JPS6045796A - High-speed pump - Google Patents

High-speed pump

Info

Publication number
JPS6045796A
JPS6045796A JP15383083A JP15383083A JPS6045796A JP S6045796 A JPS6045796 A JP S6045796A JP 15383083 A JP15383083 A JP 15383083A JP 15383083 A JP15383083 A JP 15383083A JP S6045796 A JPS6045796 A JP S6045796A
Authority
JP
Japan
Prior art keywords
pressure
blade
rotary
impeller
liquid
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
JP15383083A
Other languages
Japanese (ja)
Other versions
JPS641679B2 (en
Inventor
Toshio Aono
青野 俊男
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to JP15383083A priority Critical patent/JPS6045796A/en
Publication of JPS6045796A publication Critical patent/JPS6045796A/en
Publication of JPS641679B2 publication Critical patent/JPS641679B2/ja
Granted legal-status Critical Current

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Abstract

PURPOSE:To secure such a high-speed pump as being excellent in high lift and large flow, by installing a proper number of flow holes piercing the surface of a moving blade through the opposite back surface, while making a part of pressure fluid conductible from the moving blade to the opposite back part. CONSTITUTION:At the central part of each moving blade 3 combined with a duct type casing 1, each of moving blades 3 is attached to the surface of an impeller plate 2 provided with a boss 5 in order to be secured tight to a rotary main shaft. Each of these moving blades 3 is made up into bulgingly bent form in its front part in relation to a rotation direction of the impeller plate 2, while troughlike groove parts 7 are made up along the center line of its curved surface, and at each bulgingly bent surface of these moving blades 3 and the side wall of each groove part 7 or the bottom plate, there are provided with many flow holes having a spanning diameter being almost equal to thickness of each moving blade 3 in place each.

Description

【発明の詳細な説明】 利用分野: 本発明は、ポンプ内部の羽根の前後面間に生起する圧着
を抑止することによシ、回転羽根を高速で回転できるよ
うにし、その結果全体形状を小型となし得で使用時の汎
用性を向上させると共に駆動動力も軽少とすることがで
きる高速ポンプに係るものである。
[Detailed Description of the Invention] Field of Application: The present invention enables the rotary vanes to rotate at high speed by suppressing the crimping that occurs between the front and rear surfaces of the vanes inside the pump, and as a result, the overall shape can be reduced. The present invention relates to a high-speed pump that can be made more versatile, has improved versatility in use, and requires less driving power.

従来技術: ポンプには大別して往復式ポンプ、遠心式ポンプ、回転
式ポンプ又は特殊ポンプがあって、種種の用途ycよシ
適合した特性のものを充当しそれぞれに実効を奏してい
ることは周知のとおりである。特に遠心式ポンプは最も
汎用性の高いもので、渦巻ポンプ、タービンポンプ等の
遠心ポンプは水の遠心力を利用して、又軸流ポンプはグ
ロベラの翼揚力を利用して液体に圧力を付勢し或いは所
要の位置に送るようにされている。ポンプの回転速度は
、揚程と流量とのいずれを支配的要件に選ぶかにより最
適の比速度として策定されている。しかし、遠心式又は
回転式のポンプでは、羽根車の回転速度が過大となれば
羽根車の前面及び背面で圧着を生じ、圧力の低い部分で
は液が一部分蒸発して気泡を発生し、このときの液中の
含有空気量により気泡の発生圧力は異るが、それらの気
泡は圧力低下部分をすぎると気泡中の液の蒸気が凝縮し
て液に復し気泡は消滅するに至り、この消滅時の急激な
体積変化による衝撃で羽根面は強大な打撃を受けてその
面を壊食させる、いわゆるキャビテーションを惹起する
に至る。
Prior art: Pumps can be broadly classified into reciprocating pumps, centrifugal pumps, rotary pumps, and special pumps, and it is well known that each type of pump has characteristics that are suitable for various uses and are effective. It is as follows. In particular, centrifugal pumps are the most versatile. Centrifugal pumps such as volute pumps and turbine pumps use the centrifugal force of water, while axial flow pumps use the lift of the blades of the globebeller to apply pressure to liquids. It is designed to force or send it to a required position. The rotational speed of the pump is determined as the optimum specific speed depending on which of the head and flow rate is selected as the dominant requirement. However, in centrifugal or rotary pumps, if the rotational speed of the impeller is too high, crimping occurs on the front and back surfaces of the impeller, and in areas of low pressure, part of the liquid evaporates, creating bubbles. The pressure at which bubbles are generated differs depending on the amount of air contained in the liquid, but when these bubbles pass through a pressure drop area, the vapor of the liquid in the bubbles condenses and returns to liquid, causing the bubbles to disappear. The blade surface is subjected to a powerful blow due to the impact caused by the sudden change in volume over time, leading to erosion of the surface, causing so-called cavitation.

従って、ポンプの回転速度は、在来の羽根車と同じ構造
を採用する限シは効率又は耐用性の面よシ一定の限度が
避けられず、高揚程又は大流量を得ようとすれば羽根車
を多段とする等、複雑なものとならざるを得々かったの
である。
Therefore, the rotational speed of the pump must have a certain limit in terms of efficiency or durability unless it adopts the same structure as a conventional impeller. It was inevitable that the system would be complicated, such as using multiple stages of cars.

発明の目的: 本発明は斯かる現況に鑑がみ、羽根車の回転速度決定の
制約を解消することにより羽根車の高速回転を可能とし
、ポンプを小型化するにも拘らず高揚程又は大流量を容
易に得られるようにした高速ポンプを提案せ、んとして
なされたもので、回転羽根の要部に流通孔を穿設して圧
液の導通を可能とし、羽根車の高速回転に際しても上記
流通孔よシ回転羽根向背部に液体を導通させて核部にお
いて負圧を生ぜしめず、気泡発生とそれによる渦流成分
をなくしてキャビテーションの生起を皆無とし、羽根車
に高速回転を付与することによシ発生する大きな遠心力
を活用して高揚程又は大流量を得ることができる高速ポ
ンプの提供を目的としている。
Purpose of the invention: In view of the current situation, the present invention makes it possible to rotate the impeller at high speed by eliminating the restrictions on determining the rotation speed of the impeller. The idea was to propose a high-speed pump that could easily obtain a flow rate, and it was created with a flow hole in the main part of the rotating blade to allow pressure fluid to flow through it, even when the impeller rotates at high speed. Liquid is conducted through the above-mentioned circulation hole to the back and forth parts of the rotating blade, so that negative pressure is not generated in the core part, bubble generation and the resulting vortex component are eliminated, cavitation is completely eliminated, and high-speed rotation is imparted to the impeller. The object of the present invention is to provide a high-speed pump that can obtain a high head or a large flow rate by utilizing the large centrifugal force that is generated.

発明の構成及び実施例: 以下、本発明の1実施例を図面に基づき説明する。Structure and embodiments of the invention: Hereinafter, one embodiment of the present invention will be described based on the drawings.

第1図に示されるポンプの回転羽根及び第5図、第7図
、第14図に例示される渦室型のケーシングと組合わさ
れる各回転羽機成いは第10図に示すようにダクト型の
ケーシングと組合わされる回転羽根において、たとえば
第1図にみるごとく、中心部には回転主軸に固着するだ
めのボス(5)を設けた羽根車盤(2)の表面に回転羽
根(3)を取付ける。この回転羽根(3)は羽根車盤(
1)の回転方向に関して前面部が膨出彎曲した形状で、
その膨出彎曲面の中央線浴いには第2図又は第3図に示
すように樋状の溝部(7)をつくシだし、回転羽根(3
ンの膨出彎曲面及び溝部(7)側壁若しくは底板には、
回転羽根(3)の厚さと略略同じ程度の差渡し径を有す
る多数の流通孔(6)を適所に穿設するのである。
Each rotating impeller unit is combined with the rotary vane of the pump shown in FIG. 1 and the vortex chamber type casing illustrated in FIGS. 5, 7, and 14, and the duct as shown in FIG. 10. For example, as shown in Fig. 1, in the rotary blade that is combined with the casing of the mold, the rotary blade (3) is mounted on the surface of the impeller disk (2), which has a boss (5) in the center that is fixed to the rotating main shaft. ). This rotating blade (3) is connected to an impeller disk (
1) The front part has a bulging and curved shape with respect to the rotation direction,
As shown in Fig. 2 or 3, a gutter-like groove (7) is formed in the center line bath of the bulging curved surface, and a rotary blade (3) is provided.
The bulging curved surface and groove part (7) side wall or bottom plate of the
A large number of communication holes (6) having a diameter across the width approximately the same as the thickness of the rotary blade (3) are bored at appropriate locations.

すなわち、台座を有するケーシング(1)の腹板部又は
ダクト端寄シを吸込口(3)とする、ケーシング(1)
で形成される圧液室中において、プーリ等の伝導部を介
して外部動力によシ又は直接駆動によシ高速回転を可能
とした羽根車盤(2)又はボス(5)に直接固着した回
転羽根(3)には上記のごとく流通孔(6)を穿設し、
回転羽根の表面より向背面へ圧液を導通せしめるから、
回転羽根の回転方向(へ)の向背部で負圧となり渦流を
生じてキャビテーションを発生するような現象が防止で
きる。
In other words, the casing (1) has a pedestal, and the abdominal plate or the duct end is the suction port (3).
The impeller disk (2) or boss (5) is directly fixed to the impeller disk (2) or boss (5), which enables high-speed rotation by external power or direct drive through a transmission part such as a pulley in a pressure liquid chamber formed by a The rotating blade (3) is provided with a circulation hole (6) as described above,
Because the pressure liquid is conducted from the surface of the rotating blade to the opposite surface,
It is possible to prevent phenomena such as cavitation caused by negative pressure at the opposite and rear sides of the rotary vane in the direction of rotation (inward), creating eddy currents.

回転羽根(3)の形状としては、第1図に示すような羽
根車盤(2)の片側面にのみ回転羽根(3)を固着した
ものの他に、次に挙げる多様な各種実施例のものとする
ことができる。
In addition to the shape of the rotating blade (3) shown in Fig. 1, in which the rotating blade (3) is fixed only to one side of the impeller disk (2), there are various shapes as shown below. It can be done.

第5図に示すものは羽根車盤(2)の両面に、多数の流
通孔(6)を穿設した回転羽根(3)及び(3)′を固
着したもので、この実施例ではさらに、羽根車盤(2)
にも整流孔<6Yを穿設する。これらの整流孔(6Yは
回転羽根(3)の回転方向に)の直ぐ後位に配すること
が好ましく、第6図に示すように、ケーシング内圧液室
中において羽根車盤(2)の両側の圧液が導通自在とな
るので、回転羽根(3)及び<3Yの流通孔(6)を通
過する圧液の他、羽根車盤(2)の他面側よシも圧液が
もたらされることになり、回転羽根(3)及び(3γの
向背部分での液圧低下をより効果的に防止でき、回転羽
根の高速回転による大きな遠心力の発現中にも回転羽根
の表面及び向背面での圧着の解消に貢献する。
The one shown in FIG. 5 has rotating blades (3) and (3)', each having a large number of flow holes (6), fixed to both sides of an impeller disk (2). Impeller board (2)
Also drill a rectifying hole <6Y. It is preferable to arrange these flow straightening holes (6Y in the direction of rotation of the rotary vane (3)) directly behind, and as shown in FIG. Since the pressure liquid can be freely conducted, in addition to the pressure liquid passing through the rotating blade (3) and the <3Y communication hole (6), pressure liquid is also brought to the other side of the impeller disk (2). As a result, it is possible to more effectively prevent a drop in fluid pressure on the opposite side of the rotary blade (3) and (3γ), and even when a large centrifugal force is generated due to high-speed rotation of the rotary blade, it is possible to prevent the liquid pressure from decreasing on the surface and opposite side of the rotary blade. Contributes to eliminating crimping.

第7図又は第8図に示すものは、回転羽根(3)の中心
寄り端部がボス(5)に達して連結しており、第1図又
は第5図に示す実施例とは異って、回転羽根とボスとの
間隙より圧液が回転羽根向背面へ回流することができな
い。従って、回転羽根の表面と向背面との圧着を最小と
すべく、回転羽根(3)に穿設する流通孔(6)の数は
上記実施例のものに較べて多くし、有効流通面積が全体
としてほぼ同様となるように設定され、圧着の発生を抑
止する構成となっている。なお、このような実施例では
、流通孔を穿設した回転羽根とはなさずに第9図に示す
ように、細孔を多数穿孔した、たとえばパンチプレート
状の回転羽根となすこともでき、回転羽根の表裏の圧着
を生ぜしめずに大きな遠心力に基づく圧液を生起させる
のに効果的なものである。
The embodiment shown in FIG. 7 or 8 is different from the embodiment shown in FIG. 1 or 5 in that the end of the rotating blade (3) near the center reaches and connects to the boss (5). Therefore, the pressure liquid cannot circulate to the back surface of the rotary vane through the gap between the rotary vane and the boss. Therefore, in order to minimize the pressure bond between the surface of the rotary blade and the opposite surface, the number of flow holes (6) formed in the rotary blade (3) is increased compared to those in the above embodiment, and the effective flow area is increased. They are set to be almost the same as a whole, and are configured to suppress the occurrence of crimping. In addition, in such an embodiment, as shown in FIG. 9, instead of using a rotary blade with circulation holes, it is also possible to use a rotary blade in the form of a punch plate, for example, with a large number of pores perforated, as shown in FIG. This is effective in generating pressurized liquid based on large centrifugal force without causing pressure contact between the front and back surfaces of the blades.

第10〜12図に示すものは軸流ポンプに用いるプロペ
ラ型の回転羽根(3)であシ、放射状方向の断面を示す
第11図にみるごとく、ボス(5)と同心円状の溝部(
7)を有しこの溝部(7)の両側に流通孔(6)を配設
したものである。この実施例にみる流通孔(6)は第1
2図に示すようにプロペラ型の回転羽根(3)の回転方
向(へ)と逆向勾配に穿設することにょシ、ポリニート
ポンプ又はタービンポンプよシも回転数の大きい軸流ポ
ンプでの圧液に掛る慣性に拮抗して、回転羽根表面よシ
向背面への圧液の導通量を適値に保ち、回転羽根の表表
での圧迫のバランスをとり易くしておシ、キャビテーシ
ョンの発生防止に有効な手段である。
The one shown in Figures 10 to 12 is a propeller-type rotary vane (3) used in an axial flow pump, and as shown in Figure 11, which shows a radial cross section, it has a boss (5) and a concentric groove (3).
7), and communication holes (6) are arranged on both sides of this groove (7). The flow hole (6) seen in this example is the first
As shown in Figure 2, it is necessary to drill holes at a slope opposite to the direction of rotation of the propeller-type rotary blade (3). It counteracts the inertia applied to the liquid and maintains an appropriate amount of pressure liquid conduction from the surface of the rotating blade to the back side, making it easier to balance the pressure on the front side of the rotating blade and preventing the occurrence of cavitation. It is an effective means of prevention.

第13図に示すものは、密閉型の回転羽根としたもので
、羽根車部分には第4図に示すのと同様な溝部(7)を
形成すると共に、第10図に例示した溝部付きのプロペ
ラ型回転羽根を組合わせコンビネーションとしたもので
ある。この態様のものは遠心ポンプと軸流ポンプとの特
色を併せ有し、特に回転数の広い範囲にわたってすぐれ
た効率が得られ、適応性が大きい点で有利なものである
The one shown in Fig. 13 is a closed type rotary impeller, and the impeller part has a groove (7) similar to that shown in Fig. 4, and a grooved part (7) as shown in Fig. 10. It is a combination of propeller-type rotating blades. This embodiment has both the characteristics of a centrifugal pump and an axial flow pump, and is particularly advantageous in that excellent efficiency can be obtained over a wide range of rotational speeds, and that it is highly adaptable.

第14〜16図に示すものは、本発明の高速回転を可能
と−した回転羽根を有する高圧ポンプの実施例である。
What is shown in FIGS. 14 to 16 is an embodiment of a high-pressure pump having rotary vanes capable of high-speed rotation according to the present invention.

この実施例のものは第14図に示すように、羽根車盤(
2)に取付く回転羽根は、流通孔(6)を穿設した大き
な回転羽根(3)とボス(5)の近くに配設された小さ
な回転羽根(3′fとよシなっている。大きな回転羽根
(3)は加圧羽根で小さな回転羽根(3)′は吸込専用
羽根であり、吸込口(8)より液体を強力に吸引し且つ
強大な遠心力を与え圧液を生起させる。
As shown in Fig. 14, this embodiment has an impeller disc (
The rotary vanes attached to 2) are a large rotary vane (3) with a communication hole (6) and a small rotary vane (3'f) disposed near the boss (5). The large rotary vane (3) is a pressurizing vane, and the small rotary vane (3)' is a suction-only vane, which strongly sucks liquid from the suction port (8) and applies a strong centrifugal force to generate pressurized liquid.

ついで羽根車室で生起した圧液は、羽根車室を包囲して
穿設された圧液孔(6)αυを通じて圧液環室四を満た
し、吐出口(9)より外部へ圧送される。この態様のも
のは回転羽根の高速回転と共に圧液環基αQの圧液は各
部分で均斉した高圧となり、脈流を生ずることなく定常
圧液を得られるので揚液のみならず種種の目的に至便で
ある。
Then, the pressurized liquid generated in the impeller chamber fills the pressurized liquid ring chamber 4 through the pressurized liquid hole (6) αυ bored surrounding the impeller chamber, and is forced to the outside through the discharge port (9). In this embodiment, as the rotary blade rotates at high speed, the pressure liquid of the pressure liquid ring group αQ becomes high pressure uniformly in each part, and steady pressure liquid can be obtained without causing pulsation, so it is suitable not only for pumping liquid but also for various purposes. It's very convenient.

また、本発明では在来の各種ポンプに対比して格段に大
きな回転速度で運転できるものであるから回転羽根の枚
数は上記の各実施例にみるように比較的少ないが、第1
7図に示すような通常のポリニートポンプでも回転羽根
(3)に流通孔(6) (6)を穿設することによシ、
又、第18図に示すようなタービンポンプでは回転羽根
(3)に流通孔(6) (6)を穿設すると共に案内羽
根(4)にも流通孔(6) (6)を穿設することによ
シ、キャビテーションを発生させずに回転羽根を高速回
転となし得るから、在来の普通の回転羽根を備えたポン
プに対比して小型化することができるのみならず、高揚
程又は大流量を容易に得ることができるのである。
In addition, since the present invention can operate at a much higher rotational speed than various conventional pumps, the number of rotating blades is relatively small as seen in each of the above embodiments.
Even with a normal polyneat pump as shown in Figure 7, it is possible to
In addition, in a turbine pump as shown in Fig. 18, the rotary vane (3) is provided with circulation holes (6) (6), and the guide vane (4) is also provided with communication holes (6) (6). In particular, since the rotary vanes can be rotated at high speed without causing cavitation, not only can the pumps be made smaller compared to conventional ordinary rotary vanes, but also pumps with high head or large The flow rate can be easily obtained.

発明の効果: 回転羽根(3)をこのような淘成とした本発明の高速ポ
ンプにあっては、吸込口(8)より吸込まれてケーシン
グ(1)を満たした液体は次のように圧力が平衝した挙
動を示す。すなわち、回転羽根(3)の高速回転により
液体は随伴して遠心力を生じ、同時に多数の流通孔(6
)を通過して回転羽根(3)の向背部に達し、回転羽根
(3)の各間隔部に均斉圧をもって充満しつつ各回転羽
根の先端へと移動する。
Effects of the invention: In the high-speed pump of the present invention in which the rotary vane (3) is configured as described above, the liquid sucked through the suction port (8) and filling the casing (1) has a pressure as follows. shows balanced behavior. That is, due to the high-speed rotation of the rotary blade (3), the liquid is entrained and generates centrifugal force, and at the same time a large number of flow holes (6) are generated.
), and reaches the opposite and rear parts of the rotary blade (3), and moves to the tip of each rotary blade while filling each interval of the rotary blade (3) with uniform pressure.

従って本発明の高圧ポンプでは回転羽根の向背部に負圧
を生ずることは絶無で、回転羽根の表面部及び向背面部
共に圧力は平準化されて渦流成分はなくなシ、キャビテ
ーションは発生しないのである。その結果、液は回転羽
根の分布域外へ順層流となって移動し圧液となって吐出
口から外部へと送シ出され、その圧液押出量に見合うだ
け吸引力が生じ中心部では連続的な液の吸込が行なわれ
る。
Therefore, in the high-pressure pump of the present invention, negative pressure is never generated on the opposite sides of the rotary vane, and the pressure is leveled on both the front and rear sides of the rotary vane, there is no vortex component, and cavitation does not occur. be. As a result, the liquid moves out of the distribution area of the rotary vanes as a normal laminar flow, becomes a pressure liquid, and is sent out from the discharge port to the outside.A suction force corresponding to the amount of pressure liquid pushed out is generated at the center. Continuous suction of liquid takes place.

そして、回転羽根の回転数が高くなればなる程、ケーシ
ング内の王水室での圧液は増圧されたものとなり、吸込
口よシ吸引される液量も増加し、しかもこれらの現象が
脈動することなく連続状態で継続されるのである。
As the rotational speed of the rotary blade increases, the pressure of the liquid in the aqua regia chamber inside the casing increases, and the amount of liquid sucked into the suction port also increases. It continues in a continuous state without pulsating.

なお、回転羽根と流通孔との関連は、回転羽根が第5図
、第7図又は第14図に示すような彎曲板状のものであ
るときには、高速回転時における単位流通孔を導通する
液量は小となり易く、回転羽根の表面部と向背面部との
圧迫を円滑に解消し難くなる懸念があるので、このよう
なときには流通孔の数を多くシ、孔の配置に適当個所を
選択し圧液の全導通液量を大とすることによシ目的を達
することかできる。また、第1図、第3図、第4図又は
$13図に示すごとき回転羽根の表面がチャンネル又は
V形溝となる溝部を有するものとすれば、圧液は溝部に
よって回転羽根によく随伴肱特に溝底部又は溝、側壁部
に穿設した流通孔より回転羽根の向背部へ圧液は導通し
易く、回転羽根の表裏における圧迫を効果的に解消せし
めることができるのである。
Note that the relationship between the rotating blades and the flow holes is such that when the rotating blades are curved plate-shaped as shown in FIG. 5, FIG. 7, or FIG. The amount tends to be small, and there is a concern that it will be difficult to smoothly relieve the pressure between the surface part of the rotating blade and the opposite back part. This objective can be achieved by increasing the total amount of pressure fluid that is passed through. In addition, if the surface of the rotating blade has a groove that becomes a channel or V-shaped groove as shown in Figures 1, 3, 4, or $13, the pressure liquid will be well accompanied by the rotating blade due to the groove. In particular, the pressure liquid can be easily conducted to the opposite side of the rotary blade from the flow hole formed in the groove bottom, groove, or side wall, and the pressure on the front and back sides of the rotary blade can be effectively relieved.

本発明は、回転羽根の回転方向前面ど向背面との圧迫を
なくして、キャビテーションを発生することなく羽根車
を高速回転となすこと赤でき、小型でありながら高揚程
、大流量を得ることができるものであシ、本発明の趣旨
に従うものであればその技術的思想は上記した種種の実
施例に限定されることはなく、それらから導かれる変形
又は応用はすべて本発明の技術的範囲に包含されるもの
であることはいうまでもない。
The present invention enables the impeller to rotate at high speed without causing cavitation by eliminating pressure between the front and rear surfaces of the rotary blade in the rotational direction, and it is possible to obtain high head and large flow rate despite being small. However, as long as it is possible and complies with the spirit of the present invention, the technical idea is not limited to the various embodiments described above, and any modifications or applications derived therefrom are within the technical scope of the present invention. Needless to say, it is included.

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

第1図は本発明の1実施例の縦断説面図、第2図は第1
図の回転羽根部の■−■視断面断面図3図は第1図の回
転羽根の斜視図、第4図はその変形例を示す図、第5図
は他の実施例の説明図、第6図は第5図の■−■視断面
断面図7図は今1つの実施例の説明図、第8図は第7図
の■−■視断面断面図9図は第8図のものの変形例図、
第10図はプロペラ型の回転羽根の1実施例図、第11
図は第10図のXI−XI視断面図、第12図は第10
図の苅−刈面断面図、第13図はコンビネーションの回
転羽根とした1実施例図、第14〜16図は別の実施例
図で第14図は回転羽根の説明図、第15図は縦断面図
、第16図は第15図のxw −xvr視説明図、第1
7図はポリュートポンプとした説明図、第18図はター
ビンポングとした説明図である。 (1)・・・ケーシング (2)・・・羽根車盤(3)
 (37’・・)回転羽根 (4)・・・案内羽根(5
)・・・ボス (6)・・・流通孔(6γ・・・整流孔
 (7)・・・溝部(8)・・・吸込口 (9)・・・
吐出口σQ・・・圧液環基 (ロ)・・・圧液孔第1図 第2図 第3図 第118 第13図 7−。 3 第ブ2図
FIG. 1 is a vertical cross-sectional view of one embodiment of the present invention, and FIG.
3 is a perspective view of the rotating blade in FIG. 1, FIG. 4 is a view showing a modification thereof, FIG. 5 is an explanatory view of another embodiment, and FIG. Figure 6 is a cross-sectional view taken along ■--■ in Figure 5. Figure 7 is an explanatory diagram of one embodiment. Figure 8 is a cross-sectional view taken along ■--■ in Figure 7. Figure 9 is a modification of the one shown in Figure 8. Example diagram,
Figure 10 is a diagram of one embodiment of a propeller-type rotating blade, Figure 11
The figure is a sectional view taken along line XI-XI in Figure 10, and Figure 12 is a cross-sectional view of Figure 10.
Fig. 13 is a cross-sectional view of the cutting surface, Fig. 13 is an example of a combination rotary blade, Figs. The vertical sectional view, FIG. 16 is an xw-xvr view explanatory diagram of FIG.
FIG. 7 is an explanatory diagram of a porlute pump, and FIG. 18 is an explanatory diagram of a turbine pump. (1)...Casing (2)...Impeller board (3)
(37'...) Rotating vane (4)... Guide vane (5
)... Boss (6)... Distribution hole (6γ... Rectification hole (7)... Groove (8)... Suction port (9)...
Discharge port σQ...Pressure liquid ring group (b)...Pressure liquid hole Fig. 1 Fig. 2 Fig. 3 Fig. 118 Fig. 13 Fig. 7-. 3 Figure B2

Claims (1)

【特許請求の範囲】[Claims] 回転羽根の表面より向背面に貫通する流通孔を適当数穿
設し、該回転羽根の表面部より向背部へ圧液の一部が導
通可能とした構造の回転羽根を、吸込口及び吐出口を有
する適宜形状のケーシング内に回転可能に設けたことを
特徴とする高速ポンプ。
A rotating blade has a structure in which an appropriate number of communication holes are drilled through the rotating blade from the surface to the opposite side, and a part of the pressure liquid can be conducted from the surface to the opposite side of the blade. A high-speed pump, characterized in that it is rotatably provided within a suitably shaped casing.
JP15383083A 1983-08-22 1983-08-22 High-speed pump Granted JPS6045796A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP15383083A JPS6045796A (en) 1983-08-22 1983-08-22 High-speed pump

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP15383083A JPS6045796A (en) 1983-08-22 1983-08-22 High-speed pump

Publications (2)

Publication Number Publication Date
JPS6045796A true JPS6045796A (en) 1985-03-12
JPS641679B2 JPS641679B2 (en) 1989-01-12

Family

ID=15571018

Family Applications (1)

Application Number Title Priority Date Filing Date
JP15383083A Granted JPS6045796A (en) 1983-08-22 1983-08-22 High-speed pump

Country Status (1)

Country Link
JP (1) JPS6045796A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4720242A (en) * 1987-03-23 1988-01-19 Lowara, S.P.A. Centrifugal pump impeller
JP2005002857A (en) * 2003-06-11 2005-01-06 Tsurumi Mfg Co Ltd Impeller of submerged pump
KR20220134077A (en) * 2021-03-26 2022-10-05 주식회사 오알피이노베이션 Centrifugal pump unit

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB942648A (en) * 1961-06-27 1963-11-27 Sulzer Ag Centrifugal pumps
JPS4996302A (en) * 1972-12-06 1974-09-12
JPS59168297A (en) * 1983-03-16 1984-09-21 Hitachi Ltd Welded impeller

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB942648A (en) * 1961-06-27 1963-11-27 Sulzer Ag Centrifugal pumps
JPS4996302A (en) * 1972-12-06 1974-09-12
JPS59168297A (en) * 1983-03-16 1984-09-21 Hitachi Ltd Welded impeller

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4720242A (en) * 1987-03-23 1988-01-19 Lowara, S.P.A. Centrifugal pump impeller
JP2005002857A (en) * 2003-06-11 2005-01-06 Tsurumi Mfg Co Ltd Impeller of submerged pump
JP4539902B2 (en) * 2003-06-11 2010-09-08 株式会社鶴見製作所 Single blade impeller for submersible pump
KR20220134077A (en) * 2021-03-26 2022-10-05 주식회사 오알피이노베이션 Centrifugal pump unit

Also Published As

Publication number Publication date
JPS641679B2 (en) 1989-01-12

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