JP3124517B2 - High specific speed mixed flow pump - Google Patents

High specific speed mixed flow pump

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Publication number
JP3124517B2
JP3124517B2 JP09318939A JP31893997A JP3124517B2 JP 3124517 B2 JP3124517 B2 JP 3124517B2 JP 09318939 A JP09318939 A JP 09318939A JP 31893997 A JP31893997 A JP 31893997A JP 3124517 B2 JP3124517 B2 JP 3124517B2
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JP
Japan
Prior art keywords
hub
impeller
specific speed
mixed flow
high specific
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 - Fee Related
Application number
JP09318939A
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Japanese (ja)
Other versions
JPH11141491A (en
Inventor
富太郎 豊倉
裕久 武田
Original Assignee
株式会社電業社機械製作所
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Priority to JP09318939A priority Critical patent/JP3124517B2/en
Publication of JPH11141491A publication Critical patent/JPH11141491A/en
Application granted granted Critical
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Anticipated expiration legal-status Critical
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Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【発明の属する技術分野】本発明は、規定吐出し量より
少ない吐出し量の運転領域にあっても、サージングを生
じることがなく、また軸動力の著しい変動と増加を抑制
するようにした高比速度の斜流ポンプに関するものであ
る。
BACKGROUND OF THE INVENTION The present invention relates to a high-performance engine in which surging does not occur and remarkable fluctuations and increases in shaft power are suppressed even in an operation range in which the discharge rate is smaller than a specified discharge rate. It relates to a mixed flow pump having a specific speed.

【0002】[0002]

【従来の技術】一般的に、高揚程ポンプは比速度が小さ
く、低揚程ポンプは比速度が大きく、流量および全揚程
などの使用条件に応じて最適な形式のポンプが採用され
る。しかるに、近年にあってはポンプ設備費の軽減を図
るために、比速度の大きなポンプを高揚程で用いて、ポ
ンプを小型化することが要望されている。そこで、比速
度Nsが1000以上の高比速度の斜流ポンプを高揚程
で用いる研究が盛んになされている。
2. Description of the Related Art In general, a high-head pump has a low specific speed, and a low-head pump has a high specific speed, and a pump of an optimum type is adopted according to use conditions such as a flow rate and a total head. However, in recent years, in order to reduce the cost of pump equipment, it has been demanded to use a pump having a large specific speed at a high head and to reduce the size of the pump. Therefore, researches on using a mixed flow pump having a high specific velocity Ns of 1000 or more at a high head have been actively conducted.

【0003】従来の高比速度の斜流ポンプの一例を図6
ないし図9を参照して説明する。図6は、従来の高比速
度の斜流ポンプの要部断面図である。図7は、図6に示
す従来の高比速度の斜流ポンプの羽根車の外観斜視図で
ある。図8は、図6に示す高比速度の斜流ポンプのポン
プ特性図である。図9は、従来の高比速度の斜流ポンプ
の羽根車羽根の子午断面上の形状を示すとともに吐出し
量の少ない運転領域でサージングなどを起こす虞がある
ことを説明する図である。
FIG. 6 shows an example of a conventional mixed flow pump having a high specific speed.
This will be described with reference to FIG. FIG. 6 is a sectional view of a main part of a conventional high specific speed mixed flow pump. FIG. 7 is an external perspective view of the impeller of the conventional high specific speed mixed flow pump shown in FIG. FIG. 8 is a pump characteristic diagram of the mixed flow pump having the high specific speed shown in FIG. FIG. 9 is a diagram showing the shape of the impeller blades of the conventional high specific speed mixed flow pump on a meridional section and explaining the possibility that surging or the like may occur in an operation region where the discharge amount is small.

【0004】まず、図6を参照して、従来の高比速度の
斜流ポンプの構造を説明する。内ケーシング10に軸受
12を介して主軸14が軸回りに回転自在に支承され
る。この主軸14の先端部にハブ16が固定され、この
ハブ16の外周壁に複数枚の羽根車羽根18、18…が
設けられる。ハブ16と羽根車羽根18、18…で羽根
車が形成されている。また、内ケーシング10と同軸上
に外ケーシング20が配設され、この外ケーシング20
と内ケーシング10の間に複数枚の案内羽根22、22
…が設けられていて両者が一体化される。さらに、羽根
車羽根18、18…の外周縁の回転軌跡の外周囲で外ケ
ーシング20の先端に、吸込ケーシング24が連接され
る。
First, the structure of a conventional high specific speed mixed flow pump will be described with reference to FIG. A main shaft 14 is supported on the inner casing 10 via a bearing 12 so as to be rotatable around the axis. A hub 16 is fixed to the tip of the main shaft 14, and a plurality of impeller blades 18 are provided on the outer peripheral wall of the hub 16. The hub 16 and the impeller blades 18 form an impeller. An outer casing 20 is disposed coaxially with the inner casing 10.
And a plurality of guide vanes 22, 22
Are provided, and both are integrated. Further, a suction casing 24 is connected to the tip of the outer casing 20 around the outer periphery of the rotation trajectory of the outer peripheral edge of the impeller blades 18.

【0005】そして、比速度Nsが1250の斜流ポン
プの一例では、ハブ比D1/D2が約0.54であり、
子午断面上において、羽根車羽根18、18…のチップ
側出口端とハブ側出口端を通る直線と主軸14のなす角
θは約48度であり、羽根車羽根18、18…のハブ側
入口端とハブ側出口端を通る直線と主軸14のなす角δ
(言い換えれば、ハブ16の外周壁と主軸14のなす
角)は約30度である。ここで、D1は羽根車羽根1
8、18…のハブ側出口端の外周径であり、D2はチッ
プ側出口端の外周径である。
In an example of a mixed flow pump having a specific speed Ns of 1250, the hub ratio D1 / D2 is about 0.54,
On the meridional section, the angle θ formed between the main shaft 14 and a straight line passing through the tip-side outlet end and the hub-side outlet end of the impeller blades 18, 18,... Is about 48 degrees, and the hub-side inlet of the impeller blades 18, 18,. Angle δ between the straight line passing through the end and the outlet end on the hub side and the spindle 14
(In other words, the angle between the outer peripheral wall of the hub 16 and the main shaft 14) is about 30 degrees. Here, D1 is the impeller blade 1
8, 18... Are the outer diameters of the outlet ends on the hub side, and D2 is the outer diameter of the outlet end on the chip side.

【0006】そこで、従来のこのような比速度Nsが比
較的大きい斜流ポンプの羽根車の形状は、図7に示すご
とく、ハブ16は比較的に頂角の小さい尖った円錐状で
あり、その外周壁に突設される羽根車羽根18、18…
は全体として花弁が大きく開いたように設けられてい
る。なお、従来は、羽根車吸込側の軸方向の流れに対し
て羽根車出口側のメリディヤン流れの方向を大きく変化
させると、損失が大きくなると考えられており、羽根車
羽根18、18…のハブ側入口端とハブ側出口端を通る
直線と主軸14のなす角δは、30度以下に設定されて
いた。
Therefore, as shown in FIG. 7, the shape of the conventional impeller of the mixed flow pump having a relatively large specific speed Ns is such that the hub 16 has a sharp conical shape with a relatively small apex angle. The impeller blades 18, 18 projecting from the outer peripheral wall are provided.
Is provided so that the petals open widely as a whole. Conventionally, it is considered that the loss increases when the direction of the flow of the meridian at the exit of the impeller is greatly changed with respect to the flow in the axial direction at the suction side of the impeller, and the hub of the impeller blades 18, 18,. The angle δ between a straight line passing through the side entrance end and the hub side exit end and the main shaft 14 was set to 30 degrees or less.

【0007】[0007]

【発明が解決しようとする課題】かかる従来の高比速度
の斜流ポンプは、規定吐出し量から吐出し量を減少させ
て運転すると、図8に示すごとく、まず軸動力が規定吐
出し量の軸動力よりも著しく増加し、駆動機の限度を超
えて駆動機を破損させる虞がある。なお、駆動機の軸動
力に余裕を持たせることは、駆動機がそれだけ高価なも
のとならざるを得ず、現実的な改善策とならない。さら
に、吐出し量を減少させると、全揚程の特性が部分的に
右上がりとなって、いわゆるサージングを生じ、安定し
た運転が得られない。そしてさらに、締切点近傍では、
軸動力が非常に増大する。
When such a conventional mixed flow pump having a high specific speed is operated with the discharge amount reduced from the specified discharge amount, first, as shown in FIG. , And may exceed the limit of the driving machine and damage the driving machine. It is to be noted that providing a margin for the shaft power of the drive unit is inevitably expensive for the drive unit, and is not a practical improvement measure. Further, when the discharge amount is reduced, the characteristics of the entire head partially rise rightward, so-called surging occurs, and stable operation cannot be obtained. And further, near the deadline,
Shaft power is greatly increased.

【0008】規定吐出し量における運転では、図9に実
線矢印で示すごとく、流体はメリディヤン方向に一様に
流れる。これは、羽根車内で流体が受け取る周方向速度
による遠心力に見合う半径方向の圧力勾配を生じ、この
圧力勾配と遠心力が釣り合うので流体はメリディヤン方
向に流れ、特に半径方向に移動することはない。しか
し、吐出し量が減少してくると、この釣り合いがくず
れ、遠心力が半径方向の圧力勾配より大きくなるため
に、流体はチップ側に移動するようになり、羽根車出口
側チップ付近で圧力とメリディヤン速度が増大する。こ
の結果、羽根車外側の吸込ケーシング24に添って羽根
車吸込側から吐出し側へ向かう流れの圧力勾配が大きく
なり、羽根車出口端に近いケーシング上で流れの剥離を
生じて損矢が増大する。さらに、吐出し量が減少する
と、ついには図9に破線矢印で示すごとく、流体が羽根
車内でハブ側からチップ側にメリディヤン方向に対して
斜めに移動するような流れを生じて、ハブ側出口端で逆
流を生じ、さらには羽根車吸込側チップ付近にも逆流を
発生させる。もって、損失がより増大し、軸動力も増大
する。
In operation at the specified discharge rate, the fluid flows uniformly in the Meridian direction as shown by the solid arrow in FIG. This creates a radial pressure gradient commensurate with the centrifugal force due to the circumferential velocity that the fluid receives within the impeller, and the fluid flows in the Meridian direction and does not move in the radial direction in particular because the pressure gradient and the centrifugal force are balanced. . However, when the discharge amount decreases, this balance is lost, and the centrifugal force becomes larger than the radial pressure gradient, so that the fluid moves to the tip side, and the pressure near the tip of the impeller outlet side is increased. And Meridian speed increases. As a result, the pressure gradient of the flow from the impeller suction side to the discharge side increases along with the suction casing 24 outside the impeller, and the flow is separated on the casing close to the impeller outlet end, thereby increasing the loss. I do. Further, when the discharge amount is reduced, a flow is generated such that the fluid moves obliquely from the hub side to the tip side in the impeller in the meridian direction, as shown by a broken arrow in FIG. Backflow occurs at the end, and further backflow occurs near the impeller suction side tip. As a result, the loss increases and the shaft power also increases.

【0009】このように、従来の高比速度の斜流ポンプ
では、規定吐出し量よりも少ない吐出し量での運転は困
難であって、高比速度でかつ高揚程の使用条件における
ポンプとしては不適当であった。
As described above, in the conventional mixed flow pump having a high specific speed, it is difficult to operate with a discharge amount smaller than a specified discharge amount. Was inappropriate.

【0010】本発明は、上述のごとき従来の高比速度の
斜流ポンプの問題点を解消すべくなされたもので、羽根
車半径方向の流れを抑制することで、サージングなどの
発生を抑えるようにした高比速度の斜流ポンプを提供す
ることを目的とする。
SUMMARY OF THE INVENTION The present invention has been made to solve the problems of the conventional high specific speed mixed flow pump as described above, and suppresses the occurrence of surging by suppressing the flow in the radial direction of the impeller. It is an object of the present invention to provide a mixed flow pump having a high specific speed.

【0011】[0011]

【課題を解決するための手段】かかる目的を達成するた
めに、本発明の高比速度の斜流ポンプは、子午断面上に
おいて、羽根車羽根のチップ側出口端とハブ側出口端を
通る直線と羽根車の主軸のなす角を40度以下とし、前
記羽根車羽根のハブ側入口端とハブ側出口端を通る直線
と前記主軸のなす角を30度以上とし、羽根車出口のハ
ブ比を0.6以上として構成されている。
In order to achieve the above object, a high specific speed mixed flow pump according to the present invention has a straight line passing through a tip end end and a hub end end of an impeller blade on a meridional section. The angle between the main shaft of the impeller and the main shaft is 40 degrees or less, the angle between the straight line passing through the hub-side inlet end and the hub-side outlet end of the impeller blade and the main shaft is 30 degrees or more, and the hub ratio of the impeller outlet is It is configured as 0.6 or more.

【0012】また、比速度Nsを1150以上に構成す
ることも可能である。
It is also possible to configure the specific speed Ns to be 1150 or more.

【0013】[0013]

【発明の実施の形態】以下、本発明の一実施例を図1な
いし図5を参照して説明する。図1は、本発明の高比速
度の斜流ポンプの一実施例の要部断面図である。図2
は、図1に示す本発明の高比速度の斜流ポンプの羽根車
の外観斜視図である。図3は、図1に示す高比速度の斜
流ポンプの羽根車羽根の子午断面上の形状を示す図であ
る。図4は、図1に示す高比速度の斜流ポンプのポンプ
特性図である。図5は、羽根車出口側の寸法を固定し、
羽根車羽根のハブ側入口端とハブ側出口端を通る直線と
主軸のなす角を52度を基準として角度を減少させた場
合の必要有効吸込ヘッドの比を示す図である。図1およ
び図2において、図6および図7と同じ部材には同じ符
号を付けて重複する説明を省略する。
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS One embodiment of the present invention will be described below with reference to FIGS. FIG. 1 is a sectional view of a main portion of an embodiment of a high specific speed mixed flow pump according to the present invention. FIG.
FIG. 2 is an external perspective view of an impeller of the high specific speed mixed flow pump of the present invention shown in FIG. 1. FIG. 3 is a diagram showing the shape of the impeller blades of the high specific velocity mixed flow pump shown in FIG. 1 on a meridional section. FIG. 4 is a pump characteristic diagram of the high specific speed mixed flow pump shown in FIG. FIG. 5 fixes the dimensions of the impeller outlet side,
It is a figure which shows the ratio of the required effective suction head when the angle which the straight line which passes through the hub-side entrance end and the hub-side exit end of an impeller blade makes with the main shaft is reduced based on 52 degrees. 1 and 2, the same members as those in FIGS. 6 and 7 are denoted by the same reference numerals, and redundant description will be omitted.

【0014】図1および図2において、図6および図7
に示す高比速度の斜流ポンプの構成と基本的には同じで
あるが、ハブ16および羽根車羽根18、18…の形状
が大きく相違している。まず、比速度Nsが1365の
高比速度の斜流ポンプにおいて、ハブ比D1/D2が
0.63とされ、子午断面上において、羽根車羽根1
8、18…のチップ側出口端とハブ側出口端を通る直線
と主軸14のなす角θは35度とされ、羽根車羽根1
8、18…のハブ側入口端とハブ側出口端を通る直線と
主軸14のなす角δ(言い換えれば、ハブ16の外周壁
と主軸14のなす角)は、52度とされている。ここ
で、D1は羽根車羽根18、18…のハブ側出口端の外
周径である。なお、本発明の実施例の説明において、比
速度Nsは、数1で示される。
1 and 2, FIG. 6 and FIG.
Are basically the same as the configuration of the mixed flow pump having the high specific speed shown in FIG. 1, but the shapes of the hub 16 and the impeller blades 18, 18,... First, in a mixed flow pump having a high specific speed Ns of 1365, the hub ratio D1 / D2 is set to 0.63, and the impeller blade 1
The angle θ between the main shaft 14 and a straight line passing through the tip-side outlet end and the hub-side outlet end of 8, 18... Is 35 degrees, and the impeller blade 1
The angle δ between the main shaft 14 and a straight line passing through the hub-side inlet end and the hub-side outlet end of 8, 18,... (In other words, the angle between the outer peripheral wall of the hub 16 and the main shaft 14) is 52 degrees. Here, D1 is the outer diameter of the hub-side outlet end of the impeller blades 18, 18,.... In the description of the embodiment of the present invention, the specific speed Ns is represented by Expression 1.

【数1】 (Equation 1)

【0015】そこで、本発明の高比速度の斜流ポンプの
羽根車の形状は、図2に示すごとく、ハブ16は比較的
に頂角が大きい平たくて低い円錐状であり、その外周壁
に突設される羽根車羽根18、18…は全体として花弁
が上流側にすぼんで閉じたように設けられている。本発
明の羽根車を示す図2と、従来の羽根車を示す図7を比
較すれば、その形状の相違は明らかであろう。そして、
かかる本発明のハブ16の形状にあっては、羽根車吸込
側の軸方向の流れに対して羽根車出口側のメリディヤン
方向の流れを大きく変化させるものであり、従来の常識
に反するものである。
Therefore, as shown in FIG. 2, the shape of the impeller of the mixed flow pump having a high specific speed according to the present invention is such that the hub 16 has a flat and low conical shape having a relatively large apex angle, and has an outer peripheral wall. The protruding impeller blades 18, 18,... Are provided so that the petals as a whole are narrowed toward the upstream side and closed. By comparing FIG. 2 showing the impeller of the present invention with FIG. 7 showing the conventional impeller, the difference in the shape will be apparent. And
The shape of the hub 16 of the present invention greatly changes the flow in the meridian direction on the exit side of the impeller with respect to the flow in the axial direction on the suction side of the impeller, which is contrary to conventional common sense. .

【0016】以下、ハブ16と羽根車羽根18、18…
に上述のごとき形状を採用した理由を説明する。従来の
高比速度の斜流ポンプでは規定吐出し量よりも吐出し量
が減少すると、羽根車羽根18、18…のチップ側出口
端とハブ側出口端における流体に作用する遠心力および
揚程の差が大きいことに起因して、サージングなどが発
生している。そこで、これを改善するためには、まず羽
根車羽根18、18…のチップ側出口端とハブ側出口端
の流体に作用する遠心力および揚程の差を少なくするこ
とが望ましい。かかる目的から、まず羽根車羽根18、
18…のチップ側出口端の径D2とハブ側出口端の径D
1を近づけて、ハブ比D1/D2を大きくする。そし
て、単にハブ比を大きくするならば、羽根車羽根18、
18…の出口端の流路面積が小さくなり必要な吐出し量
が確保できない。そこで、子午断面上における羽根車羽
根18、18…のチップ側出口端とハブ側出口端を通る
直線と主軸14のなす角θを小さくすればよい。さら
に、この角θが小さくなると、子午断面上で羽根車羽根
18、18…のチップ側出口端とハブ側出口端を通る直
線とハブ16の外周壁となす角φが小さくなる。この角
φが小さくなると、羽根車羽根18、18…の出口端付
近で、流れが一様にならず不安定となって性能が劣化す
ることが知られている。そこで、この角φを大きく設定
すべく、子午断面上における羽根車羽根18、18…の
ハブ側入口端とハブ側出口端を通る直線と主軸14のな
す角δ(すなわち、ハブ16の外周壁と主軸14のなす
角)を大きくする必要がある。
The hub 16 and the impeller blades 18, 18,...
The reason why the above-described shape is adopted will be described below. In the conventional high specific speed mixed flow pump, when the discharge amount is smaller than the specified discharge amount, the centrifugal force and the head acting on the fluid at the tip-side outlet end and the hub-side outlet end of the impeller blades 18, 18,... Due to the large difference, surging or the like occurs. Therefore, in order to improve this, it is desirable to reduce the difference between the centrifugal force and the lift acting on the fluid at the tip-side outlet end and the hub-side outlet end of the impeller blades 18, 18,. For this purpose, first, the impeller blades 18,
18, the diameter D2 of the outlet end on the tip side and the diameter D of the outlet end on the hub side
1 and the hub ratio D1 / D2 is increased. And if the hub ratio is simply increased, the impeller blades 18,
And the required discharge amount cannot be secured. Therefore, the angle θ between the straight line passing through the tip-side outlet end and the hub-side outlet end of the impeller blades 18 on the meridional section and the main shaft 14 may be reduced. Is smaller, the angle φ between the straight line passing through the tip-side outlet end and the hub-side outlet end of the impeller blades 18 on the meridional section and the outer peripheral wall of the hub 16 becomes smaller. It is known that, when the angle φ becomes small, the flow becomes uneven and unstable near the outlet end of the impeller blades 18, 18. Therefore, in order to increase the angle φ, the angle δ between the main shaft 14 and a straight line passing through the hub-side entrance end and the hub-side exit end of the impeller blades 18 on the meridional section (that is, the outer peripheral wall of the hub 16) (The angle between the main shaft 14 and the main shaft 14) needs to be increased.

【0017】かかる観点から、比速度Nsが1365
で、角θが35度で、ハブ比D1/D2が0.63およ
び角δが52度となるように設定した羽根車を用いて、
主軸14の回転数を1420rpmとして、本発明の高
比速度の斜流ポンプの性能試験を実施したところ、図4
に示すごときポンプ性能が得られた。図4から明らかな
ように、規定吐出し量よりも少ない吐出し量の運転領域
でも、全揚程で部分的に右上がりとなる箇所がなく、サ
ージングを生ずる虞がない。また、吐出し量の変化に伴
う軸動力の変化が、従来の高比速度のものに比べて少な
くなっていることが確認された。なお、比較対象とする
従来の高比速度の斜流ポンプは比速度Nsが1250で
あるのに対して、上記の本発明の高比速度の斜流ポンプ
の比速度Nsは1365であって、より厳しい条件下に
おいてポンプ特性の大幅な改善がなされている。
From this viewpoint, the specific speed Ns is 1365
Using an impeller set so that the angle θ is 35 degrees, the hub ratio D1 / D2 is 0.63, and the angle δ is 52 degrees,
When the performance test of the high specific speed mixed flow pump of the present invention was performed with the rotation speed of the main shaft 14 set to 1420 rpm, FIG.
The pump performance as shown in the figure was obtained. As is clear from FIG. 4, even in the operation region where the discharge amount is smaller than the specified discharge amount, there is no portion that rises partially to the right in the entire head, and there is no possibility of surging. Also, it was confirmed that the change in the shaft power due to the change in the discharge amount was smaller than that of the conventional high specific speed. The specific speed Ns of the conventional high specific speed mixed flow pump to be compared is 1250, whereas the specific speed Ns of the high specific speed mixed flow pump of the present invention is 1365. Significant improvements in pump characteristics have been made under more severe conditions.

【0018】さらに、比速度Nsを1150として、羽
根車羽根18、18…の出口側の算術平均直径Dmとハ
ブ側出口端の外周径D1の位置で羽根車羽根18、18
…の出口角がそれぞれ25度と52度で羽根枚数が5枚
の平均的な斜流ポンプを一例として、羽根車羽根18、
18…の出口側の算術平均直径Dmとハブ側出口端の外
周径D1の位置のフローパターンについて、ハブ比D1
/D2と角θを種々に変化させてエネルギー式および力
の釣り合い式を用いて流れを演算することで、ハブ比D
1/D2と角θの影響を調べた。この結果、ハブ比D1
/D2が0.6で角θが40度のときに、ハブ側出口端
D1と算術平均直径Dmの位置におけるメリディヤン速
度比と全揚程比が、0.8:1と0.9:1となった。
このメリディヤン速度比と全揚程比が大きいほどサージ
ングなどが生じない。そこで、メリディヤン速度比と全
揚程比を上記に等しいかまたはこれより大きくするため
には、角θが40度以下でありハブ比D1/D2が0.
6以上でなければならない。
Further, assuming that the specific speed Ns is 1150, the positions of the arithmetic mean diameter Dm on the outlet side of the impeller blades 18, 18,...
, And an impeller blade 18 as an example of an average mixed flow pump having exit angles of 25 degrees and 52 degrees and five blades, respectively.
The flow pattern at the position of the arithmetic mean diameter Dm on the outlet side and the outer peripheral diameter D1 at the outlet end on the hub side of the hub ratio D1
/ D2 and the angle θ are variously changed, and the flow is calculated using the energy equation and the force balance equation.
The effects of 1 / D2 and the angle θ were examined. As a result, the hub ratio D1
/ D2 is 0.6 and the angle θ is 40 degrees, the meridian speed ratio and the total head ratio at the position of the hub-side exit end D1 and the arithmetic average diameter Dm are 0.8: 1 and 0.9: 1. became.
The greater the Meridian speed ratio and the total head ratio, the less surging occurs. Therefore, in order to make the Meridian speed ratio and the total head ratio equal to or larger than the above, the angle θ is equal to or less than 40 degrees and the hub ratio D1 / D2 is set to 0.
Must be at least 6.

【0019】さらに、羽根車出口の流れが一様で安定な
ものとするために、子午断面上における羽根車羽根1
8、18…のハブ側入口端とハブ側出口端を通る直線と
主軸14のなす角δ(すなわち、ハブ16の外周壁と主
軸14のなす角)に対して、キャビテーション性能の観
点から検討を加えた。ポンプ性能実験に用いた本発明の
高比速度の斜流ポンプにおいて、ハブ16以外の羽根車
形状を変更せずに、D1を一定に保ちつつハブ16の外
周壁と主軸14のなす角δを52度と、これより小さな
値に変化させて必要有効吸込ヘッド(NPSH)を計算
した。そして、角δが52度の必要有効吸込ヘッドを基
準として他の角δにおける必要有効吸込ヘッドとの比を
求めたところ、図5に示すごとき関係が判明した。図5
に示されるように、角δが30度と25度では、それぞ
れ1.11と1.16となっている。高比速度の運転領
域では、キャビテーション性能がより厳しくなり、必要
有効吸込ヘッドが10%増大することは、キャビテーシ
ョン性能低下の限界と考えられるが、その範囲内にある
ためには、角δは30度以上であることが必要である。
そして、角δが25度では、羽根車出口の流れが安定し
ない場合があることが明らかとなった。
Further, in order to make the flow at the outlet of the impeller uniform and stable, the impeller blade 1
The angle δ between the straight line passing through the hub-side inlet end and the hub-side outlet end and the main shaft 14 (ie, the angle formed between the outer peripheral wall of the hub 16 and the main shaft 14) is examined from the viewpoint of cavitation performance. added. In the high specific speed mixed flow pump of the present invention used in the pump performance experiment, the angle δ between the outer peripheral wall of the hub 16 and the main shaft 14 was maintained while D1 was kept constant without changing the shape of the impeller other than the hub 16. The required effective suction head (NPSH) was calculated by changing the value to 52 degrees or smaller. Then, when the ratio to the required effective suction head at another angle δ was determined based on the required effective suction head having an angle δ of 52 degrees, the relationship shown in FIG. 5 was found. FIG.
As shown in the above, when the angle δ is 30 degrees and 25 degrees, they are 1.11 and 1.16, respectively. In the high specific speed operation region, the cavitation performance becomes more severe and the required effective suction head increase by 10% is considered to be the limit of the cavitation performance reduction. It is necessary to be at least degree.
When the angle δ was 25 degrees, it became clear that the flow at the exit of the impeller might not be stable.

【0020】なお、上記実施例では、羽根車羽根18、
18…の枚数は、図2で明らかなように4枚であるが、
これに限られず、従来例のごとく3枚またはそれ以上で
あっても良い。
In the above embodiment, the impeller blades 18,
The number of 18 ... is 4 as is clear from FIG.
The present invention is not limited to this, and may be three or more as in the conventional example.

【0021】[0021]

【発明の効果】以上説明したように、本発明の高比速度
の斜流ポンプは構成されているので、以下のごとき格別
な効果を奏する。
As described above, since the high specific speed mixed flow pump according to the present invention is constituted, the following special effects can be obtained.

【0022】本発明の高比速度の斜流ポンプにあって
は、規定吐出し量より吐出し量の少ない運転領域にあっ
ても、サージングや著しい軸動力の変動が無く、広い領
域で安定して運転を行うことができる。
In the mixed flow pump having a high specific speed according to the present invention, even in an operation region where the discharge amount is smaller than the specified discharge amount, there is no surging and a remarkable fluctuation of the shaft power, and the pump is stable in a wide region. Can be operated.

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

【図1】本発明の高比速度の斜流ポンプの一実施例の要
部断面図である。
FIG. 1 is a sectional view of a main portion of an embodiment of a high specific speed mixed flow pump according to the present invention.

【図2】図1に示す本発明の高比速度の斜流ポンプの羽
根車の外観斜視図である。
FIG. 2 is an external perspective view of the impeller of the high specific speed mixed flow pump of the present invention shown in FIG.

【図3】図1に示す高比速度の斜流ポンプの羽根車羽根
の子午断面上の形状を示す図である。
FIG. 3 is a view showing the shape of the impeller blade of the high specific velocity mixed flow pump shown in FIG. 1 on a meridional section.

【図4】図1に示す高比速度の斜流ポンプのポンプ特性
図である。
FIG. 4 is a pump characteristic diagram of the high specific speed mixed flow pump shown in FIG. 1;

【図5】羽根車出口側の寸法を固定し、羽根車羽根のハ
ブ側入口端とハブ側出口端を通る直線と主軸のなす角を
52度を基準として角度を減少させた場合の必要有効吸
込ヘッドの比を示す図である。
FIG. 5 is a view showing a necessary effect when an angle between a main shaft and a straight line passing through a hub-side inlet end and a hub-side outlet end of an impeller blade is fixed with respect to 52 degrees while fixing an impeller outlet side dimension. It is a figure which shows the ratio of a suction head.

【図6】従来の高比速度の斜流ポンプの要部断面図であ
る。
FIG. 6 is a sectional view of a main portion of a conventional mixed flow pump having a high specific speed.

【図7】図6に示す従来の高比速度の斜流ポンプの羽根
車の外観斜視図である。
FIG. 7 is an external perspective view of an impeller of the conventional high specific speed mixed flow pump shown in FIG.

【図8】図6に示す高比速度の斜流ポンプのポンプ特性
図である。
FIG. 8 is a pump characteristic diagram of the mixed flow pump having a high specific speed shown in FIG. 6;

【図9】従来の高比速度の斜流ポンプの羽根車羽根の子
午断面上の形状を示すとともに吐出し量の少ない運転領
域でサージングなどを起こす虞があることを説明する図
である。
FIG. 9 is a view showing the shape of the impeller blade of the conventional mixed flow pump having a high specific speed on a meridional section and explaining the possibility that surging or the like may occur in an operation region where the discharge amount is small.

【符号の説明】[Explanation of symbols]

14 主軸 16 ハブ 18 羽根車羽根 θ 子午断面上において、羽根車羽根のチップ側出口端
とハブ側出口端を通る直線と主軸のなす角 δ 子午断面上において、羽根車羽根のハブ側入口端と
ハブ側出口端を通る直線と主軸のなす角 D1 羽根車羽根のハブ側出口端の外周径 D2 羽根車羽根のチップ側出口端の外周径 φ 子午断面上で羽根車羽根のチップ側出口端とハブ側
出口端を通る直線とハブの外周壁となす角
14 Main shaft 16 Hub 18 Impeller blade θ In the meridional section, the angle between the straight line passing through the tip-side outlet end and the hub-side outlet end of the impeller blade and the main shaft δ On the meridional section, the hub-side inlet end of the impeller blade Angle between the straight line passing through the hub-side exit end and the main shaft D1 Outer diameter of the hub-side exit end of the impeller blade D2 Outer diameter of the tip-side exit end of the impeller blade φ With the tip-side exit end of the impeller blade in meridional section Angle between the straight line passing through the hub end and the outer peripheral wall of the hub

Claims (2)

(57)【特許請求の範囲】(57) [Claims] 【請求項1】 子午断面上において、羽根車羽根のチッ
プ側出口端とハブ側出口端を通る直線と羽根車の主軸の
なす角を40度以下とし、前記羽根車羽根のハブ側入口
端とハブ側出口端を通る直線と前記主軸のなす角を30
度以上とし、羽根車出口のハブ比を0.6以上として構
成したことを特徴とする高比速度の斜流ポンプ。
1. An angle between a straight line passing through the tip-side outlet end and the hub-side outlet end of the impeller blade and the main shaft of the impeller on a meridional section is 40 degrees or less, and the impeller blade has a hub-side inlet end. The angle between the straight line passing through the outlet end on the hub side and the main shaft is 30
And a hub ratio at the impeller outlet is set to 0.6 or more.
【請求項2】 請求項1記載の斜流ポンプにおいて、比
速度Nsを1150以上に構成したことを特徴とする高
比速度の斜流ポンプ。
2. The mixed flow pump according to claim 1, wherein the specific speed Ns is 1150 or more.
JP09318939A 1997-11-05 1997-11-05 High specific speed mixed flow pump Expired - Fee Related JP3124517B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP09318939A JP3124517B2 (en) 1997-11-05 1997-11-05 High specific speed mixed flow pump

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP09318939A JP3124517B2 (en) 1997-11-05 1997-11-05 High specific speed mixed flow pump

Publications (2)

Publication Number Publication Date
JPH11141491A JPH11141491A (en) 1999-05-25
JP3124517B2 true JP3124517B2 (en) 2001-01-15

Family

ID=18104682

Family Applications (1)

Application Number Title Priority Date Filing Date
JP09318939A Expired - Fee Related JP3124517B2 (en) 1997-11-05 1997-11-05 High specific speed mixed flow pump

Country Status (1)

Country Link
JP (1) JP3124517B2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP4350122B2 (en) 2006-12-20 2009-10-21 株式会社日立産機システム Mixed flow fan

Also Published As

Publication number Publication date
JPH11141491A (en) 1999-05-25

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