JP2600955B2 - Double-flow steam turbine - Google Patents
Double-flow steam turbineInfo
- Publication number
- JP2600955B2 JP2600955B2 JP2048214A JP4821490A JP2600955B2 JP 2600955 B2 JP2600955 B2 JP 2600955B2 JP 2048214 A JP2048214 A JP 2048214A JP 4821490 A JP4821490 A JP 4821490A JP 2600955 B2 JP2600955 B2 JP 2600955B2
- Authority
- JP
- Japan
- Prior art keywords
- steam
- double
- stationary blade
- sides
- flow
- 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 - Lifetime
Links
Description
【発明の詳細な説明】 〔産業上の利用分野〕 本発明は、ケーシングの蒸気入口から流入した蒸気が
2方向に分れて蒸気入口の両側にある段落に通流して膨
脹する複流形蒸気タービン、特に蒸気流入部の第1段の
静翼列の構造に関する。Description: BACKGROUND OF THE INVENTION The present invention relates to a double-flow steam turbine in which steam flowing from a steam inlet of a casing is divided into two directions and flows through paragraphs on both sides of the steam inlet to expand. In particular, the present invention relates to the structure of a first-stage stationary blade row of a steam inflow section.
複流形蒸気タービンは、ケーシングの蒸気入口から流
入した蒸気が2方向に分れて蒸気入口の両側にあるケー
シングに備えられた静翼列の静翼と車軸に備えられる動
翼列の動翼とで形成される複数段の段落を通流して仕事
をするものであり、蒸気流入部の第1段の静翼列部の構
造として、第1段の静翼列に流入する蒸気が静翼列の先
端とこれに対向する車軸との間の隙間から洩れるのを防
止するために第3図(特開平1−163405号参照)および
第4図に示すものが知られている。The double-flow steam turbine is configured such that steam flowing from a steam inlet of a casing is divided into two directions, and a stationary blade of a stationary blade row provided on a casing on both sides of the steam inlet and a rotor blade of a rotor row provided on an axle. Work is performed by flowing through a plurality of stages of stages formed by the steam turbine. As a structure of the first stage stationary blade row portion of the steam inflow section, steam flowing into the first stage stationary blade row is FIGS. 3 (see Japanese Patent Application Laid-Open No. 1-163405) and FIG. 4 are known to prevent leakage from the gap between the front end of the vehicle and an axle facing the front end.
第3図においてケーシング1内にはケーシング1の蒸
気入口2の両側に静翼3からなる静翼列が複数列設けら
れている。車軸4には前記静翼列の静翼と段落を形成す
る動翼5からなる複数列の動翼列が設けられている。6,
7は蒸気流入部の第1段の静翼列であり、静翼列6,7の静
翼の先端を覆ってシユラウドプレート8,9が取付けら
れ、シユラウドプレート8と9との間を覆ってばね10を
介してボルト11で締付けられるブリッジ片12が取付けら
れている。In FIG. 3, a plurality of rows of stationary blades including stationary blades 3 are provided in the casing 1 on both sides of the steam inlet 2 of the casing 1. The axle 4 is provided with a plurality of rows of moving blade rows including the stationary blades of the stationary blade row and the moving blades 5 forming a paragraph. 6,
Reference numeral 7 denotes a first-stage stationary blade row of the steam inflow section, and shroud plates 8 and 9 are attached so as to cover the tips of the stationary blades of the stationary blade rows 6 and 7, and a gap between the shroud plates 8 and 9 is provided. A bridge piece 12 is mounted over which is fastened with a bolt 11 via a spring 10.
このような構造により蒸気入口2から流入した蒸気は
ブリッジ片12と、これに連結されたシユラウドプレート
8,9とにより2方向に分れて蒸気入口2の両側の段落に
流れる。この際ブリッジ片12とシユラウドプレート8,9
とにより第1段の静翼列の先端と車軸との隙間から第1
段の静翼列に流入する蒸気が洩れるのを防止している。With such a structure, the steam flowing from the steam inlet 2 is connected to the bridge piece 12 and the shroud plate connected thereto.
The steam is divided into two directions by 8, 9 and flows into the paragraphs on both sides of the steam inlet 2. At this time, the bridge piece 12 and the shroud plates 8, 9
From the gap between the tip of the first stage vane row and the axle,
This prevents the steam flowing into the stator blade row of the stage from leaking.
第4図においては第1段の静翼列6,7のシユラウド13,
14にラビリンスフイン15を設け、このラビリンスフイン
15と隙間を持たせて静翼列5,6の先端を覆うフローガイ
ド17を設けている。In FIG. 4, the shroud 13,
A labyrinth fin 15 is provided on 14 and this labyrinth fin is
A flow guide 17 is provided to cover the tips of the stationary blade rows 5 and 6 with a gap from the flow guide 17.
このような構造により蒸気入口2から流入した蒸気は
フローガイド17により2方向に分れて蒸気入口2の両側
の段落に流れるが、この際ラビリンスフイン15により静
翼列6,7の先端から洩れる蒸気をシールしている。With such a structure, the steam flowing in from the steam inlet 2 is divided into two directions by the flow guide 17 and flows to the paragraphs on both sides of the steam inlet 2, and at this time, the labyrinth fin 15 leaks from the tips of the stationary blade rows 6 and 7. Seals steam.
第3図に示した従来例ではシユラウドプレート8,9と
ブリッジ片12とをばね10を介して締付けているので、タ
ービン運転時の熱膨脹によりアキシヤル方向およびラジ
アル方向に伸びたときに、ばねの力が第1段の静翼列6,
7の静翼に伝わり、静翼列や静翼の強度,変形等に悪影
響を与えるという問題がある。In the prior art shown in FIG. 3, since the shroud plates 8, 9 and the bridge piece 12 are fastened via the spring 10, when the spring expands in the axial direction and the radial direction due to thermal expansion during the operation of the turbine, the spring is closed. The first stage stationary blade row 6,
There is a problem that it is transmitted to the stationary blade of No. 7 and adversely affects the strength and deformation of the stationary blade row and stationary blade.
第4図の従来例ではシユラウド13,14に設けたラビリ
ンスフイン15とフローガイド17との間はタービン運転時
の熱膨脹や各部材の熱変形を考慮すると適度の隙間を持
たせなくてはならないため、この隙間から蒸気が洩れて
蒸気の漏洩損失が生じ、性能上好ましくないという問題
がある。In the prior art shown in FIG. 4, an appropriate gap must be provided between the labyrinth fin 15 provided on the shrouds 13 and 14 and the flow guide 17 in consideration of thermal expansion during turbine operation and thermal deformation of each member. However, there is a problem that steam leaks from this gap to cause loss of steam leakage, which is not preferable in terms of performance.
本発明の目的は、タービン運転時の熱膨脹によりアキ
シヤル方向およびラジアル方向に伸びても第1段の静翼
列に悪影響を与えず、しかも蒸気の漏洩を防止すること
のできる複流式蒸気タービンを提供することである。SUMMARY OF THE INVENTION An object of the present invention is to provide a double-flow steam turbine which does not adversely affect the first-stage stationary blade row even if it expands in the axial direction and the radial direction due to thermal expansion during turbine operation and can prevent steam leakage. It is to be.
上記課題を解決するために、本発明によれば静翼から
なる複数の静翼列を備えるケーシングの蒸気入口の両側
に前記静翼と車軸に備えられる複数の動翼列の動翼とで
形成される複数段の段落を備え、蒸気入口から流入した
蒸気が2方向に分れ前記両側の段落を通流して膨脹する
複流形蒸気タービンにおいて、前記両側の段落を通流し
て膨張する複流形蒸気タービンにおいて、前記両側の第
1段のそれぞれの静翼列の先端を覆うシユラウドプレー
トと、この両者のシユラウドプレートの間をL形の二つ
割りの気密リングを介して閉鎖するフローガイドリング
とを設けるものとする。In order to solve the above-mentioned problem, according to the present invention, on both sides of a steam inlet of a casing provided with a plurality of stationary blade rows composed of stationary blades, the stationary blade is formed on the both sides of a steam inlet and a plurality of rotor blade rows provided on an axle. A double-flow steam turbine having a plurality of stages, wherein the steam flowing from the steam inlet is divided into two directions and flows through the two stages to expand. In the turbine, a shroud plate that covers the tip of each of the first-stage stationary blade rows on both sides, and a flow guide ring that closes between the two shroud plates via an L-shaped split airtight ring. Shall be provided.
〔作用〕 蒸気が蒸気入口から流入する蒸気流入部には、ケーシ
ング内の蒸気入口の両側にある第1段の静翼列の先端を
覆うシユラウドプレートと、この両者のシユラウドプレ
ートとの間を気密リングを介して閉鎖するフローガイド
リングとを設けたことにより、蒸気入口から流入した蒸
気はフローガイドとシユラウドプレートとにより2方向
に分れて両側の第1段の静翼列に流入するが、この際シ
ユラウドプレートとフローガイドリングとは気密リング
により接合されているので、タービン運転時の熱膨脹を
気密リングにより吸収するとともに蒸気の漏洩を防止す
る。[Operation] A steam inflow portion through which steam flows in from a steam inlet has a shroud plate that covers the tip of the first stage stationary blade row on both sides of the steam inlet in the casing, and between the two shroud plates. And a flow guide ring that closes the steam flow through an airtight ring, the steam flowing from the steam inlet is divided into two directions by the flow guide and the shroud plate and flows into the first row of stationary vanes on both sides. However, at this time, since the shroud plate and the flow guide ring are joined by an airtight ring, thermal expansion during turbine operation is absorbed by the airtight ring, and leakage of steam is prevented.
以下図面に基づいて本発明の実施例について説明す
る。第1図は本発明の実施例による複流形蒸気タービン
の蒸気流入部の部分断面図である。なお、第1図および
後述する第2図において第3図,第4図の従来例と同一
部品には同じ符号を付し、その説明を省略する。第1図
において第1段の静翼列6,7の先端を覆ってシユラウド
プレート20,21が取付けられ、そしてシユラウドプレー
ト20と21との間を閉鎖してフローガイドリング22が設け
られている。シユラウドプレート20,21とフローガイド
リング22とは第2図に示すようにL形の二つ割りの気密
リング23がシユラウドプレート21に設けられた環状の溝
24とフローガイドリング22に設けられた環状の溝25とに
挿入されて接合されている。なお、シユラウドプレート
20側も同様な構造により気密リング23が配設されてい
る。なお、フローガイドリング22は二つ割り構造であ
り、図示しない支持体によりケーシング1に支持されて
いる。Hereinafter, embodiments of the present invention will be described with reference to the drawings. FIG. 1 is a partial sectional view of a steam inflow portion of a double-flow steam turbine according to an embodiment of the present invention. In FIG. 1 and FIG. 2, which will be described later, the same parts as those in the conventional example shown in FIGS. In FIG. 1, shroud plates 20 and 21 are attached so as to cover the tips of the first stage stationary blade rows 6 and 7, and a flow guide ring 22 is provided so as to close between the shroud plates 20 and 21. ing. As shown in FIG. 2, the shroud plates 20, 21 and the flow guide ring 22 have an annular groove formed in the shroud plate 21 with an L-shaped split airtight ring 23.
24 and an annular groove 25 provided in the flow guide ring 22 are inserted and joined. The shroud plate
An airtight ring 23 is provided on the 20 side in a similar structure. The flow guide ring 22 has a split structure, and is supported by the casing 1 by a support (not shown).
このような構造により蒸気入口2から流入した蒸気は
第1段の静翼列の先端を覆うシユラウドプレート20,21
とフローガイドリング22とにより2方向に分れて両側の
第1段の静翼列6,7に流入するが、気密リング23により
静翼列6,7に流入せずに洩れる蒸気はなくなり、またタ
ービン運転時の熱膨脹を吸収することができる。With such a structure, the steam flowing from the steam inlet 2 allows the shroud plates 20, 21 covering the tips of the first stage stationary blade rows.
And flow into the first stage stationary blade rows 6 and 7 on both sides by the flow guide ring 22, but there is no steam leaking without flowing into the stationary blade rows 6 and 7 by the airtight ring 23. Also, thermal expansion during turbine operation can be absorbed.
以上の説明から明らかなように、本発明によればケー
シングの蒸気入口の両側にある第1段の静翼列の先端を
覆うシユラウドプレートの間を気密リングを介してフロ
ーガイドリングにより閉鎖したことにより、蒸気入口か
ら流入した蒸気は気密リングにより第1段の静翼列に流
入しない洩れ蒸気をなくすことができ、またタービン運
転時のアキシヤル方向およびラジアル方向の熱膨脹は吸
収されるので、第1段の静翼列の構造の健全性を確保で
きる。As is apparent from the above description, according to the present invention, the space between the shroud plates covering the tips of the first stage stationary blade rows on both sides of the steam inlet of the casing is closed by the flow guide ring via the airtight ring. Thus, the steam flowing from the steam inlet can eliminate leaked steam that does not flow into the first row of stationary blades by the hermetic ring, and thermal expansion in the axial and radial directions during turbine operation is absorbed. The soundness of the structure of the one-stage stationary blade row can be ensured.
第1図は本発明の実施例による複流形蒸気タービンの部
分断面図、第2図は第1図のA部の拡大図、第3図は従
来の複流形蒸気タービンの部分断面図、第4図は従来の
異なる複流形蒸気タービンの部分断面図である。 1:ケーシング、2:蒸気入口、3:静翼、4:車軸、5:動翼、
6,7:静翼列、20,21:シユラウドプレート、22:フローガ
イドリング、23:気密リング。1 is a partial sectional view of a double-flow steam turbine according to an embodiment of the present invention, FIG. 2 is an enlarged view of a portion A in FIG. 1, FIG. 3 is a partial sectional view of a conventional double-flow steam turbine, FIG. The figure is a partial sectional view of a different conventional double-flow steam turbine. 1: casing, 2: steam inlet, 3: stationary vane, 4: axle, 5: rotor blade,
6, 7: stationary blade row, 20, 21: shroud plate, 22: flow guide ring, 23: airtight ring.
Claims (1)
ングの蒸気入口の両側に前記静翼と車軸に備えられる複
数の動翼列の動翼とで形成される複数段の段落を備え、
蒸気入口から流入した蒸気が2方向に分かれ、前記両側
の段落を流通して膨張する複流形蒸気タービンにおい
て、前記両側の第1段のそれぞれの静翼列の先端を覆う
シユラウドプレートと、この両者のシユラウドプレート
の間をL形の二つ割りの気密リングを介して閉鎖するフ
ローガイドリングとを設けたことを特徴とする複流形蒸
気タービン。1. A stage having a plurality of stages formed by said stationary blades and a plurality of rotor blades of a plurality of rotor blade rows provided on an axle, on both sides of a steam inlet of a casing having a plurality of stator blade rows comprising stator blades. ,
In a double-flow type steam turbine in which steam flowing from a steam inlet is divided into two directions and flows through the paragraphs on both sides and expands, a shroud plate that covers the tip of each stationary blade row of the first stage on both sides, A double-flow steam turbine comprising a flow guide ring which closes between both shroud plates via an L-shaped split airtight ring.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2048214A JP2600955B2 (en) | 1990-02-28 | 1990-02-28 | Double-flow steam turbine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2048214A JP2600955B2 (en) | 1990-02-28 | 1990-02-28 | Double-flow steam turbine |
Publications (2)
Publication Number | Publication Date |
---|---|
JPH03249303A JPH03249303A (en) | 1991-11-07 |
JP2600955B2 true JP2600955B2 (en) | 1997-04-16 |
Family
ID=12797163
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2048214A Expired - Lifetime JP2600955B2 (en) | 1990-02-28 | 1990-02-28 | Double-flow steam turbine |
Country Status (1)
Country | Link |
---|---|
JP (1) | JP2600955B2 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2003008765A1 (en) * | 2001-07-19 | 2003-01-30 | Kabushiki Kaisha Toshiba | Assembly type nozzle diaphragm, and method of assembling the same |
JP2008069776A (en) * | 2006-09-11 | 2008-03-27 | General Electric Co <Ge> | Turbine nozzle assembly |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7322789B2 (en) * | 2005-11-07 | 2008-01-29 | General Electric Company | Methods and apparatus for channeling steam flow to turbines |
US8657562B2 (en) | 2010-11-19 | 2014-02-25 | General Electric Company | Self-aligning flow splitter for steam turbine |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4826395A (en) * | 1988-04-08 | 1989-05-02 | Westinghouse Electric Corp. | Turbine inlet flow deflector and sealing system |
-
1990
- 1990-02-28 JP JP2048214A patent/JP2600955B2/en not_active Expired - Lifetime
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2003008765A1 (en) * | 2001-07-19 | 2003-01-30 | Kabushiki Kaisha Toshiba | Assembly type nozzle diaphragm, and method of assembling the same |
US7179052B2 (en) | 2001-07-19 | 2007-02-20 | Kabushiki Kaisha Toshiba | Assembly type nozzle diaphragm, and method of assembling the same |
JP2008069776A (en) * | 2006-09-11 | 2008-03-27 | General Electric Co <Ge> | Turbine nozzle assembly |
Also Published As
Publication number | Publication date |
---|---|
JPH03249303A (en) | 1991-11-07 |
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