JPS634024B2 - - Google Patents

Info

Publication number
JPS634024B2
JPS634024B2 JP55072470A JP7247080A JPS634024B2 JP S634024 B2 JPS634024 B2 JP S634024B2 JP 55072470 A JP55072470 A JP 55072470A JP 7247080 A JP7247080 A JP 7247080A JP S634024 B2 JPS634024 B2 JP S634024B2
Authority
JP
Japan
Prior art keywords
runner
exhaust
chamber
pressure stage
stage
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
JP55072470A
Other languages
Japanese (ja)
Other versions
JPS57364A (en
Inventor
Kentaro Ichikawa
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 JP7247080A priority Critical patent/JPS57364A/en
Priority to US06/199,628 priority patent/US4406577A/en
Priority to DE19803040468 priority patent/DE3040468A1/en
Priority to CH8011/80A priority patent/CH658495A5/en
Publication of JPS57364A publication Critical patent/JPS57364A/en
Priority to US06/495,945 priority patent/US4547123A/en
Publication of JPS634024B2 publication Critical patent/JPS634024B2/ja
Granted 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】 本発明は多段水力機械の排気装置に係り、特に
ポンプ起動時あるいは調相運転時に水面押下げ運
転をする多段水力機械の排気装置に関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to an exhaust system for a multi-stage hydraulic machine, and more particularly to an exhaust system for a multi-stage hydraulic machine that operates to push down the water surface during pump startup or phase adjustment operation.

水力発電所が高落差化し、その落差が単段ポン
プ水車の性能の限界を越えると多段ポンプ水車が
使用されることになる。従来の多段ポンプ水車の
多くのものは可動ガイドベーンを備えていないか
ら、ポンプ起動時には水中起動方式を採用せざる
をえない。ところが、水中起動方式は機械が大容
量化してくるとポンプ起動時の軸入力が非常に大
きくなり、系統に悪影響を与え、経済的にも不利
であるという欠点を有していた。そこで、最近の
大容量の多段水力機械においては、水面押下げ状
態下で発電機をモータリングさせてランナを空転
させる調相運転や、揚水運転に対して速応できる
ように同じく水面押下げ状態でランナをポンプ方
向に空転させて揚水待機運転を行なうことが要求
されている。
When hydroelectric power plants have higher heads and the head exceeds the performance limits of single-stage pump-turbines, multi-stage pump-turbines are used. Many conventional multi-stage pump turbines do not have movable guide vanes, so they have no choice but to use an underwater startup method when starting the pump. However, the submersible starting method has the drawback that as the capacity of the machine increases, the shaft input when starting the pump becomes extremely large, which adversely affects the system and is economically disadvantageous. Therefore, in recent large-capacity multi-stage hydraulic machines, phase adjustment operation in which the generator is motored to idle the runners when the water surface is depressed, and a phase adjustment operation in which the runner is idled while the water surface is depressed, and a phase adjustment operation in which the water surface is depressed in order to quickly respond to pumping operation, have been adopted. It is required that the runner be idly rotated in the direction of the pump to perform pumping standby operation.

しかしながら、多段ポンプ水車は流路形状が複
雑なために、特に低圧段のランナ室内の圧縮空気
を排気渋滞を起すことなしに排気を完全に行なう
ことは難しく、そのために多段ポンプ水車におい
ては水面押下げ状態下にポンプ起動や調相運転を
行なうことが困難であつた。
However, because the flow path shape of multistage pump turbines is complex, it is difficult to completely exhaust the compressed air from the runner chambers of the low pressure stages without causing exhaust congestion. It was difficult to start the pump or perform phase adjustment operation under the lowered condition.

本発明はこのような事情を考慮して発明された
ものであつて、可動ガイドベーンを備えた多段水
力機械を水面押下げ運転後、各低圧段のランナ室
および流路内の空気を確実かつ完全に排出するこ
とができるようにした多段水力機械の排気装置を
提供することにある。
The present invention was devised in consideration of the above circumstances, and is designed to reliably and efficiently pump air into the runner chambers and flow paths of each low-pressure stage after operating a multi-stage hydraulic machine equipped with movable guide vanes to push down the water surface. The object of the present invention is to provide an exhaust system for a multi-stage hydraulic machine that can completely exhaust the air.

以下本発明による多段水力機械の排気装置の一
実施例を図面を参照して説明する。
An embodiment of the exhaust system for a multi-stage hydraulic machine according to the present invention will be described below with reference to the drawings.

第1図は2段ポンプ水車に対して本発明を適用
した例を示し、図において符号1は2段ポンプ水
車の主軸を示しており、この主軸1には高圧段ラ
ンナ2と低圧段ランナ3とがスペーサ4を介して
軸方向の距離をおいて固着されている。上記高圧
段ランナ2は高圧段ランナ室5内に収容される一
方、上記低圧段ランナ3は低圧段ランナ室6内に
収容されている。
FIG. 1 shows an example in which the present invention is applied to a two-stage pump-turbine. In the figure, reference numeral 1 indicates the main shaft of the two-stage pump-turbine, and this main shaft 1 has a high-pressure stage runner 2, a low-pressure stage runner 3 and are fixed at a distance in the axial direction via a spacer 4. The high pressure stage runner 2 is housed in a high pressure stage runner chamber 5, while the low pressure stage runner 3 is housed in a low pressure stage runner chamber 6.

上記高圧段ランナ2の上方には上カバー7が配
置される一方、高圧段ランナ2の下方には下カバ
ー8が配置され、この上カバー7と下カバー8の
間であつて高圧段ランナ2の半径方向外方には水
口開度を調整可能な可動ガイドベーン10が配置
されている。この可動ガイドベーン10は、その
上部ステム10aの上端にガイドベーン操作リン
ク機構11が連結されており、公知のように、ガ
イドリング12によつてガイドベーンの開閉が行
われる。
An upper cover 7 is arranged above the high-pressure stage runner 2, while a lower cover 8 is arranged below the high-pressure stage runner 2. A movable guide vane 10 whose opening degree can be adjusted is arranged radially outward. The movable guide vane 10 has a guide vane operating link mechanism 11 connected to the upper end of its upper stem 10a, and the guide vane is opened and closed by a guide ring 12, as is known in the art.

さらに、上記可動ガイドベーン10の半径方向
外側には、ステーベーン13を一体的に備えたう
ず巻ケーシング14が配置されている。
Furthermore, a spiral casing 14 integrally provided with a stay vane 13 is disposed radially outward of the movable guide vane 10.

一方、低圧段ランナ3の下方には、ステーベー
ン15を一体的に備えた下カバー16が配置さ
れ、この下カバー16の下端は吸出し管17に連
接されている。この下カバー16と上記高圧段側
の下カバー8との間には、低圧段ランナ3の上カ
バーの役目をも果たす中間スピードリング18が
組込まれており、この中間スピードリング18
は、複数個の返し羽根19を備え羽根と羽根との
間に返し流路が形成されている。
On the other hand, below the low-pressure stage runner 3, a lower cover 16 integrally provided with a stay vane 15 is arranged, and the lower end of this lower cover 16 is connected to a suction pipe 17. An intermediate speed ring 18 that also serves as an upper cover for the low pressure stage runner 3 is installed between this lower cover 16 and the lower cover 8 on the high pressure stage side.
is equipped with a plurality of return blades 19, and a return flow path is formed between the blades.

また、上記中間スピードリング18と下カバー
16の外側には、戻し流路20を内部に備えた外
筒21が配置されている。
Further, an outer cylinder 21 having a return passage 20 therein is disposed outside the intermediate speed ring 18 and the lower cover 16.

しかして、上記高圧段ランナ2のランナクラウ
ン2aと上カバー7との間には封水装置22が設
けられ、この封水装置22は上カバー7の側のカ
バーライナ23とランナクラウン2aの側の封止
環2bとの間のラビリンス通路24によつて構成
されている。同様にして、上記低圧段ランナ3の
ランナクラウン3aと中間スピードリング18と
の間にも封水装置25が設けられ、この封水装置
25は、中間スピードリング18とランナクラウ
ン3aの側の封止環3bとの間のラビリンス通路
26によつて構成されている。
A water sealing device 22 is provided between the runner crown 2a of the high pressure stage runner 2 and the upper cover 7, and this water sealing device 22 is connected to the cover liner 23 on the upper cover 7 side and the runner crown 2a on the side of the runner crown 2a. It is constituted by a labyrinth passage 24 between the sealing ring 2b and the sealing ring 2b. Similarly, a water sealing device 25 is also provided between the runner crown 3a of the low pressure stage runner 3 and the intermediate speed ring 18, and this water sealing device 25 is a seal between the intermediate speed ring 18 and the runner crown 3a. It is constituted by a labyrinth passage 26 between it and the stop ring 3b.

さらに、上記高圧段ランナ2の封水装置22の
半径方向内方には、高圧段排気室28が形成さ
れ、この排気室28と連通するように高圧段ラン
ナ2のランナクラウン2aには排気孔29が穿設
されている。上記排気室28の天井面には外部へ
排気可能な排気管路30の一端30aが接続され
ている。
Furthermore, a high-pressure stage exhaust chamber 28 is formed radially inward of the water sealing device 22 of the high-pressure stage runner 2, and an exhaust hole is formed in the runner crown 2a of the high-pressure stage runner 2 so as to communicate with this exhaust chamber 28. 29 is drilled. One end 30a of an exhaust pipe line 30 that can exhaust air to the outside is connected to the ceiling surface of the exhaust chamber 28.

同様にして、低圧段ランナ3の封水装置25の
半径方向内方には低圧段排気室31が形成され、
この排気室31と連通するように低圧段ランナ3
のランナクラウン3aであつて、ランナ出口端に
は排気孔32が穿設されている。上記排気室31
の天井面には排気通路33が開口しており、排気
通路33は、中間スピードリング18およびその
返し羽根19を横断して穿設され、排気管路34
を通じて外部へ排気できるようになつている。
Similarly, a low pressure stage exhaust chamber 31 is formed radially inward of the water sealing device 25 of the low pressure stage runner 3.
The low pressure stage runner 3 is connected to the exhaust chamber 31.
The runner crown 3a has an exhaust hole 32 formed at the runner outlet end. The above exhaust chamber 31
An exhaust passage 33 is opened on the ceiling surface of the engine, and the exhaust passage 33 is bored across the intermediate speed ring 18 and its return blades 19, and is connected to the exhaust pipe 34.
It is now possible to exhaust air to the outside through the

このように、高圧段ランナ2のランナクラウン
2aに、封水装置22、排気室28、排気孔29
及び排気管路30からなる排気系統を、低圧段ラ
ンナ3のランナクラウン3aに、封水装置25、
排気室31、排気孔32、排気通路33及び排気
管路34からなる排気系統を夫々設けることによ
り、高圧段ランナ室5及び高圧段ランナ室6内の
圧縮空気を排気管路30,34を開くことにより
排気し、これによつて排気渋滞をなくすことがで
きるよう構成されている。
In this way, the runner crown 2a of the high pressure stage runner 2 is provided with the water sealing device 22, the exhaust chamber 28, and the exhaust hole 29.
The exhaust system consisting of the exhaust pipe line 30 and the exhaust pipe line 30 is connected to the runner crown 3a of the low pressure stage runner 3, and the water sealing device 25,
By providing an exhaust system consisting of an exhaust chamber 31, an exhaust hole 32, an exhaust passage 33, and an exhaust pipe line 34, the compressed air in the high-pressure stage runner chamber 5 and high-pressure stage runner chamber 6 is released into the exhaust pipes 30, 34. The structure is such that the exhaust gas can be exhausted by this, thereby eliminating exhaust congestion.

次にこのように構成された2段ポンプ水車を使
つてポンプ起動をする場合の手順を説明する。
Next, the procedure for starting the pump using the two-stage pump turbine configured as described above will be explained.

第2図において、可動ガイドベーン10を全閉
した状態で図示を省略した圧縮空気供給管を通し
て高圧段ランナ室5内に圧縮空気を吹き込み、ラ
ンナ室5以下の水を返し羽根19、戻し流路20
を通して低圧段ランナ室6の下方へ押しやり、第
2図に示されたように、水面位WLが低圧段ラン
ナ3の直下に来るまで水面を押下げる。しかる
後、回転抵抗の減つた高圧段ランナ2および低圧
段ランナ3を比較的小容量の起動装置によつてポ
ンプ方向へ起動し、系統に並列するのと同時に排
気管路30より排気を開始する。
In FIG. 2, compressed air is blown into the high-pressure stage runner chamber 5 through a compressed air supply pipe (not shown) with the movable guide vane 10 fully closed, and the water below the runner chamber 5 is returned to the vane 19 and the return flow path. 20
The water is pushed downward through the low-pressure stage runner chamber 6, and the water surface is pushed down until the water level WL is directly below the low-pressure stage runner 3, as shown in FIG. Thereafter, the high-pressure stage runner 2 and low-pressure stage runner 3, which have reduced rotational resistance, are started toward the pump by a relatively small-capacity starting device, and at the same time as they are connected in parallel with the system, exhaust from the exhaust pipe line 30 is started. .

排気の進行につれて吸出し管17内の水位WL
は上昇し、低圧段ランナ3にかゝつた水はランナ
の遠心力によつて半径方向外方へ飛ばされ、第3
図に示すように、戻り流路20内に充水してゆ
き、この際比重の小さい空気は低圧段ランナ3の
中央部に滞留し、その外周が水壁で包み込まれた
状態になる。排気がさらに進行し水面が高圧段ラ
ンナ2に達すると、高圧段ランナ2の遠心力によ
り水は半径方向外方へ飛ばされるが、可動ガイド
ベーン10が全閉しているから、高圧段ランナ室
5内の水は、外側にはりつき水壁の表面が漸次半
径方向内方に進んできてついには第4図で示した
ような状態となる。しかして、高圧段ランナ室5
内の空気の容積が低圧段ランナ室6内に滞留して
いる空気の容積とほゞ等しくなつたところで低圧
段ランナ室6の側の排気管路34を開いて排気を
開始し、高圧段および低圧段の充水度のバランス
をとりながら排気を完了させたのち、可動ガイド
ベーン10を開いて揚水運転に入る。
As the exhaust progresses, the water level WL inside the suction pipe 17 increases.
rises, and the water that has accumulated on the low-pressure stage runner 3 is blown outward in the radial direction by the centrifugal force of the runner.
As shown in the figure, the return flow path 20 is filled with water, and at this time, air with low specific gravity remains in the center of the low-pressure stage runner 3, and its outer periphery is surrounded by a water wall. As the exhaust progresses further and the water surface reaches the high pressure stage runner 2, the centrifugal force of the high pressure stage runner 2 causes the water to be blown radially outward, but since the movable guide vane 10 is fully closed, the high pressure stage runner chamber The water inside 5 sticks to the outside, and the surface of the water wall gradually moves inward in the radial direction until it reaches the state shown in FIG. However, the high pressure stage runner chamber 5
When the volume of the air in the low pressure stage runner chamber 6 becomes approximately equal to the volume of the air remaining in the low pressure stage runner chamber 6, the exhaust pipe 34 on the side of the low pressure stage runner chamber 6 is opened to start exhausting, and the high pressure stage and After completing exhaustion while balancing the water filling level of the low pressure stage, the movable guide vane 10 is opened and water pumping operation begins.

上述した排気工程において、ややもすると、高
圧段ランナ室内に充水されていた水が流入する各
低圧段のランナ室において排気渋滞を起しがちで
あるが、本発明によれば、最高圧段ランナ以外の
低圧段ランナ3のランナクラウンに排気孔32を
穿設するとともに排気孔32の出口側に排気室3
1を設け、この排気室31から外部連通する排気
管路33を返し羽根19を横断して穿設し、さら
に上記排気室31の外側であつてランナクラウン
の背面側にラビリンス通路26を含む封水装置2
5を設けたから、低圧段のランナ室6内の圧縮空
気を排気渋滞を起すことなく外部へ排気すること
ができる。
In the above-mentioned exhaust process, exhaust congestion tends to occur in the runner chambers of each low pressure stage into which the water filled in the high pressure stage runner chamber flows, but according to the present invention, An exhaust hole 32 is bored in the runner crown of the low pressure stage runner 3 other than the runner, and an exhaust chamber 3 is provided on the outlet side of the exhaust hole 32.
1, an exhaust pipe line 33 communicating with the outside from the exhaust chamber 31 is bored across the return vane 19, and a seal including a labyrinth passage 26 is provided outside the exhaust chamber 31 and on the back side of the runner crown. water device 2
5, the compressed air in the runner chamber 6 of the low pressure stage can be exhausted to the outside without causing exhaust congestion.

上述した実施例においては、各段のランナのラ
ンナクラウンと固定側の上カバーまたは中間スピ
ードリングとの間に封水装置としてのラビリンス
通路24,26を設けたが、封水装置の他の実施
例としては、例えば第5図に示されるように、ラ
ンナクラウン3aの背面側であつて排気室31の
半径方向外側に複数個のフイン36を放射状に設
けておいても良い。このような実施例によれば、
ランナクラウン3aと中間スピードリング18と
の間のすき間を半径方向内方へ向かおうとする水
は、フイン36の遠心力による揚程で阻止され、
適切な封水効果を得ることができる。
In the embodiment described above, the labyrinth passages 24 and 26 as a water sealing device were provided between the runner crown of each stage runner and the upper cover on the fixed side or the intermediate speed ring, but other implementations of the water sealing device are possible. For example, as shown in FIG. 5, a plurality of fins 36 may be provided radially outside the exhaust chamber 31 on the back side of the runner crown 3a in the radial direction. According to such embodiments,
Water attempting to move radially inward through the gap between the runner crown 3a and the intermediate speed ring 18 is stopped by the lift caused by the centrifugal force of the fins 36.
Appropriate water sealing effect can be obtained.

また、各段のランナのランナクラウンに穿設さ
れる排気孔29,32は、第1図に、第1図に示
された実施例においては、水車主軸1の軸線と
ほゞ平行に設けられたが、第6図に示されるよう
に、例えば、低圧段ランナ3の場合について言え
ば、排気孔32の出口32oが入口32iよりも
主軸1に近い位置に開口するように、その中心線
が水車の主軸1に対して傾斜して設けても良い。
このように構成すると、入口と出口位置の半径差
に応じて排気室側から流水面側に向つて速度水頭
の差によつて揚程が生じるので封水装置によつて
完全に封水しきれず排気室内に流入してきた水を
流水面側に吐出する作用をして排気管路入口部の
閉塞を防ぐと共に、流水面側の排気孔入口迄ラン
ナ内が充水されても、その水が排気室内に流入す
ることをある程度防ぐ作用をし、ランナ室内の滞
留空気をより完全に排気することができる。
Further, in the embodiment shown in FIG. 1, exhaust holes 29 and 32 formed in the runner crown of each stage of runner are provided substantially parallel to the axis of the main shaft 1 of the water turbine. However, as shown in FIG. 6, for example, in the case of the low-pressure stage runner 3, the center line of the exhaust hole 32 is adjusted so that the outlet 32o of the exhaust hole 32 opens at a position closer to the main shaft 1 than the inlet 32i. It may be provided at an angle with respect to the main shaft 1 of the water turbine.
With this configuration, a lift is generated due to the difference in velocity head from the exhaust chamber side toward the flowing water surface depending on the radius difference between the inlet and outlet positions, so the water cannot be completely sealed by the water sealing device and the exhaust air cannot be completely sealed. It works by discharging the water that has flowed into the room toward the flowing water surface to prevent the exhaust pipe entrance from being blocked, and even if the inside of the runner is filled with water up to the exhaust hole entrance on the flowing water surface, the water will still flow into the exhaust chamber. This prevents the air from flowing into the runner chamber to some extent, and allows the stagnant air in the runner chamber to be more completely exhausted.

第7図は、ランナクラウンの排気孔32の出口
32oと中間スピードリング18を横断する排気
通路33の入口33iとの間に、その外周を中間
スピードリング18に対して一体的に固着され、
内周面との間に一定の環状隙間38を持つ円盤状
の仕切板40を設けた例である。このような実施
例によれば、排気室31内まで水が入つて来た場
合であつても水と空気の比重差と遠心力の作用に
よつて、水は排気室31内の外周側にはりついて
気水分離された状態になるため、水車主軸1に近
接した環状の隙間38からは空気だけが排気管路
33に導かれ、より完全な排気を行う事が可能と
なる。
In FIG. 7, the outer periphery is integrally fixed to the intermediate speed ring 18 between the outlet 32o of the exhaust hole 32 of the runner crown and the inlet 33i of the exhaust passage 33 that crosses the intermediate speed ring 18.
This is an example in which a disk-shaped partition plate 40 is provided with a constant annular gap 38 between it and the inner peripheral surface. According to this embodiment, even when water enters the exhaust chamber 31, the water is pushed to the outer circumferential side of the exhaust chamber 31 due to the difference in specific gravity between water and air and the action of centrifugal force. Since the air and water are stuck together and separated, only air is guided to the exhaust pipe 33 from the annular gap 38 close to the main shaft 1 of the water turbine, making it possible to perform more complete exhaustion.

第8図は排気室31内における排気管路41の
形状をL字状パイプにし、その開口端41aを排
気室31の最内周最上部としたもので、排気室3
1内で水は外周部に、又空気は内周側且つ上方に
分離されるという原理に基き、より完全な排気を
可能とするものである。
In FIG. 8, the shape of the exhaust pipe line 41 in the exhaust chamber 31 is an L-shaped pipe, and the opening end 41a is set at the top of the innermost circumference of the exhaust chamber 31.
Based on the principle that water is separated into the outer periphery and air is separated into the inner periphery and upward within the chamber, more complete exhaustion is possible.

なお、上述した実施例においては、高圧段ラン
ナの側にのみ可動ガイドベーンを設けた2段ポン
プ水車に対して本発明を適用したが、低圧段ラン
ナの側にも可動ガイドベーンを備えたものについ
ても適用可能であり、また、2段ポンプ水車に限
られることなく、3段以上のポンプ水車に対して
も適用可能である。
In the above-mentioned embodiments, the present invention was applied to a two-stage pump turbine in which a movable guide vane was provided only on the high-pressure stage runner side, but a movable guide vane was also provided on the low-pressure stage runner side. The invention is also applicable not only to two-stage pump-turbines but also to three-stage or more pump-turbines.

本発明は上記のような構成であるので、水面押
上げ状態下のポンプ起動あるいは調相運転時に、
特に低圧段ランナにおいて排気渋滞を起こすこと
なくランナ室内の空気を排気することができ、こ
れによつて流路形状が複雑な多段ポンプ水車にお
いて、系統に悪影響を与えることなく円滑なポン
プ起動が行なえ、更に系統全体の力率を改善する
調相運転が可能となるといつた効果がある。
Since the present invention has the above-mentioned configuration, when the pump is started or when the phase adjustment operation is performed under conditions where the water surface is pushed up,
In particular, the air in the runner chamber can be exhausted without causing exhaust congestion in low-pressure stage runners, and this allows smooth pump startup without adversely affecting the system in multi-stage pump turbines with complex flow path shapes. Furthermore, it is possible to perform phase adjustment operation that improves the power factor of the entire system.

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

第1図は本発明を適用した2段ポンプ水車を示
した縦断面図、第2図乃至第4図は水面押下げ状
態下でポンプ起動運転の経過を示した縦断面図、
第5図乃至第8図は封水装置の他の実施例を低圧
段ランナのランナクラウンに設けた例を示した断
面図である。 1……主軸、2……高圧段ランナ、3……低圧
段ランナ、5……高圧段ランナ室、6……低圧段
ランナ室、7……上カバー、8……下カバー、1
0………可動ガイドベーン、16……下カバー、
18……中間スピードリング、20……戻し流
路、22,25……封水装置、24,26……ラ
ビリンス通路、28,31……排気室、29,3
2……排気孔、30,34……排気管路。
FIG. 1 is a vertical cross-sectional view showing a two-stage pump turbine to which the present invention is applied, and FIGS. 2 to 4 are vertical cross-sectional views showing the progress of pump startup operation under a state in which the water surface is depressed.
5 to 8 are cross-sectional views showing other embodiments of the water sealing device provided on the runner crown of the low pressure stage runner. 1... Main shaft, 2... High pressure stage runner, 3... Low pressure stage runner, 5... High pressure stage runner chamber, 6... Low pressure stage runner chamber, 7... Upper cover, 8... Lower cover, 1
0......Movable guide vane, 16...Lower cover,
18... Intermediate speed ring, 20... Return channel, 22, 25... Water sealing device, 24, 26... Labyrinth passage, 28, 31... Exhaust chamber, 29, 3
2...exhaust hole, 30, 34...exhaust pipe line.

Claims (1)

【特許請求の範囲】 1 前段のランナ室と次段のランナ室とが返し羽
根で形成された返し通路で連絡されるようにした
複数段のランナ室内に水車主軸によつて支持され
た複数個のランナを設け、少なくとも最高圧段の
ランナ室の外側に可動ガイドベーンを設けるとと
もに、このランナクラウンにランナ流路側より背
面側に貫通する排気孔と、この排気孔の出口側に
排気室を夫々設け、この排気室から外部へ連通す
る排気管路を穿設し、さらに上記排気室の半径方
向外周部に封水装置を設けた多段水力機械であつ
て、上記最高圧段ランナ以外の低圧段ランナのラ
ンナクラウンにランナ流路側より背面側に貫通す
る排気孔を設け、この排気孔の出口側に排気室を
設け、この排気室から外部へ連通する排気管路を
上記返し羽根を横断して穿設し、さらに上記排気
室の半径方向外周部に封水装置を設けたことを特
徴とする多段水力機械の排気装置。 2 封水装置は、ランナとランナクラウンと中間
スピードリングとの間に形成されたラビリンス通
路によつて構成されていることを特徴とする特許
請求の範囲第1項記載の多段水力機械の排気装
置。 3 封水装置は、ランナクラウンの背面側に放射
状に配置された複数個のフインによつて構成され
ていることを特徴とする特許請求の範囲第1項記
載の多段水力機械の排気装置。 4 ランナクラウンに穿設される排気孔は、その
出口側が入口側よりも半径方向内方へ位置するよ
うに孔の中心線が水車主軸の軸線に対して傾斜し
て設けられたことを特徴とする特許請求の範囲第
1項記載の多段水力機械の排気装置。
[Scope of Claims] 1. A plurality of runner chambers supported by a main shaft of a water turbine in a plurality of runner chambers in which a previous stage runner chamber and a next stage runner chamber are connected by a return passage formed by return blades. A runner is provided, a movable guide vane is provided on the outside of at least the runner chamber of the highest pressure stage, an exhaust hole is provided in the runner crown that penetrates from the runner flow path side to the rear side, and an exhaust chamber is provided on the outlet side of this exhaust hole. A multi-stage hydraulic machine, which has an exhaust pipe connected to the outside from the exhaust chamber, and is further provided with a water sealing device on the radial outer circumference of the exhaust chamber, and is equipped with a low-pressure stage other than the highest-pressure stage runner. An exhaust hole is provided in the runner crown of the runner that penetrates from the runner flow path side to the back side, an exhaust chamber is provided on the outlet side of this exhaust hole, and an exhaust pipe line communicating from this exhaust chamber to the outside is connected across the return vane. 1. An exhaust system for a multi-stage hydraulic machine, characterized in that a water sealing device is provided on the radial outer periphery of the exhaust chamber. 2. The exhaust system for a multi-stage hydraulic machine according to claim 1, wherein the water sealing device is constituted by a labyrinth passage formed between a runner, a runner crown, and an intermediate speed ring. . 3. The exhaust device for a multi-stage hydraulic machine according to claim 1, wherein the water sealing device is constituted by a plurality of fins arranged radially on the back side of the runner crown. 4 The exhaust hole bored in the runner crown is characterized in that the center line of the hole is inclined with respect to the axis of the main shaft of the water turbine so that the outlet side is located radially inward than the inlet side. An exhaust system for a multi-stage hydraulic machine according to claim 1.
JP7247080A 1979-10-29 1980-05-30 Exhauster in multiplestage hydraulic machinery Granted JPS57364A (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
JP7247080A JPS57364A (en) 1980-05-30 1980-05-30 Exhauster in multiplestage hydraulic machinery
US06/199,628 US4406577A (en) 1979-10-29 1980-10-22 Multi-stage hydraulic machine and a method of operating same
DE19803040468 DE3040468A1 (en) 1979-10-29 1980-10-27 MULTI-STAGE HYDROPOWER
CH8011/80A CH658495A5 (en) 1979-10-29 1980-10-28 MULTI-STAGE HYDROPOWER.
US06/495,945 US4547123A (en) 1979-10-29 1983-05-19 Multi-stage hydraulic machine and method of operating same

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP7247080A JPS57364A (en) 1980-05-30 1980-05-30 Exhauster in multiplestage hydraulic machinery

Publications (2)

Publication Number Publication Date
JPS57364A JPS57364A (en) 1982-01-05
JPS634024B2 true JPS634024B2 (en) 1988-01-27

Family

ID=13490226

Family Applications (1)

Application Number Title Priority Date Filing Date
JP7247080A Granted JPS57364A (en) 1979-10-29 1980-05-30 Exhauster in multiplestage hydraulic machinery

Country Status (1)

Country Link
JP (1) JPS57364A (en)

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5249005U (en) * 1975-10-03 1977-04-07
JPS5517604A (en) * 1978-07-21 1980-02-07 Hitachi Ltd Method of and device for operating hydraulic turbine or pump hydraulic turbine

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5249005U (en) * 1975-10-03 1977-04-07
JPS5517604A (en) * 1978-07-21 1980-02-07 Hitachi Ltd Method of and device for operating hydraulic turbine or pump hydraulic turbine

Also Published As

Publication number Publication date
JPS57364A (en) 1982-01-05

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