JPS59105998A - Axial flow fan - Google Patents

Axial flow fan

Info

Publication number
JPS59105998A
JPS59105998A JP57214982A JP21498282A JPS59105998A JP S59105998 A JPS59105998 A JP S59105998A JP 57214982 A JP57214982 A JP 57214982A JP 21498282 A JP21498282 A JP 21498282A JP S59105998 A JPS59105998 A JP S59105998A
Authority
JP
Japan
Prior art keywords
fan
blade
guide
noise
suction
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.)
Granted
Application number
JP57214982A
Other languages
Japanese (ja)
Other versions
JPH0442559B2 (en
Inventor
Seiji Kawaguchi
清司 川口
Kazuma Matsui
松井 数馬
Yukio Hashimoto
幸雄 橋本
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Denso Corp
Original Assignee
NipponDenso Co Ltd
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 NipponDenso Co Ltd filed Critical NipponDenso Co Ltd
Priority to JP57214982A priority Critical patent/JPS59105998A/en
Publication of JPS59105998A publication Critical patent/JPS59105998A/en
Publication of JPH0442559B2 publication Critical patent/JPH0442559B2/ja
Granted legal-status Critical Current

Links

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
    • F04D29/32Rotors specially for elastic fluids for axial flow pumps
    • F04D29/38Blades
    • F04D29/384Blades characterised by form

Landscapes

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

Abstract

PURPOSE:To restrict generation of blade end vortex and reduce noise without decreasing an axial flow speed near the tip end of the blade by a method wherein both of the suction and delivery side surfaces of the tip end of the blade are provided with guides to change the direction of airflow. CONSTITUTION:When the fan blade 2 rotates into the arrow sign direction in the diagram, the angles of incidence at both ends 5, 9 in the front side of the rotating direction of the fan are zero degree. A flowout angle alpha at the end part 6 in the rear side of the rotating direction of the fan and the flowout angle beta at the end part 10 are about 10-80 degrees and 20-30 degrees are the optimum among those angles. Accordingly, the guide 5 of the suction side surface 3 is concave with respect to the centrifugal direction while the guide 8 of the delivery side surface 7 is convex with respect to the centrifugal direction. The widths of the guides 5, 9 are 2-10mm.. Air flows along the guide 4 at the suction side surface 3 centrifugally by the rotation of the fan, but the same flows centripetally along the guide 8 at the delivery side surface 7, and these airflows are cancelled mutually. Accordingly, the blade end vortex may be attenuated remarkably and the noise may be reduced.

Description

【発明の詳細な説明】 本発明は軸流ファンに関するもので、例えばエンジンの
ラジェータファン、換気扇のファン、扇風機のファンと
して用いて有効である。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to an axial flow fan, and is effective for use as, for example, a radiator fan for an engine, a fan for a ventilation fan, and a fan for an electric fan.

従来、種々の低騒音ファンが考え出され、その中には翼
先端付近の翼取付角を大きくして軸流速度を増加させ、
翼端渦の翼への干渉を小さくして騒音低減を図ったもの
があった。
In the past, various low-noise fans have been devised, some of which increase the axial velocity by increasing the blade attachment angle near the blade tip.
There was one that attempted to reduce noise by reducing the interference of the blade tip vortices with the blade.

しかし、このようなものでは翼取付角を大きくしたため
に、翼先端における揚力変化力(大きくなり、それだけ
翼端渦の温度も大きくなる。その結果、翼面の圧力変化
が大きくなり、騒音力く発生するという問題点があった
However, in this type of blade, because the blade attachment angle is increased, the lift force changing force at the blade tip increases, and the temperature of the blade tip vortex increases accordingly.As a result, the pressure change on the blade surface increases, and the noise force increases. There was a problem that occurred.

本発明は、上記問題点に鑑みてなされたものであり、翼
先端付近の軸流速度は下げするこ翼a尚渦の発生を抑制
し、低騒音軸流ファンを提供することを目的とする。
The present invention has been made in view of the above-mentioned problems, and an object of the present invention is to provide a low-noise axial flow fan by reducing the axial velocity near the tip of the blade, thereby suppressing the generation of vortices in the blade a. .

この目的を達するために、本発明で(よ翼先端6Bの吸
入側面、吐出側面の両面に気流の方向を変えるためのガ
イドを設け、このガイド番こより吸入(肛11面では空
気が遠心方向に流れ、吐出側面でlよ中ノシ・方向に空
気が流れるようにした。
In order to achieve this objective, the present invention provides guides for changing the direction of airflow on both the suction side and the discharge side of the wing tips 6B, The air was made to flow in the direction of the air at the discharge side.

次に本発明をラジェータファンGこ用b)た+易合の第
一実施例を図に基づいて説明する。
Next, a first embodiment of the present invention in which the present invention is applied to a radiator fan will be described with reference to the drawings.

第1図は軸流ファン1の吸入側面を示すもので、図中矢
印方向に回転する軸流ファン1を暑葺成1−るファンブ
レード2の吸入側面3に番よ、力゛イ1!4カベ設けら
れている。このガイド4はファン回転方向前方の011
1部5から、ファン回転方向後方の端部6に向っ“ζ徐
々に軸流ファン1の回転中心までの距離が長くなってい
る。
Fig. 1 shows the suction side of the axial fan 1, and the axial fan 1 rotating in the direction of the arrow in the figure is placed on the suction side 3 of the fan blade 2, which has a heat shield. There are 4 walls. This guide 4 is located at 011 in front of the fan rotation direction.
The distance to the rotation center of the axial fan 1 gradually increases from the first part 5 toward the rear end 6 in the fan rotation direction.

第2図は軸流ファン1の吐出側面を示すものであり、図
中矢印方向に回転する。そして、ファンブレード2の吐
出側面7にもガイド8が設けられている。このガイド8
はファン回転方向後方の端部9からファン回転方向前方
の端部1oに向って徐々に軸流ファン1の回転中心まで
の距離が長くなっている。
FIG. 2 shows the discharge side of the axial fan 1, which rotates in the direction of the arrow in the figure. A guide 8 is also provided on the discharge side surface 7 of the fan blade 2. This guide 8
The distance to the rotation center of the axial fan 1 gradually increases from the rear end 9 in the fan rotation direction to the front end 1o in the fan rotation direction.

つまり第3図に示すように、図中矢印方向にファンブレ
ード2が回転するとき、ファン回転方向前方の端部5.
9における流入角は0“である。
That is, as shown in FIG. 3, when the fan blade 2 rotates in the direction of the arrow in the figure, the front end 5.
The inflow angle at 9 is 0''.

また、ファン回転方向後方の端部6における流出角α及
び端部10における流出角βは共に約10’〜80°て
あり、内でも20°〜30’が最適である。従って吸入
側面3のガイド5は遠心方向に凹であり、吐出側面7の
ガイド8は遠心方向に凸である。尚、このガイド5.8
の幅は2〜10龍である。
Further, the outflow angle α at the rear end 6 in the rotational direction of the fan and the outflow angle β at the end 10 are both approximately 10' to 80°, with an optimal range of 20° to 30'. Therefore, the guide 5 on the suction side 3 is concave in the centrifugal direction, and the guide 8 on the discharge side 7 is convex in the centrifugal direction. In addition, this guide 5.8
The width is 2 to 10 dragons.

第4図はファンブレード2の斜視図であり、このファン
ブレード2に設けたガイド4,8の形状がこの図より一
目瞭然である。
FIG. 4 is a perspective view of the fan blade 2, and the shapes of the guides 4 and 8 provided on the fan blade 2 are clearly seen from this figure.

第5図はファンブレード2の横断面図である。FIG. 5 is a cross-sectional view of the fan blade 2.

尚、このファンの材質はポリプロピレンを用いている。The material used for this fan is polypropylene.

次に、以上の様に構成した軸流ファンをラジェータファ
ンとしてエンジンとラジェータの間に配設した時の作用
を従来のガイドなしのファンの作用と関連させながら説
明する。
Next, the operation when the axial fan configured as described above is disposed as a radiator fan between an engine and a radiator will be explained in relation to the operation of a conventional fan without a guide.

第6図に示す様な従来のファンlが回転すると、第7図
に示す様にファンブレード2の吸入側面3には負圧が生
じる。そのため、吐出側面3と吸入側面7との間に圧力
差が生じ、その圧力差によって吐出側面7から吸入側面
3へと空気がまわり込んでいる。その結果翼端渦11が
発生し第8図の様にこの翼端渦11がファンブレード2
の後方のファンブレード2′の表面と干渉し、騒音の原
因となっていた。そこで、本発明ではエンジン又はモー
タから回転力を受けてファンが回転すると、その回転に
よってラジェータを貫流した空気は、吸入側面3ではカ
ー(F4に沿っ゛ζ遠心方向に流れ、吐出側面7ではガ
イド8に沿って中心方向に流れる。つまり、この空気の
流れは前述したカイトがない場合の吐出側面7から吸入
側面3へとまわり込む空気と流れる方向が逆である。だ
から、これらの空気の流れは互いに相殺される。従って
翼端渦は著しく減衰し、翼端渦が生じていたファンブレ
ード2の後方のファンブレード2′との干渉もなくなり
、騒音が低減する。
When a conventional fan 1 as shown in FIG. 6 rotates, negative pressure is generated on the suction side 3 of the fan blade 2 as shown in FIG. Therefore, a pressure difference occurs between the discharge side surface 3 and the suction side surface 7, and air flows from the discharge side surface 7 to the suction side surface 3 due to the pressure difference. As a result, a blade tip vortex 11 is generated, and as shown in FIG.
This caused interference with the surface of the rear fan blade 2', causing noise. Therefore, in the present invention, when the fan rotates by receiving rotational force from the engine or motor, the air flowing through the radiator due to the rotation flows in the centrifugal direction along the car (F4) at the suction side 3, and in the centrifugal direction along the direction F4 at the discharge side 7. 8 toward the center.In other words, this air flow is opposite to the air flowing from the discharge side 7 to the suction side 3 when there is no kite.Therefore, these air flows Therefore, the blade tip vortex is significantly attenuated, and there is no interference with the rear fan blade 2' of the fan blade 2 where the blade tip vortex was generated, reducing noise.

第9図は本発明者等による騒音測定結果を示すもので、
従来の軸流ファン(実線イ)と本実施例(71ij+h
流ファン(破線口)との騒音レベルを比較したものであ
る。この第9図より、翼端渦による乱流騒音成分である
周波数lKH2〜5 K Hzにかけての騒音が低下し
ていることが明らかである。
Figure 9 shows the noise measurement results by the inventors.
Conventional axial flow fan (solid line A) and this example (71ij+h
This is a comparison of the noise level with a flow fan (dashed line). From FIG. 9, it is clear that the noise in the frequency range lKH2 to 5 KHz, which is the turbulent noise component due to the blade tip vortices, is reduced.

尚、本実施例ではファンブレード2の両面にガイドを一
条づつ設けたが、第10図に示す様に複数配設してもよ
い。
In this embodiment, one guide is provided on each side of the fan blade 2, but a plurality of guides may be provided as shown in FIG.

また、第11図に示す様にガイドを途中から複数に分離
して配設してもよい。
Further, as shown in FIG. 11, the guide may be separated into a plurality of parts and arranged in the middle.

さらにまた、第12図に示す様に翼厚が比較的厚い場合
、翼厚を変化させることにより、カイトを構成してもよ
い。第13図は第12図の廻−刈断面図である。第13
図に示す様に、吐出側面7に翼厚の厚い部分12を設け
、この翼厚の厚い部分11の是さdlを回転方向前端か
ら後端に向けて長くしていく。また、吸入側面3に溝部
13を設け、この溝部12の長さd2を回転方向前輪か
ら後端に向けて短かくしていく。この翼厚の厚い部分1
2と溝部13とがガイドを構成し、騒音を低減させる。
Furthermore, when the blade thickness is relatively thick as shown in FIG. 12, the kite may be configured by changing the blade thickness. FIG. 13 is a cross-sectional view of FIG. 12. 13th
As shown in the figure, a thick blade portion 12 is provided on the discharge side surface 7, and the height dl of the thick blade portion 11 increases from the front end to the rear end in the rotational direction. Further, a groove portion 13 is provided on the suction side surface 3, and the length d2 of this groove portion 12 is decreased from the front wheel toward the rear end in the rotational direction. This thick part of the wing thickness 1
2 and the groove portion 13 constitute a guide and reduce noise.

【図面の簡単な説明】[Brief explanation of drawings]

第1〜5図は本発明の第一実施例を示すもので、第1図
は吸入側から見た軸流ファンの正面図、第2図は吐出側
から見た軸流ファンの正面図、ff13図はファンブレ
ード要部正面図、第4図はファンブレード要部斜視図、
第5図はファンブレードの横断面図、第6〜8図は従来
の軸流ファンを示すもので、第6図は正面図、第7図及
び第8図はフアンブレー1′に′生じる翼端渦を示す図
、第9図はは従来の軸lんファンと第一実施例の軸流フ
ァンとの騒音レベルを比較した図、第10図は本発明の
第二実施例を示すものでファンブレード要部正面図、f
flll図は本発明の第三実施例を示すファンブレード
要部正面図、第12図及び第13図は本発明の第三実施
例を示すもので、第12図はファンブレード要部正面図
、第13−図は第12図の店−刈断面図である。 1・・・ボス、2・・・ファンブレード、4.8・・・
ガイド。 代理人弁理士 岡 部   隆 第4図 第5図 第7図 第8図 第9図 第10図      第11図
1 to 5 show a first embodiment of the present invention, FIG. 1 is a front view of an axial fan seen from the suction side, FIG. 2 is a front view of the axial fan seen from the discharge side, ff Figure 13 is a front view of the main part of the fan blade, Figure 4 is a perspective view of the main part of the fan blade,
Fig. 5 is a cross-sectional view of a fan blade, Figs. 6 to 8 show a conventional axial flow fan, Fig. 6 is a front view, and Figs. 7 and 8 are blade tips formed at fan brake 1'. 9 is a diagram showing the noise level of the conventional axial fan and the axial fan of the first embodiment, and FIG. 10 is a diagram showing the second embodiment of the present invention. Blade main part front view, f
FIG. 12 is a front view of the main part of a fan blade showing a third embodiment of the present invention, FIGS. 12 and 13 are a front view of the main part of a fan blade, and FIG. FIG. 13 is a cross-sectional view of FIG. 12. 1...Boss, 2...Fan blade, 4.8...
guide. Representative Patent Attorney Takashi Okabe Figure 4 Figure 5 Figure 7 Figure 8 Figure 9 Figure 10 Figure 11

Claims (1)

【特許請求の範囲】[Claims] ボスと、このボスの周囲に配設された複数のファンブレ
ードとを有し、このファンブレードの吸入面側にファン
ブレード回転方向前輪から後端に向って徐々にファン回
転中心から遠くなるようなガイドを設け、吐出面側には
ファンブレード回転方向後端から前端に向って徐々にフ
ァン回転中心から遠くなるようなガイドを設けたことを
特徴とする軸流ファン。
It has a boss and a plurality of fan blades arranged around the boss, and has a fan blade on the suction surface side of the fan blade that gradually moves away from the center of rotation of the fan from the front wheel toward the rear end in the direction of rotation of the fan blade. An axial flow fan characterized in that a guide is provided on the discharge surface side so that the guide gradually becomes farther from the fan rotation center from the rear end in the fan blade rotation direction toward the front end.
JP57214982A 1982-12-08 1982-12-08 Axial flow fan Granted JPS59105998A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP57214982A JPS59105998A (en) 1982-12-08 1982-12-08 Axial flow fan

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP57214982A JPS59105998A (en) 1982-12-08 1982-12-08 Axial flow fan

Publications (2)

Publication Number Publication Date
JPS59105998A true JPS59105998A (en) 1984-06-19
JPH0442559B2 JPH0442559B2 (en) 1992-07-13

Family

ID=16664750

Family Applications (1)

Application Number Title Priority Date Filing Date
JP57214982A Granted JPS59105998A (en) 1982-12-08 1982-12-08 Axial flow fan

Country Status (1)

Country Link
JP (1) JPS59105998A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2007040197A (en) * 2005-08-03 2007-02-15 Mitsubishi Heavy Ind Ltd Propeller fan
JP2009250190A (en) * 2008-04-10 2009-10-29 Panasonic Corp Ceiling fan
CN104329291A (en) * 2014-09-02 2015-02-04 安徽江淮汽车股份有限公司 Mechanical cooling fan of engine
JP2015031164A (en) * 2013-07-31 2015-02-16 日本電産株式会社 Impeller and air blower
WO2015029245A1 (en) * 2013-09-02 2015-03-05 三菱電機株式会社 Propeller fan, air-blowing device, and outdoor unit
EP3280918A4 (en) * 2015-04-08 2018-12-19 Horton, Inc. Fan blade surface features
CN109958630A (en) * 2017-12-14 2019-07-02 苏州宝时得电动工具有限公司 Suction and blowing device and its impeller

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5263707U (en) * 1975-11-07 1977-05-11
JPS57191495A (en) * 1981-05-19 1982-11-25 Toyota Central Res & Dev Lab Inc Axial-flow fan

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5263707U (en) * 1975-11-07 1977-05-11
JPS57191495A (en) * 1981-05-19 1982-11-25 Toyota Central Res & Dev Lab Inc Axial-flow fan

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2007040197A (en) * 2005-08-03 2007-02-15 Mitsubishi Heavy Ind Ltd Propeller fan
JP4508974B2 (en) * 2005-08-03 2010-07-21 三菱重工業株式会社 Propeller fan
JP2009250190A (en) * 2008-04-10 2009-10-29 Panasonic Corp Ceiling fan
JP2015031164A (en) * 2013-07-31 2015-02-16 日本電産株式会社 Impeller and air blower
WO2015029245A1 (en) * 2013-09-02 2015-03-05 三菱電機株式会社 Propeller fan, air-blowing device, and outdoor unit
CN104329291A (en) * 2014-09-02 2015-02-04 安徽江淮汽车股份有限公司 Mechanical cooling fan of engine
EP3280918A4 (en) * 2015-04-08 2018-12-19 Horton, Inc. Fan blade surface features
US10539157B2 (en) 2015-04-08 2020-01-21 Horton, Inc. Fan blade surface features
AU2016246617B2 (en) * 2015-04-08 2020-03-19 Horton, Inc. Fan blade surface features
US10662975B2 (en) 2015-04-08 2020-05-26 Horton, Inc. Fan blade surface features
CN109958630A (en) * 2017-12-14 2019-07-02 苏州宝时得电动工具有限公司 Suction and blowing device and its impeller

Also Published As

Publication number Publication date
JPH0442559B2 (en) 1992-07-13

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