JPS6119835B2 - - Google Patents
Info
- Publication number
- JPS6119835B2 JPS6119835B2 JP56117298A JP11729881A JPS6119835B2 JP S6119835 B2 JPS6119835 B2 JP S6119835B2 JP 56117298 A JP56117298 A JP 56117298A JP 11729881 A JP11729881 A JP 11729881A JP S6119835 B2 JPS6119835 B2 JP S6119835B2
- Authority
- JP
- Japan
- Prior art keywords
- pump
- blade
- impeller
- casing
- conical
- 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
Links
- 238000013459 approach Methods 0.000 claims description 2
- 239000007787 solid Substances 0.000 description 7
- 239000007788 liquid Substances 0.000 description 6
- 238000010586 diagram Methods 0.000 description 4
- 230000005855 radiation Effects 0.000 description 4
- 239000012530 fluid Substances 0.000 description 3
- 238000011144 upstream manufacturing Methods 0.000 description 3
- 230000007423 decrease Effects 0.000 description 2
- 238000009434 installation Methods 0.000 description 1
- 230000000414 obstructive effect Effects 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 239000010865 sewage Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/18—Rotors
- F04D29/22—Rotors specially for centrifugal pumps
- F04D29/2238—Special flow patterns
- F04D29/225—Channel wheels, e.g. one blade or one flow channel
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Description
【発明の詳細な説明】
本発明は一板の円錐ねじ羽根の翼を有するポン
プに関する。DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a pump having a single-plate conical screw vane blade.
汚水、汚物、パルプ液等の移送用ポンプとして
は固形物、繊維物質等の異物が詰つたり、引つ掛
つたりすることのない無閉塞性のポンプが要求さ
れる。この種のポンプとしては一枚又は小数枚の
翼を持つ羽根車を備えたものがある。 Pumps for transferring sewage, filth, pulp liquid, etc. are required to be non-obstructive pumps that do not become clogged or caught by foreign matter such as solid matter or fibrous substances. Some pumps of this type are equipped with an impeller having one or a few blades.
第4図は従来例の小数枚の翼を備えたポンプの
例である。図において翼2を備えた羽根車1は図
示する中心線3を中心に回転するようポンプケー
シング4に支持されている。ポンプケーシング4
と翼2の縁辺との間に図示δの間隙がある。 FIG. 4 is an example of a conventional pump having a small number of blades. In the figure, an impeller 1 having blades 2 is supported by a pump casing 4 so as to rotate about a center line 3 shown in the figure. pump casing 4
There is a gap δ shown in the figure between the blade 2 and the edge of the blade 2.
第5図は第4図の羽根車の一部正面図である。
翼2の翼端5は中心線3よりの放射線の方向より
角β後退した位置にある。このような例では第4
図に矢印で示されるように固形物等を含んだ液体
が流れるため、間隙δの部分に固形物等が入つて
も間隙δが大きいから通過し得る。しかし乍らこ
の構造では液の漏洩損失が大きく、従つてポンプ
効率を低下せしめる。 FIG. 5 is a partial front view of the impeller shown in FIG. 4.
The blade tip 5 of the blade 2 is located at a position set back by an angle β from the direction of the radiation from the center line 3. In such an example, the fourth
As shown by the arrow in the figure, the liquid containing solid matter flows, so even if solid matter enters the gap δ, it can pass through because the gap δ is large. However, with this structure, leakage loss of liquid is large, and therefore pump efficiency is reduced.
他の従来例としては母線が直線、曲線の円錐形
回転面をなすポンプケーシングとねじ羽根の翼の
外周回転面が同円錐形回転面の羽根車を備えたも
のがある(特公昭43―15006号公報)。この公知例
のポンプは円錐様の第一ハブに第一のハブの軸に
対し角度がずれている第二のハブを備えて第一,
第二のハブを取巻き、第二の軸のずれたハブから
軸方向に上流に延びた略一定の厚みをもつた単一
の連続した螺旋形のねじ板を備えた羽根車がケー
シング中に隙間少く納められている。この種のポ
ンプではねじ羽根を第一ハブより先に出すことに
よりポンプ性能の向上が認められる。 Another conventional example includes a pump casing whose generatrix is a straight line and a curved conical rotating surface, and an impeller whose outer circumferential rotating surface of the screw vane is the same conical rotating surface (Japanese Patent Publication No. 43-15006 Publication No.). This known pump includes a conical first hub and a second hub that is angularly offset from the axis of the first hub.
An impeller with a single continuous helical threaded plate of substantially constant thickness surrounding a second hub and extending axially upstream from the second off-axis hub is provided with a gap in the casing. A small amount is paid. In this type of pump, pump performance can be improved by having the screw vanes come out before the first hub.
特願昭56―66035号に係わる発明「一枚翼羽根
車ポンプ」は、
「吸込口と吐出ケーシング間が円錐様回転面をな
したポンプケーシングに、外周回転面がポンプケ
ーシングの円錐様回転面に隙間少く接近する円錐
様をなしたねじ羽根の翼を円錐用ハブに形成した
羽根車をケーシング内にて回転可能に支持した一
枚翼羽根車ポンプにおいて、吸込側翼根本を円錐
様ハブ頂点近傍にて終らせた該翼根本よりポンプ
軸中心線よりの放射線よりも翼端正面が前進する
方向に翼端を傾けた一枚翼羽根車ポンプ。」
であつて、一枚翼羽根車ポンプでは効率が前記各
従来例に比して良好ではあつても極めて良好とは
いえず尚高効率化を計る必要がある。 The invention related to Japanese Patent Application No. 56-66035, ``Single-blade impeller pump,'' consists of a ``pump casing with a conical rotating surface between the suction port and the discharge casing, and an outer circumferential rotating surface of the pump casing with a conical rotating surface. In a single-blade impeller pump, in which an impeller is rotatably supported in a casing, the impeller is rotatably supported in a casing, and the blade of the conical hub is formed with conical screw blades that are close to each other with a small gap. A single-blade impeller pump in which the blade tip is inclined in a direction in which the front of the blade tip moves forward from a radiation line from the center line of the pump shaft from the root of the blade. Although the efficiency is better than those of the conventional examples, it is not extremely good, and it is necessary to improve the efficiency even further.
本発明の目的は一枚翼羽根車ポンプの効率の向
上を計ることである。 The purpose of the invention is to improve the efficiency of single-blade impeller pumps.
本発明の一枚翼羽根車ポンプは吸込口と吐出ケ
ーシング間が円錐様回転面をなしたポンプケーシ
ングに、外周回転面がポンプケーシングの円錐様
回転面に隙間少く接近する円錐様をなしたねじ羽
根の翼を円錐用ハブに形成した羽根車をケーシン
グ内にて回転可能に支持した一枚翼羽根車ポンプ
において、翼の羽根車のハブへの取付角が入口側
において30〜60度、出口側において0〜40度夫々
ポンプ主軸より吸込口側に傾いており且つ翼の傾
きは入口側より出口側に次第にポンプ主軸軸心と
なす角が小となるようになつている。 The single-blade impeller pump of the present invention has a pump casing with a conical rotating surface between the suction port and the discharge casing, and a conical screw whose outer peripheral rotating surface approaches the conical rotating surface of the pump casing with little clearance. In a single-blade impeller pump in which an impeller whose blades are formed into conical hubs is rotatably supported within a casing, the attachment angle of the blades to the hub is 30 to 60 degrees on the inlet side and 30 to 60 degrees on the outlet side. The blades are inclined from 0 to 40 degrees toward the suction port side from the pump main shaft, and the angle between the blades and the pump main shaft axis gradually decreases from the inlet side to the outlet side.
以下、図面に従つて本発明の実施例について説
明する。第1図は本発明のポンプ軸を含む縦断面
図である。ポンプケーシング4は吸込口6が一体
に形成せられ、吸込口6側を小端として内周は直
線又は曲線もしくはそれらを組合せた母線をポン
プ主軸3′を中心にして回転させた円錐様形状で
あり、ポンプケーシング4には吐出ケーシング7
が固定され、吐出ケーシング7に軸方向移動を制
止され、回転可能に軸承され軸封(説明は省略す
る)されたポンプ主軸3′には羽根車1の円錐様
ハブ8がポンプ主軸3′の締り勝手方向になるよ
うにねじ込まれている。円錐様ハブ8は母線が直
線又は曲線又はそれらを組合せた回転曲面であ
り、ポンプケーシング4との間の流体通路が適当
になるように選ばれている。 Embodiments of the present invention will be described below with reference to the drawings. FIG. 1 is a longitudinal sectional view including the pump shaft of the present invention. The pump casing 4 is integrally formed with a suction port 6, and has a cone-like shape with the suction port 6 side as the small end and the inner periphery rotated around the pump main shaft 3' with a generatrix of a straight line, a curve, or a combination thereof. Yes, the pump casing 4 has a discharge casing 7
The conical hub 8 of the impeller 1 is attached to the pump main shaft 3', which is fixed and whose axial movement is restrained by the discharge casing 7, rotatably supported and sealed (description will be omitted). It is screwed in so that it is in the tightening direction. The conical hub 8 has a generatrix of a straight line, a curved line, or a rotating curved surface with a combination thereof, and is selected so as to provide an appropriate fluid passage between the conical hub 8 and the pump casing 4.
円錐様ハブ8にはねじ羽根の翼2が一体に形成
せられている。翼2の吸込口6の側は円錐様ハブ
8の頂点附近もしくは頂点で終つており、その位
置より翼端5が翼2の外周に向う。翼2の外周は
ポンプケーシング4の内周面と隙間少ない位置に
ある直線又は曲線もしくはこれらを組合せた母線
を有するポンプ主軸3′を中心とする回転面上に
ある。 A screw blade 2 is integrally formed on the conical hub 8. The suction port 6 side of the blade 2 ends near or at the apex of the conical hub 8, from which point the blade tip 5 points toward the outer periphery of the blade 2. The outer periphery of the blade 2 is on a rotating surface centered on the pump main shaft 3', which has a straight line, a curved line, or a generatrix of a combination thereof, which is located at a position with little clearance from the inner circumferential surface of the pump casing 4.
第2図は翼2の先端中心部の拡大正面図であ
る。円錐様ハブ8と翼2の根本の境界線9は中心
線3(紙面に直交している)近傍にて終つてお
り、中心線3よりの放射線10より翼端5が進ん
で行く方向に翼端5は放射線10より次第に離れ
て行くような凹な曲線をなしている。これは曲率
が大きいときは直線に代えてもよいが後に説明さ
れる流体の流れを中心に向けるように図のような
中心より離れるに従つて切線角7が次第に大とな
る曲線が望ましい。中心線3と翼端5と翼2の外
周11との交点12とを結ぶ線と放射線10が中
心線3に張る角βは図示実例の大きさである。 FIG. 2 is an enlarged front view of the center of the tip of the wing 2. The boundary line 9 between the conical hub 8 and the root of the wing 2 ends near the center line 3 (perpendicular to the plane of the paper), and the wing tip 5 extends in the direction in which the wing tip 5 advances from the line 10 from the center line 3. The end 5 has a concave curve that gradually moves away from the radiation 10. When the curvature is large, this may be replaced with a straight line, but it is preferable to use a curved line in which the tangential angle 7 gradually increases as the distance from the center increases, as shown in the figure, so as to direct the flow of fluid toward the center, which will be explained later. The angle β between the center line 3 and the line connecting the center line 3, the intersection 12 of the blade tip 5 and the outer periphery 11 of the blade 2, and the ray 10 is the size of the illustrated example.
第6図は羽根車1の翼2の吸込口側より見る正
面図であつて翼2のおもて側シユラウド側角が示
されている。第7図は第6図における中心線を含
む羽根車1の断面図である。 FIG. 6 is a front view of the impeller 1 viewed from the suction port side of the blades 2, showing the front shroud side corner of the blades 2. FIG. 7 is a sectional view of the impeller 1 including the center line in FIG. 6.
第6図の翼2の吸込口側の翼端の0―a断面は
第7図において翼2a、0―b断面は翼2b、0
―c断面は翼2c、吐出口に近い0―d断面は翼
2d、0―e断面は翼2eで表わされる。翼2a
の断面の厚さはシユラウド側t1、翼根本側t2とす
るとt1=t2即ち平板状である。 The 0-a section of the blade tip on the suction port side of the blade 2 in FIG. 6 is the blade 2a in FIG. 7, and the 0-b cross section is the blade 2b, 0.
The -c section is represented by the blade 2c, the 0-d cross section near the discharge port is represented by the blade 2d, and the 0-e cross section is represented by the blade 2e. Wing 2a
Assuming that the thickness of the cross section is t 1 on the shroud side and t 2 on the blade root side, t 1 =t 2 , that is, it has a flat plate shape.
翼2と円錐様ハブ8との取付角α、即ちポンプ
主軸3′を含む平面上において、翼2のおもて側
とポンプ主軸3′の中心線3とのなす角αは入口
側の翼2aにてはα=30〜60度であり出口側の翼
2eにてはα=0〜40度であり、入口側より出口
側に向つて角αは次第に小となつている。 The mounting angle α between the blade 2 and the conical hub 8, that is, the angle α between the front side of the blade 2 and the center line 3 of the pump main shaft 3' on the plane including the pump main shaft 3' is the angle α between the blade 2 and the center line 3 of the pump main shaft 3'. In the blade 2a, α=30 to 60 degrees, and in the outlet side blade 2e, α=0 to 40 degrees, and the angle α gradually becomes smaller from the inlet side to the outlet side.
以上に対して従来例の一枚翼羽根車ポンプの翼
の上記諸元は第6図の断面線を第8図で示すよう
な翼断面を有し、入口部の翼2aの翼厚t1<t2で
あり、翼取付角α=50〜60度であつて入口側の翼
2aより出口側の翼2eまで一定である。 In contrast to the above, the above specifications of the blade of the conventional single-blade impeller pump have a blade cross section such that the cross-sectional line of FIG. 6 is shown in FIG . < t2 , and the blade attachment angle α=50 to 60 degrees, which is constant from the blade 2a on the inlet side to the blade 2e on the outlet side.
第1図において羽根車1が回転すると固形物を
含んだ流体は吸込まれ、ポンプケーシング4中で
翼2の空間を移動して吐出ケーシング7に送られ
吐出される。その際、第3図の説明図に示される
ように翼端5の部分で固形物等は矢印14の方向
に流れる。円錐様ハブ8の先端は図示されてはい
るが翼2の厚さにより実際にはなく、翼端5は円
錐様ハブ8に滑かに連続しているから、翼2と円
錐様ハブ8及びポンプケーシング4間の空間に障
害なく入る。かくして固形物等を含む液体も翼2
外周とポンプケーシング4間の隙間につまること
なく送られる。即ち、本発明の一枚翼羽根車ポン
プも従来例も同様に動作する。こゝにおいて入口
側の翼5aは一定厚さであることにより従来例に
比して固形物等が滑らかに翼間に入ることが判明
した。 In FIG. 1, when the impeller 1 rotates, fluid containing solids is sucked in, moves through the space of the blades 2 in the pump casing 4, is sent to the discharge casing 7, and is discharged. At this time, as shown in the explanatory view of FIG. 3, the solid matter flows in the direction of the arrow 14 at the blade tip 5. Although the tip of the cone-like hub 8 is shown, it is not actually present due to the thickness of the wing 2, and since the wing tip 5 is smoothly continuous with the cone-like hub 8, the wing 2, the cone-like hub 8, and To enter the space between the pump casings 4 without any obstruction. In this way, liquids containing solids etc.
It is fed without clogging the gap between the outer periphery and the pump casing 4. That is, the single-blade impeller pump of the present invention and the conventional example operate in the same manner. It has been found that since the blades 5a on the inlet side have a constant thickness, solids etc. can enter between the blades more smoothly than in the conventional example.
尚羽根車1の形状により、吸込部はポンプ主軸
に対して翼2a等が立つているので軸流作用を行
ない後流側は翼2e等がポンプ主軸に対して寝て
いるので遠心作用を行なう。従つて従来例の第8
図の様に吸込側から後流側まで翼の羽根車の円錐
様ハブ8への取付角がほぼ同一である軸流作用主
体のものと異なり、同一の外径をもつた従来例の
羽根車に比較しこの発明の羽根車1では高揚程が
期待でき、効率も上昇する。これは後述の実験結
果からも明らかである。 Due to the shape of the impeller 1, the suction section has blades 2a, etc. standing up against the pump main shaft, so it performs an axial flow action, and on the wake side, the blades 2e, etc. lie against the pump main shaft, so it performs a centrifugal action. . Therefore, the eighth conventional example
As shown in the figure, the angle of attachment of the blade impeller to the conical hub 8 is almost the same from the suction side to the wake side, unlike the conventional impeller that has the same outer diameter, unlike the one that mainly acts on axial flow. Compared to the impeller 1 of the present invention, a higher head can be expected and the efficiency will also increase. This is also clear from the experimental results described below.
この効率上昇は次の様に考えられる。 This efficiency increase can be considered as follows.
本発明の羽根車1は吸込部で、軸流作用を行な
い、後流側で遠心作用を行なわせるものであり、
一般的に羽根車の特性として次のことが云える。 The impeller 1 of the present invention performs an axial flow action at the suction part and a centrifugal action at the downstream side,
In general, the following characteristics can be said about impellers:
1) 軸流ポンプの吐出量〜揚程曲線は急勾配と
なる。1) The displacement-head curve of an axial flow pump has a steep slope.
2) 軸流ポンプでは遠心ポンプに比較し、締切
点側での軸動力が大きく吐出量増加に対して
水平もしくは下がる傾向にある。2) In axial flow pumps, compared to centrifugal pumps, the shaft power on the cutoff point side is large and tends to level off or decrease as the discharge rate increases.
3) 軸流ポンプではポンプ効率曲線は遠心ポン
プに比較し丸味が小さくなる。言いかえれ
ば、吐出量に対する高効率の範囲が狭くな
る。3) For axial flow pumps, the pump efficiency curve is less rounded than for centrifugal pumps. In other words, the range of high efficiency relative to the discharge amount becomes narrower.
上記傾向は周知のことであり、図示すると第1
0図の如くなる。第10図は横軸に吐出し量を縦
軸には全揚程と効率をとつたもので、実線で示さ
れるものは遠心ポンプに関するものであり、点線
は軸流ポンプに関するもので両ポンプ要項は同一
とした場合である。本発明のポンプは軸流、遠心
両特性を併せもつた特性を有している。更に本発
明では吐出側に近い翼程その翼端とポンプケーシ
ング4間の隙間から、後流側より上流側へ洩れる
量が従来例では多いのであるが本発明のものは少
ないものと考えられる。なんとなれば従来例では
翼2の作用面の液体はより遠心力を大きく与えら
れるにもかゝわらず翼2のポンプ主軸の中心線3
となす取付角αは一定であるため出口側に行く程
翼2の先端とポンプケーシング4の隙間から後流
側より上流側へ洩れる量が増大するが本発明では
後流側程翼2がポンプ主軸の中心線3となす取付
角が小さいから、翼面上を翼端側へ液体を附勢す
る力が生じないか或は従来例に比較して小さくで
きるからである。これらの理由により本発明の一
枚翼羽根車ポンプは従来例に比して高効率を得る
ことができたものと考えられる。尚、実験結果で
は最高効率値が従来例に比して高いのは前記二つ
の理由の内、後に説明した理由がより働いている
ためと考えられる。 The above trends are well known, and to illustrate, the first
It will look like Figure 0. Figure 10 shows the discharge amount on the horizontal axis and the total head and efficiency on the vertical axis.The solid line is for the centrifugal pump, and the dotted line is for the axial flow pump, and the requirements for both pumps are as follows. This is the case where they are the same. The pump of the present invention has characteristics that combine both axial flow and centrifugal flow characteristics. Furthermore, in the present invention, the amount of leakage from the gap between the tip of the blade closer to the discharge side and the pump casing 4 to the upstream side than to the wake side is larger in the conventional example, but it is considered to be less in the present invention. This is because in the conventional example, although a larger centrifugal force is applied to the liquid on the working surface of the blade 2, the center line 3 of the pump main shaft of the blade 2
Since the mounting angle α is constant, the amount of leakage from the gap between the tip of the blade 2 and the pump casing 4 increases from the downstream side to the upstream side as it goes toward the outlet side. This is because the mounting angle formed with the center line 3 of the main shaft is small, so the force that urges the liquid on the blade surface toward the blade tip side is not generated or can be made smaller compared to the conventional example. It is believed that for these reasons, the single-blade impeller pump of the present invention was able to achieve higher efficiency than the conventional example. In addition, the reason why the maximum efficiency value is higher than that of the conventional example according to the experimental results is considered to be that of the above two reasons, the reason explained later is more effective.
第9図は以上に説明した本発明の一枚翼羽根車
ポンプと従来例のもののポンプ性能の比較を示す
線図である。横軸に吐出し量を縦軸には全揚程と
効率をとつたもので、実線で示されるものは本発
明の一枚翼羽根車ポンプに関するものであり、点
線は従来例に関するものである。図より明らかな
ように最大効率において本発明の一枚翼羽根車ポ
ンプのほうが従来例より改良されており、その点
における本発明の一枚翼羽根車ポンプの揚程を
H1、従来例のものをH2とするとH1/H2=1.2〜
1.5であつた。 FIG. 9 is a diagram showing a comparison of pump performance between the single-blade impeller pump of the present invention and the conventional pump described above. The horizontal axis shows the discharge amount, and the vertical axis shows the total head and efficiency.The solid line shows the single-blade impeller pump of the present invention, and the dotted line shows the conventional example. As is clear from the figure, the single-blade impeller pump of the present invention is improved in terms of maximum efficiency over the conventional example, and the pump head of the single-blade impeller pump of the present invention in this respect is
H 1 and the conventional example as H 2 , H 1 /H 2 = 1.2~
It was 1.5.
このように本発明の一枚翼羽根車ポンプは従来
例よりも効率よく揚程大であるから、逆に同揚程
のものとするとポンプを小さくできる訳である。 As described above, since the single-blade impeller pump of the present invention is more efficient than the conventional example and has a larger head, conversely, if the pump has the same head, the pump can be made smaller.
以上のとおり、本発明は円錐様ポンプケーシン
グに外周が円錐様のねじ羽根の翼を有する羽根車
を納めたポンプにおいて、翼のハブへの取付角を
入口側から出口側に向つて取付角を次第に小さく
するようにしたからポンプ効率は増大し、同一吐
出し量に対する揚程は増大し、ポンプ容量を同一
とするとポンプを小さくできる。 As described above, the present invention provides a pump in which an impeller having threaded blades with a conical outer circumference is housed in a conical pump casing, in which the installation angle of the blades to the hub is changed from the inlet side to the outlet side. Since the pump is gradually made smaller, the pump efficiency increases, and the head for the same discharge amount increases, and if the pump capacity is kept the same, the pump can be made smaller.
以上のポンプ効率の向上により一枚翼羽根車ポ
ンプを小型軽量化できる。 By improving the pump efficiency as described above, the single-blade impeller pump can be made smaller and lighter.
第1図は本発明の実施例の縦断面図、第2図は
第1図の一部拡大正面図、第3図は第1図の作用
の説明図、第4図は従来例の作用を説明する縦断
面図、第5図は第4図の一部拡大正面図、第6
図、第7図は本発明の翼形を示す図面であつて、
第6図は正面図、第7図は縦断面図、第8図は従
来例の翼形の縦断面図、第9図はポンプ性能の比
較線図、第10図は遠心ポンプと軸流ポンプの性
能比較線図である。
1…羽根車、2…翼、3…中心線、3′…ポン
プ主軸、4…ポンプケーシング、5…翼端、6…
吸込口、7…吐出ケーシング、8…円錐様ハブ、
9…境界線、10…放射線、11…外周、12…
交点、2a〜2e…翼、α…取付角。
Fig. 1 is a longitudinal sectional view of an embodiment of the present invention, Fig. 2 is a partially enlarged front view of Fig. 1, Fig. 3 is an explanatory diagram of the operation of Fig. 1, and Fig. 4 is an illustration of the operation of the conventional example. A vertical sectional view to be explained, FIG. 5 is a partially enlarged front view of FIG. 4, and FIG.
7 and 7 are drawings showing the airfoil of the present invention,
Figure 6 is a front view, Figure 7 is a longitudinal sectional view, Figure 8 is a longitudinal sectional view of a conventional airfoil, Figure 9 is a comparison diagram of pump performance, and Figure 10 is a centrifugal pump and an axial flow pump. It is a performance comparison diagram. 1... Impeller, 2... Blade, 3... Center line, 3'... Pump main shaft, 4... Pump casing, 5... Blade tip, 6...
Suction port, 7...Discharge casing, 8...Conical hub,
9... Boundary line, 10... Radiation, 11... Outer circumference, 12...
Intersection, 2a to 2e...wings, α...mounting angle.
Claims (1)
なしたポンプケーシングに、外周回転面がポンプ
ケーシングの円錐様回転面に隙間少く接近する円
錐様をなしたねじ羽根の翼を円錐様ハブに形成し
た羽根車をケーシング内にて回転可能に支持した
一枚翼羽根車ポンプにおいて、翼の羽根車のハブ
への取付角が入口側において30〜60度、出口側に
おいて0〜40度夫々ポンプ主軸より吸込口側に傾
いており且つ翼の傾きは入口側より出口側に次第
にポンプ主軸軸心となす角が小となるようになつ
ている一枚翼羽根車ポンプ。1. On a pump casing that has a conical rotating surface between the suction port and the discharge casing, a conical hub is formed with a conical screw blade whose outer circumferential rotating surface approaches the conical rotating surface of the pump casing with little clearance. In a single-blade impeller pump in which a rotatably supported impeller is rotatably supported within a casing, the angle at which the blades are attached to the hub of the impeller is 30 to 60 degrees on the inlet side and 0 to 40 degrees on the outlet side, respectively. A single-blade impeller pump that is tilted more toward the suction port, and the angle of the blade with the pump main axis becomes smaller gradually from the inlet side to the outlet side.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP11729881A JPS5818591A (en) | 1981-07-27 | 1981-07-27 | Single balde type turbine pump |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP11729881A JPS5818591A (en) | 1981-07-27 | 1981-07-27 | Single balde type turbine pump |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS5818591A JPS5818591A (en) | 1983-02-03 |
| JPS6119835B2 true JPS6119835B2 (en) | 1986-05-19 |
Family
ID=14708284
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP11729881A Granted JPS5818591A (en) | 1981-07-27 | 1981-07-27 | Single balde type turbine pump |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS5818591A (en) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS59138792A (en) * | 1983-01-27 | 1984-08-09 | Furukawa Mining Co Ltd | Mixed flow pump of single impeller vane |
| JPH0637879B2 (en) * | 1985-03-15 | 1994-05-18 | 大平洋機工株式会社 | Centrifugal pump |
| JPS62183096U (en) * | 1986-05-12 | 1987-11-20 |
-
1981
- 1981-07-27 JP JP11729881A patent/JPS5818591A/en active Granted
Non-Patent Citations (1)
| Title |
|---|
| DIE KREISELPUMPEN=1949 * |
Also Published As
| Publication number | Publication date |
|---|---|
| JPS5818591A (en) | 1983-02-03 |
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