JPS59131703A - Repairing method for moving blade of steam turbine - Google Patents
Repairing method for moving blade of steam turbineInfo
- Publication number
- JPS59131703A JPS59131703A JP530983A JP530983A JPS59131703A JP S59131703 A JPS59131703 A JP S59131703A JP 530983 A JP530983 A JP 530983A JP 530983 A JP530983 A JP 530983A JP S59131703 A JPS59131703 A JP S59131703A
- Authority
- JP
- Japan
- Prior art keywords
- tenon
- shroud
- steam turbine
- rotor blade
- moving blade
- 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
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/005—Repairing methods or devices
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
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動翼テノン部の補修法に関するも
のである。DETAILED DESCRIPTION OF THE INVENTION [Technical Field of the Invention] The present invention relates to a method for repairing a tenon portion of a steam turbine rotor blade.
従来、蒸気タービンは第1図に示すような構造になって
いる。すなわち同図において、タービンケーンング1の
内部にあるロータ2には削υ出しく焼きばめの場合もあ
る)の羽根車3の外周に複数本の動翼4が植込まれてい
る。また動1!4は、第2図に示すように動翼4の先端
を削)出して成形してなるテノン5を有しており、この
テノン5には第3図に示すシュラウド6の孔7を嵌合さ
せテノン5の先端をかしめてシュラウド6′を固定して
動翼群を構成するようになっている。そして、このよう
な動翼群を構成することによって動翼4はその剛性が向
上し、またシュラウドは動力流体の半径方向漏れの防止
による性能向上に役立っている。Conventionally, a steam turbine has a structure as shown in FIG. That is, in the figure, a plurality of rotor blades 4 are embedded in a rotor 2 inside a turbine caning 1 on the outer periphery of an impeller 3 (which may be shrink-fitted in some cases). Furthermore, the rotor 1!4 has a tenon 5 formed by cutting out the tip of the rotor blade 4 as shown in FIG. 2, and this tenon 5 has a hole in the shroud 6 shown in FIG. 7 and caulking the tip of the tenon 5 to fix the shroud 6' to form a rotor blade group. By configuring such a rotor blade group, the rigidity of the rotor blade 4 is improved, and the shroud is useful for improving performance by preventing leakage of power fluid in the radial direction.
蒸気タービン運転中は動翼4には遠心力が作用する他に
、上流のノズル8からの噴流により毎秒数千回以上の高
サイクルの励振力を受け、さらに個々のノズル面積の不
均一による動力流体の偏在、固転による重力の方向変化
等による低サイクルの励振力も加わっている。設計時に
おいては、動翼4に与えられる励振力と動@4の固有蚕
動数とが一致しないようになっているが、ノズル8は浸
食等罠よって個々のノズル面積が経年的に変化するので
、結果として動翼4に与えられる励振周源数と動翼4の
固有振動数が一致してしまうと、動翼4またはシュラク
ト6に大きな振動応力が発生し、群翼のなかでも特に応
力的に厳しい箇所であるテノン5が損傷してシュラウド
6を支持固定できなくなる。また、ボイtKて生成され
る蒸気中には不純物が含まれてお)、蒸気とともに蒸気
タービン内に飛び込んで来る。この不純物は金属粒子を
主成分とし、蒸気タービン内の各部を浸食あるいは摩耗
させる。また蒸気タービンの低圧部においては蒸気が復
水し水滴となり、この水滴も蒸気タービン内の各部を浸
食あるいは摩耗させる。特にノズル8から噴出後動翼4
に衝突しないでシュラウド6の外側を通る蒸気は、動翼
4の先端において蒸気流速が速くなるので、浸食あるい
は摩耗の程度が大きくなる傾向にある。なかでもテノン
5は最も浸食あるいは摩耗烙れ易い。セしてテノン5が
浸食あるいは摩耗されると、シュラクト6を支持固定す
ることができなくなるので補修が必要となる゛。この場
合の補修方法としては、テノン5が動翼4と一体構造と
なっているため、一つのシュラウドで連結されている動
翼群を羽根車3から抜き取シ、損傷した動翼は新製して
再組立てし再び羽根車に挿入するという方法であった。During steam turbine operation, in addition to the centrifugal force that acts on the rotor blades 4, the rotor blades 4 are also subjected to high-cycle excitation force of several thousand times per second or more due to the jet flow from the upstream nozzle 8, and are also subjected to power generation due to the unevenness of the individual nozzle areas. Low-cycle excitation forces are also applied due to uneven distribution of fluid and changes in the direction of gravity due to fixed rotation. At the time of design, the excitation force applied to the rotor blade 4 and the characteristic number of worms of the rotor blade 4 do not match, but the area of each nozzle of the nozzle 8 changes over time due to erosion and other traps. Therefore, if the excitation frequency applied to the rotor blades 4 and the natural frequency of the rotor blades 4 match, large vibration stress will occur in the rotor blades 4 or shracto 6, and the stress will be particularly high among the group of blades. The tenon 5, which is a critical location, is damaged and cannot support and fix the shroud 6. In addition, the steam generated by boiling water contains impurities), which flow into the steam turbine together with the steam. These impurities are mainly composed of metal particles and corrode or wear out various parts within the steam turbine. Further, in the low pressure section of the steam turbine, steam condenses and becomes water droplets, and these water droplets also erode or wear out various parts within the steam turbine. In particular, after jetting from the nozzle 8, the rotor blade 4
If the steam passes through the outside of the shroud 6 without colliding with the rotor blade 4, the steam flow velocity will be higher at the tip of the rotor blade 4, so the degree of erosion or wear will tend to increase. Among them, Tenon 5 is the most susceptible to erosion and wear. If the tenon 5 becomes eroded or worn out, it will no longer be able to support and fix the shracto 6 and will need to be repaired. In this case, the repair method is to remove the rotor blades, which are connected by one shroud, from the impeller 3, as the tenon 5 has an integral structure with the rotor blades 4, and replace the damaged rotor blades with new ones. The method was to reassemble it and insert it into the impeller again.
このように動翼を新製しなければならないので多大の工
数を必要とし補修期間が長くなるという欠点があった。Since the rotor blades must be newly manufactured in this way, there is a drawback that a large number of man-hours are required and the repair period becomes long.
本発明は上記従来方法の欠点を除くためになされたもの
で、動Rを新製することなく損傷した動翼を簡単な加工
によって再使用することによシ補修期間が短縮できるよ
うな蒸気タルピン動翼の補修方法を提供することを目的
とする。The present invention has been made in order to eliminate the drawbacks of the above-mentioned conventional methods, and it is a steam talpin that can shorten the repair period by reusing damaged rotor blades through simple processing without having to manufacture a new rotor blade. The purpose is to provide a method for repairing rotor blades.
上記目的を達成するため本発明は、テノン部が損傷した
動翼をシュ2ウドから取り外し、その先端肩部を均一に
ナシ下げて新たなテノンを形成させた後、再びシュラウ
ドの孔に挿入し、かしめにニジ固定することを4I敵と
するものである。In order to achieve the above object, the present invention removes a rotor blade with a damaged tenon part from a shroud, lowers its tip shoulder uniformly to form a new tenon, and then reinserts it into a hole in the shroud. , 4I is the enemy of fixing the nails by caulking.
以下本発明の一実施例につき第4図を参照して説明する
。第4図に示す如く損傷の認められた動翼4はシュ2ウ
ドから取外し、斜線で示す肩部Aを均一にす)下げてテ
ノン5を新たに形成するOこの場合、一般的にはこのテ
ノン5のかしめ代i=2・40程度となるようKする。An embodiment of the present invention will be described below with reference to FIG. As shown in Figure 4, the rotor blade 4 that has been found to be damaged is removed from the shroud and lowered to make a new tenon 5 (to make the shoulder A shown with diagonal lines uniform). K the tenon 5 so that the caulking distance i is approximately 2.40.
つぎに従来技術と同様に第2図に示す如くシュラウド6
の孔7をテノン5に嵌合させ、かしめによりシュラウド
°を固定して動翼群を構成させて復旧する。Next, as in the prior art, as shown in FIG.
The hole 7 is fitted into the tenon 5, and the shroud is fixed by caulking to form a rotor blade group and restored.
この補修方法によれば、動翼4の高さが幾分低くなるの
で、第1図におけるチップフィン9とシュラウド6との
半径方向間隙が大きくなり、動翼先端部からの漏洩蒸気
量が増加し蒸気タービンの性能が低下することになるが
、その低下量は一般に熱消費率で0.001.、S程度
で極めて微少であ)、性能的には問題になることはない
ものである。According to this repair method, the height of the rotor blade 4 is somewhat lowered, so the radial gap between the tip fin 9 and the shroud 6 in FIG. 1 becomes larger, and the amount of steam leaking from the tip of the rotor blade increases. However, the performance of the steam turbine decreases, but the amount of decrease is generally 0.001. , S, which is extremely small) and poses no problem in terms of performance.
また全周の動翼4について本発明による補修方法を行な
うならば、動翼肩部Aのすり下げた量だけ長いチップフ
ィン9を新製することによって半径方向間隙を変わらな
いようにすることができるので、動翼先端部からの漏洩
蒸気量は増〃口することなく、性能的には問題のないこ
とになる0〔発明の効果〕
以上説明したように本発明によれば、損傷した動翼の先
端肩部を均一にすり下げて新たなテノン全形成させると
いう簡単な加工を施行することKよシ、動翼を新製する
ことなくして補修が可能となるので、補修期間を大幅に
短縮できるという効果が得られる。Furthermore, if the repair method according to the present invention is applied to the rotor blade 4 around the entire circumference, it is possible to keep the radial gap unchanged by manufacturing a new tip fin 9 that is longer by the amount that the rotor blade shoulder A is slid down. Therefore, the amount of steam leaking from the tip of the rotor blade does not increase, and there is no problem in terms of performance. [Effects of the Invention] As explained above, according to the present invention, the amount of steam leaking from the tip of the rotor blade does not increase. By carrying out a simple process such as uniformly sliding down the tip shoulder of the blade to form a new tenon, it is possible to perform the repair without having to manufacture a new rotor blade, which significantly shortens the repair period. This has the effect of shortening the time.
第1図は従来の蒸気タービンの内部構造を示す断面図、
第2図は蒸気タービン動翼の斜視図、第3図は動翼の先
端部のテノンおよびシュラウドを示す正面図、第4図は
本発明の一実施例を示す正面図である。
4・・動翼、 5 ・テノン、 6・・シュラウド
、7・・シュラウドの孔、 A・動翼先端肩部。
代理人 弁理士則 近 憲 佑 (ほか1名)第1図
/
第2図
第3図
第4図
5りFigure 1 is a sectional view showing the internal structure of a conventional steam turbine;
FIG. 2 is a perspective view of a steam turbine rotor blade, FIG. 3 is a front view showing a tenon and shroud at the tip of the rotor blade, and FIG. 4 is a front view showing an embodiment of the present invention. 4. Moving blade, 5. Tenon, 6. Shroud, 7. Shroud hole, A. Moving blade tip shoulder. Agent Patent Attorney Rules Kensuke Chika (and 1 other person) Figure 1 / Figure 2 Figure 3 Figure 4 Figure 5
Claims (1)
孔に挿入し、かしめによシこのシュラウドを固定する構
造の蒸気タービン動翼の補修方法において、テノン部が
損傷した動翼を前記シュラウドから取シ外し、その先端
肩部を均一にすシ下げて新たなテノンを形成させた後、
再び前記シュラウドの孔に挿入し、かしめによシ固定す
ることrを特徴とする蒸気タービン動翼の補修方法。In a method for repairing steam turbine rotor blades, a tenon cut out integrally at the tip of the rotor blade is inserted into a hole in the shroud, and the shroud is fixed by caulking. After removing it from the shroud and lowering its tip shoulder evenly to form a new tenon,
A method for repairing a steam turbine rotor blade, comprising reinserting the shroud into the hole and fixing it by caulking.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP530983A JPS59131703A (en) | 1983-01-18 | 1983-01-18 | Repairing method for moving blade of steam turbine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP530983A JPS59131703A (en) | 1983-01-18 | 1983-01-18 | Repairing method for moving blade of steam turbine |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS59131703A true JPS59131703A (en) | 1984-07-28 |
Family
ID=11607669
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP530983A Pending JPS59131703A (en) | 1983-01-18 | 1983-01-18 | Repairing method for moving blade of steam turbine |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS59131703A (en) |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5493657A (en) * | 1977-12-12 | 1979-07-24 | Cretella Salvatore | Restoring method of wornnout turbine blade |
-
1983
- 1983-01-18 JP JP530983A patent/JPS59131703A/en active Pending
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5493657A (en) * | 1977-12-12 | 1979-07-24 | Cretella Salvatore | Restoring method of wornnout turbine blade |
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