JPH0533793A - Mixed flow pump - Google Patents
Mixed flow pumpInfo
- Publication number
- JPH0533793A JPH0533793A JP18494091A JP18494091A JPH0533793A JP H0533793 A JPH0533793 A JP H0533793A JP 18494091 A JP18494091 A JP 18494091A JP 18494091 A JP18494091 A JP 18494091A JP H0533793 A JPH0533793 A JP H0533793A
- Authority
- JP
- Japan
- Prior art keywords
- diffuser
- impeller
- blade
- pump
- blades
- 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
(57)【要約】
【目的】羽根付きディフューザにおける流れの剥離発生
を抑制してポンプ効率を高め、併せてポンプ外径寸法も
小形化できるようにした斜流ポンプを提供する。
【構成】羽根車1と、羽根車カバー2と、羽根車カバー
を外周を包囲するケーシング3とからなり、かつ羽根車
カバーの周上に開口した吐出通路5にディフューザ羽根
6aを円形翼列に並べた羽根付きディフューザ6を設け
た斜流ポンプに対して、ディフューザ羽根の翼前縁を羽
根車の近くまで延長して羽根車の吐出口端面と平行に配
置し、さらに羽根付きディフューザの出口部にはディフ
ューザ羽根の翼列相互間に補助翼7を設ける。
(57) [Summary] [Object] To provide a mixed flow pump which suppresses the occurrence of flow separation in a diffuser with vanes to improve pump efficiency and, at the same time, can reduce the outer diameter dimension of the pump. [Structure] An impeller 1, an impeller cover 2, and a casing 3 surrounding the impeller cover, and a diffuser blade 6a in a circular blade row in a discharge passage 5 opened on the circumference of the impeller cover. For a mixed flow pump provided with aligned vaned diffusers 6, the blade leading edges of the diffuser vanes are extended to near the impeller and arranged parallel to the end face of the impeller outlet, and the outlet of the diffuser with vanes Is provided with auxiliary wings 7 between the rows of diffuser blades.
Description
【0001】[0001]
【産業上の利用分野】本発明は、蒸気タービン設備のボ
イラ水循環ポンプなどに適用される斜流ポンプ、特に該
ポンプに組み込んだ羽根付きディフューザの構成に関す
る。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a mixed flow pump applied to a boiler water circulation pump of a steam turbine facility, and more particularly to the structure of a vaned diffuser incorporated in the pump.
【0002】[0002]
【従来の技術】頭記したボイラ水循環ポンプのように高
温, 高圧の熱水を扱う斜流ポンプでは、ケーシングを堅
牢な半球形ケーシングとなし、かつ羽根車の出口とケー
シングとの間を連通するように羽根車カバーの周上に開
口した吐出通路に羽根付きディフューザを設けてポンプ
特性の向上化を図るようにした構成のものが従来より多
く採用されている。2. Description of the Related Art In a mixed flow pump that handles high temperature and high pressure hot water, such as the boiler water circulation pump described above, the casing is a robust hemispherical casing and the outlet of the impeller is connected to the casing. As described above, a structure in which a diffuser with blades is provided in a discharge passage opened on the circumference of an impeller cover to improve pump characteristics has been widely used.
【0003】図3,図4は従来におけるポイラ水循環ポ
ンプの構造を示すものであり、1は羽根車、2は羽根車
カバー、3は羽根車カバー2の外周を取り巻く半球形の
ケーシング、4は羽根車の駆動軸であり、羽根車1の吐
出側端面に対向してカバー2には半径方向の吐出通路5
が開口し、この吐出通路内に羽根付きディフューザ6が
設けてある。3 and 4 show the structure of a conventional boiler water circulation pump, wherein 1 is an impeller, 2 is an impeller cover, 3 is a hemispherical casing surrounding the outer circumference of the impeller cover 2, and 4 is The drive shaft of the impeller, which faces the discharge side end surface of the impeller 1 and has a radial discharge passage 5 in the cover 2.
Is opened, and a diffuser 6 with vanes is provided in the discharge passage.
【0004】ここで、羽根付きディフューザ6の従来構
造を図4で示すと、吐出通路5の入口側部分に空間を残
してその下流側の半径方向の通路部に多数枚のディフュ
ーザ羽根6aを周上に並べた円形翼列(減速翼列)が配
置されている。なお、図3でD1はケーシング3の外径、
d1は羽根車カバー2 の外径、また図4の翼列でβ1 はデ
ィフューザ羽根6aの入口角、Lは翼弦長、F1は流体の
流入方向、F2は流出方向を表す。FIG. 4 shows the conventional structure of the diffuser 6 with blades. A large number of diffuser blades 6a are formed in the radial passage portion downstream of the discharge passage 5 leaving a space at the inlet side portion. Circular blade rows (deceleration blade rows) arranged above are arranged. In FIG. 3, D1 is the outer diameter of the casing 3,
d1 is the outer diameter of the impeller cover 2, and in the blade row of FIG. 4, β1 is the inlet angle of the diffuser blade 6a, L is the chord length, F1 is the inflow direction of the fluid, and F2 is the outflow direction.
【0005】[0005]
【発明が解決しようとする課題】ところで、図3,図4
に示した従来構造の羽根付きディフューザでは次のよう
に欠点がある。
(1)ディフューザでの圧力回復を高めるようにディフ
ューザ羽根の翼弦長Lを大きくすると必然的に羽根車カ
バー2の外径d1、したがってケーシング3の外径D1も増
大してポンプ全体の図体が大形化する。By the way, FIG. 3 and FIG.
The conventional vaned diffuser shown in (1) has the following drawbacks. (1) When the chord length L of the diffuser blade is increased so as to enhance the pressure recovery in the diffuser, the outer diameter d1 of the impeller cover 2 and thus the outer diameter D1 of the casing 3 also inevitably increase, and the whole body of the pump is drawn. To become larger.
【0006】(2)羽根車1に対する出口線A−B(シ
ュラウド1aとハブ1bの外周縁を結んだ線)と羽根付
きディフューザ6の入口線C−D(ディフューザ羽根6
aの翼前縁)との間に残る吐出通路5の入口側空間領域
Pでは、通路壁の曲率半径r1が極端に小さいために流体
の流れの方向が急変し、羽根車1とディフューザ羽根6
aとが相互干渉して複雑な三次元の流れを形成する。特
にディフューザの入口線C−D上での速度分布について
見ると、羽根車1のシュラウド1aに近い側の流速がハ
ブ1bに近い側の流速に比べて極端に速くなる。このた
めにディフューザ羽根6aの入口角β1 を羽根車1 から
流入する流体の流れ方向にマッチさせるように設計する
ことが極めて困難であり、この結果としてポンプ運転時
にはディフューザ羽根6aの入口側部では表面に流れの
剥離が生じて剥離渦v1が発生し易くなる。また、ディフ
ューザ羽根6aの出口側においても、翼弦長Lが十分で
ないとディフューザ内で流速の急減が原因でディフュー
ザ羽根6aの表面から流れが剥離し、前記と同様に剥離
渦v2が生じ易くなる。しかも、このように剥離渦v1, v2
が発生すると、流体の流れのエネルギー損失が増えるた
めにポンプ効率が低下するほか、剥離渦が成長するとキ
ャビテーションが発生して騒音発生の原因にもなる。(2) Outlet line AB (line connecting the outer peripheral edges of shroud 1a and hub 1b) to impeller 1 and inlet line CD of diffuser 6 with blades (diffuser blade 6)
In the inlet side space area P of the discharge passage 5 remaining between the blade a and the blade leading edge (a), the direction of the fluid flow suddenly changes because the radius of curvature r1 of the passage wall is extremely small, and the impeller 1 and the diffuser blade 6
and a interfere with each other to form a complicated three-dimensional flow. Especially when looking at the velocity distribution on the inlet line CD of the diffuser, the flow velocity on the side of the impeller 1 close to the shroud 1a becomes extremely higher than the flow velocity on the side close to the hub 1b. For this reason, it is extremely difficult to design the inlet angle β1 of the diffuser vane 6a so as to match the flow direction of the fluid flowing from the impeller 1, and as a result, the surface of the inlet side of the diffuser vane 6a is not affected during pump operation. Separation of the flow occurs in the flow path and the separation vortex v1 is easily generated. Also, on the outlet side of the diffuser blade 6a, if the chord length L is not sufficient, the flow is separated from the surface of the diffuser blade 6a due to the rapid decrease of the flow velocity in the diffuser, and the separation vortex v2 is likely to occur as described above. .. Moreover, in this way the separation vortexes v1, v2
In addition to the above, the pump efficiency decreases due to an increase in the energy loss of the fluid flow, and when the separation vortex grows, cavitation occurs and causes noise.
【0007】本発明は上記の点にかんがみなされたもの
であり、その目的は羽根付きディフューザを改良するこ
とにより、ディフューザ内における流れの剥離渦の発生
を抑制してポンプ効率を高め、併せてポンプ外径寸法の
小形化が図れるようにした斜流ポンプを提供することに
ある。The present invention has been made in view of the above points, and an object thereof is to improve a diffuser with vanes to suppress the generation of flow separation vortices in the diffuser to improve pump efficiency and also to improve the pump efficiency. An object is to provide a mixed flow pump whose outer diameter size can be reduced.
【0008】[0008]
【課題を解決するための手段】上記目的は本発明によ
り、ディフューザ羽根の翼前縁を羽根車の近くまで延長
して羽根車の吐出口端と平行配置することにより達成さ
れる。また、前記の構成において、ディフューザの出口
部にはディフューザ羽根の翼列と組合わせて補助翼をデ
ィフューザ羽根の相互間に配列することができる。The above object is achieved according to the invention by extending the blade leading edge of the diffuser vane close to the impeller and parallel to the outlet end of the impeller. Further, in the above configuration, auxiliary blades may be arranged between the diffuser blades at the outlet of the diffuser in combination with the blade row of the diffuser blades.
【0009】[0009]
【作用】上記の構成において、まず、ディフューザ羽根
の翼前縁を羽根車の近くまで延長して羽根車の吐出口端
面と平行に配置することにより、ディフューザの入口部
で羽根車からディフューザに流入する流体の流れの3次
元性が弱まり、かつその入口線上での流体の流れについ
ても均一な速度分布が得られるようになる。したがっ
て、ディフューザ入口における流体の流入角をより正確
に予測してディフューザ羽根の入口角を流体の流入角に
マッチさせることが設計面で容易となるので、これによ
りディフューザ入口部での剥離渦の発生を良好に抑制で
きる。また、ディフューザ羽根の翼前縁を内径側(半径
の小さな方)へ伸ばした分だけディフューザ羽根の翼弦
長,つまりディフューザの実効的な流路長が長くとれる
ので、ディフューザの外径寸法,したがって羽根車カバ
ー,ケーシングの外径を縮小してポンプを小形に構成で
きる。さらに、ディフューザの出口部にはディフューザ
羽根の翼列と組合わせて補助翼を配列することにより、
翼弦長を敢えて長く設計しなくても、ディフューザ内の
流体通路に対する広がり角が小となり、出口側領域に発
生する流れの剥離を良好に防止できる。In the above structure, first, the blade leading edge of the diffuser blade is extended to the vicinity of the impeller and is arranged in parallel with the end face of the discharge port of the impeller so that the diffuser impinges from the impeller into the diffuser. The three-dimensionality of the flowing fluid is weakened, and a uniform velocity distribution can be obtained for the fluid flowing on the inlet line. Therefore, it becomes easier in terms of design to more accurately predict the inflow angle of the fluid at the diffuser inlet and match the inlet angle of the diffuser blade with the inflow angle of the fluid. Can be suppressed well. Also, since the chord length of the diffuser blade, that is, the effective flow path length of the diffuser, can be increased by the amount of extending the leading edge of the diffuser blade toward the inner diameter side (smaller radius), the outer diameter dimension of the diffuser, The pump can be made compact by reducing the outer diameter of the impeller cover and casing. Furthermore, by arranging auxiliary blades at the outlet of the diffuser in combination with the cascade of diffuser blades,
Even if the chord length is not designed to be long, the divergence angle with respect to the fluid passage in the diffuser becomes small, and the separation of the flow generated in the outlet side region can be favorably prevented.
【0010】[0010]
【実施例】図1,図2は本発明実施例の構成図であり、
図3,図4に対応する同一部材には同じ符号が付してあ
る。すなわち、図1,図2の構成において、羽根車カバ
ー2に開口した湾曲状の吐出通路5には、その内径(入
口側)から外径(出口側)に亙る全長域に羽根付きディ
フューザ6のディフューザ羽根6aの円形翼列が設けて
あり、かつディフューザ羽根6aの翼前縁(入口線C−
D)は羽根車1の吐出口端に接近してその出口線A−B
と平行となるよう傾斜して形成されている。さらにディ
フューザ6の出口部(ディフューザのスロート部より下
流側の領域)には、ディフューザ羽根6aの円形翼列に
対し、ディフューザ羽根の相互間に1枚ずつ翼弦長の短
い補助翼7が設けてある。なお、吐出通路5の壁面の曲
率半径r2は図3における曲率半径r1よりも大きく設計さ
れている。DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS FIGS. 1 and 2 are block diagrams of an embodiment of the present invention.
The same members corresponding to those in FIGS. 3 and 4 are denoted by the same reference numerals. That is, in the configuration of FIGS. 1 and 2, in the curved discharge passage 5 opened in the impeller cover 2, the vaned diffuser 6 is provided in the entire length region from the inner diameter (inlet side) to the outer diameter (outlet side). Circular blade rows of the diffuser blades 6a are provided, and the blade leading edge of the diffuser blades 6a (inlet line C-
D) approaches the discharge port end of the impeller 1 and its exit line AB
Is formed so as to be parallel to. Further, at the outlet of the diffuser 6 (a region on the downstream side of the throat of the diffuser), auxiliary blades 7 each having a short chord length are provided between the diffuser blades one by one with respect to the circular blade row of the diffuser blades 6a. is there. The radius of curvature r2 of the wall surface of the discharge passage 5 is designed to be larger than the radius of curvature r1 in FIG.
【0011】かかる構成により、先記[作用]の項で述
べたような作用効果が得られ、ディフューザ6での流れ
損失が少なくなってポンプ特性が向上するほか、羽根車
カバー2の外径d2, ケーシング3の外径D2を図3の外径
d1, D1よりも小さくしてポンプ全体を小形に構成でき
る。With such a configuration, the operation and effect described in the above section [Operation] can be obtained, the flow loss in the diffuser 6 is reduced to improve the pump characteristics, and the outer diameter d2 of the impeller cover 2 is improved. , The outer diameter D2 of the casing 3 is the outer diameter of FIG.
The entire pump can be made smaller by making it smaller than d1 and D1.
【0012】[0012]
【発明の効果】本発明の斜流ポンプは、以上説明したよ
うに構成されているので、ディフューザに発生する流体
の流れの剥離を抑制してポンプ効率の向上化が図れ、併
せて従来の構成と比べてポンプ全体の外径寸法を小形に
構成できる。Since the mixed flow pump of the present invention is constructed as described above, the separation of the flow of the fluid generated in the diffuser can be suppressed to improve the pump efficiency, and also the conventional construction. Compared with, the outer diameter of the entire pump can be made smaller.
【図1】本発明実施例の構成断面図FIG. 1 is a sectional view showing the configuration of an embodiment of the present invention.
【図2】図1における羽根付きディフューザの翼列を示
す吐出通路に沿った断面図FIG. 2 is a sectional view taken along the discharge passage showing a blade row of the vaned diffuser in FIG.
【図3】従来における斜流ポンプの構成断面図FIG. 3 is a sectional view showing the structure of a conventional mixed flow pump.
【図4】図2における羽根付きディフューザの翼列を示
す吐出通路に沿った断面図FIG. 4 is a sectional view taken along the discharge passage showing a blade row of the vaned diffuser in FIG.
1 羽根車 2 羽根車カバー 3 ケーシング 4 駆動軸 5 吐出通路 6 羽根付きディフューザ 6a ディフューザ羽根 7 補助翼 F1 流体の流入方向 F2 流体の流出方向 A−B 羽根車の出口線 C−D ディフューザの入口線 1 impeller 2 impeller cover 3 casing 4 drive shaft 5 discharge passages 6 Diffuser with blade 6a diffuser blade 7 Aileron F1 fluid inflow direction F2 fluid outflow direction Exit line of AB impeller Entrance line of CD diffuser
Claims (2)
を外周を包囲するケーシングとからなり、かつ羽根車カ
バーの周上に開口した吐出通路にディフューザ羽根を円
形翼列に並べた羽根付きディフューザを設けた斜流ポン
プにおいて、ディフューザ羽根の翼前縁を羽根車の近く
まで延長して羽根車の吐出口端と平行に配置したことを
特徴とする斜流ポンプ。1. A blade comprising an impeller, an impeller cover, and a casing surrounding the impeller cover, and a diffuser blade arranged in a circular blade row in a discharge passage opened on the circumference of the impeller cover. A mixed-flow pump provided with a diffuser, wherein the blade leading edge of the diffuser blade is extended to near the impeller and arranged parallel to the discharge port end of the impeller.
フューザ羽根の翼列と組合わせてディフューザの出口部
にはディフューザ羽根の相互間に補助翼を配列したこと
を特徴とする斜流ポンプ。2. The mixed flow pump according to claim 1, wherein auxiliary blades are arranged between the diffuser blades at the outlet of the diffuser in combination with the blade row of the diffuser blades.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP18494091A JPH0533793A (en) | 1991-07-25 | 1991-07-25 | Mixed flow pump |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP18494091A JPH0533793A (en) | 1991-07-25 | 1991-07-25 | Mixed flow pump |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH0533793A true JPH0533793A (en) | 1993-02-09 |
Family
ID=16162019
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP18494091A Pending JPH0533793A (en) | 1991-07-25 | 1991-07-25 | Mixed flow pump |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0533793A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2006046168A (en) * | 2004-08-04 | 2006-02-16 | Hitachi Ltd | Axial flow pump and mixed flow pump |
| JP2017214896A (en) * | 2016-06-01 | 2017-12-07 | 株式会社クボタ | Impeller |
| JP2017214897A (en) * | 2016-06-01 | 2017-12-07 | 株式会社クボタ | Impeller |
-
1991
- 1991-07-25 JP JP18494091A patent/JPH0533793A/en active Pending
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2006046168A (en) * | 2004-08-04 | 2006-02-16 | Hitachi Ltd | Axial flow pump and mixed flow pump |
| JP2017214896A (en) * | 2016-06-01 | 2017-12-07 | 株式会社クボタ | Impeller |
| JP2017214897A (en) * | 2016-06-01 | 2017-12-07 | 株式会社クボタ | Impeller |
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