JPH06108996A - Fan - Google Patents
FanInfo
- Publication number
- JPH06108996A JPH06108996A JP25516792A JP25516792A JPH06108996A JP H06108996 A JPH06108996 A JP H06108996A JP 25516792 A JP25516792 A JP 25516792A JP 25516792 A JP25516792 A JP 25516792A JP H06108996 A JPH06108996 A JP H06108996A
- Authority
- JP
- Japan
- Prior art keywords
- fan
- blade
- negative pressure
- pressure side
- side face
- 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
Landscapes
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
Description
【0001】[0001]
【産業上の利用分野】本発明はファンに関し、特に低騒
音化したファンに関する。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a fan, and more particularly to a fan with reduced noise.
【0002】[0002]
【従来の技術】従来、一般的にファンの翼10は、図4
のように略平滑な面によって形成されていた。2. Description of the Related Art Conventionally, a fan blade 10 is generally shown in FIG.
Was formed by a substantially smooth surface.
【0003】このような翼10を用いたファンを運転さ
せ場合、翼10の負圧側面11を流れる気流は、その下
流側部分の表面近傍において、気流の境界層に剥離流1
2が発生していた。そして、このような剥離流12の発
生によって、ファン自体の運転効率が低下してしまうと
共に、騒音も大きくなってしまうことになる。When a fan using such a blade 10 is operated, the airflow flowing on the suction side 11 of the blade 10 is separated into the boundary layer of the airflow in the vicinity of the surface of the downstream side thereof.
2 had occurred. Then, due to the generation of the separated flow 12 as described above, the operation efficiency of the fan itself is reduced and the noise is also increased.
【0004】そこで、例えば実開昭63−160399
号公報に示されるような構造のファンによって、翼10
の負圧側面11における剥離流12の発生を防止するこ
とが行われている。Therefore, for example, Japanese Utility Model Laid-Open No. 63-160399.
The fan 10 having the structure shown in Japanese Patent Publication No.
The generation of the separated flow 12 on the negative pressure side surface 11 is performed.
【0005】即ち、図5で示すように、ファンの翼13
の負圧側面14の上流側部分に剥離流防止部15として
一対の凹部(もしくは突起部)を軸心方向に向けて負圧
側面14の全体に亙って形成し、この剥離流防止部15
によって気流の上流側部分において境界層を乱流境界層
に遷移させ、ファン本体の運転効率の向上と騒音の低下
を図っているThat is, as shown in FIG. 5, the fan blades 13
A pair of recesses (or protrusions) are formed as the separation flow prevention portion 15 on the upstream side of the suction side surface 14 of the suction pressure side surface 14 in the axial direction, and the separation flow prevention portion 15 is formed.
The transition of the boundary layer to the turbulent boundary layer in the upstream part of the air flow improves the operation efficiency of the fan body and reduces noise.
【0006】[0006]
【発明が解決しようとする課題】しかしながら、上述し
たな翼の負圧側面の上流側部分に凹凸状の剥離流防止部
を形成したものにおいては、剥離流防止部が上流側部分
にのみ形成されているため、気流の上流側部分での境界
層を乱流境界層に遷移させることはできるが、この剥離
流防止部を通過した気流が翼の後半で境界層が成長する
ことになり、結果的には下流側部分の表面近傍におい
て、比較的大きな剥離流が発生すると言う問題点があっ
た。However, in the above-described case where the uneven flow preventing portion is formed on the upstream side portion of the suction side surface of the blade, the separate flow preventing portion is formed only on the upstream side portion. Therefore, the boundary layer in the upstream part of the airflow can be transited to the turbulent boundary layer, but the airflow passing through this separation flow prevention part grows in the latter half of the blade, resulting in In particular, there is a problem that a relatively large separated flow is generated near the surface of the downstream side portion.
【0007】また、凸状のものではそれ自体が風切音を
生じ、凹状のものでは上流側部分の強度が低下してしま
うことにもなる。Further, the convex shape itself causes wind noise, and the concave shape reduces the strength of the upstream side portion.
【0008】そこで、図6(a)のようにファンの翼の
強度を考慮して、剥離流防止部16を略円状にして、相
互ピッチP1 、P2 を大きくし、径lを小さくすること
も考えられるが、剥離流防止部を通過しない気流があ
り、剥離流の発生を確実の防止することができない。Therefore, considering the strength of the fan blade as shown in FIG. 6 (a), the separation flow prevention portion 16 is formed into a substantially circular shape to increase the mutual pitches P 1 and P 2 and decrease the diameter l. However, there is an air flow that does not pass through the separation flow prevention unit, and thus the generation of the separation flow cannot be reliably prevented.
【0009】さらに、図6(b)のように剥離流防止部
17の径l´を大きくして、全ての気流が剥離流防止部
を通過するようにすることも考えられるが、剥離流防止
部の径が大きい分だけ乱流効果が低下し、境界層が厚く
なり、効果的に剥離流の発生を防止することができな
い。Further, as shown in FIG. 6 (b), it is conceivable to increase the diameter l'of the separation flow prevention part 17 so that all the airflow passes through the separation flow prevention part. The larger the diameter of the part, the lower the turbulence effect and the thicker the boundary layer, so that it is impossible to effectively prevent the generation of the separated flow.
【0010】本発明は上記のような問題点を解消し、翼
の強度を保ちながら、風切音等を発生させることなく、
剥離流の発生を確実に防止することによって、ファン本
体の運転効率の向上と騒音の低下を図ることのできるフ
ァンを提供することを目的とする。The present invention solves the above problems and maintains the strength of the wing without generating wind noise or the like.
An object of the present invention is to provide a fan capable of improving the operation efficiency of the fan body and reducing noise by surely preventing the generation of a separated flow.
【0011】[0011]
【課題を解決するための手段】上記目的を解決するため
に、本願第1の発明は、ほぼ円筒状に形成されたハブの
周囲に複数枚の翼を設けてなるファンにおいて、翼の負
圧側面に複数個のL形の凹部を設けて構成している。In order to solve the above-mentioned problems, the first invention of the present application is a fan in which a plurality of blades are provided around a hub formed in a substantially cylindrical shape. It is configured by providing a plurality of L-shaped recesses on the side surface.
【0012】また、本願第2の発明は、翼の負圧側面に
設けられたL形の凹部の角部が気流流入方向に対向させ
て構成している。The second aspect of the present invention is configured so that the corners of the L-shaped recess provided on the suction side surface of the blade are opposed to each other in the air flow inflow direction.
【0013】[0013]
【作用】このような構成によれば、剥離流防止部として
の凹部を大きくしないため、翼の強度が低下することな
く、乱流効果が低下することもない。また、全ての気流
が剥離流防止部としての凹部を効果的に通過するため、
剥離流の発生を確実に防止することができる。According to this structure, since the recess serving as the separation flow prevention portion is not enlarged, the strength of the blade does not decrease and the turbulent flow effect does not decrease. Moreover, since all the airflows effectively pass through the concave portion as the separation flow prevention portion,
It is possible to reliably prevent the generation of a separated flow.
【0014】[0014]
【実施例】以下、本発明の実施例を図面を参照して説明
する。Embodiments of the present invention will be described below with reference to the drawings.
【0015】図1において、ファン1は略円筒状に形成
されたハブ2の周囲に複数枚の翼3を設けてなり、翼3
の負圧側面4の表面に剥離流防止部5としてL形の凹部
6が設けられている。この剥離流防止部5は気流の流れ
方向Aに対して、格子状に翼の負圧側面4上全面にわた
って配設されている。この剥離流防止部5の縦ピッチP
1 と、横ピッチP2 は、ファンの回転軸に対する気流の
角度をθ0 として、以下のように設定される。In FIG. 1, the fan 1 comprises a plurality of blades 3 provided around a hub 2 formed in a substantially cylindrical shape.
An L-shaped concave portion 6 is provided as a separation flow prevention portion 5 on the surface of the negative pressure side surface 4. The separation flow prevention unit 5 is arranged in a lattice shape over the entire suction side surface 4 of the blade in the flow direction A of the air flow. The vertical pitch P of the separation flow prevention unit 5
1 and the lateral pitch P 2 are set as follows, where θ 0 is the angle of the airflow with respect to the rotation axis of the fan.
【0016】[0016]
【数1】tanθ0 =P1 /P2 ## EQU1 ## tan θ 0 = P 1 / P 2
【0017】そして、このピッチに対応してL形の角部
7を配置し、この角部7を基準点Bとして、L形の縦方
向の片8を気流方向Aに対して角度θ1 、横方向の片9
を角度θ2 としてL形の凹部を形成する(ここではθ0
=θ1 )。Then, the L-shaped corner portion 7 is arranged corresponding to this pitch, and with this corner portion 7 as a reference point B, the L-shaped longitudinal piece 8 is angle θ 1 with respect to the air flow direction A, Lateral piece 9
At an angle θ 2 to form an L-shaped recess (here, θ 0
= Θ 1 ).
【0018】この時、気流が剥離流防止部5を通過する
割合をΨとするならば、0.9>Ψとなるように、縦片
長L1 と横片長L2 のそれぞれの値が以下の式に基づい
て決定される。At this time, if the ratio of the air flow passing through the separation flow prevention portion 5 is Ψ, the respective values of the vertical piece length L 1 and the horizontal piece length L 2 are as follows so that 0.9> Ψ. It is determined based on the formula.
【0019】[0019]
【数2】 0.9>Ψ=(L1 sinθ1 +L2 sinθ2 )/P1 sinθ0 2>0.9> Ψ = (L 1 sin θ 1 + L 2 sin θ 2 ) / P 1 sin θ 0
【0020】また、この凹部6の深さtは翼の厚みTに
対して、5%<t/T<50%となるように形成されれ
ば、強度的には信頼性がおけるものとなる。Further, if the depth t of the recess 6 is formed so as to satisfy 5% <t / T <50% with respect to the thickness T of the blade, the reliability can be ensured in terms of strength. .
【0021】このようにして、ファンの回転軸に対して
角度をθ0 で流入した気流は、必ず剥離流防止部5を通
過することになり、翼の負圧側面での剥離による境界層
の発達が防止され、図2に示すように、1500m3 /
hにおいて剥離流防止部のないものに対して1.0dB
A,円形の剥離流防止部を形成したものに対して0.5
dBA騒音が低下することになる。In this way, the airflow flowing in at an angle of θ 0 with respect to the rotation axis of the fan always passes through the separation flow prevention unit 5, and the boundary layer of the boundary layer due to separation on the suction side of the blade is formed. Development is prevented, as shown in Figure 2, 1500 m 3 /
1.0dB for h without hose
A, 0.5 for those with a circular separation flow prevention part
The dBA noise will be reduced.
【0022】[0022]
【発明の効果】以上のように本発明によれば、ほぼ円筒
状に形成されたハブの周囲に複数枚の翼を設けてなるフ
ァンにおいて、翼の負圧側面に複数個のL形の凹部を設
けたことにより、翼の強度を保ちながら、風切音等を発
生させることなく、剥離流の発生を確実に防止し、ファ
ン本体の運転効率の向上と騒音の低下を図ることができ
る。As described above, according to the present invention, in a fan in which a plurality of blades are provided around a hub formed into a substantially cylindrical shape, a plurality of L-shaped recesses are formed on the suction side surface of the blade. By providing the blades, it is possible to reliably prevent the generation of separated flow without generating wind noise while maintaining the strength of the blades, thereby improving the operating efficiency of the fan body and reducing noise.
【図1】本発明の一実施例におけるファンを示す図であ
る。FIG. 1 is a diagram showing a fan according to an embodiment of the present invention.
【図2】図1の要部拡大図である。FIG. 2 is an enlarged view of a main part of FIG.
【図3】本願発明の騒音特性図である。FIG. 3 is a noise characteristic diagram of the present invention.
【図4】従来のファンの翼断面図である。FIG. 4 is a blade cross-sectional view of a conventional fan.
【図5】従来のファンの剥離流防止部を示す図である。FIG. 5 is a view showing a separation flow prevention unit of a conventional fan.
【図6】従来のファンの他の剥離流防止部を示す図であ
る。FIG. 6 is a diagram showing another separation flow prevention unit of a conventional fan.
1…ファン、2…ハブ、3…翼、4…負圧側面、6…L
形の凹部、7…角部1 ... Fan, 2 ... Hub, 3 ... Wing, 4 ... Suction side, 6 ... L
-Shaped recess, 7 ... Corner
Claims (2)
複数枚の翼を設けてなるファンにおいて、翼の負圧側面
に複数個のL形の凹部を設けたことを特徴とするファ
ン。1. A fan comprising a plurality of blades provided around a substantially cylindrical hub, wherein a plurality of L-shaped recesses are provided on the suction side surface of the blade.
の角部が気流流入方向に対向していることを特徴とする
請求項1記載のファン。2. The fan according to claim 1, wherein the corners of the L-shaped concave portion provided on the suction side surface of the blade are opposed to each other in the air flow inflow direction.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP25516792A JPH06108996A (en) | 1992-09-25 | 1992-09-25 | Fan |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP25516792A JPH06108996A (en) | 1992-09-25 | 1992-09-25 | Fan |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH06108996A true JPH06108996A (en) | 1994-04-19 |
Family
ID=17274992
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP25516792A Pending JPH06108996A (en) | 1992-09-25 | 1992-09-25 | Fan |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH06108996A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1997033091A1 (en) * | 1996-03-06 | 1997-09-12 | Hitachi, Ltd. | Propeller fan and outdoor machine using the same for air-conditioners |
US8231331B2 (en) | 2008-03-14 | 2012-07-31 | Wayne State University | Reduction of flow-induced noise in a centrifugal blower |
-
1992
- 1992-09-25 JP JP25516792A patent/JPH06108996A/en active Pending
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1997033091A1 (en) * | 1996-03-06 | 1997-09-12 | Hitachi, Ltd. | Propeller fan and outdoor machine using the same for air-conditioners |
US8231331B2 (en) | 2008-03-14 | 2012-07-31 | Wayne State University | Reduction of flow-induced noise in a centrifugal blower |
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