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JPS648162B2 - - Google Patents
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JPS648162B2 - - Google Patents

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Publication number
JPS648162B2
JPS648162B2 JP7138781A JP7138781A JPS648162B2 JP S648162 B2 JPS648162 B2 JP S648162B2 JP 7138781 A JP7138781 A JP 7138781A JP 7138781 A JP7138781 A JP 7138781A JP S648162 B2 JPS648162 B2 JP S648162B2
Authority
JP
Japan
Prior art keywords
steam
turbine
cooling
exhaust
temperature
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
JP7138781A
Other languages
Japanese (ja)
Other versions
JPS57188707A (en
Inventor
Shinichi Morya
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 JP7138781A priority Critical patent/JPS57188707A/en
Publication of JPS57188707A publication Critical patent/JPS57188707A/en
Publication of JPS648162B2 publication Critical patent/JPS648162B2/ja
Granted 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
    • F01D25/24Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/26Double casings; Measures against temperature strain in casings

Landscapes

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

Description

【発明の詳細な説明】 本発明は超高温蒸気タービンにおける内部車室
水平フランジ締付ボルトの冷却方法に関するもの
である。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a method for cooling internal casing horizontal flange fastening bolts in an ultra-high temperature steam turbine.

内部車室と外部車室との二重車室構造を備えた
蒸気タービンにおける内部車室の水平フランジ締
付ボルトの冷却は、従来一般に第1図のような方
法が用いられている。
BACKGROUND ART Conventionally, a method as shown in FIG. 1 has been generally used to cool horizontal flange tightening bolts of an inner casing in a steam turbine having a double casing structure of an inner casing and an outer casing.

この図は内部車室13を上下に分解して上半部
を取除き、タービンロータを取除いた状態を示し
ている。内部車室13の上,下半部を結合するた
め、内部車室13の水平フランジ37にはタービ
ン軸の中心線ABを挾んで両側にボルト孔29
a,29b……29gが設けられ、比較的大きい
遊隙を介して締付ボルト28a,28b……28
gが挿通されている。
This figure shows a state in which the internal casing 13 has been disassembled into upper and lower parts, the upper half has been removed, and the turbine rotor has been removed. In order to connect the upper and lower halves of the internal casing 13, bolt holes 29 are provided on both sides of the horizontal flange 37 of the internal casing 13, sandwiching the center line AB of the turbine shaft.
a, 29b...29g are provided, and tightening bolts 28a, 28b...28 are provided through a relatively large play.
g is inserted.

図においてA側は高圧蒸気の流入側、B側は排
気側である。A側からB側に至る蒸気流路の途中
に冷却蒸気取入孔30を設け、付記矢印のごとく
ボルト28c,28d……28gを順次に通過し
た後、冷却蒸気出口32を経て外部車室11内に
流出する冷却蒸気流路が設けられている。
In the figure, side A is the high-pressure steam inflow side, and side B is the exhaust side. A cooling steam intake hole 30 is provided in the middle of the steam flow path from the A side to the B side, and after passing through the bolts 28c, 28d, . A cooling steam flow path is provided which exits into the chamber.

上記の構造から容易に理解されるように、ター
ビン排気側に近いボルト28aおよび同28bは
冷却されない。このような構造が用いられている
理由は次のごとくである。
As can be easily understood from the above structure, the bolts 28a and 28b near the turbine exhaust side are not cooled. The reason why such a structure is used is as follows.

(イ) タービンの駆動蒸気はA側からB側に流動し
つつ圧力・温度が降下する。従つてタービンを
構成している部材もA側は高温、B側は低温で
あり、締付ボルトも左方から28a,28b…
…28gの順に高温となる。このため、左端付
近の締付ボルト28a,28bは冷却の必要度
が小さい。
(a) The driving steam of the turbine flows from side A to side B, and its pressure and temperature drop. Therefore, the members that make up the turbine are high temperature on the A side and low temperature on the B side, and the tightening bolts are also 28a, 28b, etc. from the left.
...The temperature increases in the order of 28g. Therefore, the tightening bolts 28a and 28b near the left end require less cooling.

(ロ) 冷却蒸気取入孔30から冷却蒸気を取り入れ
て冷却蒸気出口32から外部車室11内に放出
するためには、冷却蒸気取入孔30を外部車室
11内の圧力よりも若干高圧の個所に連通させ
ねばならない。即ち、このタービンの排気側に
おける蒸気の圧力は外部車室11内の圧力と等
しいので、タービン排気を用いて冷却しようと
しても、排気には冷却蒸気出口32まで流動す
るに必要な差圧が無い。
(b) In order to take in cooling steam from the cooling steam intake hole 30 and release it into the external compartment 11 from the cooling steam outlet 32, the cooling steam intake hole 30 is heated to a pressure slightly higher than the pressure inside the external compartment 11. It must be connected to the location. That is, since the pressure of the steam on the exhaust side of this turbine is equal to the pressure inside the external casing 11, even if an attempt is made to use the turbine exhaust for cooling, the exhaust does not have the differential pressure necessary to flow to the cooling steam outlet 32. .

従来、一般の高温蒸気タービンにおいては、前
述の第1図のような締付ボルト冷却方法で実用上
充分であつたが、近時、570℃以上の超高温ター
ビンが開発されるに伴い、前述のような締付ボル
ト冷却方法では不充分となり、内部車室の水平フ
ランジ締付ボルトの全数を排気蒸気で冷却する必
要を生じた。その事情を次に略述する。
Conventionally, for general high-temperature steam turbines, the tightening bolt cooling method shown in Figure 1 described above was practically sufficient, but with the recent development of ultra-high temperature turbines of 570°C or higher, This method of cooling the tightening bolts was insufficient, and it became necessary to cool all the horizontal flange tightening bolts in the internal casing with exhaust steam. The circumstances are briefly explained below.

たとえば、主蒸気温度650℃、排気温度約530℃
といつた超高温高圧タービンにおいては、主蒸気
圧力も350Kg/cm2・gというように、従来の246
Kg/cm2・g程度の高圧タービンに比して約1.4倍
となり、締付ボルトに生じる応力も大きくなつて
いる。
For example, main steam temperature 650℃, exhaust temperature approximately 530℃
In ultra-high temperature and high pressure turbines, the main steam pressure is 350Kg/ cm2・g, compared to the conventional 246Kg/cm2・g.
This is approximately 1.4 times the pressure of a high-pressure turbine (kg/ cm2.g ), and the stress generated in the tightening bolts is also greater.

一方、耐熱高抗張力ボルトの材料的な改良も行
われているが、現状において約570℃が実用的に
耐えられる限度である。従つて前記のように主蒸
気温度650℃程度の超高温蒸気を使用するには、
従来のような冷却方法(第1図)では充分でな
い。
On the other hand, improvements have been made to the materials of heat-resistant, high-tensile strength bolts, but at present the maximum temperature that they can practically withstand is approximately 570°C. Therefore, as mentioned above, in order to use ultra-high temperature steam with a main steam temperature of about 650℃,
Conventional cooling methods (Fig. 1) are not sufficient.

上述の超高温高圧タービンは第2図のようにし
て発電プラントの構成機器として使用される。
The above-mentioned ultra-high temperature and high pressure turbine is used as a component of a power generation plant as shown in FIG.

超高温高圧蒸気はスーパーヒータ1から超高温
高圧タービン2に供給される。この超高温高圧タ
ービン2は、高圧タービン4、中圧タービン6、
および低圧タービン7と同一軸心状に直結されて
発電機9を駆動する。
The super high temperature and high pressure steam is supplied from the super heater 1 to the super high temperature and high pressure turbine 2 . This ultra high temperature high pressure turbine 2 includes a high pressure turbine 4, an intermediate pressure turbine 6,
It is directly connected coaxially with the low pressure turbine 7 to drive the generator 9.

超高温高圧タービン2の排気は第1段再熱器3
を経て高圧タービン4に供給され、その排気は第
2段再熱器5を経て中圧タービン6に、次いで低
圧タービン7に供給され、その排気は復水器8に
導かれる。
The exhaust gas of the ultra-high temperature and high pressure turbine 2 is sent to the first stage reheater 3.
The exhaust gas is supplied to a high pressure turbine 4 via a second stage reheater 5, and then to an intermediate pressure turbine 6, and then to a low pressure turbine 7, and the exhaust gas is led to a condenser 8.

以上のように用いられる超高温高圧タービン2
の冷却用蒸気としては、当該タービン2の排気を
使用することが最も望ましい。たとえば矢印Cの
ようにスーパーヒータ1の入口から高圧低温の蒸
気を抽出して超高温高圧タービン2の冷却用蒸気
として用いようとすると、配管系統の構造および
超高温高圧タービン2の内部構造が複雑となるの
で好ましくない。
Ultra high temperature and high pressure turbine 2 used as described above
It is most desirable to use the exhaust gas of the turbine 2 as the cooling steam. For example, if you try to extract high-pressure, low-temperature steam from the inlet of the superheater 1 as shown by arrow C and use it as cooling steam for the ultra-high-temperature, high-pressure turbine 2, the structure of the piping system and the internal structure of the ultra-high-temperature, high-pressure turbine 2 will be complicated. This is not desirable.

本発明は以上の事情に鑑みて為され、その目的
とするところは、二重車室構造を有する蒸気ター
ビンにおいて、当該タービンの排気を用いて、内
部車室水平フランジ締付ボルトの全数を、簡単な
構成で有効に冷却し得る方法を提供しようとする
ものである。
The present invention has been made in view of the above-mentioned circumstances, and its purpose is to tighten all the internal casing horizontal flange tightening bolts in a steam turbine having a double casing structure using the exhaust gas of the turbine. The purpose of this invention is to provide a method that can perform effective cooling with a simple configuration.

第3図は、第4図と第5図とについて後述する
ごとく本発明を適用すべき超高温高圧タービンの
全体的構造を示す縦断面図である。
FIG. 3 is a longitudinal sectional view showing the overall structure of an ultra-high temperature and high pressure turbine to which the present invention is applied, as will be described later with reference to FIGS. 4 and 5.

350Kg/cm2・g,650℃の蒸気は主蒸気入口管1
0に供給され、耐熱のため球形に作られた外部車
室11の壁を貫通し、内部車室13内に設けられ
たノズルボツクス14に導かれる。
350Kg/cm 2・g, 650℃ steam is main steam inlet pipe 1
0, penetrates the wall of an external chamber 11 made into a spherical shape for heat resistance, and is guided to a nozzle box 14 provided in an internal chamber 13.

上記のノズルボツクス14および数段からなる
ダイヤフラム17で加速された蒸気は動翼16を
回転させてロータ15に回転エネルギーを与え、
約530℃の排気となつて外部車室11内に流出し、
排気口25から次の機器(第1段再加熱器)に流
動する。12は伸縮継手、18,19,20はシ
ヤフトグランド、21,22は主軸受、23,2
4はメカニカルシールである。
The steam accelerated by the nozzle box 14 and the diaphragm 17 consisting of several stages rotates the rotor blades 16 and gives rotational energy to the rotor 15.
Exhaust gas with a temperature of approximately 530°C flows into the external compartment 11,
It flows from the exhaust port 25 to the next device (first stage reheater). 12 is an expansion joint, 18, 19, 20 is a shaft gland, 21, 22 is a main bearing, 23, 2
4 is a mechanical seal.

本発明は、前記の目的を達成するため、当該タ
ービンの排気蒸気を冷却蒸気として用い、これを
水平フランジ締付ボルトの排気側締付ボルトから
順次に主蒸気入口側締付ボルトに流動させるとと
もに、上記の排気側締付ボルトを通過した蒸気を
タービンロータのシヤフトグランド中間抽出ライ
ンに連通せしめることにより、前記の冷却用蒸気
の流路の出,入口間に流動に必要な差圧を生じさ
せ、内部車室の水平フランジ締付ボルト全数を低
温の排気蒸気で冷却することを特徴とする。
In order to achieve the above object, the present invention uses the exhaust steam of the turbine as cooling steam, and sequentially flows this from the exhaust side tightening bolt of the horizontal flange tightening bolt to the main steam inlet side tightening bolt. By communicating the steam that has passed through the exhaust side tightening bolt to the shaft gland intermediate extraction line of the turbine rotor, a pressure difference necessary for flow is created between the outlet and inlet of the cooling steam flow path. , all horizontal flange tightening bolts in the internal compartment are cooled with low-temperature exhaust steam.

次に、本発明の一実施例を第4図および第5図
について説明する。
Next, an embodiment of the present invention will be described with reference to FIGS. 4 and 5.

第4図は、第3図に示した超高温高圧蒸気ター
ビンに本発明にかかる冷却方法を適用するために
構成した冷却蒸気流路部分を含む縦断面であり、
第5図は、外部車室の上半と内部車室の上半とを
取り外し、ロータの中央部を切除した状態の平面
図で、従来の冷却方法を用いた第1図と対応する
図である。
FIG. 4 is a vertical cross section including a cooling steam flow path portion configured to apply the cooling method according to the present invention to the ultra-high temperature and high pressure steam turbine shown in FIG. 3;
Figure 5 is a plan view of the rotor with the upper half of the outer compartment and the upper half of the internal compartment removed and the central part of the rotor cut out, and corresponds to Figure 1 using the conventional cooling method. be.

本発明においては、冷却用の蒸気を当該タービ
ンを駆動している蒸気を途中から抽出することな
く、駆動を終つた排気を用いる。即ち、二重構造
車室からなる蒸気タービンにおいて、内部車室内
で仕事を終つて外部車室の中に流出した蒸気を冷
却用の蒸気として用いる。
In the present invention, the exhaust gas that has finished driving the turbine is used as the cooling steam without extracting the steam that is driving the turbine from the middle. That is, in a steam turbine having a double-structured casing, steam that has completed its work in the inner casing and flows out into the outer casing is used as cooling steam.

従来の方法は第1図のように段落の途中から蒸
気を分流させて冷却を行つたので、冷却蒸気出口
32を外部車室11内に開口せしめておくことに
よつて冷却蒸気流を生ぜしめるための差圧が得ら
れたが、本発明においては前述のように外部車室
内の排気を冷却用蒸気として用いるために、冷却
蒸気流路の末端を外部車室内よりも圧力の低い個
所に連通させねば冷却蒸気の流動に必要な差圧が
得られない。本発明においては、冷却を終つた蒸
気を、タービンロータのシヤフトグランド中間抽
出ラインに流出せしめて上記の差圧を生じさせ
る。
In the conventional method, as shown in FIG. 1, cooling was performed by separating steam from the middle of the paragraph, so by opening the cooling steam outlet 32 into the external compartment 11, a cooling steam flow was generated. However, in the present invention, as mentioned above, in order to use the exhaust gas inside the external vehicle compartment as cooling steam, the end of the cooling steam flow path is connected to a location where the pressure is lower than that in the external compartment. Otherwise, the differential pressure necessary for the flow of cooling steam cannot be obtained. In the present invention, the steam that has been cooled is allowed to flow out into the shaft gland intermediate extraction line of the turbine rotor to generate the above-mentioned differential pressure.

上述の方法の一例を第5図について具体的に説
明すると次のごとくである。高圧側シヤフトグラ
ンドのパツキングは、一般に、No.1パツキング1
9aとNo.2パツキング19bとに区分され、その
中間に形成される蒸気だめ35に中間リーク抽出
口36を設けて差圧調整が行われる。本例におい
ては冷却蒸気出口32′を連絡管33と蒸気通路
34とによつて前記の中間リーク抽出口36に接
続する。これにより、前記のNo.1パツキング19
aが受け持つている差圧が冷却蒸気取入口30′
と冷却蒸気出口32′との間にかかり、外部車室
11内の蒸気の一部が次記に詳述する冷却流路を
経て中間リーク蒸気抽出口36に流動する。本例
においては、蒸気抽出口36から流出した蒸気を
給水予熱に利用して熱経済の向上をはかつてい
る。
An example of the above method will be specifically explained with reference to FIG. 5 as follows. The packing of the shaft gland on the high pressure side is generally No. 1 packing 1.
9a and No. 2 packing 19b, and an intermediate leak extraction port 36 is provided in a steam reservoir 35 formed in the middle to adjust the differential pressure. In this example, the cooling steam outlet 32' is connected to the intermediate leak extraction port 36 by a connecting pipe 33 and a steam passage 34. As a result, the above-mentioned No. 1 Packing 19
The differential pressure handled by a is the cooling steam intake 30'
and the cooling steam outlet 32', and a portion of the steam in the outer casing 11 flows to the intermediate leak steam extraction port 36 via a cooling passage described in detail below. In this example, the steam flowing out from the steam extraction port 36 is used to preheat the feed water, thereby improving the heat economy.

本発明は、上述のようにして得られた差圧で流
動する冷却蒸気流を、内部車室水平フランジ37
の排気側締付ボルト28aから順次に主蒸気入口
側締付ボルト28gまで、全部の締付ボルトを経
由して流動せしめる。
The present invention directs the cooling vapor flow flowing under the differential pressure obtained as described above to the internal casing horizontal flange 37.
The flow is made to flow through all the tightening bolts sequentially from the exhaust side tightening bolt 28a to the main steam inlet side tightening bolt 28g.

本例においては、締付ボルト28a,28aか
ら同28g,28gまで、各7本の締付ボルトが
2列に配設されているので、各例ごとに、排気側
の締付ボルト28aから順次に同28b,同28
c,…を経て最後に主蒸気入口側の締付ボルト2
8gの冷却を行わせるように流路を形成してあ
る。
In this example, seven tightening bolts are arranged in two rows from tightening bolts 28a, 28a to 28g, 28g, so for each example, the tightening bolts 28a on the exhaust side are 28b, 28
c,... and finally tightening bolt 2 on the main steam inlet side.
A flow path was formed to cool 8 g.

各締付ボルトに供給される冷却蒸気流は、水平
面内では第5図に矢印で示したようにボルトの切
線方向に吹きつけられて回転流を生じ、垂直面内
では第4図に矢印で示したように締付ボルトの長
さ方向に沿つて交互に上向き,下向きに流れ、各
締付ボルトと充分に接触してこれを冷却する。
The cooling steam flow supplied to each tightening bolt is blown in the tangential direction of the bolt in the horizontal plane as shown by the arrow in Fig. 5, creating a rotational flow, and in the vertical plane as shown by the arrow in Fig. 4. As shown, the flow alternately flows upward and downward along the length of the tightening bolts, sufficiently contacting each tightening bolt to cool it.

各列の締付ボルトは主蒸気入口側に近いものほ
ど周囲温度が高く、締付ボルト28a→28gの
順に高熱を受けている。本例では上記と同じ順序
に冷却蒸気を流すので次記のように冷却が行われ
る。例えば締付ボルト28bを冷却した蒸気は、
同ボルトの熱を吸収して昇温するとともに膨脹に
のる温度降下によつて上記の昇温が若干緩和さ
れ、次の締付ボルト28cに吹きつけられる。こ
の締付ボルト28cは前行程の締付ボルト28b
よりも高熱を受けているので、前行程の締付ボル
ト28bに触れて若干昇温した蒸気で冷却するこ
とが全体的なバランスから見て合理的である。こ
のように各締付ボルトごとに、全体的なバランス
に適つた冷却が行われる。
The closer the tightening bolts in each row are to the main steam inlet side, the higher the ambient temperature is, and the tightening bolts 28a to 28g receive high heat in this order. In this example, since the cooling steam is flowed in the same order as above, cooling is performed as follows. For example, the steam that cooled the tightening bolt 28b is
The heat of the bolt is absorbed and the temperature rises, and the above temperature rise is slightly alleviated by the temperature drop caused by the expansion, and then the bolt is blown onto the next tightening bolt 28c. This tightening bolt 28c is the tightening bolt 28b of the previous stroke.
Since the heat is higher than that of the bolt 28b, it is reasonable from the overall balance point of view to cool it with the steam that has slightly risen in temperature when it touches the tightening bolt 28b in the previous process. In this way, each tightening bolt is cooled in a way that is appropriate for the overall balance.

以上説明したように、本発明は、内部車室と外
部車室との二重構造からなる蒸気タービンにおい
て、内部車室の水平フランジ締付ボルトの冷却蒸
気源として当該蒸気タービンの排気蒸気を用い、
上記の排気蒸気を水平フランジの排気側締付ボル
トから順次に主蒸気入口側締付ボルトに流動させ
るとともに、上記の排気側締付ボルトを通過し終
つた蒸気をタービンロータのシヤフトグランド中
間抽出ラインに流出せしめて前記の冷却用蒸気を
流動させるための差圧を生じさせることにより、
簡単な構成で内部車室水平フランジの締付ボルト
全数を当該蒸気タービンの排気を用いて有効に、
かつ、経済的に冷却することができる。
As explained above, the present invention provides a steam turbine having a dual structure of an inner casing and an outer casing, in which exhaust steam of the steam turbine is used as a cooling steam source for horizontal flange tightening bolts in the inner casing. ,
The above exhaust steam is made to flow sequentially from the exhaust side tightening bolt of the horizontal flange to the main steam inlet side tightening bolt, and the steam that has passed through the above exhaust side tightening bolt is sent to the shaft gland intermediate extraction line of the turbine rotor. By creating a pressure difference to cause the cooling steam to flow,
With a simple configuration, all the tightening bolts on the horizontal flange of the internal casing can be effectively tightened using the exhaust gas of the steam turbine.
Moreover, it can be cooled economically.

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

第1図は従来一般に用いられている蒸気タービ
ンの分解平面図、第2図は超高温高圧蒸気タービ
ンを用いた発電プラントの系統図、第3図は超高
温高圧タービンの縦断面図、第4図は本発明に係
るボルトクーリング方法を実施できるように構成
した超高温高圧蒸気タービンの縦断面図、第5図
は同、一部を切断した分解平面図である。 11……外部車室、13……内部車室、18,
19……高圧側シヤフトグランド、19a……高
圧側シヤフトグランドのNo.1パツキング、19b
……同No.2パツキング、20……低圧側シヤフト
グランド、28a,28b〜28g……水平フラ
ンジ締付ボルト、29a,29b〜29g……同
ボルト孔、30,30′……冷却蒸気取入口、3
2,32′……冷却蒸気出口、33……連絡管、
36……中間リーク蒸気抽出口、37……水平フ
ランジ。
Figure 1 is an exploded plan view of a steam turbine commonly used in the past, Figure 2 is a system diagram of a power generation plant using an ultra-high-temperature, high-pressure steam turbine, Figure 3 is a longitudinal cross-sectional view of an ultra-high-temperature, high-pressure turbine, and Figure 4 The figure is a longitudinal cross-sectional view of an ultra-high-temperature, high-pressure steam turbine configured to implement the bolt cooling method according to the present invention, and FIG. 5 is an exploded plan view, partially cut away, of the same. 11...External compartment, 13...Internal compartment, 18,
19...High pressure side shaft gland, 19a...High pressure side shaft gland No.1 packing, 19b
...Same No. 2 packing, 20...Low pressure side shaft gland, 28a, 28b to 28g...Horizontal flange tightening bolt, 29a, 29b to 29g...Same bolt hole, 30, 30'...Cooling steam intake ,3
2, 32'... Cooling steam outlet, 33... Communication pipe,
36...Intermediate leak steam extraction port, 37...Horizontal flange.

Claims (1)

【特許請求の範囲】[Claims] 1 内部車室と外部車室との二重車室構造からな
る蒸気タービンにおいて、上記蒸気タービンの排
気蒸気を前記内部車室の水平フランジ締付ボルト
の冷却用蒸気として使用し、前記の排気蒸気を水
平フランジの排気側締付ボルトから順次に主蒸気
入口側締付ボルトまで流動せしめるとともに、排
気側締付ボルトを通過し終つた蒸気をタービンロ
ータのシヤフトグランド中間抽出ラインに流出せ
しめることにより前記冷却用蒸気の流路の出,入
口間に適宜の差圧を生じさせて、内部車室の水平
フランジ締付ボルトの全数を排気蒸気で冷却する
ことを特徴とする蒸気タービンにおけるボルトク
ーリング方法。
1. In a steam turbine having a double casing structure of an inner casing and an outer casing, the exhaust steam of the steam turbine is used as cooling steam for horizontal flange tightening bolts of the inner casing, and the exhaust steam is The steam is made to flow sequentially from the exhaust side tightening bolt of the horizontal flange to the main steam inlet side tightening bolt, and the steam that has passed through the exhaust side tightening bolt is allowed to flow out to the shaft gland intermediate extraction line of the turbine rotor. 1. A method for bolt cooling in a steam turbine, characterized in that all horizontal flange fastening bolts in an internal casing are cooled with exhaust steam by creating an appropriate differential pressure between the outlet and inlet of a cooling steam flow path.
JP7138781A 1981-05-14 1981-05-14 Cleaning method of steam turbine bolt Granted JPS57188707A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP7138781A JPS57188707A (en) 1981-05-14 1981-05-14 Cleaning method of steam turbine bolt

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP7138781A JPS57188707A (en) 1981-05-14 1981-05-14 Cleaning method of steam turbine bolt

Publications (2)

Publication Number Publication Date
JPS57188707A JPS57188707A (en) 1982-11-19
JPS648162B2 true JPS648162B2 (en) 1989-02-13

Family

ID=13459042

Family Applications (1)

Application Number Title Priority Date Filing Date
JP7138781A Granted JPS57188707A (en) 1981-05-14 1981-05-14 Cleaning method of steam turbine bolt

Country Status (1)

Country Link
JP (1) JPS57188707A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH044663U (en) * 1990-04-27 1992-01-16

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH044663U (en) * 1990-04-27 1992-01-16

Also Published As

Publication number Publication date
JPS57188707A (en) 1982-11-19

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