JPS6098268A - Shaft seal for axial-flow rotary machine - Google Patents
Shaft seal for axial-flow rotary machineInfo
- Publication number
- JPS6098268A JPS6098268A JP20575983A JP20575983A JPS6098268A JP S6098268 A JPS6098268 A JP S6098268A JP 20575983 A JP20575983 A JP 20575983A JP 20575983 A JP20575983 A JP 20575983A JP S6098268 A JPS6098268 A JP S6098268A
- Authority
- JP
- Japan
- Prior art keywords
- shaft
- backing
- tooth
- shape
- revolution
- 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
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J15/00—Sealings
- F16J15/44—Free-space packings
- F16J15/445—Free-space packings with means for adjusting the clearance
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
- F05C2251/00—Material properties
- F05C2251/08—Shape memory
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Sealing Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)
Abstract
Description
【発明の詳細な説明】
〔発明の技術分野〕
本発明は蒸気およびガスタービンのシール部分に設けら
れる2ビリンスおよびダイヤ7シムパツキングなどを採
用した軸6iL回転儀械の軸封装置に関する。DETAILED DESCRIPTION OF THE INVENTION [Technical Field of the Invention] The present invention relates to a shaft sealing device for a 6iL rotary machine that employs a 2-birinse and a 7-diamond shim packing provided in the sealing portion of a steam and gas turbine.
〔発り1の技術的背景とその問題点〕
蒸気タービンの振動問題は、入力元−所の運転ならびに
保守上の大きな比重を占めているが、近年蒸気タービン
の大谷量化に伴なう軸受間の距離。[Technical background of origin 1 and its problems] The problem of vibration in steam turbines occupies a large proportion of the operation and maintenance of the input source. distance.
ロータ型皿および車室数などの増加のため、一層複雑化
する順向にある。この振動間」に関し、時に蒸気タービ
ンの運転上発生する可能性のある単室の上下半部の温度
差は、車室の猫背または逆猫背変形と呼ばれる変形を生
じ、この結果としてバッキング位置も垂直方向に夏位し
、このために回転軸とバッキングが接触して振@を起こ
し、ロータ(二悪影曽を与え′Cいた。Due to the increase in rotor type plates and the number of compartments, they are becoming more complex. Regarding this vibration, the temperature difference between the upper and lower halves of the single chamber that can sometimes occur during steam turbine operation causes a deformation called hunchback or reverse hunchback deformation of the cabin, and as a result, the backing position also becomes vertical. As a result, the rotating shaft and the backing came into contact, causing vibration and causing the rotor (two negative effects).
rなわち、蒸気タービンの軸封−、A置は、第1図およ
び第2図に示すようにロータ1の外周には。In other words, the shaft seal of the steam turbine is located at the outer periphery of the rotor 1 as shown in FIGS. 1 and 2.
バッキング2がシャフトバッキングケース4tbるいは
ダイヤフラム5(=取りつけられ、かつこのバッキング
2は、ロータ1の円周方向に複数個に分割さIしてこ7
′Lを包囲し−Cいる構成(ニなっている。The backing 2 is attached to the shaft backing case 4tb or the diaphragm 5, and this backing 2 is divided into a plurality of parts in the circumferential direction of the rotor 1.
'L is surrounded by -C (2).
このような諏気タービンの軸封装置において、車室の猫
背まIこは逆猫背変形に起因する振動対策として、垂1
亘方向間間隙が水平方間間隙よりも大きな2ビリンスパ
ツキ/を用いることが、たとえば特公昭54−1598
5号公報に述べらスして周知になっている。この特公昭
54−15985号公報(二おいて、第3図1=示すよ
うにバッキング2は、ロータ1の中心点0よυ上下に偏
心mxs、心あるいは下1+41に調心iXtだけ偏心
させて夫々円弧Rを画き、パツキングー先3がロータ1
(二対して円状(=なるよう配置され、上下15μ分の
間隙V、 、 V、は、左右部分の間隙H1、H2よシ
ロータ1に対して#1ぼ1.3〜3.4倍の広い間隙を
有している。In such a shaft sealing device for a wind turbine, the hunchback of the casing is designed to prevent vibrations caused by reverse hunchback deformation.
For example, in Japanese Patent Publication No. 54-1598, it is possible to use a 2-billin spacing whose transverse gap is larger than the horizontal gap.
It is well known as described in Publication No. 5. In this Japanese Patent Publication No. 54-15985 (2), as shown in Fig. 3, the backing 2 is eccentric mxs above and below the center point 0 of the rotor 1, and eccentric iXt is centered or below 1+41. Each draws an arc R, and the packing end 3 is the rotor 1.
(The two are arranged in a circular shape (=), and the vertical and vertical gaps V, , V, are 1.3 to 3.4 times as large as the gaps H1 and H2 in the left and right portions and the distance between #1 and rotor 1. It has a wide gap.
偏心址X、、X2は、0.15間〜1.84ぐらいがよ
くタービンの8頑、容虐、運転条件などによって適宜選
定さJ’Lるもの′C必る。すなわち、バッキング2の
内径を回転軸の上下方向に対し、楕円状にしたので、ケ
ーシングが上下に猫背に変形しても回転軸とバッキング
が接触することを防止できるととも(二、両者間からの
漏洩蒸気量を最小に保持でき、タービン効率の低下を防
止することが可能にしにと述べている。The eccentricities X, X2 are preferably between 0.15 and 1.84, and must be appropriately selected depending on the turbine's rigidity, severity, operating conditions, etc. That is, since the inner diameter of the backing 2 is made elliptical with respect to the vertical direction of the rotating shaft, it is possible to prevent the rotating shaft and the backing from coming into contact even if the casing deforms vertically into a hunched position (2. This makes it possible to keep the amount of leaked steam to a minimum and prevent a decrease in turbine efficiency.
しかし、ケーシングの猫背または逆猫背変形は、タービ
ンの起鯛、停止あるいは急激な負荷変化などの:+I!
i1度的な状態のもとでのみまオ℃に発生し、しかもそ
の変形は永続的なものでなく、時間ととも(二元の形状
に復帰するものである。したがって、従来技術(二おけ
るように過度的な最悪の状態を想定して、上下部分を右
左都よりも広い間隙に設定しておくことは、タービンの
定常4転中にその広い間?I!部分から作動流体である
蒸気またはガスがむだ(二漏洩してしまうことにより、
省エネルギー時代の高効率蒸気およびガスタービンに対
しては効率の1氏下の原因となるという欠点があった。However, slouching or reverse slouching deformation of the casing may cause the turbine to start up, stop, or suddenly change in load: +I!
This deformation occurs only under temporary conditions, and the deformation is not permanent and returns to its original shape over time. Assuming the worst-case scenario, setting the upper and lower parts to a wider gap than the left and right parts means that the steam, which is the working fluid, will flow from the wide gap during steady four-wheel rotation of the turbine. Or the gas is wasted (by leaking)
The high-efficiency steam and gas turbines of the energy-saving era had the drawback of being the cause of a 1 degree drop in efficiency.
〔発1男の目的)
本発明の目的は、回転軸とラビリンスおよびダイイノ2
ムパツキングの歯先との間隙ト必要1欧小限として軸封
幼果を高め、車室の変形(二起因する績−間j、r生じ
ない閥効率蒸気およびガスタービン(二層いりAする軸
流回転機械の軸封装置と提供するにらる。[Purpose of the invention] The purpose of the present invention is to provide a rotary shaft, a labyrinth, and a
It is necessary to increase the shaft sealing by keeping the gap between the tip of the teeth and the shaft to a minimum, and to reduce the deformation of the casing (2). Provides a shaft sealing device for rotating machinery.
本発明による細流回転機械の軸封装置は、バッキングの
膚全形状躬憶は金としたこと金特畝とし、特(二d1.
数閏(二分割されたバッキングのうち回転軸の上方しよ
び下方の肉11111 ’l:たは上方あるいは下方の
片1tllll=位置するバッキングの歯を形状記憶合
金としたことを特徴とするものである。In the shaft sealing device for a trickle rotating machine according to the present invention, the entire shape of the backing is made of gold and has special ridges.
It is characterized by the fact that the teeth of the backing located above and below the rotating shaft 11111'l of the backing divided into two parts are made of shape memory alloy. be.
〔発明の実施例) 以下不発明を第4図に示す=実施例について説明する。[Embodiments of the invention] The embodiment shown in FIG. 4 will be described below.
第4図(二おいて、円周方向に複数個に分割されたバッ
キングリング2のうち、回転軸1の上方および下方の両
側または上方あるいは下方の片開に位置するバンキング
2の@ a/を例えばTi −Ni合金よシなる形状記
憶合金を細片に分割して構成し、残シのバッキングリン
グ2の歯3は、従来の材料ご構成し、回転軸1とバッキ
ング2の!13゜3′の半径方向間隙は、据付時に全周
均一にしだ軸封装置にある。FIG. 4 (2) Among the backing rings 2 divided into a plurality of parts in the circumferential direction, the banking 2 located on both sides above and below the rotating shaft 1 or on one side open above or below is @a/ For example, a shape memory alloy such as a Ti-Ni alloy is divided into small pieces, and the teeth 3 of the remaining backing ring 2 are made of a conventional material. The radial clearance of ' is uniform around the entire circumference of the shaft sealing device during installation.
バッキング2の1)li 3’に使用する形状記憶合金
は、マルテンダ°イト変態点よシ高い一度で記1腫させ
た形状を覚え′Cいて、マルテンサイトの状態(おおよ
そ気温)で変形を与えても変態点以上の温度に再加熱す
ると、元の形状に榎元する性質(これを逆変趨という)
がろシ、多くの場曾形状回復に伴ない大きな力を発生T
ることが知られている。The shape memory alloy used for 1)li 3' of backing 2 has a shape that is higher than the martensite transformation point and is deformed in the martensite state (approximately at room temperature). However, when reheated to a temperature above the transformation point, it returns to its original shape (this is called a reverse transformation trend).
Garoshi generates a large amount of force as it recovers its original shape.
It is known that
さて、菌3′は素材の段階で第5図aに示すように平板
の端部を曲げた形状に形成され、これを記1させておく
。これをマルテンサイトの状態で再び平板形状に戻し、
第5図す、cのようにバッキングリング2(二植込んで
歯先を形成する。歯3′は細片状に分割して形成するが
、これは元の形状に復元しやすいように考慮しているた
めでちゃ1分割数は歯3′の曲率半径によって決められ
るものである。さらに歯3′は蒸気の人口側に曲がるよ
うにしておく。そして回転l14111とバッキング歯
3′とが接触あるいは歯3′が逆変態点温度以上になる
と、歯3′は第6図に示すように元の形状(二榎帰し、
丙3′と回転軸lとの間隙が広くなって接触することは
なくなる。Now, the bacteria 3' is formed in the shape of a flat plate with bent ends as shown in FIG. This is returned to a flat plate shape in the state of martensite,
As shown in Figure 5, the backing ring 2 (2) is implanted to form the tip of the tooth.The tooth 3' is formed by dividing it into strips, but this is done so that it can be easily restored to its original shape. Therefore, the number of divisions per division is determined by the radius of curvature of the tooth 3'.Furthermore, the tooth 3' is bent toward the artificial side of the steam.Then, the rotation l14111 and the backing tooth 3' come into contact. Alternatively, when the temperature of the tooth 3' reaches or exceeds the reverse transformation temperature, the tooth 3' returns to its original shape (returns to its original shape) as shown in FIG.
The gap between Hei 3' and the rotating shaft I is widened and they no longer come into contact with each other.
歯3′の一丸を逆変態点温度以上(二するためのひとつ
の方法としては、回転IIIIl]1と歯3′金接危さ
せることがある。接触させた場合の摩擦熱による温度上
昇は急激なものであシ、このため歯3′の逆変應も直ち
に起こり、このJdJ独が長時間就くことはなく、接触
(=もとすくタービン運転の振αbに対しては問題はな
い。他の方法は、爾3′の逆変態点温度を作励へ不髄度
以1・′に調整しておくことである。One way to raise the entire tooth 3' to above the reverse transformation point temperature (2) is to bring the rotation III1 and the tooth 3' into metal contact.When they come into contact, the temperature rise due to frictional heat is rapid. Therefore, the reverse deterioration of the tooth 3' will occur immediately, and this JdJ will not work for a long time, and there will be no problem with the vibration αb of the turbine operation. The method is to adjust the reverse transformation point temperature of 3' to 1.' below the degree of unmyelinating.
この場合は、タービンを運転すれば必ず圃3′の通変悪
が起り、回転軸1とバッキング歯3′とは必ず所定の間
隙となることはいうまでもない。In this case, it goes without saying that when the turbine is operated, the field 3' will inevitably change, and there will always be a predetermined gap between the rotating shaft 1 and the backing teeth 3'.
第7図(二本発明の軸封装置の回転mA 1とバッキン
グ11113,3’の間隙図を示している。形状記憶合
金で形成されたバッキング歯3′は、逆KJI:よシ元
の形状に戻るため、回転軸中心0を中心とした半径R2
の円弧を形成する。第8図は本発明の実施例を実扉で、
特公昭54−15985号公報に述べられている従来技
術によるバッキング歯と回転軸の間隙図を破線で重ね合
わせて示している。水平間隙Hと垂直間隙■は両者同じ
である。第8図から明らかなように、本発明によるもの
は従来技術によるものに対し、asの面積はわずかに大
きいが、bJの面積はずっと小さくなっており、全体を
見ると本発明の方が間隙面積は小さくなっておシ、改良
されていることがわかる。Figure 7 (2) shows the gap diagram between the rotation mA 1 and the backing 11113, 3' of the shaft sealing device of the present invention. To return to , the radius R2 centered on the rotation axis center 0
form an arc. Figure 8 shows an embodiment of the present invention with an actual door.
A diagram of the gap between the backing teeth and the rotating shaft according to the prior art described in Japanese Patent Publication No. 54-15985 is shown superimposed with broken lines. The horizontal gap H and the vertical gap ■ are both the same. As is clear from FIG. 8, the area of as is slightly larger in the case of the present invention than in the case of the prior art, but the area of bJ is much smaller, and overall the gap is smaller in the case of the present invention. It can be seen that the area has become smaller and has been improved.
また第3図に示す従来の方法では、バッキングの歯の内
径加工は、中心位置を偏心させて行なわなくてはならな
いという困難さがあった。これに対し本発明の場合は、
回転軸の中心0を中心にして回転切削加工を行なうだけ
であるので、バッキングの歯の加工が者しく容易である
。Further, in the conventional method shown in FIG. 3, there is a difficulty in machining the inner diameter of the teeth of the backing by making the center position eccentric. On the other hand, in the case of the present invention,
Since rotary cutting is only performed around the center 0 of the rotation axis, machining of the teeth of the backing is straightforward and easy.
以上の本発明の実施例によれば、バッキング歯明と従来
の回転軸とバッキング歯先の関係を重ねて示す説明図で
ある。According to the above-described embodiment of the present invention, it is an explanatory diagram showing the relationship between the backing tooth profile, the conventional rotating shaft, and the backing tooth tip in an overlapping manner.
1・・・ロータ 2・・・バッキング 3.3′・・・バッキング歯先 4・・・シャフトバッキングケース 5・・・ダイヤフラム1... Rotor 2... Backing 3.3'...backing tooth tip 4...Shaft backing case 5...Diaphragm
Claims (1)
を形状記tI!合金としたことを特徴とする軸流回転機
械の軸封装置。 12) 回転軸を非接触状態に包囲するようにその円周
方向に複数個(二区分してバッキングを設け、このfJ
数個のバッキングのうち回転軸の上方および下方の両1
Illlまたは上方あるいは下方の片側に位置するバッ
キングの歯を形状記憶合金としたことを特徴とする特I
f!f請求の範囲第1項記載の一流回転機械の軸封装置
。 (3) バッキング爾(二使用する形状記憶合金は複数
個に分割した細片状に形成したことを特徴とする特許請
求の範囲第1項および第2項の一流回転機械の佃封装d
0 (4)形状i己1麓曾金はマルテンサイト変態点よシ高
い直度C端部を曲げた形状に^己憶させ、これをマルテ
ンサイトの状態で再び平板形状に戻してバッキングリン
グに植込んで構成したことを特徴とする特許請求の範囲
第2項および第3JA記載の軸流回転機械の軸封装置。[Claims] (1) The teeth of the backing that surround the rotating shaft in a non-contact state have a shape tI! A shaft sealing device for an axial flow rotating machine characterized by being made of an alloy. 12) A plurality of backings are provided in the circumferential direction so as to surround the rotating shaft in a non-contact state (divided into two, and this fJ
One of the several backings, one above and one below the rotating shaft.
Special feature I, characterized in that the teeth of the backing located on one side of the upper or lower side are made of a shape memory alloy.
f! f A shaft sealing device for a first-class rotating machine according to claim 1. (3) Packaging for first-class rotating machinery according to claims 1 and 2, characterized in that the shape memory alloy used in the backing is formed into a plurality of divided strips.
0 (4) Shape i Self 1 The metal has a straightness higher than the martensitic transformation point C The end is bent into a shape, and this is returned to the flat plate shape in the martensite state and used as a backing ring. A shaft sealing device for an axial flow rotating machine according to claims 2 and 3JA, characterized in that it is configured by being implanted.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP20575983A JPS6098268A (en) | 1983-11-04 | 1983-11-04 | Shaft seal for axial-flow rotary machine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP20575983A JPS6098268A (en) | 1983-11-04 | 1983-11-04 | Shaft seal for axial-flow rotary machine |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS6098268A true JPS6098268A (en) | 1985-06-01 |
Family
ID=16512190
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP20575983A Pending JPS6098268A (en) | 1983-11-04 | 1983-11-04 | Shaft seal for axial-flow rotary machine |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS6098268A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH02173302A (en) * | 1988-12-23 | 1990-07-04 | Fuji Electric Co Ltd | Seal-fin mechanism at blade end of geothermal steam turbine static blade |
JP2001200937A (en) * | 2000-01-17 | 2001-07-27 | Mitsubishi Heavy Ind Ltd | Active seal of rotating machine |
JP2001289328A (en) * | 2000-04-10 | 2001-10-19 | Senshin Zairyo Riyo Gas Generator Kenkyusho:Kk | Sealing device |
JP2006132635A (en) * | 2004-11-04 | 2006-05-25 | Toshiba Corp | Shaft seal |
EP1914388A1 (en) * | 2006-10-20 | 2008-04-23 | Siemens Aktiengesellschaft | Sealing element for sealing a leakage passage between a rotor and a stator of a turbomachine. |
CN102322529A (en) * | 2010-05-11 | 2012-01-18 | 通用电气公司 | Crooked labyrinth seal |
-
1983
- 1983-11-04 JP JP20575983A patent/JPS6098268A/en active Pending
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH02173302A (en) * | 1988-12-23 | 1990-07-04 | Fuji Electric Co Ltd | Seal-fin mechanism at blade end of geothermal steam turbine static blade |
JP2001200937A (en) * | 2000-01-17 | 2001-07-27 | Mitsubishi Heavy Ind Ltd | Active seal of rotating machine |
JP2001289328A (en) * | 2000-04-10 | 2001-10-19 | Senshin Zairyo Riyo Gas Generator Kenkyusho:Kk | Sealing device |
JP2006132635A (en) * | 2004-11-04 | 2006-05-25 | Toshiba Corp | Shaft seal |
JP4643228B2 (en) * | 2004-11-04 | 2011-03-02 | 株式会社東芝 | Shaft seal |
EP1914388A1 (en) * | 2006-10-20 | 2008-04-23 | Siemens Aktiengesellschaft | Sealing element for sealing a leakage passage between a rotor and a stator of a turbomachine. |
CN102322529A (en) * | 2010-05-11 | 2012-01-18 | 通用电气公司 | Crooked labyrinth seal |
EP2386724A3 (en) * | 2010-05-11 | 2013-12-18 | General Electric Company | Rotary machine with a labyrinth seal with curved teeth |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US6131910A (en) | Brush seals and combined labyrinth and brush seals for rotary machines | |
US6578849B2 (en) | Sealing configuration, in particular for a rotary machine | |
US4375891A (en) | Seal between a turbine rotor of a gas turbine engine and associated static structure of the engine | |
KR100912997B1 (en) | In situ load sharing brush seals | |
US2619317A (en) | Rotor for turbomachines | |
JP2007071203A (en) | Method and apparatus for assembling rotary machine | |
JPH0435601B2 (en) | ||
CN110206592B (en) | High-temperature and high-pressure resistant integrated impeller-sealing structure for radial-flow impeller machinery | |
JP2002544432A (en) | Fluid machine with leak prevention device for rotor | |
JPH11257014A (en) | Working fluid leakage prevention apparatus for axial-flow turbine | |
EP3190267B1 (en) | Structure for multi-stage sealing of turbine | |
EP2233800A1 (en) | Seal member, assembly and method | |
JP2002544430A (en) | Fluid machinery with leak-proof device for rotor, especially gas turbine | |
WO2015115400A1 (en) | Shaft seal device and rotary machine | |
JP2011140943A (en) | Adverse pressure gradient seal mechanism | |
JP2017519156A (en) | Radial flow turbomachine | |
JPS6098268A (en) | Shaft seal for axial-flow rotary machine | |
WO2018038899A1 (en) | Centrifugally activatable seal for a rotary machine and method of assembling same | |
JP3382802B2 (en) | Shaft seal | |
Stephen et al. | Development of brush seal technology for steam turbine retrofit applications | |
KR101638480B1 (en) | brush sealing apparatus for turbine | |
CN210289849U (en) | Elastic steam seal | |
JPH05187396A (en) | Drum type rotor of turbomachinery | |
JPH0629521B2 (en) | Gas turbine rotor cooling device | |
US20130001886A1 (en) | Twist proof flexures of seal assemblies |