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JPS5918553B2 - runner - Google Patents
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JPS5918553B2 - runner - Google Patents

runner

Info

Publication number
JPS5918553B2
JPS5918553B2 JP50149710A JP14971075A JPS5918553B2 JP S5918553 B2 JPS5918553 B2 JP S5918553B2 JP 50149710 A JP50149710 A JP 50149710A JP 14971075 A JP14971075 A JP 14971075A JP S5918553 B2 JPS5918553 B2 JP S5918553B2
Authority
JP
Japan
Prior art keywords
runner
blade
pump
flow rate
leading edge
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
Application number
JP50149710A
Other languages
Japanese (ja)
Other versions
JPS5273253A (en
Inventor
菊生 中島
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.)
Toshiba Corp
Original Assignee
Tokyo Shibaura Electric 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 Tokyo Shibaura Electric Co Ltd filed Critical Tokyo Shibaura Electric Co Ltd
Priority to JP50149710A priority Critical patent/JPS5918553B2/en
Priority to GB52450/76A priority patent/GB1573196A/en
Publication of JPS5273253A publication Critical patent/JPS5273253A/en
Priority to US05/944,682 priority patent/US4225547A/en
Publication of JPS5918553B2 publication Critical patent/JPS5918553B2/en
Expired legal-status Critical Current

Links

Classifications

    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/20Hydro energy

Landscapes

  • Hydraulic Turbines (AREA)

Description

【発明の詳細な説明】 本発明はランナに係り、特にポンプ運転時の羽根の前縁
曲線の形状を改良して低流量運転時に起るランナ内の偏
流現象を低減できるようにしたランナに関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a runner, and more particularly to a runner in which the shape of the leading edge curve of the vane during pump operation is improved to reduce the drift phenomenon within the runner that occurs during low flow rate operation.

一般にフランシス形ランナは、第1図に示されるように
クラウン1とバンド2と羽根3とが一体に構成されてい
る。
In general, a Francis-type runner has a crown 1, a band 2, and a blade 3 integrally constructed as shown in FIG.

羽根3は、第1図のI−I。■〜■・・・・・・、v−
■断面に示すように定格運転時の流水面上で、それぞれ
の断面について第2図に示すように翼素’1x−xが設
計され、第1図のI〜I、II〜■、・・・・・・、V
〜■に沿うそれぞれの翼素4I〜4vの連続体として形
づくられる。
The blade 3 is shown on I-I in FIG. ■~■・・・・・・,v-
■As shown in the cross section, on the flowing water surface during rated operation, blade elements '1x-x are designed for each cross section as shown in Figure 2, and I to I, II to ■ in Figure 1,... ..., V
It is formed as a continuum of wing elements 4I to 4v along ~■.

なお翼素4I〜4■の形状については図示しないが、第
2図に示す翼素4 と同様に、第1図のI−X −I、・・・、V−V線に沿うそれぞれの断面について
その設計がなされる。
Although the shapes of the blade elements 4I to 4■ are not shown, similar to the blade element 4 shown in FIG. 2, the respective cross sections along lines I-X-I, . The design is made for.

この場合に、1個の羽根3を形成する各翼素4I〜4■
の周方向の配置は、製作上の理由から、第1図に示すポ
ンプ運転時の前縁曲線5が、第3図に示されるように、
回転軸芯を通る一平面上にあるように設計されている。
In this case, each blade element 4I to 4■ forming one blade 3
Due to manufacturing reasons, the leading edge curve 5 during pump operation shown in FIG. 1 is arranged in the circumferential direction as shown in FIG.
It is designed to lie on a plane passing through the axis of rotation.

ところが、このようにして設計されたランナは、定格時
の60〜65%附近の流量(120〜130係附近の揚
程)で激しい水圧脈動を発生する。
However, the runner designed in this manner generates severe water pressure pulsations at a flow rate of around 60 to 65% of the rated value (head of around 120 to 130%).

大容量機にあってはこの脈動エネルギが強大であり、主
機のみならず発電所建屋を振動せしめ、当該脈動領域に
相当する水車負荷、ポンプ揚程時の運転を困難にしてい
た。
In large-capacity machines, this pulsating energy is so strong that it vibrates not only the main machine but also the power plant building, making it difficult to operate at turbine loads and pump lifts corresponding to the pulsating range.

発明者の実験の結果、上記水圧脈動は、−ポンプ低流量
域におけるランナ内の流れ中、局部的に超低圧領域が発
生して一部に偏流を生じ、羽根3の前縁曲線5のバンド
側、および羽根3の後縁7のクラウン側に発生する逆流
によることが明らかになった。
As a result of the inventor's experiments, the above-mentioned water pressure pulsation is caused by: - During the flow in the runner in the low flow region of the pump, an ultra-low pressure region occurs locally, causing a partial flow, and the band of the leading edge curve 5 of the blade 3. It has become clear that this is due to backflow occurring on the side and on the crown side of the trailing edge 7 of the blade 3.

ものと考えられる。この現象を説明するために、各運転
条件下でのランナ内の水の流れを示すと、第4図に示す
とおりとなり、図中aポンプ定格流計時bポンプ低流量
運転時、C水車低流量運転時のランナ内の流れをそれぞ
れ示している。
considered to be a thing. In order to explain this phenomenon, the flow of water in the runner under various operating conditions is as shown in Figure 4. Each figure shows the flow inside the runner during operation.

これらの図から明らかなように、第4図すおよびCにお
いて、偏流現象が認められ、偏流の起きた部分で流れの
エネルギレベルがバランスを失っているものと考えられ
る。
As is clear from these figures, a drifting phenomenon is observed in FIGS. 4A and 4C, and it is considered that the energy level of the flow has lost its balance in the portion where the drifting has occurred.

本発明の目的は、低流量運転時に惹起されるランナ内の
偏流現象を低減し、もって機器建屋の振動、騒音を低減
して経済的でかつ信頼度の高いランナを提供することに
ある。
An object of the present invention is to provide an economical and highly reliable runner that reduces the drifting phenomenon in the runner that occurs during low flow rate operation, thereby reducing vibration and noise in the equipment building.

以下、本発明によるランチの一実施例を図面を参照して
説明する。
Hereinafter, an embodiment of the lunch according to the present invention will be described with reference to the drawings.

本発明によれば、羽根3の各設計断面の翼素4I〜4■
は、バンド2側の翼素4Iをクラウン1側の翼素4Vに
対して相対的にポンプ回転方向の前方となるように周方
向に配列されている。
According to the present invention, blade elements 4I to 4■ of each design cross section of the blade 3
are arranged in the circumferential direction so that the vane elements 4I on the band 2 side are located forward in the pump rotational direction relative to the vane elements 4V on the crown 1 side.

この結果、羽根3の前縁曲線5の形状はその周方向分布
が、第5図において符号5′で示されるように従来とは
異なり、外径部分ではポンプとしての回転方向前方に、
内径部分では後方に相対的に位置するように形成される
As a result, the shape of the leading edge curve 5 of the blade 3 is different from the conventional one in its circumferential distribution, as shown by reference numeral 5' in FIG.
The inner diameter portion is formed so as to be relatively located at the rear.

このように構成された羽根3の断面形状を従来のものと
比較して示すと第6図のようになる。
The cross-sectional shape of the blade 3 constructed in this manner is shown in FIG. 6 in comparison with a conventional blade.

第6図は、第3図および第5図のそれぞれA−A断面に
相当するものを破線および実線で示している。
In FIG. 6, sections corresponding to the A-A cross sections in FIGS. 3 and 5 are shown by broken lines and solid lines, respectively.

同図から明らかなように、両者は、クラウン1の側で同
一の位置Rを占めているが、バンド2の側では異った2
つの位置p/ 、 Q/でそれぞれ終端している。
As is clear from the figure, both occupies the same position R on the crown 1 side, but they occupy different positions R on the band 2 side.
They terminate at two positions p/ and Q/, respectively.

従来のものと本発明によるものとの間の流体のエネルギ
レベルについて比較するに、本発明の羽根3上の点P′
および従来の羽根3上の点Q′は、第2図におけるP、
Q点に対応しており、P′点のエネルギレベルがより高
く、その結果、第4図すに示したような偏流の発生を防
止できるわけである。
Comparing the energy level of the fluid between the conventional one and the one according to the invention, the point P' on the vane 3 of the invention
And the point Q' on the conventional blade 3 is P in FIG.
This corresponds to point Q, and the energy level at point P' is higher, and as a result, the occurrence of drifting as shown in FIG. 4 can be prevented.

第7図は、本発明によるランナと従来のランナとの特性
を比較した線図であって、図中、実線は発明によるラン
ナ、破線は従来のランナをそれぞれ示している。
FIG. 7 is a diagram comparing the characteristics of the runner according to the present invention and the conventional runner. In the figure, the solid line indicates the runner according to the invention, and the broken line indicates the conventional runner.

同図から明らかなように、水圧脈動は、同一流量におい
て著しく低減され、最大脈動値の発生領域も高揚程少流
量側へ移行していることが認められ、少流量時には脈動
エネルギの絶対量が少なく水圧脈動の最大値も低減され
る。
As is clear from the figure, the water pressure pulsation is significantly reduced at the same flow rate, and the region where the maximum pulsation value occurs also shifts to the high head and low flow rate side, and at low flow rates, the absolute amount of pulsation energy decreases. The maximum value of water pressure pulsation is also reduced.

一方、定格流量附近の運転においては、流れがランナ内
に充満しており、かつ局部的な低圧領域が存在し得ない
ため、設計断面I −Vを横切る流量率が低く、かつ時
間的にゆるやかである。
On the other hand, in operation near the rated flow rate, the flow fills the runner and there is no local low pressure area, so the flow rate across the design cross section I-V is low and slow over time. It is.

そのためにランナ内の流れは、本発明の影響を二次的に
は受けるが性能上の差異は微差といえる。
Therefore, the flow within the runner is secondarily affected by the present invention, but the difference in performance can be said to be slight.

上述したように、本発明によれば、ランナの羽根のポン
プ運転時の前縁曲線の形状をその周方向の分布が、外径
部分ではポンプとしての回転方向前方に、内径部分では
後方に相対的に位置するよう形成したことによってラン
ナ内の偏流現象に起因して発生しがちの低流量運転時の
振動騒音現象をより低流量域へ移行せしめ、かつその最
大値を低減せしめることが可能である。
As described above, according to the present invention, the shape of the leading edge curve of the runner blade during pump operation is such that its distribution in the circumferential direction is relative to the front in the rotational direction of the pump at the outer diameter portion, and backward relative to the inner diameter portion. By forming the pipe so that it is located at the same position, it is possible to shift the vibration and noise phenomena that tend to occur during low flow rate operation due to drifting phenomena in the runner to a lower flow rate region, and to reduce the maximum value. be.

したがって、本発明によるランナをポンプ・水車として
利用した場合、指定された運転領域における振動、騒音
現象を低減できると共に連続運転の可能領域を拡大し、
ポンプ低流量運転時の効率を改善することができる。
Therefore, when the runner according to the present invention is used as a pump or water turbine, it is possible to reduce vibration and noise phenomena in the specified operating range, and expand the range of possible continuous operation.
Efficiency during low flow pump operation can be improved.

また、本発明によるランナをフランシス水車に利用した
場合低流量運転時の効率が著しく改善される等の効果を
期待できる。
Further, when the runner according to the present invention is used in a Francis turbine, effects such as a marked improvement in efficiency during low flow rate operation can be expected.

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

第1図はフランシス形ランナを示す縦断面図、第2図は
第1図のX−X線に沿う翼素の形状を示す図、第3図は
従来のランナをポンプ入口側からみた平面図、第4図a
、b、cは、各種条件下のランナ内の流れを示す図、第
5図は本発明のランナをポンプ入口側からみた平面図、
第6図はランナ縦断面における羽根の断面形状を従来の
ものと1 比較して示す断面図、第7図はランナの比較
特性線図である。 1・・・クラウン、2・・・バンド、3・・・羽根、4
・・・翼素、5・・・前縁曲線、7・・・後縁。
Figure 1 is a longitudinal cross-sectional view showing a Francis-type runner, Figure 2 is a diagram showing the shape of the blade element taken along line X-X in Figure 1, and Figure 3 is a plan view of a conventional runner as seen from the pump inlet side. , Figure 4a
, b, and c are diagrams showing the flow inside the runner under various conditions; FIG. 5 is a plan view of the runner of the present invention viewed from the pump inlet side;
FIG. 6 is a sectional view showing a comparison of the cross-sectional shape of the blade in the longitudinal section of the runner with that of a conventional blade, and FIG. 7 is a comparative characteristic diagram of the runner. 1... Crown, 2... Band, 3... Feather, 4
... wing element, 5 ... leading edge curve, 7 ... trailing edge.

Claims (1)

【特許請求の範囲】[Claims] 1 クラウンとバンドと羽根とからなるランナにおいて
、上記羽根のポンプ運転時の前縁曲線の形状をその周方
向の分布が、外径部分ではポンプとしての回転方向前方
に、内径部分では後方に相対的に位置するように形成し
たことを特徴とするランナ。
1. In a runner consisting of a crown, a band, and a vane, the shape of the leading edge curve of the vane during pump operation is such that its distribution in the circumferential direction is relative to the front in the rotational direction of the pump at the outer diameter part, and backward relative to the inner diameter part. A runner characterized by being formed so as to be located at a specific position.
JP50149710A 1975-12-15 1975-12-16 runner Expired JPS5918553B2 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
JP50149710A JPS5918553B2 (en) 1975-12-16 1975-12-16 runner
GB52450/76A GB1573196A (en) 1975-12-15 1976-12-15 Method and apparatus for extruding polytetrafluoroethlene tubing
US05/944,682 US4225547A (en) 1975-12-15 1978-09-22 Extrusion process of polytetrafluoroethylene tubing materials and apparatus therefor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP50149710A JPS5918553B2 (en) 1975-12-16 1975-12-16 runner

Publications (2)

Publication Number Publication Date
JPS5273253A JPS5273253A (en) 1977-06-18
JPS5918553B2 true JPS5918553B2 (en) 1984-04-27

Family

ID=15481118

Family Applications (1)

Application Number Title Priority Date Filing Date
JP50149710A Expired JPS5918553B2 (en) 1975-12-15 1975-12-16 runner

Country Status (1)

Country Link
JP (1) JPS5918553B2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7198470B2 (en) 2003-06-16 2007-04-03 Kabushiki Kaisha Toshiba Francis turbine

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP4751165B2 (en) * 2005-10-12 2011-08-17 株式会社東芝 Francis pump turbine

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE548479A (en) * 1955-06-18

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7198470B2 (en) 2003-06-16 2007-04-03 Kabushiki Kaisha Toshiba Francis turbine

Also Published As

Publication number Publication date
JPS5273253A (en) 1977-06-18

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