JPS59192898A - Centrifugal impeller - Google Patents
Centrifugal impellerInfo
- Publication number
- JPS59192898A JPS59192898A JP6743083A JP6743083A JPS59192898A JP S59192898 A JPS59192898 A JP S59192898A JP 6743083 A JP6743083 A JP 6743083A JP 6743083 A JP6743083 A JP 6743083A JP S59192898 A JPS59192898 A JP S59192898A
- Authority
- JP
- Japan
- Prior art keywords
- angle
- blade
- impeller
- rotation
- blade part
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Landscapes
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
Description
【発明の詳細な説明】
本発明は、煎・Dボンデ、遠心送風機、遠・け圧縮機、
および過給機など、遠、()形の流体機械に用いられる
遠ノcy羽根車に関するものである。[Detailed Description of the Invention] The present invention provides a blower/D bonder, a centrifugal blower, a distant compressor,
The present invention relates to a cylindrical impeller used in a cylindrical fluid machine such as a supercharger or a supercharger.
第1図に従来のバックワード式の近心羽根車が示されて
藝る。すなわち入口側1から見た正面視に2ける羽根(
1)の形状會、内側から外、1111Mこ行<′Jcつ
れて、先ず直線放射方向1c伸びる直線放射羽根部CI
A)と1回転後方1i111区カーブするバックワード
羽根’J(IB)とから形成している。ここで(r、)
は入口弔径、(r2)は賦同部の半径、 (r3)は出
口半径、(のけ転向角、(β)は出口角、(A)は回転
方向を夫々示す。このよりなif成のバックワード式遠
心羽根車は、その他の速・U羽根車(直線放射式速Iu
羽根車。FIG. 1 shows a conventional backward type mesial impeller. In other words, when viewed from the front from the entrance side 1, the blades (
In the shape of 1), from the inside to the outside, 1111M row <'Jc, first, the linear radial blade part CI extends in the linear radial direction 1c.
A) and a backward blade 'J (IB) that curves 1i111 backwards by one rotation. where (r,)
is the inlet diameter, (r2) is the radius of the dispensing part, (r3) is the exit radius, (bending angle, (β) is the exit angle, and (A) is the rotation direction. The backward type centrifugal impeller of
impeller.
またはバックワード式it>羽根車)に比べて、/クッ
クワード羽根部(IB)Kよる流路の曲かり影響のため
、第1図(イ)で示す直線放射羽根部(tA)における
回転後方側に位置する流速の高い領域を、第1図(ロ)
で示すように流路の中央側にひきもどして羽根車出口で
の流速分布を均一化に近づける効果力玉ある。このよう
な均一化は、結果的に流体機械の流体動H< 6より高
めることができるのであるカニ、バックワード羽根邪(
IE)icThける流路の自力;りの大きさく転向角θ
)は、出口角βに制約カニあるので設定に限界があり、
流速分布のより均一化には限界があった。or backward type it > impeller), due to the bending influence of the flow path by the /cookward blade part (IB) K, the rotation backward in the straight radiating blade part (tA) shown in Fig. 1 (a). The area with high flow velocity located on the side is shown in Figure 1 (b).
As shown in , there is an effect ball that returns to the center of the flow path to bring the flow velocity distribution at the impeller outlet closer to uniformity. Such homogenization can result in higher fluid dynamics of fluid machinery than H < 6.
IE) The self-reliance of the flow path; the magnitude of the turning angle θ
), there is a limit to the setting because there is a constraint on the exit angle β.
There was a limit to making the flow velocity distribution more uniform.
本発明の目的とするところは、転向角を従来よりも大き
くし得る遠心羽根車を提供するところにある。An object of the present invention is to provide a centrifugal impeller that can have a larger turning angle than conventional impellers.
上記目的を達成するために本発明における速、L>羽根
車は、入口側から見た正面視に2ける羽根形状を、内側
から外側1に行くにつれて、先ず回転方向伺IVcカー
ブしたのち回転後方11vこカーブすべくS字形1c形
成して構成して藝る。In order to achieve the above object, the impeller of the present invention has a blade shape in the front view from the inlet side.As going from the inside to the outside 1, the impeller first curves in the rotation direction IVc, and then curves backward in the rotation direction. In order to curve 11v, an S-shape 1c is formed and constructed.
かかるイ4成iCよると、羽根形状をS字状に形成する
ことによって、出ロ丙ケ変史することなく転向角を大さ
くし得る。According to such a four-structure iC, by forming the blade shape into an S-shape, the turning angle can be increased without changing the starting point.
以丁に本発明の第1′大施例を第2図に基づhて説明す
る。木実施例ic>いては、入口側から見た正面視ニー
おける羽根(1)の形状を、内側1から外側4(行くに
つれて、先ず回転方向(A) 1111 i4−カーブ
したフォワード羽根部(Ic)と、回転後方側にカーブ
したバックワード羽根部(ID)とに上りS字形に形成
している。この実施例Qてよると、出口角(β)を変虻
することなく転向角(θ)を大きくし得、したがって第
2図し→で示すフォワード羽根部(Ic)における回転
後方11111に位置する流速の品い領域全、第2図に
)で示すように流路の中央ml IC、すなわち従来(
第1図)VC比べてざらに流路の中央側にひきもどして
。A first embodiment of the present invention will now be described with reference to FIG. 1111 i4 - The shape of the blade (1) in the front knee viewed from the inlet side is changed from the inner side 1 to the outer side 4 (as it goes, first the rotation direction (A) 1111 i4-curved forward blade part (Ic ) and the backward blade portion (ID) curved toward the rear side of rotation, forming an upward S-shape. According to this embodiment Q, the turning angle (θ) can be adjusted without changing the exit angle (β). ) can be increased, and therefore the entire flow velocity region located at the rear of rotation 11111 in the forward vane (Ic) shown by → in Figure 2, the central ml IC of the flow path as shown by ) in Figure 2, In other words, conventionally (
Figure 1) Compared to VC, roughly move it back to the center of the flow path.
羽根車出口での流速分布をより均一化し得る。The flow velocity distribution at the impeller outlet can be made more uniform.
第3図、第4図は本発明の@2実施例を示す。3 and 4 show @2 embodiment of the present invention.
すなわち羽根(1)の入口側をインデューサ部(IE)
を形成している。この矢施例による速IL:?羽根車は
、退・むポンプ、遠心送風機、遠・b圧縮機、2よび過
給機用として広範囲Vこ冶用し得る。In other words, the inlet side of the blade (1) is the inducer part (IE).
is formed. Fast IL according to this arrow example:? The impeller can be used in a wide range of V-type applications for retracting pumps, centrifugal blowers, far-b compressors, turbochargers, and superchargers.
上記構成の本発明νこおける速む羽根軍シ・ζよると、
羽根形状をS字状Jこ形成することによって、出口角を
変更することなく転向角を大きくすることができ、した
かつて流路の曲がり4(よる効果を大きくできて、流速
の諸い領域を流路のより中央1Illjへひきもどして
流速分布の均一化をはかることができる。According to the present invention ν with the above configuration, the speeding blade army ζ is
By forming the blade shape into an S-shape, the turning angle can be increased without changing the exit angle, and the bending effect of the flow path can be increased, and various regions of flow velocity can be improved. The flow velocity distribution can be made uniform by returning the flow to the center 1Illj of the flow path.
第1図は従来例全示す概略正面図、第2図は本発明の第
1要施例會示す概略正面図、第3図、第4図は本発明の
第2実施例を示し、第3図は概略正面図、第4図は概略
縦断側面図である。
(1)・・・羽根+ (tC)・・・フォワード羽根部
、(ID)・・・バックワード羽根部、 (IE)・・
・インデューサ部、(rl)・・・入口半径、(r、)
・・・転向部半径、(r3)・・・出口半径、(θ)・
・・転向角、(β)・・・出口角、(A)・・・回転方
向、(ハ)(勾・・・流速分布
手続補正書(陶6)
1.事件の表示
昭和 58 イ1持 γ1 願第 67430
′52発明の名称
遠心羽根中
3補正をする者
事件との関係 特許出願人
冬称 (511)日立造船株式会仁
4代 理 人
住 所 〒550大阪市西区立売堀1丁目6番171号
アマノビル電話犬阪06 (532) 4025番(代
)氏名 (6808)弁理士森 本 義 弘5
の日付(発送日)昭和 年 月
日
6 補正により増加する発明の数
7補正の対象
1明細書の発1す]の詳細な説明の欄
(1)第2頁第3行目
「バンクワード式」とあるを1フづソー1式」と1;]
正する。
(2)第4頁第3行目
]−治用」とあるを1活川」と、II正する1、59FFig. 1 is a schematic front view showing the entire conventional example, Fig. 2 is a schematic front view showing the first embodiment of the present invention, Figs. 3 and 4 show the second embodiment of the invention, and Fig. 3 is a schematic front view showing the entire conventional example. is a schematic front view, and FIG. 4 is a schematic longitudinal sectional side view. (1)...Blade + (tC)...Forward blade part, (ID)...Backward blade part, (IE)...
・Inducer part, (rl)...Inlet radius, (r,)
... Turning part radius, (r3) ... Exit radius, (θ)
... Turning angle, (β) ... Exit angle, (A) ... Rotating direction, (c) (Gradient ... Flow velocity distribution procedure amendment form (Ceramics 6) 1. Indication of the incident Showa 58 I1 γ1 Application No. 67430
'52 Name of the invention Relationship with the person making the third amendment to the centrifugal vane Patent applicant Name: Fuyu (511) Hitachi Zosen Co., Ltd. Hitachi Zosen Co., Ltd., 4th generation director Personal address: Amano Building, 1-6-171 Tateuribori, Nishi-ku, Osaka 550 Telephone: Inusaka 06 (532) No. 4025 (Main) Name (6808) Patent Attorney Yoshihiro Morimoto 5
Date (shipment date) Showa year month
Day 6 Number of inventions increased by amendment 7 Target of amendment 1 Issue of specification 1 Detailed explanation column (1) 2nd page, 3rd line, ``Bank word type'' expression” and 1;]
Correct. (2) Page 4, line 3] - Correct 1, 59F, which says "Cure" as "1 life river"
Claims (1)
から外1111に行くにつれて、先ず回転方向1111
1にカーブしたのち回転後方側にカーブすべくS字形に
形成したこと金持欣とする速・U羽根車。1 The feather-shaped autumnal equinox seen from the front view KD from the population 1 rule, as you go from the inside to the outside 1111, first the rotation direction 1111
The U impeller is unique in that it is formed into an S-shape so that it curves in the direction of 1 and then curves toward the rear of rotation.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP6743083A JPS59192898A (en) | 1983-04-15 | 1983-04-15 | Centrifugal impeller |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP6743083A JPS59192898A (en) | 1983-04-15 | 1983-04-15 | Centrifugal impeller |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS59192898A true JPS59192898A (en) | 1984-11-01 |
Family
ID=13344682
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP6743083A Pending JPS59192898A (en) | 1983-04-15 | 1983-04-15 | Centrifugal impeller |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS59192898A (en) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4737077A (en) * | 1986-09-12 | 1988-04-12 | Aciers Et Outillage Peugeot | Profiled blade of a fan and its application in motor-driven ventilating devices |
JPH0367097A (en) * | 1989-05-26 | 1991-03-22 | Taiheiyo Kiko Kk | Impeller for turbo pump for water-jet propeller and turbo pump provided with same |
JP2004100663A (en) * | 2002-09-13 | 2004-04-02 | Hitachi Home & Life Solutions Inc | Air conditioner |
DE10250776A1 (en) * | 2002-10-30 | 2004-05-13 | Siemens Ag | Impeller for a centrifugal pump |
US7241114B2 (en) | 2002-10-30 | 2007-07-10 | Siemens Ag | Rotor for a centrifugal pump |
JP2014511973A (en) * | 2011-04-21 | 2014-05-19 | カーエスベー・アクチエンゲゼルシャフト | Impeller used for centrifugal pump |
CN104019056A (en) * | 2014-05-29 | 2014-09-03 | 江苏大学 | Method for designing hydraulic model of blade front bent type circulating booster pump |
WO2017012825A1 (en) * | 2015-07-17 | 2017-01-26 | Ksb Aktiengesellschaft | Centrifugal pump blade profile |
-
1983
- 1983-04-15 JP JP6743083A patent/JPS59192898A/en active Pending
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4737077A (en) * | 1986-09-12 | 1988-04-12 | Aciers Et Outillage Peugeot | Profiled blade of a fan and its application in motor-driven ventilating devices |
JPH0367097A (en) * | 1989-05-26 | 1991-03-22 | Taiheiyo Kiko Kk | Impeller for turbo pump for water-jet propeller and turbo pump provided with same |
JP2004100663A (en) * | 2002-09-13 | 2004-04-02 | Hitachi Home & Life Solutions Inc | Air conditioner |
DE10250776A1 (en) * | 2002-10-30 | 2004-05-13 | Siemens Ag | Impeller for a centrifugal pump |
US7241114B2 (en) | 2002-10-30 | 2007-07-10 | Siemens Ag | Rotor for a centrifugal pump |
JP2014511973A (en) * | 2011-04-21 | 2014-05-19 | カーエスベー・アクチエンゲゼルシャフト | Impeller used for centrifugal pump |
CN104019056A (en) * | 2014-05-29 | 2014-09-03 | 江苏大学 | Method for designing hydraulic model of blade front bent type circulating booster pump |
WO2017012825A1 (en) * | 2015-07-17 | 2017-01-26 | Ksb Aktiengesellschaft | Centrifugal pump blade profile |
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