JPH05195989A - Impeller for centrifugal pump - Google Patents

Impeller for centrifugal pump

Info

Publication number
JPH05195989A
JPH05195989A JP801292A JP801292A JPH05195989A JP H05195989 A JPH05195989 A JP H05195989A JP 801292 A JP801292 A JP 801292A JP 801292 A JP801292 A JP 801292A JP H05195989 A JPH05195989 A JP H05195989A
Authority
JP
Japan
Prior art keywords
blade
impeller
blades
pump
blade inlet
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.)
Granted
Application number
JP801292A
Other languages
Japanese (ja)
Other versions
JP3276011B2 (en
Inventor
Tetsuo Fukazawa
徹雄 深沢
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.)
Pacific Machinery and Engineering Co Ltd
Original Assignee
Pacific Machinery and Engineering 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 Pacific Machinery and Engineering Co Ltd filed Critical Pacific Machinery and Engineering Co Ltd
Priority to JP00801292A priority Critical patent/JP3276011B2/en
Publication of JPH05195989A publication Critical patent/JPH05195989A/en
Application granted granted Critical
Publication of JP3276011B2 publication Critical patent/JP3276011B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Abstract

PURPOSE:To provide an impeller rotatable at high speed with little resistance as well as having a smaller number of blades than an existing one so as to provide a centrifugal pump with higher efficiency compared to a centrifugal pump of existing design. CONSTITUTION:A blade inlet edge 26 on the boss shroud 24a side is smoothly continued to the cylindrical boss shroud and projects largely to a blade eye part, and a blade inlet edge 26b is extended almost at a right angle to a rotary shaft. These blade inlet edges are connected by a circular smooth curve formed into protruding shape on the upper side to form a blade inlet edge, and a blade inlet angle is set to be almost 0 deg. at the boss shroud side inlet edge. In such an impeller, the pump specific speed, which is the pump design value, is to be in a range of 100-1,000, and the number of blades is to be three.

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、遠心ポンプの羽根車に
関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an impeller of a centrifugal pump.

【0002】[0002]

【従来の技術】従来の遠心ポンプの設計では、羽根数の
無限大の理論より理論式が導かれ、ポンプ発生揚程が決
定される。従って、羽根数が多ければ多いほどよいので
あるが、羽根数が多いと摩擦損失の増加とか、羽根厚の
影響による損失の増大が起こるので、或る羽根枚数が最
良の効率を与えることになる。
2. Description of the Related Art In the design of a conventional centrifugal pump, a theoretical formula is derived from the theory of infinite number of blades to determine the pump head. Therefore, the larger the number of blades, the better. However, the larger the number of blades, the more the friction loss increases and the loss due to the influence of the blade thickness. Therefore, a certain number of blades gives the best efficiency. ..

【0003】これらを加味した経験的な実験式として、
フライデーの式 または、ステパノフの式 (式中、Z:最高効率を生じる羽根数 D1 :羽根車入口径 D2 :羽根車出口径 β1 :羽根入口角 β2 :羽根出口角) などがあり、これらの式の最良羽根数としてZは5〜9
程度の間に計算されるので、従来設計の羽根車の羽根数
は5枚から9枚が最も多く採用される羽根数である。
As an empirical empirical formula that takes these into consideration,
Friday ceremony Or the Stepanov formula (Where Z is the number of blades that produce the highest efficiency, D 1 is the impeller inlet diameter, D 2 is the impeller outlet diameter, β 1 is the blade inlet angle, β 2 is the blade outlet angle), and so on. As Z is 5-9
The number of blades of the impeller of the conventional design is 5 to 9, which is the most adopted number of blades, since it is calculated within a period of time.

【0004】一方、幾何学的寸法が制約される羽根入口
では、羽根入口面積と羽根枚数の関係から見れば、羽根
枚数は少ない方が良い。羽根枚数を多くすると、同一メ
リデイアン断面の羽根車で実質的な羽根入口面積が減少
し、羽根入口部が抵抗となって損失が増大し、効率の劣
化を招くことになる。これに伴って、当然ポンプの吸込
能力も劣化することになる。羽根枚数を少なくすると、
発生揚程が減ることになるので、これを防ぐために羽根
車の回転数を増加して、ポンプケーシングの固定側で見
た羽根車の回転時に通過する羽根数を多くすればよいの
であるが、従来設計の羽根入口では高速化できないため
これを行うことができない。従って、前記のような羽根
数が採用される。
On the other hand, at the blade entrance where the geometrical size is restricted, the smaller number of blades is better in view of the relationship between the blade entrance area and the number of blades. When the number of blades is increased, the blade entrance area of the impeller having the same Meridian cross section is reduced, the blade entrance becomes resistance, and the loss is increased, resulting in deterioration of efficiency. Along with this, naturally the suction capacity of the pump also deteriorates. If you reduce the number of blades,
Since the generated head is reduced, in order to prevent this, the number of rotations of the impeller should be increased to increase the number of blades that pass when the impeller rotates as seen on the fixed side of the pump casing. This cannot be done because the blade entrance of the design cannot speed up. Therefore, the number of blades as described above is adopted.

【0005】[0005]

【発明が解決しようとする課題】本発明の目的は、従来
より少ない羽根枚数を有すると共に、高速でかつ小さい
抵抗で回転可能な羽根車であって、従来設計の遠心ポン
プより高い効率を与える遠心ポンプの羽根車を提供する
ことである。
SUMMARY OF THE INVENTION An object of the present invention is a centrifugal impeller that has a smaller number of blades than conventional ones and can rotate at a high speed and with a small resistance, and provides higher efficiency than a centrifugal pump of a conventional design. It is to provide a pump impeller.

【0006】[0006]

【課題を解決するための手段】上記の目的を達成するた
めに、本発明による遠心ポンプの羽根車は、特願平3-98
941 号に記載された羽根車の羽根形状を用いる。すなわ
ち、ポンプ用羽根車の回転軸に嵌合するボスに連なるシ
ュラウドの子午面形状を凹形の円弧状回転面とし、羽根
入口縁が取りつくボスシュラウドは回転軸にほぼ平行な
円筒状に形成し、羽根入口縁はこの入口側ボスシュラウ
ド面からなめらかに連続させ、羽根車目玉部へ大きく張
り出させ、ケーシング側の羽根入口縁は回転軸に対して
ほぼ直角に延びるようにし、円筒状のボスシュラウドに
取りつく羽根入口縁とケーシング側羽根入口縁の間を上
流側に凸形をなす円弧状のなめらかな曲線によって結ん
で羽根入口縁を形成し、この羽根の入口角はボスシュラ
ウド側入口縁ではほぼ0°に、ケーシング側入口縁では
ほぼ従来の設計で計算される角度に設定し、かつボスシ
ュラウド側とケーシング側の間の羽根入口角をなめらか
に変化させた形状の羽根入口を有し、前記羽根形状の羽
根入口から羽根出口端までなめらかな曲面で結んで形成
した羽根を有する遠心ポンプの羽根車において、そのポ
ンプ設計値であるポンプ比速度が100 〜1,000(m3/min・
m ・r.p.m)の範囲で羽根枚数を3枚とすることを特徴と
する。
In order to achieve the above object, an impeller of a centrifugal pump according to the present invention is disclosed in Japanese Patent Application No. 3-98.
The blade shape of the impeller described in No. 941 is used. That is, the meridian surface shape of the shroud connected to the rotation shaft of the pump impeller is a concave arc-shaped rotation surface, and the boss shroud attached to the blade inlet edge is formed in a cylindrical shape substantially parallel to the rotation shaft. The blade inlet edge is smoothly continuous from this inlet-side boss shroud surface, and is greatly extended to the impeller eyeball portion. The blade inlet edge that is attached to the boss shroud and the casing-side blade inlet edge are connected by an arc-shaped smooth curve that is convex toward the upstream side to form the blade inlet edge. The inlet angle of this blade is the boss shroud side inlet The edge is set to about 0 °, the casing side inlet edge is set to an angle calculated by the conventional design, and the blade inlet angle between the boss shroud side and the casing side is changed smoothly. In a centrifugal pump impeller having a blade inlet having a shape and having blades formed by connecting the blade-shaped blade inlet to the blade outlet end with a smooth curved surface, the pump specific speed, which is the pump design value, is 100 to 1,000. (m 3 / min ・
The number of blades is 3 in the range of m.rpm).

【0007】本発明の遠心ポンプの羽根車に用いられる
羽根入口角は、羽根入口径では従来設計手法を用いた羽
根入口角と同様に設定されるが、ボス径側ではほぼ0°
となるように設定されている。このような羽根入口角と
すると、従来設計理論では羽根入口のボス近辺では、羽
根への水の流入が全くできないことになり、ポンプ特性
およびキャビテーション特性の劣化を招くことになる。
しかしながら、実際は全く逆で、ボス側羽根入口縁を羽
根目玉部へ大きく張り出し、ケーシング側の入口縁は回
転軸にほぼ直角に形成して、ボス側羽根入口縁とケーシ
ング側羽根入口縁の間を上流に凸形になす円弧状のなめ
らかな曲線で形成することによって、羽根入口の流路面
積が広く確保され、ボスまたはシュラウドつけ根近傍の
流れをそぎ取るようにして効率よく羽根内へ導くことが
可能になり、羽根入口での流れが均一となり、羽根全域
(ボスからチップまで)で作用する羽根車とすることが
でき、キャビテーション特性やポンプ特性を改善するこ
とができる。この入口形状の羽根を子午面形状が凹形の
円弧状回転面をなすシュラウドと組み合わせることで、
このシュラウドによって軸方向から流入してくる水流を
なめらかに径方向へ方向変換することができ、羽根車内
損失を最小として最良のポンプ特性が得られる。以上の
ような羽根入口形状とすることにより、羽根入口通路面
積が確保され、羽根入口への均一な流入が実現できるの
で、羽根入口メリデイアン流速を従来設計のそれより増
加させることができ、以上のような羽根入口形状とする
ことによって羽根車の回転数を増加させ高速ポンプとす
ることができる。その結果、ポンプケーシングの固定側
で見た羽根車の回転時に通過する羽根数は、通例の遠心
ポンプが1,500r.p.m×5枚=7,500 枚/ 分であるが、本
発明の羽根車の回転数を8,000r.p.mとすると、8,000r.
p.m×3枚=24,000枚/ 分となり、1,500r.p.mでは16枚
の羽根枚数に相当することになり、回転数を増加させれ
ばさせるほど前述の羽根数無限大の理論に近づくことに
なり、効率が向上する。なお、後述するように、上記の
形状の羽根を有する羽根車を比速度100 〜1,000 の範囲
で羽根数を変えて実験すると、羽根枚数3枚のときに最
良の効率が得られた。
The blade inlet angle used in the impeller of the centrifugal pump of the present invention is set in the same manner as the blade inlet angle using the conventional design method in the blade inlet diameter, but is almost 0 ° on the boss diameter side.
Is set to be With such a blade inlet angle, according to the conventional design theory, in the vicinity of the boss of the blade inlet, water cannot flow into the blade at all, resulting in deterioration of pump characteristics and cavitation characteristics.
However, in fact, it is completely the opposite, the boss side blade inlet edge is greatly extended to the blade eyeball portion, the casing side inlet edge is formed substantially at right angles to the rotation axis, and the boss side blade inlet edge and the casing side blade inlet edge are formed. By forming a convex arc-shaped smooth curve upstream, a wide flow area at the blade inlet can be secured, and the flow near the boss or shroud root can be cut off and guided efficiently into the blade. It becomes possible, the flow at the blade inlet becomes uniform, and the impeller can operate in the entire blade area (from the boss to the tip), and the cavitation characteristics and the pump characteristics can be improved. By combining this inlet-shaped blade with a shroud that forms an arcuate surface of revolution with a concave meridian surface,
With this shroud, the water flow flowing in from the axial direction can be smoothly changed in the radial direction, and the loss in the impeller is minimized to obtain the best pump characteristics. With the blade inlet shape as described above, the blade inlet passage area is secured and uniform inflow to the blade inlet can be realized, so the blade inlet meridian flow velocity can be increased more than that of the conventional design. With such a blade inlet shape, the rotational speed of the impeller can be increased to provide a high-speed pump. As a result, the number of blades that the impeller rotates when viewed from the stationary side of the pump casing is 1,500 rpm × 5 sheets = 7,500 sheets / minute for a typical centrifugal pump, but the number of rotations of the impeller of the present invention is At 8,000 rpm, 8,000 r.
pm × 3 = 24,000 / min, which is equivalent to 16 blades at 1,500 rpm, and the more the rotation speed is increased, the closer to the theory of infinite number of blades. Is improved. As will be described later, when the number of blades of the impeller having the above-mentioned shape of blades was changed in the range of 100 to 1,000, the best efficiency was obtained when the number of blades was three.

【0008】また、請求項1の羽根車において、その比
速度が100 〜600(m3/min・m ・r.p.m)の範囲において、
羽根数を3枚とすると共に、羽根車外周部のこれらの3
枚の羽根の間に任意の枚数の部分羽根を設けると、後述
するように低比速度ポンプの効率を大幅に向上させるこ
とができる。
Further, in the impeller of claim 1, when the specific speed is in the range of 100 to 600 (m 3 / min · m · rpm),
The number of blades is set to 3 and these 3
If an arbitrary number of partial blades are provided between the blades, the efficiency of the low specific speed pump can be significantly improved as described later.

【0009】[0009]

【実施例】以下、本発明の遠心ポンプの羽根車を図面に
示す実施例により詳細に説明する。
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS An impeller of a centrifugal pump according to the present invention will be described in detail below with reference to embodiments shown in the drawings.

【0010】図1に本発明による羽根車を有する遠心ポ
ンプの縦断面を示す。この遠心ポンプは、ボリュートケ
ーシング11を有するポンプハウジング12を有し、こ
のポンプハウジング12はベースフレーム13に取りつ
けられている。このベースフレーム13には、回転軸1
4がベアリング15、16により回転可能に支持され、
この回転軸14の外側端部にはプーリー17が固定され
ていると共に、ポンプハウジング12のボリュートケー
シング11の中心へ突出する回転軸14の内側端部に
は、本発明による羽根車20が固定され、この羽根車に
隣接してメカニカルシール18が装着されている。ポン
プハウジング12の前端面には、羽根車20の羽根入口
21に流入する水の流れを案内するために、吸入口19
をフロントケーシング22が取りつけられている。
FIG. 1 shows a longitudinal section of a centrifugal pump having an impeller according to the present invention. This centrifugal pump has a pump housing 12 with a volute casing 11, which is mounted on a base frame 13. This base frame 13 has a rotary shaft 1
4 is rotatably supported by bearings 15 and 16,
A pulley 17 is fixed to the outer end of the rotary shaft 14, and an impeller 20 according to the present invention is fixed to the inner end of the rotary shaft 14 protruding to the center of the volute casing 11 of the pump housing 12. A mechanical seal 18 is attached adjacent to this impeller. The front end surface of the pump housing 12 has a suction port 19 for guiding the flow of water flowing into the blade inlet 21 of the impeller 20.
The front casing 22 is attached.

【0011】本発明による遠心ポンプの羽根車20の羽
根形状は、特願平3-98941 号に記載された羽根形状を用
いる。この羽根形状を図2および図3により説明する。
図4にその斜視図を示す。
As the blade shape of the impeller 20 of the centrifugal pump according to the present invention, the blade shape described in Japanese Patent Application No. 3-98941 is used. This blade shape will be described with reference to FIGS. 2 and 3.
FIG. 4 shows a perspective view thereof.

【0012】図2は回転軸方向から見た羽根車形状を表
す正面図、図3はこの羽根車の回転中心を通るメリデイ
アン断面を示す。図5、6および7は、図2の羽根車の
羽根入口から羽根出口に向かって各羽根断面形状を子午
線B、CおよびDに沿って切断した断面図である。な
お、図2の羽根のA矢印とE矢印から見た羽根の形状は
それぞれ図3のAの実線とEの実線で示されている。
FIG. 2 is a front view showing the shape of the impeller as seen from the direction of the rotation axis, and FIG. 3 is a meridian section passing through the center of rotation of this impeller. 5, 6 and 7 are cross-sectional views taken along meridians B, C and D of each blade cross-sectional shape from the blade inlet to the blade outlet of the impeller of FIG. The shapes of the blades viewed from the arrows A and E of the blades in FIG. 2 are shown by the solid lines A and E in FIG. 3, respectively.

【0013】こような形状の羽根を有する羽根車におい
て、本発明により、そのポンプ設計値であるポンプ比速
度が100 〜1,000(m3/min・m ・r.p.m)の範囲で羽根枚数
を3枚とする。これは、100 〜1,000 の比速度の範囲内
の3 種類程度の比速度で前記羽根形状の羽根車を有する
ポンプを用いて羽根枚数を2 枚から5 枚の範囲で変えて
実験を行った場合、図8のように羽根枚数3 枚のときに
最良の効率を示す特性から明らかである。
According to the present invention, in an impeller having blades of such a shape, the number of blades is 3 in the range of a pump specific speed of 100 to 1,000 (m 3 / min · m · rpm), which is a design value of the pump. And This is the case when an experiment was performed by changing the number of blades from 2 to 5 using a pump having the blade-shaped impeller at about 3 specific speeds within the range of 100 to 1,000. It is clear from the characteristic that the best efficiency is obtained when the number of blades is 3, as shown in FIG.

【0014】次に、前述した形状の3枚の羽根を有する
遠心ポンプ羽根車において、その比速度が100 〜600(m3
/min・m ・r.p.m)の低比速度の範囲で、図9に示すよう
に本発明により羽根外周部に3枚の羽根125 の間に任意
の数の部分羽根131 を設けることができる。前の実施例
と同様な部品には100 をプラスした参照数字を付けてあ
る。
Next, in the centrifugal pump impeller having three blades of the above-mentioned shape, the specific speed thereof is 100 to 600 (m 3
In the range of low specific speed (/ min · m · rpm), as shown in FIG. 9, according to the present invention, an arbitrary number of partial blades 131 can be provided between the three blades 125 on the outer peripheral portion of the blade. Parts similar to the previous embodiment are provided with a reference numeral plus 100.

【0015】図9は回転軸方向から見た羽根形状を表す
正面図、図10はこの羽根車の回転中心を通るメリデイ
アン断面を示す。図11〜図15は、図8の羽根車の羽
根入口から羽根出口に向かって3枚羽根と部分羽根の断
面形状をそれぞれ子午線F、B、G、C、Dに沿って切
断した断面図である。
FIG. 9 is a front view showing the blade shape as seen from the direction of the rotation axis, and FIG. 10 shows a Meridian section passing through the center of rotation of this impeller. 11 to 15 are cross-sectional views obtained by cutting the cross-sectional shapes of the three blades and the partial blade from the blade inlet to the blade outlet of the impeller of FIG. 8 along meridians F, B, G, C, and D, respectively. is there.

【0016】部分羽根131 の羽根形状も3枚羽根125 の
羽根形状と同様に形成されているので、詳細な説明は省
略する。
Since the blade shape of the partial blade 131 is also the same as the blade shape of the three-blade 125, detailed description thereof will be omitted.

【0017】一般に比速度の小さい羽根車の場合、羽根
数が3枚では少なすぎて揚程が得られないが、本発明の
ようにこの入口羽根形状と羽根外周部に設けた部分羽根
131とを組み合わせて高速化することにより羽根数無限
大に近づき、図16に示すように実線の曲線から点線の
曲線に顕著に揚程を向上させることができ、高揚程が得
られ、これによって低比速度ポンプの効率を大幅に向上
させることができる。
Generally, in the case of an impeller having a small specific speed, if the number of blades is 3 it is too small to obtain a lift, but as in the present invention, the shape of the inlet blade and the partial blade provided on the outer peripheral portion of the blade
By combining with 131 to increase the speed, the number of blades approaches infinity, and as shown in FIG. 16, the head can be significantly improved from the solid curve to the dotted curve, and a high head can be obtained. The efficiency of the specific speed pump can be greatly improved.

【0018】[0018]

【発明の効果】以上説明したように、本発明では、前述
した形状の羽根を有する羽根車において、そのポンプ設
計値であるポンプ比速度100 〜1,000 の範囲で羽根枚数
を3枚とすることにより、最良の効率が得られる。
As described above, according to the present invention, in the impeller having the above-mentioned blades, the number of blades is set to 3 within the range of the pump specific speed of 100 to 1,000 which is the pump design value. , The best efficiency is obtained.

【0019】また、前記羽根車において、その比速度が
100 〜600 程度の低い範囲で3枚の羽根の間の羽根車外
周部に任意の枚数の部分羽根を設けることにより高い揚
程が得られ、その結果低比速度ポンプの効率を大幅に向
上させることができる。
In the impeller, the specific speed is
A high lift can be obtained by providing an arbitrary number of partial blades on the outer peripheral part of the impeller between the three blades in the low range of 100 to 600, and as a result, the efficiency of the low specific speed pump can be greatly improved. You can

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

【図1】本発明による羽根車を有する遠心ポンプの縦断
面図である。
FIG. 1 is a vertical sectional view of a centrifugal pump having an impeller according to the present invention.

【図2】図1に組み込まれた本発明の3枚羽根の羽根車
の一実施例の正面図である。
FIG. 2 is a front view of an embodiment of the three-blade impeller of the present invention incorporated into FIG.

【図3】図2の羽根車の中心軸線を通る縦断面図であ
る。
FIG. 3 is a vertical cross-sectional view taken along the central axis of the impeller of FIG.

【図4】図2と3の羽根車の斜視図である。4 is a perspective view of the impeller of FIGS. 2 and 3. FIG.

【図5】図2の羽根を線Bに沿って切断したメリデイア
ン断面である。
5 is a Meridian cross section of the blade of FIG. 2 taken along line B. FIG.

【図6】図2の羽根を線Cに沿って切断したメリデイア
ン断面である。
6 is a Meridian cross section of the vane of FIG. 2 taken along line C. FIG.

【図7】図2の羽根を線Dに沿って切断したメリデイア
ン断面である。
7 is a Meridian cross section of the vane of FIG. 2 taken along line D. FIG.

【図8】羽根車の羽根数を変えて実験した結果をポンプ
効率について示すグラフである。
FIG. 8 is a graph showing a result of an experiment in which the number of blades of the impeller is changed and the pump efficiency is shown.

【図9】本発明による部分羽根を有する3枚羽根の羽根
車の正面図である。
FIG. 9 is a front view of a three-bladed impeller having partial blades according to the present invention.

【図10】図9の羽根車の中心軸線を通る縦断面図であ
る。
FIG. 10 is a vertical cross-sectional view taken along the central axis of the impeller of FIG.

【図11】図9の羽根を線Fに沿って切断したメリデイ
アン断面である。
11 is a Meridian cross section of the vane of FIG. 9 taken along line F. FIG.

【図12】図9の羽根を線Bに沿って切断したメリデイ
アン断面である。
12 is a Meridian cross section of the vane of FIG. 9 taken along line B. FIG.

【図13】図9の羽根を線Gに沿って切断したメリデイ
アン断面である。
13 is a Meridian section taken along line G of the vane of FIG.

【図14】図9の羽根を線Cに沿って切断したメリデイ
アン断面である。
14 is a Meridian cross section of the vane of FIG. 9 taken along line C. FIG.

【図15】図9の羽根を線Dに沿って切断したメリデイ
アン断面である。
FIG. 15 is a Meridian cross section of the blade of FIG. 9 taken along line D.

【図16】本発明の3枚羽根の羽根車と部分羽根を有す
る3枚羽根の羽根車とを比較実験した結果を示すグラフ
である。
FIG. 16 is a graph showing the results of a comparative experiment of a three-blade impeller of the present invention and a three-blade impeller having partial blades.

【符号の説明】[Explanation of symbols]

14 回転軸 20,120 羽根車 24,124 シュラウド 24a,124a ボスシュラウド 26,126 羽根入口縁 26a,126a ボスシュラウド側羽根入口縁 26b,126b ケーシング側羽根入口縁 27,127 羽根出口 131 部分羽根 14 rotating shaft 20,120 impeller 24,124 shroud 24a, 124a boss shroud 26,126 blade inlet edge 26a, 126a boss shroud side blade inlet edge 26b, 126b casing side blade inlet edge 27, 127 blade outlet 131 partial blade

Claims (2)

【特許請求の範囲】[Claims] 【請求項1】 ポンプ用羽根車の回転軸に嵌合するボス
に連なるシュラウドの子午面形状を凹形の円弧状回転面
とし、羽根入口縁が取りつくボスシュラウドは回転軸に
ほぼ平行な円筒状に形成し、羽根入口縁はこの入口側ボ
スシュラウド面からなめらかに連続させ、羽根目玉部へ
大きく張り出させ、ケーシング側の羽根入口縁は回転軸
に対してほぼ直角に延びるようにし、円筒状のボスシュ
ラウドに取りつく羽根入口縁とケーシング側羽根入口縁
の間を上流側に凸形をなす円弧状のなめらかな曲線によ
って結んで羽根入口縁を形成し、この羽根の入口角はボ
スシュラウド側入口縁ではほぼ0°に、ケーシング側入
口縁ではほぼ従来の設計で計算される角度に設定し、か
つボスシュラウド側とケーシング側の間の羽根入口角を
なめらかに変化させた形状の羽根入口を有し、前記羽根
形状の羽根入口から羽根出口端までなめらかな曲面で結
んで形成した羽根を有する遠心ポンプの羽根車におい
て、そのポンプ設計値であるポンプ比速度が100 〜1,00
0(m3/min・m・r.p.m)の範囲で羽根枚数を3枚としたこ
とを特徴とする遠心ポンプの羽根車。
1. A boss shroud to which a blade inlet edge is attached is a cylinder substantially parallel to a rotation axis, wherein a meridian surface shape of a shroud connected to a boss fitted to a rotation axis of a pump impeller has a concave arc-shaped rotation surface. The blade inlet edge is made smooth and continuous from this inlet side boss shroud surface, and it is extended to the blade eyeball portion so that the casing side blade inlet edge extends almost at right angles to the rotation axis. -Shaped boss shroud The blade inlet edge and the casing-side blade inlet edge are connected by an arc-shaped smooth curve that is convex toward the upstream side to form the blade inlet edge, and the inlet angle of this blade is the boss shroud. The side inlet edge is set to almost 0 °, the casing side inlet edge is set to an angle calculated by the conventional design, and the blade inlet angle between the boss shroud side and the casing side is smoothly changed. In a centrifugal pump impeller having a blade inlet having a shape, and having blades formed by connecting the blade-shaped blade inlet to the blade outlet end with a smooth curved surface, the pump specific speed which is the pump design value is 100 to 1 , 00
An impeller for a centrifugal pump, characterized in that the number of blades is three in the range of 0 (m 3 / min ・ m ・ rpm).
【請求項2】 請求項1の羽根車において、その比速度
が100 〜600(m3/min・m ・r.p.m)の範囲において、羽根
数を3枚とすると共に、羽根車外周部のこれらの3枚の
羽根の間に任意の枚数の部分羽根を設けたことを特徴と
する遠心ポンプの羽根車。
2. The impeller according to claim 1, wherein the specific speed is within a range of 100 to 600 (m 3 / min · m · rpm), the number of blades is three, and the peripheral portion of the impeller is An impeller of a centrifugal pump, characterized in that an arbitrary number of partial blades are provided between three blades.
JP00801292A 1992-01-21 1992-01-21 Centrifugal pump impeller Expired - Lifetime JP3276011B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP00801292A JP3276011B2 (en) 1992-01-21 1992-01-21 Centrifugal pump impeller

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP00801292A JP3276011B2 (en) 1992-01-21 1992-01-21 Centrifugal pump impeller

Publications (2)

Publication Number Publication Date
JPH05195989A true JPH05195989A (en) 1993-08-06
JP3276011B2 JP3276011B2 (en) 2002-04-22

Family

ID=11681439

Family Applications (1)

Application Number Title Priority Date Filing Date
JP00801292A Expired - Lifetime JP3276011B2 (en) 1992-01-21 1992-01-21 Centrifugal pump impeller

Country Status (1)

Country Link
JP (1) JP3276011B2 (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102588332A (en) * 2012-03-08 2012-07-18 江苏大学 Centrifugal impeller designing method of nuclear main pump
CN102979759A (en) * 2012-12-11 2013-03-20 江苏大学 Design method for impeller of multiphase mixed transportation pump
CN103047173A (en) * 2011-10-12 2013-04-17 中国石油化工股份有限公司 Method for obtaining high-efficiency low-noise impeller of centrifugal pump volute
CN103115019A (en) * 2013-03-07 2013-05-22 江苏大学 Hydraulic design method of total external characteristics of nuclear main pump
US9145894B2 (en) 2011-09-15 2015-09-29 Mitsubishi Heavy Industries, Ltd. Magnetic coupling pump and pump unit comprising the same

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9145894B2 (en) 2011-09-15 2015-09-29 Mitsubishi Heavy Industries, Ltd. Magnetic coupling pump and pump unit comprising the same
CN103047173A (en) * 2011-10-12 2013-04-17 中国石油化工股份有限公司 Method for obtaining high-efficiency low-noise impeller of centrifugal pump volute
CN102588332A (en) * 2012-03-08 2012-07-18 江苏大学 Centrifugal impeller designing method of nuclear main pump
CN102979759A (en) * 2012-12-11 2013-03-20 江苏大学 Design method for impeller of multiphase mixed transportation pump
CN103115019A (en) * 2013-03-07 2013-05-22 江苏大学 Hydraulic design method of total external characteristics of nuclear main pump

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