JPH04334797A - Diffuser for centrifugal pump - Google Patents

Diffuser for centrifugal pump

Info

Publication number
JPH04334797A
JPH04334797A JP10709791A JP10709791A JPH04334797A JP H04334797 A JPH04334797 A JP H04334797A JP 10709791 A JP10709791 A JP 10709791A JP 10709791 A JP10709791 A JP 10709791A JP H04334797 A JPH04334797 A JP H04334797A
Authority
JP
Japan
Prior art keywords
guide vane
flow
pressure surface
vane
separation
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
JP10709791A
Other languages
Japanese (ja)
Inventor
Toto Takatani
高谷 任人
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.)
Hitachi Ltd
Original Assignee
Hitachi 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 Hitachi Ltd filed Critical Hitachi Ltd
Priority to JP10709791A priority Critical patent/JPH04334797A/en
Publication of JPH04334797A publication Critical patent/JPH04334797A/en
Pending legal-status Critical Current

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Abstract

PURPOSE:To reduce peeling-off from a guide vane at a low-flow range for highly reliable pump operation. CONSTITUTION:A guide vane inlet part 4 is provided with a projecting part 8 where a vane width 6 on the negative-pressure side is larger than a vane width 7 on the pressure side of the guide vane to a vane thickness center line 5 of the guide vane 2, and a communicating hole 12 communicating with a guide vane pressure surface 11 is provided at the guide vane negative-pressure surface 10 of a recessed part 9 on an final point of the projecting part. It is thus possible to reduce peeling-off flow from the guide vane inlet at the low-flow range, and prevent a head-discharge curve from becoming flat for highly reliable pump operation control.

Description

【発明の詳細な説明】[Detailed description of the invention]

【0001】0001

【産業上の利用分野】本発明は遠心ポンプに係り、特に
、ボイラ給水ポンプなど高圧のポンプに好適な遠心ポン
プのディフューザに関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a centrifugal pump, and more particularly to a diffuser for a centrifugal pump suitable for a high-pressure pump such as a boiler feed pump.

【0002】0002

【従来の技術】遠心形のポンプでは、羽根車から出た流
れを十分に静圧回復させ、ポンプの高効率化をはかるた
め、羽根車から出た後のディフューザ部には案内羽根を
持つディフューザ付遠心ポンプが用いられている(実開
昭54−147803号公報)。
[Prior Art] In a centrifugal pump, in order to sufficiently restore the static pressure of the flow coming out of the impeller and increase the efficiency of the pump, a diffuser with guide vanes is used in the diffuser section after the flow comes out of the impeller. A centrifugal pump with an attached centrifugal pump is used (Japanese Utility Model Publication No. 147803/1983).

【0003】従来のディフューザ付遠心ポンプでは大流
量から締切り状態の小流量までの広い流量範囲で運転さ
れる。このため、設計点からはずれた低流量域では、羽
根車から出た流れの案内羽根への流入角は、案内羽根の
入口角と異なって小さくなり、流れは案内羽根の負圧面
から剥離する。この剥離領域の大きさは小流量になるほ
ど大きくなる。
Conventional centrifugal pumps with diffusers operate in a wide flow rate range from large flow rates to small flow rates in a shut-off state. Therefore, in a low flow rate range away from the design point, the inflow angle of the flow from the impeller into the guide vane becomes smaller than the inlet angle of the guide vane, and the flow separates from the negative pressure surface of the guide vane. The size of this separation area increases as the flow rate decreases.

【0004】そこで、この剥離流れによる剥離損失のた
めディフューザ部では、十分な静圧回復が得られず、図
2に示すように、低流量域12では揚程曲線がフラット
11になる特性が発生する。このため、ポンプ運転の回
転数制御による流量の制御がうまく行われず運転の信頼
性を損う原因となる。
[0004] Therefore, due to the separation loss caused by this separation flow, sufficient static pressure recovery cannot be obtained in the diffuser section, and as shown in FIG. 2, a characteristic occurs in which the head curve becomes flat 11 in the low flow area 12. . For this reason, the flow rate cannot be properly controlled by controlling the rotational speed of the pump, resulting in a loss of operational reliability.

【0005】上述した低流量域での剥離流れを防止する
ために、実開昭59−192699号公報に記載のよう
に、案内羽根の圧力面と負圧面を貫通する貫通孔を設け
、圧力面と負圧面の圧力差により負圧面の貫通孔からは
負圧面に沿う流れを起こさせて案内羽根負圧面からの剥
離を低減する構造や、剥離の発生原因となる流れの流入
角と案内羽根の羽根入口角の不一致による剥離を生じな
いように、実開昭54−147803号公報に開示され
るような案内羽根を可変にする構造、さらに、特開昭5
9−231199号公報に記載のように羽根入口角をシ
ュラウド側とハブ側で異なるようにする構造などが考案
されている。
[0005] In order to prevent the above-mentioned separation flow in the low flow rate region, as described in Japanese Utility Model Application Publication No. 59-192699, a through hole passing through the pressure surface and the negative pressure surface of the guide vane is provided, and the pressure surface The structure reduces the separation of the guide vane from the suction surface by causing a flow from the through hole of the suction surface along the suction surface due to the pressure difference between the suction surface and the suction surface, and the inflow angle of the flow and the guide vane that cause separation. In order to prevent separation due to mismatch of blade entrance angles, a structure that makes the guide vanes variable as disclosed in Japanese Utility Model Application No. 54-147803, and furthermore,
As described in Japanese Patent No. 9-231199, a structure in which the blade inlet angle is made different between the shroud side and the hub side has been devised.

【0006】[0006]

【発明が解決しようとする課題】しかし、上記従来技術
の案内羽根の圧力面と負圧面を貫通する貫通孔を設け、
圧力面と負圧面の圧力差により負圧面に沿う流れを起こ
させて、案内羽根負圧面からの剥離を低減する構造の場
合には、貫通孔は案内羽根の強度上の制約から、剥離流
れが最も生じやすい案内羽根入口先端部には設けられず
、このため、剥離流れを低減する効果は小さい。また、
案内羽根を可変するものは、構造が複雑になり価格が高
くなるだけでなくケーシングが可動機構を設けるために
、ケーシングの強度上の問題があった。
[Problem to be Solved by the Invention] However, in the prior art, a through hole passing through the pressure surface and the negative pressure surface of the guide vane is provided,
In the case of a structure in which the flow along the suction surface is caused by the pressure difference between the pressure surface and the suction surface to reduce separation of the guide vane from the suction surface, the through hole is designed to prevent separation flow due to the strength constraints of the guide vane. It is not provided at the tip of the guide vane inlet where it is most likely to occur, and therefore the effect of reducing separation flow is small. Also,
Those with variable guide vanes not only have a complicated structure and high price, but also have problems with the strength of the casing because the casing is provided with a movable mechanism.

【0007】さらに、案内羽根の入口角をシュラウド側
とハブ側で異なるようにひねった三次元形状の案内羽根
では価格が高くなるほかに、羽根の強度が低下するとい
う問題があった。
[0007]Furthermore, a guide vane having a three-dimensional shape in which the entrance angle of the guide vane is twisted differently on the shroud side and the hub side has the problem that not only is the cost high, but the strength of the blade is reduced.

【0008】本発明の目的は、低流量運転域において、
案内羽根負圧面からの剥離を低減することにより、その
剥離により起こる揚程曲線がフラットになることを防止
して、全流量運転域において信頼性の高いポンプ運転制
御を行うことにある。
[0008] The object of the present invention is to:
By reducing the separation from the negative pressure surface of the guide vane, the lift curve caused by the separation is prevented from becoming flat, and highly reliable pump operation control is performed in the entire flow rate operation range.

【0009】[0009]

【課題を解決するための手段】上記目的は案内羽根入口
部に案内羽根の羽根厚中心線に対して、負圧面側の羽根
厚さを圧力面側の羽根厚さより大きくした凸部を設け、
かつ、その凸部の終点の凹部の案内羽根負圧面には案内
羽根圧力面に連通する連通孔を設けることにより達成さ
れる。
[Means for Solving the Problems] The above object is to provide a convex portion at the inlet of the guide vane with a thickness larger on the suction side than on the pressure side with respect to the blade thickness center line of the guide vane.
Moreover, this is achieved by providing a communication hole communicating with the guide vane pressure surface on the guide vane negative pressure surface of the concave portion at the end point of the convex portion.

【0010】0010

【作用】低流量域では案内羽根の羽根入口角度に対して
流れの流入角は小さくなる。このため、流れは案内羽根
の負圧面から剥離しやすくなるが、剥離のしやすい案内
羽根の入口部には、案内羽根の羽根中心線に対して負圧
面側の羽根厚さを圧力面側の羽根厚さより大きくした凸
部を設けかつ、その凸部の終点の凹部の案内羽根負圧面
には案内羽根圧力面に連通する連通孔を設けている。従
って、低流量域で流れの流入角が小さくなり、案内羽根
の負圧面から剥離が生じやすい流れになった場合、案内
羽根の負圧面の流れは低流量域での流れ方向に沿うよう
に設けた凸部に沿って剥離することなく流れ、かつ、そ
の凸部の終点の凹部には圧力面と連通する連通孔を設け
ているので圧力面と負圧面の圧力差により、負圧面側の
連通孔からは負圧面形状に沿った流れが生じるので、こ
の凹部でも流れは剥離あるいはよどむことなく羽根面に
沿って流れるので、羽根入口負圧面からの剥離流れは大
幅に低減することができる。
[Operation] In a low flow rate region, the inflow angle of the flow becomes smaller than the vane inlet angle of the guide vane. For this reason, the flow tends to separate from the suction side of the guide vane, but at the inlet of the guide vane where separation is likely, the blade thickness on the suction side with respect to the blade center line of the guide vane should be A convex portion larger than the blade thickness is provided, and a communication hole communicating with the guide vane pressure surface is provided on the guide vane negative pressure surface of the concave portion at the end of the convex portion. Therefore, if the inflow angle of the flow becomes small in the low flow rate region and the flow tends to separate from the negative pressure surface of the guide vane, the flow on the negative pressure surface of the guide vane should be arranged along the flow direction in the low flow rate region. The flow flows along the convex part without separation, and the concave part at the end of the convex part has a communication hole that communicates with the pressure surface, so the pressure difference between the pressure surface and the negative pressure surface causes the flow to flow on the negative pressure side. Since a flow is generated from the hole along the shape of the suction surface, the flow flows along the blade surface without separation or stagnation even in this recess, so that the separation flow from the suction surface at the blade inlet can be significantly reduced.

【0011】このため、案内羽根からの剥離流れの剥離
損失によって揚程曲線がフラットになることを防止でき
、全流量運転域において、信頼性の高いポンプの運転制
御ができる。
Therefore, it is possible to prevent the lift curve from becoming flat due to separation loss of the separated flow from the guide vanes, and highly reliable pump operation control can be performed in the entire flow rate operation range.

【0012】0012

【実施例】以下、本発明の一実施例を図1により説明す
る。羽根車1を出た後に配置された複数の案内羽根2を
持つディフューザ3で案内羽根の羽根入口部4には案内
羽根の羽根厚中心線5に対して案内羽根負圧面側の羽根
厚さt1 を圧力面側の羽根厚さt2 より大きくした
凸部6を設け、かつ、その凸部の終点の凹部7の案内羽
根負圧面8には案内羽根圧力面9に連通する連通孔10
を設けている。
[Embodiment] An embodiment of the present invention will be explained below with reference to FIG. In a diffuser 3 having a plurality of guide vanes 2 arranged after exiting the impeller 1, the vane inlet portion 4 of the guide vanes has a vane thickness t1 on the suction side of the guide vanes with respect to the vane thickness center line 5 of the guide vanes. A convex portion 6 is provided which is larger than the blade thickness t2 on the pressure surface side, and a communication hole 10 communicating with the guide vane pressure surface 9 is provided on the guide vane negative pressure surface 8 of the concave portion 7 at the end point of the convex portion.
has been established.

【0013】次に、その動作について説明する。設計流
量では羽根車を出てディフューザに流入する流れは案内
羽根2に沿った一様な流れである。しかし、低流量にな
るにつれて羽根車を出た流れは内向きとなり、案内羽根
の入口部4に流入する流れは案内羽根の入口角より小さ
くなる。このため、流れは案内羽根の負圧面8から剥離
しやすくなるが案内羽根入口部4では、案内羽根に流入
する流れは低流量域の流れ方向に合うように形成した案
内羽根負圧面8側の凸部6に沿って流れるので剥離する
ことはない。また、凸部6の終点の凹部7では、案内羽
根圧力面9と案内羽根負圧面8を連通させる連通孔10
を設けているので、圧力差により、流れの剥離やよどみ
が生じやすい凹部7からは案内羽根負圧面8に沿う流れ
が生じるので、この凹部7からも剥離が生じることはな
い。
Next, its operation will be explained. At the design flow rate, the flow leaving the impeller and entering the diffuser is a uniform flow along the guide vanes 2. However, as the flow rate decreases, the flow exiting the impeller becomes inward, and the flow entering the guide vane inlet 4 becomes smaller than the guide vane entrance angle. Therefore, the flow tends to separate from the negative pressure surface 8 of the guide vane, but at the guide vane inlet 4, the flow flowing into the guide vane is separated from the negative pressure surface 8 of the guide vane, which is formed to match the flow direction of the low flow rate region. Since it flows along the convex portion 6, it does not peel off. Further, in the concave portion 7 at the end point of the convex portion 6, a communication hole 10 is provided that communicates the guide vane pressure surface 9 with the guide vane negative pressure surface 8.
Since the flow along the guide vane negative pressure surface 8 is generated from the recess 7 where flow separation or stagnation is likely to occur due to the pressure difference, separation does not occur from the recess 7 either.

【0014】[0014]

【発明の効果】本発明によれば、低流量域で、案内羽根
負圧面からの剥離を防止し、剥離損失を大幅に低減でき
るので、全流量運転域で揚程曲線はフラットにならずに
右下がりにすることができるので、全流量運転域で信頼
性の高いポンプ運転の運転制御ができる。
Effects of the Invention According to the present invention, it is possible to prevent separation of the guide vane from the negative pressure surface in the low flow rate range, and to significantly reduce separation loss, so that the head curve is not flat in the full flow rate operation range but is rightward. Since the flow rate can be lowered, highly reliable pump operation control can be performed in the entire flow rate operation range.

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

【図1】本発明のディフューザ部の正面図。FIG. 1 is a front view of a diffuser section of the present invention.

【図2】従来の遠心ポンプディフューザの場合の揚程特
性図。
FIG. 2 is a head characteristic diagram of a conventional centrifugal pump diffuser.

【符号の説明】[Explanation of symbols]

1…羽根車、2…案内羽根、3…ディフューザ、4…案
内羽根の入口部、5…羽根厚中心線、6…負圧面側の羽
根厚さ、7…圧力面側の羽根厚さ、8…凸部、9…凹部
、10…案内羽根負圧面。
DESCRIPTION OF SYMBOLS 1... Impeller, 2... Guide vane, 3... Diffuser, 4... Inlet part of guide vane, 5... Blade thickness center line, 6... Blade thickness on suction side, 7... Blade thickness on pressure side, 8 ... Convex portion, 9... Concave portion, 10... Guide vane negative pressure surface.

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】案内羽根入口部には案内羽根の羽根厚中心
線に対して、前記案内羽根負圧面側の羽根厚さを前記案
内羽根圧力面側の羽根厚さより大きくした凸部を設け、
前記凸部の終点の前記凹部の前記案内羽根負圧面には前
記案内羽根圧力面に連通する連通孔を設けたことを特徴
とする遠心ポンプのディフューザ。
1. A convex portion is provided at the guide vane inlet, with respect to the blade thickness center line of the guide vane, the thickness of the blade on the negative pressure side of the guide vane being larger than the thickness of the blade on the pressure side of the guide vane,
A diffuser for a centrifugal pump, characterized in that a communication hole communicating with the guide vane pressure surface is provided on the guide vane negative pressure surface of the concave portion at the end point of the convex portion.
JP10709791A 1991-05-13 1991-05-13 Diffuser for centrifugal pump Pending JPH04334797A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP10709791A JPH04334797A (en) 1991-05-13 1991-05-13 Diffuser for centrifugal pump

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP10709791A JPH04334797A (en) 1991-05-13 1991-05-13 Diffuser for centrifugal pump

Publications (1)

Publication Number Publication Date
JPH04334797A true JPH04334797A (en) 1992-11-20

Family

ID=14450384

Family Applications (1)

Application Number Title Priority Date Filing Date
JP10709791A Pending JPH04334797A (en) 1991-05-13 1991-05-13 Diffuser for centrifugal pump

Country Status (1)

Country Link
JP (1) JPH04334797A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN100374733C (en) * 2004-02-23 2008-03-12 孙敏超 Radial single raw blade diffuser
GB2446918A (en) * 2007-02-20 2008-08-27 Schlumberger Holdings Centrifugal pump
JP2013194558A (en) * 2012-03-16 2013-09-30 Mitsubishi Heavy Ind Ltd Centrifugal pump

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN100374733C (en) * 2004-02-23 2008-03-12 孙敏超 Radial single raw blade diffuser
GB2446918A (en) * 2007-02-20 2008-08-27 Schlumberger Holdings Centrifugal pump
GB2446918B (en) * 2007-02-20 2009-12-02 Schlumberger Holdings Methods of making centrifugal pump impellers and/or diffusers, and centrifugal pumps incorporating such impellers and/or diffusers
US7857577B2 (en) 2007-02-20 2010-12-28 Schlumberger Technology Corporation System and method of pumping while reducing secondary flow effects
JP2013194558A (en) * 2012-03-16 2013-09-30 Mitsubishi Heavy Ind Ltd Centrifugal pump

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