JPS61218704A - Gland steam pipe device for steam turbine - Google Patents
Gland steam pipe device for steam turbineInfo
- Publication number
- JPS61218704A JPS61218704A JP6352986A JP6352986A JPS61218704A JP S61218704 A JPS61218704 A JP S61218704A JP 6352986 A JP6352986 A JP 6352986A JP 6352986 A JP6352986 A JP 6352986A JP S61218704 A JPS61218704 A JP S61218704A
- Authority
- JP
- Japan
- Prior art keywords
- steam
- pressure side
- gland
- intermediate chamber
- labyrinth packing
- 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
Links
Landscapes
- 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] This 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 that 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 in a timely manner.
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
ツキンお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
Iこしている。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.
A labyrinth packing is usually used to prevent air from leaking or leaking in, and a part of the main steam is supplied as gland steam from the high-pressure side gland to the low-pressure side gland to create a complete airtight seal. I am trying to maintain my gender.
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lに、翼列部2等によって生
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。To explain the conventional gland steam pipe system in terms of the reaction type steam turbine shown in Fig. 1, in the reaction type steam turbine, the axial thrust generated by the blade row parts 2, etc. is transmitted to the axle l provided with the blade row parts 2 in multiple stages. Balance piston 3 for balancing purpose
is equipped with.
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が設けてアル。A labyrinth packing 5 is provided between the balance piston 3 and the casing 4 as an airtight device.
符号7は高圧部ケーシング6と車軸l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l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1】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から
復水器15に入って回収される。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。■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、n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
。Reference numeral 7 denotes a high-pressure side gland part provided between the high-pressure part casing 6 and the axle l, and 9 denotes a low-pressure side gland part provided between the low-pressure part casing 8 and the axle l, each of which constitutes a labyrinth packing. There is. 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 1. 14 is a low pressure casing, and the blade row section 2
The main steam led to the low pressure casing 14 via the condenser 15 enters the condenser 15 through the pipe 16 and is recovered. A main steam bleed pipe 18 bleeds main steam from an intermediate stage of the blade row section 2. ■ is a shaft seal main tube that connects the intermediate parts of the high-pressure side gland section 7 and the low-pressure side gland section 9, and n is the labyrinth packing 5.
This is a balance pipe that connects the rear end of the main steam bleed pipe 18 to the main steam bleed pipe 18.
上記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(9)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ケ水器に導いて回
収し、残りの漏れ蒸気を低圧側グランド[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n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。Through the piping system as described above, a part of the high-temperature, high-pressure main steam supplied to the high-pressure casing 10 flows as leaked steam from the front end A of the labyrinth packing 5 in the direction of the arrow shown 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 further, part of the leaked steam sent from the middle part of the high-pressure side gland part 7 to the shaft seal main pipe (9) is The remaining leaked steam is supplied to the middle part of the low-pressure side gland [9] and is used as sealing steam for the high-pressure side gland part 7 and the low-pressure side gland part 9, respectively. . Among the leaked steam that has flowed out from the labyrinth packing 5, the remaining amount of leaked steam that is not used as sealing steam between the high-pressure side and the low-pressure side gland section 7.9 is combined with the bleed air of the main steam bleed pipe 18 through the balance pipe n. 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あるた
め、翼列部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、高圧車室の主蒸気
温度とほぼ等しい高温蒸気がその才ま高圧側・低圧側グ
ランド部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 ground steam is leaked steam that is discharged after being subjected to the throttling action by the labyrinth packing 5, so unlike the main steam that has passed through the blade cascade and performed expansion work, its temperature drop is extremely low. The high-temperature steam, which is small in size and has a temperature almost equal to the main steam temperature in the high-pressure casing, is then supplied to the high-pressure side and low-pressure side gland sections and the gland steam condenser.
このため、タービン車軸l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、才たケーシング4のグラン
ド部が熱応力により肇形するなど、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った。Therefore, low cycle fatigue and creep occur due to expansion and contraction due to temperature differences on the outer peripheral surface and shaft center of the balancing piston 3, which has a larger diameter than the turbine axle l. There are problems in that the mechanical strength of parts that come in contact with high-temperature steam decreases, 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 bent casing 4 becoming bent due to thermal stress. was there.
さらに、高圧車室からエンタルピの高い主蒸気の系外漏
出による損失や、ケーシングのグランド部が熱゛応力に
より9形してラビリンスパツキン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っ
ていた。Furthermore, losses due to leakage of main steam with high enthalpy from the high-pressure casing to the outside of the system, and the gland of the casing becoming 9-shaped due to thermal stress, increasing the fin gap of the labyrinth packing, reduce the performance of the steam turbine. This was a contributing factor.
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、幽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、貴荷節
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8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か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った。These problems are particularly noticeable when the main steam pressure and temperature conditions are high, and in single-casing steam turbines that have large geometries and do not have a speed stage. A speed gear is provided to reduce the pressure and temperature of the main steam in the high-pressure vehicle compartment, which is the source of leakage steam. However, with such means, a large amount of thermal energy is consumed in the governor stage, which has inferior performance compared to the 8-row section, which further adds to the factors that reduce the performance of the turbine. 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 sealing steam by injecting water into the shaft sealing main tube connecting the high-pressure side gland section 7 and the low-pressure side gland section 9 is also adopted. However, since 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h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 blade row 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 lower the amount of water and supply it to h.
上記の目的は、この発明によれば、ラビリンスパツキン
のケーシング側に中間室を形成するとともに、該中間室
とタービン翼列の抽気段よりも高圧側の中間段とを連通
する接続管を設け、前記高圧側の中間段よりの抽気を前
記中間段を介して、ラビリンスパツキン前端部からの漏
れ蒸気に混入して、ラビリンス後端部へ通流し、ざらに
抽気管と高圧側グランド部および低圧側グランド部とへ
それぞれ分流するようlこして達成される。According to the present invention, an intermediate chamber is formed on the casing side of the labyrinth packing, and a connecting pipe is provided that communicates the intermediate chamber with an intermediate stage on a higher pressure side than the bleed stage of the turbine blade row. The bleed air from the intermediate stage on the high pressure side passes through the intermediate stage, mixes with the steam leaking from the front end of the labyrinth packing, and flows to the rear end of the labyrinth, and connects the bleed air to the high pressure side gland section and the low pressure side. This is achieved by dividing the flow into the ground section.
以下この発明の実施例の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の系統図で
ある。蒸気タービンの構造及び軸封母管、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
をもっ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. Second
The figure is a system diagram of a grand steam pipe showing an embodiment of the present invention. Since the structure of the steam turbine and the arrangement of the shaft seal header tube and the balance tube are the same as those of the conventional example shown in FIG. 1, they will be 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の中
間部でケーシング4側に釣合ピストン3側に開口部Cを
向けて設けられている。17は中間室13と主蒸気抽気
管18の入口@Dより高圧側に寄ったタービン翼列2の
中間段E点とを連通ずる接続管で、E点からの抽気を中
間室13へ通気するためのものである。この場合中間室
13の圧力はE点の圧力と同一となり、またラビリンス
パツキン5の後端部Bの圧力もm2者とほぼ同一の圧力
となる。In FIG. 2, reference numeral 13 denotes an intermediate chamber, which is provided in the middle part of the labyrinth packing 5 between the balance piston 3 and the casing 4, with an opening C facing the casing 4 side and the balance piston 3 side. There is. 17 is a connecting pipe that communicates the intermediate chamber 13 with point E of the intermediate stage of the turbine blade row 2 which is closer to the high pressure side than the inlet @D of the main steam bleed pipe 18, and vents the bleed air from point E to the intermediate chamber 13. It is for. In this case, the pressure in the intermediate chamber 13 will be the same as the pressure at point E, and the pressure at the rear end B of the labyrinth packing 5 will also be approximately the same as that at point m2.
いま、ラビリンスパツキン5の前端部Aと中間室13の
開口部Cとの間の漏れ蒸気量をGl、中間室13の開口
部C(!:ラビリンスバ、キン5の後端部Bとの間の漏
れ蒸気量をG2とする゛と、G t > G2の場合は
、 (Gl−G、)の蒸気量は中間室13から接続管
17を通ってに列部2の中間段に戻され、蒸気量G2
カ中間室13の開口部Cからラビリンスパツキン5の後
端部Bに流れる。これと反対に、Gz>Gtの場合は、
(Gz Gl)の蒸気量が翼列部2高圧側の中間
段E点から接続管17を図示矢印方向に流れて中間室1
3に入り、蒸気tGtと混合した蒸気量G2がラビリン
スパツキン5の後端部Bに流れることになる。Now, the amount of leaked steam between the front end A of the labyrinth seal 5 and the opening C of the intermediate chamber 13 is Gl, and the amount of leakage steam between the opening C of the intermediate chamber 13 (!: between the labyrinth seal and the rear end B of the kin 5 Let G2 be the amount of leaked steam, and if Gt > G2, the amount of steam (Gl-G,) is returned from the intermediate chamber 13 to the intermediate stage of the row section 2 through the connecting pipe 17, Steam amount G2
The liquid flows from the opening C of the intermediate chamber 13 to the rear end B of the labyrinth packing 5. On the contrary, if Gz>Gt,
The amount of steam (Gz Gl) flows from point E of the intermediate stage on the high pressure side of the blade row section 2 through the connecting pipe 17 in the direction of the arrow shown in the figure, and flows into the intermediate chamber 1.
3, and the amount of steam G2 mixed with steam tGt flows to the rear end B of the labyrinth packing 5.
そこで、 G2>Glとするためには、ラビリンスパツ
キンを通る漏れ蒸気量に関して一般に知られている下記
式を用いればよい。Therefore, in order to make G2>Gl, the following formula, which is generally known regarding the amount of steam leaking through the labyrinth packing, may be used.
ここに、Gz漏れ蒸気量 (Kf/S )φ=流’を係
数
F=ラビリンスの環状面積 (コ)
P、=漏れ始め点の蒸気圧力 (N/rrP)P2=漏
れ込み点の蒸気圧力 (N7m )Z=ラビリンスのひ
れ枚数
■+=漏れ始め点の蒸気比容積 −V〜)釣合ピストン
3のラビリンスパツキン5の前端部Aと後端部Bの蒸気
圧力は主蒸気条件側よび主蒸気抽気管の入口部E点の圧
力により定まるから、ラビリンスパツキン5の環状面積
を一定とすれば、中間室13の開口部Cから前端部Aと
後端部Bとの間のひれ枚数を適宜選定して開口部Cの位
置を設定するととも−こ、接続管17と翼列部2の高圧
−の中間段Eとの接続部が適宜の圧力となるように設定
すれば、G2>Glとなるように設定するこ々ができる
。Here, Gz leakage steam amount (Kf/S) φ = flow', coefficient F = annular area of the labyrinth (k) P, = steam pressure at the leakage starting point (N/rrP) P2 = steam pressure at the leakage point ( N7m) Z = Number of fins in the labyrinth ■ + = Steam specific volume at the point where leakage starts -V ~) The steam pressure at the front end A and rear end B of the labyrinth seal 5 of the balancing piston 3 is the main steam condition side and the main steam Since it is determined by the pressure at the inlet point E of the air bleed pipe, if the annular area of the labyrinth packing 5 is constant, the number of fins between the front end A and the rear end B from the opening C of the intermediate chamber 13 is selected as appropriate. If we set the position of the opening C and set the connection part between the connecting pipe 17 and the high-pressure intermediate stage E of the blade row section 2 to an appropriate pressure, then G2>Gl. You can configure settings like this.
従って、中間室13の開口部Cの位置は、図示実施例の
ように、AC間の長さがC8間よりも小さくなるように
設定する。Therefore, the position of the opening C of the intermediate chamber 13 is set so that the length between AC and C8 is smaller than the length between C8 and C8, as in the illustrated embodiment.
このようにすると、高圧車室10からラビリンスパツキ
ン5の前端部Aを経て流入された高温の漏れ蒸気は、接
続管17を通って翼列部2のE中間段から中間室13に
流入した主蒸気と混合してラビリンスパツキン5の後端
部Bへ流れる。接続管17を通る主蒸気は翼列部で膨張
仕事をしたあとの比較的低温の蒸気であるから、中間室
13の開口部Cから後流は減温された漏れ蒸気であり、
これが高圧側グランド部7に供給されたのち、軸封母管
mを経て低圧側グランド部9に供給されて、それぞれの
グランド部の餠じ蒸気とともに、残分は釣合管ρを介し
て抽気管18へ分流される。In this way, high-temperature leaked steam that has flowed from the high-pressure casing 10 through the front end A of the labyrinth packing 5 can be removed from the main steam that has flowed from the intermediate stage E of the blade row section 2 to the intermediate chamber 13 through the connecting pipe 17. It mixes with steam and flows to the rear end B of the labyrinth packing 5. Since the main steam passing through the connecting pipe 17 is relatively low-temperature steam that has undergone expansion work in the blade cascade, the wake from the opening C of the intermediate chamber 13 is leaked steam whose temperature has been reduced.
After this is supplied to the high-pressure side gland section 7, it is supplied to the low-pressure side gland section 9 via the shaft-sealed main pipe m, and the remainder is extracted together with the steam in each gland section via the balance pipe ρ. It is diverted to the trachea 18.
この実施例によると、中間室13は常に低温蒸気で溝さ
れるから、中間室の容積を大きくすることにより、釣合
ピストンの加熱による影響を軽減することができる。According to this embodiment, since the intermediate chamber 13 is always filled with low-temperature steam, by increasing the volume of the intermediate chamber, the influence of heating of the balance piston can be reduced.
この発明は、上述のように、釣合ピストンとケーシング
と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高圧側の中間段とを接
続して、高温の漏れ蒸気を翼列部で膨張仕事をしたあと
の低温蒸気を中間室へ流入させ、中間室からラビリンス
パツキン後端部へ流れるようにして漏れ蒸気を減温する
ように構成されている。従って、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
臂形によるグランド部のラビリンスひれ隙の増大等によ
るタービンの性卯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, and connects this intermediate chamber with the intermediate stage on the high pressure side of the turbine blade row to prevent high-temperature leakage. The structure is such that the low-temperature steam that has undergone expansion work in the blade row section flows into the intermediate chamber, and flows from the intermediate chamber to the rear end of the labyrinth packing to reduce the temperature of the leaked steam. Therefore, according to the present invention, it is possible to lower the gland steam temperature in the high-pressure side gland section and the low-pressure side gland section, which not only solves the strength problems caused by heating of the balance piston and the low-pressure side axle. At the same time, it becomes possible to solve problems such as leakage of main steam with high enthalpy out of the system and a decrease in turbine performance due to an increase in the labyrinth fin gap in the gland part due to the shape of the casing arm. This has the effect of improving performance 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
明の諏$実施例を示すグランド蒸気管系統図・諏鬼−叡
畝双幽裾朗*亀久叢磯狽賑臭水文養へ松吟鶏瞥策鎮匈N
あt2Fig. 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. Hematsuginkeimetsukuchinen匈N
At2
Claims (1)
との間のラビリンスパッキンを通る漏れ蒸気の一部を、
ラビリンスパッ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
ラビリンスパッキンの前記ケーシング側に中間室を形成
するとともに、該中間室と前記タービン翼列の抽気段よ
りも高圧側の中間段とを連通する接続管を設け、前記高
圧側の中間段よりの抽気を前記中間室を介して、前記ラ
ビリンスパッキン前端部からの漏れ蒸気に混入して、前
記ラビリンスパッキン後端部へ通流し、前記抽気管と前
記高圧側グランド部および低圧側グランド部とへそれぞ
れ分流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) Part of the leaked steam passing through the labyrinth packing between the balancing piston and casing installed on the turbine axle is
The rear end of the labyrinth packing is connected to the bleed pipe from the intermediate stage of the turbine blade row through the balance pipe, and
In a steam turbine configured to supply remaining leakage steam to a high-pressure side gland section and a low-pressure side gland section, an intermediate chamber is formed on the casing side of the labyrinth packing, and an air extraction stage between the intermediate chamber and the turbine blade row is formed. A connecting pipe is provided that communicates with the intermediate stage on the higher pressure side, and the bleed air from the intermediate stage on the higher pressure side is mixed with the leaking steam from the front end of the labyrinth packing through the intermediate chamber, and the steam is removed from the labyrinth packing. 1. A gland steam pipe device for a steam turbine, characterized in that the air flows to a rear end portion and branches to the bleed pipe, the high-pressure side gland portion, and the low-pressure side gland portion.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP6352986A JPS61218704A (en) | 1986-03-20 | 1986-03-20 | Gland steam pipe device for steam turbine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP6352986A JPS61218704A (en) | 1986-03-20 | 1986-03-20 | Gland steam pipe device for steam turbine |
Related Parent Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP4186880A Division JPS56138405A (en) | 1980-03-31 | 1980-03-31 | Gland steam pipe device for steam turbine |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS61218704A true JPS61218704A (en) | 1986-09-29 |
JPS6410642B2 JPS6410642B2 (en) | 1989-02-22 |
Family
ID=13231834
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP6352986A Granted JPS61218704A (en) | 1986-03-20 | 1986-03-20 | Gland steam pipe device for steam turbine |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS61218704A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2013119860A (en) * | 2011-12-06 | 2013-06-17 | Man Diesel & Turbo Se | Turbine |
EP2211016A3 (en) * | 2009-01-22 | 2013-09-04 | General Electric Company | Systems, Methods, and Apparatus for Controlling Gas Leaking in a Turbine |
-
1986
- 1986-03-20 JP JP6352986A patent/JPS61218704A/en active Granted
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2211016A3 (en) * | 2009-01-22 | 2013-09-04 | General Electric Company | Systems, Methods, and Apparatus for Controlling Gas Leaking in a Turbine |
JP2013119860A (en) * | 2011-12-06 | 2013-06-17 | Man Diesel & Turbo Se | Turbine |
Also Published As
Publication number | Publication date |
---|---|
JPS6410642B2 (en) | 1989-02-22 |
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