JPH0367002A - Assembly of steam turbine - Google Patents

Assembly of steam turbine

Info

Publication number
JPH0367002A
JPH0367002A JP20289489A JP20289489A JPH0367002A JP H0367002 A JPH0367002 A JP H0367002A JP 20289489 A JP20289489 A JP 20289489A JP 20289489 A JP20289489 A JP 20289489A JP H0367002 A JPH0367002 A JP H0367002A
Authority
JP
Japan
Prior art keywords
turbine
mandrel
assembling
time
lower half
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
JP20289489A
Other languages
Japanese (ja)
Inventor
Takuji Fujikawa
卓爾 藤川
Kenichiro Yamaguchi
山口 賢一郎
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.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries 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 Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP20289489A priority Critical patent/JPH0367002A/en
Publication of JPH0367002A publication Critical patent/JPH0367002A/en
Pending legal-status Critical Current

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  • Length Measuring Devices With Unspecified Measuring Means (AREA)

Abstract

PURPOSE:To appropriately set a gap between a static part and a rotary part on the side of a turbine rotor, which is required at the time of completion of assembly, at the time of measuring clearance by temporarily assembling a turbine casing and correctly finding a displacement value of the static part at the time of the clearance measurement and the time of the completion of the temporary assembly. CONSTITUTION:The lower half part of a static part 2 such as a blade ring 2a or a dummy ring 2b is detached to the lower half part la of a turbine casing, and a mandrel 4 is mounted on the position of the turbine casing to detach a rotor. And an arm 5 is set on the position of the mandrel 4 to cope with the static part 2. Subsequently, the distance from the shaft center of the mandrel 4 to the static part 2 is measured with a displacement gauge 6 and the result is regarded as G1, and the upper half of the static part 2 is detached on the lower half part la and then the upper half part 1b is detached to complete the temporary assembly of the turbine. Then the distance from the shaft center of the mandrel 4 to the static part 2 is measured with the displacement gauge 6 and the result is regarded as G2. Thereafter, the difference between the distance G1 and the distance G2 is obtained and the result is regarded as a displacement value m of the static part 2 at the time of the measurement of clearance and the time of the completion of the temporary assembly. Thereafter, the mandrel 4 is removed, and a regular turbine rotor is detached to have the gap between the static pat and the rotary part at a planned clearance value plus (m).

Description

【発明の詳細な説明】 産業上の利用分野 本発明は、タービン車室に設けられている翼環やダミー
環などの静止部品とタービンロータに取付けられている
回転部品との隙間を、極力設計値に近付は得るようにし
た蒸気タービンの組立方法に関する。
DETAILED DESCRIPTION OF THE INVENTION Field of Industrial Application The present invention aims to minimize the gap between stationary parts such as blade rings and dummy rings provided in the turbine casing and rotating parts attached to the turbine rotor. The present invention relates to a method of assembling a steam turbine that approaches a value close to that value.

従来の技術 蒸気タービンにおいて、タービンロータと翼環やダミー
環などの静止部品との間に形成する隙間(これを遊隙と
呼んでいる)の設定は、性能と信頼性の確保に極めて重
要な意味を持っている。すなわち、遊隙が大き過ぎると
蒸気の漏洩量が増加するため性能の低下を招き、逆に遊
隙が小さ過ぎると回転部分が静止部分に接触することに
なって信頼性を損なうことになる。
Conventional technology In steam turbines, setting the gap (this is called play) between the turbine rotor and stationary parts such as blade rings and dummy rings is extremely important to ensure performance and reliability. It has meaning. That is, if the play is too large, the amount of steam leaking will increase, leading to a decline in performance, while if the play is too small, the rotating parts will come into contact with the stationary parts, impairing reliability.

ところで、この遊隙は、タービン車室の下半部に翼環や
ダミー環などの静止部品の下半分を組付けた状態と、所
定の位置にタービンロータを組付けたタービンの組立完
了状態とでは異なってくるため、その調整と設定が困難
なものであった。この遊隙に差を生ずるのは、次のよう
な理由によるものである。
By the way, this play differs between a state in which the lower half of stationary parts such as a blade ring and a dummy ring are assembled to the lower half of the turbine casing, and a state in which the turbine is fully assembled with the turbine rotor assembled in a predetermined position. The adjustment and settings have been difficult because they differ. The reason for this difference in play is as follows.

すなわち、タービン組立過程において、遊隙を調整した
り計測するのに適した時は、タービン車室の下半部に、
翼環やダミー環などの静止部品の下半分を組付けた時(
以下この状態を遊隙計測時の状態という)であり、この
状態ではタービン車室は半円筒状となるので剛性はそれ
ほど強いものではない。
In other words, during the turbine assembly process, when it is appropriate to adjust or measure the play, the lower half of the turbine casing is
When assembling the lower half of stationary parts such as blade rings or dummy rings (
This state is hereinafter referred to as the state at the time of play measurement), and in this state, the turbine casing has a semi-cylindrical shape, so its rigidity is not so strong.

一方、タービン組立完了時は、翼環やダミー環などの静
止部品の上半分も組付けられており、更にタービン車室
の上半部も取付けられるので、自重による荷重が増加す
る。しかし、タービンの上下の単室は、水平継手面でフ
ランジボルトによって締付けられるので、車室は円筒状
となり、剛性が増す。
On the other hand, when the turbine assembly is completed, the upper half of stationary parts such as the blade ring and the dummy ring are also assembled, and the upper half of the turbine casing is also attached, so the load due to its own weight increases. However, since the upper and lower single chambers of the turbine are tightened by flange bolts at the horizontal joint surface, the casing becomes cylindrical and has increased rigidity.

これらの様子を第3図ないし第5図に示しである。These situations are shown in FIGS. 3 to 5.

第3図は遊隙計測時の状態を示しており、タービン車室
は下半部1aのみのため剛性は小さいが、翼環2aやグ
ミー環2bなどの静止部品は下半分のみを組付けた状態
なので重量は軽い。
Figure 3 shows the state during play measurement, and the turbine casing has only the lower half 1a, so its rigidity is small, but stationary parts such as the blade ring 2a and gummy ring 2b are only assembled in the lower half. Due to its condition, it is light in weight.

第4図は静止部品2a、 2bの上半分も組付けた状態
を示したもので、タービン車室の剛性は第3図と同様で
小さいが、静止部品は上半分も加わるので重量が増し、
従ってたわみは第3図の状態より増す。
Figure 4 shows the state in which the upper halves of the stationary parts 2a and 2b are also assembled.The rigidity of the turbine casing is similar to that in Figure 3 and is small, but the weight of the stationary parts increases because the upper halves are also added.
Therefore, the deflection increases compared to the state shown in FIG.

第5図はタービン車室の上半部1bも取付けたタービン
組立完了時の状態を示しており、重量は増加するがター
ビン車室は上半部1bと下半部1aとが締付けられてい
るので、剛性が増す。従って、たわみは下半部1aだけ
の場合よりも小さくなる。
Figure 5 shows the state when the turbine casing is assembled with the upper half 1b also attached, and although the weight increases, the upper half 1b and lower half 1a of the turbine casing are tightened. Therefore, rigidity increases. Therefore, the deflection is smaller than in the case of only the lower half portion 1a.

このように、遊隙計測時とタービン組立完了時とでは、
たわみ量が変化する。これに対して、ロータのたわみは
常に同じなので、ロータと静止部品との間の遊隙は夫々
の場合に応じて異なることになる。しかし、タービン組
立完了時に遊隙を調整することができないので、通常、
は遊隙計測時にこの差を考慮して、遊隙値を調整してい
る。
In this way, between the time of play measurement and the time of turbine assembly completion,
The amount of deflection changes. On the other hand, since the deflection of the rotor is always the same, the play between the rotor and the stationary part will be different in each case. However, since the play cannot be adjusted when the turbine is assembled,
takes this difference into account when measuring the play and adjusts the play.

そのため、第6図および第7図に示すように、ダイヤル
インジケータ3をタービン車室の下半部1aの最低部に
取付け、遊隙計測時ダイヤルインジケータ3の指示値(
変位)M+とタービン組立完了時のダイヤルインジケー
タ3の指示値(変位)Lを読み、その差(M、−M、)
を以て静止部品2 (2a、 2b)の上下方向の変位
mとし、そして、タービン組立完了時に確保されていな
ければならない遊隙値をδI(すなわち設計値)、遊隙
計測時に設定する遊隙値をδ、とすると、 δt0 δ、+、    ・◆−(1)となるように遊
隙計測時の隙間の大きさを設定している。この従来の方
法を、ボトムリーディング法と呼んでいる。
Therefore, as shown in FIGS. 6 and 7, the dial indicator 3 is attached to the lowest part of the lower half 1a of the turbine casing, and the indicated value of the dial indicator 3 (
Read the indicated value (displacement) M+ and the indicated value (displacement) L of the dial indicator 3 when the turbine assembly is completed, and find the difference (M, -M,)
is the vertical displacement m of the stationary parts 2 (2a, 2b), and the play value that must be secured at the time of completion of turbine assembly is δI (i.e., design value), and the play value set at the time of play measurement is When δ, the size of the gap at the time of play measurement is set so that δt0 δ, +, ◆-(1). This conventional method is called the bottom reading method.

発明が解決しようとする課題 ところで、上述のボトムリーディング法は、タービン車
室の下半部1aの変位を静止部品2の変位とみなしてい
るので、どのようケースにもあてはまるものではなく、
必ずしも正しくはないという問題があった。
Problems to be Solved by the Invention By the way, the above-mentioned bottom reading method regards the displacement of the lower half portion 1a of the turbine casing as the displacement of the stationary component 2, so it does not apply to all cases.
The problem was that it wasn't necessarily correct.

すなわち、第8図および第9図に示すように、静止部品
2の上下を一体として締付けた時と下半分のみを納めた
時とで、水平継手面の軸に直角な方向の傾きが変化する
ような場合は、これによる静止部品2の変位はボトムリ
ーディング法では求めることはできない。このような現
象は各部品が新しい状態でも起こり得るが、−度使用さ
れたタービンでは部品の変形があるので特に著しくなる
In other words, as shown in Figs. 8 and 9, the inclination of the horizontal joint surface in the direction perpendicular to the axis changes depending on when the upper and lower parts of the stationary part 2 are tightened together and when only the lower half is retracted. In such a case, the resulting displacement of the stationary component 2 cannot be determined by the bottom reading method. Although such a phenomenon can occur even when each part is new, it is particularly noticeable in a turbine that has been used several times because the parts are deformed.

本発明は、従って、このような問題を解決し、組立完了
時における回転部品と静止部品との間の所望の隙間が、
組立過程での鍔整で、できるだけ設計値に近付けて設定
できるような蒸気タービンの組立方法を提供することを
目的としてなされたものである。
The present invention therefore solves such problems and ensures that the desired gap between the rotating and stationary parts upon completion of assembly is
This was done with the purpose of providing a method for assembling a steam turbine that allows the flange adjustment to be made as close to the design value as possible during the assembly process.

課題を解決するための手段 本発明は、タービン車室の下半部に翼環やダミー環など
の静止部品の下半分を組付けていわゆる遊隙計測時の状
態とする工程と、タービン車室のタービンロータの取付
は位置に要所に変位計測機が設けられたマンドレルを設
置する工程と、前記変位計測機によってマンドレルの軸
心から前記静止部品までの距離G、を計測する工程と、
タービン車室の下半部上に前記翼環やダミー環などの静
止部品の上半分を組付けた後タービン車室の上半部を組
付けてタービンの仮組立を行う工程と、この状態で前記
変位計測機によってマンドレルの軸心から前記静止部品
までの距離G!を計測する工程と、これらの計測値G+
、 Gyの差から遊隙計測時とタービンの仮組立完了時
とにおける静止部品の変位置m(m=G+  Gt)を
検知する工程と、タービン車室の上半部を開放して前記
マンドレルを取除く工程と、マンドレルを取除いた後に
正規のタービンロータを組付ける工程とから成り、ター
ビンロータを組付ける際に前記静止部品とタービンロー
タ側の回転部品との隙間δ、を、組立完了時の設計遊隙
値δ1に前記変位置mを加えた値となるように凋整する
ようにしたものである。
Means for Solving the Problems The present invention provides a process for assembling the lower half of stationary parts such as a blade ring or a dummy ring into the lower half of the turbine casing to bring it into a state for so-called play measurement, and The installation of the turbine rotor includes a step of installing a mandrel equipped with a displacement measuring device at key points, and a step of measuring a distance G from the axis of the mandrel to the stationary component using the displacement measuring device.
A step of temporarily assembling the turbine by assembling the upper half of stationary parts such as the blade ring and dummy ring on the lower half of the turbine casing and then assembling the upper half of the turbine casing; The distance G from the mandrel axis to the stationary part is measured by the displacement measuring device! and the process of measuring these measured values G+
, a step of detecting the displacement position m (m=G+Gt) of the stationary component between the time of measuring the play and the time of completion of temporary assembly of the turbine from the difference in Gy, and the step of opening the upper half of the turbine casing and removing the mandrel. and a step of assembling a regular turbine rotor after removing the mandrel, and when assembling the turbine rotor, the gap δ between the stationary component and the rotating component on the turbine rotor side is adjusted to The design clearance value δ1 is adjusted to a value obtained by adding the displacement position m.

作用 上記の手段によると、タービンの組立過程における遊隙
計測時と、タービンの仮組立完了時とにおける静止部品
の変位置を計測することにより、両状態間での静止部品
の変位置が求められ、この変位置を考慮して遊隙計測時
に静止部品とタービン側の回転部品との隙間を設定する
ので、゛タービンの組立完了時での遊隙値を所望の値に
極力近付けることができる。
According to the above-mentioned means, by measuring the displacement of the stationary components at the time of measuring the play during the turbine assembly process and at the time of completion of temporary assembly of the turbine, the displacement of the stationary components between the two states can be determined. Since the clearance between the stationary component and the rotating component on the turbine side is set in consideration of this positional displacement when measuring the clearance, it is possible to bring the clearance value as close as possible to the desired value when the turbine is assembled.

実施例 以下本発明の一実施例を第1図および第2図を参照して
詳細に説明する。
EXAMPLE Hereinafter, an example of the present invention will be described in detail with reference to FIGS. 1 and 2.

第1図は本発明に係る蒸気タービンの組立過程の一例を
示したもので、第2図は第1図の■−■線に沿う断面図
である。
FIG. 1 shows an example of the process of assembling a steam turbine according to the present invention, and FIG. 2 is a cross-sectional view taken along the line ■-■ in FIG.

先ず従来と同様に、タービン車室の下半部1aに翼環2
aやグミー環2bなどの静止部品2の下半分を組付ける
。次に、タービン車室のタービンロータの取付は位置に
、ロータに代えてマンドレル4を据付ける。このマンド
レル4の支持は、ロータの支持軸受を利用することがで
きる。そして、マンドレル4には、軸方向の必要な箇所
すなわち翼環2aやグミー環2bなどの静止部品2に対
応する位置に腕5を取付ける。この腕5の先端には、遠
隔操作が可能な変位計測機6を取付ける。
First, as in the conventional case, a blade ring 2 is attached to the lower half 1a of the turbine casing.
Assemble the lower half of the stationary parts 2 such as a and the gummy ring 2b. Next, a mandrel 4 is installed in place of the rotor at the position where the turbine rotor is to be installed in the turbine casing. This mandrel 4 can be supported using a rotor support bearing. Arms 5 are attached to the mandrel 4 at necessary locations in the axial direction, that is, at positions corresponding to the stationary parts 2 such as the blade ring 2a and the gummy ring 2b. A remote-controlled displacement measuring device 6 is attached to the tip of the arm 5.

なお、変位計測機6としては非接触式のものを用いる場
合を図示したが、状況に応じて可能であれば、ダイヤル
インジケータのような接触式のものを用いてもよい。た
だし、この場合にも遠隔操作が可能なものであることが
必要である。その理由は、タービン車室の上半部を組立
た状態で変位計測機6による計測を必要とするからであ
る。
Although a non-contact type displacement measuring device 6 is shown in the figure, a contact type device such as a dial indicator may be used if possible depending on the situation. However, even in this case, it is necessary that remote control is possible. The reason for this is that measurement by the displacement measuring device 6 is required with the upper half of the turbine casing in an assembled state.

そこで先ず、タービン車室の下半部1aに翼環2aやグ
ミー環2bなどの静止部品2の下半分を組付けた状態(
すなわち遊隙計測状態)で、タービンロータの取付は位
置にセットされたマンドレル4の変位計測機6を用いて
、マンドレル4の軸心から静止部品2までの距離を計測
し、これをG、とする。
Therefore, first, the lower half of the stationary parts 2 such as the blade ring 2a and the gummy ring 2b are assembled to the lower half 1a of the turbine casing (
In other words, when the turbine rotor is installed (in the play measurement state), the distance from the axis of the mandrel 4 to the stationary component 2 is measured using the displacement measuring device 6 of the mandrel 4 set in position, and this is defined as G. do.

次に、タービン車室の下半部la上に、翼環2aやグミ
ー環2bなどの静止部品2の上半分を組付け、更にター
ビン車室の上半部1b(第5図参照)を組付けてタービ
ンの仮組立を完了させる。この状態で、再度マンドレル
4の変位計測機6を用いて、マンドレル4の軸心から静
止部品2までの距離を計測し、これをG、とする。
Next, the upper half of the stationary parts 2 such as the blade ring 2a and the gummy ring 2b are assembled onto the lower half la of the turbine casing, and then the upper half 1b of the turbine casing (see Fig. 5) is assembled. Attach it to complete the temporary assembly of the turbine. In this state, the distance from the axis of the mandrel 4 to the stationary component 2 is measured again using the displacement measuring device 6 of the mandrel 4, and this distance is defined as G.

これらの計測値G+、 Gtの差を求め、遊隙計測時と
仮組立完了時における静止部品2の変位ff1mとする
。すなわち、m=G+  Gyとなる。
The difference between these measured values G+ and Gt is determined and taken as the displacement ff1m of the stationary component 2 at the time of measuring the play and at the time of completion of temporary assembly. That is, m=G+Gy.

その後、タービン車室の上半部1bを開放して、マンド
レル4を取除き、マンドレル4を取除いた後に正規のタ
ービンロータを組付ける。この正規のタービンロータを
組付ける際に、静止部品2とタービンロータ側の回転部
品との隙間を、組立完了時の設計遊隙値に前記変位置m
を加えた値となるように凋整する。
Thereafter, the upper half 1b of the turbine casing is opened, the mandrel 4 is removed, and after the mandrel 4 is removed, a regular turbine rotor is assembled. When assembling this regular turbine rotor, the gap between the stationary part 2 and the rotating part on the turbine rotor side is adjusted to the design clearance value at the time of assembly completion at the displacement position m.
Adjust the value so that it is the sum of .

すなわち、調整時の静止部品2とターヒンロータ例の回
転部品との隙間をδ7、組立完了時の設計遊隙値をδ1
、遊隙計測時と仮組立完了時における静止部品2の変位
置をmとすると、遊隙計測時に、 δ、−δ、十 m    ・ ・ ・(2)となるよう
に、静止部品2とタービンロータ側の回転部品との隙間
を凋整する。
In other words, the gap between the stationary part 2 and the rotating part of the Tahin rotor example during adjustment is δ7, and the design clearance value at the time of assembly completion is δ1.
, if the displacement of the stationary part 2 at the time of play measurement and at the time of completion of temporary assembly is m, then at the time of play measurement, the stationary part 2 and the turbine are adjusted so that δ, -δ, 10 m ・ ・ ・ (2) Reduce the gap between the rotor and the rotating parts.

発明の効果 以上詳述したように、本発明によれば、タービン車室の
仮組立を行い、遊隙計測時と仮組立完了時における静止
部品の変位置を正確に求めることにより、組立完了時に
必要とする静止部品とタービンロータ側の回転部品との
隙間を、遊隙計測時に適正に設定することができる。
Effects of the Invention As detailed above, according to the present invention, by temporarily assembling the turbine casing and accurately determining the displacement position of the stationary parts at the time of play measurement and at the time of completion of the temporary assembly, The required gap between the stationary component and the rotating component on the turbine rotor side can be appropriately set when measuring the play.

従って、本発明によれば、タービンの性能と信頼性を高
めることのできる蒸気タービンの組立方法が提供される
Therefore, according to the present invention, a method for assembling a steam turbine is provided that can improve the performance and reliability of the turbine.

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

第1図は本発明に係る蒸気タービンの組立方法の一実施
例を説明するために、マンドレルによる変位の計測状況
を示したタービン車室の部分的な側面図、第2図は同じ
く本発明を説明するために示した第1図の■−■線に沿
う断面図、第3図ないし第5図は蒸気タービンの組立過
程における静止部品の変位の状況を説明するために示し
たタービン車室の部分的な側面図、第6図は従来のボト
ムリーディング法を説明するために示したタービン車室
の部分的な側面図、第7図は第6図の■−■線に沿う断
面図、第8図および第9図はボトムリーディング法によ
る問題点を説明するために示したタービン車室の部分的
な断面図である。 la・・蒸気タービン車室の下半部、1b・・上半部、
2・・静止部品、2a・・翼環、2b・・ダミー環、3
・・ダイヤルインジケータ、4・・マンドレル、5・・
腕、6・・変位計測機。
FIG. 1 is a partial side view of a turbine casing showing how displacement is measured by a mandrel in order to explain an embodiment of the method of assembling a steam turbine according to the present invention, and FIG. A sectional view taken along the line ■-■ in FIG. 1 shown for explanation, and FIGS. 3 to 5 are views of the turbine casing shown to explain the displacement of stationary parts during the assembly process of the steam turbine. 6 is a partial side view of the turbine casing shown to explain the conventional bottom reading method; FIG. 7 is a sectional view taken along the line ■-■ in FIG. 6; 8 and 9 are partial sectional views of the turbine casing shown for explaining the problems caused by the bottom reading method. la... lower half of the steam turbine casing, 1b... upper half,
2...Stationary parts, 2a...Blade ring, 2b...Dummy ring, 3
...Dial indicator, 4...Mandrel, 5...
Arm, 6...displacement measuring device.

Claims (1)

【特許請求の範囲】[Claims] タービン車室の下半部に翼環やダミー環などの静止部品
の下半分を組付けていわゆる遊隙計測時の状態とする工
程と、タービン車室のタービンロータの取付け位置に要
所に変位計測機が設けられたマンドレルを設置する工程
と、前記変位計測機によってマンドレルの軸心から前記
静止部品までの距離G_1を計測する工程と、タービン
車室の下半部上に前記翼環やダミー環などの静止部品の
上半分を組付けた後タービン車室の上半部を組付けてタ
ービンの仮組立を行う工程と、この状態で前記変位計測
機によってマンドレルの軸心から前記静止部品までの距
離G_2を計測する工程と、これらの計測値G_1、G
_2の差から遊隙計測時とタービンの仮組立完了時とに
おける静止部品の変位置m(m=G_1−G_2)を検
知する工程と、タービン車室の上半部を開放して前記マ
ンドレルを取除く工程と、マンドレルを取除いた後に正
規のタービンロータを組付ける工程とから成り、タービ
ンロータを組付ける際に前記静止部品とタービンロータ
側の回転部品との隙間δ_2を、組立完了時の設計遊隙
値δ_1に前記変位置mを加えた値となるように調整す
るようにしたことを特徴とする蒸気タービンの組立方法
The process involves assembling the lower half of stationary components such as blade rings and dummy rings into the lower half of the turbine casing to create a state for so-called play measurement, and displacing the turbine rotor at key locations in the turbine casing. A step of installing a mandrel equipped with a measuring device, a step of measuring the distance G_1 from the axis of the mandrel to the stationary component using the displacement measuring device, and a step of installing the blade ring or dummy on the lower half of the turbine casing. A process of temporarily assembling the turbine by assembling the upper half of stationary parts such as rings and then assembling the upper half of the turbine casing; The process of measuring the distance G_2 and these measured values G_1, G
A step of detecting the displacement position m (m=G_1-G_2) of the stationary parts between the time of measuring the play and the time of completion of temporary assembly of the turbine from the difference of _2, and opening the upper half of the turbine casing and removing the mandrel. The process consists of a removing process and a process of assembling a regular turbine rotor after removing the mandrel. When assembling the turbine rotor, the gap δ_2 between the stationary part and the rotating part on the turbine rotor side is adjusted to A method for assembling a steam turbine, characterized in that adjustment is made to a value obtained by adding the displacement position m to a design clearance value δ_1.
JP20289489A 1989-08-07 1989-08-07 Assembly of steam turbine Pending JPH0367002A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP20289489A JPH0367002A (en) 1989-08-07 1989-08-07 Assembly of steam turbine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP20289489A JPH0367002A (en) 1989-08-07 1989-08-07 Assembly of steam turbine

Publications (1)

Publication Number Publication Date
JPH0367002A true JPH0367002A (en) 1991-03-22

Family

ID=16464963

Family Applications (1)

Application Number Title Priority Date Filing Date
JP20289489A Pending JPH0367002A (en) 1989-08-07 1989-08-07 Assembly of steam turbine

Country Status (1)

Country Link
JP (1) JPH0367002A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR101148813B1 (en) * 2007-10-23 2012-05-24 미츠비시 쥬고교 가부시키가이샤 Method for demounting blade ring and member for demounting blade ring
CN103210184A (en) * 2011-03-31 2013-07-17 三菱重工业株式会社 Steam turbine casing position adjusting apparatus
JP2018084169A (en) * 2016-11-22 2018-05-31 三菱日立パワーシステムズ株式会社 Method for assembling turbine
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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR101148813B1 (en) * 2007-10-23 2012-05-24 미츠비시 쥬고교 가부시키가이샤 Method for demounting blade ring and member for demounting blade ring
US8276273B2 (en) 2007-10-23 2012-10-02 Mitsubishi Heavy Industries, Ltd. Method for removing blade ring and member for removing blade ring
CN103210184A (en) * 2011-03-31 2013-07-17 三菱重工业株式会社 Steam turbine casing position adjusting apparatus
US9441500B2 (en) 2011-03-31 2016-09-13 Mitsubishi Heavy Industries, Ltd. Steam turbine casing position adjusting apparatus
JP2018084169A (en) * 2016-11-22 2018-05-31 三菱日立パワーシステムズ株式会社 Method for assembling turbine
KR20180118051A (en) 2017-04-20 2018-10-30 미츠비시 히타치 파워 시스템즈 가부시키가이샤 Method of assembling turbine, assembly work supporting system, and control program
EP3392470A1 (en) 2017-04-20 2018-10-24 Mitsubishi Hitachi Power Systems, Ltd. Method of assembling turbine, assembly work supporting system, and control program
US10635086B2 (en) 2017-04-20 2020-04-28 Mitsubishi Hitachi Power Systems, Ltd. Method of assembling turbine, assembly work supporting system, and control program
EP3467271A1 (en) 2017-10-06 2019-04-10 Mitsubishi Hitachi Power Systems, Ltd. Turbine assembling support program, turbine assembling support system, and turbine assembling method
KR20190039857A (en) 2017-10-06 2019-04-16 미츠비시 히타치 파워 시스템즈 가부시키가이샤 Turbine assembly support program, turbine assembly support system and turbine assembly method
CN109630215A (en) * 2017-10-06 2019-04-16 三菱日立电力系统株式会社 Turbine assembles the assemble method of support program, turbine assembling support system and turbine
CN109630215B (en) * 2017-10-06 2021-07-06 三菱动力株式会社 Turbine assembly support program, turbine assembly support system, and turbine assembly method
US11149589B2 (en) 2017-10-06 2021-10-19 Mitsubishi Power, Ltd. Turbine assembly support program, turbine assembly support system, and turbine assembly method using corrected finite element model

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