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JPS60156997A - Centrifugal type blower fan - Google Patents

Centrifugal type blower fan

Info

Publication number
JPS60156997A
JPS60156997A JP1288484A JP1288484A JPS60156997A JP S60156997 A JPS60156997 A JP S60156997A JP 1288484 A JP1288484 A JP 1288484A JP 1288484 A JP1288484 A JP 1288484A JP S60156997 A JPS60156997 A JP S60156997A
Authority
JP
Japan
Prior art keywords
blade
disc
disk
centrifugal blower
blower 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.)
Pending
Application number
JP1288484A
Other languages
Japanese (ja)
Inventor
Koji Ito
功治 伊藤
Sei Tamaru
田丸 聖
Masashi Takagi
正支 高木
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 JP1288484A priority Critical patent/JPS60156997A/en
Publication of JPS60156997A publication Critical patent/JPS60156997A/en
Pending legal-status Critical Current

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Abstract

PURPOSE:To prevent exfoliation of an air current and reduce a noise and further improve efficiency of ventilation and strength of a blade by shaping a wing of each blade in such a manner as its thickness near the lifting line is large in the basal part to a disc and is gradually reduced as it parts from the disc. CONSTITUTION:The shape of a wing of a blade 2 is, as illustrated, such that its thickness near the lifting lines 21A-23A is large in the basal part to a disc 3, that is, on the swelling side face 31 of the disc 3, and is gradually reduced as it parts from said disc. This prevents exfoliation of an air current from the blade 2 and pressure change of the air current does not occur, and a noise can be prevented. Further, since the tip part of the blade 2 is shaped like a thin plate, the loss of the air current is small and the efficiency of ventilation is largely improved. Furthermore, since the tip part is shaped like a thin plate, the mass of the tip part is reduced. On the other hand, since the thickness of the basal part is shaped large, combined dimensions with the disc 3 can be largely taken and the strength of the blade 2 is augmented.

Description

【発明の詳細な説明】 [分野] 本発明は、遠心式送風機用ファンの騒音低減に関する。[Detailed description of the invention] [Field] The present invention relates to noise reduction in a fan for a centrifugal blower.

[従来技術] 遠心式送風機は、第3図に示す如く上方に空気流入口6
1を有し、外周に空気吐出口62を有する円筒状のケー
シング6と、該ケーシング6内に前記空気流入口61に
対応して配された遠心式送風機用ファン1と、遠心式送
風機用ファンlの駆動用モータ5とからなり、遠心式送
風機用ファン1は、中心部が一方に膨出した円盤状のデ
ィスク3と、一端が前記ディスク3の膨出がわ面に固着
され前記ディスク3の外周から等間隔で筒面状に列設さ
れ翼列を形成する多数のブレード2とから構成され、各
ブレード2の大型は製造上の観点から第1図に示す如く
前縁24Aから後縁25Aに向づて同一の肉厚を有して
いる。しかるにブレード2Aを横切る気流は、第3図に
示す如くブレード2の空気流入口61付近では軸方向の
成分が大きく3次元的に、ディスク3付近では半径方向
の成分が大きく2次元的になるため、翼弦方向(半径方
向)の流速が大きいブレード2のディスク3への付根付
近では第1図に示す如く翼腹面27に剥離域aが存在し
、この剥離域aが空気流の圧力変動を起こし騒音の主原
因になっている。このため第2図に示す如く特願昭33
−30700号にブレード2Bに肉盛りを行う遠心式送
風機用ファンが提案されている。しかるに空気流が3次
元的にブレード2Bを通過するため、空気流入「」61
では通路面積が減り、空気流の損失が大きく、遠心式送
風機としては送風効率が悪くなる欠点があった。
[Prior art] A centrifugal blower has an air inlet 6 at the top as shown in Fig. 3.
1, a cylindrical casing 6 having an air outlet 62 on its outer periphery, a centrifugal blower fan 1 disposed within the casing 6 in correspondence with the air inlet 61, and a centrifugal blower fan. The centrifugal blower fan 1 consists of a disk-shaped disk 3 whose central portion bulges to one side, and one end of which is fixed to the bulging side of the disk 3. It is composed of a large number of blades 2 which are arranged in a cylindrical shape at equal intervals from the outer circumference to form a row of blades, and from a manufacturing standpoint, the large size of each blade 2 is from the leading edge 24A to the trailing edge as shown in FIG. It has the same wall thickness towards 25A. However, as shown in FIG. 3, the airflow that crosses the blade 2A has a large axial component near the air inlet 61 of the blade 2 and becomes three-dimensional, and the airflow near the disk 3 has a large radial component and becomes two-dimensional. As shown in FIG. 1, a separation area a exists on the blade vent surface 27 near the root of the blade 2 to the disk 3 where the flow velocity in the chord direction (radial direction) is high, and this separation area a suppresses pressure fluctuations in the airflow. It is the main cause of noise. For this reason, as shown in Figure 2, the patent application
No. 30700 proposes a fan for a centrifugal blower in which blades 2B are built up. However, since the air flow passes through the blade 2B three-dimensionally, the air inflow "" 61
However, the passage area was reduced, the loss of air flow was large, and the blowing efficiency of the centrifugal blower was poor.

[発明の目的] 本発明の目的は、騒音を低減でき、且つ送風効果の良い
遠心式送風機用ファンの提供にある。
[Object of the Invention] An object of the present invention is to provide a fan for a centrifugal blower that can reduce noise and has a good air blowing effect.

[発明の構成] 本発明の遠心式送風機用ファンは、中心部が一方に膨出
した円盤状のディスクと、一端が前記ディスクの膨出が
わ面に固着されディスクの外周に等間隔で筒面状に列設
された多数のブレードとからなる遠心式送風機用ファン
において、前記各ブレードの大型は、揚力縁付近の肉厚
がディスクへの付根部で大きく、ディスクから離れるに
従って漸減することを構成とする。
[Structure of the Invention] The fan for a centrifugal blower of the present invention includes a disk-shaped disk whose center portion bulges out to one side, and one end of which is fixed to the bulging side surface of the disk, and cylinders arranged at equal intervals around the outer periphery of the disk. In a centrifugal blower fan consisting of a large number of blades arranged in a plane, each of the blades is large, and the wall thickness near the lifting edge is large at the root of the disk and gradually decreases as the distance from the disk increases. composition.

[発明の効果] 以上の構成により本発明の遠心式送風機用ファンは次の
効果を奏する。
[Effects of the Invention] With the above configuration, the centrifugal blower fan of the present invention has the following effects.

イ)ブレードからの空気流の剥離を防止できるため空気
流の圧力変動が生ぜず、騒音を低減できる。
b) Since separation of airflow from the blades can be prevented, pressure fluctuations in the airflow do not occur, and noise can be reduced.

口)ブレードの先端部を薄板形状としているため、空気
流の損失が少なく送風効果が非常に良い。
Mouth) Since the tip of the blade is shaped like a thin plate, there is little loss of air flow and the blowing effect is very good.

ハ)ブレードの先端部を薄板形状としているため、先端
部の質量が低減され、付根部の肉厚を大きくしであるた
めディスクとの結合面積が大きくとれるためブレードの
強度が増し、且つブレードの耐久性が向上する。
c) Since the tip of the blade is shaped like a thin plate, the mass of the tip is reduced, and the thickness of the root is increased, which increases the bonding area with the disk, increasing the strength of the blade. Improves durability.

[実施例] 本発明の遠心式送風機用ファンを第3図ないし第7図に
示す一実施例に基づき説明する。
[Example] The centrifugal blower fan of the present invention will be described based on an example shown in FIGS. 3 to 7.

本発明にかかる遠心式送風機用ファン1は、ブレード2
と、円盤状ディスク3と、前記ブレード2とディスク3
とを多数遠心方向に設けたシロッコファン4と、該シロ
ッコファン4を駆動軸51により駆動する駆動用モータ
5とからなり、これらは空気流入口61、空気吐出口6
2を形成したケーシング6に内嵌されている。
The centrifugal blower fan 1 according to the present invention has blades 2
, a circular disc 3, the blade 2 and the disc 3
It consists of a sirocco fan 4 in which a large number of scirocco fans are disposed in a centrifugal direction, and a drive motor 5 that drives the sirocco fan 4 by a drive shaft 51.
2 is fitted inside the casing 6.

ブレード2は、第4図に示す如く、一端2aが前記ディ
スク3の膨出がわ面31に固着され、ディスク3の外周
3aから筒面状に多数列設され、他端外周211にリン
グ212を嵌着し、先端部(図示左端部)21、中央部
22、付根部(図示右端部)23からなり、これらは一
体重に形成され、空気の流入側である前縁24、空気の
流出側である後縁25を形成している。
As shown in FIG. 4, the blades 2 have one end 2a fixed to the bulging side surface 31 of the disk 3, and are arranged in multiple rows in a cylindrical shape from the outer periphery 3a of the disk 3, and have a ring 212 on the outer periphery 211 of the other end. It is made up of a tip part (left end in the figure) 21, a center part 22, and a base part (right end in the figure) 23, which are formed into a single piece, with a front edge 24 that is the air inflow side, and an air outflow side. It forms a trailing edge 25 which is the side.

先端部21は、第5図に示す如く前縁24aに円弧状面
213を形成し、後縁25aに駆動軸51を軸心とする
円弧状面214を形成し、前縁24aと後縁25aとを
結び一定の半径を有した平均矢高曲線26a(半径r1
:約8.8cm)と、翼腹面(図示左面)27a(半径
r2 :約11.1cm)、および翼背面(図示右面)
28a(半径r3 :約8.1cm)とを同軸心とした
薄板形状(揚力線21A付近肉厚H:約1.0 cm)
を呈する。
As shown in FIG. 5, the tip portion 21 has a front edge 24a formed with an arcuate surface 213, a rear edge 25a with an arcuate surface 214 centered around the drive shaft 51, and a front edge 24a and a rear edge 25a. Average arrow height curve 26a (radius r1
: approx. 8.8 cm), wing ventral surface (left side in the figure) 27a (radius r2 : approx. 11.1 cm), and wing back surface (right side in the figure)
28a (radius r3: approx. 8.1 cm) is a thin plate shape (wall thickness near lift line 21A: approx. 1.0 cm)
exhibits.

中央部22は、第6図に示す如く前縁24bを先端部2
1の前縁24aより大きい半径を有する円弧状面223
を形成し、後縁25bは先端部21の後縁25aと同様
に駆動軸51を軸心とする円弧状面224を形成し、先
端部21の平均矢高曲線26aより揚力線22A付近に
おいて翼腹面27b方向に肉盛り(厚さh:約2cm)
を行い凸状面213bを形成してなる。
As shown in FIG.
An arcuate surface 223 having a radius larger than the leading edge 24a of
Similarly to the trailing edge 25a of the tip part 21, the trailing edge 25b forms an arcuate surface 224 with the drive shaft 51 as the axis, and from the average height curve 26a of the tip part 21, the wing ventral surface near the lift line 22A. Filling in direction 27b (thickness h: approx. 2cm)
The convex surface 213b is formed by performing this step.

付根部23は、第7図に示す如く前縁24cを中央部2
2の前縁24bより大きい半径を有する円弧状面233
を形成し、後縁25cは先端部21の後縁25aと同様
に駆動軸51を軸心とする円弧状面234を形成し、先
端部21の平均矢高曲線2[1aより揚力線23A付近
において翼腹面2?c方向に肉盛り(厚さh:約8cm
)を行い、凸状面29cを形成してなる。
As shown in FIG.
An arcuate surface 233 having a radius larger than the front edge 24b of No. 2
Similarly to the trailing edge 25a of the tip 21, the trailing edge 25c forms an arcuate surface 234 with the drive shaft 51 as the axis, and the average arrow height curve 2[1a of the tip 21 near the lift line 23A] Wing ventral surface 2? Filling in direction c (thickness h: approx. 8cm)
) to form the convex surface 29c.

このようにブレード2の大型は揚力線21A、22A、
23A伺近の肉厚がディスク3の膨出がわ面31で大き
く、ディスク3から離れるにしたがって漸減する。
In this way, the large blade 2 has lift lines 21A, 22A,
The wall thickness near 23A is large at the bulging side surface 31 of the disk 3, and gradually decreases as it moves away from the disk 3.

ディスク3は、第4図に示す如く円盤状を呈し、ブレー
ド2を固着する膨出がわ面31と、駆動輔51に固着さ
れる軸心部32と、前記膨出がわ面31と軸心部32と
を結ぶボス部33とからなり、軸心部32は、第3図に
示す如く駆動軸51の先端部51aに固着された円筒で
あり、中空部321で駆動軸51を挿通している。
The disk 3 has a disk shape as shown in FIG. 4, and has a protruding side surface 31 to which the blade 2 is fixed, an axial center portion 32 fixed to the driving member 51, and a bulging surface 31 and the shaft. The shaft center portion 32 is a cylinder fixed to the tip end 51a of the drive shaft 51 as shown in FIG. 3, and the drive shaft 51 is inserted through the hollow portion 321. ing.

空気は、ケーシング6の空気流入口61を通過してシロ
ッコファン4のブレード2の前縁24側より吸い込まれ
、各ブレード2の翼腹面27(27a、27b 、2?
c)、翼背面28(28a) (1)形状に沿った空気
流となって駆動軸51を中心とした遠心方向へ吹き出さ
れ、ケーシング6の空気吐出口62から吐出される。
Air passes through the air inlet 61 of the casing 6 and is sucked in from the leading edge 24 side of the blades 2 of the sirocco fan 4, and is sucked into the blade vent surface 27 (27a, 27b, 2?) of each blade 2.
c), the airflow following the shape of the blade back surface 28 (28a) (1) is blown out in a centrifugal direction around the drive shaft 51, and is discharged from the air outlet 62 of the casing 6.

A)本実施例ではプレート2の先端部21、中央部22
、イづ根部23の平均矢高曲線26aがらの肉盛の厚さ
hを各々約0.5cm 、約2cm 、約8cmとした
が、 翼弦長X:揚力線上の肉厚H の各部での比は、 表1 であれば1本実施例と同様な効果を有する。
A) In this embodiment, the tip portion 21 and center portion 22 of the plate 2
, the thickness h of the overlay on the average arrow height curve 26a of the root portion 23 was set to approximately 0.5 cm, approximately 2 cm, and approximately 8 cm, respectively, and the ratio of the chord length X to the wall thickness H on the lift line at each part If it is as shown in Table 1, it has the same effect as this embodiment.

B)本発明の遠心式送風機用ファンは、自動車または車
内の空気調和装置、工場の排風機などに使用される。
B) The centrifugal blower fan of the present invention is used in automobiles, air conditioners in cars, exhaust fans in factories, and the like.

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

第1.2図は従来の遠心式送風機用ファンのシュミレー
ション図、第3図は本発明の遠心式送風機用ファンの概
略図、第4図は本発明の遠心式送風機用ファンにかかる
ブレードの正面図、第5.6.7図は本発明の遠心式送
風機用ファンにかかるブレードの側面断面図である。 図中 1・・・・遠心式送風機用ファン 2・・・・ブ
レード 3・・・・ディスク 4・・・・シロッコファ
ン 5・・・・駆動用モータ 6・・・・ケーシン代 
理 人 石 黒 軒 二
Figures 1 and 2 are simulation diagrams of a conventional centrifugal blower fan, Figure 3 is a schematic diagram of the centrifugal blower fan of the present invention, and Figure 4 is a front view of the blades of the centrifugal blower fan of the present invention. Figures 5.6.7 are side sectional views of the blades of the centrifugal blower fan of the present invention. In the diagram: 1...Centrifugal blower fan 2...Blade 3...Disc 4...Sirocco fan 5...Drive motor 6...Casing allowance
Rito Ishiguro Ken 2

Claims (1)

【特許請求の範囲】 中心部が一方に1膨出した円盤状のディスクと。 一端が前記ディスクの膨出がわ而に固着されディスクの
外周に等間隔で筒面状に列設された多数のブレードとか
らなる遠心式送風機用ファンにおいて、 前記各ブレードの大型は、揚力線伺近の肉厚がディスク
への4=J根部で大きく、ディスクから離れるに従って
漸減することを特徴とする遠心式送風機用ファン・
[Claims] A disc-shaped disk with a central portion bulging out on one side. In a centrifugal blower fan comprising a number of blades having one end fixed to the bulge of the disk and arranged in a cylindrical shape at equal intervals around the outer periphery of the disk, the large size of each blade has a lift line. A fan for a centrifugal blower characterized in that the wall thickness near the disk is large at the root of 4=J and gradually decreases as it moves away from the disk.
JP1288484A 1984-01-26 1984-01-26 Centrifugal type blower fan Pending JPS60156997A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1288484A JPS60156997A (en) 1984-01-26 1984-01-26 Centrifugal type blower fan

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1288484A JPS60156997A (en) 1984-01-26 1984-01-26 Centrifugal type blower fan

Publications (1)

Publication Number Publication Date
JPS60156997A true JPS60156997A (en) 1985-08-17

Family

ID=11817825

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1288484A Pending JPS60156997A (en) 1984-01-26 1984-01-26 Centrifugal type blower fan

Country Status (1)

Country Link
JP (1) JPS60156997A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH04262093A (en) * 1990-09-28 1992-09-17 Lamson Corp Regenerative centrifugal compressor
JP2002168194A (en) * 2000-12-04 2002-06-14 Mitsubishi Heavy Ind Ltd Multiblade blower
JP2005320881A (en) * 2004-05-07 2005-11-17 Matsushita Electric Ind Co Ltd Turbofan and air conditioner using the same
US6984111B2 (en) 2002-07-24 2006-01-10 Sanden Corporation Multiblade blower
WO2007138673A1 (en) * 2006-05-30 2007-12-06 Mitsubishi Electric Corporation Centrifugal multi-blade fan
JP2008545086A (en) * 2005-07-04 2008-12-11 ベール ゲーエムベーハー ウント コー カーゲー Impeller
WO2009139422A1 (en) * 2008-05-14 2009-11-19 ダイキン工業株式会社 Centrifugal fan
US7744350B2 (en) * 2004-09-13 2010-06-29 Panasonic Corporation Multiblade fan

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5462504A (en) * 1977-10-28 1979-05-19 Hitachi Ltd Runner
JPS5654991A (en) * 1979-10-11 1981-05-15 Kubota Ltd Open-type impeller of mixed flow pump

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5462504A (en) * 1977-10-28 1979-05-19 Hitachi Ltd Runner
JPS5654991A (en) * 1979-10-11 1981-05-15 Kubota Ltd Open-type impeller of mixed flow pump

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH04262093A (en) * 1990-09-28 1992-09-17 Lamson Corp Regenerative centrifugal compressor
JP2002168194A (en) * 2000-12-04 2002-06-14 Mitsubishi Heavy Ind Ltd Multiblade blower
US6984111B2 (en) 2002-07-24 2006-01-10 Sanden Corporation Multiblade blower
JP2005320881A (en) * 2004-05-07 2005-11-17 Matsushita Electric Ind Co Ltd Turbofan and air conditioner using the same
US7744350B2 (en) * 2004-09-13 2010-06-29 Panasonic Corporation Multiblade fan
JP2008545086A (en) * 2005-07-04 2008-12-11 ベール ゲーエムベーハー ウント コー カーゲー Impeller
EP1902220B1 (en) * 2005-07-04 2012-09-12 Behr GmbH & Co. KG Blower wheel
US8337157B2 (en) 2005-07-04 2012-12-25 Behr Gmbh & Co. Kg Blower wheel
WO2007138673A1 (en) * 2006-05-30 2007-12-06 Mitsubishi Electric Corporation Centrifugal multi-blade fan
US7771169B2 (en) 2006-05-30 2010-08-10 Mitsubishi Electric Corporation Centrifugal multiblade fan
WO2009139422A1 (en) * 2008-05-14 2009-11-19 ダイキン工業株式会社 Centrifugal fan

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