JPH03249303A - Double-current steam turbine - Google Patents

Double-current steam turbine

Info

Publication number
JPH03249303A
JPH03249303A JP4821490A JP4821490A JPH03249303A JP H03249303 A JPH03249303 A JP H03249303A JP 4821490 A JP4821490 A JP 4821490A JP 4821490 A JP4821490 A JP 4821490A JP H03249303 A JPH03249303 A JP H03249303A
Authority
JP
Japan
Prior art keywords
steam
sides
flow
flow guide
guide ring
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.)
Granted
Application number
JP4821490A
Other languages
Japanese (ja)
Other versions
JP2600955B2 (en
Inventor
Hiromi Sakamoto
坂元 浩美
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.)
Fuji Electric Co Ltd
Original Assignee
Fuji 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 Fuji Electric Co Ltd filed Critical Fuji Electric Co Ltd
Priority to JP2048214A priority Critical patent/JP2600955B2/en
Publication of JPH03249303A publication Critical patent/JPH03249303A/en
Application granted granted Critical
Publication of JP2600955B2 publication Critical patent/JP2600955B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

PURPOSE:To avoid bad influence of thermal expansion and prevent leakage of steam by blocking the passage between both shroud plates which cover ends of first step static blade lines on both sides and a flow guide ring through airtight rings. CONSTITUTION:Shroud plates 6, 7 which cover ends of first step static blade lines 6, 7 on both sides, and a flow guide ring 22 which blocks the passage between the shroud plates 20 and 21 through airtight rings 23, are provided. In flow of stem from a stem inlet 2 is divided into two directions by means of the flow guide ring 22 and the shroud plates 20, 21, and introduced into the first step static blade lines 6, 7 on both sides. In this case, the shroud plates 20, 21 are connected to the flow guide ring 22 by means of the airtight rings 23, so that thermal expansion during operation of a turbine is eliminated by the airtight rings 23 and the leakage of steam is prevented.

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
翼列の礪造をこ関する。
[Detailed Description of the Invention] [Industrial Application Field] The present invention is characterized in that the steam flowing in from the steam inlet of the casing is
This invention relates to a double-flow steam turbine in which the air flows through stages on both sides of the steam inlet for expansion, and in particular to the elongation of the row of stator blades in the first stage of the steam inlet.

〔従来の技術〕[Conventional technology]

a、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2万同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里軸に備えられる′
#4列のwJ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
の荷造として、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Gこi3図(tvjp平1−16340
5 号g照> オよび第1図に示すものか知られている
a. In a flow-type steam turbine, the steam that flows in from the steam inlet of the casing is divided into 20,000 parts and is installed between the stator blades of the stator blade rows provided in the casing on both sides of the steam inlet and the shaft.
Work is carried out by passing the flow through multiple stages of stages formed by the #4 row of wJ blades. In order to prevent the inflowing steam from leaking from the gap between the tip of the stationary blade row and the axle that opposes it, the
No. 5 g Sho > O and those shown in Figure 1 are known.

第3図においてケーシング1内にはケーシングlの蒸気
人口2の両側に静lX3からなる静翼列が:!!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からなる複数列の静翼列が投げられている
。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ュラウドプレート8,9
が取付けられ、シュラウドプレート8と9との間を榎り
てばf210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, inside the casing 1, on both sides of the steam population 2 of the casing 1, there are rows of stator blades consisting of 1 x 3:! ! There are several rows. A plurality of rows of stator blades are disposed on the axle 4 and are composed of rotor blades 5 that form a stage with the stator blades of the stator blade rows. Reference numerals 6 and 7 indicate the stator blade rows of the first stage of the steam inflow section, and shroud plates 8 and 9 cover the tips of the stator blades of the stator blade rows 6 and 7.
is attached, and a bridge piece 12 is attached which extends between the shroud plates 8 and 9 and is tightened with bolts 11 via f210.

このような構造により蒸気人口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ュラウドプレート
8,9とにより2方向に分れて蒸気人口2の両側の段落
に流れる。この際ブリ、ジ片12とシュラウドプレート
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 this structure, the steam flowing in from the steam port 2 is divided into two directions by the bridge piece 12 and the shroud plates 8 and 9 connected thereto, and flows to the stages on both sides of the steam port 2. At this time, the bridge and jig pieces 12 and the shroud plates 8 and 9 prevent the steam flowing into the first stage stator blade row from leaking through the gap between the tip of the first stage stator blade row and the axle.

第4図においては第1段の静翼列6,7のシュラウド1
3.14tこラビリンスフィン15を設け、このラビリ
ンスフィン15と隙間を持たせて静翼列5゜6の先端を
榎うフローカイト17を設けている。
In Fig. 4, the shroud 1 of the stator blade rows 6 and 7 of the first stage is shown.
A 3.14 t labyrinth fin 15 is provided, and a flow kite 17 is provided which takes out the tip of the stationary blade row 5.6 with a gap between the labyrinth fin 15 and the labyrinth fin 15.

このような構造により蒸気人口2から流入した蒸気はフ
ローガイドエフにより2万同に分れて蒸気人口2の両側
の段落に流れるが、この際ラビリンスフィン15により
静翼列6.7の先端から洩れる蒸気をソールしている。
With this structure, the steam flowing in from the steam population 2 is divided into 20,000 parts by the flow guide F and flows to the stages on both sides of the steam population 2, but at this time, the labyrinth fins 15 separate the steam from the tip of the stationary blade row 6.7. Sole leaking steam.

〔発明が解決しようとする課題〕[Problem to be solved by the invention]

第3図に示した従来例ではンユラウドプレート8.9と
ブリッジ片12とをばj210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ャル方向およ
びラジアル方向に伸びたときに、ばnの力か第1段の静
翼列6,7の静翼に伝わり、静翼列や静翼の強匣、変形
等に悪影響を与えるという問題がある。
In the conventional example shown in FIG. 3, the round plate 8.9 and the bridge piece 12 are fastened together via the baffles 210, so that when the baffles expand in the axial and radial directions due to thermal expansion during turbine operation, There is a problem in that the force is transmitted to the stator blades of the stator blade rows 6 and 7 of the first stage, which adversely affects the strength, deformation, etc. of the stator blade rows and the stator blades.

第4図の従来例ではシュラウド13 、14に設置jた
ラビリンスフィン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漣すると適度
の隙間を持たせなくてはならないため、この実間から蒸
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 conventional example shown in FIG. 4, an appropriate gap must be provided between the labyrinth fins 15 installed on the shrouds 13 and 14 and the flow guide 17 in consideration of thermal expansion and thermal deformation of each member during turbine operation. Therefore, there is a problem in that steam leaks from this space, resulting in steam leakage loss, which is unfavorable 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
ャ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。
An object of the present invention is to provide a double-flow steam turbine that does not adversely affect the stator blade rows of the first stage even if they are extended in the axial and radial directions due to thermal expansion during turbine operation, and that can prevent steam leakage. It is to be.

〔課題を解決するための手段〕[Means to solve the problem]

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(l数の動翼列の動翼とで
形成される複数段の段落を備え、蒸気人口から流入した
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、前記両側の第1段の静翼
列の先端を傍うシュラウドプレートと、この両者のシュ
ラウドプレートの間を気M IJ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 problems, according to the present invention, the stator blades and the axle are provided on both sides of the steam inlet of a casing provided with a plurality of stator blade rows (l number of rotor blade rows). In a double-flow steam turbine, the steam flowing in from the steam turbine is divided into two directions and is expanded by flowing through the stages on both sides. A shroud plate adjacent to the tip and a flow guide ring that closes the space between the two shroud plates via an air MIJ ring are provided.

〔作用〕[Effect]

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段のむ翼列の先端を覆
うシュラウドプレートと、この両者のシュラウドプレー
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
はフローカイトとシュラフトプレートとにより2方向に
分れて両側の第1段の静翼列に流入するが、この際ンユ
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#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
The steam inlet where steam flows from the steam inlet has a shroud plate that covers the tips of the blade rows containing the first stage on both sides of the steam inlet in the casing, and an airtight ring between these two shroud plates. By providing a flow guide ring that closes with Since the air-tight ring connects the air-tight plate and the flow guide ring, the air-tight ring absorbs heat and swelling during turbine operation and prevents steam leakage.

〔実施例〕〔Example〕

以下図面に基づいて本発明の実施例について説明する1
、第1図は本発明の実施例1゛こ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3、第1図およ
び後述する第2図において第3図。
Embodiments of the present invention will be described below based on the drawings.
Embodiment 1 FIG. 1 is a partial sectional view of a steam inlet portion of a double flow steam turbine according to Embodiment 1 of the present invention. 3. FIG. 3 in FIG. 1 and FIG. 2, which will be described later.

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
先端を覆ってシュラウドプレート21)。
Components that are the same as those in the conventional example shown in FIG. 4 are given the same reference numerals, and their explanations will be omitted. In FIG. 1, a shroud plate 21) covers the tips of the first stage stator blade rows 6 and 7.

−ガイド牢γニドηとは第2図に示すようにL形の二つ
割りの気密リングおかシュラウドプレート21に設けら
れた環状の?*冴とフローガイドリンクnに設けられた
環状の溝5とに挿入されて接合されている。なお、シュ
ラウドプレート2tJ側も同様な構造により気密リング
乙が配設されている。なお、フローガイドリング乙は二
つ割り構造であり、図示しない支持体(こよりケーシン
グ1に支持されている。
- What is the guide cell ?nid η? As shown in Fig. 2, it is an annular ? *It is inserted into and joined to the annular groove 5 provided in the flow guide link n. Note that an airtight ring B is disposed on the shroud plate 2tJ side with a similar structure. Note that the flow guide ring B has a two-piece 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人口2から流入したレート2
0 、2]とフローカイト兎−;六匹とにより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
リング乙により静翼列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。
Due to this structure, the rate of inflow from steam population 2 is 2
0, 2] and six flow kites, the flow is divided into two directions and flows into the first stage stator blade rows 6 and 7 on both sides, but the airtight ring B prevents the flow into the stator blade rows 6 and 7. This eliminates steam leakage and absorbs thermal expansion during turbine operation.

〔発明の効果〕〔Effect of the invention〕

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
覆うシュラウドプレートの間を気密リングを介してフロ
ーカイトリングfこ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
運転時のアキシャル方向εよびラジアル方向の熱#脹は
吸収されるので、第1段の静翼列の構造の健全性を1株
できる。
As is clear from the above description, according to the present invention, the flow kite ring is closed between the shroud plates covering the tips of the first stage stator blade rows on both sides of the steam inlet of the casing via an airtight ring. As a result, the steam flowing in from the steam inlet can be prevented from leaking into the first stage stator blade row by the airtight ring, and the heat expansion in the axial direction ε and radial direction during turbine operation can be absorbed. Therefore, the structural integrity of the first stage stator blade row can be confirmed.

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

第1図は本発明の実汎例1こ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、2$乳入口 ・1ケーレンフ 第 図 第 図 第 図 第 図
Fig. 1 is a partial sectional view of a double flow steam turbine according to practical example 1 of the present invention, Fig. 2 is an enlarged view of section A in Fig. 1, and Fig. 3 is a partial sectional view of a conventional double flow steam turbine. , FIG. 4 is a partial sectional view of a different conventional double-flow steam turbine. 1: Casing, 2: Steam inlet, 3: Stationary blade, 2 milk inlet, 1 cable head diagram diagram diagram diagram diagram diagram

Claims (1)

【特許請求の範囲】[Claims] 1)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を特徴と
する複流形蒸気タービン。
1) On both sides of the steam inlet of a casing having a plurality of rows of stator blades, a plurality of stages formed by the stator blades and rotor blades of a plurality of rows of rotor blades provided on an axle are provided, and the steam inlet A shroud plate that covers the tips of the stator blade rows of the first stage on both sides of the double flow steam turbine in which steam flowing from the turbine is divided into two directions and expanded by flowing through the stages on both sides;
A double flow steam turbine characterized by being provided with a flow guide ring that closes the space between the two shroud plates via an airtight ring.
JP2048214A 1990-02-28 1990-02-28 Double-flow steam turbine Expired - Lifetime JP2600955B2 (en)

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 true JPH03249303A (en) 1991-11-07
JP2600955B2 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)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2007132348A (en) * 2005-11-07 2007-05-31 General Electric Co <Ge> Device conveying steam to turbine and double-flow steam turbine having the device
JP2012112380A (en) * 2010-11-19 2012-06-14 General Electric Co <Ge> Self-aligning flow splitter for steam turbine

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP4040922B2 (en) * 2001-07-19 2008-01-30 株式会社東芝 Assembly type nozzle diaphragm and its assembly method
US7874795B2 (en) * 2006-09-11 2011-01-25 General Electric Company Turbine nozzle assemblies

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH01301902A (en) * 1988-04-08 1989-12-06 Westinghouse Electric Corp <We> Double-current steam turbine

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH01301902A (en) * 1988-04-08 1989-12-06 Westinghouse Electric Corp <We> Double-current steam turbine

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2007132348A (en) * 2005-11-07 2007-05-31 General Electric Co <Ge> Device conveying steam to turbine and double-flow steam turbine having the device
JP2012112380A (en) * 2010-11-19 2012-06-14 General Electric Co <Ge> Self-aligning flow splitter for steam turbine
DE102011055469B4 (en) 2010-11-19 2022-07-28 General Electric Company Self-aligning flow divider for steam turbine

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JP2600955B2 (en) 1997-04-16

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