JPS6365840B2 - - Google Patents

Info

Publication number
JPS6365840B2
JPS6365840B2 JP21305281A JP21305281A JPS6365840B2 JP S6365840 B2 JPS6365840 B2 JP S6365840B2 JP 21305281 A JP21305281 A JP 21305281A JP 21305281 A JP21305281 A JP 21305281A JP S6365840 B2 JPS6365840 B2 JP S6365840B2
Authority
JP
Japan
Prior art keywords
passage
impeller
return passage
plate
outlet
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
JP21305281A
Other languages
Japanese (ja)
Other versions
JPS58117395A (en
Inventor
Tadami Tanaka
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 JP21305281A priority Critical patent/JPS58117395A/en
Publication of JPS58117395A publication Critical patent/JPS58117395A/en
Publication of JPS6365840B2 publication Critical patent/JPS6365840B2/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

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】 本発明は燃焼機器や家庭用機器などに使用され
る円筒形送風機に関するものである。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a cylindrical blower used in combustion equipment, household equipment, and the like.

従来のこの種の送風機は第1,2図に示すよう
に、円筒形ケーシングa内に回転自在に配設した
羽根車bを、円板形状の上面板b1と下面板b2間に
複数枚の羽根cを放射状に固定して形成し、これ
らの上下面板b1,b2と羽根cの外端径とを同一寸
法に形成すると共に羽根車bの下面板b2に近接し
て配設した戻り通路dの上面板d1を羽根車bの外
径と等しくして羽根車b及び戻り通路dの外周開
口端とケーシングaの内周面間に環状にデイヒユ
ーザー空間部eを設けてなる構造を有している。
As shown in Figures 1 and 2, a conventional blower of this type has a plurality of impellers b rotatably disposed within a cylindrical casing a between a disc-shaped upper plate b 1 and a lower plate b 2 . A number of blades c are fixed in a radial manner, and the upper and lower surface plates b 1 and b 2 and the outer end diameter of the blade c are formed to have the same size, and the blades are arranged close to the lower surface plate b 2 of the impeller b. The upper surface plate d1 of the return passage d provided is made equal to the outer diameter of the impeller b, and an annular day user space e is formed between the outer peripheral opening end of the impeller b and the return passage d and the inner peripheral surface of the casing a. It has a structure.

しかしながらこのような構造によれば、羽根車
bの出口から流出する空気流はケーシングaの内
周面に衝突したのちデイヒユーザー空間部eで大
部分が周方向の速度成分の流れとなつて環状のデ
イヒユーザー空間部内を回流することになるの
で、ケーシングaの内周面に衝突した際に大きな
圧力損失が生じると共に回流する空気流にケーシ
ングaの内周面によつて壁面摩擦損失が発生し、
又、戻り通路d側に空気流が流通する際に径方向
の速度成分を軸方向に指向させなければならない
ために曲がり損失が生じることになる。
However, according to such a structure, the airflow flowing out from the outlet of the impeller b collides with the inner circumferential surface of the casing a and then becomes a flow with a velocity component mostly in the circumferential direction in the day user space e. Since the air circulates within the annular day user space, a large pressure loss occurs when it collides with the inner peripheral surface of casing a, and wall friction loss is caused by the inner peripheral surface of casing a in the circulating air flow. occurs,
Furthermore, when the air flow flows to the return passage d side, the velocity component in the radial direction must be directed in the axial direction, resulting in bending loss.

さらに、戻り通路dに流入する際においても、
戻り通路の入口に対する流れの方向が不一致によ
る損失が生じ、羽根車aの有する送風全圧力が戻
り通路dと連通するフアン出口fに達するまでに
大巾に低下して送風性能が悪くなり、このため、
燃焼機器の特性等を良くするに必要なフアン圧力
を得るにはフアンを大型化しなければならない等
の欠点があつた。
Furthermore, even when flowing into the return passage d,
A loss occurs due to the mismatch in the direction of the flow with respect to the inlet of the return passage, and the total air blowing pressure of the impeller a decreases significantly by the time it reaches the fan outlet f communicating with the return passage d, resulting in poor air blowing performance. For,
There were drawbacks such as the need to increase the size of the fan in order to obtain the fan pressure necessary to improve the characteristics of the combustion equipment.

このような欠点を解消するために、第3図に示
すように、ケーシングaの内周面と羽根車bの外
周開口端間で形成した環状空間部に、渦巻状通路
gを複数個、周方向に所定間隔毎に設け、これら
の通路gの上方開口端を羽根車bの外周方に連通
させると共に下方開口端を戻り通路側に連通させ
た構造の送風機が提案されている。
In order to eliminate such drawbacks, as shown in FIG. A blower has been proposed in which the upper opening ends of these passages g are provided at predetermined intervals in the direction of the impeller b, and the lower opening ends thereof are connected to the return passage side.

しかしながら、このような構造によれば、渦巻
状通路gを形成する通路壁g1の始端部g2は高速回
転する羽根車bの外周に接線方向に近接している
ため、羽根車bからの空気の流れが前記始端部g2
で瞬間的にカツトされる状態となつて羽根車bの
羽根枚数と回転数との積で決定される周波数のサ
イレン音が発生し、このサイレン音の発生を抑制
するには、消音装置が必要となる。又、渦巻状通
路gを前記環状空間部に各々独立して構成するに
は構造が複雑になり、ケーシングaを大きくする
必要が生じるばかりでなく、形成し得る通路面積
が制約されて通路内での流速が早くなり、一定風
量以上では渦巻状通路g内で圧力損失が増大して
フアン圧力を低下させる等の欠点がある。
However, according to such a structure, the starting end g2 of the passage wall g1 forming the spiral passage g is tangentially close to the outer periphery of the impeller b which rotates at high speed. The air flow starts at the starting end g 2
When the impeller B is cut off momentarily, a siren sound with a frequency determined by the product of the number of blades and the rotation speed of impeller B is generated, and a silencer is required to suppress the generation of this siren sound. becomes. In addition, if the spiral passages g are formed independently in each of the annular spaces, the structure becomes complicated and the casing a needs to be enlarged, and the area of the passages that can be formed is restricted. The flow velocity increases, and when the air volume exceeds a certain level, the pressure loss increases in the spiral passage g, resulting in a decrease in fan pressure.

又、羽根車の構造を改良することによつて前記
欠点を解消しようとする送風機も案出されている
が、単に羽根車の形状を変えただけでは羽根車の
もつている圧力を損失なく流通させる通風路が構
成されていないために大巾な改善は得られないも
のである。
In addition, blowers have been devised to solve the above drawbacks by improving the structure of the impeller, but simply changing the shape of the impeller does not allow the pressure of the impeller to flow through without loss. However, since there is no ventilation path in place for this purpose, it is not possible to make any significant improvements.

本発明はこのような従来の送風機の欠点をなく
するために、羽根車出口での流れによる動圧をそ
の出口からフアン出口までの通路内で圧力に変換
し、流れの運動エネルギーを殆んど損失させるこ
となく圧力回収するように構成してフアン性能を
従来の150%という大巾な改善を可能にしたこと
を特長とする送風機を提供するものである。
In order to eliminate these drawbacks of conventional blowers, the present invention converts the dynamic pressure caused by the flow at the impeller outlet into pressure within the passage from the impeller outlet to the fan outlet, thereby reducing most of the kinetic energy of the flow. The present invention provides an air blower characterized by being configured to recover pressure without loss, making it possible to significantly improve fan performance by 150% compared to conventional fans.

その技術的手段は軸方向に環状出口を開口する
羽根車と、この羽根車の下流側に配設される戻り
通路の戻り通路入口を、内端が羽根車の下面板の
外径と等しく、一方の側端面が戻り通路の案内羽
根の凸側曲面と等しく他方の側端面が次の案内羽
根の外端から径方向に直線的に延びる形状とし、
かつ戻り通路を戻り通路入口の内端で分割するご
とき昇圧羽根片を、戻り通路入口の内端で案内羽
根の背面となる凸側曲面に密接させて配設した簡
単な構成で従来の欠点であつた羽根車外周上のデ
イヒユーザ空間での流れの回流ロスを軸方向に環
状出口を有する羽根車で改善し、この羽根車の環
状出口と戻り通路入口とを対向させて、戻り通路
入口での流入損失を改善し、戻り通路内に昇圧羽
根片を配設し、戻り通路内での流れの圧力回収を
図らんとするものである。
The technical means consists of an impeller with an annular outlet opening in the axial direction and a return passage inlet of a return passage arranged downstream of the impeller, the inner end of which is equal to the outer diameter of the lower plate of the impeller; One side end surface is equal to the convex curved surface of the guide vane of the return passage, and the other side end surface is shaped to extend linearly in the radial direction from the outer end of the next guide vane,
Moreover, it has a simple structure in which the booster blade pieces that divide the return passage at the inner end of the return passage inlet are arranged in close contact with the convex curved surface that forms the back surface of the guide vane at the inner end of the return passage inlet. The recirculation loss of the flow in the day user space on the outer periphery of the impeller is improved by using an impeller having an annular outlet in the axial direction, and the annular outlet of this impeller and the return passage inlet are made to face each other, so that the flow loss at the return passage inlet is improved. The purpose is to improve the inflow loss, provide pressure boosting vanes in the return passage, and recover the pressure of the flow in the return passage.

本発明の実施例を図面について説明すると、1
は円筒形ケーシングで、その上端に天面板2を一
体に設けてあり、この天面板2の中央に吸入口3
を穿設してある。4は吸入口3の上方に配設した
電動機で、天面板2に固着した支持金具5に取付
けられてあり、その回転軸6の下端部にケーシン
グ1内に配設した羽根車7を固定具8により固着
してある。
Embodiments of the present invention will be explained with reference to the drawings: 1
is a cylindrical casing, with a top plate 2 integrally provided at its upper end, and an inlet 3 in the center of the top plate 2.
has been drilled. Reference numeral 4 denotes an electric motor disposed above the suction port 3, which is attached to a support fitting 5 fixed to the top plate 2. An impeller 7 disposed inside the casing 1 is attached to the lower end of the rotating shaft 6 by a fixing device. It is fixed by 8.

この羽根車7は、中央部に前記吸入口3と連通
する入口9を設けた上面板10と、この上面板1
0に対して下方一定間隔を存し且つその中心部に
前記回転軸6を固着させた円形の下面板11との
間の羽根出口角が50〜110゜である複数枚の羽根1
2を放射状に取付けてなるものである。
This impeller 7 includes a top plate 10 provided with an inlet 9 communicating with the suction port 3 in the center thereof;
a plurality of blades 1 which are spaced apart from each other at a constant distance downward from zero and have a blade exit angle of 50 to 110 degrees with a circular lower plate 11 to which the rotating shaft 6 is fixed at the center thereof;
2 are attached radially.

羽根車7の上面板10は下面板11よりも大径
に形成され、且つその入口9から外周部に向つて
下方に緩傾斜していると共に外周部を下方に彎曲
させた椀形状に形成されてあり、その彎曲下端を
下面板11の外周延長上に位置させるかやや下方
に位置させて彎曲下端と下面板11の外周端面間
に下向きに開口した環状出口13を形成してあ
る。又、この上面板10の彎曲下端をケーシング
1の内周面間に小隙間を存してある。
The upper surface plate 10 of the impeller 7 is formed to have a larger diameter than the lower surface plate 11, and is formed in a bowl shape with a gentle slope downward from the inlet 9 toward the outer periphery, and the outer periphery is curved downward. The lower end of the curve is located on the extension of the outer periphery of the lower plate 11 or slightly below, and an annular outlet 13 opening downward is formed between the lower end of the curve and the outer peripheral end surface of the lower plate 11. Further, a small gap is provided between the curved lower end of the upper surface plate 10 and the inner peripheral surface of the casing 1.

羽根12は平面円弧状ないしはS字状或いは平
板状に形成され、その上下端を羽根車7の上下面
板10,11に沿つた形状に形成して上下面板1
0,11に一体に固着してあり、さらにその外端
部を下面板11から外周方に延出させて環状出口
13に位置させてある。
The blades 12 are formed in a planar arc shape, an S-shape, or a flat plate shape, and the upper and lower ends thereof are formed in a shape that follows the upper and lower surface plates 10 and 11 of the impeller 7.
0 and 11, and its outer end extends outward from the bottom plate 11 and is located at the annular outlet 13.

14は戻り通路で、前述した羽根車7の下面板
11の下方に小隙間を介して水平に並設した円形
の通路上板15と、この通路上板15の下方に一
定間隔を存して配設した通路底板16と、これら
の通路上板15及び底板16間に放射状に配設し
た複数枚の案内羽根17と、昇圧羽根片とより構
成されている。
Reference numeral 14 denotes a return passage, which includes a circular upper passage plate 15 horizontally arranged below the lower plate 11 of the impeller 7 with a small gap therebetween, and a constant interval below the upper passage plate 15. It is composed of a passage bottom plate 16, a plurality of guide blades 17 radially arranged between the passage top plate 15 and the bottom plate 16, and a booster blade piece.

戻り通路上板15は、その外周部複数個所に前
記羽根車7の環状出口13と間隙を存して対向さ
せてその環状出口13と同一軸方向に開口してい
る戻り通路入口18を設け、この通路入口18の
内端円弧面18aを羽根車7の下面板11の外
径、即ち環状出口13の内端面に等しい垂直面上
に設けると共に外端開口部を羽根車7の上面板1
0の外径、即ち環状出口13の外端面に等しい垂
直面上に設けてあり、さらに一方の側端面18b
は案内羽根17の背面側の曲線と同一彎曲端面に
形成すると共に他方の側端面18cは前記案内羽
根17に隣接する次の案内羽根17の外端位置か
ら径方向と同一方向かやゝ傾斜した方向に直線状
の端面に形成されてある。従つて、この戻り通路
入口18と案内羽根17とは同数であり、戻り通
路入口18を外周端部の周方向の開口巾は隣接す
る案内羽根17,17の外端間の寸法に等しくな
つているものである。又、この通路入口18の両
側端面18b,18cは羽根車7の出口における
羽根12の外端部と垂直面上で一致することがな
いように形成して羽根車7の羽根12の数と回転
数との積で決定される周波数のサイレン音の発生
の時間的ずれを生じさせてその発生を抑制してい
るものである。
The return passage upper plate 15 is provided with return passage inlets 18 at a plurality of locations on its outer periphery, facing the annular outlet 13 of the impeller 7 with a gap therebetween and opening in the same axial direction as the annular outlet 13, The inner end circular arc surface 18a of the passage inlet 18 is provided on the outer diameter of the lower surface plate 11 of the impeller 7, that is, on a vertical plane equal to the inner end surface of the annular outlet 13, and the outer end opening is arranged on the upper surface plate 11 of the impeller 7.
0, that is, on a vertical plane equal to the outer end surface of the annular outlet 13, and one side end surface 18b.
is formed on the same curved end surface as the curve on the back side of the guide vane 17, and the other side end surface 18c is slightly inclined in the same direction as the radial direction from the outer end position of the next guide vane 17 adjacent to the guide vane 17. It is formed with a straight end face in the direction. Therefore, the number of the return passage inlets 18 and the guide vanes 17 are the same, and the opening width in the circumferential direction at the outer peripheral end of the return passage inlet 18 is equal to the dimension between the outer ends of the adjacent guide vanes 17, 17. It is something that exists. Further, both side end surfaces 18b and 18c of this passage entrance 18 are formed so as not to coincide with the outer ends of the blades 12 at the outlet of the impeller 7 on a vertical plane, so that the number and rotation of the blades 12 of the impeller 7 can be adjusted. The generation of siren sounds is suppressed by creating a time lag in the generation of siren sounds whose frequency is determined by multiplying the frequency by the number of siren sounds.

案内羽根17は第6図に示すように、羽根車7
の回転方向に略円弧状に彎曲形成され、その内端
を通路底板16の中央に設けた戻り通路出口19
の上端開口縁上に位置させると共に外端を通路上
板15及び底板16の外周端面と一体にケーシン
グ1の内周面に密接、固定させてあり、隣接する
案内羽根17,17間に独立した戻り通路14a
を形成して気体の流れの回流及び漏れをなくして
ある。
The guide vane 17 is connected to the impeller 7 as shown in FIG.
A return passage outlet 19 is curved in a substantially arc shape in the direction of rotation of the return passage outlet 19 and has an inner end located at the center of the passage bottom plate 16.
The guide vanes 17, 17 are located on the upper opening edge, and are closely fixed to the inner circumferential surface of the casing 1, integrally with the outer circumferential end surfaces of the top plate 15 and the bottom plate 16, and are independent between the adjacent guide vanes 17, 17. Return passage 14a
is formed to eliminate circulation and leakage of gas flow.

さらに、これらの案内羽根17を立設した通路
底板16を、その外周端より戻り通路出口19に
向つて漸次下方に傾斜させると共に前記案内羽根
17の高さをその傾斜に従つて外端より内端に向
かい徐々に高くして戻り通路14の高さを漸次拡
大させることにより、戻り通路14での流速を
徐々に減速させて流れの運動エネルギーを圧力に
変換し、圧力回収をする形状に形成してある。
Further, the passage bottom plate 16 on which these guide vanes 17 are erected is gradually inclined downward from its outer peripheral end toward the return passage outlet 19, and the height of the guide vanes 17 is adjusted inwardly from the outer end according to the inclination. By gradually increasing the height of the return passage 14 toward the end, the flow velocity in the return passage 14 is gradually decelerated, the kinetic energy of the flow is converted into pressure, and the pressure is recovered. It has been done.

なお、案内羽根17と戻り通路上板15との一
体化は、これらの案内羽根17の上端に突設した
係止爪20を戻り通路上板15に穿設した係合細
孔21に挿着、係止させることにより行つてお
り、又、図示していないが、案内羽根17の下端
も戻り通路底板16に対して同一構造で固定され
てある。
The guide vanes 17 and the return passage upper plate 15 are integrated by inserting locking claws 20 protruding from the upper ends of these guide vanes 17 into engagement holes 21 bored in the return passage upper plate 15. Although not shown, the lower end of the guide vane 17 is also fixed to the return passage bottom plate 16 with the same structure.

22は昇圧羽根片で、戻り通路上板15の各通
路入口18の内端円弧面18aにその上端を一体
的に連設させて戻り通路上板15に対し、下方に
直角に垂下してなるものであり、その一側端面を
案内羽根17の背面に全高を亘つて密接させて戻
り通路14の一部にケーシング1の内周面と同心
円状の通路を形成し、通路上板15の通路入口1
8からの流れの圧力回収を行うものである。
Reference numeral 22 denotes a booster blade piece, whose upper end is integrally connected to the inner end circular arc surface 18a of each passage inlet 18 of the return passage upper plate 15, and hangs downward at right angles to the return passage upper plate 15. One end surface of the guide blade 17 is brought into close contact with the back surface of the guide vane 17 over the entire height to form a passage concentric with the inner peripheral surface of the casing 1 in a part of the return passage 14, and the passage of the passage upper plate 15 is Entrance 1
This is to perform pressure recovery of the flow from 8.

この昇圧羽根片22は、羽根車下面板11の外
径と略等しい半径の位置に設けるのが良く、その
周方向の長さ(横巾)も通路入口18の周方向の
長さの60〜85%の長さにすると圧力回収の効果が
最大となる。
This booster blade piece 22 is preferably provided at a position with a radius that is approximately equal to the outer diameter of the impeller lower plate 11, and its circumferential length (width) is also 60 to 60 mm larger than the circumferential length of the passage entrance 18. A length of 85% maximizes the pressure recovery effect.

以上のように構成した実施例の作用を述べる
と、電動機4を始動して羽根車7を回転させれ
ば、気流は吸入口3から羽根車7の入口9に流入
し、羽根12の昇圧作用により圧力を高めながら
遠心方向に流れ、羽根車7の上面板10の外周彎
曲部によつて下方(軸方向)にその流れを滑らか
に変化させて羽根車出口13から流出する。
To describe the operation of the embodiment configured as described above, when the electric motor 4 is started and the impeller 7 is rotated, airflow flows from the suction port 3 to the inlet 9 of the impeller 7, and the pressure increase effect of the impeller 12 is achieved. It flows in the centrifugal direction while increasing the pressure, and the flow is smoothly changed downward (in the axial direction) by the curved outer circumference of the upper surface plate 10 of the impeller 7 and flows out from the impeller outlet 13.

この羽根車出口13における流速分布は、出口
13の内外周端縁が同一平面上にあり、且つ戻り
通路上板15の開口されていない部分が近接状態
で平行に対設しているので略均一となり、その流
れは戻り通路上板15に穿設した複数個の通路入
口18に分割されて流入し、各通路入口18と連
通した分割戻り通路14a内を夫々流通する。
The flow velocity distribution at the impeller outlet 13 is approximately uniform because the inner and outer circumferential edges of the outlet 13 are on the same plane, and the unopened portions of the return passage upper plate 15 are disposed close to each other in parallel. The flow is divided into a plurality of passage entrances 18 formed in the return passage upper plate 15 and flows into the divided return passages 14a communicating with each passage entrance 18.

各戻り通路14aの入口部には案内羽根17の
外面側に突出させた昇圧羽根片22が設けられて
いるため、この昇圧羽根片22の外周空間が圧力
空気室的な働きをなし、戻り通路入口18からの
流れの速度が一担減速され、静圧変換されて圧力
上昇する。すなわち昇圧することとなる。また、
この昇圧羽根片22をもうける事により、戻り通
路入口からの流れの乱流や変動等を有する流れが
均一化されて、そのロスを改善すると共に、是圧
羽根片22より後流側では、整流され均一化され
た流れになり、昇圧羽根片以降での流速の低下に
相応する圧力の回収を効率化せしめてより昇圧さ
れる。
Since a booster blade piece 22 protruding from the outer surface of the guide blade 17 is provided at the entrance of each return passage 14a, the outer circumferential space of this booster blade piece 22 functions like a pressure air chamber, and the return passage The velocity of the flow from the inlet 18 is reduced once, and the static pressure is converted to increase the pressure. In other words, the pressure will be increased. Also,
By providing this pressure-boosting blade piece 22, the turbulent flow or fluctuation of the flow from the return passage inlet is made uniform, and the loss is improved. This results in a homogenized flow, which makes it possible to efficiently recover the pressure corresponding to the decrease in flow velocity after the booster vane piece, resulting in a higher pressure.

さらに本実施例においては、通路底板16は流
れの方向に外端から中心に向かつて下方に傾斜し
ているので、流れが通路底板16に強く衝突した
り大きく規制されることなく円滑に通路出口19
まで流れ、圧力損失の低減を図ることができる。
Furthermore, in this embodiment, the passage bottom plate 16 is inclined downward from the outer end toward the center in the flow direction, so that the flow can smoothly exit the passage without colliding strongly with the passage bottom plate 16 or being greatly restricted. 19
It is possible to reduce pressure loss.

第6図は、第4図で示す本発明の送風機と、第
1図、第2図で示す従来例の送風機とを、ケーシ
ング内径180mmの同じ寸法で、羽根車の羽根枚数、
戻り通路の案内羽根数も同一にして製作し、それ
ぞれ2400rpmの同一回転数で運転した時の圧力一
風量特性の比較を示したものであり、実線は本発
明の一実施例の特性を表わし、破線は従来の送風
機のフアン特性を表わしている。
Fig. 6 shows a comparison between the blower of the present invention shown in Fig. 4 and the conventional blower shown in Figs.
This shows a comparison of the pressure-airflow characteristics when the return passages were manufactured with the same number of guide vanes and each was operated at the same rotation speed of 2400 rpm, and the solid line represents the characteristics of one embodiment of the present invention. The broken line represents the fan characteristics of a conventional blower.

この図からも明らかなように、本発明の送風機
によれば、軸方向に環状出口13を有する羽根車
7と、この環状出口13と対面する戻り通路入口
18の形状と、戻り通路入口18の内端円弧面に
配設した昇圧羽根片22との相乗効果により、フ
アン圧力が従来の送風機に比べて1.5倍にもなり、
高圧化を達成し得るものでである。
As is clear from this figure, according to the blower of the present invention, the impeller 7 has an annular outlet 13 in the axial direction, the shape of the return passage inlet 18 facing the annular outlet 13, and the shape of the return passage inlet 18. Due to the synergistic effect with the booster blade piece 22 arranged on the inner arcuate surface, the fan pressure is 1.5 times that of a conventional blower.
This makes it possible to achieve high pressure.

以上のように本発明は、ケーシング内に羽根車
を回転自在に配設すると共にこの羽根車の下方に
近接させて通路上板と通路底板間に略円弧状に彎
曲した複数枚の案内羽根を放射状に設けてなる戻
り通路を固設し、この戻り通路の前記上板外周部
に前記羽根車の出口と連通する通路入口を開設す
ると共に通路底板中央にフアン出口を開口させ、
さらに戻り通路の案内羽根の凸彎曲面側に昇圧羽
根片を配設した送風機に係るものであるから、羽
根車に近接させて通路上板を配設し、この通路上
板の外周部に羽根車の出口と連通する通路入口を
設けているので、羽根車からの流れが迅速且つ円
滑に通路入口に流入して流れの漏洩や回流が生じ
ることがなく、且つケーシングの内周面に流れが
衝突したり壁面との摩擦損失等を生じさせること
がないものであり、従つて、圧力損失を大巾に減
少させて効率の良い送風を可能にし得るものであ
る。
As described above, the present invention includes an impeller rotatably disposed within a casing, and a plurality of guide vanes curved in an approximately arc shape between a passage top plate and a passage bottom plate, which are placed close to the bottom of the impeller. A return passage formed in a radial manner is fixedly installed, a passage entrance communicating with the outlet of the impeller is opened at the outer periphery of the upper plate of the return passage, and a fan outlet is opened at the center of the passage bottom plate,
Furthermore, since this relates to a blower in which a booster blade piece is arranged on the convex curved surface side of the guide vane of the return passage, a passage upper plate is arranged close to the impeller, and the blades are placed on the outer periphery of this passage upper plate. Since the passage entrance is provided to communicate with the car outlet, the flow from the impeller quickly and smoothly flows into the passage entrance, preventing flow leakage or circulation, and preventing the flow from forming on the inner peripheral surface of the casing. It does not cause collision or friction loss with the wall surface, and therefore can greatly reduce pressure loss and enable efficient air blowing.

又、羽根車の出口を戻り通路入口に平行状態で
対向させて通路の始端部をなくし得るので、サイ
レン音の発生を殆んどなくすることができ、その
上、羽根車の外周壁面をケーシングの内周面に接
近させて流れの漏洩を両者間の細隙で防止できる
構造に形成でき、構造の簡素化を図ることができ
る。
In addition, since the outlet of the impeller is parallel to and faces the entrance of the return passage and the starting end of the passage can be eliminated, the generation of siren noise can be almost completely eliminated. The structure can be formed so that leakage of flow can be prevented by the narrow gap between the two, which can simplify the structure.

さらに本発明は、戻り通路内に放射状に配設し
た案内羽根を略円弧状に彎曲させて且つその凸彎
曲面側に昇圧羽根片を配設したので、戻り通路に
流入する気流がこの昇圧羽根片によつて均一な流
れに整流され且つその流速が低下して圧力の回収
による昇圧を図ることができると共に案内羽根に
より滑らかに通路出口まで導出させて大巾にフア
ン圧力を向上させることができるものである。
Further, in the present invention, the guide vanes arranged radially in the return passage are curved in a substantially arc shape, and the booster vane piece is arranged on the convex curved surface side, so that the airflow flowing into the return passage is directed to the booster vane. The flow is rectified into a uniform flow by the piece, and the flow velocity is reduced, making it possible to increase the pressure by recovering pressure, and by guiding it smoothly to the passage outlet by the guide vane, it is possible to greatly increase the fan pressure. It is something.

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

第1図は従来例における送風機の一部切欠斜視
図、第2図はその簡略断面図、第3図は同じく従
来例の別な送風機の一部切欠斜視図、第4図は本
発明の実施例を示す一部切欠斜視図、第5図は戻
り通路の構成部分を示す分解斜視図、第6図は本
発明と従来の送風機とのP−Q特性図である。 1はケーシング、3は吸入口、4は電動機、7
は羽根車、9は入口、12は羽根、13は環状出
口、14は戻り通路、15は通路上板、16は通
路底板、17は案内羽根、18は通路入口、19
は通路出口。
FIG. 1 is a partially cutaway perspective view of a conventional blower, FIG. 2 is a simplified sectional view thereof, FIG. 3 is a partially cutaway perspective view of another conventional blower, and FIG. 4 is an embodiment of the present invention. FIG. 5 is a partially cutaway perspective view showing an example, FIG. 5 is an exploded perspective view showing the constituent parts of the return passage, and FIG. 6 is a P-Q characteristic diagram of the present invention and a conventional blower. 1 is the casing, 3 is the intake port, 4 is the electric motor, 7
is an impeller, 9 is an inlet, 12 is a blade, 13 is an annular outlet, 14 is a return passage, 15 is a passage top plate, 16 is a passage bottom plate, 17 is a guide vane, 18 is a passage entrance, 19
is the passage exit.

Claims (1)

【特許請求の範囲】 1 円筒形ケーシング1内に、上面板10を下面
板11よりも大径にして軸方向に環状出口13を
開口する羽根車7を回転自在に配設し、この羽根
車7の下方に近接させて通路上板15と通路底板
16間に羽根車7の回転方向側に湾曲した複数の
案内羽根17を放射状に設けてなる戻り通路14
を固設し、この戻り通路14の通路上板15の外
周部に前記羽根車7の環状出口13と連通する戻
り通路入口18を開設すると共に、前記通路底板
16中央に戻り通路出口19を開口させ、さらに
前記戻り通路14の案内羽根17の背面に密接
し、前記通路上板15に対してほぼ直角に垂下し
てなる昇圧羽根片22を配設した送風機。 2 通路上板15に開口する戻り通路入口18
を、内端円孤面18aが羽根車7の下面板11の
外径と等しく外端面がケーシング1の内径と等し
い形状とし、且つ一方の側端面18bが案内羽根
17の湾曲面の凸側の曲面と等しく他方の側端面
18cが回転方向の次の案内羽根17の外端位置
から径方向直線状に延びる形状とした特許請求の
範囲第1項記載の送風機。 3 戻り通路14内に配設した昇圧羽根片22の
周方向の長さを戻り通路入口18の周方向の最小
開口巾よりも短くした特許請求の範囲第1項又は
第2項記載の送風機。
[Scope of Claims] 1. An impeller 7 having an upper plate 10 having a larger diameter than a lower plate 11 and an annular outlet 13 opening in the axial direction is rotatably disposed in a cylindrical casing 1, A return passage 14 in which a plurality of guide vanes 17 curved in the rotational direction of the impeller 7 are provided radially between a passage top plate 15 and a passage bottom plate 16 in close proximity to the lower side of the impeller 7.
A return passage inlet 18 communicating with the annular outlet 13 of the impeller 7 is opened at the outer periphery of the upper passage plate 15 of the return passage 14, and a return passage outlet 19 is opened at the center of the passage bottom plate 16. The blower is further provided with a booster blade piece 22 which is closely attached to the back surface of the guide blade 17 of the return passage 14 and hangs down approximately at right angles to the passage upper plate 15. 2 Return passage entrance 18 that opens in the passage upper plate 15
has a shape in which the inner circular arc surface 18a is equal to the outer diameter of the lower plate 11 of the impeller 7, and the outer end surface is equal to the inner diameter of the casing 1, and one side end surface 18b is the same as the convex side of the curved surface of the guide vane 17. 2. The blower according to claim 1, wherein the other side end surface 18c is equal to the curved surface and extends linearly in the radial direction from the outer end position of the next guide vane 17 in the rotational direction. 3. The blower according to claim 1 or 2, wherein the length in the circumferential direction of the booster blade piece 22 disposed in the return passage 14 is shorter than the minimum opening width in the circumferential direction of the return passage entrance 18.
JP21305281A 1981-12-31 1981-12-31 Fan Granted JPS58117395A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP21305281A JPS58117395A (en) 1981-12-31 1981-12-31 Fan

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP21305281A JPS58117395A (en) 1981-12-31 1981-12-31 Fan

Publications (2)

Publication Number Publication Date
JPS58117395A JPS58117395A (en) 1983-07-12
JPS6365840B2 true JPS6365840B2 (en) 1988-12-16

Family

ID=16632726

Family Applications (1)

Application Number Title Priority Date Filing Date
JP21305281A Granted JPS58117395A (en) 1981-12-31 1981-12-31 Fan

Country Status (1)

Country Link
JP (1) JPS58117395A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11357390B2 (en) 2017-10-13 2022-06-14 Olympus Winter & Ibe Gmbh Optical system for a stereo video endoscope

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11357390B2 (en) 2017-10-13 2022-06-14 Olympus Winter & Ibe Gmbh Optical system for a stereo video endoscope

Also Published As

Publication number Publication date
JPS58117395A (en) 1983-07-12

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