JPS63295802A - Repairing of nozzle plate of steam turbine - Google Patents
Repairing of nozzle plate of steam turbineInfo
- Publication number
- JPS63295802A JPS63295802A JP12961087A JP12961087A JPS63295802A JP S63295802 A JPS63295802 A JP S63295802A JP 12961087 A JP12961087 A JP 12961087A JP 12961087 A JP12961087 A JP 12961087A JP S63295802 A JPS63295802 A JP S63295802A
- Authority
- JP
- Japan
- Prior art keywords
- nozzle
- nozzle plate
- cut
- thin plate
- welding
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P6/00—Restoring or reconditioning objects
- B23P6/002—Repairing turbine components, e.g. moving or stationary blades, rotors
- B23P6/007—Repairing turbine components, e.g. moving or stationary blades, rotors using only additive methods, e.g. build-up welding
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Description
【発明の詳細な説明】
し発明の目的コ
(産業上の利用分野)
本発明は蒸気タービンの運転中にエロージョンによって
ノズル板の後縁部に欠損部が生じた場合、これを正常な
形状に復元するノズル板補修方法に関する。[Detailed Description of the Invention] Purpose of the Invention (Industrial Field of Application) The present invention is directed to a method for restoring a defective portion to a normal shape when a defective portion occurs at the rear edge of a nozzle plate due to erosion during operation of a steam turbine. This article relates to a nozzle plate repair method for restoration.
(従来の技術)
火力発電所において、ボイラ内のパイプ内壁などには次
第番二酸化スケールが付着する。この酸化スケールは小
さな固体粒子(パーティクル)として蒸気内に混入し、
蒸気とともに蒸気タービンに流入する。(Prior Art) In thermal power plants, carbon dioxide scale often adheres to the inner walls of pipes in boilers. This oxidized scale is mixed into the steam as small solid particles (particles),
It flows into the steam turbine along with the steam.
タービン内に流入した蒸気はノズルにて圧力を低下させ
ながら急速に増速し、流れの方向も大きく変化する(転
向量=約70°〜75°)が、酸化スクールパーティク
ルPは蒸気に比べると質量が大きく、慣性力の影響を強
く受けるため、タービンノズル内での大きな方向転換に
追従することができず、第5図の矢符に示すように、ノ
ズル板lの腹側後縁部に衝突する。その結果、ノズル板
1の後縁部は第2図に示すように次第に欠損し、いわゆ
るパーティクル・エロージョンEが発生する。The steam that has flowed into the turbine rapidly increases in speed while decreasing the pressure at the nozzle, and the direction of the flow changes greatly (amount of turning = about 70° to 75°), but the oxidized school particles P are smaller than the steam. Since the mass is large and is strongly affected by inertial force, it is unable to follow large changes in direction within the turbine nozzle, and as shown by the arrow in Fig. 5, the ventral rear edge of the nozzle plate l collide. As a result, the rear edge of the nozzle plate 1 gradually breaks off as shown in FIG. 2, and so-called particle erosion E occurs.
同図中、符号2はノズル外輪を、3はノズル内輪を示す
。In the figure, numeral 2 indicates the nozzle outer ring, and 3 indicates the nozzle inner ring.
このパーティクル・エロージョンによって欠損が生じた
ノズル板によって形成される蒸気流路は設計流路から大
きく逸脱しており、蒸気タービンの性能を著しく低下さ
せる上、タービン動翼に励振力を作用させ、蒸気タービ
ンの信頼性を低下させる。The steam flow path formed by the nozzle plate that has been damaged due to particle erosion greatly deviates from the designed flow path, which not only significantly reduces the performance of the steam turbine, but also causes an excitation force to act on the turbine rotor blades, causing the steam Reduces turbine reliability.
従って、定期的に実施される蒸気タービンの解放点検に
おいて上述のような欠損部を生じているノズル板が発見
されると、正常な形状に復元するため、ノズル板の補修
が行われる。Therefore, if a nozzle plate having a defect as described above is discovered during a periodic overhaul inspection of a steam turbine, the nozzle plate is repaired to restore it to its normal shape.
第6図と第7図は従来のノズル板補修方法を模式的に示
すもので、外端と内端をそれぞれノズル外輪2とノズル
内輪3に固定したノズルダイヤフラムをノズル板1の蒸
気流出側が上面を向くようにセツティングし、先ず、ノ
ズル板の欠損部をグラインダー等で開先造形する0次に
、補修部分の腹側にノズル板1の腹側と同形状の銅板4
を当てがい、下向きTIG溶接により、符号■〜■で示
す順番で肉盛り5を施す。Figures 6 and 7 schematically show a conventional nozzle plate repair method, in which a nozzle diaphragm whose outer and inner ends are fixed to the nozzle outer ring 2 and the nozzle inner ring 3, respectively, is attached so that the steam outflow side of the nozzle plate 1 faces upward. First, the defective part of the nozzle plate is shaped with a grinder or the like. Next, a copper plate 4 having the same shape as the ventral side of the nozzle plate 1 is placed on the ventral side of the repaired part.
, and apply the build-up 5 by downward TIG welding in the order shown by symbols ① to ②.
肉盛りの完了後、ノズル板1を焼鈍し、しかる後、肉盛
り部5をグラインダー等で整形し、正常なノズル板形状
になるよう補修する。After the build-up is completed, the nozzle plate 1 is annealed, and then the build-up portion 5 is shaped with a grinder or the like and repaired to have a normal nozzle plate shape.
(発明が解決しようとする問題点)
上述のように従来の補修方法では、ノズル板欠損部の復
元をすべて溶接肉盛りで行っているが、ノズル板は円弧
を滑らかに連接した曲線形状である上、肉盛り部の表面
が溶接特有の凹凸面であるため、肉盛り溶接部に肉不足
が生じやすい。しがも、この肉不足はグラインダーなど
による肉盛り部の整形作業後でないと判明しにくいため
、整形作業後に肉不足が判明したときは、再度、肉盛り
溶接、焼鈍、グラインダー整形等の作業を行わねばなら
ず、作業効率が低下するという問題点があった。(Problems to be solved by the invention) As mentioned above, in the conventional repair method, the damaged part of the nozzle plate is entirely restored by welding, but the nozzle plate has a curved shape with smoothly connected circular arcs. On the other hand, since the surface of the build-up part is uneven, which is unique to welding, insufficient thickness tends to occur in the build-up weld part. However, it is difficult to detect this lack of thickness until after the fill-up area has been shaped using a grinder, etc., so if it is found that there is a lack of fillet after shaping, work such as build-up welding, annealing, and grinder shaping should be performed again. There was a problem in that work efficiency was lowered.
本発明はこのような問題点を解消し、作業が容易で信頼
性の高い蒸気タービンの制御装置を提供することを目的
とするものである。An object of the present invention is to solve these problems and provide a steam turbine control device that is easy to operate and has high reliability.
[発明の構成]
(問題点を解決するための手段)
本発明の蒸気タービンのノズル板補修方法は固体粒子に
よるエロージョンによってノズル板の後縁部に欠損が生
じた場合、この欠損部分を含むノズル板後縁部全体を直
線状に切断除去し、そこに、前記切断除去したノズル板
後縁部の原形と同一形状の薄板小片を開先溶接すること
を特徴とするものである。[Structure of the Invention] (Means for Solving the Problems) The method for repairing a nozzle plate of a steam turbine according to the present invention is a method for repairing a nozzle plate including the defective portion when a defect occurs at the trailing edge of the nozzle plate due to erosion by solid particles. This method is characterized in that the entire rear edge of the plate is cut and removed in a straight line, and a small piece of thin plate having the same shape as the original shape of the cut and removed rear edge of the nozzle plate is groove-welded thereto.
(作用)
上述のように、本発明の蒸気タービンのノズル板補修方
法においては、薄板小片をノズル板の欠損部にはめこん
で溶接するようにしたので、溶接領域は大幅に減少し、
肉不足が生じた場合にもこれを一目で判別することがで
きる。(Function) As described above, in the steam turbine nozzle plate repair method of the present invention, a small piece of thin plate is inserted into the defective part of the nozzle plate and welded, so the welding area is significantly reduced.
Even if there is a shortage of meat, this can be determined at a glance.
(実施例) 以下、本発明の詳細な説明する。(Example) The present invention will be explained in detail below.
第2図に示すように、ノズル板1にパーティクルエロー
ジョンによる欠損部Eが生じている場合には、欠損部E
が含まれるノズル板の後縁部全体を一点鎖線りにて示す
ように直線状に切断除去し、その端面を開先形状に仕上
げる0次に、第3図および第4図に示すように、切除し
たノズル板の後縁部分の原形と同一形状の薄板小片6を
切除部分と同じ長さに切断し、その切断面を開先整形す
る。As shown in FIG. 2, when the nozzle plate 1 has a defective part E due to particle erosion, the defective part E
Cut and remove the entire rear edge of the nozzle plate in a straight line as shown by the dash-dotted line, and finish the end face in a beveled shape. Next, as shown in FIGS. 3 and 4, A small thin plate piece 6 having the same shape as the original shape of the rear edge portion of the cut nozzle plate is cut to the same length as the cut portion, and the cut surface is beveled.
この薄板小片6がノズル板1の切断面に滑らかに接合す
ることを確認した後、薄板小片6の溶接を行う。After confirming that this small thin plate piece 6 is smoothly joined to the cut surface of the nozzle plate 1, the small thin plate piece 6 is welded.
この溶接に際しては、第4図に示すようにノズル板1と
薄板小片6との突合わせ部の裏側に規定の曲面形状の銅
板4を当てがい、突合わせ開先面間をTIG溶接で仮溶
接7し、続いて、薄板小片とノズル外輪2およびノズル
内輪3との間をTIG溶接で仮溶接する。For this welding, as shown in Fig. 4, a copper plate 4 with a prescribed curved shape is applied to the back side of the butt part between the nozzle plate 1 and the small thin plate piece 6, and the butt groove surfaces are temporarily welded by TIG welding. 7, and then the thin plate pieces and the nozzle outer ring 2 and the nozzle inner ring 3 are temporarily welded by TIG welding.
次に、第1図に示すように後退溶接法により突合わせ開
先面間を多層盛り溶接7し、更に薄板小片6の両端とノ
ズル内外輪との間を一層ずつ交互に多Raり溶接8.9
する。Next, as shown in FIG. 1, multi-layer welding 7 is performed between the butt groove surfaces using the backward welding method, and then multi-Ra welding 8 is performed alternately between both ends of the thin plate piece 6 and the inner and outer rings of the nozzle. .9
do.
溶接の完了後、焼鈍を行い、余盛りビード部をグライン
ダー等で整形する。After welding is completed, annealing is performed and the excess bead portion is shaped using a grinder or the like.
[発明の効果]
上述のように、本発明のノズル板補修方法はエロージョ
ンによって欠損した部分を直線状に切断除去し、そこに
切除部分と同一の寸法の薄板小片を突合わせ溶接するも
のであるから、第1図と第8図とを対比すれば明らかな
ように、溶接領域を大幅に低減させることができ、グラ
インダー整形作業に要する時間も短縮できる上、従来の
肉盛り溶接と比べて溶接性が飛躍的に向上する。また、
薄板小片全体の肉不足は溶接施行前に確認できるので、
従来のような、溶接肉盛り→焼鈍→グラインダー整形と
いったような修正作業を再度行う必要がなく、作業性は
大幅に向上する。[Effects of the Invention] As described above, the nozzle plate repair method of the present invention involves cutting and removing the portion damaged by erosion in a straight line, and butt welding a small thin plate piece having the same dimensions as the cut portion thereto. As is clear from comparing Figures 1 and 8, the welding area can be significantly reduced, the time required for grinder shaping work can be shortened, and the welding process is faster than conventional overlay welding. Sexuality improves dramatically. Also,
The lack of thickness in the entire small piece of thin plate can be confirmed before welding, so
There is no need to repeat the conventional correction work such as weld build-up → annealing → grinder shaping, and work efficiency is greatly improved.
第1図は本発明方法によって補修した蒸気タービンのノ
ズルダイヤフラムの斜視図、第2図は欠損部分が生じて
いるノズルダイヤフラムの斜視図、第3図と第4図は本
発明方法の工程を示す説明図、第5図は蒸気タービン内
における固体粒子の動きを示す説明図、第6図と第7図
は従来方法の工程を示す説明図、第8図は従来方法によ
って補修した蒸気タービンのノズルダイヤフラムの斜視
図である。
1・・・・・・・・・ノズル板
2・・・・・・・・・ノズル外輪
3・・・・・・・・・ノズル内輪
4・・・・・・・・・銅板
5・・・・・・・・・溶接部
6・・・・・・・・・薄板小片
7.8.9・・・溶接部
代理人 弁理士 則 近 憲 佑
同 第子丸 健
第1図
第2図
第3図
第4図
第5図
第6図
第7図Fig. 1 is a perspective view of a nozzle diaphragm of a steam turbine repaired by the method of the present invention, Fig. 2 is a perspective view of a nozzle diaphragm with a defective part, and Figs. 3 and 4 show the steps of the method of the present invention. Explanatory diagram: Figure 5 is an explanatory diagram showing the movement of solid particles in the steam turbine; Figures 6 and 7 are explanatory diagrams showing the steps of the conventional method; Figure 8 is a nozzle of a steam turbine repaired by the conventional method. FIG. 3 is a perspective view of a diaphragm. 1... Nozzle plate 2... Nozzle outer ring 3... Nozzle inner ring 4... Copper plate 5... ...Welding section 6... Thin plate small piece 7.8.9... Welding section agent Patent attorney Nori Chika Ken Yudo Ken Daishimaru Figure 1 Figure 2 Figure 3 Figure 4 Figure 5 Figure 6 Figure 7
Claims (2)
後縁部に欠損が生じた場合、この欠損部分を含むノズル
板後縁部全体を直線状に切断除去し、そこに、前記切断
除去したノズル板後縁部の原形と同一形状の薄板小片を
開先溶接することを特徴とする蒸気タービンのノズル板
補修方法。(1) If a defect occurs at the rear edge of the nozzle plate due to erosion by solid particles, cut and remove the entire rear edge of the nozzle plate including the defective part in a straight line, and place the cut and removed part on the rear edge of the nozzle plate. A method for repairing a nozzle plate for a steam turbine, characterized by groove welding a small piece of thin plate having the same shape as the original shape of the edge.
輪に溶接することを特徴とする特許請求の範囲第1項記
載の蒸気タービンのノズル板補修方法。(2) A method for repairing a nozzle plate for a steam turbine according to claim 1, characterized in that the inner and outer circumferential surfaces of the thin plate pieces are welded to the nozzle inner ring and the nozzle outer ring.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP12961087A JPS63295802A (en) | 1987-05-28 | 1987-05-28 | Repairing of nozzle plate of steam turbine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP12961087A JPS63295802A (en) | 1987-05-28 | 1987-05-28 | Repairing of nozzle plate of steam turbine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS63295802A true JPS63295802A (en) | 1988-12-02 |
Family
ID=15013717
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP12961087A Pending JPS63295802A (en) | 1987-05-28 | 1987-05-28 | Repairing of nozzle plate of steam turbine |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS63295802A (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2002004883A (en) * | 2000-06-20 | 2002-01-09 | Ishikawajima Harima Heavy Ind Co Ltd | Wing repair method and wing repair jig |
| JP2002006911A (en) * | 2000-03-02 | 2002-01-11 | General Electric Co <Ge> | Nominal moving machining |
| USRE37562E1 (en) | 1988-05-05 | 2002-02-26 | Siemens Westinghouse Power Corporation | Turbine system having more failure resistant rotors and repair welding of low alloy ferrous turbine components by controlled weld build-up |
| WO2006026695A3 (en) * | 2004-08-30 | 2006-04-20 | Honeywell Int Inc | Welding shield for automated welding of impellers and blisks, sized to match within vallexs of a particular designed impeller ; method to provide protection from welding related damage in an impeller |
| EP1721697A1 (en) * | 2005-05-06 | 2006-11-15 | United Technologies Corporation | Superalloy repair methods and inserts |
| EP1721696A1 (en) * | 2005-05-06 | 2006-11-15 | United Technologies Corporation | Superalloy repair methods and inserts |
| EP1371439B2 (en) † | 2002-06-10 | 2014-06-25 | United Technologies Corporation | Method of weld repairing a component for a turbine engine with a refractory metal backing material |
-
1987
- 1987-05-28 JP JP12961087A patent/JPS63295802A/en active Pending
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| USRE37562E1 (en) | 1988-05-05 | 2002-02-26 | Siemens Westinghouse Power Corporation | Turbine system having more failure resistant rotors and repair welding of low alloy ferrous turbine components by controlled weld build-up |
| JP2002006911A (en) * | 2000-03-02 | 2002-01-11 | General Electric Co <Ge> | Nominal moving machining |
| JP2002004883A (en) * | 2000-06-20 | 2002-01-09 | Ishikawajima Harima Heavy Ind Co Ltd | Wing repair method and wing repair jig |
| EP1371439B2 (en) † | 2002-06-10 | 2014-06-25 | United Technologies Corporation | Method of weld repairing a component for a turbine engine with a refractory metal backing material |
| WO2006026695A3 (en) * | 2004-08-30 | 2006-04-20 | Honeywell Int Inc | Welding shield for automated welding of impellers and blisks, sized to match within vallexs of a particular designed impeller ; method to provide protection from welding related damage in an impeller |
| US7247000B2 (en) | 2004-08-30 | 2007-07-24 | Honeywell International, Inc. | Weld shielding device for automated welding of impellers and blisks |
| EP1721697A1 (en) * | 2005-05-06 | 2006-11-15 | United Technologies Corporation | Superalloy repair methods and inserts |
| EP1721696A1 (en) * | 2005-05-06 | 2006-11-15 | United Technologies Corporation | Superalloy repair methods and inserts |
| EP1721697B2 (en) † | 2005-05-06 | 2015-03-11 | United Technologies Corporation | Superalloy repair methods and inserts |
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