JPS6148613B2 - - Google Patents
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- Publication number
- JPS6148613B2 JPS6148613B2 JP4186880A JP4186880A JPS6148613B2 JP S6148613 B2 JPS6148613 B2 JP S6148613B2 JP 4186880 A JP4186880 A JP 4186880A JP 4186880 A JP4186880 A JP 4186880A JP S6148613 B2 JPS6148613 B2 JP S6148613B2
- Authority
- JP
- Japan
- Prior art keywords
- steam
- pipe
- gland
- pressure side
- halfway
- 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
Links
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- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Description
【発明の詳細な説明】
〔発明が属する技術分野〕
この発明は、蒸気タービンのグランド蒸気管装
置に関し、高温の漏れ蒸気をタービン翼列部から
の低温蒸気と混合してグランド蒸気の温度を低下
させて供給するものである。DETAILED DESCRIPTION OF THE INVENTION [Technical field to which the invention pertains] The present invention relates to a gland steam pipe device for a steam turbine, and the present invention relates to a gland steam pipe device for a steam turbine, which mixes high-temperature leaked steam with low-temperature steam from a turbine blade cascade to lower the temperature of the gland steam. We will supply it to you.
一般に、蒸気タービンの車軸がケーシングを貫
く部分には、高圧側グランド部と低圧側グランド
部とを設けて、空気の漏出と漏入とを防止してい
るが、このグランドパツキンとして通常ラビリン
スパツキンが用いられ、主蒸気の一部をグランド
蒸気として高圧側グランド部から低圧側グランド
部に供給して完全な気密性を保持するようにして
いる。
Generally, the part where the axle of a steam turbine passes through the casing is provided with a high-pressure side gland part and a low-pressure side gland part to prevent air leakage and inflow, but this gland packing is usually a labyrinth packing. Part of the main steam is supplied as gland steam from the high-pressure side gland section to the low-pressure side gland section to maintain complete airtightness.
従来のグランド蒸気管装置を第1図の反動式蒸
気タービンについて説明すると、反動式蒸気ター
ビンでは、複数段の翼列部2を設けた車軸1に、
翼列部2等によつて生ずる軸方向推力をバランス
させる目的で釣合ピストン3が装備されている。
釣合ピストン3とケーシング4との間には、気密
装置としてラビリンスパツキン5が設けてある。
符号7は高圧部ケーシング6と車軸1との間に設
けた高圧側グランド部、9は低圧部ケーシング8
と車軸1との間に設けた低圧側グランド部であ
り、それぞれラビリンスパツキンを構成してい
る。10は高圧車室であり、該高圧車室10には
主蒸気止弁11を介して管路12から主蒸気が供
給される。14は低圧車室であり、翼列部2を経
て低圧車室14に導かれた主蒸気は、管路16等
が復水器15に入つて回収される。18は主蒸気
抽気管であり、翼列部2の中間段から主蒸気を抽
気する。20は高圧側グランド部7及び低圧側グ
ランド部9のそれぞれの中間部を接続する軸封母
管、22はラビリンスパツキン5の後端部と主蒸
気抽気管18とを接続する釣合管である。 A conventional gland steam pipe system will be explained with reference to the reaction type steam turbine shown in FIG.
A balancing piston 3 is provided for the purpose of balancing the axial thrust generated by the blade row section 2 and the like.
A labyrinth packing 5 is provided between the balance piston 3 and the casing 4 as an airtight device.
Reference numeral 7 indicates a high-pressure side gland section provided between the high-pressure section casing 6 and the axle 1, and 9 indicates a low-pressure section casing 8.
and the axle 1, each forming a labyrinth packing. 10 is a high pressure casing, and main steam is supplied to the high pressure casing 10 from a pipe 12 via a main steam stop valve 11. Reference numeral 14 denotes a low pressure casing, and the main steam led to the low pressure casing 14 via the blade row section 2 enters the condenser 15 through a pipe 16 and the like and is recovered. A main steam bleed pipe 18 bleeds main steam from an intermediate stage of the blade row section 2. 20 is a shaft-sealing main tube that connects the intermediate portions of the high-pressure side gland section 7 and the low-pressure side gland section 9, and 22 is a balance pipe that connects the rear end of the labyrinth packing 5 and the main steam bleed pipe 18. .
蒸気のような配管系統により、高圧車室10に
供給された高温・高圧の主蒸気の一部は漏れ蒸気
として図示矢印方向にラビリンスパツキン5の前
端部Aから流入して後端部Bを通過させ、後端部
Bから流出した漏れ蒸気を分岐して高圧側グラン
ド部7に供給し、さらに高圧側グランド部7の中
間部から軸封母管20に送入された漏れ蒸気の一
部を図示しないグランド蒸気復水器に導いて回収
し、残りの漏れ蒸気を低圧側グランド部9の中間
部に供給して、それぞれ高圧側グランド部7と低
圧側グランド部9の封じ蒸気としている。ラビリ
ンスパツキン5から流出した漏れ蒸気のうち、高
圧側・低圧側グランド部7,9の封じ蒸気として
用いられない残量の漏れ蒸気は、釣合管22を経
て主蒸気抽気管18の抽気と合流して回収する
か、あるいは翼列部2の中間段で主蒸気流に導入
する。 A part of the high-temperature, high-pressure main steam supplied to the high-pressure casing 10 through a steam-like piping system flows as leaked steam from the front end A of the labyrinth packing 5 in the direction of the arrow in the figure and passes through the rear end B. The leaked steam flowing out from the rear end part B is branched and supplied to the high-pressure side gland part 7, and a part of the leaked steam fed into the shaft seal main pipe 20 from the middle part of the high-pressure side gland part 7 is further diverted. The remaining leaked steam is introduced into a gland steam condenser (not shown) and collected, and the remaining leaked steam is supplied to the intermediate portion of the low-pressure side gland section 9 to serve as sealing steam for the high-pressure side gland section 7 and the low-pressure side gland section 9, respectively. Among the leaked steam that has flowed out from the labyrinth packing 5, the remaining leaked steam that is not used as sealing steam for the high-pressure side and low-pressure side gland sections 7 and 9 passes through the balance pipe 22 and merges with the bleed air from the main steam bleed pipe 18. Alternatively, it may be introduced into the main steam flow at an intermediate stage of the blade row section 2.
このように従来のグランド蒸気は、ラビリンス
パツキン5により絞り作用を受けて排出される漏
れ蒸気でしるため、翼列部2を通過して膨張仕事
をしたあとの主蒸気と異なり、その温度降下は極
めて小さく、高圧車室10の主蒸気温度とほぼ等
しい高温蒸気がそのまま高圧側・低圧側グランド
部7,9やグランド蒸気復水器に供給されること
になる。 In this way, conventional gland steam is leaked steam that is discharged after being throttled by the labyrinth packing 5, so unlike main steam that has passed through the blade cascade section 2 and done expansion work, its temperature decreases. is extremely small, and high-temperature steam almost equal to the main steam temperature of the high-pressure casing 10 is supplied as it is to the high-pressure side/low-pressure side gland sections 7, 9 and the gland steam condenser.
このため、タービン車軸1よりも直径の大きい
釣合ピストン3の外周面や軸心には温度差に基づ
く膨縮により低サイクル疲労やクリープ等が生ず
るほか、高圧側車軸に比べて直径の大きい低圧側
車軸の端面や軸心が熱衝撃を受けて脆性破壊を生
じたり、またケーシング4のグランド部が熱応力
により変形するなど、高温蒸気に触れる部材の機
械的強度が低下するという問題点があつた。 For this reason, low-cycle fatigue and creep occur on the outer peripheral surface and shaft center of the balancing piston 3, which has a larger diameter than the turbine axle 1, due to expansion and contraction due to temperature differences. There are problems in that the mechanical strength of parts that come in contact with high-temperature steam is reduced, such as the end face and shaft center of the side axle receiving thermal shock and causing brittle fracture, and the gland part of the casing 4 being deformed due to thermal stress. Ta.
さらに、高圧車室10からエンタルピの高い主
蒸気の系外漏出による損失や、ケーシング4のグ
ランド部が熱応力により変形してラビリンスパツ
キン5のひれ隙を増大させること等は、蒸気ター
ビンの性能を低下させる要因となつていた。 Furthermore, losses due to leakage of high-enthalpy main steam from the high-pressure casing 10 to the outside of the system, and deformation of the gland section of the casing 4 due to thermal stress, which increases the fin gap of the labyrinth seal 5, etc., impair the performance of the steam turbine. This was a contributing factor to the decline.
これらの問題点は、主蒸気の圧力、温度条件が
高い場合において、形状寸法が大きく、調速段を
有しない単車室の蒸気タービンでは、特に顕著に
表われるため、負荷能力の大きい調速段を設け、
漏れ蒸気源である高圧車室内の主蒸気の圧力、温
度を低く設計する手段が採られている。しかし、
このような手段では翼列部に比べて性能が劣る調
速段で大きい熱エネルギーが消費されるため、タ
ービンの性能を低下させる要因がさらに加重され
ることになる。また、低圧側グランド部9の封じ
蒸気の温度を低下させるために、高圧側グランド
部7と低圧側グランド部9とを接続する軸封母管
20に注水して減温する手段も採られているが、
注水量が極めて小量であるため、その効果には限
度があるなど、蒸気タービンの運転性と信頼性の
点で問題があつた。 These problems are particularly noticeable in single-casing steam turbines that have large shapes and dimensions and do not have a governor stage when main steam pressure and temperature conditions are high. established,
Measures are taken to reduce the pressure and temperature of the main steam inside the high-pressure vehicle, which is the source of leakage steam. but,
With such means, a large amount of thermal energy is consumed in the governing stage, which has inferior performance compared to the blade row, and thus the factors that reduce the performance of the turbine are further aggravated. In addition, in order to lower the temperature of the sealed steam in the low-pressure side gland section 9, a method of cooling the shaft sealing main tube 20 that connects the high-pressure side gland section 7 and the low-pressure side gland section 9 by injecting water is also adopted. There are, but
Because the amount of water injected was extremely small, its effectiveness was limited, and there were problems with the operability and reliability of the steam turbine.
この発明は、上記のような問題点を解決するた
めになされたものであり、釣合ピストンのラビリ
ンスパツキンに流入する高温の漏れ蒸気にタービ
ン翼列部の低温蒸気を混合してグランド蒸気の温
度を低下させて供給するようにしたものである。
This invention was made to solve the above-mentioned problems, and mixes low-temperature steam from the turbine blade cascade with high-temperature leaked steam flowing into the labyrinth packing of the balancing piston to lower the temperature of the gland steam. It is designed to reduce the amount of water and supply it.
上記の目的は、この発明によれば、ラビリンス
パツキンのケーシング側の中間に中間室を形成す
るとともに、該中間室と釣合管と抽気管との合流
点より上流側で前記抽気管とが連通する接続管を
設け、前記中間室を介して漏れ蒸気の大部分を前
記抽気管へ戻しタービン翼列中間段からの抽気に
混入させて、前記釣合管を介して高圧側グランド
部へ送りさらに低圧側グランド部へ供給するよう
にして達成される。
According to the present invention, an intermediate chamber is formed in the middle of the casing side of the labyrinth packing, and the intermediate chamber communicates with the bleed pipe on the upstream side of the confluence of the balance pipe and the bleed pipe. Most of the leaked steam is returned to the bleed pipe through the intermediate chamber, mixed with the bleed air from the intermediate stage of the turbine blade row, and sent to the high-pressure side gland section via the balance pipe. This is achieved by supplying it to the low-pressure side ground section.
以下、この発明の実施例を図面を参照して説明
する。第2図は、この発明の実施例を示すグラン
ド蒸気管系統図である。蒸気タービンの構造およ
軸封母管、釣合管の配置は第1図の従来例と異な
るところがないから、同一符号をもつて示し詳細
な説明は省略する。
Embodiments of the present invention will be described below with reference to the drawings. FIG. 2 is a grand steam pipe system diagram showing an embodiment of the present invention. Since the structure of the steam turbine and the arrangement of the shaft-sealed main tube and balance tube are the same as those of the conventional example shown in FIG. 1, they are designated by the same reference numerals and detailed explanation will be omitted.
第2図において、符号13は中間室であり、釣
合ピストン3とケーシング4との間のラビリンス
パツキン5のケーシング側でその中間部よりやや
ラビリンスパツキンの後端部に片寄つた位置にあ
つて、釣合ピストン3に対向させて開口部Cを設
ける。17は中間室13と主蒸気抽気管18とを
結合する接続管であり、釣合管22と主蒸気抽気
管18との合流点Hよりも上流側の点Iに接続す
る。 In FIG. 2, reference numeral 13 denotes an intermediate chamber, which is located on the casing side of the labyrinth packing 5 between the balance piston 3 and the casing 4, and is located slightly toward the rear end of the labyrinth packing from the middle part thereof. An opening C is provided facing the balancing piston 3. A connecting pipe 17 connects the intermediate chamber 13 and the main steam bleed pipe 18, and is connected to a point I upstream of the confluence H of the balance pipe 22 and the main steam bleed pipe 18.
このため、高圧車室10からラビリンスパツキ
ン5の前端部Aを経て導入された漏れ蒸気は、中
間室13の開口部Cからその大部分が中間室13
に入り、接続管17を図示矢印方向に流れて主蒸
気抽気管18の抽気と合流するから、中間室13
の開口部Cとラビリンスパツキン5の後端部Bの
間の漏れ蒸気量は極めて僅少となる。従つて、中
間室13の圧力をPC、タービン翼列部2の中間
段Dの圧力をPDおよびラビリンスパツキン5の
後端部Bの圧力をPBとすれば、その圧力関係は
PC>PD>PBとなる。接続管17を経て主蒸気
抽気管18に入つた漏れ蒸気は、翼列部2の中間
段までで膨張仕事をしたあとの比較的低温の抽気
と混合して抽気の温度を若干高くしたのち、釣合
管22を図示矢印方向に流れて高圧側グランド部
7に供給され、さらに高圧側グランド部7の中間
部から軸封母管20を経て低圧グランド部9に供
給され、それぞれ高圧側・低圧側グランド部7,
9の封じ蒸気となる。 Therefore, most of the leaked steam introduced from the high-pressure casing 10 through the front end A of the labyrinth packing 5 is transferred to the intermediate chamber 13 from the opening C of the intermediate chamber 13.
It flows through the connecting pipe 17 in the direction of the arrow shown and merges with the bleed air in the main steam bleed pipe 18, so that the intermediate chamber 13
The amount of steam leaking between the opening C and the rear end B of the labyrinth packing 5 is extremely small. Therefore, if the pressure in the intermediate chamber 13 is P C , the pressure in the intermediate stage D of the turbine blade row 2 is P D , and the pressure at the rear end B of the labyrinth packing 5 is P B , then the pressure relationship is P C >P D >P B. The leaked steam that entered the main steam bleed pipe 18 via the connecting pipe 17 mixes with the relatively low-temperature bleed air that has undergone expansion work up to the intermediate stage of the blade row section 2, raising the temperature of the bleed air slightly, and then It flows through the balancing pipe 22 in the direction of the arrow in the figure and is supplied to the high-pressure side gland section 7, and is further supplied from the middle section of the high-pressure side gland section 7 to the low-pressure gland section 9 via the shaft seal main tube 20, so that the high-pressure side and low-pressure side ground part 7,
9 sealed steam.
このようにして、釣合ピストン3のラビリンス
パツキン5に導入された高温の漏れ蒸気は、中間
室13を介してほぼ全量が主蒸気抽気管18に回
収され、主蒸気抽気管18の比較的低温の抽気に
よつてその大部分が希釈されるため、高温の封じ
蒸気が高圧側・低圧側グランド部7,9に供給さ
れることはない。 In this way, almost all of the high temperature leaked steam introduced into the labyrinth packing 5 of the balancing piston 3 is recovered into the main steam bleed pipe 18 via the intermediate chamber 13, and the relatively low temperature Since most of the steam is diluted by the bleed air, high-temperature sealed steam is not supplied to the high-pressure side and low-pressure side gland sections 7 and 9.
ラビリンスパツキン5の中間室13の開口部C
と後端部Bとの間には、殆ど蒸気流が生じないか
ら、この間の漏れ蒸気がグランド部の封じ蒸気の
温度に与える影響は極めて少ない。 Opening C of intermediate chamber 13 of labyrinth packing 5
Since almost no steam flow occurs between the rear end portion B and the rear end portion B, leaking steam during this period has extremely little influence on the temperature of the sealed steam in the gland portion.
中間室13の開口部Cの位置は、ラビリンスパ
ツキン5の前端部Aと該開口部Cとの間のラビリ
ンスパツキン効果との関係を考慮して適宜の位置
を選定する必要があり、できるだけ後端部Bに近
い位置とするのが望ましい。 The position of the opening C of the intermediate chamber 13 needs to be selected appropriately considering the relationship between the front end A of the labyrinth packing 5 and the opening C, and the labyrinth packing effect. It is desirable to set it at a position close to part B.
図示実施例では、接続管17を主蒸気抽気管1
8と直接接続してあるが、接続管17を主蒸気抽
気管18とは別個に同一の翼列部の圧力点に接続
し、該圧力点より若干低圧側から抽気し、釣合管
へ接続する管路を設けても前記と同様の作用効果
が得られる。 In the illustrated embodiment, the connecting pipe 17 is connected to the main steam bleed pipe 1.
8, but the connecting pipe 17 is connected to the pressure point of the same blade cascade separately from the main steam bleed pipe 18, and air is extracted from a slightly lower pressure side than the pressure point, and then connected to the balance pipe. Even if a conduit is provided, the same effects as described above can be obtained.
この発明は、上述のように、釣合ピストンとケ
ーシングとの間のラビリンスパツキンのケーシン
グ側に中間室を設け、この中間室とタービン翼列
部の中間段からの抽気管とを接続して、高温の漏
れ蒸気を翼列部で膨張仕事をしたあとの低温蒸気
で希釈させて減温するように構成されている。従
つて、この発明によれば、高圧側グランド部およ
び低圧側グランド部のグランド蒸気温度を低下さ
せることができ、釣合ピストンや低圧側車軸の加
熱による強度上の問題点が解決されるだけでな
く、エンタルピの高い主蒸気の系外漏出や、ケー
シングの変形によるグランド部のラビリンスひれ
隙の増大等によるタービンの性能低下の問題点を
同時に解決することが可能となるとともに、蒸気
タービンの運転性と信頼性とを向上させる効果を
得ることができる。
As described above, this invention provides an intermediate chamber on the casing side of the labyrinth packing between the balancing piston and the casing, connects this intermediate chamber with the bleed pipe from the intermediate stage of the turbine blade row, It is configured to reduce the temperature of high-temperature leaked steam by diluting it with low-temperature steam that has undergone expansion work in the blade cascade. Therefore, according to the present invention, the temperature of the gland steam in the high-pressure side gland section and the low-pressure side gland section can be lowered, and the strength problems caused by heating of the balance piston and the low-pressure side axle are solved. This makes it possible to simultaneously solve problems such as leakage of main steam with high enthalpy out of the system and deterioration of turbine performance due to increased labyrinth fin gaps in the gland due to deformation of the casing, and improve operability of the steam turbine. It is possible to obtain the effect of improving both reliability and reliability.
第1図は従来のグランド蒸気管系統図、第2図
はこの発明の実施例を示すグランド蒸気管系統図
である。
1:タービン車軸、2:タービン翼列部、3:
釣合ピストン、4:ケーシング、5:ラビリンス
パツキン、7:高圧側グランド、9:低圧側グラ
ンド部、13:中間室、17:接続管、18:主
蒸気抽気管、22:釣合管。
FIG. 1 is a conventional grand steam pipe system diagram, and FIG. 2 is a grand steam pipe system diagram showing an embodiment of the present invention. 1: Turbine axle, 2: Turbine blade cascade, 3:
Balance piston, 4: casing, 5: labyrinth packing, 7: high pressure side gland, 9: low pressure side gland section, 13: intermediate chamber, 17: connecting pipe, 18: main steam bleed pipe, 22: balancing pipe.
Claims (1)
シングとの間のラビリンスパツキンを通る漏れ蒸
気の1部を、ラビリンスパツキンの後端部から釣
合管を介してタービン翼列の中間段からの抽気管
中へ合流させるとともに、残りの漏れ蒸気を高圧
側グランド部および低圧側グランド部へ供給する
ようにした蒸気タービンにおいて、前記ラビリン
スパツキンの前記ケーシング側の中間に中間室を
形成するとともに、該中間室と前記釣合管と抽気
管との合流点より上流側で前記抽気管とが連通す
る接続管を設け、前記中間室を介して漏れ蒸気の
大部分を前記抽気管へ戻しタービン翼列中間段か
らの抽気に混入させて、前記釣合管を介して高圧
側グランド部へ送り、さらに低圧側グランド部へ
供給するようにしたことを特徴とする蒸気タービ
ンのグランド蒸気管装置。1. A part of the leaked steam passing through the labyrinth packing between the balancing piston and the casing installed on the turbine axle is drained from the rear end of the labyrinth packing through the balancing pipe and into the bleed pipe from the intermediate stage of the turbine blade row. In the steam turbine in which the remaining leaked steam is supplied to the high-pressure side gland section and the low-pressure side gland section, an intermediate chamber is formed in the middle of the labyrinth packing on the casing side, and the remaining leaked steam is connected to the intermediate chamber. A connecting pipe communicating with the bleed pipe is provided upstream of the confluence of the balancing pipe and the bleed pipe, and most of the leaked steam is returned to the bleed pipe via the intermediate chamber from the intermediate stage of the turbine blade row. A gland steam pipe device for a steam turbine, characterized in that the bleed air is mixed with the bleed air and sent to a high-pressure side gland section through the balancing pipe, and further supplied to a low-pressure side gland section.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP4186880A JPS56138405A (en) | 1980-03-31 | 1980-03-31 | Gland steam pipe device for steam turbine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP4186880A JPS56138405A (en) | 1980-03-31 | 1980-03-31 | Gland steam pipe device for steam turbine |
Related Child Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP6352986A Division JPS61218704A (en) | 1986-03-20 | 1986-03-20 | Gland steam pipe device for steam turbine |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS56138405A JPS56138405A (en) | 1981-10-29 |
| JPS6148613B2 true JPS6148613B2 (en) | 1986-10-24 |
Family
ID=12620230
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP4186880A Granted JPS56138405A (en) | 1980-03-31 | 1980-03-31 | Gland steam pipe device for steam turbine |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS56138405A (en) |
Families Citing this family (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5993903A (en) * | 1982-11-22 | 1984-05-30 | Hitachi Ltd | Turbine gland steam attemperator for steam power plant |
| JPS6170103A (en) * | 1984-09-12 | 1986-04-10 | Mitsubishi Heavy Ind Ltd | Steam turbine |
| US4661043A (en) * | 1985-10-23 | 1987-04-28 | Westinghouse Electric Corp. | Steam turbine high pressure vent and seal system |
| JPS63167001A (en) * | 1986-12-26 | 1988-07-11 | Fuji Electric Co Ltd | Reaction turbine |
| JPS63223304A (en) * | 1987-03-11 | 1988-09-16 | Mitsubishi Heavy Ind Ltd | Shaft sealing device for gas expansion turbine |
| US8147185B2 (en) * | 2009-01-22 | 2012-04-03 | General Electric Company | Systems, methods, and apparatus for controlling gas leakage in a turbine |
| DE102011087824A1 (en) * | 2011-12-06 | 2013-06-06 | Man Diesel & Turbo Se | turbine |
| JP5917324B2 (en) | 2012-07-20 | 2016-05-11 | 株式会社東芝 | Turbine and turbine operating method |
-
1980
- 1980-03-31 JP JP4186880A patent/JPS56138405A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS56138405A (en) | 1981-10-29 |
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