JPS648199B2 - - Google Patents

Info

Publication number
JPS648199B2
JPS648199B2 JP58251252A JP25125283A JPS648199B2 JP S648199 B2 JPS648199 B2 JP S648199B2 JP 58251252 A JP58251252 A JP 58251252A JP 25125283 A JP25125283 A JP 25125283A JP S648199 B2 JPS648199 B2 JP S648199B2
Authority
JP
Japan
Prior art keywords
section
centrifugal blower
axial distance
impeller
proportion
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.)
Expired
Application number
JP58251252A
Other languages
Japanese (ja)
Other versions
JPS60145497A (en
Inventor
Makoto Kaihara
Kunitake Sakai
Masaaki Okabe
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.)
Panasonic Holdings Corp
Original Assignee
Matsushita Electric Industrial 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 Matsushita Electric Industrial Co Ltd filed Critical Matsushita Electric Industrial Co Ltd
Priority to JP58251252A priority Critical patent/JPS60145497A/en
Publication of JPS60145497A publication Critical patent/JPS60145497A/en
Publication of JPS648199B2 publication Critical patent/JPS648199B2/ja
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/40Casings; Connections of working fluid
    • F04D29/42Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/44Fluid-guiding means, e.g. diffusers
    • F04D29/441Fluid-guiding means, e.g. diffusers especially adapted for elastic fluid pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/50Inlet or outlet
    • F05D2250/52Outlet

Landscapes

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

Description

【発明の詳細な説明】 産業上の利用分野 本発明は、空気調和機等に利用されている遠心
送風機の送風性能の向上と運転騒音の低下に関す
るものである。
DETAILED DESCRIPTION OF THE INVENTION Field of Industrial Application The present invention relates to improving the blowing performance and reducing operating noise of centrifugal blowers used in air conditioners and the like.

従来例の構成とその問題点 従来、遠心送風機の送風性能の向上については
渦巻ケーシングの形状を、多翼羽根車の回転方向
に回転角度に比例して半径方向距離を大きくする
と共に、一定角度の傾斜部を設け軸方向距離も回
転角度に比例して大きくすることが有効であるこ
とが知られていた。すなわち、第1図に示すごと
く、羽根車(図示せず)に半径方向で最も近い舌
部aより羽根車の回転方向xに沿つて、回転角度
に比例してケーシング半径bを大きくすると共
に、空気吸込面c上に一定角度の傾斜部dを設
け、軸方向距離uを回転角度に比例して大きくす
る形状となる。
Conventional structure and its problems Conventionally, in order to improve the air blowing performance of a centrifugal blower, the shape of the spiral casing was changed by increasing the radial distance in proportion to the rotation angle in the rotation direction of the multi-blade impeller, and It has been known that it is effective to provide an inclined portion and increase the axial distance in proportion to the rotation angle. That is, as shown in FIG. 1, the casing radius b is increased in proportion to the rotation angle along the rotational direction x of the impeller from the tongue a closest to the impeller (not shown) in the radial direction, An inclined portion d having a constant angle is provided on the air suction surface c, and the shape is such that the axial distance u increases in proportion to the rotation angle.

しかしこの形状では、渦巻終了部eの軸方向距
離vが大きなものとなり、この遠心送風機が組込
まれる空気調和機等の機器が大きなものとなると
いう問題があつた。さらに空気調和機等の構造の
容易さ、美観上の目的より空気吹出部fの形状は
矩形断面であることが要求されるが、渦巻部終了
部eの流路断面は隅切四角形状となつており、こ
れを空気の乱れをおさえつつゆるやかに矩形断面
に変形するために吹出流路の長さwが大きくな
る。この点も遠心送風機が組込まれる機器の大き
さを大きくしてしまうという問題点となつてい
た。
However, this shape has a problem in that the axial distance v of the spiral ending portion e becomes large, and the equipment such as an air conditioner in which this centrifugal blower is incorporated becomes large. Furthermore, for ease of construction of an air conditioner, etc., and for aesthetic purposes, the shape of the air blowing part f is required to have a rectangular cross section, but the flow path cross section of the spiral part end part e is a square corner shape. In order to gently transform this into a rectangular cross section while suppressing air turbulence, the length w of the blowout passage becomes large. This also poses a problem in that it increases the size of the equipment in which the centrifugal blower is incorporated.

発明の目的 本発明は、このような問題点を解決するもの
で、遠心送風機の送風性能を向上し、騒音を低下
することを実現し、これを小さな機器に組み込み
可能とすることを目的とするものである。
Purpose of the Invention The present invention solves these problems, and aims to improve the blowing performance of a centrifugal blower, reduce noise, and enable it to be incorporated into small equipment. It is something.

発明の構成 この目的を達成するため、本発明は遠心送風機
のケーシングの形状を渦巻途中まで従来例と同様
に一定角度の傾斜部を設け、軸方向距離が大きく
なる形状とし、渦巻途中より軸方向距離を一定に
し、断面積を回転角度に比例して大きくするべく
傾斜面の傾斜角を大きくする形状としたものであ
る。
Structure of the Invention In order to achieve this object, the present invention provides a casing of a centrifugal blower with an inclined part at a constant angle up to the middle of the spiral, similar to the conventional example, and a shape in which the distance in the axial direction increases. The distance is constant, and the slope angle of the slope is increased in order to increase the cross-sectional area in proportion to the rotation angle.

この構成による遠心送風機を運転した場合、多
翼羽根車より流出した空気は、渦巻の始点から終
点に至るまで十分確保された流路内に流れ、送風
性能が向上されると共に、軸方向距離の小さく、
また渦巻終了部の断面形状は矩形に近い形となる
ので吹出部の通風方向長さも小さくすることがで
きる。
When a centrifugal blower with this configuration is operated, the air flowing out from the multi-blade impeller flows into a sufficiently secured flow path from the start point to the end point of the vortex, improving the blowing performance and reducing the axial distance. small,
Furthermore, since the cross-sectional shape of the spiral end portion is nearly rectangular, the length of the blowout portion in the ventilation direction can also be reduced.

実施例の説明 以下、本発明をその一実施例を示す第2図〜第
4図を参考に説明する。
DESCRIPTION OF EMBODIMENTS The present invention will be described below with reference to FIGS. 2 to 4 showing one embodiment thereof.

第2図〜第4図において、1は羽根車、2は駆
動軸で前記羽根車1に固定されている。3はケー
シング渦巻面、4はケーシング側面でノズル5が
配設されている。6は吹出口で矩形断面形状をし
ている。第3図は第4図をX−X′線で切つた断
面図を示す。第3図中羽根車1に半径方向で最も
近い渦巻始点7より羽根車1の回転方向Mに沿つ
て回転角度に比例して半径方向長さ(半径R)が
大となるよう渦巻面3が配されている。渦巻始点
7より中間点8までの区間Bは軸方向長さFが一
定で羽根車1との適切なクリアランスを保持して
いる。第1中間点8より第2中間点9までの区間
Cでは、ケーシング側面4に対し一定角度を持つ
第1傾斜面10が形成され、回転角度に比例して
軸方向長さFが増加する。中間点9より渦巻終点
11までの区間Dでは、軸方向長さFは一定で、
第2傾斜面12の傾斜角度は軸方向長さが回転角
度に比例して増加するに等しい断面積を確保する
ように大きくなる。渦巻終点11より吹出中間点
13までの区間Eでは第3傾斜面14の傾斜角度
が大きくなるように変化し、吹出中間点13での
断面形状は矩形となる。さらに吹出口6までの区
間Gは適当な拡大角で矩形形状のまま流路が拡大
している。
In FIGS. 2 to 4, 1 is an impeller, and 2 is a drive shaft fixed to the impeller 1. 3 is a spiral surface of the casing, and 4 is a side surface of the casing, on which a nozzle 5 is disposed. Reference numeral 6 denotes an air outlet, which has a rectangular cross-sectional shape. FIG. 3 shows a sectional view of FIG. 4 taken along line X-X'. In Fig. 3, the spiral surface 3 is arranged so that the radial length (radius R) increases in proportion to the rotation angle along the rotation direction M of the impeller 1 from the spiral starting point 7 that is radially closest to the impeller 1. It is arranged. The section B from the spiral start point 7 to the intermediate point 8 has a constant axial length F and maintains an appropriate clearance with the impeller 1. In the section C from the first intermediate point 8 to the second intermediate point 9, a first inclined surface 10 having a constant angle with respect to the casing side surface 4 is formed, and the axial length F increases in proportion to the rotation angle. In the section D from the intermediate point 9 to the spiral end point 11, the axial length F is constant,
The angle of inclination of the second inclined surface 12 increases so as to ensure a cross-sectional area equal to the axial length increasing in proportion to the angle of rotation. In the section E from the spiral end point 11 to the blowout intermediate point 13, the inclination angle of the third inclined surface 14 changes to become larger, and the cross-sectional shape at the blowout intermediate point 13 becomes rectangular. Further, in the section G up to the air outlet 6, the flow path is expanded at an appropriate enlargement angle while keeping the rectangular shape.

上記構成において駆動軸2にて羽根車1が回転
すると、空気はケーシング側面4に設けられたノ
ズル5を通つて羽根車1に吸込まれケーシング内
でエネルギを与えられて吹出口6に送り出され
る。この際ノズル5の周囲は第1傾斜面10、第
2傾斜面12となつており空気がなめらかに流入
できる。また羽根車1を出た空気は、区間Cおよ
び区間Dにおいて確保された十分な流路面積によ
り大量に送り込まれ、送風性能が向上する。また
渦巻終点11での断面形状は矩形に近いものとな
るため、矩形断面に推移する区間Eの距離lは短
いものとなる。
In the above configuration, when the impeller 1 rotates on the drive shaft 2, air is sucked into the impeller 1 through the nozzle 5 provided on the side surface 4 of the casing, is given energy within the casing, and is sent out to the outlet 6. At this time, the nozzle 5 is surrounded by a first inclined surface 10 and a second inclined surface 12, allowing air to flow in smoothly. Moreover, the air that has exited the impeller 1 is sent in a large amount due to the sufficient flow path area secured in the section C and the section D, and the air blowing performance is improved. Further, since the cross-sectional shape at the spiral end point 11 is close to a rectangle, the distance l of the section E that changes to a rectangular cross-section is short.

発明の効果 上記実施例より明らかなように、本発明におけ
る遠心送風機は、ケーシングの断面形状が傾斜部
のない軸方向距離が一定の区間、一定の傾斜角度
をもつ傾斜部を有し回転角度に比例して軸方向距
離が増大する区間、および傾斜部を有するが、軸
方向距離が一定で、傾斜部の傾斜角度が流路面積
を増大するように増大する区間よりなるもので、
従来例に比して小さな軸方向距離と、小さな吹出
部長さで、大きな流路面積を確保し、送風性能の
向上と騒音の低下を計りつつ小形化を実現するも
のである。
Effects of the Invention As is clear from the above embodiments, the centrifugal blower according to the present invention has a cross-sectional shape of the casing that has a section with a constant axial distance without an inclined part and an inclined part with a fixed inclination angle, and has a rotation angle. It has a section in which the axial distance increases proportionally, and a section having an inclined part, but the axial distance is constant and the inclination angle of the inclined part increases so as to increase the flow path area,
Compared to the conventional example, the axial distance and the length of the blowing part are small, ensuring a large flow path area, improving air blowing performance and reducing noise while reducing the size.

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

第1図は従来の遠心送風機の一例を示す斜視
図、第2図は本発明の遠心送風機の一例を示す斜
視図、第3図は第4図のX−X′線での平面断面
図、第4図は本発明の一例を示す遠心送風機の正
面図である。 1……羽根車、3……ケーシング渦巻面、4…
…ケーシング側面、5……ノズル、6……吹出
口、7……渦巻始点、10……第1傾斜面、11
……渦巻終点、12……第2傾斜面、14……第
3傾斜面。
FIG. 1 is a perspective view showing an example of a conventional centrifugal blower, FIG. 2 is a perspective view showing an example of the centrifugal blower of the present invention, and FIG. 3 is a plan sectional view taken along line X-X' in FIG. FIG. 4 is a front view of a centrifugal blower showing an example of the present invention. 1... Impeller, 3... Casing spiral surface, 4...
...Casing side surface, 5... Nozzle, 6... Air outlet, 7... Swirl starting point, 10... First inclined surface, 11
...Spiral end point, 12...Second slope, 14...Third slope.

Claims (1)

【特許請求の範囲】[Claims] 1 多翼羽根車を有する遠心送風機において、渦
巻形ケーシグの形状が、半径方向距離が前記多翼
羽根車に最も近い舌部より前記多翼羽根車の回転
方向に沿つて軸方向距離が一定の区間、傾斜部を
有し軸方向距離が回転角度に比例して大きくなる
区間および隅切四角形状断面を有し軸方向距離が
一定で傾斜部の角度が変化し、隅切四角形状断面
部の面積が回転角度に比例して大きくなる区間の
3区間より構成される遠心送風機。
1 In a centrifugal blower having a multi-blade impeller, the shape of the spiral casing is such that the axial distance is constant along the rotational direction of the multi-blade impeller from the tongue portion whose radial distance is closest to the multi-blade impeller. A section, a section that has an inclined part and whose axial distance increases in proportion to the rotation angle, and a section that has a truncated rectangular cross section and whose axial distance is constant but the angle of the slanted part changes; A centrifugal blower consisting of three sections whose area increases in proportion to the rotation angle.
JP58251252A 1983-12-29 1983-12-29 Centrifugal blower Granted JPS60145497A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP58251252A JPS60145497A (en) 1983-12-29 1983-12-29 Centrifugal blower

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP58251252A JPS60145497A (en) 1983-12-29 1983-12-29 Centrifugal blower

Publications (2)

Publication Number Publication Date
JPS60145497A JPS60145497A (en) 1985-07-31
JPS648199B2 true JPS648199B2 (en) 1989-02-13

Family

ID=17219997

Family Applications (1)

Application Number Title Priority Date Filing Date
JP58251252A Granted JPS60145497A (en) 1983-12-29 1983-12-29 Centrifugal blower

Country Status (1)

Country Link
JP (1) JPS60145497A (en)

Cited By (3)

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Publication number Priority date Publication date Assignee Title
WO2012056990A1 (en) * 2010-10-25 2012-05-03 三菱重工業株式会社 Multi-blade centrifugal fan and air conditioner using same
WO2016147437A1 (en) * 2015-03-19 2016-09-22 サンデンホールディングス株式会社 Blower
CN109931294A (en) * 2017-12-18 2019-06-25 现代自动车株式会社 Binary vortices formula bidirectional blower

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JPS6477800A (en) * 1987-09-18 1989-03-23 Hitachi Ltd Air conditioner
US4919592A (en) * 1989-01-18 1990-04-24 Superstill Technology, Inc. Radially compact fluid compressor
US5156524A (en) * 1990-10-26 1992-10-20 Airflow Research And Manufacturing Corporation Centrifugal fan with accumulating volute
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US6499954B1 (en) 2000-08-21 2002-12-31 Textron Automotive Company Inc. Centrifugal impeller and housing
US6742989B2 (en) * 2001-10-19 2004-06-01 Mitsubishi Heavy Industries, Ltd. Structures of turbine scroll and blades
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Cited By (4)

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WO2012056990A1 (en) * 2010-10-25 2012-05-03 三菱重工業株式会社 Multi-blade centrifugal fan and air conditioner using same
US9334875B2 (en) 2010-10-25 2016-05-10 Mitsubishi Heavy Industries, Ltd. Multiblade centrifugal fan and air conditioner equipped with the same
WO2016147437A1 (en) * 2015-03-19 2016-09-22 サンデンホールディングス株式会社 Blower
CN109931294A (en) * 2017-12-18 2019-06-25 现代自动车株式会社 Binary vortices formula bidirectional blower

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Publication number Publication date
JPS60145497A (en) 1985-07-31

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