JPS6179802A - Turbine blade of steam turbine - Google Patents
Turbine blade of steam turbineInfo
- Publication number
- JPS6179802A JPS6179802A JP20059684A JP20059684A JPS6179802A JP S6179802 A JPS6179802 A JP S6179802A JP 20059684 A JP20059684 A JP 20059684A JP 20059684 A JP20059684 A JP 20059684A JP S6179802 A JPS6179802 A JP S6179802A
- Authority
- JP
- Japan
- Prior art keywords
- blade
- steam
- turbine
- covering
- amorphous
- 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】
産業上の利用分野
この発明は、特に低圧側の蒸気タービンのタービンブレ
ードに関する。DETAILED DESCRIPTION OF THE INVENTION Field of the Invention The present invention relates to turbine blades of steam turbines, particularly on the low-pressure side.
従来の技術
蒸気タービンにおける過熱蒸気は、高圧側の蒸気入口か
ら送流されて膨張してその圧力を低下しながら各段を通
過し、第2および3図に図示する低圧側のタービンブレ
ード01に作用して図示していないロータを回転させて
から、低圧側の排出口(同じく図示していない)から排
出されるようになっているが、その際の蒸気のエンタル
ピの低下にともなって、復水タービンにおいては、低圧
側の最終段近傍になると湿り蒸気になるので、蒸気中の
水滴が矢印06の方向から該ブレードにたたき付けられ
てそのブレード表面に腐食が発生する。そのために前記
表面腐食の防止の目的で従来は、前記ブレードの蒸気衝
突部にステライトと称されるCo −Cr −W合金薄
板04(以下ステライト薄板)を銀ろう05によって貼
付しているが、この方法にはつぎに述べる欠点がある。BACKGROUND OF THE INVENTION Superheated steam in a conventional steam turbine is sent from the steam inlet on the high pressure side, expands and passes through each stage while reducing its pressure, and is transferred to the turbine blades 01 on the low pressure side shown in FIGS. 2 and 3. After the steam is activated and rotates a rotor (not shown), the steam is discharged from the low-pressure side outlet (also not shown), but as the enthalpy of the steam decreases at that time, the recovery In a water turbine, near the final stage on the low-pressure side, the steam becomes wet, so water droplets in the steam strike the blades from the direction of arrow 06, causing corrosion on the blade surfaces. For this purpose, conventionally, for the purpose of preventing the surface corrosion, a Co-Cr-W alloy thin plate 04 called Stellite (hereinafter referred to as Stellite thin plate) was attached to the vapor collision part of the blade using silver solder 05. The method has the following drawbacks.
すなわち、■銀ろう05ろ5付けのために、タービンブ
レード01母材の疲労限が低下して該ブレードの強度設
計上の制約が厳しくなり、また■ステライト薄板04の
硬度が400〜450 Hv と高いので、該ブレード
の曲面に整合させて曲折してブレード表面に密着させる
ことが困難である上に、ろう付は作業が低能率的である
ために前記ブレードの製作に多大な工数が使わられる。In other words, (1) the fatigue limit of the base material of the turbine blade 01 is lowered due to the silver soldering (05), and restrictions on the strength design of the blade become stricter, and (2) the hardness of the Stellite thin plate 04 is 400 to 450 Hv. Since the blade is expensive, it is difficult to bend it to match the curved surface of the blade and make it adhere tightly to the blade surface, and brazing is an inefficient process, so a large amount of man-hours are required to manufacture the blade. .
発明の解決しようとする問題点
この発明は、タービンブレードの蒸気中の水滴の衝突に
よる衝突面の腐食を防止することを安価に生産性高(実
現することにある。Problems to be Solved by the Invention The object of the present invention is to prevent corrosion of the collision surface of a turbine blade due to collision of water droplets in steam at low cost and with high productivity.
問題点を解決するための手段
この発明は、タービンブレードの被腐食表面にアモルフ
ァス生成合金を蒸発被覆させてなるものである。Means for Solving the Problems In the present invention, an amorphous forming alloy is evaporated and coated on the surface of a turbine blade to be corroded.
作用
したがって、この発明の構成によれば、ブレード表面に
蒸発被覆したアモルファス生成合金は耐腐食性に優秀で
あるとともに、該合金の蒸着はブレード材の疲労限を低
下させることがなく、さらに該蒸着作業が容易に自動化
が可能であってその生産性を格段に向上させられる。Therefore, according to the configuration of the present invention, the amorphous forming alloy coated on the blade surface by evaporation has excellent corrosion resistance, and the vapor deposition of the alloy does not lower the fatigue limit of the blade material. Work can be easily automated and productivity can be greatly improved.
実施例
つぎに、この発明の実施例を図面によって説明すれば、
第1図において、低圧側のタービンブレードlの蒸気衝
突面に硬質アモルファス被膜7、例えば”e80B20
s Fe46Cr16M020C18等をレーザ、電
子ビーム等を加熱源として真空蒸着してなるもので、該
ブレードの下部に設けであるルート2は図示しないロー
タディスクの外周部のルート溝に嵌入されてあり、他の
多数のブレード1がともに固定しであるとともに、該ブ
レード上部に突設させであるテノンビン3は他の多数の
ブレード1ともども図示しないシュラウドバンドの対応
穴に挿嵌してからその先端の突出部分を圧壊させて固定
させているが、したがって、前記合金は、その蒸着粒子
がブレード表面に付着すると急冷されてアモルファス被
膜が容易に形成される。なお、前記真空蒸着方式以外の
他の蒸着手段を利用してもその効果に変わりがない。Embodiments Next, embodiments of the present invention will be described with reference to the drawings.
In FIG. 1, a hard amorphous coating 7, for example "e80B20
s Fe46Cr16M020C18 etc. is vacuum-deposited using a laser, an electron beam, etc. as a heating source, and the root 2 provided at the bottom of the blade is fitted into the root groove on the outer periphery of the rotor disk (not shown). A number of blades 1 are fixed together, and a tenon pin 3, which is protruded from the upper part of the blades, is inserted into a corresponding hole in a shroud band (not shown) together with a number of other blades 1, and then the protruding part at the tip is inserted. Although the alloy is crushed and fixed, when the vapor deposited particles adhere to the blade surface, the alloy is rapidly cooled and an amorphous film is easily formed. Incidentally, even if a vapor deposition method other than the above-mentioned vacuum vapor deposition method is used, the effect remains the same.
発明の効果
上述したように、この発明は、ブレード1の矢印6の方
向からの水滴を含有した蒸気がアモルファス生成合金被
覆表面に衝突しても該被覆金属は耐腐食性に富んでいる
ので、腐食発生が完全に防止され、しかもブレード母材
の疲労限を低下させることがないから、従来ステライト
薄板の貼付方式に比較して強度設計が楽になって高速化
、長翼化等のタービン高効率化への対応が容易となると
ともに、アモルファス生成合金被覆作業は極めて簡単に
自動化作業を実現させられるので、従来のステライト薄
板貼付作業に比較して大幅な原価低減を行なえるなど、
この発明の産業上の利用価値は極めて多大である。Effects of the Invention As mentioned above, in this invention, even if steam containing water droplets from the direction of the arrow 6 of the blade 1 collides with the surface of the amorphous-forming alloy coating, the coating metal is highly corrosion resistant. Since corrosion is completely prevented and the fatigue limit of the blade base material is not lowered, strength design is easier compared to the conventional method of attaching thin stellite plates, resulting in high efficiency turbines such as higher speeds and longer blades. In addition to making it easier to respond to changes in technology, the amorphous-forming alloy coating work can be automated extremely easily, resulting in significant cost reductions compared to the conventional stellite thin plate pasting work.
The industrial utility value of this invention is extremely large.
第1図は、この発明の実施例を示す斜視図、第2図は、
従来の蒸気タービンのタービンブレードの耐腐食性付与
方式を示す平面図、第3図は、前回のX−X矢視図であ
る。
l・・タービンブレード、7・・アモルファス(ほか7
名)
第2図FIG. 1 is a perspective view showing an embodiment of the invention, and FIG. 2 is a perspective view showing an embodiment of the invention.
FIG. 3 is a plan view showing a conventional method for imparting corrosion resistance to turbine blades of a steam turbine, and is a previous view taken along the line X--X. l...Turbine blade, 7...Amorphous (and 7 others)
Figure 2
Claims (1)
蒸発被覆させることを特徴とする蒸気タービンのタービ
ンブレード。A turbine blade for a steam turbine, characterized in that an amorphous-forming alloy is evaporated and coated on a surface on which water droplets in wet steam collide.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP20059684A JPS6179802A (en) | 1984-09-27 | 1984-09-27 | Turbine blade of steam turbine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP20059684A JPS6179802A (en) | 1984-09-27 | 1984-09-27 | Turbine blade of steam turbine |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS6179802A true JPS6179802A (en) | 1986-04-23 |
Family
ID=16426982
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP20059684A Pending JPS6179802A (en) | 1984-09-27 | 1984-09-27 | Turbine blade of steam turbine |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS6179802A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1217095A1 (en) * | 2000-12-23 | 2002-06-26 | ALSTOM Power N.V. | Protective coating for an article used at high temperatures, particularly turbine components |
US20100329884A1 (en) * | 2009-06-25 | 2010-12-30 | Hitachi, Ltd. | Turbine rotor blade |
-
1984
- 1984-09-27 JP JP20059684A patent/JPS6179802A/en active Pending
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1217095A1 (en) * | 2000-12-23 | 2002-06-26 | ALSTOM Power N.V. | Protective coating for an article used at high temperatures, particularly turbine components |
US20100329884A1 (en) * | 2009-06-25 | 2010-12-30 | Hitachi, Ltd. | Turbine rotor blade |
US8632313B2 (en) * | 2009-06-25 | 2014-01-21 | Hitachi, Ltd. | Turbine rotor blade |
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