JPH10299410A - Moisture discharging structure of steam turbine - Google Patents

Moisture discharging structure of steam turbine

Info

Publication number
JPH10299410A
JPH10299410A JP10425097A JP10425097A JPH10299410A JP H10299410 A JPH10299410 A JP H10299410A JP 10425097 A JP10425097 A JP 10425097A JP 10425097 A JP10425097 A JP 10425097A JP H10299410 A JPH10299410 A JP H10299410A
Authority
JP
Japan
Prior art keywords
moisture
outer ring
slit
steam turbine
drain
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
JP10425097A
Other languages
Japanese (ja)
Inventor
Koji Ishibashi
光司 石橋
Norio Yasugadaira
紀雄 安ヶ平
Yoshiaki Yamazaki
義昭 山崎
Yasuaki Sawamura
保昭 澤村
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.)
Hitachi Ltd
Original Assignee
Hitachi 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 Hitachi Ltd filed Critical Hitachi Ltd
Priority to JP10425097A priority Critical patent/JPH10299410A/en
Publication of JPH10299410A publication Critical patent/JPH10299410A/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/32Collecting of condensation water; Drainage ; Removing solid particles

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

PROBLEM TO BE SOLVED: To prevent erosion of a dynamic blade from occurring, by installing a moisture induction groove, which promotes the drain discharging downstream from the back edge end of a stator blade, on an inner wall of an external ring which holds the stator blade of a stream turbine, and by structuring the moisture induction groove such that its width is widened in the flowing direction of fluid or its depth is slanted. SOLUTION: In a stream turbine, plural stator blades 3 are radially arranged in the enlarged passage, these stator blades 3 are held by an external and an internal ring forming the enlarged passage, and a dynamic blade is installed downstream of these static blades 3. On the outer surface of the inflow end downstream of the outer ring, a annual circumferencial slit 7 is formed, and in this case, a moisture induction groove 9 which expands from a back edge end 8 of the stator blade 3 to the circumferencial slit 7 is installed along the flow direction of the fluid from the back edge end 8 of each stator blade 3 to the end of the outer ring. Therefore, drain gathered on a inner wall 10 of the outer ring is flown down by the moisture induction groove 9, and all drain are lead to the circumferencial slit 7, and are discharged from the slit 7 in an annular groove on outside of the turbine passage.

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【発明の属する技術分野】本発明は蒸気タービンの湿分
排出構造に関する。
The present invention relates to a structure for discharging moisture from a steam turbine.

【0002】[0002]

【従来の技術】大容量の蒸気タービンでは、タービン通
路内の湿り蒸気中の液滴が動翼に衝突して発生するエロ
ージョンを防止するため、タービン通路から水滴や水膜
などの湿分を排出する構造が設けられている。
2. Description of the Related Art In a large-capacity steam turbine, moisture, such as water droplets and a water film, is discharged from a turbine passage in order to prevent erosion caused by droplets in wet steam in a turbine passage colliding with a rotor blade. Is provided.

【0003】図8は蒸気タービンの低圧最終段に設けら
れたドレン排出構造の従来例を示した。図8で、動翼5
の前方に配置される静翼3を保持する外輪2と、この外
輪2の下流側の動翼5先端の流入端外周部に環状の周方
向スリット7が形成されている。
FIG. 8 shows a conventional example of a drain discharge structure provided in a low-pressure final stage of a steam turbine. In FIG.
And an outer circumferential ring 7 which holds a stationary blade 3 disposed in front of the outer ring 2 and an annular circumferential slit 7 is formed in the outer peripheral portion of the inflow end at the tip of the moving blade 5 downstream of the outer ring 2.

【0004】そして、外輪2の内壁10に集積したドレ
ン11が蒸気流により下流側に流動して、周方向スリッ
ト7からタービン通路外の環状溝12に排出され、さら
に孔13より図示しない復水器などの低圧力側に排出さ
れるようになっている。
The drain 11 accumulated on the inner wall 10 of the outer ring 2 flows downstream by the steam flow, is discharged from the circumferential slit 7 into an annular groove 12 outside the turbine passage, and is further condensed through a hole 13 (not shown). It is discharged to the low pressure side of the vessel.

【0005】[0005]

【発明が解決しようとする課題】以上述べた構造で、外
輪2の内壁10では、図9に詳細に示すように、低圧部
で凝縮したドレン11は蒸気に比べて慣性が大きいため
に静翼3の腹面15に押し付けられて流れる。また、腹
面15に集中したドレン11の一部は翼列内の二次流れ
によって翼背面16にも到達する。
In the above-described structure, on the inner wall 10 of the outer race 2, as shown in detail in FIG. 9, the drain 11 condensed in the low pressure portion has a higher inertia than the steam, so that the stationary blade 3 is pressed against the abdominal surface 15 and flows. Further, a part of the drain 11 concentrated on the abdominal surface 15 reaches the blade back surface 16 by the secondary flow in the cascade.

【0006】その結果、ドレン11は静翼3の腹面15
及び背面16に集中して、静翼3の翼後縁端8に到達す
る。翼後縁端8には翼厚みがあり、ドレン11の水膜流
の一部は引き裂かれて水滴17となる。この水滴17は
遠心力により一部は再び外輪2の内壁10に付着するも
のの、静翼3の翼後縁端8より初速度ゼロで流出するた
め遠心力が小さく、大部分は蒸気流とともに流下し、周
方向スリット7より排出することが困難になっている。
As a result, the drain 11 is formed on the abdominal surface 15 of the stationary blade 3.
Then, it concentrates on the back surface 16 and reaches the trailing edge 8 of the vane 3. The wing trailing edge 8 has a wing thickness, and a part of the water film flow of the drain 11 is torn to become a water droplet 17. Although a part of the water droplet 17 adheres again to the inner wall 10 of the outer ring 2 due to the centrifugal force, the water droplet 17 flows out from the trailing edge 8 of the vane 3 at an initial velocity of zero, so that the centrifugal force is small, and most of the water droplet flows down with the steam flow. However, it is difficult to discharge from the circumferential slit 7.

【0007】その結果、外輪2の内壁10に沿って流れ
ているドレン11の一部は、周方向スリット7に到達す
る前に外輪2の内壁10から離脱し、後方に配置されて
いる動翼5の先端部に水滴17が集中して流下するた
め、動翼5の先端部での部分的なエロージョンの発生が
問題となっていた。
As a result, a part of the drain 11 flowing along the inner wall 10 of the outer ring 2 separates from the inner wall 10 of the outer ring 2 before reaching the circumferential slit 7, and the rotor blades arranged rearward Since the water droplets 17 are concentrated and flow down to the tip of the blade 5, the occurrence of partial erosion at the tip of the bucket 5 has been a problem.

【0008】また、周方向スリット7は極力蒸気が漏れ
ないように狭いギャップとなっているため、周方向スリ
ット7に流入したドレン11は水膜となって周方向スリ
ット7を閉塞し、流入量と排出量のバランスが保てなく
なる。この結果、周方向スリット7で排出されなかった
ドレン11は蒸気流とともに動翼5へと流下し、エロー
ジョン発生の原因になる。
Further, since the circumferential slit 7 has a narrow gap so as to prevent steam from leaking as much as possible, the drain 11 flowing into the circumferential slit 7 becomes a water film and closes the circumferential slit 7, so that the amount of inflow is reduced. And the balance of emissions cannot be maintained. As a result, the drain 11 not discharged by the circumferential slit 7 flows down to the rotor blade 5 together with the steam flow, which causes erosion.

【0009】本発明の目的は、外輪の内壁に沿って流れ
るドレンを通路外に確実に排出し、これにより動翼のエ
ロージョン発生を有効に防止することができる蒸気ター
ビンのドレン排出構造を提供することにある。
An object of the present invention is to provide a drain discharge structure for a steam turbine which can reliably discharge drain flowing along the inner wall of an outer ring to the outside of a passage, thereby effectively preventing erosion of a moving blade. It is in.

【0010】[0010]

【課題を解決するための手段】上記の課題を解決するた
めに、本発明は、蒸気タービンの静翼を保持する外輪の
内壁に、前記静翼の後縁端より下流にドレン排出を促進
させる湿分誘導溝を設け、かつ前記静翼後縁から前記周
方向スリットまで延びている湿分誘導溝の形状を流体の
流れ方向に徐々に拡幅あるいは溝深さを傾斜されたもの
である。
SUMMARY OF THE INVENTION In order to solve the above-mentioned problems, the present invention promotes drain discharge on the inner wall of an outer ring holding a stationary blade of a steam turbine, downstream of the trailing edge of the stationary blade. A moisture guiding groove is provided, and the shape of the moisture guiding groove extending from the trailing edge of the stationary blade to the circumferential slit is gradually widened or inclined in the flow direction of the fluid.

【0011】更に周方向スリットへ導かれた湿分が水膜
となって周方向スリットを閉塞しないよう、スリット長
さを縮小したり、周方向スリットに沿って複数の水膜防
止の細溝を設けたものである。
Further, the length of the slit is reduced or a plurality of narrow grooves for preventing water film are formed along the circumferential slit so that moisture guided to the circumferential slit does not block the circumferential slit as a water film. It is provided.

【0012】[0012]

【発明の実施の形態】以下図示した実用例に基づいて本
発明を詳細に説明する。図1には蒸気タービンに採用さ
れている段落部の部分断面が縦断面図で示されている。
この段落部は、タービン内ケーシング1に保持される外
輪2及び静翼3を保持している内輪4で拡大流路を形成
しており、この拡大流路内に静翼3が放射状に複数本配
置されている。静翼3は、拡大流路を形成する外輪2と
内輪4により保持されている。また、静翼3の下流には
動翼5がディスク6に植えられている。動翼5の前方に
配置される静翼3を保持する外輪2と、この外輪2の下
流側の動翼5の流入端外周部に環状の周方向スリット7
が形成されている。そして、静翼3の後縁端8から周方
向スリットまで延びている湿分誘導溝が、図2および図
3に示すように各静翼3の翼後縁端8から外輪2の端部
まで流体の流れ方向に沿って設けられている。
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS The present invention will be described below in detail with reference to the illustrated practical examples. FIG. 1 is a longitudinal sectional view showing a partial section of a paragraph section employed in a steam turbine.
In this paragraph, an enlarged flow path is formed by the outer ring 2 held by the turbine inner casing 1 and the inner ring 4 holding the stationary blades 3. Are located. The stationary blade 3 is held by the outer ring 2 and the inner ring 4 forming an enlarged flow path. A moving blade 5 is planted on a disk 6 downstream of the stationary blade 3. An outer ring 2 that holds a stationary blade 3 disposed in front of a moving blade 5, and an annular circumferential slit 7 in an outer peripheral portion of an inflow end of the moving blade 5 downstream of the outer ring 2.
Are formed. A moisture guiding groove extending from the trailing edge 8 of the stationary blade 3 to the circumferential slit extends from the trailing edge 8 of each stationary blade 3 to the end of the outer ring 2 as shown in FIGS. It is provided along the flow direction of the fluid.

【0013】このような本実施例の構成によると、外輪
2の内壁10上に静翼3の翼後縁端8から周方向スリッ
ト7まで延びている湿分誘導溝9を設けたので、外輪2
の内壁10に集合したドレン11は前記湿分誘導溝9に
よって流下し、外輪2の内壁10に集合したドレンをす
べてドレン排出用の周方向スリット7に導くことができ
る。そして、周方向スリット7からタービン通路外の環
状溝12に排出され、さらに孔13より図示しない復水
器などの低圧力側に排出される。
According to the configuration of this embodiment, the moisture guide groove 9 extending from the trailing edge 8 of the stator vane 3 to the circumferential slit 7 is provided on the inner wall 10 of the outer ring 2. 2
The drain 11 gathered on the inner wall 10 of the outer ring 2 flows down by the moisture guiding groove 9, and all the drain gathered on the inner wall 10 of the outer ring 2 can be guided to the circumferential slit 7 for drain discharge. Then, the gas is discharged from the circumferential slit 7 into the annular groove 12 outside the turbine passage, and further discharged through the hole 13 to a low pressure side such as a condenser (not shown).

【0014】したがって、従来の構造と異なり、外輪2
の内壁10に集積したドレン11の一部が後方に配置さ
れている動翼5の先端部に到達することが有効に回避さ
れ、動翼5の先端部にエロージョンが集中的に発生する
ことを防止できるようになる。
Therefore, unlike the conventional structure, the outer ring 2
Part of the drain 11 accumulated on the inner wall 10 of the moving blade 5 is effectively prevented from reaching the tip of the moving blade 5 disposed behind, and erosion is intensively generated at the tip of the moving blade 5. Can be prevented.

【0015】次に図4により、本発明の他の実施例につ
いて説明する。静翼3の翼後縁端8から周方向スリット
7まで延びている湿分誘導溝9を、周方向スリット7側
へ向かうとともに溝幅が拡幅していくような構造にする
ことによって、湿分誘導溝9内に流入するドレン11の
量が増加しても、周方向スリット7に到達する際には湿
分誘導溝9の溝幅が拡幅しているため周方向スリット7
の局所にドレンが集中せず、液膜による周方向スリット
7の閉塞を防止できる。そのため、周方向スリット7か
らドレンが溢れることがないので、水滴の飛散がなく動
翼5の先端部にエロージョンが発生することを防止でき
る。
Next, another embodiment of the present invention will be described with reference to FIG. The moisture guiding groove 9 extending from the trailing edge 8 of the stator vane 3 to the circumferential slit 7 has a structure in which the groove width is increased toward the circumferential slit 7 and the groove width is increased. Even when the amount of the drain 11 flowing into the guide groove 9 increases, when the moisture guide groove 9 reaches the circumferential slit 7, the groove width of the moisture guide groove 9 is increased, so that the circumferential slit 7 is increased.
The drain does not concentrate on the local area, and the closure of the circumferential slit 7 by the liquid film can be prevented. Therefore, since the drain does not overflow from the circumferential slit 7, there is no scattering of water droplets, and it is possible to prevent erosion from being generated at the tip of the bucket 5.

【0016】また図5に示すように、湿分誘導溝9の深
さを周方向スリット7側へ向かうとともに溝深さが深く
なっていくような構造にすることによっても、前述の効
果を得ることができ、より確実にドレンを周方向スリッ
ト7へ排出することが可能となる。
Further, as shown in FIG. 5, the above-mentioned effect can also be obtained by adopting a structure in which the depth of the moisture guiding groove 9 is increased toward the circumferential slit 7 and the groove depth is increased. It is possible to discharge the drain to the circumferential slit 7 more reliably.

【0017】次に図6により、本発明の他の実施例につ
いて説明する。周方向スリット7を形成する外輪2の端
部上の湿分誘導溝9出口部などの側壁にスリットの出口
方向へ向かった複数の水膜防止スリット14を設けるこ
とにより、湿分誘導溝9に流下したドレンが周方向スリ
ット7へ流入した際に水膜となることがないため周方向
スリット7を閉塞することを防止できる。また、湿分誘
導溝9出口部のみスリット面積を広くして、他の部分の
スリット幅は従来と同様もしくは狭くすることができる
ため、ドレンとともに排出される蒸気の量を減らすこと
ができ、タービン性能を向上できる。
Next, another embodiment of the present invention will be described with reference to FIG. By providing a plurality of water film preventing slits 14 directed toward the exit direction of the slit on a side wall such as an exit portion of the moisture guiding groove 9 on an end portion of the outer ring 2 forming the circumferential slit 7, the moisture guiding groove 9 is formed. When the drained water flows into the circumferential slit 7, it does not become a water film, so that it is possible to prevent the circumferential slit 7 from being closed. Further, since the slit area can be increased only at the outlet of the moisture guiding groove 9 and the slit width of the other portions can be reduced or reduced as in the related art, the amount of steam discharged together with the drain can be reduced, and Performance can be improved.

【0018】次に図7により、本発明の他の実施例につ
いて説明する。周方向スリット7の周方向長さを短くす
ることにより、周方向スリット7へ流入したドレンが液
膜となる領域が減少するため、周方向スリット7を閉塞
することがなく、より確実にドレンを排出することが可
能となる。
Next, another embodiment of the present invention will be described with reference to FIG. By reducing the circumferential length of the circumferential slit 7, the area where the drain flowing into the circumferential slit 7 becomes a liquid film is reduced, so that the circumferential slit 7 is not blocked and the drain can be more reliably discharged. It becomes possible to discharge.

【0019】以上述べたことを実施することにより、周
方向スリット7からドレンを効率よく排出できるため、
周方向スリット7からドレンが溢れることもなく水滴が
飛散しない。よって、動翼5の先端部へのエロージョン
の発生を防止することができる。
By performing the above, drain can be efficiently discharged from the circumferential slit 7.
The drain does not overflow from the circumferential slit 7 and water droplets do not scatter. Therefore, it is possible to prevent erosion from occurring at the tip of the bucket 5.

【0020】[0020]

【発明の効果】本発明によれば、蒸気タービンにおい
て、外輪の内壁に沿って流れるドレンを通路外に確実に
排出することができ、これにより動翼のエロージョン発
生を有効に防止することができる。
According to the present invention, in the steam turbine, the drain flowing along the inner wall of the outer ring can be reliably discharged to the outside of the passage, whereby the erosion of the rotor blade can be effectively prevented. .

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

【図1】本発明の蒸気タービンの段落を示す部分縦断面
図。
FIG. 1 is a partial longitudinal sectional view showing a stage of a steam turbine of the present invention.

【図2】本発明の湿分誘導溝を示す説明図。FIG. 2 is an explanatory view showing a moisture guiding groove of the present invention.

【図3】本発明の湿分誘導溝を示す縦断面図。FIG. 3 is a longitudinal sectional view showing a moisture guiding groove of the present invention.

【図4】本発明の他の実施例を示す湿分誘導溝の説明
図。
FIG. 4 is an explanatory view of a moisture guiding groove showing another embodiment of the present invention.

【図5】本発明の他の実施例を示す湿分誘導溝の縦断面
図。
FIG. 5 is a longitudinal sectional view of a moisture guiding groove showing another embodiment of the present invention.

【図6】本発明の他の実施例を示す水膜防止スリットの
説明図。
FIG. 6 is an explanatory view of a water film prevention slit showing another embodiment of the present invention.

【図7】本発明の他の実施例を示す周方向スリットの縦
断面図。
FIG. 7 is a longitudinal sectional view of a circumferential slit showing another embodiment of the present invention.

【図8】従来の蒸気タービンの湿分排出構造を示す縦断
面図。
FIG. 8 is a longitudinal sectional view showing a conventional moisture discharge structure of a steam turbine.

【図9】図8における湿分の説明図。FIG. 9 is an explanatory diagram of moisture in FIG. 8;

【符号の説明】[Explanation of symbols]

1…ケーシング、2…外輪、3…静翼、4…内輪、5…
動翼、6…ディスク、7…周方向スリット、8…動翼縁
端、9…湿分誘導溝、10…内壁、11…ドレン、12
…環状溝、13…孔、14…水膜防止スリット、15…
腹面、16…背面、17…水滴。
DESCRIPTION OF SYMBOLS 1 ... Casing, 2 ... Outer ring, 3 ... Static wing, 4 ... Inner ring, 5 ...
Rotor blade, 6 disk, 7 peripheral slit, 8 blade edge, 9 moisture guiding groove, 10 inner wall, 11 drain, 12
... annular groove, 13 ... hole, 14 ... water film prevention slit, 15 ...
Abdominal surface, 16 ... rear surface, 17 ... water droplets.

───────────────────────────────────────────────────── フロントページの続き (72)発明者 澤村 保昭 茨城県日立市大みか町七丁目2番1号 株 式会社日立製作所電力・電機開発本部内 ──────────────────────────────────────────────────の Continued on the front page (72) Inventor Yasuaki Sawamura 7-2-1, Omika-cho, Hitachi City, Ibaraki Pref. Hitachi, Ltd. Power & Electricity Development Division

Claims (5)

【特許請求の範囲】[Claims] 【請求項1】蒸気タービンの複数の静翼が固定されてい
る外輪の下流側に復水器などの低圧部分に湿分を排出す
る周方向スリットを設けた湿分排出機構において、前記
複数の静翼を保持する外輪の内壁に静翼の後縁から外輪
の端部まで湿分誘導溝を設けたことを特徴とする蒸気タ
ービンの湿分排出構造。
1. A moisture discharging mechanism provided with a circumferential slit for discharging moisture to a low pressure portion such as a condenser downstream of an outer ring to which a plurality of stationary blades of a steam turbine are fixed. A moisture discharge structure for a steam turbine, wherein a moisture guide groove is provided on an inner wall of an outer ring holding a stationary blade from a trailing edge of the stationary blade to an end of the outer ring.
【請求項2】前記湿分誘導溝は静翼の後縁から外輪の端
部まで延びると共に溝幅が徐々に変化する請求項1に記
載の蒸気タービンの湿分排出構造。
2. The moisture discharge structure for a steam turbine according to claim 1, wherein the moisture guide groove extends from a trailing edge of the stationary blade to an end of the outer ring, and the groove width gradually changes.
【請求項3】前記湿分誘導溝は静翼の後縁から外輪の端
部まで延びると共に溝深さが徐々に変化するようにした
請求項1に記載の蒸気タービンの湿分排出構造。
3. A moisture discharge structure for a steam turbine according to claim 1, wherein said moisture guide groove extends from the trailing edge of the stationary blade to the end of the outer ring, and the groove depth is gradually changed.
【請求項4】前記湿分誘導溝の端部である前記周方向ス
リットを形成する側壁に複数の水膜防止スリットを設け
た請求項1に記載の蒸気タービンの湿分排出構造。
4. The moisture discharging structure of a steam turbine according to claim 1, wherein a plurality of water film preventing slits are provided on a side wall forming the circumferential slit, which is an end of the moisture guiding groove.
【請求項5】前記湿分を排出する周方向スリットの周方
向長さを短くすることにより水膜停滞領域を小さくした
請求項1に記載の蒸気タービンの湿分排出構造。
5. The moisture discharge structure for a steam turbine according to claim 1, wherein a water film stagnation region is reduced by shortening a circumferential length of the circumferential slit for discharging the moisture.
JP10425097A 1997-04-22 1997-04-22 Moisture discharging structure of steam turbine Pending JPH10299410A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP10425097A JPH10299410A (en) 1997-04-22 1997-04-22 Moisture discharging structure of steam turbine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP10425097A JPH10299410A (en) 1997-04-22 1997-04-22 Moisture discharging structure of steam turbine

Publications (1)

Publication Number Publication Date
JPH10299410A true JPH10299410A (en) 1998-11-10

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
JP10425097A Pending JPH10299410A (en) 1997-04-22 1997-04-22 Moisture discharging structure of steam turbine

Country Status (1)

Country Link
JP (1) JPH10299410A (en)

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JP2016017509A (en) * 2014-07-11 2016-02-01 三菱日立パワーシステムズ株式会社 Steam turbine seal device and steam turbine system
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