axial blower according to the present invention will be described below with reference to the drawings. still,
In order to avoid duplication, the parts having the same configurations as those of the conventional example are denoted by the same reference numerals and the description thereof will be omitted.
【0015】図1、図2は、本発明の第1の実施例にお
ける軸流送風機の羽根車の構造を示すものであり、図3
は、図1の軸流送風機の羽根車のB−B’線断面図を示
すものである。1 and 2 show the structure of an impeller of an axial flow fan according to the first embodiment of the present invention.
[Fig. 2] is a cross-sectional view of the impeller of the axial blower of Fig. 1 taken along the line BB '.
【0016】図において、5は軸流送風機の羽根車で、
モータ6と、モータ6に取り付けられたハブ2と、ハブ
2の周囲に設けられた複数の第1の羽根7と、ハブ2の
周囲に設けられ、第1の羽根7の気流の流れ方向上流側
に位置し、第1の羽根7の翼弦長より短い複数の第2の
羽根8とで羽根車を構成し、第2の羽根8の後縁8aを
第1の羽根7の負圧面側7aの前縁7b近傍に設け、近
接した第1の羽根7と前記第2の羽根8とが1つの翼を
形成している。Gは、第1の羽根7の負圧面側7aに沿
って流れる気流を示すものである。In the figure, 5 is an impeller of an axial blower,
A motor 6, a hub 2 attached to the motor 6, a plurality of first blades 7 provided around the hub 2, and a plurality of first blades 7 provided around the hub 2 and upstream of the airflow of the first blade 7 And a plurality of second blades 8 located on the side of the first blades 7 and having a chord length shorter than the chord length of the first blades 7, and the trailing edge 8a of the second blades 8 is located on the suction surface side of the first blades 7. The first blade 7 and the second blade 8 which are provided in the vicinity of the front edge 7b of 7a and are adjacent to each other form one blade. G indicates an airflow flowing along the suction surface side 7a of the first blade 7.
【0017】以上のように構成された軸流送風機の羽根
車について以下その動作を説明する。The operation of the impeller of the axial blower configured as above will be described below.
【0018】まず、モータ6の駆動力によって羽根車5
が所定の回転方向に回転すると、空気が羽根車5内に流
入され、複数の第1の羽根7と第2の羽根8からなる翼
の間を通過する際に静圧と動圧を付加され羽根車5から
外に吐出され送風作用を為す。First, the impeller 5 is driven by the driving force of the motor 6.
Is rotated in a predetermined rotation direction, air is introduced into the impeller 5 and static pressure and dynamic pressure are added when passing between the blades composed of the plurality of first blades 7 and the second blades 8. It is discharged to the outside from the impeller 5 and acts as an air blower.
【0019】ここで、第1の羽根7の負圧面側7aの気
流Gの流れ方向上流側に第2の羽根8を配置し、第2の
羽根8の後縁8aを第1の羽根7の負圧面側7aの前縁
7b近傍に設けて、近接した第1の羽根7と第2の羽根
8とが1つの翼となるよう形成しているので、高静圧条
件下で使用される場合など、羽根車の設計条件以外にお
いても、第2の羽根8の加圧面側8bで偏向された気流
Gは、第1の羽根7の前縁7bから負圧面側7aに流れ
込み、第1の羽根7の負圧面側7aでの境界層の成長を
安定的なものとして、第1の羽根7の前縁部7bから後
縁部7cまで気流Gの剥離を抑制するため、送風能力の
低下と乱流騒音の増加を抑えることを可能とする。Here, the second blade 8 is disposed on the suction side 7a of the first blade 7 on the upstream side in the flow direction of the air flow G, and the trailing edge 8a of the second blade 8 is located on the first blade 7. It is provided in the vicinity of the front edge 7b on the negative pressure surface side 7a, and the first blade 7 and the second blade 8 which are adjacent to each other are formed as one blade, so that it is used under a high static pressure condition. The airflow G deflected by the pressure surface side 8b of the second blade 8 flows into the suction surface side 7a from the front edge 7b of the first blade 7 even under conditions other than the design condition of the impeller, such as the first blade. The growth of the boundary layer on the suction surface side 7a of No. 7 is made stable, and the separation of the air flow G from the front edge 7b to the rear edge 7c of the first blade 7 is suppressed. It is possible to suppress the increase of flow noise.
【0020】以上のように本実施例によれば、第1の羽
根7の負圧面側7aの気流Gの流れ方向上流側に第2の
羽根8を配置し、第2の羽根8の後縁8aを第1の羽根
7の負圧面側7aの前縁7b近傍に設け、第1の羽根7
と第2の羽根8とが1つの翼を形成しているので、第2
の羽根8により偏向された気流Gが第1の羽根7の負圧
面側7aの気流境界層の安定的な成長に役立ち、気流G
が剥離することなく流れるため、送風能力の低下と乱流
騒音の増加を抑える。As described above, according to this embodiment, the second blade 8 is arranged upstream of the suction surface side 7a of the first blade 7 in the flow direction of the air flow G, and the trailing edge of the second blade 8 is arranged. 8a is provided in the vicinity of the front edge 7b on the suction surface side 7a of the first blade 7 and
Since the second blade 8 and the second blade 8 form one blade,
The airflow G deflected by the blades 8 of the first blade 7 helps the stable growth of the airflow boundary layer on the suction surface side 7a of the first blade 7,
Since the air flows without being separated, it suppresses a decrease in the blowing capacity and an increase in turbulent noise.
【0021】従って、第1の羽根7の負圧面側7aに沿
って流れる気流Gが剥離することを防止し、送風能力の
低下と乱流騒音の増加を効果的に抑えることができる。Therefore, it is possible to prevent the airflow G flowing along the negative pressure surface side 7a of the first blade 7 from being separated, and to effectively suppress the reduction of the blowing capacity and the increase of the turbulent noise.
【0022】以下、本発明による軸流送風機の羽根車の
第2の実施例について図面を参照しながら説明する。A second embodiment of the impeller of the axial blower according to the present invention will be described below with reference to the drawings.
【0023】図4、図5は、本発明の第2の実施例にお
ける軸流送風機の羽根車の構造を示すものであり、図6
は、本発明の第2の実施例における軸流送風機の羽根車
の羽根負圧面側要部拡大図を、図7は、図4の軸流送風
機の羽根車のD−D’線断面図を示すものである。4 and 5 show the structure of the impeller of the axial blower according to the second embodiment of the present invention.
FIG. 7 is an enlarged view of an essential part of a blade negative pressure surface side of an impeller of an axial flow fan according to a second embodiment of the present invention, and FIG. 7 is a sectional view taken along line DD ′ of the impeller of the axial flow fan of FIG. 4. It is shown.
【0024】図において、第1の実施例と異なるのは、
略同心円上に位置し、第1の羽根7と第2の羽根8とを
連結する複数の連結板10を設けた点である。In the figure, the difference from the first embodiment is that
The point is that a plurality of connecting plates 10 that connect the first blade 7 and the second blade 8 are provided on substantially concentric circles.
【0025】以上のように構成された軸流送風機の羽根
車について以下その動作を説明する。The operation of the impeller of the axial blower configured as above will be described below.
【0026】まず、モータ6の駆動力によって羽根車9
が所定の回転方向に回転すると、空気が羽根車9内に流
入され、複数の第1の羽根7と第2の羽根8からなる翼
の間を通過する際に静圧と動圧を付加され羽根車9から
外に吐出され送風作用を為す。First, the impeller 9 is driven by the driving force of the motor 6.
Is rotated in a predetermined rotation direction, air is introduced into the impeller 9 and static pressure and dynamic pressure are added when passing between the blades composed of the plurality of first blades 7 and the second blades 8. The air is discharged from the impeller 9 and functions as an air blower.
【0027】ここで、略同心円上に位置し、第1の羽根
7と第2の羽根8とを連結する複数の連結板10を設け
ているので、羽根車9内に流入した気流Hが羽根車外周
側に向かって流れるのを連結板10により羽根吐出側へ
の流れに偏向されるため送風能力の向上と乱流騒音の増
加を抑え、さらに、羽根車9の一体成型がしやすくな
り、羽根車9の強度も増加する。Since a plurality of connecting plates 10 for connecting the first blade 7 and the second blade 8 are provided on the substantially concentric circles, the air flow H flowing into the impeller 9 is a blade. Since the flow toward the outer peripheral side of the vehicle is deflected by the connecting plate 10 to the flow toward the blade discharge side, the improvement of the blowing capacity and the increase of turbulent noise are suppressed, and further, the impeller 9 is easily molded integrally. The strength of the impeller 9 also increases.
【0028】以上のように本実施例によれば、略同心円
上に位置し、第1の羽根7と第2の羽根8とを連結する
複数の連結板10を設けることにより、羽根車9内に流
入した気流Hが羽根車9の外周側に向かって流れるのを
羽根吐出側への流れに偏向されるため送風能力の向上と
乱流騒音の増加を抑え、さらに、羽根車9の一体成型が
しやすくなり、羽根車9の強度も増加する。As described above, according to this embodiment, the inside of the impeller 9 is provided by providing the plurality of connecting plates 10 which are located on substantially concentric circles and which connect the first blade 7 and the second blade 8. The airflow H flowing into the blade is deflected toward the outer peripheral side of the impeller 9 so as to be deflected to the blade discharge side, so that the blowing ability is improved and turbulent noise is prevented from increasing, and the impeller 9 is integrally molded. It becomes easier to remove, and the strength of the impeller 9 also increases.
【0029】従って、羽根車9への流入気流の偏向によ
る送風能力向上と乱流騒音増加を抑え、羽根車9の成型
性・強度の向上を図ることができる。Therefore, it is possible to improve the blowing ability and the increase of turbulent noise due to the deflection of the inflow airflow to the impeller 9, and to improve the moldability and strength of the impeller 9.
【0030】[0030]
【発明の効果】以上のように本発明の軸流送風機の羽根
車は、モータと、前記モータに取り付けられたハブと、
前記ハブの周囲に設けられた複数の第1の羽根と、前記
ハブの周囲に設けられ、前記第1の羽根の負圧面側の気
流の流れ方向上流側に位置し、前記第1の羽根の翼弦長
より短い複数の第2の羽根とで羽根車を構成し、前記第
2の羽根の後縁を前記第1の羽根の負圧面側前縁近傍に
設け、近接した前記第1の羽根と前記第2の羽根とが1
つの翼を形成することにより、前記第2の羽根の加圧面
側で偏向された気流が前記第1の羽根の負圧面側の気流
境界層の安定的な成長に役立つため、前記第1の羽根の
負圧面側を沿って流れる気流が剥離することなく流れ、
送風能力の低下と乱流騒音の増加を抑えることができ
る。As described above, the impeller of the axial blower according to the present invention includes a motor, a hub attached to the motor,
A plurality of first blades provided around the hub; and a plurality of first blades provided around the hub and located upstream of the negative pressure surface side of the first blades in the flow direction of the air flow. An impeller is constituted by a plurality of second blades having a shorter chord length, a trailing edge of the second blade is provided in the vicinity of a suction surface side front edge of the first blade, and the first blade is in close proximity. And the second blade is 1
By forming two blades, the airflow deflected on the pressure surface side of the second blade helps the stable growth of the airflow boundary layer on the suction surface side of the first blade, and thus the first blade is formed. The airflow flowing along the negative pressure surface side of the
It is possible to suppress a decrease in the blowing capacity and an increase in turbulent noise.
【0031】さらに、略同心円上に位置し、第1の羽根
と第2の羽根とを連結する複数の連結板を設けることに
より、羽根車内に流入した気流が前記羽根車の外周側に
向かって流れるのを前記連結板で前記羽根吐出側への流
れに偏向されるため、送風能力の向上と乱流騒音の増加
を抑え、さらに、羽根車の一体成型を容易とし、前記羽
根車の強度も増加させることができる。Further, by providing a plurality of connecting plates located on substantially concentric circles and connecting the first blade and the second blade, the airflow flowing into the impeller is directed toward the outer peripheral side of the impeller. Since the flow is deflected by the connecting plate to the flow toward the blade discharge side, the improvement of the blowing capacity and the increase of turbulent noise are suppressed, and further, the integral molding of the impeller is facilitated and the strength of the impeller is increased. Can be increased.
【図1】本発明の第1の実施例における軸流送風機の羽
根車の平面図FIG. 1 is a plan view of an impeller of an axial blower according to a first embodiment of the present invention.
【図2】本発明の第1の実施例における軸流送風機の羽
根車の断面図FIG. 2 is a sectional view of an impeller of an axial blower according to the first embodiment of the present invention.
【図3】図1の軸流送風機の羽根車のB−B’線要部断
面図FIG. 3 is a cross-sectional view of the main part of the impeller of the axial blower of FIG. 1 taken along the line BB ′.
【図4】本発明の第2の実施例における軸流送風機の羽
根車の平面図FIG. 4 is a plan view of an impeller of an axial blower according to a second embodiment of the present invention.
【図5】本発明の第2の実施例における軸流送風機の羽
根車の断面図FIG. 5 is a sectional view of an impeller of an axial blower according to a second embodiment of the present invention.
【図6】本発明の第2の実施例における軸流送風機の羽
根車の羽根要部拡大図FIG. 6 is an enlarged view of a main portion of an impeller of an axial blower according to a second embodiment of the present invention.
【図7】図4の軸流送風機の羽根車のC−C’線要部断
面図FIG. 7 is a cross-sectional view of the main part of the impeller of the axial blower of FIG. 4 taken along the line CC ′.
【図8】従来の軸流送風機の羽根車の斜視図FIG. 8 is a perspective view of an impeller of a conventional axial blower.
【図9】図8の軸流送風機の羽根車のA−A’線要部断
面図9 is a cross-sectional view of the main part of the impeller of the axial blower of FIG. 8 taken along the line AA ′.
【図10】従来の軸流送風機羽根車の羽根負圧面側要部
拡大図FIG. 10 is an enlarged view of a blade negative pressure surface side main part of a conventional axial blower impeller.
2 ハブ 5 羽根車 6 モータ 7 第1の羽根 8 第2の羽根 9 羽根車 10 連結板 2 hub 5 impeller 6 motor 7 first blade 8 second blade 9 impeller 10 connecting plate
Claims (2)
ハブと、前記ハブの周囲に設けられた複数の第1の羽根
と、前記ハブの周囲に設けられ、前記第1の羽根の気流
の流れ方向上流側に位置し、前記第1の羽根の翼弦長よ
り短い複数の第2の羽根とで羽根車を構成し、前記第2
の羽根の後縁を前記第1の羽根の負圧面側前縁近傍に設
け、近接した前記第1の羽根と前記第2の羽根とが1つ
の翼を形成する軸流送風機の羽根車。1. A motor, a hub attached to the motor, a plurality of first blades provided around the hub, and a flow of air flow of the first blade provided around the hub. A plurality of second blades located upstream in the direction and having a chord length shorter than the chord length of the first blade, and forming an impeller.
The impeller of an axial blower in which the trailing edge of the blade is provided in the vicinity of the suction-side front edge of the first blade, and the adjacent first blade and second blade form one blade.
の羽根とを連結する複数の連結板を設けた請求項第1記
載の軸流送風機の羽根車。2. The first vane and the second vane are located on substantially concentric circles.
The impeller of an axial blower according to claim 1, further comprising a plurality of connecting plates for connecting the blades of the fan.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP29516493A JPH07145798A (en) | 1993-11-25 | 1993-11-25 | Impeller of axial blower |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP29516493A JPH07145798A (en) | 1993-11-25 | 1993-11-25 | Impeller of axial blower |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH07145798A true JPH07145798A (en) | 1995-06-06 |
Family
ID=17817078
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP29516493A Pending JPH07145798A (en) | 1993-11-25 | 1993-11-25 | Impeller of axial blower |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH07145798A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7462014B2 (en) | 2002-09-27 | 2008-12-09 | Delta Eletronics, Inc. | Axial flow fan with multiple segment blades |
JP2010275986A (en) * | 2009-06-01 | 2010-12-09 | Mitsubishi Electric Corp | Fan and axial flow blower |
JP2012017750A (en) * | 2011-10-26 | 2012-01-26 | Mitsubishi Electric Corp | Axial fan and outdoor unit for air conditioner |
WO2013104513A1 (en) * | 2012-01-12 | 2013-07-18 | Ebm-Papst St. Georgen Gmbh & Co. Kg | Axial or diagonal fan with trip edge on the rotor blade suction side |
US20180149168A1 (en) * | 2015-06-11 | 2018-05-31 | Beijing Deepcool Industries Co., Ltd. | Heat dissipation fan |
IT202100020579A1 (en) * | 2021-07-30 | 2023-01-30 | Cofimco Srl | INDUSTRIAL AXIAL FAN |
-
1993
- 1993-11-25 JP JP29516493A patent/JPH07145798A/en active Pending
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7462014B2 (en) | 2002-09-27 | 2008-12-09 | Delta Eletronics, Inc. | Axial flow fan with multiple segment blades |
JP2010275986A (en) * | 2009-06-01 | 2010-12-09 | Mitsubishi Electric Corp | Fan and axial flow blower |
JP2012017750A (en) * | 2011-10-26 | 2012-01-26 | Mitsubishi Electric Corp | Axial fan and outdoor unit for air conditioner |
WO2013104513A1 (en) * | 2012-01-12 | 2013-07-18 | Ebm-Papst St. Georgen Gmbh & Co. Kg | Axial or diagonal fan with trip edge on the rotor blade suction side |
US20180149168A1 (en) * | 2015-06-11 | 2018-05-31 | Beijing Deepcool Industries Co., Ltd. | Heat dissipation fan |
US10954958B2 (en) * | 2015-06-11 | 2021-03-23 | Beijing Deepcool Industries Co., Ltd. | Heat dissipation fan |
IT202100020579A1 (en) * | 2021-07-30 | 2023-01-30 | Cofimco Srl | INDUSTRIAL AXIAL FAN |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
JP3204208B2 (en) | Mixed-flow blower impeller | |
JP3979388B2 (en) | Blower | |
WO2007114090A1 (en) | Multi-blade fan | |
JP3050144B2 (en) | Axial fan | |
JP3756079B2 (en) | Impeller, blower, and refrigerator-freezer | |
JP3598900B2 (en) | Impeller for blower | |
EP1210264B1 (en) | Centrifugal impeller with high blade camber | |
JP2000087898A (en) | Axial flow blower | |
JP4140236B2 (en) | Blower and outdoor unit for air conditioner | |
JP2669448B2 (en) | Centrifugal blower impeller | |
JPH10306796A (en) | Centrifugal sirocco fan | |
JPH07145798A (en) | Impeller of axial blower | |
JPH09195988A (en) | Multiblade blower | |
JPH03210093A (en) | Cross flow fan | |
JP2000018194A (en) | Impeller for blower | |
JP2002054596A (en) | Axial-flow fan | |
JPH08247090A (en) | Centrifugal blower | |
JP3938252B2 (en) | Multi-blade blower | |
JP2871515B2 (en) | Centrifugal blower | |
EP1382856B1 (en) | Blower and air conditioner with the blower | |
WO2019181317A1 (en) | Propeller fan | |
JPH06101696A (en) | Centrifugal blower | |
JP2002285996A (en) | Multi-blade blower fan | |
JP3409747B2 (en) | Impeller for blower | |
JPH11201091A (en) | Runner for blower |