JPS6410642B2 - - Google Patents

Info

Publication number
JPS6410642B2
JPS6410642B2 JP6352986A JP6352986A JPS6410642B2 JP S6410642 B2 JPS6410642 B2 JP S6410642B2 JP 6352986 A JP6352986 A JP 6352986A JP 6352986 A JP6352986 A JP 6352986A JP S6410642 B2 JPS6410642 B2 JP S6410642B2
Authority
JP
Japan
Prior art keywords
steam
pressure side
gland
pipe
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.)
Expired
Application number
JP6352986A
Other languages
Japanese (ja)
Other versions
JPS61218704A (en
Inventor
Takao Yamamoto
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 JP6352986A priority Critical patent/JPS61218704A/en
Publication of JPS61218704A publication Critical patent/JPS61218704A/en
Publication of JPS6410642B2 publication Critical patent/JPS6410642B2/ja
Granted legal-status Critical Current

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  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

PURPOSE:To prevent reduction of the strength of an axle by communicating an intermediate chamber formed in a portion of a labyrinth packing adjacent to the casing and an intermediate stage of an array of turbine blades on the higher pressure side than the bleeding stage. CONSTITUTION:An intermediate chamber 13 is formed in a portion of a labyrinth packing 5 adjacent to the casing 4. The intermediate chamber 13 is communicated through a connecting pipe 17 with an intermediate stage E of an array of turbine blades on the higher pressure side than the bleeding stage D. This causes the bleed from the intermediate stage E to be leaked through the intermediate chamber 13 and mixed with steam, so that the temperature of gland steam is lowered, preventing reduction of the strength of the axle 1 due to heating thereof.

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.

〔従来技術とその問題点〕[Prior art and its problems]

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か
ら復水器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 main steam led to the low pressure casing 14 via the blade row section 2 enters the condenser 15 through a pipe 16 and is recovered. A main steam bleed pipe 18 bleeds main steam from an intermediate stage of the blade row section 2. Reference numeral 20 designates a shaft-sealing main pipe that connects the intermediate portions of the high-pressure side gland portion 7 and the low-pressure side gland portion 9, and 22 represents a balance pipe that connects the rear end of the labyrinth packing 5 and 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。
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 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. or 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脹仕事を
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
温蒸気がそのまま高圧側・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 throttled 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 supplied as is 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
部が熱応力により変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つていた。
Furthermore, losses due to main steam with high enthalpy leaking out of the system from the high-pressure casing, and deformation of the gland section of the casing due to thermal stress, increasing the fin gap of the labyrinth seal, are factors that reduce the performance of the steam turbine. It was becoming.

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 in the high-pressure vehicle interior, 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.

〔発明の目的〕[Purpose of the invention]

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 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 before supplying it.

〔発明の要旨〕[Summary of the invention]

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、さらに抽気管
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にして達成される。
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. Bleed air from the intermediate stage on the high pressure side is passed through the intermediate stage,
This is achieved by mixing the steam leaking from the front end of the labyrinth packing, flowing it to the rear end of the labyrinth, and then branching it to the bleed pipe, the high-pressure side gland section, and the low-pressure side gland 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 system diagram of a gland steam pipe showing an embodiment of the present invention. Since the structure of the steam turbine and the arrangement of the shaft-sealing 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 description thereof 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。1
7は中間室13と主蒸気抽気管18の入口部Dよ
り高圧側に寄つたタービン翼列2の中間段E点と
を連通する接続管で、E点からの抽気を中間室1
3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の圧力も前2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. 1
Reference numeral 7 denotes a connecting pipe that communicates the intermediate chamber 13 with a point E in 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 bleeds air from the point E to the intermediate chamber 1.
This is for ventilation to 3. 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 the former two.

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G1、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との間の漏れ蒸気量をG2とすると、G1
G2の場合は、(G1−G2)の蒸気量は中間室13か
ら接続管17を通つて翼列部2の中間段に戻さ
れ、蒸気量G2が中間室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、G2>G1の場合は、(G2−G1)の蒸気量が
翼列部2に高圧側の中間段E点から接続管17を
図示矢印方向に流れて中間室13に入り、蒸気量
G1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 leaking steam between the front end A of the labyrinth packing 5 and the opening C of the intermediate chamber 13 is G1 , and the amount of leaking steam between the opening C of the intermediate chamber 13 and the rear end B of the labyrinth packing 5 is G1. If the quantity is G 2 , then G 1 >
In the case of G 2 , the amount of steam (G 1 - G 2 ) is returned from the intermediate chamber 13 to the intermediate stage of the blade row section 2 through the connecting pipe 17, and the amount of steam G 2 is returned to the opening C of the intermediate chamber 13. From there, it flows to the rear end B of the labyrinth packing 5. On the other hand, if G 2 > G 1 , the amount of steam (G 2 - G 1 ) flows into the blade row section 2 from point E of the intermediate stage on the high pressure side through the connecting pipe 17 in the direction of the arrow shown in the figure, and flows into the intermediate chamber. 13, steam volume
The amount of steam G 2 mixed with G 1 is labyrinth packing 5
It will flow to the rear end B of.

そこで、G2>G1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 satisfy G 2 >G 1 , the following formula, which is generally known regarding the amount of steam leaking through the labyrinth packing, may be used.

ここに、G=漏れ蒸気量(Kg/S) φ=流量係数 F=ラビリンスの環状面積(m2) P1=漏れ始め点の蒸気圧力(N/m2) P2=漏れ込み点の蒸気圧力(N/m2) Z=ラビリンスのひれ枚数 V1=漏れ始め点の蒸気比容積(m3/Kg) 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および主
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に、接続管17と翼列部2
の高圧側の中間段Eとの接続部が適宜の圧力とな
るように設定すれば、G2>G1となるように設定
することができる。
Here, G = Leakage steam amount (Kg/S) φ = Flow coefficient F = Labyrinth annular area (m 2 ) P 1 = Steam pressure at the leakage start point (N/m 2 ) P 2 = Steam at the leakage point Pressure (N/m 2 ) Z = Number of fins in the labyrinth V 1 = Steam specific volume at the starting point of leakage (m 3 /Kg) The steam pressure at the front end A and rear end B of the labyrinth seal 5 of the balancing piston 3 is Since it is determined by the main steam conditions and the pressure at the inlet point E of the main steam bleed pipe, if the annular area of the labyrinth packing 5 is constant, there is a gap between the opening C of the intermediate chamber 13 and the front end A and the rear end B. The number of fins is appropriately selected and the position of the opening C is set, and the connection pipe 17 and the blade row section 2 are
If the connection part with the intermediate stage E on the high pressure side is set to have an appropriate pressure, it is possible to set G 2 > G 1 .

従つて、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CB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 is smaller than the length between CB, 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を通つて翼列部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脹仕事をしたあ
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20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封じ蒸気とともに、
残分は釣合管22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 into the intermediate chamber 13 from the intermediate stage E of the blade row section 2 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 seal main tube 20, and together with the sealing steam of each gland section,
The remainder is diverted to the bleed pipe 18 via the balance pipe 22.

この実施例によると、中間室13は常に低温蒸
気で満されるから、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, the intermediate chamber 13 is always filled with low-temperature steam, so by increasing the volume of the intermediate chamber, the influence of heating of the balance piston can be reduced.

〔発明の効果〕〔Effect of the invention〕

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
翼列部で膨脹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, 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. and can have the effect of improving reliability.

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

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。 1:タービン車軸、2:翼列部、3:釣合ピス
トン、5:ラビリンスパツキン、7:高圧側グラ
ンド部、9:低圧側グランド部、10:高圧車
室、13:中間室、17:接続管、18:主蒸気
抽気管、20:軸封母管、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: Blade row section, 3: Balancing piston, 5: Labyrinth packing, 7: High pressure side gland section, 9: Low pressure side gland section, 10: High pressure casing, 13: Intermediate chamber, 17: Connection Pipe, 18: Main steam bleed pipe, 20: Shaft-sealed main pipe, 22: Balance pipe.

Claims (1)

【特許請求の範囲】[Claims] 1 タービン車軸に装備した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を通る漏れ蒸
気の一部を、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、前記ラビリンスパツキン前端部からの
漏れ蒸気に混入して、前記ラビリンスパツキン後
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. A part of the leaked steam passing through the labyrinth packing between the balancing piston and the casing installed on the turbine axle is transferred from the rear end of the labyrinth packing to the bleed pipe from the intermediate stage of the turbine blade row via the balancing pipe. 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 on the casing side of the labyrinth packing, and the intermediate chamber and the turbine A connecting pipe is provided that communicates with an intermediate stage on a higher pressure side than the bleed air stage of the blade row, and the bleed air from the intermediate stage on the high pressure side is mixed with the steam leaking from the front end of the labyrinth packing through the intermediate chamber. A gland steam pipe device for a steam turbine, characterized in that the flow is conducted to the rear end portion of the labyrinth packing, and is branched to the bleed pipe, the high-pressure side gland portion, and the low-pressure side gland portion.
JP6352986A 1986-03-20 1986-03-20 Gland steam pipe device for steam turbine Granted JPS61218704A (en)

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 JPS61218704A (en) 1986-09-29
JPS6410642B2 true 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)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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

Also Published As

Publication number Publication date
JPS61218704A (en) 1986-09-29

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