JP2000282803A - Moving blade castings for steam turbine - Google Patents
Moving blade castings for steam turbineInfo
- Publication number
- JP2000282803A JP2000282803A JP11093616A JP9361699A JP2000282803A JP 2000282803 A JP2000282803 A JP 2000282803A JP 11093616 A JP11093616 A JP 11093616A JP 9361699 A JP9361699 A JP 9361699A JP 2000282803 A JP2000282803 A JP 2000282803A
- Authority
- JP
- Japan
- Prior art keywords
- casting
- steam turbine
- moving blade
- water pressure
- static water
- 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
Landscapes
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Description
【0001】[0001]
【発明が属する技術分野】本発明は、蒸気タービン用動
翼に関するものである。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a moving blade for a steam turbine.
【0002】[0002]
【従来の技術】一般的に蒸気タービン用動翼には長時間
蒸気に晒されるため、酸化腐食しにくいステンレス鋼ま
たは耐熱鋼が用いられている。また、動翼は回転体であ
るため高速回転に耐え得る強度、更に回転始動時および
停止時の衝撃に耐え得る衝撃特性が必要とされる。その
ため従来は鍛造材を機械加工して成形されるのが一般的
であった。2. Description of the Related Art Generally, stainless steel or heat-resistant steel, which is hardly oxidized and corroded, is used for a rotor blade for a steam turbine because it is exposed to steam for a long time. Further, since the rotor blade is a rotating body, it is required to have a strength capable of withstanding high-speed rotation and an impact characteristic capable of withstanding the impact at the start and stop of rotation. For this reason, conventionally, forging materials have generally been formed by machining.
【0003】[0003]
【発明が解決しようとする課題】従来蒸気タービン用動
翼として必要な特性を得るためには前述のように鍛造材
を用いるのが一般的であるが、これを機械加工により成
形した場合は加工工数が非常に大きく、材料歩留まりが
悪いためコスト高であるという問題点がある。また、型
打鍛造を使用して成形した場合は型抜けの可否により成
形できる形状が制限されるという問題点もある。Conventionally, in order to obtain the characteristics required for a moving blade for a steam turbine, it is common to use a forged material as described above. There is a problem that the man-hour is very large and the material yield is low, so that the cost is high. In addition, when molding is performed using stamping forging, there is also a problem that the shape that can be molded is limited depending on whether or not the mold is removed.
【0004】精密鋳造による成形は機械加工工数が鍛造
品に比べ大幅に削減されるため安価に生産できる上、形
状に関する制限がほとんど無いといった点で有利であ
る。しかしながら、ステンレス鋼または耐熱鋼鋳物を鋳
造ままもしくは従来の熱処理のみを実施した材料では、
動翼として必要とされる機械的特性を満たすことができ
ないという問題点がある。鋳物であってもNi基などの
超耐熱合金であれば必要な特性を得ることは可能である
が、これらの合金は材料コストが高いため、やはり実用
的ではない。本発明の目的は、蒸気タービン用動翼に関
して上記のようなコスト高および形状制限の問題を解決
し、さらに動翼としての機械的特性を有する蒸気タービ
ン用動翼を提供することである。[0004] The molding by precision casting is advantageous in that the number of machining steps is significantly reduced as compared with a forged product, so that it can be produced at low cost and that there is almost no restriction on the shape. However, in the case of a stainless steel or heat-resistant steel casting as-cast or a material subjected to only conventional heat treatment,
There is a problem that the mechanical properties required for the rotor blade cannot be satisfied. Even if it is a casting, it is possible to obtain the required characteristics as long as it is a super heat-resistant alloy such as Ni-base, but these alloys are still not practical because of high material cost. SUMMARY OF THE INVENTION An object of the present invention is to solve the above-described problems of high cost and shape limitation with respect to a moving blade for a steam turbine, and to further provide a moving blade for a steam turbine having mechanical characteristics as a moving blade.
【0005】[0005]
【課題を解決するための手段】本発明者は、蒸気タービ
ン用動翼の成形におけるコスト高の問題を検討し、ステ
ンレス鋼または耐熱鋼鋳物に熱間静水圧処理を行なうこ
とで鋳物の機械的特性を大きく改善できることを見出し
本発明に到達した。SUMMARY OF THE INVENTION The present inventor has studied the problem of high cost in forming a moving blade for a steam turbine, and has conducted a hot isostatic pressure treatment on a stainless steel or heat-resistant steel casting to thereby obtain a mechanical strength of the casting. The inventors have found that the characteristics can be greatly improved, and have reached the present invention.
【0006】すなわち、本発明はステンレス鋼または耐
熱鋼において、成形後に熱間静水圧処理が施されている
ことを特徴とする蒸気タービン用動翼鋳物であり、さら
に、前記ステンレス鋼または耐熱鋼がマルテンサイト系
であること、および精密鋳造により成形され、成形後に
熱間静水圧処理が施されていることを特徴とする蒸気タ
ービン用動翼鋳物である。[0006] That is, the present invention is a moving blade casting for a steam turbine, characterized in that a hot isostatic pressure treatment is performed after forming the stainless steel or the heat-resistant steel. A moving blade casting for a steam turbine, which is a martensite system, is formed by precision casting, and is subjected to a hot isostatic pressure treatment after the forming.
【0007】[0007]
【発明の実施の形態】上述したように、本発明の重要な
特徴はステンレス鋼または耐熱鋼で鋳造成形した蒸気タ
ービン用動翼に熱間静水圧処理を施し、その後に必要に
応じて適当な熱処理を行ない、該動翼の機械的特性を鍛
造材と同等にまで改善したことにある。DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS As described above, an important feature of the present invention is that a steam turbine rotor blade cast and formed of stainless steel or heat-resistant steel is subjected to hot isostatic pressure treatment, and then to a suitable Heat treatment is performed to improve the mechanical properties of the blade to the same level as that of a forged material.
【0008】鋳造材の場合、鋳造時の溶湯の乱流による
ガスの巻き込みや、溶湯と鋳型材との反応から生じるミ
クロポロシティや、凝固収縮時に生じるミクロシュリン
ケージが鋳物内部に存在する場合がある。このような鋳
造欠陥が存在する材料に外部から応力が発生した場合、
これらの欠陥が起点となって比較的低い応力で破断する
ことが多い。鍛造材の場合は外部から材料に圧力を加え
ることによりこれらの欠陥は潰れてしまうため、一般的
には鋳造材よりも高い強度を示す。つまり、鋳造材にお
いて鍛造材に近い特性を得るためには前述のようなミク
ロポロシティやミクロシュリンケージを何らかの方法で
除去することが必要となる。In the case of a cast material, gas entrainment due to turbulence of the molten metal during casting, microporosity resulting from the reaction between the molten metal and the mold material, and microshrinkage generated during solidification shrinkage may be present inside the casting. . When stress is applied to the material having such casting defects from outside,
In many cases, these defects serve as starting points and break at relatively low stress. In the case of a forged material, these defects are crushed when pressure is applied to the material from the outside, and thus generally show higher strength than a cast material. That is, in order to obtain characteristics similar to those of a forged material in a cast material, it is necessary to remove the above-described microporosity and microshrinkage by some method.
【0009】鋳造時の溶湯の乱流を防ぐ方法としては真
空中で金属材料を溶解および注湯する真空鋳造等が有効
である。また、溶湯と鋳型との反応を防ぐには、熱力学
的に安定しているジルコニア、イットリア等の耐火物を
鋳型材に使用する方法が挙げられる。しかしながら、こ
れらの鋳造方法および耐火物は作業費、材料費が非常に
高価であり実用的ではない。その他、金型鋳造により溶
湯との反応は防ぐことは可能であるが、金型鋳造では金
型の耐久性に問題があり、これも実用的ではない。As a method for preventing the turbulence of the molten metal during casting, vacuum casting or the like in which a metal material is melted and poured in a vacuum is effective. Further, in order to prevent the reaction between the molten metal and the mold, there is a method in which a refractory such as zirconia or yttria which is thermodynamically stable is used for the mold material. However, these casting methods and refractories are not practical because of extremely high working and material costs. In addition, it is possible to prevent the reaction with the molten metal by die casting, but there is a problem in the durability of the die in die casting, which is not practical.
【0010】以上のことから、鋳造欠陥を完全に防ぐの
は実質的に非常に困難であり、本発明者は鋳造欠陥の発
生を防ぐのではなく、発生した欠陥を物理的に除去する
方法を検討した。その結果、高温中で鋳物材料に外部か
ら均等に圧力をかけて欠陥を押しつぶす熱間静水圧処理
が有効であることを見出した。From the above, it is practically very difficult to completely prevent casting defects, and the present inventor has proposed a method of physically removing the generated defects instead of preventing the occurrence of the defects. investigated. As a result, it has been found that hot isostatic pressure treatment in which a pressure is uniformly applied to the casting material from outside at a high temperature to crush the defects is effective.
【0011】熱間静水圧処理では内部欠陥をなるべく低
い圧力で潰しやすくするため、900℃以上の高温中で
軟化した材料に応力を負荷することが望ましい。また、
負荷圧力を静水圧としたのは鋳物の変形を最小限に抑え
るためである。さらに圧力負荷に使用する媒体は材料の
高温酸化腐食を抑えるためAr等の不活性ガスを用いる
ことが望ましい。In the hot isostatic pressure treatment, it is desirable to apply a stress to a material softened at a high temperature of 900 ° C. or higher in order to easily crush internal defects at a pressure as low as possible. Also,
The load pressure was set to be a hydrostatic pressure in order to minimize the deformation of the casting. Further, it is desirable to use an inert gas such as Ar for the medium used for the pressure load in order to suppress high-temperature oxidation corrosion of the material.
【0012】蒸気タービン用動翼は通常、翼を一枚ずつ
成形し、リング状に組み立てて使用するのが一般的であ
る。このため、使用されるステンレス鋼または耐熱鋼は
熱膨張率の大きいオーステナイト系よりも、熱膨張率が
小さいフェライト系、または熱膨張率が小さくさらに強
度的にも優れているマルテンサイト系の材料が多く用い
られている。マルテンサイト系の材料は通常焼入れ、焼
戻しの熱処理を行なってから使用されるが、熱間静水圧
処理を行なった材料もそれだけでは動翼として必要な特
性が得られないことがあるため、その場合は熱間静水圧
処理後に必要に応じて適切な焼入れ、焼戻し処理を行な
い、必要とする特性を得なければならない。本発明は、
マルテンサイト系材料で実施したが、フェライト系材料
としてもよい。Generally, a moving blade for a steam turbine is generally used by forming the blades one by one and assembling them into a ring shape. For this reason, the stainless steel or heat-resistant steel used is a ferrite-based material having a small coefficient of thermal expansion or a martensitic-based material having a small coefficient of thermal expansion and excellent strength compared to an austenitic material having a large coefficient of thermal expansion. Many are used. Martensitic materials are usually used after heat treatment such as quenching and tempering.However, materials that have been subjected to hot isostatic pressure treatment alone may not be able to obtain the characteristics required as a moving blade. After the hot isostatic pressure treatment, appropriate quenching and tempering treatment must be performed as necessary to obtain the required characteristics. The present invention
Although a martensite-based material was used, a ferrite-based material may be used.
【0013】[0013]
【実施例】実施例として従来から蒸気タービン用動翼に
用いられているJIS G4311で規定するマルテン
サイト系耐熱鋼SUH600およびJIS G4303
で規定するマルテンサイト系ステンレス鋼SUS403
の2種類の材料の鋳造材の引張特性および衝撃特性を熱
間静水圧処理を行なったものと行なっていないものにつ
いて鍛造材と比較した。EXAMPLES As examples, martensitic heat-resistant steels SUH600 and JIS G4303 specified in JIS G4311, which have been conventionally used for moving blades for steam turbines.
Martensitic stainless steel SUS403 specified in
The tensile properties and the impact properties of the two types of cast materials were compared with those of the forged material after the hot isostatic pressure treatment and without the hot isostatic pressure treatment.
【0014】鋳造材はシリカ、アルミナ、ジルコニアを
主成分とする耐火物で直径11mm×長さ90mmおよ
び11mm×11mm×55mmの空孔部を数箇所成形
した鋳型に、大気中で溶解した溶湯を鋳造し、耐火物を
除去した後に押し湯部から切り離して試験片素材を採取
した。採取した素材の半数は1180℃のAr雰囲気炉
内で1000気圧の静水圧を負荷する熱間静水圧処理を
施した。その後、SUH600はJIS G4311、
SUS403はJIS G4303で規定する焼入れ、
焼戻しの熱処理を行なった。熱処理が完了した素材は、
機械加工により平行部の直径6.35mm、標点距離3
5.0mmの引張試験片、および10mm×10mm×
55mmにSUH600は深さ2mmのU形ノッチ、S
US403は深さ2mmのV形ノッチを付したシャルピ
ー衝撃試験片に加工し、それぞれ常温で引張試験および
シャルピー衝撃試験を行なった。The casting material is a refractory containing silica, alumina, and zirconia as main components. A molten metal melted in the air is cast into a mold in which holes of 11 mm × 90 mm and 11 mm × 11 mm × 55 mm are formed at several places. After casting and removing the refractory, the test piece material was cut off from the riser. Half of the collected materials were subjected to a hot isostatic pressure treatment of applying a hydrostatic pressure of 1000 atm in an Ar atmosphere furnace at 1180 ° C. After that, SUH600 became JIS G4311,
SUS403 is quenching specified in JIS G4303,
Tempering heat treatment was performed. The material after the heat treatment is
6.35mm diameter of parallel part by machining, gauge length 3
5.0 mm tensile test specimen, and 10 mm x 10 mm x
SUH600 is a U-shaped notch with a depth of 2mm to 55mm, S
US403 was processed into a Charpy impact test specimen having a V-shaped notch having a depth of 2 mm, and subjected to a tensile test and a Charpy impact test at room temperature.
【0015】鍛造材は溶製した10kgのマスターイン
ゴットを30mm角の棒材になるように鍛伸した後、疵
取し、SUH600はJIS G4311、SUS40
3はJIS G4303で規定する熱処理を行ない、鋳
造材の場合と同形状の引張試験片およびシャルピー衝撃
試験片になるよう切り出し、機械加工により試験片を作
製した。試験片は鋳造材と同様、常温で引張試験および
シャルピー衝撃試験を行なった。The forged material was prepared by forging and elongating a melted 10 kg master ingot into a 30 mm square bar and then removing the flaws. SUH600 was JIS G4311, SUS40.
Sample No. 3 was subjected to a heat treatment specified in JIS G4303, cut out into a tensile test piece and a Charpy impact test piece having the same shape as that of the cast material, and manufactured a test piece by machining. The test specimen was subjected to a tensile test and a Charpy impact test at room temperature in the same manner as the cast material.
【0016】[0016]
【表1】 [Table 1]
【0017】[0017]
【表2】 [Table 2]
【0018】表1は常温引張試験の結果をまとめたもの
である。材質がSUH600,SUS403ともに熱間
静水圧処理を行なうことにより耐力、引張強さ、伸びが
向上し、鍛造材とほぼ同等の値が得られた。また、表2
は常温シャルピー衝撃試験の結果をまとめたものであ
り、シャルピー衝撃値も材質SUH600,SUS40
3ともに熱間静水圧処理を行なうことにより向上し、鍛
造材に匹敵する値を示した。更に熱間静水圧処理を行な
った材料は未処理のものに比べて値のばらつきが小さく
なっている。Table 1 summarizes the results of the room temperature tensile test. For both materials SUH600 and SUS403, the proof stress, tensile strength and elongation were improved by performing the hot isostatic pressure treatment, and values almost equivalent to those of the forged material were obtained. Table 2
Is a summary of the results of the room temperature Charpy impact test, and the Charpy impact value is also set for materials SUH600 and SUS40.
All of the samples No. 3 were improved by performing the hot isostatic pressure treatment, and showed values comparable to those of forged materials. Further, the material subjected to the hot isostatic pressure treatment has a smaller value variation than the untreated material.
【0019】[0019]
【発明の効果】本発明によれば鋳造材に熱間静水圧処理
を施すことにより蒸気タービン用動翼に必要な引張特性
および衝撃特性を鍛造材並みに飛躍的に改善することが
でき、蒸気タービン用動翼鋳物の実用化にとって欠くこ
とのできない技術となる。According to the present invention, by subjecting a cast material to hot isostatic pressure treatment, the tensile properties and impact properties required for a moving blade for a steam turbine can be remarkably improved to the level of a forged material. This is an indispensable technology for practical use of turbine bucket castings.
Claims (3)
形後に熱間静水圧処理が施されていることを特徴とする
蒸気タービン用動翼鋳物。1. A moving blade casting for a steam turbine, wherein a stainless steel or heat-resistant steel is subjected to hot isostatic pressure treatment after forming.
イト系であることを特徴とする請求項1に記載の蒸気タ
ービン用動翼鋳物。2. The moving blade casting for a steam turbine according to claim 1, wherein the stainless steel or the heat-resistant steel is martensitic.
よって成形されることを特徴とする請求項1および請求
項2に記載の蒸気タービン用動翼鋳物。3. The bucket casting for a steam turbine according to claim 1, wherein the bucket casting for a steam turbine is formed by a precision casting method.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP11093616A JP2000282803A (en) | 1999-03-31 | 1999-03-31 | Moving blade castings for steam turbine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP11093616A JP2000282803A (en) | 1999-03-31 | 1999-03-31 | Moving blade castings for steam turbine |
Publications (1)
Publication Number | Publication Date |
---|---|
JP2000282803A true JP2000282803A (en) | 2000-10-10 |
Family
ID=14087266
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP11093616A Pending JP2000282803A (en) | 1999-03-31 | 1999-03-31 | Moving blade castings for steam turbine |
Country Status (1)
Country | Link |
---|---|
JP (1) | JP2000282803A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2011522121A (en) * | 2008-05-29 | 2011-07-28 | インデクスター アクチボラゲット | Semi-finished products and methods |
JP2017106076A (en) * | 2015-12-10 | 2017-06-15 | 山陽特殊製鋼株式会社 | Manufacturing method of steel for machine component excellent in rolling motion fatigue life |
JP2017106077A (en) * | 2015-12-10 | 2017-06-15 | 山陽特殊製鋼株式会社 | Manufacturing method of steel for machine component excellent in rolling motion fatigue life |
-
1999
- 1999-03-31 JP JP11093616A patent/JP2000282803A/en active Pending
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2011522121A (en) * | 2008-05-29 | 2011-07-28 | インデクスター アクチボラゲット | Semi-finished products and methods |
JP2017106076A (en) * | 2015-12-10 | 2017-06-15 | 山陽特殊製鋼株式会社 | Manufacturing method of steel for machine component excellent in rolling motion fatigue life |
JP2017106077A (en) * | 2015-12-10 | 2017-06-15 | 山陽特殊製鋼株式会社 | Manufacturing method of steel for machine component excellent in rolling motion fatigue life |
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