JPH07167095A - Electric fan - Google Patents

Electric fan

Info

Publication number
JPH07167095A
JPH07167095A JP31829693A JP31829693A JPH07167095A JP H07167095 A JPH07167095 A JP H07167095A JP 31829693 A JP31829693 A JP 31829693A JP 31829693 A JP31829693 A JP 31829693A JP H07167095 A JPH07167095 A JP H07167095A
Authority
JP
Japan
Prior art keywords
blade
fan
blades
angle
electric fan
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
JP31829693A
Other languages
Japanese (ja)
Other versions
JP3467815B2 (en
Inventor
Shuji Komoda
周司 菰田
Kazuhiro Takeuchi
和宏 竹内
Akira Yamanaka
章 山中
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 JP31829693A priority Critical patent/JP3467815B2/en
Priority to US08/220,014 priority patent/US5513951A/en
Publication of JPH07167095A publication Critical patent/JPH07167095A/en
Application granted granted Critical
Publication of JP3467815B2 publication Critical patent/JP3467815B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Abstract

PURPOSE:To reduce the generation of noise and to provide a sufficient blast amount by a method wherein the specified number of blades are arranged separately from each other in a peripheral direction on the periphery of a boss part rotated through the drive force of an electric motor and each blade is formed such a manner that a portion ranging from a blade root to a blade tip forms an advance blade having a specified angle of advance. CONSTITUTION:A fan used as a forced fan arranged on a position situated upper stream from a capacitor comprises a cylindrical boss part 200: and blades 300 arranged at equal intervals around the boss part 200. The number of blades 300 is set to 9-13 blades and each blade 300 forms an advance blade and has an angle of advance phi fronting on a portion ranging from a blade root 301 to a blade tip 302 and being set to 35-45 deg.. An angle (an inclination angle) thetabetween the tangential line of the front edge in a rotation direction of the blade 300 and a radial line from the center of the boss part 200 is set to 20-10 deg. at the blade root part 301 and 50-70 deg. at the blade tip part 302 and the shape of the blade 300 is formed such a manner that a warp ratio obtained by dividing a warp height by the length of a chord is set to 7-15% at the blade root 301.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】本発明は電動ファンに関し、特に
自動車用ラジエータもしくは自動車用空調装置のコンデ
ンサに冷却風を送り込む押し込み式の電動ファンとして
用いて有効である。従来、図2に示すように自動車用の
押し込み式電動ファンとしては、自動車のエンジンルー
ム内に配置されたコンデンサ100の前方に配置され、
コンデンサ100へ冷却風を送り込む押し込み式電動フ
ァン101と、ラジエータ102の背後に配置され、コ
ンデンサ100及びラジエータ102より冷却風を吸い
込む吸い込み式の電動ファン103とが知られている。
なお、図2において104は自動車走行用のエンジン、
105はエンジンルームに車速風を吸い込むフロントグ
リルである。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an electric fan, and is particularly effective when used as a push-in type electric fan for sending cooling air to a radiator of an automobile or a condenser of an air conditioner for an automobile. 2. Description of the Related Art Conventionally, as shown in FIG. 2, a push-type electric fan for an automobile is arranged in front of a condenser 100 arranged in an engine room of the automobile,
A push-in electric fan 101 that sends cooling air to the condenser 100 and a suction-type electric fan 103 that is disposed behind the radiator 102 and sucks cooling air from the condenser 100 and the radiator 102 are known.
In FIG. 2, 104 is an engine for driving a car,
Reference numeral 105 is a front grill that draws in vehicle speed air into the engine room.

【0002】このうち、特に押し込み式電動ファン10
1はフロントグリル105の近傍に配置される結果、そ
の騒音が問題となっていた。ただ、従来では押し込み式
電動ファン101の騒音を、そのオーバーオール値での
み評価していた。
Of these, particularly the push-type electric fan 10
No. 1 is arranged near the front grill 105, and as a result, its noise has been a problem. However, conventionally, the noise of the push-type electric fan 101 was evaluated only by the overall value.

【0003】[0003]

【発明が解決しようとする課題】本発明は、この押し込
み式に用いる電動ファンの騒音を、オーバーオール値の
みでなく人が騒音として不快に感じるかどうか官能評価
を行うことで、ファンの実質的な騒音低下を図るように
することを課題とする。さらに、本発明では、上記の如
く実質的な騒音低下を図るようなファンとしたものにお
いて、充分な送風量が得られるようにすることを目的と
する。
SUMMARY OF THE INVENTION According to the present invention, the noise of the electric fan used in the push-in type is subjected to a sensory evaluation not only as an overall value but also as to whether a person feels uncomfortable as noise. The task is to reduce noise. A further object of the present invention is to make it possible to obtain a sufficient amount of air flow in a fan that can substantially reduce noise as described above.

【0004】[0004]

【課題を解決するための手段】本発明は、上記課題のも
と本発明者らによる種々の実験検討の成果として、ファ
ンをボス部の周辺に周方向に離れて9乃至13枚の羽根
を有する形状とした。さらにそのファンの形状を、羽根
の翼元部から翼先端を臨んだ前進角φが35乃至45度
の前進翼とした。また、羽根の回転方向前側の接線方向
とボス部中心からの放射線とのなす傾斜角θが、羽根の
翼元において−20から10度でかつ翼先端において5
0度から70度となっており、しかも翼元から翼先端に
向けて連続的に漸次増加する形状とした。
As a result of various experiments conducted by the present inventors based on the above problems, the present invention provides a fan with 9 to 13 blades circumferentially spaced around the boss portion. The shape was set. Further, the shape of the fan is a forward blade having an advancing angle φ of 35 to 45 degrees when the blade tip faces the blade tip. Further, the inclination angle θ formed by the tangential direction on the front side in the rotation direction of the blade and the radiation from the center of the boss portion is −20 to 10 degrees at the blade root of the blade and 5 at the blade tip.
The shape is from 0 degree to 70 degrees, and the shape is such that it gradually and continuously increases from the blade root toward the blade tip.

【0005】[0005]

【実施例】以下本発明の一例を図に基づいて説明する。
本発明の電動ファンは、上述の図2におけるコンデンサ
上流側に配置される押し込み式のファンとして用いられ
る。このファンは、図1に示すように円筒状をしたボス
部200と、このボス部の周囲に等間隔離れて配置され
た羽根300とからなる。
DESCRIPTION OF THE PREFERRED EMBODIMENTS An example of the present invention will be described below with reference to the drawings.
The electric fan of the present invention is used as a push-in type fan arranged on the upstream side of the condenser in FIG. This fan is composed of a cylindrical boss portion 200 as shown in FIG. 1 and blades 300 arranged around the boss portion at equal intervals.

【0006】本発明の望ましい例では、図1に示すよう
に羽根300を周方向に11枚配置したものであるが、
この羽根枚数の望ましい数について、本発明者らの行っ
た実験検討をまず説明する。図3はファンの音圧レベル
と周波数との関係を示す説明図で、この図3に示された
音圧レベルは、各種ファンの典型的な例を表す。
In a preferred example of the present invention, 11 blades 300 are arranged in the circumferential direction as shown in FIG.
Regarding the desirable number of blades, the experimental study conducted by the present inventors will be described first. FIG. 3 is an explanatory diagram showing the relationship between the sound pressure level of the fan and the frequency. The sound pressure level shown in FIG. 3 represents a typical example of various fans.

【0007】図3においては音圧レベル全体のオーバ
ーオール値で従来の典型的なファンにおいては60から
80dBである。またはファン回転一次成分のピーク
音のグランドノイズからの突出量であり、はその回転
一次成分の周波数である。この周波数は、〔回転数〕×
〔羽根枚数〕/60 (Hz)で表わされる。従来の典型的
な5枚羽根のファンの場合、回転数2000rpm で突出
量が20乃至30db、周波数が167Hzであった。
In FIG. 3, the overall value of the overall sound pressure level is 60 to 80 dB in the conventional typical fan. Or, it is the protrusion amount of the peak sound of the fan rotation primary component from the ground noise, and is the frequency of the rotation primary component. This frequency is [rotation speed] ×
[Number of blades] / 60 (Hz) In the case of a conventional typical five-blade fan, the amount of protrusion was 20 to 30 db and the frequency was 167 Hz at a rotation speed of 2000 rpm.

【0008】従来はこのファン騒音をオーバーオール値
のみで評価していたが、このオーバーオール値のみ
では人が騒音として不快に感じるかどうか正確に判断す
ることができなかった。これは、人間の聴覚特性上、オ
ーバーオール値のみではなくピーク音が騒音として
不快感に大きな影響を及ぼす為である。即ち、ピーク音
は突出している程耳障りとなり、かつ、ピーク音の周波
数も音色に関連することで耳障りとなるか否かの大き
な要因となる。
Conventionally, this fan noise was evaluated only by the overall value, but it was not possible to accurately determine whether or not a person feels uncomfortable as noise only by this overall value. This is because not only the overall value but also the peak sound greatly affects discomfort as noise due to human hearing characteristics. That is, the more prominent the peak sound is, the more annoying it is, and the frequency of the peak sound is also related to the timbre.

【0009】このように、ファン騒音を考えるに際して
は、従来検討されていたオーバーオール値のみなら
ず、ピーク音突出量や周波数も重大な影響を与え
る。そこで、本発明者らはこのピーク音突出量につき
さらに実験検討を進めた。一次成分は、羽根の回転によ
る周期的な圧力変動に起因して生じるものと推察される
為、この周期的圧力変動を可変すれば、ピーク音突出量
及びピーク音の周波数を制御することができると考
えられる。
As described above, when considering the fan noise, not only the overall value which has been conventionally examined, but also the peak sound protrusion amount and the frequency have a significant influence. Therefore, the inventors further conducted an experimental study on the peak sound protrusion amount. The primary component is presumed to occur due to the periodic pressure fluctuation due to the rotation of the blades. Therefore, by varying the periodic pressure fluctuation, the peak sound protrusion amount and the peak sound frequency can be controlled. it is conceivable that.

【0010】周期的圧力変動を可変するためには、ファ
ンを駆動するモータの回転数を可変すればよいが、図2
に示すような自動車用押し込み式電動ファンに用いるモ
ータでは、モータの回転数を可変制御することは一般的
ではない。自動車用に用いる押し込み式電動ファンのモ
ータは、回転数が2000rpm 程度で一定となってい
る。そこで、本発明者らは、ファンの羽根枚数を最適値
に設定することにより、騒音に対する官能評価を最良と
なるようにした。
In order to change the periodic pressure fluctuation, it is sufficient to change the rotation speed of the motor for driving the fan.
In a motor used in a push-type electric fan for an automobile as shown in (4), it is not common to variably control the rotation speed of the motor. The motor of the push-type electric fan used for automobiles has a constant rotation speed of about 2000 rpm. Therefore, the present inventors set the number of blades of the fan to an optimum value to optimize the sensory evaluation for noise.

【0011】図4は本発明者等の行った実験結果を示
す。図4に示すようにファンの羽根枚数を5,7,9,
11,13とし、且つ、それぞれのファンの径を300
mmとした上で、ピーク音周波数、ピーク音突出量
及びオーバーオール値を測定した。この図4より明ら
かなように、オーバーオール値は、ファンの羽根枚数
増加とともに増大する傾向にあるが、ピーク音突出量
は、ファンの羽根枚数増加に伴い減少する。さらに、ピ
ーク音の生ずる周波数も、ファンの羽根枚数増加に応
じて高い周波数に変化する。ピーク音突出量は、羽根
枚数増加により官能評価が良くなることが予想される
が、オーバーオール値についてはその逆で、両者相反す
る傾向である。したがって羽根枚数によって官能評価に
対する最適値が存在すると予測される。
FIG. 4 shows the result of an experiment conducted by the present inventors. As shown in FIG. 4, the number of blades of the fan is 5, 7, 9,
11 and 13, and the diameter of each fan is 300
Then, the peak sound frequency, the peak sound projection amount, and the overall value were measured. As is clear from FIG. 4, the overall value tends to increase as the number of fan blades increases, but the peak sound protrusion amount decreases as the number of fan blades increases. Further, the frequency at which the peak sound is generated also changes to a higher frequency as the number of blades of the fan increases. It is expected that the sensory evaluation of the peak sound protrusion amount will be improved by increasing the number of blades, but the overall value is the opposite, and both tend to be in conflict. Therefore, it is predicted that there is an optimum value for sensory evaluation depending on the number of blades.

【0012】そこで、本発明者らはこのピーク音突出量
、ピーク音の周波数及びオーバーオール値に基づ
いて、ファンの羽根枚数に関し総合的な官能評価を行っ
た。これは、十数人の聴者が実際に耳で聞くことによ
り、各ファンの騒音についてそれぞれ良し悪しを5段階
で点数をつけ、その平均点を官能点として評価したもの
である。その結果、図5のような傾向が得られた。すな
わち、この図5に示すように、ファンは羽根枚数を11
枚としたのが最もよい評価となり、羽根枚数は9枚以上
15枚程度で騒音の不快感を抑えることができる。この
ような実験結果に基づき、前述の図1に示した如く、本
発明の実施例では、羽根300の枚数を11枚とした。
Therefore, the present inventors conducted a comprehensive sensory evaluation on the number of blades of the fan based on the peak sound protrusion amount, the peak sound frequency and the overall value. This is to evaluate whether the noise of each fan is good or bad by actually listening to the sound by a dozen or more listeners in five grades, and evaluate the average score as a sensory point. As a result, the tendency as shown in FIG. 5 was obtained. That is, as shown in FIG. 5, the fan sets the number of blades to 11
The number of blades is the best evaluation, and the number of blades is 9 or more and 15 or less, and the discomfort of noise can be suppressed. Based on such experimental results, the number of blades 300 was set to 11 in the embodiment of the present invention, as shown in FIG.

【0013】ただ、確かに本発明の例では、ファンの羽
根300の枚数を11枚とすることで、騒音の問題を軽
減したものであるが、図4に示すように、羽根300の
枚数を増やせば、オーバーオール値は漸増する傾向が
認められる。そこで、本発明者らは、次にこのオーバー
オール値の低下を図ることを新たな課題として着目し
た。
However, in the example of the present invention, the number of the blades 300 of the fan is set to 11 to alleviate the problem of noise. However, as shown in FIG. The overall value tends to gradually increase as it is increased. Therefore, the present inventors next focused on reducing the overall value as a new subject.

【0014】そこで、本発明者らがファンの羽根300
部における実際の空気流れを可視化にて調べたところ、
図6(b)のような傾向がみられた。図6(a)に示す
ようにファンの回転方向の接線400と実際の空気の流
れ方向401との角度、すなわち斜流角δを調べたとこ
ろ、翼元300では斜流角δはほぼ0であるのに対し、
羽根300の先端302側に行くにつれ、この斜流角δ
が大きくなっていることが確かめられた。これは軸流フ
ァンは斜流角δが0となるのが通常であり、斜流角δが
大きいということは風の流れに異常をきたしていると考
えられる。本発明者等は、この斜流角δが大きくなるこ
とにより、ファン全体として騒音のオーバーオール値を
高めているものと考え、斜流角δを小さくすべく、図1
に示すような前進翼を採用した。
Therefore, the present inventors have made the fan blades 300
When the actual air flow in the section was examined by visualization,
A tendency as shown in FIG. 6 (b) was observed. As shown in FIG. 6 (a), the angle between the tangent line 400 of the fan rotation direction and the actual air flow direction 401, that is, the mixed flow angle δ was examined. While there are
As the blade 300 moves toward the tip 302 side, this mixed flow angle δ
Was confirmed to have grown. This is because an axial fan normally has a mixed flow angle δ of 0, and a large mixed flow angle δ is considered to cause an abnormality in the flow of wind. The inventors of the present invention consider that the overall value of noise is increased in the fan as a whole by increasing the mixed flow angle δ, and in order to reduce the mixed flow angle δ,
Adopted forward wing as shown in.

【0015】図7に示すように前進翼の前進角φは、羽
根300の回転方向前縁側303の翼元301部分(図
中Aで示す)におけるボス部200中心からの放射線2
01と翼元301部分(A)と翼先端302部分(B)
とを結ぶ仮想線Lとの角度で規定する。なお、前進翼の
回転方向前縁303側の翼先端302側(図中Bで示
す)は、ファンの外径点304上の仮想点となる。これ
は、図7より明らかなように、実際の羽根300は先端
302の前縁側303に丸みを生ずるため、前縁303
側の先端302は仮想上の先端Bより多少後退する為で
ある。
As shown in FIG. 7, the advancing angle φ of the advancing blade is determined by the radiation 2 from the center of the boss portion 200 at the blade base 301 portion (shown by A in the drawing) on the leading edge side 303 in the rotational direction of the blade 300.
01 and wing base 301 (A) and wing tip 302 (B)
It is defined by the angle with the imaginary line L connecting with. The blade tip 302 side (indicated by B in the drawing) on the front edge 303 side in the rotation direction of the advancing blade is a virtual point on the outer diameter point 304 of the fan. This is because, as is clear from FIG. 7, since the actual blade 300 has a rounded shape on the leading edge side 303 of the tip 302, the leading edge 303 is rounded.
This is because the tip 302 on the side is slightly retracted from the virtual tip B.

【0016】図8は、ファンの羽根枚数を11枚とした
上で、上述の定義で規定した前進角φを適宜変化させ、
先端部の斜流角δおよびファン騒音のオーバーオール値
を測定したものである。図8の実験結果では、前進角φ
を大きくするに従い、羽根300の先端部302におけ
る斜流角δは小さくなってくる。前進角φが40度程度
の時に、斜流角δは0となり、前進角φを60度まで大
きくすると、逆に斜流角δはマイナスとなる。
FIG. 8 shows that the number of blades of the fan is 11, and the advance angle φ defined by the above definition is appropriately changed.
The mixed flow angle δ at the tip and the overall value of fan noise are measured. In the experimental result of FIG. 8, the forward angle φ
The larger the value of, the smaller the mixed flow angle δ at the tip portion 302 of the blade 300 becomes. When the advancing angle φ is about 40 degrees, the mixed flow angle δ becomes 0, and when the advancing angle φ is increased to 60 degrees, the mixed flow angle δ becomes negative.

【0017】従って、先端部302における斜流角δが
0となる近傍の前進角φが40度程度で、ファン騒音の
オーバーオール値は最も低減する。前進角φが20度及
び60度のファンとの比較より、オーバーオール値を下
げるには、前進角φを30乃至50度とすれば良く、特
に望ましくは35乃至45度程度であると認められる。
Therefore, the overall angle of fan noise is reduced most when the advancing angle φ in the vicinity of the mixed flow angle δ at the tip portion 302 is 0 is about 40 degrees. Compared with the fans having the advancing angles φ of 20 ° and 60 °, in order to lower the overall value, the advancing angle φ may be set to 30 to 50 °, and it is recognized that the advancing angle φ is particularly preferably about 35 to 45 °.

【0018】図1に示した本発明の実施例のファンで
は、この実験結果に基づいて、ファンの前進角φを40
度とした前進翼としている。次に本発明者等は、前進角
φを40度とした前進翼において、羽根300の回転方
向前縁303の形状を、図6に規定した斜流角δが羽根
の翼元から先端にかけほぼ全ての位置で0度となるよう
な形状とすべく、検討を進めた。
In the fan of the embodiment of the present invention shown in FIG. 1, the advancing angle φ of the fan is set to 40 based on the result of this experiment.
It is a forward wing. Next, in the advancing blade with the advancing angle φ of 40 degrees, the inventors of the present invention set the shape of the leading edge 303 in the rotating direction of the blade 300 so that the mixed flow angle δ defined in FIG. We proceeded with the study to make the shape 0 degrees at all positions.

【0019】図6(b)の実験結果より斜流角δは羽根
300の翼元301より翼先端302に向けて漸増して
いる点に着目し、羽根300の傾斜角θを翼元301か
ら翼先端302に向けて漸増する形状とした。なお、傾
斜角θは、図7に示すように、羽根300の前縁部30
3における接線mとボス部200の中心Oからの放射線
Pとの間の角度である。
From the experimental results shown in FIG. 6B, attention is paid to the fact that the mixed flow angle δ gradually increases from the blade tip 301 of the blade 300 toward the blade tip 302. The shape is gradually increased toward the blade tip 302. The inclination angle θ is, as shown in FIG. 7, the front edge portion 30 of the blade 300.
3 is the angle between the tangent line m at 3 and the radiation P from the center O of the boss 200.

【0020】そして、ファンの羽根300形状を上記の
ように設定した上で、ファンにより生ずる流れの可視化
を行ったところ、その実験結果は図9(b)のようなも
のであった。すなわち、傾斜角θを上記のように設定す
ることで、斜流角δを翼元から先端にかけほぼ全ての位
置で0に抑えることができた。なお、図9には前進角φ
を0度とした羽根枚数11枚のファンにおける斜流角δ
を比較例として示す。
When the shape of the fan blades 300 was set as described above and the flow generated by the fan was visualized, the experimental results were as shown in FIG. 9 (b). That is, by setting the inclination angle θ as described above, the mixed flow angle δ could be suppressed to 0 at almost all positions from the blade root to the tip. In addition, in FIG. 9, the forward angle φ
Angle of flow in a fan with 11 blades, where
Is shown as a comparative example.

【0021】以上のように、前進角φを40度とした前
進翼において、羽根300の前縁303における傾斜角
θを翼元301で小さく翼先端302で大きくすること
が、羽根300部分の斜流角δを0度に近づけ、騒音の
オーバーオール値を下がる上でも有効である。さらに、
本発明者等は次に羽根300の中間部位に於ける傾斜角
θをどの様に設定するのが望ましいかに付き検討を進め
た。その結果、図10に示すような傾斜角θとすること
が望ましいことが認められた。すなわち、翼元301に
おける傾斜角θが0度で翼先端302の傾斜角θB が6
0度ぐらいとし、その間を連続的に増加させたものが望
ましい。そして、前進翼の羽根の回転方向前縁303の
形状を決める傾斜角θは、それぞれ上記値から10度程
度変更させても図9(a)に示すような斜流角δをほぼ
0にすることができる旨確かめられた。
As described above, in an advancing blade having an advancing angle φ of 40 degrees, it is necessary to make the inclination angle θ at the leading edge 303 of the blade 300 smaller at the blade base 301 and larger at the blade tip 302. It is also effective in reducing the overall noise value by making the flow angle δ close to 0 degree. further,
The present inventors next proceeded with a study on how it is desirable to set the inclination angle θ at the intermediate portion of the blade 300. As a result, it was confirmed that it is desirable to set the inclination angle θ as shown in FIG. That is, the inclination angle θ at the blade base 301 is 0 degree and the inclination angle θ B of the blade tip 302 is 6 degrees.
It is desirable to set it to about 0 degree and to increase continuously during that time. The inclination angle θ that determines the shape of the front edge 303 of the blade of the advancing blade in the rotational direction makes the mixed flow angle δ as shown in FIG. I was confirmed that I could do it.

【0022】このように、羽根300を前進角φが40
度程度の前進翼とし、かつ傾斜角θを翼元301部分で
小さく、翼先端302部分で大きくすることにより、羽
根を枚数11枚としてファン騒音の官能評価を向上させ
つつ、かつ騒音のオーバーオール値を低減することがで
きた。しかしながら、本発明者の検討では、このように
騒音低減が十分図れるものの、ファンの羽根枚数を増や
すことで、送風性能が低下する傾向にあることが認めら
れた(図11参照)。
In this way, the advancing angle φ of the blade 300 is 40
The number of blades is 11, and the overall value of noise is improved while improving the sensory evaluation of fan noise by making the forward blade of about 10 degrees and making the inclination angle θ small at the blade base 301 portion and large at the blade tip 302 portion. Could be reduced. However, according to the study by the present inventor, although the noise can be sufficiently reduced as described above, it is recognized that the blowing performance tends to be reduced by increasing the number of blades of the fan (see FIG. 11).

【0023】なお、図11の実験は、羽根300のそり
高さhを翼弦長lで割ったそり比h/l(図12参
照)、羽根300の翼取付角β(図12参照)、及び翼
弦長lを翼ピッチtで割ったソリディティl/t(図7
参照)を、従来のファンと同一形状とし、かつ上述した
本発明の前進翼としたファンを複数作成し、その羽根枚
数と送風性能との関係を示したものである。図11に示
すように、羽根300の形状が前述のように従来通りで
は、羽根枚数を増すと送風性能が低下してしまう。
In the experiment of FIG. 11, the warp ratio h / l obtained by dividing the warp height h of the blade 300 by the chord length l (see FIG. 12), the blade mounting angle β of the blade 300 (see FIG. 12), And the solidity 1 / t obtained by dividing the chord length 1 by the blade pitch t (see FIG. 7).
(Refer to FIG. 4) has the same shape as a conventional fan and has a plurality of fans that are the advancing blades of the present invention described above, and shows the relationship between the number of blades and the blowing performance. As shown in FIG. 11, if the shape of the blades 300 is the same as that of the conventional one, as the number of blades is increased, the blowing performance is deteriorated.

【0024】そこで、本発明者等は次にファンの送風性
能向上を目指して実験検討を行った。なお、この検討に
際しては特願昭平3−338667号に開示済の手法に
よった。本発明者等はそり比h/lを翼先端302部分
では2.5%とし、翼元のそり比(h/l)bを4%,
8%,10%,12%,14%,及び16%とした、そ
れぞれ図13にA,B,C,D,E,Fで示すそり比分
布をもったファンを作成し、それらの送風性能の比較を
行った。
Therefore, the inventors of the present invention next conducted an experimental study aiming at improving the blowing performance of the fan. The method disclosed in Japanese Patent Application No. 3-338667 was used for this examination. The present inventors set the warpage ratio h / l to 2.5% at the blade tip 302, and set the blade base warpage ratio (h / l) b to 4%.
The fans having the warp ratio distributions shown in FIG. 13 as A, B, C, D, E, and F, which are 8%, 10%, 12%, 14%, and 16%, respectively, are created, and their blowing performances are created. Were compared.

【0025】その比較結果を図14に示す。図14よ
り、そり比(h/l)bを変化させることで、送風性能
が向上し、特に翼元301部分のそり比(h/l)bを
7〜15%とすれば送風性能が向上することが確かめら
れた。なかでも、翼元301のそり比(h/l)bが1
2%前後で送風性能が最大となることが確かめられた。
しかし、図14に従来の5枚羽根レベルとの比較で示す
ように、翼元そり比(h/l)bを工夫しても、それの
みでは従来と同等の送風性能を、羽根枚数11枚とした
際には達成できていない。
The comparison result is shown in FIG. From FIG. 14, the air blowing performance is improved by changing the warpage ratio (h / l) b, and particularly the air blowing performance is improved by setting the warpage ratio (h / l) b of the blade root 301 portion to 7 to 15%. It was confirmed to do. Above all, the warpage ratio (h / l) b of the blade base 301 is 1
It was confirmed that the ventilation performance becomes maximum at around 2%.
However, as shown in FIG. 14 in comparison with the conventional 5-blade level, even if the blade sled ratio (h / l) b is devised, it is possible to obtain the same blowing performance as the conventional one with 11 blades. It was not achieved at that time.

【0026】これはソリディティl/tが同じ場合、羽
根枚数を多くしていくと翼弦長lが小さくなるためであ
ると考えられる。そこで、本発明者らはこの羽根枚数が
増すと送風性能が低下していくことと翼弦長lが小さく
なっていることとの関連性に着目した。ファンは、風を
起こす作用と共にファン前後に圧力差を発生させてい
る。特に、図2に示すような押し込みタイプのファンで
は、コンデンサ100やラジエータ102に風を送り込
むために、コンデンサ100及びラジエータ102の通
風抵抗分の圧力差をファン101前後で発生させなけれ
ばならない。
It is considered that this is because when the solidity 1 / t is the same, the chord length 1 becomes smaller as the number of blades is increased. Therefore, the present inventors have paid attention to the relationship between the fact that the blowing performance decreases as the number of blades increases and the chord length l decreases. The fan produces a pressure difference between the front and the back of the fan as well as the action of generating wind. In particular, in a push-in type fan as shown in FIG. 2, in order to blow air into the condenser 100 and the radiator 102, a pressure difference corresponding to the ventilation resistance of the condenser 100 and the radiator 102 must be generated before and after the fan 101.

【0027】ここで、翼弦長lは小さいが羽根300の
枚数が多いファンと、逆に翼弦長lは大きいが羽根30
0の枚数が少ないファンとを比較検討する。ファン径が
同じで、熱交換器に同一風量を送り込んでいる場合、フ
ァン前後の圧力差は同じと考えられる。従って、両方の
ファンがその前後圧力差が同じであると仮定した場合、
同一送風量を送るためには、翼弦長lが小さく羽根枚数
が多いファンは、ファン前後の圧力勾配が大きくなる。
Here, a fan having a small chord length l but a large number of blades 300 and a fan 30 having a large chord length l but having a large chord length l
We will compare it with a fan with a small number of zero. When the fan diameter is the same and the same air volume is sent to the heat exchanger, the pressure difference before and after the fan is considered to be the same. Therefore, assuming that both fans have the same pressure difference across them,
In order to send the same amount of air, a fan having a small chord length l and a large number of blades has a large pressure gradient before and after the fan.

【0028】圧力勾配が大きいということは、羽根30
0面上の流れが剥離しやすくなるということである。流
れの剥離は送風性能の低下につながるもので、このこと
が、翼弦長lが小さいファンの送風性能低下に関連する
ものと考えられる。そこで、本発明者らは、送風性能を
更に向上する手段として、翼弦長lを大きくすることに
着目した。すなわち翼ピッチtに対する翼弦長lの比で
あるソリディティl/tを大きくすることで、送風性能
の向上を試みた。なお、従来の一般的なファンのソリデ
ィティl/tは翼先端で0.6弱である。
The large pressure gradient means that the blade 30
This means that the flow on the 0th surface is easily separated. The flow separation leads to a reduction in the blowing performance, and this is considered to be related to the reduction in the blowing performance of a fan having a small chord length l. Therefore, the present inventors have focused on increasing the chord length l as a means for further improving the blowing performance. That is, an attempt was made to improve the blowing performance by increasing the solidity 1 / t, which is the ratio of the chord length 1 to the blade pitch t. The solidity 1 / t of a conventional general fan is less than 0.6 at the blade tip.

【0029】本発明者らは、図15に示すように、翼先
端302部分のソリディティl/tの値を0.58,
0.7,0.8,0.9,及び1.0としたファンG,
H,I,J,Kのファンについてそれぞれ送風性能を比
較した。その結果、図16のような送風性能特性が認め
られ翼先端302でのソリディティ(l/t)tを0.
7〜0.95の範囲にすれば、従来の5枚羽根で得られ
ていた送風性能は得られることが認められた。
As shown in FIG. 15, the present inventors set the value of solidity 1 / t of the blade tip 302 portion to 0.58,
Fan G with 0.7, 0.8, 0.9, and 1.0
The fan performances of the H, I, J, and K fans were compared. As a result, the blowing performance characteristics as shown in FIG. 16 were recognized, and the solidity (l / t) t at the blade tip 302 was set to 0.
It was confirmed that if the range is from 7 to 0.95, the blowing performance obtained with the conventional five blades can be obtained.

【0030】このように、本発明者らの検討によれば、
そり比h/lの分布を翼中央部から翼元301にかけて
急激に増大させるような分布とし、かつそり比h/lを
翼元301部分で7〜15%とするとともに、ソリディ
ティl/tの分布を翼元301から翼先端302にかけ
て一定もしくは滑らかに減少させかつ翼先端のソリディ
ティ(l/t)tを0.7〜0.95とすれば、前述の
如く羽根枚数を11枚の前進翼として、騒音を低減させ
たファンであっても、同時に十分な送風性能を発揮する
ことが確かめられた。なお、そり比の分布は図13に示
したように翼元301から翼中央にかけて単一減少とな
る曲線でなくてもよく、例えば翼元301部分にそり比
h/lがほぼ一定となる部分があってもよい。またそり
比h/lを翼中央から翼先端302にかけてやや増加す
る形状としてもよい。本発明者らの検討では、このよう
にそり比を翼元から翼先端にかけ多少変更させてもほぼ
同等の送風性能が認められた。
As described above, according to the study by the present inventors,
The distribution of the sled ratio h / l is set so as to rapidly increase from the blade central portion to the blade root 301, and the sled ratio h / l is set to 7 to 15% at the blade root 301 portion, and the solidity l / t If the distribution is constantly or smoothly reduced from the blade tip 301 to the blade tip 302 and the blade tip solidity (l / t) t is 0.7 to 0.95, the number of blades is 11 as described above. As a result, it was confirmed that even a fan with reduced noise can exhibit sufficient blowing performance at the same time. It should be noted that the distribution of the warpage ratio does not have to be a curve having a single decrease from the blade root 301 to the blade center as shown in FIG. 13, and for example, a portion where the warpage ratio h / l is almost constant in the blade root 301 portion. There may be. The warp ratio h / l may be slightly increased from the blade center to the blade tip 302. According to the study by the present inventors, even if the warp ratio is slightly changed from the blade root to the blade tip as described above, almost the same blowing performance is recognized.

【0031】[0031]

【発明の効果】以上説明したように、本発明では押し込
みファンの羽根枚数を9から13枚とし、かつ前進角φ
が35乃至45度の角度としたため、ファン騒音の低減
を図ることができた。さらに羽根の回転方向前縁の傾斜
角θが、翼元部では−20度から+10度であり、翼先
端部では50度から70度であり、かつ翼元から翼先端
にかけて連続的に漸増する形状としたため、上記の騒音
低減効果をさらに向上させることができた。
As described above, according to the present invention, the number of blades of the pushing fan is 9 to 13, and the advance angle φ is
Since the angle is 35 to 45 degrees, the fan noise can be reduced. Further, the inclination angle θ of the leading edge of the blade in the rotation direction is −20 to +10 degrees at the blade tip portion, is 50 to 70 degrees at the blade tip portion, and gradually increases from the blade tip to the blade tip. Because of the shape, the above noise reduction effect could be further improved.

【0032】また、ファンの羽根翼元でのそり比を7〜
15%とすることにより、上記の騒音低減効果ととも
に、送風性能の維持を図るようにすることができた。さ
らに、翼先端でのソリディティを0.7〜0.95とす
ることで、この騒音低減効果と、送風性能の効果との両
立を一層高めることができた。
Further, the warpage ratio of the fan blades is 7 to
By setting it to 15%, it was possible to maintain the blowing performance as well as the above noise reduction effect. Furthermore, by setting the solidity at the blade tip to be 0.7 to 0.95, it was possible to further improve both the effect of reducing noise and the effect of air blowing performance.

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

【図1】本発明ファンの一実施例を示す正面図FIG. 1 is a front view showing an embodiment of a fan of the present invention.

【図2】押し込みファンの設置例を示す説明図FIG. 2 is an explanatory diagram showing an installation example of a pushing fan.

【図3】押し込みファンの音圧レベルを示す説明図FIG. 3 is an explanatory diagram showing the sound pressure level of the pushing fan.

【図4】ファン枚数とファン騒音との関係を示す説明図FIG. 4 is an explanatory diagram showing the relationship between the number of fans and fan noise.

【図5】ファン枚数と騒音官能評価との関係を示す説明
FIG. 5 is an explanatory diagram showing the relationship between the number of fans and the sensory evaluation of noise.

【図6】従来ファンの空気流れを示す説明図FIG. 6 is an explanatory view showing an air flow of a conventional fan.

【図7】本発明ファンの要部を示す正面図FIG. 7 is a front view showing a main part of the fan of the present invention.

【図8】羽根の前進角と騒音との関係を示す説明図FIG. 8 is an explanatory diagram showing the relationship between the advancing angle of the blade and noise.

【図9】本発明ファンの空気流れを示す説明図FIG. 9 is an explanatory view showing the air flow of the fan of the present invention.

【図10】本発明ファンに関わる傾斜角θを示す説明図FIG. 10 is an explanatory view showing an inclination angle θ related to the fan of the present invention.

【図11】羽根枚数と送風性能との関係を示す説明図FIG. 11 is an explanatory diagram showing the relationship between the number of blades and the blowing performance.

【図12】図7のX−X線に沿う断面図FIG. 12 is a sectional view taken along line XX of FIG.

【図13】翼断面位置とそり比との関係を示す説明図FIG. 13 is an explanatory diagram showing the relationship between the blade cross-section position and the warpage ratio.

【図14】翼元そり比と送風性能との関係を示す説明図FIG. 14 is an explanatory diagram showing the relationship between the blade sled ratio and the blowing performance.

【図15】翼断面位置とソリディティとの関係を示す説
明図
FIG. 15 is an explanatory diagram showing a relationship between a blade cross-section position and solidity.

【図16】翼先端ソリディティと送風性能との関係を示
す説明図
FIG. 16 is an explanatory diagram showing the relationship between blade tip solidity and air blowing performance.

【符号の説明】[Explanation of symbols]

200 ボス部 300 羽根 301 翼元部 302 翼先端部 200 Boss 300 Blade 301 Blade Base 302 Blade Tip

Claims (4)

【特許請求の範囲】[Claims] 【請求項1】 電動モータによって回転駆動される電動
ファンであって、 電動モータの駆動力を受けて回転するボス部と、 このボス部の周囲に周方向に離れて9乃至13枚配置さ
れた羽根とを備え、 前記羽根は翼元から翼先端を臨んだ前進角φが35乃至
45度の前進翼としたことを特徴とする電動ファン。
1. An electric fan rotatably driven by an electric motor, comprising: a boss portion that receives a driving force of the electric motor to rotate; and 9 to 13 boss portions that are circumferentially separated from each other around the boss portion. An electric fan, comprising: a blade, the blade being a forward blade having a forward angle φ of 35 to 45 degrees with the blade tip facing the blade tip.
【請求項2】 請求項1の電動ファンにおいて、 前記羽根の回転方向前縁側の接線とボス部中心からの放
射線とのなす傾斜角θが、翼元部では−20から10度
であり、翼先端部では50から70度であり、かつ翼元
から翼先端にかけて連続的に漸次増加することを特徴と
する電動ファン。
2. The electric fan according to claim 1, wherein an inclination angle θ formed by a tangent line on the leading edge side in the rotation direction of the blade and radiation from the center of the boss portion is −20 to 10 degrees at the blade root portion, An electric fan having a tip portion of 50 to 70 degrees and a gradual increase from the blade root to the blade tip.
【請求項3】 請求項1もしくは2の電動ファンにおい
て、 羽根のそり高さhを翼弦長lで割ったそり比h/lを、
翼中央から翼元にかけて急激に増大させかつ翼元部のそ
り比h/lを7〜15%としたことを特徴とする電動フ
ァン。
3. The electric fan according to claim 1, wherein a warpage ratio h / l obtained by dividing a blade warpage height h by a chord length l is:
An electric fan characterized in that the warp ratio h / l of the blade root portion is set to 7 to 15% by rapidly increasing from the blade center to the blade root.
【請求項4】 請求項1乃至3いずれかの電動ファンに
おいて、 羽根の翼弦長lを翼ピッチtで割ったソリディティl/
tの分布を翼元から翼先端にかけて一定もしくは滑らか
に減少させかつ翼先端のソリディティl/tを0.7乃
至0.95としたことを特徴とする電動ファン。
4. The electric fan according to any one of claims 1 to 3, wherein the blade length chord length l is divided by a blade pitch t to determine solidity 1 /
An electric fan characterized in that the distribution of t is reduced uniformly or smoothly from the blade root to the blade tip, and the blade solidity 1 / t is set to 0.7 to 0.95.
JP31829693A 1993-03-29 1993-12-17 Electric fan Expired - Lifetime JP3467815B2 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
JP31829693A JP3467815B2 (en) 1993-12-17 1993-12-17 Electric fan
US08/220,014 US5513951A (en) 1993-03-29 1994-03-28 Blower device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP31829693A JP3467815B2 (en) 1993-12-17 1993-12-17 Electric fan

Publications (2)

Publication Number Publication Date
JPH07167095A true JPH07167095A (en) 1995-07-04
JP3467815B2 JP3467815B2 (en) 2003-11-17

Family

ID=18097622

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Country Link
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JP2002520993A (en) * 1998-07-20 2002-07-09 エヌエムビー(ユーエスエイ)・インコーポレイテッド Axial fan
JP2010151137A (en) * 1998-07-20 2010-07-08 Minebea Co Ltd Vane for impeller, impeller using the vane, and axial flow fan using impeller
JP4796691B2 (en) * 1998-07-20 2011-10-19 ミネベア株式会社 Axial fan
JP4662608B2 (en) * 2000-06-09 2011-03-30 エルジー エレクトロニクス インコーポレイティド Fan motor with integrated axial fan and motor
KR100379498B1 (en) * 2000-10-18 2003-04-10 엘지전자 주식회사 an axial flow fan for package air conditioner outdoor unit
EP3267043A1 (en) 2005-08-03 2018-01-10 Mitsubishi Heavy Industries, Ltd. Axial rotary vane wheel of propeller fan
EP1750015A2 (en) 2005-08-03 2007-02-07 Mitsubishi Heavy Industries, Ltd. Shroud and rotary vane wheel of propeller fan and propeller fan
JP2007040201A (en) * 2005-08-03 2007-02-15 Mitsubishi Heavy Ind Ltd Propeller fan
US7815418B2 (en) 2005-08-03 2010-10-19 Mitsubishi Heavy Industries, Ltd. Shroud and rotary vane wheel of propeller fan and propeller fan
JP4576304B2 (en) * 2005-08-03 2010-11-04 三菱重工業株式会社 Propeller fan
US7909572B2 (en) 2005-08-03 2011-03-22 Mitsubishi Heavy Industries, Ltd. Shroud and rotary vane wheel of propeller fan and propeller fan
EP3267044A1 (en) 2005-08-03 2018-01-10 Mitsubishi Heavy Industries, Ltd. Propeller fan comprising an axial rotary vane wheel
JP2007247501A (en) * 2006-03-15 2007-09-27 Hitachi Plant Technologies Ltd Jet fan
JP2013209884A (en) * 2012-03-30 2013-10-10 Mitsubishi Electric Corp Axial-flow blower
US9551345B2 (en) 2012-09-06 2017-01-24 Sanyo Denki Co., Ltd. Axial flow fan
JP2014051914A (en) * 2012-09-06 2014-03-20 Sanyo Denki Co Ltd Axial flow fan

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