JPS6073094A - Variable vane mixed flow pump - Google Patents

Variable vane mixed flow pump

Info

Publication number
JPS6073094A
JPS6073094A JP17927483A JP17927483A JPS6073094A JP S6073094 A JPS6073094 A JP S6073094A JP 17927483 A JP17927483 A JP 17927483A JP 17927483 A JP17927483 A JP 17927483A JP S6073094 A JPS6073094 A JP S6073094A
Authority
JP
Japan
Prior art keywords
blade
vane
impeller
inlet
flow path
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
JP17927483A
Other languages
Japanese (ja)
Inventor
Masao Ooshima
大嶋 正夫
Kaoru Endo
薫 遠藤
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.)
Ebara Corp
Original Assignee
Ebara Corp
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 Ebara Corp filed Critical Ebara Corp
Priority to JP17927483A priority Critical patent/JPS6073094A/en
Publication of JPS6073094A publication Critical patent/JPS6073094A/en
Pending legal-status Critical Current

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Abstract

PURPOSE:To improve suction performance, pump efficiency while to reduce hydraulic loss by employing a rotary face having an arch the center of which is in the downstream of vane turning shaft in a face containing the rotary axis as a bus line on the surface of hab while enlarging the width of vane flow path at the vane inlet. CONSTITUTION:The surface of hab 3 is formed into a rotari face containing a conical face having an arch or similar curve the center of which is in the downstream of vane turning axis (l) in the face containing the rotary axis as the bus line. Consequently the height of vane at the inlet 4 of vane 2 is made higher than that at the outlet 5 to widen the flow path of vane 2 at the inlet. Since the flow-in speed to the impeller 1 decreases, it causes no cavitation thus to improve the suction performance while the increasing rate of flow path area from the inlet toward the outlet is reduced. Consequently, the flow in the impeller 1 will never decrease abruptly to reduce the hydraulic loss in the impeller 1 resulting in improvement of pump efficiency.

Description

【発明の詳細な説明】 面状に形成した可動羽根斜流ポンプに関する。[Detailed description of the invention] This invention relates to a planar movable blade mixed flow pump.

従来、可動羽根斜流ポンプの羽根車では、第1図に示す
ように、旋回軸線tを軸にして羽根角度を自由に変える
ことができるように、羽根λの外周面.2a及びハブ3
の表面は、回転軸m上の共通の中心Oをもつ半径几tと
Rhの球面にされてきた。
Conventionally, in the impeller of a movable blade mixed flow pump, as shown in FIG. 2a and hub 3
The surface of has been made into a spherical surface of radius t and Rh with a common center O on the axis of rotation m.

このため、羽根2の高さけ羽根入口lから羽根出口まま
で全く同一となっており、それに伴い羽根流路面積は、
回転+!]lt心に近い羽根人口弘では小さく、回転軸
心より遠い羽根出口!へ向がって著しく増大している。
Therefore, the height of the blade 2 is exactly the same from the blade inlet l to the blade outlet, and accordingly, the blade flow path area is
Rotation +! ]It is small in the blade close to the center, and the blade exit is far from the rotation axis! It is increasing significantly towards.

上記のように、羽根入口が同出口に比べて流路面積が著
しく絞られた形となるため、羽根車への流入速度が増し
、キャビテーションが生じ易くなシ、吸込性能が著しく
撰なわh.る。(7かも羽根入口から同出口へ向かつて
流路面積が著しく増大するのに伴い、羽根車内の流れが
急激に減速するので、羽根車内の水力損失が工■ρして
ポンプ効率の低下をももたらしている。その上、可動羽
根斜流羽根車では、締切IIIIII動力比を低くする
ために、ハブ比(ハブ半径/羽根外周半径)が大きくさ
れるので、前記のように羽根外周面とハブ表面が同心球
面とされていると、羽根入口よシ同出口へ向がって流路
面積の増加する割合が増し、それにつれて吸込性能が更
に悪くなる結果となる等の欠点があった。
As mentioned above, since the flow path area of the blade inlet is significantly narrowed compared to the blade outlet, the speed of flow into the impeller increases, cavitation is less likely to occur, and the suction performance is significantly reduced.h. Ru. (7) As the flow path area increases significantly from the impeller inlet to the impeller outlet, the flow inside the impeller rapidly decelerates, causing hydraulic loss inside the impeller and reducing pump efficiency. Furthermore, in movable blade mixed flow impellers, the hub ratio (hub radius/blade outer radius) is increased in order to lower the cut-off III power ratio, so as mentioned above, the blade outer circumferential surface and the hub If the surfaces were concentric spherical surfaces, there was a drawback that the rate of increase in the area of the flow path increased from the inlet to the outlet of the blade, resulting in further deterioration of suction performance.

本発明者は、先に、上記の欠点を除去するために、球面
状のハブの球面中心を、回転軸線上において球面状の羽
根外周の球面中心より流れ方向に見て後方にずらせたこ
とを特徴とする可動羽根斜流ポンプを特願昭j♂−/、
2グA77号として出願した。
In order to eliminate the above-mentioned drawbacks, the present inventor first discovered that the center of the spherical surface of the spherical hub was shifted rearward on the axis of rotation from the center of the spherical surface of the outer periphery of the spherical blade when viewed in the flow direction. Special application for a movable vane mixed flow pump featuring the following characteristics:
The application was filed as No. 2GA77.

ところで、このものにおいては、羽根車入口流路幅(入
口での羽根高さ)を広げることができるので、ポンプ効
率が高く吸込性能がよく、かつ低締切軸動力比を得るこ
とができるけれども、羽根の入口部よシ出ロ部までの流
路において、ハブ球面中心が回転軸線上に存在すること
を条件とするため、それだけハブ表面の形状が制約され
ることKなり、したがって、上記流路面積の変化の割合
を自由に設計することに制約を受ける恐れがあった。
By the way, in this case, the width of the impeller inlet flow path (the height of the blades at the inlet) can be widened, so it is possible to achieve high pump efficiency, good suction performance, and a low shut-off shaft power ratio. In the flow path from the inlet to the exit of the blade, the center of the hub's spherical surface must lie on the axis of rotation, which limits the shape of the hub surface. There was a risk that there would be restrictions on designing freely the rate of change in area.

本発明の目的は、上記従来のものの欠点を除去すること
ができ、ポンプ効率が高く、吸込性能もよく、更に締切
軸動力比が低り、シかも羽根の入口部より出口部までの
流路面積の変化の割合を比較的自由に設計できるように
した 可動羽根斜流ポンプを提供するにある。
It is an object of the present invention to eliminate the drawbacks of the conventional ones as described above, to provide high pump efficiency, good suction performance, low shut-off shaft power ratio, and a flow path from the inlet to the outlet of the impeller. To provide a movable vane mixed flow pump in which the rate of change in area can be designed relatively freely.

この目的を達成するために、本発明は、 回転軸線を含
む面内で、羽根旋回軸よ9下流側の回転a線上を除いた
区域に中心をもつ円弧又は類似の曲線を母線とする回転
面(円錐面を含む)として、ハブ面を形成したことを特
徴としている。
In order to achieve this object, the present invention provides a rotating surface whose generating line is a circular arc or similar curve having its center in the area 9 downstream of the blade rotation axis, excluding the area on the rotation a line, within a plane including the rotation axis. (including a conical surface) is characterized by forming a hub surface.

以下、本発明の実施例を図面第2図と共に説明する。Embodiments of the present invention will be described below with reference to FIG. 2.

第一図は、本発明の一実施例を示す可動羽根斜流ポンプ
の軸方向の断面図であって、羽根車/のボス3には、羽
a2が、旋回軸線lを軸にして羽根角度が自由に調節で
きるように取り付けられてお勺、その念めに羽根コの外
周面コaは、回転軸線m上の点0(旋回軸線りと回転軸
線mとの交点)を中心にし几tを半径とした球面に形成
され、同様の形状に作られたケーシング内面とは羽根の
外周面で細隙が形成されている。一方、ボス3の表面は
、 回転軸線を含む面内において羽根旋回軸tより下流
側に中心Qa をもつ円弧又は類似の曲線を−fE:線
とする回転面(円錐面を含む)として 形成されている
。
FIG. 1 is an axial cross-sectional view of a movable blade mixed flow pump showing an embodiment of the present invention, in which a boss 3 of an impeller has blades a2 at an angle of blade angle about the rotation axis l. The blade is attached so that it can be adjusted freely.In order to make sure of this, the outer circumferential surface of the blade is centered at point 0 on the rotation axis m (the intersection of the rotation axis and the rotation axis m). A spherical surface with a radius of On the other hand, the surface of the boss 3 is formed as a rotating surface (including a conical surface) whose -fE: line is a circular arc or similar curved line with the center Qa downstream of the blade rotation axis t in a plane that includes the rotational axis. ing.

したがって、羽根コの入口部での羽根高さは、回出口!
寸の羽&!筒さよシ大きく形成される。また、羽根コは
、点0を通る旋回軸線tを軸にして羽根角度が調節され
るので、羽根コの内周面(根部)と、ハブ表面3とは、
従来のもの(第1図)のように密着せず、したがって、
羽根入口ハブ端、2 bは、羽根角度を小さくした(す
なわち、羽根を回転方向に近づくようにねかぜる)とき
、ハブ表面に突き当らないように予め切欠いておく。な
おこの際、羽根出口ハブ端にはハブ表面との間に若干の
細隙が形成されるが、ポンプ性りしには殆んど影響がな
い。図中、tはポンプケーシングの入口部を形成するベ
ルマウス、7は案内ケーシング、tは吐出f、71 タ
は駆動軸、IOは往復動させて羽根角度を変更させるテ
ンションロッドヲ示ス。
Therefore, the height of the blade at the entrance of the blade is equal to the height of the blade at the exit!
Wings of size &! The tube is formed with a large parting. In addition, since the blade angle of the blade is adjusted around the rotation axis t passing through point 0, the inner circumferential surface (root) of the blade and the hub surface 3 are
It does not fit tightly like the conventional one (Fig. 1), and therefore,
The blade inlet hub end 2b is notched in advance so that it does not hit the hub surface when the blade angle is reduced (that is, the blade is rolled closer to the direction of rotation). At this time, a slight gap is formed between the hub end of the blade outlet and the hub surface, but this has almost no effect on the performance of the pump. In the figure, t is a bell mouth forming the inlet of the pump casing, 7 is a guide casing, t is a discharge f, 71 is a drive shaft, and IO is a tension rod that reciprocates to change the blade angle.

本実施例は前述のような構成になっているので、駆動軸
rの回転により羽根車/が回転すると、液ハヘルマウス
tよシ吸込まれ、羽根2によってエネルギを与えられた
抜、案内ケーシング7を通って矢印Aの方向に流れ、吐
出し管lを経て外部へ給送さ第1.る。壕だ羽根角度は
、テンションロッド10を上下往復動させることによっ
て変化さ第71、そiによってfAL量が制御されるが
、これらのことは従来のもの(Dr’J 7図)と変9
はない。
Since this embodiment has the above-mentioned configuration, when the impeller rotates due to the rotation of the drive shaft r, the liquid is sucked in through the blade 2 and the guide casing 7 is energized by the blades 2. The first . Ru. The groove blade angle is changed by reciprocating the tension rod 10 up and down.
There isn't.

しかしながら従来のものと異な9本発明では、回転軸線
を含む面内で羽根旋回軸より下流11i11の回転軸線
m上を除いた区域に中心をもつ円弧又は類似の曲線を母
線とする回転面(円錐面を含む)として、ハブ面3が 
形成されているので、I!?I示のように羽根式1」弘
の羽根旨さは羽根出口jの羽根高さよシ大きくなジ、そ
れだけ羽根流路幅が羽根入口で広くなっている。
However, in the present invention, which is different from the conventional one, the rotating surface (conical ), the hub surface 3 is
Since it is formed, I! ? As shown in I, the blade quality of the blade type 1'' is larger than the blade height at the blade outlet j, and the blade flow path width is correspondingly wider at the blade inlet.

このように、羽根車出口寸法がほぼ同じま1で羽根車人
口の流路幅(羽根高さ)が広がることにより、羽根車へ
の流入速度が減少するので、キャビテーションの発生の
恐れもなく、吸込性能を高めることができるはがシてな
く、羽根入口よシ同出口へ向って流路面積が増大する割
合も小さくなるので、それだけ羽根車内の流れが第1図
に示す従来のもののよりに急激に減速されることがなく
、したがって、羽根車内の水力損失が減少し、ポンプ効
率も向上する。
In this way, the flow path width (blade height) of the impeller population is increased while the impeller outlet dimensions remain approximately the same, and the inflow speed into the impeller is reduced, so there is no risk of cavitation occurring. The suction performance can be improved, and the rate of increase in the flow path area from the impeller inlet to the impeller outlet is also smaller, so the flow inside the impeller is much better than that of the conventional impeller shown in Figure 1. There is no rapid deceleration, thus reducing hydraulic losses in the impeller and increasing pump efficiency.

しかも、ハブ面の回転中心が、回転軸線を含む面内で羽
根旋回転よシ下流側の回転軸線上を除く広い区域の何れ
かに存在するため、ハブ面の形を、前記本発明者による
先願に係るものよシ、比較的自由に選択できるので、羽
根の入口部より出口部までの流路面積の変化の割合を、
ポンプに与えられる種々の条件に応じて比較的自由に選
定できる。そのため、上記のような吸込性能及びポンプ
性能の向上が一層促進される。
Moreover, since the center of rotation of the hub surface exists in any of a wide area within the plane including the rotation axis, excluding the rotary axis on the downstream side of the rotary rotation of the impeller, the shape of the hub surface is Compared to the previous application, it can be selected relatively freely, so the rate of change in the flow path area from the inlet to the outlet of the blade can be set as follows:
It can be selected relatively freely depending on various conditions given to the pump. Therefore, the improvement in suction performance and pump performance as described above is further promoted.

更に、この種の可動羽根斜流ポンプでは、締切軸動力比
を低くするためにハブ比が大きくされるが、本発明のも
のは、比較的大きくされているハブ比を変える必要なく
、羽根車入口流路幅(入口での羽根高さ)を広げること
ができるので、第1図に示すような従来の低締切軸動力
比としたものが有する前記のような欠点を除去すること
ができる。
Furthermore, in this type of movable blade mixed flow pump, the hub ratio is increased in order to lower the shut-off shaft power ratio, but in the present invention, the impeller can be adjusted without changing the relatively large hub ratio. Since the width of the inlet flow path (the height of the blades at the inlet) can be increased, the above-mentioned drawbacks of the conventional low cut-off shaft power ratio as shown in FIG. 1 can be eliminated.

本発明は、前述のような(14成になっているので、こ
れによシポンプ効率が高く、吸込性能がよく、かつ低締
切軸動力比の可動羽根斜流ポンプが得られる。
Since the present invention has the above-mentioned (14) structure, a movable vane mixed flow pump with high pump efficiency, good suction performance, and low shut-off shaft power ratio can be obtained.

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

第1図は従来形式の可動羽根斜流ポンプの軸方向断面図
、第2図は本発明の一実施例を示す可動羽根斜流ポンプ
の軸方向断面図である。 /・・・羽根車、コ・・・羽根、ム・・・羽根外周、3
・・・ハブ、l・・・羽根入口、!・・・羽根出口、0
・・・羽根外周の球面中心、Oa・・・)・、プ球面の
中心。
FIG. 1 is an axial sectional view of a conventional movable vane mixed flow pump, and FIG. 2 is an axial sectional view of a movable vane mixed flow pump showing an embodiment of the present invention. /...impeller, ko...blade, m...blade outer circumference, 3
...Hub, l...Blade inlet,! ...Blade outlet, 0
...The center of the spherical surface of the outer circumference of the blade, Oa...), the center of the spherical surface.

Claims (1)

【特許請求の範囲】[Claims] / 羽根外周面を球面状に形成した可動羽根斜流71?
ンプにおいて、回転軸線を含む面内で羽根旋回軸よシ下
流側の回転軸線上を除いた区域に中心をもつ円弧又は類
似の曲線を母線とする回転面(円錐面を含む)として、
ハブ面を形成したことを特徴とする可動羽根斜流ポンプ
。
/ Movable blade diagonal flow 71 with a spherical blade outer peripheral surface?
In a pump, as a rotating surface (including a conical surface) whose generating line is an arc or similar curve having a center in the area including the rotating axis, excluding the area on the downstream side of the rotating axis of the blade rotation axis,
A movable vane mixed flow pump characterized by forming a hub surface.
JP17927483A 1983-09-29 1983-09-29 Variable vane mixed flow pump Pending JPS6073094A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP17927483A JPS6073094A (en) 1983-09-29 1983-09-29 Variable vane mixed flow pump

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP17927483A JPS6073094A (en) 1983-09-29 1983-09-29 Variable vane mixed flow pump

Publications (1)

Publication Number Publication Date
JPS6073094A true JPS6073094A (en) 1985-04-25

Family

ID=16062972

Family Applications (1)

Application Number Title Priority Date Filing Date
JP17927483A Pending JPS6073094A (en) 1983-09-29 1983-09-29 Variable vane mixed flow pump

Country Status (1)

Country Link
JP (1) JPS6073094A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5310316A (en) * 1991-08-28 1994-05-10 Itt Flygt Ab Impeller for a propeller pump
EP2295808B1 (en) 2009-09-10 2016-06-08 Nijhuis Pompen BV Fish friendly pump or turbine apparatus

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS54128802A (en) * 1978-03-29 1979-10-05 Hitachi Ltd High specific speed pump
JPS5742174B2 (en) * 1980-04-08 1982-09-07

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS54128802A (en) * 1978-03-29 1979-10-05 Hitachi Ltd High specific speed pump
JPS5742174B2 (en) * 1980-04-08 1982-09-07

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5310316A (en) * 1991-08-28 1994-05-10 Itt Flygt Ab Impeller for a propeller pump
EP2295808B1 (en) 2009-09-10 2016-06-08 Nijhuis Pompen BV Fish friendly pump or turbine apparatus
EP2295808B2 (en) † 2009-09-10 2019-11-20 Nijhuis Pompen BV Fish friendly pump or turbine apparatus

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