JPS58138204A - Steam turbine blade - Google Patents
Steam turbine bladeInfo
- Publication number
- JPS58138204A JPS58138204A JP2088682A JP2088682A JPS58138204A JP S58138204 A JPS58138204 A JP S58138204A JP 2088682 A JP2088682 A JP 2088682A JP 2088682 A JP2088682 A JP 2088682A JP S58138204 A JPS58138204 A JP S58138204A
- Authority
- JP
- Japan
- Prior art keywords
- blade
- erosion
- prevention plate
- vane
- view
- 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
- F01D5/12—Blades
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Materials Engineering (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羽根のうち特に、翼先端部におけ
る浸食を防ぐことができるようKしたものに関する。DETAILED DESCRIPTION OF THE INVENTION [Technical Field of the Invention] The present invention relates to steam turbine blades, particularly those having a K-shaped blade to prevent erosion at the tip of the blade.
一般の蒸気タービン羽根のうち最終段などを構成する翼
部の長いものは第1図に示す如く、翼/の下部にはター
ビン円板に挿入する脚部/’&が一体的に形成される2
ともに、翼根元と翼先端とにおける蒸気の相対速度を等
しくするためK、第コそして、翼lの先端の間隔を正し
くし、且つ蒸気が外周に飛び出すのを防ぐため、翼lの
先端部に羽根カパーコを一体的に削り出し、第3図に示
す如く、この羽根カパーコの両端部コa、コbを近接す
る翼の羽根カバーλの端部と溶接するよう圧して一個の
動翼などを作るようにしている・そして、最終段などで
は低温低圧の浸り蒸気中で運転するため、羽根は湿分が
凝集粗大化した水滴の衝突圧する浸食を受けやすい。こ
のため高硬度の合金からなる浸食防止板3を翼lの先端
部に溶接にて取り付けている。Among general steam turbine blades, those with a long blade section constituting the final stage, etc., have a leg section /'& that is inserted into the turbine disk integrally formed at the bottom of the blade, as shown in Figure 1. 2
In order to equalize the relative velocity of the steam at the blade root and the blade tip, the distance between the tips of the blade K and the tip of the blade L is correct, and in order to prevent the steam from flying out to the outer periphery, there is a The blade cover is cut out as one piece, and as shown in Fig. 3, both ends of the blade cover λ are welded to the ends of the blade cover λ of the adjacent blade to form a single rotor blade. Since the final stage and other stages operate in low-temperature, low-pressure immersed steam, the blades are susceptible to erosion due to the impact pressure of water droplets that have aggregated and coarsened moisture. For this purpose, an erosion prevention plate 3 made of a high-hardness alloy is attached to the tip of the blade 1 by welding.
この浸食防止板3はコざ参クロム、4!:11タングス
テン・コバルト合金からなり、その形状は第弘図(IL
) (正面図)及び(b)(平面図)に示す如く一方の
側端部が゛膨出した板状をなし、この浸食防止板3を翼
lK溶着するには第3図及び第1図に示す如く浸食防止
板Jの外周に沿って溶接開先参を設け、第7図に示す如
く、溶接開先ダのうち翼lとの間に設けた溶接開先70
−ニッケル・x91クロム合金からなる溶着金属参1を
盛9込み、また羽根カバーコとの間に設けた溶接開先に
浸食防止板Jと同じ組成からなる溶着金属abを盛り上
げて硬さを増すようにしている。This erosion prevention plate 3 is made of Kozasan chrome, 4! :11 Made of tungsten-cobalt alloy, its shape is as shown in Fig.
) As shown in (front view) and (b) (plan view), it has a plate shape with one side end bulged, and in order to weld this erosion prevention plate 3 to the blade lK, the steps shown in Figures 3 and 1 are as follows. As shown in FIG. 7, a welding groove 70 is provided along the outer periphery of the erosion prevention plate J, and as shown in FIG.
- Weld metal 1 made of nickel x91 chromium alloy is added, and weld metal ab made of the same composition as the corrosion prevention plate J is heaped up on the weld groove provided between the blade cover and the blade cover to increase its hardness. I have to.
しかしながら、溶着金属#bを盛り上げ、表面仕上げを
行なう際に、溶着金属pbの一部が削り取られ、厚さに
バラツキが生じる。その結果、長年運転すると、第を図
及び第り図に示す如傘浸食部!の発生が避けられず、ま
た溶着金属を厚くしても羽根カバー2は翼lと同様Vc
lコ優クロム鋼であるかめ水滴による浸食は避は難いと
いう量販がある。However, when welding metal #b is heaped up and surface finishing is performed, part of welding metal pb is scraped off, resulting in variations in thickness. As a result, after many years of operation, the erosion part as shown in Figures 1 and 2! The occurrence of Vc is unavoidable, and even if the welded metal is made thicker, the blade cover 2 has a Vc
There are mass marketers who say that corrosion due to water droplets is unavoidable due to the use of chromium-rich steel.
本発明は上述の如き羽根完成後の浸食を有効に防止し得
る蒸気ターピッ羽根を提供することを目的としている。An object of the present invention is to provide a steam turpentine blade that can effectively prevent erosion after the blade is completed as described above.
上記の目的を連破すべく、本発笥は翼から一体的に削9
出した羽根カバーの翼の直上部の少くとも一部に凹部を
形成し、との凹部に羽根カバーの先端部を嵌め込むよう
に一体化し、羽根カバー直下に浸食防止板を溶着する溶
着金属が露出しないように構成したことを要旨としてい
る。In order to continuously achieve the above purpose, this launcher was designed by cutting 9 integrally from the wing.
A recess is formed in at least a part of the blade cover directly above the blade, and the tip of the blade cover is fitted into the recess, and the welding metal for welding the erosion prevention plate is placed directly under the blade cover. The main point is that the structure is designed to prevent exposure.
以下に本発明の実施の一例を第10図乃至第13図に基
いて説明する。An example of the implementation of the present invention will be described below with reference to FIGS. 10 to 13.
第1O図(aJは本発明の浸食防止板tを正面から見た
図、第1O図(b)は浸食防止板乙の先端部をA方向か
ら見た図であり、浸食防止板6は略々板状をなし、その
先端部には突出部daを形成している。Figure 1O (aJ is a front view of the erosion prevention plate t of the present invention, Figure 1O (b) is a view of the tip of the erosion prevention plate B viewed from the direction A, and the erosion prevention plate 6 is approximately Each plate is shaped like a plate, and a protrusion da is formed at its tip.
第1/図及び第72図は上記浸食防止板tを翼/に増り
付けた状態を示すものであり、羽根カバー7に溶接開先
となる凹部tを形成しており、この四部jK上上記食防
止板乙の突出部6aを嵌め込み、第73図に示す如く溶
着金属pbによりそ溶接する。Fig. 1/ and Fig. 72 show the state in which the above-mentioned erosion prevention plate t is added to the blade/, and the blade cover 7 is formed with a recessed portion t which becomes a welding groove, and the four parts jK The protrusion 6a of the corrosion prevention plate A is fitted and welded with the weld metal pb as shown in FIG. 73.
尚、凹部tを形成する部分の羽根カッ(−7の厚みはλ
〜jifJが適尚である゛。そして凹ませたことで生じ
た段差分は浸食防止板4と同じ組成の溶着金属で盛り上
げておくようにすれば翼群の羽根カッ(−を面一に仕上
げる上で都合がよい。In addition, the thickness of the blade cutter (-7) of the part forming the recess t is λ
~ jifJ is appropriate゛. If the step difference caused by the depression is raised with welded metal having the same composition as the erosion prevention plate 4, it is convenient to finish the blades of the blade group flush.
以上の如く本発1jlKよれば、翼から一体的に削り出
した羽根カバーの翼の直上部、即ち浸食を受けやすい部
分まで浸食を受けKくい浸食防止板で覆うようにしたの
で、浸食防止の観点から品質が不均一となり易い部分を
なくすことができ、長期間運転しても浸食を受けること
がない。As described above, according to the main engine 1jlK, the blade cover cut out integrally from the wing is covered with the corrosion prevention plate directly above the wing, that is, the part that is susceptible to erosion, so that it is covered with the corrosion prevention plate. From this point of view, it is possible to eliminate areas where quality is likely to be uneven, and there is no erosion even after long-term operation.
図面は従来例及び本発明の実施の一例を示すものであり
、第7図は従来のターピッ羽根の正面図、第2図は同タ
ービン羽根を1方向から見た平面図、第3図は従来の羽
根カバーの拡大図、第参図(aJ)i従来の羽根カバー
の正面図、第φ図ft)Jは同カッ(−を真方向から見
た平面図、第3図は従来の溶接開先の部分を示す図、第
を図は第5図のVl−Vl線断面図、第7図は溶接開先
に溶着金属を盛り込んだ状態を示す正面図、第を図は浸
食部分を示した正面図、第2図は浸食部分を示した第2
図のff−W線断面図、第10図(&)は本発明に一体
る浸食防止板の正面図、第10図(b)は浸食防止板の
真方向から見た平面陶、第1/図は本発明に浸食防止板
を溶着した状態を示す平面図、第72図は浸食防止板を
溶着した羽根の正面図、第13図は溶着部を示した斜視
図である。
ハ・・翼、2.7・・・羽根カバー、3.1・・浸食防
止板、da・・・浸食防止板の突出部、r・・・凹部。The drawings show a conventional example and an example of the implementation of the present invention. Fig. 7 is a front view of a conventional turbine blade, Fig. 2 is a plan view of the same turbine blade as seen from one direction, and Fig. 3 is a conventional turbine blade. An enlarged view of the blade cover in Figure (aJ), i) Front view of the conventional blade cover, Figure φft) Figure 7 is a cross-sectional view taken along the line Vl-Vl in Figure 5, Figure 7 is a front view showing the welding groove with deposited metal, and Figure 7 shows the eroded part. Front view, Figure 2 shows the eroded area.
10(&) is a front view of the erosion prevention plate integrated in the present invention, and FIG. 10(b) is a flat ceramic viewed from the direct direction of the erosion prevention plate. The figure is a plan view showing the state in which the erosion prevention plate is welded to the present invention, FIG. 72 is a front view of the blade to which the erosion prevention plate is welded, and FIG. 13 is a perspective view showing the welded part. c... wing, 2.7... vane cover, 3.1... erosion prevention plate, da... protrusion of erosion prevention plate, r... recess.
Claims (1)
止板を溶着するようKしたタービン羽根において、上記
羽根カバーの翼と連続する翼の直上部分の少くとも一部
に凹部を形成し、との凹部に浸食防止板の先端部を一体
的に嵌着してなる蒸気タービン羽根。In a turbine blade in which a blade cover is cut out at the tip of the blade and an erosion prevention plate is welded to the blade, a recess is formed in at least a part of the blade cover immediately above the blade, which is continuous with the blade; A steam turbine blade in which the tip of an erosion prevention plate is integrally fitted into a recess.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2088682A JPS58138204A (en) | 1982-02-12 | 1982-02-12 | Steam turbine blade |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2088682A JPS58138204A (en) | 1982-02-12 | 1982-02-12 | Steam turbine blade |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS58138204A true JPS58138204A (en) | 1983-08-17 |
Family
ID=12039683
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2088682A Pending JPS58138204A (en) | 1982-02-12 | 1982-02-12 | Steam turbine blade |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS58138204A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20190101000A1 (en) * | 2016-04-14 | 2019-04-04 | Mitsubishi Hitachi Power Systems, Ltd. | Steam turbine rotor blade, steam turbine, and method for manufacturing steam turbine rotor blade |
-
1982
- 1982-02-12 JP JP2088682A patent/JPS58138204A/en active Pending
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20190101000A1 (en) * | 2016-04-14 | 2019-04-04 | Mitsubishi Hitachi Power Systems, Ltd. | Steam turbine rotor blade, steam turbine, and method for manufacturing steam turbine rotor blade |
US10934847B2 (en) * | 2016-04-14 | 2021-03-02 | Mitsubishi Power, Ltd. | Steam turbine rotor blade, steam turbine, and method for manufacturing steam turbine rotor blade |
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