JPH11132194A - Axial flow fan - Google Patents

Axial flow fan

Info

Publication number
JPH11132194A
JPH11132194A JP29252597A JP29252597A JPH11132194A JP H11132194 A JPH11132194 A JP H11132194A JP 29252597 A JP29252597 A JP 29252597A JP 29252597 A JP29252597 A JP 29252597A JP H11132194 A JPH11132194 A JP H11132194A
Authority
JP
Japan
Prior art keywords
blade
straight line
axial flow
flow fan
angle
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
JP29252597A
Other languages
Japanese (ja)
Other versions
JP3803184B2 (en
Inventor
Mitsuyoshi Ishijima
満義 石嶋
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.)
Toshiba Corp
Original Assignee
Toshiba Corp
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 Toshiba Corp filed Critical Toshiba Corp
Priority to JP29252597A priority Critical patent/JP3803184B2/en
Publication of JPH11132194A publication Critical patent/JPH11132194A/en
Application granted granted Critical
Publication of JP3803184B2 publication Critical patent/JP3803184B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Abstract

PROBLEM TO BE SOLVED: To reduce an air blowing noise, and increase an air blowing quantity by molding respective blades so that a cross section running along a circular arc in a prescribed radius forms a streamline shape in an axial flow fan by arranging plural blades along a peripheral surface of a cylindrical boss hub. SOLUTION: An axial flow fan of an air blower used for an outdoor unit of an air conditioner, is formed by arranging three blades 2 through a triangular rib 3 along a peripheral surface of a cylindrical boss hub 1 fitted to and installed on a rotary shaft of a fan motor. In the respective blades 2, its outer peripheral part 4 is formed into a curved shape where a front edge part 6 is projected larger than a connecting part 5 of the triangular rib 3 and the boss hub 1. In the respective blades 2, the front edge part 6 side is thick by being formed into a cross-sectional spindle shape, and has the almost same thickness toward a rear edge part 7 from an intermediate part, and is thin in a cross-sectional pointed shape over the front edge from the rear edge part 7 side, and a negative pressure surface is smoothly bent toward the rear edge part 7 and an outer peripheral part 4 from a maximum thickness part on the front edge part 6 side.

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【発明の属する技術分野】本発明は、たとえば空気調和
機の室外ユニットに配置され、吸込み側の熱交換器を介
して熱交換風を外部へ吹出す送風機であり、特に軸流フ
ァンにおけるブレードに関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a blower which is disposed, for example, in an outdoor unit of an air conditioner and blows heat exchange air to the outside through a heat exchanger on a suction side, and particularly relates to a blade in an axial fan. .

【0002】[0002]

【従来の技術】たとえば空気調和機の室外ユニットに
は、熱交換器と離間対向して送風機が配置されている。
この送風機は、ファン吸込み側を上記熱交換器に対向
し、吹出し側をユニット本体前面に設けられる吹出し口
に対向する。
2. Description of the Related Art For example, in an outdoor unit of an air conditioner, a blower is disposed so as to be opposed to a heat exchanger.
In this blower, the fan suction side faces the heat exchanger, and the blowout side faces a blowout port provided on the front surface of the unit main body.

【0003】送風機の構成は、ファンモータと、このフ
ァンモータの回転軸に嵌着されるファンとからなる。上
記ファンの形状構造の選択にあたっては、室外ユニット
の薄形化が促進されて内部スペースが狭く、かつ熱交換
器に対する熱交換効率を確保するために、軸流ファンが
多用される。
[0003] The structure of the blower is composed of a fan motor and a fan fitted to a rotating shaft of the fan motor. In selecting the shape of the fan, an axial fan is frequently used in order to promote the thinning of the outdoor unit, to reduce the internal space, and to ensure heat exchange efficiency with the heat exchanger.

【0004】上記軸流ファンは、ファンモータの回転軸
に嵌着される円筒状のボスハブと、このボスハブの周面
に沿って三角状リブを介して設けられる翼(以下、ブレ
ードと言う)とからなる。このブレードは、3枚もしく
は4枚が所定間隔を存して設けられる。
The axial fan has a cylindrical boss hub fitted on a rotating shaft of a fan motor, and blades (hereinafter referred to as blades) provided along triangular ribs along the peripheral surface of the boss hub. Consists of Three or four blades are provided at predetermined intervals.

【0005】[0005]

【発明が解決しようとする課題】ところで、従来の上記
ブレードは、半径rにおける円弧に沿う断面が均一な肉
厚であるか、あるいは前縁部のみ厚肉の形状であった。
そして、これらブレードを負圧面から見た状態で、前縁
部から後縁部まで滑らかに曲成されていない。
The conventional blade has a uniform thickness in the cross section along the circular arc at the radius r, or has a thicker shape only at the leading edge.
When viewed from the negative pressure surface, these blades are not smoothly curved from the front edge to the rear edge.

【0006】そのため、負圧面に発生する境界層乱れが
大きく、吹き出し後縁部に大きな渦(後流渦)が生成さ
れて送風騒音が増大する。特に前縁部のみ厚肉の場合
は、厚肉部と薄肉部との境界において境界層乱れが大き
くなり、大きな騒音発生の要因となっている。
[0006] Therefore, the boundary layer turbulence generated on the negative pressure surface is large, and a large vortex (wake vortex) is generated at the trailing edge of the blowout, thereby increasing the blowing noise. In particular, in the case where only the leading edge portion is thick, boundary layer turbulence increases at the boundary between the thick portion and the thin portion, which causes a large noise.

【0007】そして、上記ブレードの外周部における変
曲点位置は、前縁部長さと異なって設定されている。こ
の変曲点位置が前縁部長さより大の場合は、送風騒音が
低くなる反面風量が減少し、また変曲点位置が前縁部長
さよりも小の場合は、逆に風量は増大するが送風騒音は
高くなる。
The position of the inflection point on the outer periphery of the blade is set differently from the length of the leading edge. When this inflection point position is larger than the front edge length, the airflow noise decreases, but the air volume decreases, and when the inflection point position is smaller than the front edge length, the air volume increases but the airflow increases. The noise increases.

【0008】また、上記三角状リブと連結されるブレー
ド後縁部の位置について、回転軸方向および回転方向に
対する取付け角度によって、回転中のファンモータにか
かる負荷が変化することが知られている。
It is also known that the load applied to the rotating fan motor varies depending on the position of the trailing edge of the blade connected to the triangular rib and the direction of rotation with respect to the rotation axis and the rotation direction.

【0009】従来のファンでは、ブレードの弦長とファ
ン高さから決定されるブレード取付け角度が、回転軸方
向および回転方向に対する取付け角度より大きく設定さ
れているので、モータへの負荷も大きくなっている。
In the conventional fan, since the blade mounting angle determined from the chord length of the blade and the fan height is set to be larger than the mounting angle with respect to the rotation axis direction and the rotation direction, the load on the motor also increases. I have.

【0010】本発明は、上記事情に鑑みなされたもので
あり、その目的とするところは、ファンモータに対する
負荷の低減を図って、送風騒音の低減化を得るとともに
送風量の増大化をなして、送風性能の向上を図れるブレ
ードを備えた軸流ファンを提供しようとするものであ
る。
The present invention has been made in view of the above circumstances, and an object of the present invention is to reduce the load on the fan motor, thereby reducing the blowing noise and increasing the blowing amount. Another object of the present invention is to provide an axial fan having a blade capable of improving the blowing performance.

【0011】[0011]

【課題を解決するための手段】上記目的を満足するため
本発明の軸流ファンは、請求項1として、円筒状のボス
ハブの周面に沿って複数枚の翼であるブレードが設けら
れてなる軸流ファンであり、上記ブレードは、所定の半
径rにおける円弧に沿う断面が、流線形状をなすよう成
形されることを特徴とする。
According to a first aspect of the present invention, there is provided an axial-flow fan comprising a plurality of blades along a peripheral surface of a cylindrical boss hub. An axial fan, wherein the blade is formed so that a cross section along an arc at a predetermined radius r forms a streamline shape.

【0012】請求項2として、請求項1記載の軸流ファ
ンにおいて、上記ブレードは、前縁部側の最大厚部から
後縁部と外周部に向かって滑らかに負圧面が曲成される
ことを特徴とする。
According to a second aspect of the present invention, in the axial flow fan according to the first aspect, the negative pressure surface of the blade is smoothly curved from a maximum thickness portion on a front edge portion side to a rear edge portion and an outer peripheral portion. It is characterized by.

【0013】請求項3として、請求項1記載の軸流ファ
ンにおいて、上記ブレードは、前縁部と後縁部それぞれ
の長さの中点を通る前縁R部と後縁R部の接垂線(接線
に対して垂直な線)に沿う断面で、前縁部および後縁部
の断面厚さの比率が、前縁部厚さ:後縁部厚さ=3:1
となすよう設定されることを特徴とする。
According to a third aspect of the present invention, in the axial flow fan according to the first aspect, the blade is perpendicular to a leading edge R and a trailing edge R passing through a midpoint of the length of each of the leading edge and the trailing edge. In the cross section along the line (perpendicular to the tangent), the ratio of the cross-sectional thicknesses of the leading edge and the trailing edge is: leading edge thickness: trailing edge thickness = 3: 1.
Is set to be

【0014】請求項4として、請求項1記載の軸流ファ
ンにおいて、上記ブレードは、外周部と前縁部との間に
形成されるR部の中点から外周部側へ向かって前縁部長
さと同じ長さのところへブレード変曲点Pが設けられ、
前縁部から上記変曲点までは吹き出し側へ突出され、変
曲点Pから後縁部までは吸込み側へ突出されることを特
徴とする。
According to a fourth aspect of the present invention, in the axial flow fan according to the first aspect, the blade has a front edge length extending from a midpoint of an R portion formed between the outer circumference and the front edge toward the outer circumference. A blade inflection point P is provided at the same length as
It is characterized in that it projects from the leading edge to the above-mentioned inflection point toward the outlet side, and projects from the inflection point P to the trailing edge toward the suction side.

【0015】請求項5として、請求項1記載の軸流ファ
ンにおいて、上記ボスハブとブレードとの間に、ブレー
ド取付け部である三角状リブが形成され、この三角状リ
ブと後縁部との交点をMとし、外周部と後縁部の交点を
Nとし、ファン回転中心をOとしたとき、直線ON=
(2.2〜2.4)×直線OMとなすよう設定されるこ
とを特徴とする。
According to a fifth aspect of the present invention, in the axial flow fan according to the first aspect, a triangular rib serving as a blade mounting portion is formed between the boss hub and the blade, and an intersection between the triangular rib and a trailing edge portion. Is M, the intersection of the outer peripheral portion and the rear edge portion is N, and the center of rotation of the fan is O, the straight line ON =
(2.2 to 2.4) × the straight line OM.

【0016】請求項6として、請求項5記載の軸流ファ
ンにおいて、上記直線ONと、直線OMとのなす角度θ
は、15°〜20°の範囲となすよう設定されることを
特徴とする。
According to a sixth aspect, in the axial fan according to the fifth aspect, an angle θ between the straight line ON and the straight line OM is defined.
Is set to be in the range of 15 ° to 20 °.

【0017】請求項7として、請求項5記載の軸流ファ
ンにおいて、上記前縁部と外周部との交点Sとファン回
転中心Oとを結ぶ直線OSと、上記直線OMとのなす角
度βは、95°〜105°の範囲となすよう設定される
ことを特徴とする。
According to a seventh aspect of the present invention, in the axial flow fan according to the fifth aspect, an angle β formed between a straight line OS connecting an intersection S between the front edge portion and the outer peripheral portion and the center of rotation O of the fan and the straight line OM is , 95 ° to 105 °.

【0018】請求項8として、請求項5記載の軸流ファ
ンにおいて、上記直線OMと、上記ボスハブのファン回
転軸と垂直な面とのなす角度αは、直線OMと直線ON
とのなす角度θと同じ範囲(15°〜20°)となすよ
う設定されることを特徴とする。
According to an eighth aspect of the present invention, in the axial flow fan according to the fifth aspect, an angle α formed between the straight line OM and a plane perpendicular to the fan rotation axis of the boss hub is equal to the straight line OM and the straight line ON.
Are set to be in the same range (15 ° to 20 °) as the angle θ formed by

【0019】請求項9として、請求項5記載の軸流ファ
ンにおいて、上記直線OMと直線ONとのなす角度θ
は、ブレード取付け角γ(sinγ=弦長CL/ファン
高さH)に対して、γ>θとなすよう設定されることを
特徴とする。
According to a ninth aspect, in the axial flow fan according to the fifth aspect, an angle θ between the straight line OM and the straight line ON is provided.
Is set to satisfy γ> θ with respect to the blade mounting angle γ (sin γ = string length CL / fan height H).

【0020】このような課題を解決するための手段を採
用することにより、ファンモータに対する負荷の低減を
図って、送風騒音の低減化を得るとともに送風量の増大
化をなして、送風性能の向上を得る。
By adopting the means for solving such a problem, the load on the fan motor is reduced, the blowing noise is reduced, and the blowing volume is increased to improve the blowing performance. Get.

【0021】[0021]

【発明の実施の形態】以下、本発明の一実施の形態を、
図面を参照して説明する。図1は、たとえば空気調和機
の室外ユニットに用いられる送風機の軸流ファンの吹き
出し側である正圧面側を示す。
DESCRIPTION OF THE PREFERRED EMBODIMENTS Hereinafter, an embodiment of the present invention will be described.
This will be described with reference to the drawings. FIG. 1 shows, for example, a positive pressure surface side which is an outlet side of an axial fan of a blower used for an outdoor unit of an air conditioner.

【0022】この軸流ファンは、図示しないファンモー
タの回転軸に嵌着される円筒状のボスハブ1と、このボ
スハブ1の周面に沿って設けられた翼であるブレード2
とからなる。
The axial flow fan includes a cylindrical boss hub 1 fitted on a rotating shaft of a fan motor (not shown), and blades 2 as wings provided along a peripheral surface of the boss hub 1.
Consists of

【0023】そして、ブレード2のボスハブ1連結部分
には、三角状リブ3が介在される。この三角状リブ3の
正圧面側は三角枠状をなすが、吸込み側である負圧面側
は蓋部によって閉成されている。
Then, a triangular rib 3 is interposed at the connecting portion of the boss hub 1 of the blade 2. The pressure side of the triangular rib 3 has a triangular frame shape, while the suction side, which is the suction side, is closed by a lid.

【0024】上記複数枚のブレード2は、この外周部4
が三角状リブ3とボスハブ1との連結部5に比べて回転
方向側である前縁部6に大きく突き出す一方、反回転方
向側である後縁部7は、回転方向とほぼ直交する方向に
大きな曲率半径の曲線状に形成される。
The above-mentioned plurality of blades 2
Of the triangular rib 3 and the connecting portion 5 of the boss hub 1 protrude largely to the front edge 6 on the rotation direction side, while the rear edge 7 on the anti-rotation direction side extends in a direction substantially orthogonal to the rotation direction. It is formed in a curved shape with a large radius of curvature.

【0025】図2(A)は、ボスハブ1に対して1枚の
ブレード2のみを取り出して、正圧面側から示す。ボス
ハブ1中心であるファン回転中心をOとして、所定の半
径rにおける円弧を描いたとき、この円弧状線3F−3
Fに沿って切断したブレード2の断面は、図3で示すよ
うになる。
FIG. 2A shows only one blade 2 taken out from the boss hub 1 and shown from the pressure side. When an arc having a predetermined radius r is drawn with the fan rotation center which is the center of the boss hub 1 as O, this arc-shaped line 3F-3
A cross section of the blade 2 cut along F is as shown in FIG.

【0026】すなわち、ブレード2は、前縁部6側が断
面紡錘状に形成されて厚く、中間部から後縁部7に向か
ってほぼ同一の厚さであり、後縁部7側から端縁に亘っ
て断面尖鋭状の薄肉に形成される。
That is, the blade 2 is thick at the front edge 6 side and is formed to have a spindle shape in cross section, has substantially the same thickness from the middle portion to the rear edge 7, and extends from the rear edge 7 side to the edge. It is formed to be thin with a sharp cross section throughout.

【0027】また、図5に示すように、ブレード2の負
圧面においては、その前縁部6における流線形断面の最
大厚部に沿うa〜a線から、後縁部7および外周部4に
向かって滑らかに曲成されている。
As shown in FIG. 5, on the negative pressure surface of the blade 2, the leading edge 6 extends from the line a to a along the maximum thickness portion of the streamlined section to the trailing edge 7 and the outer peripheral portion 4. It is smoothly curved toward.

【0028】再び図2(A)および同図(B)に示すよ
うに、ブレード2において、外周部4と前縁部6との間
に形成されるR部の中点8から外周部4側へ向かって前
縁部6長さと同じ長さのところへ、ブレード変曲点Pが
設けられる。
As shown in FIGS. 2A and 2B again, in the blade 2, the middle portion 8 of the R portion formed between the outer peripheral portion 4 and the front edge portion 6 extends from the midpoint 8 to the outer peripheral portion 4 side. A blade inflection point P is provided at the same length as the length of the front edge 6 toward the blade.

【0029】再び図3で示すように、軸流ファンの回転
方向におけるブレード2の断面は、前縁部6から変曲点
Pまでが吹き出し側へ突出し、変曲点Pから後縁部7ま
では吸込み側へ突出させた複合曲面となっている。
As shown in FIG. 3 again, the cross section of the blade 2 in the direction of rotation of the axial fan is such that the portion from the leading edge 6 to the inflection point P projects toward the blowing side, and the portion from the inflection point P to the trailing edge 7. Has a compound curved surface protruding toward the suction side.

【0030】図6(A)に示すように、ブレード2の前
縁部6と後縁部7において、それぞれの長さの中点b,
cを通る前縁R部と後縁R部の接垂線(接線に対する垂
直な線)4B−4B,4C−4Cに沿って断面した形状
を、同図(B)と同図(C)で示す。
As shown in FIG. 6A, at the leading edge 6 and the trailing edge 7 of the blade 2, the midpoints b,
(B) and (C) show cross sections taken along perpendicular lines (perpendicular to the tangent line) 4B-4B and 4C-4C of the leading edge R and trailing edge R passing through c. .

【0031】同図(B)は前縁部6側の断面形状であ
り、同図(C)は後縁部7側の断面形状である。すなわ
ち、先に図3において後縁部7の断面は尖鋭状として説
明したが、実際には最小限の厚さが確保されている。
FIG. 3B shows a cross-sectional shape on the front edge portion 6 side, and FIG. 3C shows a cross-sectional shape on the rear edge portion 7 side. That is, although the cross section of the trailing edge portion 7 has been described in FIG. 3 as being sharp, the minimum thickness is actually secured.

【0032】そして、ここでは上記部位4B−4B,4
C−4Cにおいて前縁部6および後縁部7を切断した断
面厚さの比率が、前縁部6厚さ:後縁部7厚さ=3:1
となるように設定されている。
In this case, the portions 4B-4B, 4
In C-4C, the ratio of the cross-sectional thickness obtained by cutting the leading edge 6 and the trailing edge 7 is such that the leading edge 6 thickness: the trailing edge 7 thickness = 3: 1.
It is set to be.

【0033】図7に示すように、ボスハブ1とブレード
2との間の三角状リブ3と、後縁部7との交点をMと
し、かつ外周部4と後縁部7の交点をNとしたとき、フ
ァン回転中心Oと交点Nとを結ぶ直線ONが、ファン回
転中心Oと交点Mとを結ぶ直線OMの2.2〜2.4倍
となすよう設定されている。
As shown in FIG. 7, the intersection between the triangular rib 3 between the boss hub 1 and the blade 2 and the rear edge 7 is M, and the intersection between the outer peripheral portion 4 and the rear edge 7 is N. At this time, the straight line ON connecting the fan rotation center O and the intersection point N is set to be 2.2 to 2.4 times the straight line OM connecting the fan rotation center O and the intersection point M.

【0034】そして、上記直線ONと、直線OMとのな
す角度θが、15°〜20°の範囲となすよう設定され
ている。また、前縁部6と外周部4との交点をSとし、
ファン回転中心Oとを結ぶ直線OSと、上記直線OMと
のなす角度βが、95°〜105°の範囲となすよう設
定されている。
The angle θ between the straight line ON and the straight line OM is set to be in the range of 15 ° to 20 °. Also, the intersection of the front edge 6 and the outer periphery 4 is denoted by S,
The angle β between the straight line OS connecting the fan rotation center O and the straight line OM is set to be in the range of 95 ° to 105 °.

【0035】図8に示すように、上記直線OMと、ファ
ン回転軸OLに垂直なボスハブ上面1aとのなす角度α
は、先に説明した直線OMと直線ONとのなす角度θ
と、同じ範囲である15°〜20°となるよう設定され
ている。
As shown in FIG. 8, the angle α between the straight line OM and the boss hub upper surface 1a perpendicular to the fan rotation axis OL.
Is the angle θ between the straight line OM and the straight line ON described above.
Is set in the same range of 15 ° to 20 °.

【0036】図9に示すように、上記直線OMと直線O
Nとのなす角度θは、ブレード取付け角γ(sinγ=
弦長CL/ファン高さH)よりも小さく(γ>θ)なす
よう設定されている。
As shown in FIG. 9, the straight line OM and the straight line O
The angle θ made with N is the blade mounting angle γ (sin γ =
It is set to be smaller than the chord length CL / fan height H (γ> θ).

【0037】このようにして構成される軸流ファンのブ
レード2であって、以下に述べるような特性を有する。
すなわち、ブレード2は、所定半径rの円弧に沿う断面
を流線形状とした。そしてブレード2は、前縁部6側の
最大厚部から後縁部7と外周部4に向かって滑らかに負
圧面が曲成される。前縁部6と後縁部7の長さの中点を
通る前縁R部および後縁R部の接垂線に沿う断面で、前
縁部厚さ:後縁部厚さ=3:1となるように設定した。
The blade 2 of the axial fan configured as described above has the following characteristics.
That is, the blade 2 has a streamlined cross section along an arc having a predetermined radius r. The negative pressure surface of the blade 2 is smoothly curved from the thickest portion on the front edge portion 6 side to the rear edge portion 7 and the outer peripheral portion 4. The cross section along the tangent line of the leading edge R and the trailing edge R passing through the midpoint of the length of the leading edge 6 and the trailing edge 7, where the leading edge thickness: the trailing edge thickness = 3: 1. It was set to become.

【0038】その結果、図4(A)に示すように、ブレ
ード2面の風流れによって発生する境界層乱れKが小さ
くなり、吹き出し後縁部7付近にできる後流渦Zが減少
し、送風騒音が小さくなる。
As a result, as shown in FIG. 4A, the boundary layer turbulence K generated by the wind flow on the blade 2 surface is reduced, and the wake vortex Z formed near the trailing edge 7 of the blowout is reduced. Noise is reduced.

【0039】これに対して同図(B)に示すように、従
来の均一肉厚のブレード2Aの場合および同図(C)に
示すように、従来の前縁部のみ厚肉としたブレード2B
の場合は、いずれも風流れによって発生する境界層乱れ
Ka,Kbが大きく、後縁部付近にできる後流渦Za,
Zbが大きく生成して、送風騒音が大きい。
On the other hand, as shown in FIG. 3B, the conventional blade 2A having a uniform thickness and the conventional blade 2B having a thicker front edge only as shown in FIG.
In both cases, the boundary layer turbulences Ka and Kb generated by the wind flow are large, and the wake vortices Za and K formed near the trailing edge.
Zb is generated large, and the blowing noise is large.

【0040】また、上記ブレード2は、外周部4と前縁
部6との間に形成されるR部の中点8から外周部4側へ
向かって前縁部6長さと同じ長さのところへブレード変
曲点Pを設けた。
The blade 2 has the same length as the front edge portion 6 from the midpoint 8 of the R portion formed between the outer peripheral portion 4 and the front edge portion 6 toward the outer peripheral portion 4. A blade inflection point P was provided.

【0041】上記変曲点Pの位置によって、ブレード2
面上の風の流れが変化することが知られている。外周部
4における変曲点P位置が前縁部6長さよりも大の場合
は、送風騒音が低くなるが風量が減少する。変曲点P位
置が前縁部6長さよりも小の場合は、逆に風量が増大す
るが、送風騒音が高くなる。そこで、先に説明したよう
に、変曲点Pの位置を前縁部6長さと同じ長さにしたの
で、送風騒音と風量のバランスがよくなる。
Depending on the position of the inflection point P, the blade 2
It is known that the flow of wind over a surface changes. When the position of the inflection point P on the outer peripheral portion 4 is larger than the length of the front edge portion 6, the blowing noise decreases but the air volume decreases. When the position of the inflection point P is smaller than the length of the front edge portion 6, the air volume increases, but the blowing noise increases. Therefore, as described above, the position of the inflection point P is set to the same length as the front edge portion 6, so that the balance between the blowing noise and the air volume is improved.

【0042】また、直線ONを2.2〜2.4×直線O
Mの範囲に設定した。直線ONと直線OMとのなす角度
θを15°〜20°の範囲に設定した。直線OSと直線
OMとのなす角度βを95°〜105°の範囲に設定し
た。
Further, the straight line ON is set to 2.2 to 2.4 × the straight line O.
M was set in the range. The angle θ between the straight line ON and the straight line OM was set in a range of 15 ° to 20 °. The angle β between the straight line OS and the straight line OM was set in the range of 95 ° to 105 °.

【0043】これらの設定によつて、後述するようにフ
ァン回転軸OLに対して垂直な面における後縁部7の位
置と、後縁部7に対する前縁部6の位置についての有効
な条件が揃うことになる。
With these settings, as will be described later, effective conditions for the position of the trailing edge 7 on a plane perpendicular to the fan rotation axis OL and the position of the leading edge 6 with respect to the trailing edge 7 are set. It will be aligned.

【0044】すなわち、ファン回転軸OLに対して垂直
な面で見た場合、後縁部7の位置(直線MNの位置)が
ファン回転中心Oから後縁部7の終端Nを結ぶ直線(基
準線ON)に対してどの位置にあるかによって、回転中
のファンモータにかかる負荷が変化する。
That is, when viewed from a plane perpendicular to the fan rotation axis OL, the position of the rear edge 7 (the position of the straight line MN) is a straight line (reference line) connecting the fan rotation center O to the end N of the rear edge 7. The load on the rotating fan motor changes depending on the position with respect to the line (ON).

【0045】基準線ONに対して後縁部7の位置(直線
MNの位置)が図の上方にある場合、換言すれば直線O
Mと直線ONとのなす角度θが大きいと、ファンモータ
にかかる負荷が大きくなる。
When the position of the trailing edge 7 (the position of the straight line MN) is above the drawing with respect to the reference line ON, in other words, the straight line O
If the angle θ between M and the straight line ON is large, the load on the fan motor increases.

【0046】そこで、先に述べたように、ON=2.2
〜2.4×OMとするとともに、θ=15°〜20°と
して後縁部7位置(直線MNの位置)の最適化をなす。
さらにまた、後縁部7に対する前縁部6の位置について
も、β=95〜105°に設定することにより、前縁部
6位置の最適化が行われて、大風量でもファンモータに
かかる負荷をより小さく抑えられる。
Therefore, as described above, ON = 2.2.
22.4 × OM, and θ = 15 ° -20 ° to optimize the position of the trailing edge 7 (the position of the straight line MN).
Furthermore, the position of the leading edge 6 with respect to the trailing edge 7 is also set to β = 95 to 105 °, so that the position of the leading edge 6 is optimized, and the load applied to the fan motor even when the air volume is large. Can be kept smaller.

【0047】また、直線OMと、ボスハブ上面1aとの
なす角度αは、直線OMと直線ONとのなす角度θと、
同じ範囲である15°〜20°に設定した。直線OMと
直線ONとのなす角度θは、ブレード取付け角γ(si
nγ=弦長CL/ファン高さH)よりも小さく(γ>
θ)なるよう設定した。
The angle α between the straight line OM and the boss hub upper surface 1a is the angle θ between the straight line OM and the straight line ON,
The same range, 15 ° to 20 °, was set. The angle θ between the straight line OM and the straight line ON is the blade mounting angle γ (si
nγ = string length CL / fan height H) (γ>
θ).

【0048】このような角度設定により、ファン回転軸
OL方向に対する後縁部7の位置が定まる。すなわち、
図8におけるXZ面に対して見たときも、後縁部7の位
置(直線MNの位置)がブレードXZ面の基準線q(ボ
スハブ上面1aをX方向へ延長した直線)に対してどの
位置にあるかによって、回転中のファンモータにかかる
負荷が変化する。
The position of the trailing edge 7 in the direction of the fan rotation axis OL is determined by such an angle setting. That is,
8, when viewed from the XZ plane, the position of the trailing edge 7 (the position of the straight line MN) is any position relative to the reference line q of the blade XZ plane (the straight line extending from the boss hub upper surface 1a in the X direction). , The load applied to the rotating fan motor changes.

【0049】後縁部7の位置(直線MNの位置)がボス
ハブ上面1aから離間するにしたがって、すなわち直線
OMとボスハブ上面1aのなす角度αが大きくなるにし
たがって、ファンモータにかかる負荷が大きくなる。
As the position of the trailing edge 7 (the position of the straight line MN) moves away from the boss hub upper surface 1a, that is, as the angle α between the straight line OM and the boss hub upper surface 1a increases, the load on the fan motor increases. .

【0050】そこで、先に説明した角度α=θ=15°
〜20°で、かつγ>θの関係を設定して、ファン回転
軸OL方向に対する後縁部7の位置(直線MNの位置)
を最適化し、大風量でもファンモータにかかる負荷を小
さく抑えられる。
Therefore, the previously described angle α = θ = 15 °
20 ° and a relationship of γ> θ is set, and the position of the trailing edge 7 in the direction of the fan rotation axis OL (the position of the straight line MN)
And the load on the fan motor can be kept small even with a large air volume.

【0051】[0051]

【発明の効果】以上説明したように本発明は、ファン半
径Rに沿って切断した断面が流線形状をなすブレードを
備えたから、ファンモータに対する負荷の低減を図っ
て、送風騒音の低減化を得るとともに送風量の増大化を
なし、送風性能の向上を得るなどの効果を奏する。
As described above, according to the present invention, since the cross section cut along the fan radius R is provided with a blade having a streamlined shape, the load on the fan motor is reduced and the blowing noise is reduced. In addition to this, there is an effect that the amount of air blow is increased and the air blowing performance is improved.

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

【図1】本発明における一実施の形態を示す、軸流ファ
ンの正圧側から見た正面図。
FIG. 1 is a front view showing an embodiment of the present invention, as viewed from a positive pressure side of an axial fan.

【図2】(A)は、同実施の形態の、ボスハブと1枚の
ブレードの正圧側から見た正面図。(B)は、ブレード
一部の拡大図。
FIG. 2A is a front view of the boss hub and one blade viewed from the positive pressure side in the embodiment. (B) is an enlarged view of a part of the blade.

【図3】同実施の形態の、ブレードの半径Rにおける円
弧に沿う断面図。
FIG. 3 is a cross-sectional view of the embodiment along an arc at a radius R of the blade.

【図4】(A)は、同実施の形態の、ブレードに沿う風
の流れの特性図。(B)は、従来のブレードに沿う風の
流れの特性図。(C)は、さらに異なる従来のブレード
に沿う風の流れの特性図。
FIG. 4A is a characteristic diagram of a flow of wind along a blade according to the embodiment. (B) is a characteristic diagram of a wind flow along a conventional blade. (C) is a characteristic diagram of the wind flow along a different conventional blade.

【図5】同実施の形態の、ブレード負圧面側から見た前
縁部最大厚部と後縁部前縁部および外周部の位置を説明
する図。
FIG. 5 is a view for explaining positions of a leading edge maximum thickness portion, a trailing edge, a leading edge, and an outer peripheral portion as viewed from the blade negative pressure surface side in the embodiment.

【図6】(A)は、同実施の形態の、ブレードの前縁部
と後縁部におけるそれぞれの長さの中点を通る前縁R部
と後縁R部の接垂線の位置を説明する図。(B)は、図
6(A)の4B−4B線に沿う断面図。(C)は、図6
(A)の4C−4C線に沿う断面図。
FIG. 6A illustrates positions of perpendicular lines of a leading edge R and a trailing edge R passing through a middle point of each length of the leading edge and the trailing edge of the blade in the embodiment. Figure to do. (B) is sectional drawing which follows the 4B-4B line | wire of FIG. 6 (A). (C) shows FIG.
Sectional drawing which follows the 4C-4C line of (A).

【図7】(A)は、同実施の形態の、ファン回転軸に対
して垂直な面で見たブレード後縁部位置を説明する図。
(B)は、ブレード一部の拡大図。
FIG. 7A is a diagram illustrating the position of the trailing edge of the blade viewed from a plane perpendicular to the fan rotation axis according to the embodiment;
(B) is an enlarged view of a part of the blade.

【図8】同実施の形態の、ファン回転軸方向に沿って見
たブレード後縁部位置を説明する図。
FIG. 8 is a view for explaining the position of the trailing edge of the blade as viewed along the direction of the fan rotation axis according to the embodiment;

【図9】同実施の形態の、ボスハブに対するブレードの
取付け角度を説明する図。
FIG. 9 is a diagram illustrating an attachment angle of the blade to the boss hub according to the embodiment.

【符号の説明】[Explanation of symbols]

1…ボスハブ、 2…ブレード、 4…前縁部、 7…後縁部、 3…三角状リブ。 1 boss hub, 2 blade, 4 front edge, 7 rear edge, 3 triangular rib.

Claims (9)

【特許請求の範囲】[Claims] 【請求項1】円筒状のボスハブの周面に沿って複数枚の
翼であるブレードが設けられてなる軸流ファンであり、 上記ブレードは、所定の半径rにおける円弧に沿う断面
が、流線形状をなすように成形されることを特徴とする
軸流ファン。
1. An axial flow fan comprising a plurality of blades provided along a peripheral surface of a cylindrical boss hub, wherein the blade has a streamline cross section along an arc at a predetermined radius r. An axial fan characterized by being formed into a shape.
【請求項2】上記ブレードは、前縁部側の最大厚部から
後縁部と外周部に向かって滑らかに負圧面が曲成される
ことを特徴とする請求項1記載の軸流ファン。
2. The axial flow fan according to claim 1, wherein said blade has a negative pressure surface smoothly curved from a maximum thickness portion on a front edge portion side to a rear edge portion and an outer peripheral portion.
【請求項3】上記ブレードは、前縁部と後縁部それぞれ
の長さの中点を通る前縁R部と後縁R部の接垂線(接線
に対して垂直な線)に沿う断面で、前縁部および後縁部
の断面厚さの比率が、前縁部厚さ:後縁部厚さ=3:1
となすよう設定されることを特徴とする請求項1記載の
軸流ファン。
3. The blade according to claim 1, wherein the blade has a cross section along a tangent line (a line perpendicular to the tangent line) of the leading edge portion and the trailing edge portion passing through the midpoint of the respective lengths of the leading edge portion and the trailing edge portion. , The ratio of the cross-sectional thicknesses of the leading edge and the trailing edge is: leading edge thickness: trailing edge thickness = 3: 1
The axial flow fan according to claim 1, wherein the axial flow fan is set to:
【請求項4】上記ブレードは、外周部と前縁部との間に
形成されるR部の中点から外周部側へ向かって前縁部長
さと同じ長さのところへブレード変曲点Pが設けられ、 前縁部から上記変曲点までは吹き出し側へ突出され、変
曲点Pから後縁部までは吸込み側へ突出されることを特
徴とする請求項1記載の軸流ファン。
4. The blade has a blade inflection point P at the same length as the front edge portion from the midpoint of the R portion formed between the outer peripheral portion and the front edge portion toward the outer peripheral portion. 2. The axial flow fan according to claim 1, wherein the axial flow fan is provided so as to protrude from the front edge portion to the inflection point toward the blowing side, and protrude from the inflection point P to the rear edge portion toward the suction side.
【請求項5】上記ボスハブとブレードとの間に、ブレー
ド取付け部である三角状リブが形成され、この三角状リ
ブと後縁部との交点をMとし、外周部と後縁部の交点を
Nとし、ファン回転中心をOとしたとき、直線ON=
(2.2〜2.4)×直線OMとなすよう設定されるこ
とを特徴とする請求項1記載の軸流ファン。
5. A triangular rib, which is a blade mounting portion, is formed between the boss hub and the blade. An intersection between the triangular rib and the rear edge is defined as M, and an intersection between the outer peripheral portion and the rear edge is defined as M. When N is set and the rotation center of the fan is set to O, the straight line ON =
2. The axial flow fan according to claim 1, wherein the axial flow fan is set so as to form (2.2-2.4) × straight line OM.
【請求項6】上記直線ONと、直線OMとのなす角度θ
は、15°〜20°の範囲となすよう設定されることを
特徴とする請求項5記載の軸流ファン。
6. An angle θ between the straight line ON and the straight line OM.
The axial fan according to claim 5, wherein the angle is set to be in a range of 15 ° to 20 °.
【請求項7】上記ブレード前縁部と外周部との交点Sと
ファン回転中心部Oとを結ぶ直線OSと、上記直線OM
とのなす角度βは、95°〜105°の範囲となすよう
設定されることを特徴とする請求項5記載の軸流ファ
ン。
7. A straight line OS connecting an intersection point S between the blade leading edge portion and the outer peripheral portion and a fan rotation center portion O;
6. The axial flow fan according to claim 5, wherein the angle β is set to be in a range of 95 ° to 105 °.
【請求項8】上記直線OMと、上記ボスハブのファン回
転軸と垂直な面とのなす角度αは、直線OMと直線ON
とのなす角度θと同じ範囲(15°〜20°)となすよ
う設定されることを特徴とする請求項5記載の軸流ファ
ン。
8. An angle α between the straight line OM and a plane perpendicular to the fan rotation axis of the boss hub is defined by a straight line OM and a straight line ON.
The axial flow fan according to claim 5, wherein the angle? Is set to be in the same range (15 to 20) as the angle?
【請求項9】上記直線OMと直線ONとのなす角度θ
は、ブレード取付け角γ(sinγ=弦長CL/ファン
高さH)に対して、γ>θとなすよう設定されることを
特徴とする請求項5記載の軸流ファン。
9. An angle θ between the straight line OM and the straight line ON.
6. The axial flow fan according to claim 5, wherein is set so that γ> θ with respect to a blade mounting angle γ (sin γ = string length CL / fan height H).
JP29252597A 1997-10-24 1997-10-24 Axial fan Expired - Lifetime JP3803184B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP29252597A JP3803184B2 (en) 1997-10-24 1997-10-24 Axial fan

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP29252597A JP3803184B2 (en) 1997-10-24 1997-10-24 Axial fan

Publications (2)

Publication Number Publication Date
JPH11132194A true JPH11132194A (en) 1999-05-18
JP3803184B2 JP3803184B2 (en) 2006-08-02

Family

ID=17782943

Family Applications (1)

Application Number Title Priority Date Filing Date
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Country Status (1)

Country Link
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Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100487339B1 (en) * 2002-11-18 2005-05-03 엘지전자 주식회사 axial flow fan
KR100487375B1 (en) * 2002-11-21 2005-05-03 엘지전자 주식회사 axial flow fan
JP2013517406A (en) * 2010-01-12 2013-05-16 雪龍集団有限公司 Energy saving fan
CN106287959A (en) * 2016-08-17 2017-01-04 芜湖美智空调设备有限公司 Stator blade wind wheel, cabinet air-conditioner and air-conditioner
CN107725478A (en) * 2017-11-23 2018-02-23 珠海格力电器股份有限公司 Fan blade and fan
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WO2019153535A1 (en) * 2018-02-07 2019-08-15 广东美的制冷设备有限公司 Axial flow fan and air conditioner
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Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100487339B1 (en) * 2002-11-18 2005-05-03 엘지전자 주식회사 axial flow fan
KR100487375B1 (en) * 2002-11-21 2005-05-03 엘지전자 주식회사 axial flow fan
JP2013517406A (en) * 2010-01-12 2013-05-16 雪龍集団有限公司 Energy saving fan
TWI625467B (en) * 2016-07-27 2018-06-01 Sharp Kk Propeller fan and fluid delivery device
CN106287959A (en) * 2016-08-17 2017-01-04 芜湖美智空调设备有限公司 Stator blade wind wheel, cabinet air-conditioner and air-conditioner
CN106287959B (en) * 2016-08-17 2022-03-22 芜湖美智空调设备有限公司 Quiet leaf wind wheel, cabinet air conditioner and air conditioner
CN107725478A (en) * 2017-11-23 2018-02-23 珠海格力电器股份有限公司 Fan blade and fan
WO2019153535A1 (en) * 2018-02-07 2019-08-15 广东美的制冷设备有限公司 Axial flow fan and air conditioner
US11306729B2 (en) 2018-02-07 2022-04-19 Gd Midea Air-Conditioning Equipment Co., Ltd. Axial flow impeller and air conditioner
CN108180169A (en) * 2018-02-09 2018-06-19 广东美的厨房电器制造有限公司 Fan and micro-wave oven
CN116783394A (en) * 2021-01-21 2023-09-19 大金工业株式会社 Axial fan and air conditioner
CN116783394B (en) * 2021-01-21 2024-04-26 大金工业株式会社 Axial fan and air conditioner

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