JPS5918208A - Labyrinth packing - Google Patents

Labyrinth packing

Info

Publication number
JPS5918208A
JPS5918208A JP12592382A JP12592382A JPS5918208A JP S5918208 A JPS5918208 A JP S5918208A JP 12592382 A JP12592382 A JP 12592382A JP 12592382 A JP12592382 A JP 12592382A JP S5918208 A JPS5918208 A JP S5918208A
Authority
JP
Japan
Prior art keywords
packing
fin
turbine
leakage
rotor
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
JP12592382A
Other languages
Japanese (ja)
Inventor
Miharu Fukazawa
深沢 美治
Mitsuo Kawai
光雄 河合
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.)
Toshiba Corp
Original Assignee
Toshiba Corp
Tokyo Shibaura 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 Toshiba Corp, Tokyo Shibaura Electric Co Ltd filed Critical Toshiba Corp
Priority to JP12592382A priority Critical patent/JPS5918208A/en
Publication of JPS5918208A publication Critical patent/JPS5918208A/en
Pending 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
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/02Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00Materials; Properties thereof
    • F05D2300/50Intrinsic material properties or characteristics
    • F05D2300/505Shape memory behaviour

Abstract

PURPOSE:To reduce the leakage of turbine working fluid by a method wherein a packing fin for composing a narrow part and an enlarged part on a leakage passage of the turbine working fluid is formed by a shape memory alloy which displaces the packing fin toward the direction narrowing the leakage passage under high temperature environment. CONSTITUTION:Plural circumferential grooves 2 are provided on a surface of a turbine rotor 1, and a packing ring 4 is fixed on a casing 3 by an expansion and contraction member 5. Plural packing fins 6 are provided on a surface opposing to the rotor 1 of the packing ring 4, a narrow part of the leakage passage is formed by a clearance between the top ends of the fins 6 and the surface of the rotor 1, also an enlarged part is formed by respectively adjacent each fin 6. In this case, said fins 6 are formed by a shape memory alloy which stores the configuration to displace said fins 6 toward the direction narrowing the clearance between the top ends of the fins 6 and the surface of the rotor 1. Thereby, the narrow part of the leakage passage can be adequately maintained at all time.

Description

【発明の詳細な説明】 〔発明の技術分野〕 本発明は蒸気タービン等に用いられるラビリンスパツキ
ンに関する。
DETAILED DESCRIPTION OF THE INVENTION [Technical Field of the Invention] The present invention relates to a labyrinth packing used in steam turbines and the like.

〔発明の技術的背景とその問題点〕[Technical background of the invention and its problems]

一般にタービンのタービン作動流体、例えば蒸気の漏洩
防止のために各種パツキンが用いられている。例えば蒸
気タービンのタービンロータとケーシングとの隙間等で
生じるロータ軸線方向に沿つた蒸気の漏洩通路からの漏
洩を防止するために用いられるものにラビリンスパツキ
ンがある。このラビリンスパツキンは、タービンロータ
の表面にタービンロータの軸と同軸の円周溝が多数膜け
られ、ケーシングに一端が固定されたパツキンフィンの
他端が自由端として溝が設けられたタービンロータ表面
に近接するように設けられている。
Generally, various gaskets are used to prevent leakage of turbine working fluid, such as steam, of a turbine. For example, a labyrinth packing is used to prevent leakage of steam from a leakage passage along the rotor axis that occurs in a gap between a turbine rotor and a casing of a steam turbine. This labyrinth seal has many circumferential grooves on the surface of the turbine rotor that are coaxial with the axis of the turbine rotor, and one end of the labyrinth fin is fixed to the casing.The other end of the labyrinth fin is a free end. is located close to.

このパツキンフィンはタービンロータ軸方向に複数個設
けられ、タービンロータとケーシングとの隙間に狭部、
拡大部を多数形成する。
A plurality of these packing fins are provided in the axial direction of the turbine rotor, and are installed in narrow parts in the gap between the turbine rotor and the casing.
A large number of enlarged portions are formed.

このようにラビリンスパツキンが設けられていると、漏
洩する蒸気が狭部にて絞られ、拡大部にて速度が減殺さ
れることを繰返し、蒸気の漏洩が防止される。
When the labyrinth packing is provided in this manner, leaking steam is repeatedly constricted in the narrow portion and its velocity is reduced in the enlarged portion, thereby preventing steam leakage.

しかしながら、蒸気タービン作動には例えば566℃2
46 hlct&程度の高温高圧蒸気金柑いるので、蒸
気タービン作動時の温度上昇に伴ない、ケーシングとタ
ービンロータとの隙間等の漏洩通路が熱膨張により広が
ってし壕い、漏洩蒸気量が増加してしまうという問題点
があった。このような漏洩蒸気の増加:は圧力損失をも
たらし蒸気タービンの効率を低下させてしまうという問
題点もあった。このようカ熱膨張による蒸気の漏洩は、
高効率化のための蒸気の高温高圧化に伴ない顕著なもの
となってきた。
However, for steam turbine operation, e.g.
Since kumquats contain high-temperature, high-pressure steam of approximately 46 hlct&, as the temperature rises during operation of the steam turbine, leakage passages such as the gap between the casing and the turbine rotor expand due to thermal expansion, causing an increase in the amount of leakage steam. There was a problem with it being put away. There is also the problem that such an increase in leakage steam causes pressure loss and reduces the efficiency of the steam turbine. Steam leakage due to thermal expansion is
This problem has become more prominent as steam becomes hotter and more pressurized in order to achieve higher efficiency.

以上のような漏洩を防止するためには、パツキンフィン
とロータとの間隔の縮少、パツキンフィンの数の増加等
の方法が考えられるが、前者はラビングという運転上の
トラブル、後者はスパンの増長につながりこれに伴いタ
ービンロータが長くなる等の問題があるため、おのずか
ら限界があり、漏洩蒸気量の減少は非常に難しい問題で
あった。
In order to prevent the above-mentioned leakage, methods such as reducing the distance between the packing fins and the rotor and increasing the number of packing fins can be considered, but the former causes the operational trouble of rubbing, and the latter reduces the span. Since this leads to problems such as the turbine rotor becoming longer, there is a natural limit, and reducing the amount of leaked steam has been a very difficult problem.

〔発明の目的〕[Purpose of the invention]

本発明は以上の点を考慮してなされたもので、タービン
作動流体の漏洩を減少し、タービン効率を向上するラビ
リンスパツキンを提供することを目的とする。
The present invention has been made in consideration of the above points, and an object of the present invention is to provide a labyrinth packing that reduces leakage of turbine working fluid and improves turbine efficiency.

〔発明の概要〕 本発明のラビリンスパツキンは、タービンロータとケー
シングの隙間、タービンロータとノズルダイヤフラムの
内輪との隙間、ケーシングと動翼との隙間等のタービン
作動流体の漏洩通路に狭部、拡大部を形成するように形
状記憶合金からなるパツキンフィンが設けられている、
この形状記憶合金からなるパツキンフィンはタービン作
動時の高温環境で、この漏洩通路を狭くする方向に変位
するように構成されている。
[Summary of the Invention] The labyrinth packing of the present invention is designed to prevent leakage of turbine working fluid from narrow or enlarged areas such as the gap between the turbine rotor and the casing, the gap between the turbine rotor and the inner ring of the nozzle diaphragm, or the gap between the casing and the rotor blades. A packing fin made of a shape memory alloy is provided to form a part.
This packing fin made of a shape memory alloy is configured to be displaced in a direction that narrows this leakage passage in a high-temperature environment during turbine operation.

タービン作動流体としては蒸気、高温燃焼ガス等の高温
高圧の流体を用いるので、タービン作動時の温度上昇に
伴なうケーシング、タービンロータ等の熱膨張により前
述の漏洩通路の隙間が広がるが、本発明によればパツキ
ンフィンが形状記憶効果によりこの漏洩通路を狭くする
ように変位するので、熱膨張による漏洩通路の広がりに
よるタービン作動流体の漏洩量の増加を防止することが
できる。
As the turbine working fluid uses high-temperature, high-pressure fluid such as steam or high-temperature combustion gas, the gaps in the leakage passages described above widen due to the thermal expansion of the casing, turbine rotor, etc. as the temperature rises during turbine operation. According to the invention, the packing fin is displaced to narrow the leakage passage due to the shape memory effect, so it is possible to prevent an increase in the leakage amount of the turbine working fluid due to the expansion of the leakage passage due to thermal expansion.

〔発明の実施例〕[Embodiments of the invention]

本発明を蒸気タービンのタービンロータとケーシングと
の隙間からの蒸気漏洩の防止に用いた実施例を示す。第
1図に蒸気タービンの部分断面図全示し、第2図に第1
図中要部aの拡大図を示す。
An embodiment in which the present invention is used to prevent steam leakage from a gap between a turbine rotor and a casing of a steam turbine will be shown. Fig. 1 shows a complete partial cross-sectional view of the steam turbine, and Fig. 2 shows a partial cross-sectional view of the steam turbine.
An enlarged view of main part a in the figure is shown.

タービンロータ(1)の表面には、タービンロータ(1
)の回転軸と同軸の円周溝(2)が軸方向に複数個設け
られている。またケーシング(3)には円弧状のパツキ
ンリング(4)が例えばバネ等の伸縮可能な固定部材(
5)にて固定され、このようなパツキンリング(3)は
複数個組合わせられ、円環状に構成されている。このパ
ツキンリング(3)のタービンロータ(1)ニ対向する
表面にはパツキンフィン(6)がタービンロータf1.
)軸線方向にそって複数個設けられており、このパツキ
ンフィン(6)の一端はパツキンリング(4)に固定さ
れ、他端は自由端としてタービンロータ(1)の円周溝
(2)が設けられた表面に近接するように設けられてい
る。従ってパツキンフィン(6)の自由端とタービンロ
ータ(1)表面との隙間で漏洩通路の狭部を構成し、隣
りあうパツキンフィン(6)の間が拡大部となり、この
狭部、拡大部のくり返しにより蒸気の漏洩を防ぐことに
なる。
On the surface of the turbine rotor (1), there is a surface of the turbine rotor (1).
) A plurality of circumferential grooves (2) coaxial with the rotating shaft are provided in the axial direction. In addition, the casing (3) has an arc-shaped packing ring (4) attached to an expandable and contractible fixing member such as a spring (
A plurality of such packing rings (3) are combined to form an annular shape. A packing fin (6) is provided on the surface of the packing ring (3) facing the turbine rotor (1).
) A plurality of packing fins (6) are provided along the axial direction, one end of which is fixed to the packing ring (4), and the other end is a free end that is connected to the circumferential groove (2) of the turbine rotor (1). It is provided in close proximity to the surface on which it is provided. Therefore, the gap between the free end of the packing fin (6) and the surface of the turbine rotor (1) constitutes a narrow part of the leakage passage, and the space between adjacent packing fins (6) becomes an enlarged part. Repeating this will prevent steam leakage.

このパツキンフィン(6)はタービン作動時の高温環境
でパツキンフィン(6)の先端とタービンロータ(1)
の表面との距離が狭くなる方向に変位するような形状を
記憶させた例えばニッケル・ψタン合金等の形状記憶合
金からなる。例えば第1図第2図に示すようにパツキン
フィン(6)ヲ湾曲板形状にし、高温環境下でこの湾曲
の程度が小さくたり平板に近づくように変位するごとく
に形状を記憶させておけばこのような動作が可能となる
This packing fin (6) connects the tip of the packing fin (6) and the turbine rotor (1) in a high-temperature environment during turbine operation.
It is made of a shape memory alloy, such as a nickel/ψ tan alloy, which has a shape memorized such that it is displaced in a direction in which the distance from the surface becomes narrower. For example, as shown in Fig. 1 and Fig. 2, the packing fin (6) can be made into a curved plate shape, and the shape can be memorized so that the degree of curvature becomes smaller or the shape becomes closer to a flat plate in a high-temperature environment. It is possible to perform operations like this.

以上のように構成された蒸気タービンにおいては、高温
蒸気によりタービンロータ(1)及びケーシグ(3)と
もに熱膨張を生じ、タービンロータ(1)とケーシング
(3)との隙間が広がるが、形状記憶効果によりパツキ
ンフィン(6)がこの隙間を狭くする方向に変位するの
で、前記隙間の広がりをうちけすことができ、パツキン
フィン(6)の自由端の先端とタービンロータ(11表
面との間隔が広がることがない。
In the steam turbine configured as described above, both the turbine rotor (1) and the casing (3) undergo thermal expansion due to the high temperature steam, and the gap between the turbine rotor (1) and the casing (3) widens. As a result of this effect, the packing fin (6) is displaced in the direction of narrowing this gap, so that the gap can be prevented from widening, and the distance between the free end of the packing fin (6) and the surface of the turbine rotor (11) is reduced. It never spreads.

よってこの間隔の広がりによる漏洩蒸気量の増加を防止
することができるので、蒸気タービン効率が向上される
。また形状記憶効果による変位は、記憶された形状と設
計時の形状との差圧よって決まり、この変位量はかなり
大きくとることができるので、蒸気漏洩量を大幅に抑え
ることが可能である。また形状記憶合金を使用すること
により、部品数はまったくかえることなく漏洩防止を行
なうことができ非常に有効である。形状記憶効果を用い
ることにより、変位後の隙間の設定を寸法精度よく比較
的容易に行なうことができ、設計上も非常に有効である
Therefore, it is possible to prevent an increase in the amount of leaked steam due to the widening of this interval, thereby improving steam turbine efficiency. Further, the displacement due to the shape memory effect is determined by the differential pressure between the memorized shape and the designed shape, and since this amount of displacement can be quite large, it is possible to significantly suppress the amount of steam leakage. Furthermore, by using a shape memory alloy, leakage can be prevented without changing the number of parts, which is very effective. By using the shape memory effect, the gap after displacement can be set relatively easily with good dimensional accuracy, which is very effective in terms of design.

近年熱効率向上を目的とし蒸気の高温・高圧化の傾向が
あるが、高温となるにつれこの熱膨張により間隙の広が
りが顕著になるので、本発明の間隙の広がりを防止する
効果は非常に有効となり、タービン効率の向上につなが
る。また高温・高圧化に伴ないタービンロータ、ケーシ
ング等の材料に、従来の鉄基フェライト系鋼にかえて鉄
基オーステナイト鋼の使用が検討されているが、前者の
熱膨張係数的12.5 X 10 ’/ 1:に比べ後
者は約18,5×lO7℃と1.5倍も大きい。よって
熱膨張による間隙の広がりも顕著となるので、本発明の
効果は特に有効となる。
In recent years, there has been a trend to increase the temperature and pressure of steam in order to improve thermal efficiency, but as the temperature increases, the gap widens more significantly due to this thermal expansion, so the effect of the present invention in preventing gap widening is extremely effective. , leading to improved turbine efficiency. In addition, as temperatures and pressures increase, the use of iron-based austenitic steel instead of conventional iron-based ferritic steel is being considered for materials such as turbine rotors and casings, but the former has a thermal expansion coefficient of 12.5 Compared to 10'/1:, the latter is approximately 18.5×lO7°C, which is 1.5 times larger. Therefore, the gap widens significantly due to thermal expansion, so the effects of the present invention are particularly effective.

またパツキンリング(4)は伸縮可能な固定部材(5)
にて固定されているので、何らかの原因でパツキンフィ
ン(6)がタービンロータに接触した場合、この固定部
材(51が縮み、パツキンフィン(6) 、!:タービ
ンロータ(1)との接触を緩和することができ、この接
触によるタービンロータ(1)の損傷を防止することが
できる。さらに湾曲しているパツキンフィン(6)自体
がバネ効果を有するので、このような接触がおこった場
合速かにパツキンフィン(6)が縮み、タービンロータ
(1)の損傷を防止することができる。
In addition, the packing ring (4) is an expandable fixing member (5).
If the packing fin (6) comes into contact with the turbine rotor for some reason, this fixing member (51) will contract and the packing fin (6), !: will reduce contact with the turbine rotor (1). This can prevent damage to the turbine rotor (1) due to this contact.Furthermore, the curved packing fin (6) itself has a spring effect, so if such a contact occurs, it can be quickly removed. The packing fin (6) is retracted and damage to the turbine rotor (1) can be prevented.

またパツキンフィン(6)の先端に摩耗しやすい軟かい
物質を設けておけばさらにこの損傷を防止することがで
きる。
Moreover, if a soft material that is easily worn is provided at the tip of the packing fin (6), this damage can be further prevented.

パツキンフィン(6)のパツキンリング(4)への固定
方法は、植入み、ボルト止め、溶接、ピン止め、カシメ
などの一般の固定方法でよい。さらにパツキンフィン(
6)の凹面を高圧側A1凸面を低圧側Bに位置するよう
に設ければ、高圧の蒸気によりパツキンフィン(6)が
押され、パツキンフィン(6) ハ蒸気漏洩通路を狭く
する方向に変位するので、さらに蒸気の漏洩量を減少す
ることができる。
The packing fin (6) may be fixed to the packing ring (4) by a general fixing method such as implantation, bolting, welding, pinning, or caulking. In addition, Patsukinfin (
If the concave surface of 6) is placed so that the high pressure side A1 and the convex surface are located on the low pressure side B, the packing fin (6) will be pushed by the high pressure steam, and the packing fin (6) will be displaced in the direction of narrowing the steam leakage passage. Therefore, the amount of steam leakage can be further reduced.

またパツキンフィンを構成する形状記憶合金の材料、形
状、板厚等は、タービンの大きさ、使用材料等により適
宜選択し、パツキンフィンがタービンロータに接触しラ
ビングをおこさない程度に設計することが必要である。
In addition, the material, shape, plate thickness, etc. of the shape memory alloy that constitutes the packing fin should be selected appropriately depending on the size of the turbine, the materials used, etc., and designed to the extent that the packing fin does not come into contact with the turbine rotor and cause rubbing. is necessary.

またラビングを生じ念際、速やかに摩耗するように、タ
ービンロータの材料よりも軟かい材料を用いることが好
ましい。さらにラビリンスパツキンを設ける場所の温度
条件によっても材料はかえることができ、例えば比較的
低温のところでは黄銅等の材料を用いることもできる。
Further, it is preferable to use a material that is softer than the material of the turbine rotor so that it wears out quickly in case of rubbing. Furthermore, the material can be changed depending on the temperature conditions at the location where the labyrinth packing is provided; for example, a material such as brass may be used in a relatively low temperature location.

この実施例に示【7たパツキンフィンの形状以外でも、
高温環境で蒸気の漏洩通路を狭くする方向に変位するバ
イメタルで構成されたパツキンフィンを用いれば本発明
の効果が得られることは言うまでもない。例えば、くの
字状に曲げられた形状記憶合金を用いてもよいし、一部
に湾曲状部を有する形状の形状記憶合金でもよい。また
湾曲状部を複数個有する形状でもよい。いずれの場合も
タービンロータ方向へのパツキンフィンの長さがのびる
ような形状を記憶させておけばよい。このように複数個
の湾曲部を設けることによりパツキンフィンの変位量を
大きくすることもできる。また湾曲させなくても、斜め
に植込んだ形状のパツキンフィンでも同様の効果を得る
。この場合、タービンロータ(1)方向にむかつて湾曲
するよう々形状を記憶させておけばよい。
In addition to the shape of the packing fin shown in this example,
It goes without saying that the effects of the present invention can be obtained by using a packing fin made of bimetal that is displaced in a direction to narrow the steam leakage passage in a high-temperature environment. For example, a shape memory alloy bent into a dogleg shape may be used, or a shape memory alloy having a partially curved portion may be used. Alternatively, the shape may include a plurality of curved portions. In either case, it is sufficient to memorize a shape in which the length of the packing fin increases in the direction of the turbine rotor. By providing a plurality of curved portions in this manner, the amount of displacement of the packing fin can also be increased. Further, even if the fin is not curved, a similar effect can be obtained by using a patch fin that is implanted diagonally. In this case, the shape may be memorized so that it curves toward the turbine rotor (1).

またパツキンフィンを構成する板材の板厚も一様である
必要はなく、例えば先端に近づくにつれ板厚が薄くなる
ように構成してもよい。とのように構成すれば、パツキ
ンフィンがタービンロータに接触した場合、摩耗しやす
いので、タービンロータの損傷を防止できる。また一枚
の板に限らすとなる一端をそろえずに互いにずらすよう
に接合すれば、蒸気漏洩通路の広狭を増やすことができ
実質的にパツキンフィンの数を増加したことになり、ラ
ビリンスパツキンの効果をさらに有効とすることができ
る。
Further, the thickness of the plate material constituting the packing fin does not need to be uniform; for example, the thickness may become thinner as it approaches the tip. With this configuration, when the packing fin comes into contact with the turbine rotor, it is likely to wear out, so damage to the turbine rotor can be prevented. Also, if you limit it to one plate and join it so that one end is not aligned but offset from each other, the width of the steam leakage passage can be increased and the number of packing fins has been increased, and the labyrinth packing. The effect can be made even more effective.

2枚の板材(6’)、(6″)を用いてパツキンフィン
(6)を構成した本発明の他の実施例を第3図に概略的
に示す。形状記憶合金からなる板材(6’)、(6つ全
接合したパツキンフィン(6)の一端をパツキンリング
(4)に固定し、他端を自由端としてタービンロータ(
1)表面に近接するように設けられている。このパツキ
ンフィン(6)の自由端では各々の板材(6’) 、 
(6’)が先端をそろえずに接合されており、2ケ所の
狭部C2σを1枚のパツキンフィン(6)で構成してい
る。パツキンフィン(6)はくの字状に湾曲1.ており
、タービン作動時の高温環境でこの湾曲の度合が小さく
なるような形状が記憶されている。他の構成は第1図に
示した実施例と同様とする7、このように構成された第
3図に示す実施例では、前述のような漏洩通路を狭くす
る効果、パツキンフィン(6)自体のバネ効果によるタ
ービンロータ(1)の損傷を防止する効果を得る他に、
1枚のパツキンフィン(6)で狭部’f2ケ所設けるこ
とができるので、パツキンフィンの数を増加して漏洩防
止の効果をあげるのと同等の効果を得ることができる。
Another embodiment of the present invention in which the packing fin (6) is constructed using two plates (6') and (6'') is schematically shown in FIG. 3. The plate (6') made of a shape memory alloy is ), (One end of the six fully connected packing fins (6) is fixed to the packing ring (4), and the other end is set as a free end to the turbine rotor (
1) Provided close to the surface. At the free end of this packing fin (6) each plate (6'),
(6') are joined without aligning their tips, and the two narrow parts C2σ are formed by one packing fin (6). Patsukin fin (6) curved in a dogleg shape1. The shape is memorized so that the degree of curvature is reduced in the high temperature environment during turbine operation. The other configurations are the same as the embodiment shown in FIG. 17. In the embodiment shown in FIG. In addition to obtaining the effect of preventing damage to the turbine rotor (1) due to the spring effect of
Since two narrow portions 'f can be provided with one packing fin (6), the same effect as increasing the number of packing fins to prevent leakage can be obtained.

また第3図に示した実施例においてタービンロータ(1
)に近い方の板材(6’) ’!i=形状記憶合金とせ
ずに摩耗性の材料を用いてもよい。このように構成すれ
ばたとえパツキンフィン(6)がタービンロータ(1)
に接触した場合でも速やかにパツキンフィン(6)が摩
耗するのでタービンロータ(1)に損傷を与えるおそれ
がない。
Furthermore, in the embodiment shown in FIG. 3, the turbine rotor (1
) nearer the board (6') '! An abrasive material may be used instead of i=shape memory alloy. With this configuration, even if the packing fin (6) is the turbine rotor (1)
Even if the gasket fin (6) comes into contact with the turbine rotor (1), the gasket fin (6) will quickly wear out, so there is no risk of damaging the turbine rotor (1).

以上の実施例ではパツキンリングにパツキンフィンを接
合した場合を説明し、たが、直接ケーシングにパツキン
フィンを設けてもよい。このように直接ケーシングにパ
ツキンフィンを設けた場合でも、前述のようにパツキン
フィン自体にバネ効果音もたせることができるので、パ
ツキンリングを伸縮可能な固定部材で固定したのと同等
の効果を得ることができる。さらに本発明では漏洩通路
の広がりを防止できるので、蒸気漏洩減少のために設け
られているタービンロータ表面の円周溝の深さを小さく
又はなくしてしまうことが可能である。
In the above embodiments, the case where the packing fin is joined to the packing ring is explained, but the packing fin may be provided directly to the casing. Even if the packing fin is provided directly on the casing in this way, the spring sound effect can be created on the packing fin itself as described above, so it is possible to obtain the same effect as fixing the packing ring with an expandable fixing member. Can be done. Furthermore, since the present invention can prevent the leakage passage from widening, it is possible to reduce or eliminate the depth of the circumferential groove on the surface of the turbine rotor, which is provided to reduce steam leakage.

この円周溝は熱応力の集中、蒸気密が起こり易く応力腐
食割れ、腐食疲労などのタービンロータの環境破壊の一
因とがり、このように円周溝を小さく又はなくすことに
より、このようなタービンロータの環境破壊の一因を除
去することができ、タービンの信頼性を向上することが
できる。
This circumferential groove tends to cause concentration of thermal stress and steam tightness, which contributes to environmental damage to the turbine rotor such as stress corrosion cracking and corrosion fatigue. A cause of environmental damage to the rotor can be eliminated, and the reliability of the turbine can be improved.

この実施例では、タービンロータとケーシングとの隙間
からの蒸気漏洩を防止するのにラビリンスパツキンを用
いたが、この他にケーシングと動翼との隙間、ノズルダ
イヤフラムとタービンロータとの隙間等のタービンロー
タ軸線方向の蒸気漏洩通路からの蒸気漏洩を防止するた
めに用いてもよい。
In this example, the labyrinth packing was used to prevent steam leakage from the gap between the turbine rotor and the casing, but the labyrinth packing was also used to prevent steam leakage from the gap between the casing and the rotor blades, the gap between the nozzle diaphragm and the turbine rotor, etc. It may also be used to prevent steam leakage from a steam leakage passage in the rotor axial direction.

第4図に動翼(9)とケーシング(3)との隙間からの
タービン作動流体の漏洩を防止するためにラビリンスパ
ツキンを用いた本発明の他の実施例を概略的に示す。形
状記憶合金からなる板材(力と摩耗性材料からなる板材
(8)とが接合されてなるパツキンフィン(6)は、板
材(7)から板材(8)に向かう方向に凸とがるように
湾曲している。さらにこの形状記憶合金からなる板材(
力は、タービン作動時の高温環境でこの湾曲の度合が小
さくなりパツキンフィン(6)の実質的な長さが増加す
るように変位する形状が記憶されている。またパツキン
フィン(6)は一端がケーシグ(3)に同定され先端は
動翼(9)に近接するように設定されるが、この際もつ
とも動翼(9)の近くに位置するのは摩耗性材料からな
る板材(8)とする。
FIG. 4 schematically shows another embodiment of the present invention in which a labyrinth packing is used to prevent leakage of turbine working fluid from the gap between the rotor blade (9) and the casing (3). The packing fin (6) is formed by joining a plate material (8) made of a shape memory alloy and an abrasive material so that it is convex and pointed in the direction from the plate material (7) to the plate material (8). It is curved.Furthermore, a plate material made of this shape memory alloy (
The force is stored in a shape that is displaced in a high temperature environment during turbine operation such that the degree of this curvature decreases and the substantial length of the packing fin (6) increases. In addition, one end of the packing fin (6) is identified with the casing (3), and the tip is set close to the rotor blade (9), but in this case, the part located near the rotor blade (9) is abrasive. Let it be a plate material (8) made of material.

このように構成されたラビリンスパツキンにおいては、
タービン作動時の温度上昇に伴なう熱膨張による隙間の
広が9を、パツキンフィン(6)の形状記憶効果により
打消すことができるのでタービン作動流体の漏洩量を減
少することができる。またパツキンフィン(6)がバネ
効果を有するので、何らかの原因でパツキンフィン(6
)が動翼(9)に接触した場合でもこの接触全緩和する
ことができ動翼(9)に損傷を与えるのを防止する。さ
らに摩耗性材料を設けることにより接触した場合パツキ
ンフィン(6)が速かに摩耗するので、この接触による
動*、(9)の損傷を防止するのに効果的である。
In the labyrinth patchkin configured in this way,
The shape memory effect of the packing fins (6) can cancel out the widening of the gap 9 due to thermal expansion accompanying the temperature rise during turbine operation, so the amount of leakage of the turbine working fluid can be reduced. Also, since the Patsukin fin (6) has a spring effect, for some reason the Patsukin fin (6)
) comes into contact with the rotor blade (9), this contact can be completely relieved and damage to the rotor blade (9) can be prevented. Furthermore, by providing an abrasive material, the packing fins (6) will quickly wear out when they come into contact, and this is effective in preventing damage to the fins (9) caused by this contact.

〔発明の効果〕〔Effect of the invention〕

以上説明したように本発明によれば、熱膨張によるター
ビン作動流体の漏洩通路の拡張に伴なう作動流体の漏洩
の増加を防止することができるので、タービン効率を向
上することができる。したがって大幅な燃料費の節約等
の利点も生じ非常に有効である。
As described above, according to the present invention, it is possible to prevent an increase in the leakage of the working fluid due to the expansion of the leakage passage of the turbine working fluid due to thermal expansion, and thus it is possible to improve the turbine efficiency. Therefore, there are also advantages such as significant fuel cost savings, which is very effective.

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

第1図は本発明の詳細な説明するための蒸気面概略図。 6・・・パツキンフィン (7317)  代理人 弁理士 則 近 憲 佑 (
ほか1名)第  1  図 第2図 ? 第8図
FIG. 1 is a schematic diagram of a steam plane for explaining the present invention in detail. 6...Patsukinfin (7317) Agent: Patent Attorney Noriyuki Chika (
1 other person) Figure 1 Figure 2? Figure 8

Claims (1)

【特許請求の範囲】[Claims] タービン作動流体の漏洩通路に狭部及び拡大部を形成す
るように設けられたパツキンフィンを具備するラビリン
スパツキンにおいて、前記パツキンフィンがタービン作
動時の高温環境で漏洩通路を狭くする方向に変位する形
状が記憶された形状記憶合金からなること全特徴とする
ラビリンスパツキン。
A labyrinth packing including a packing fin provided to form a narrow part and an enlarged part in a leakage passage of turbine working fluid, wherein the packing fin is shaped to be displaced in a direction to narrow the leakage passage in a high temperature environment during turbine operation. The labyrinth patchkin is made of a shape memory alloy that has a memorized memory.
JP12592382A 1982-07-21 1982-07-21 Labyrinth packing Pending JPS5918208A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP12592382A JPS5918208A (en) 1982-07-21 1982-07-21 Labyrinth packing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP12592382A JPS5918208A (en) 1982-07-21 1982-07-21 Labyrinth packing

Publications (1)

Publication Number Publication Date
JPS5918208A true JPS5918208A (en) 1984-01-30

Family

ID=14922288

Family Applications (1)

Application Number Title Priority Date Filing Date
JP12592382A Pending JPS5918208A (en) 1982-07-21 1982-07-21 Labyrinth packing

Country Status (1)

Country Link
JP (1) JPS5918208A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3542762A1 (en) * 1985-12-04 1987-06-11 Mtu Muenchen Gmbh DEVICE FOR CONTROLLING OR CONTROLLING GAS TURBINE ENGINES OR GAS TURBINE JET ENGINES
FR2738046A1 (en) * 1995-08-23 1997-02-28 Snecma Labyrinth seal between stator and rotor in gas turbine of e.g. aircraft engine
US7367776B2 (en) * 2005-01-26 2008-05-06 General Electric Company Turbine engine stator including shape memory alloy and clearance control method
EP2116621A2 (en) * 2008-02-27 2009-11-11 General Electric Company High temperature shape memory alloy actuators
CN106170608A (en) * 2014-01-21 2016-11-30 通用电器技术有限公司 For rotating or the mechanical fastening system of static component
EP4269752A1 (en) * 2022-04-28 2023-11-01 Hamilton Sundstrand Corporation Additively manufactured multi-metallic adaptive rotor tip seals

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3542762A1 (en) * 1985-12-04 1987-06-11 Mtu Muenchen Gmbh DEVICE FOR CONTROLLING OR CONTROLLING GAS TURBINE ENGINES OR GAS TURBINE JET ENGINES
FR2738046A1 (en) * 1995-08-23 1997-02-28 Snecma Labyrinth seal between stator and rotor in gas turbine of e.g. aircraft engine
US7367776B2 (en) * 2005-01-26 2008-05-06 General Electric Company Turbine engine stator including shape memory alloy and clearance control method
EP2116621A2 (en) * 2008-02-27 2009-11-11 General Electric Company High temperature shape memory alloy actuators
EP2116621A3 (en) * 2008-02-27 2010-11-17 General Electric Company High temperature shape memory alloy actuators
CN106170608A (en) * 2014-01-21 2016-11-30 通用电器技术有限公司 For rotating or the mechanical fastening system of static component
EP4269752A1 (en) * 2022-04-28 2023-11-01 Hamilton Sundstrand Corporation Additively manufactured multi-metallic adaptive rotor tip seals

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