JPS62113804A - Steam turbine - Google Patents

Steam turbine

Info

Publication number
JPS62113804A
JPS62113804A JP25405485A JP25405485A JPS62113804A JP S62113804 A JPS62113804 A JP S62113804A JP 25405485 A JP25405485 A JP 25405485A JP 25405485 A JP25405485 A JP 25405485A JP S62113804 A JPS62113804 A JP S62113804A
Authority
JP
Japan
Prior art keywords
wheel
turbine
turbine rotor
steam turbine
rotor 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
Application number
JP25405485A
Other languages
Japanese (ja)
Inventor
Shuichi Inagaki
修一 稲垣
Kiyoshi Imai
潔 今井
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Toshiba Corp
Original Assignee
Toshiba Corp
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Toshiba Corp filed Critical Toshiba Corp
Priority to JP25405485A priority Critical patent/JPS62113804A/en
Publication of JPS62113804A publication Critical patent/JPS62113804A/en
Pending legal-status Critical Current

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  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

PURPOSE:To prevent erosion of a wheel and generation of vibrations, by placing a single or plural layers of metals with intermediate values of erosion potential between those of turbine runners of a titanium alloy and a wheel of a low-grade alloy, at the portion connecting the runners and the wheel. CONSTITUTION:At the periphery of a wheel 1 of a turbine rotor, is formed a turbine runner installing member 1a with recessed portions of plural steps, to which are geared implanting portions 2a of the turbine runners 2. In such a composition, the surfaces in the implanting portion 2a contacting to the runner installing member 1a are fixed by plating in plural layers with pure metals 3 with intermediate erosion potential values between those of the turbine runners 2 and the wheel 1. The order of the erosion potentials is arranged increasing from the wheel 1, the plating metal layers 3a-3c, and the turbine runners 2 in this order. Therefore, generation of erosion of the wheel 1 during the steam turbine operation can be prevented.

Description

【発明の詳細な説明】 (発明の技術分野〕 本発明は、チタン合金製のタービン動翼を有する蒸気タ
ービンに係り、特にタービン動翼とホイールとの間に生
じる電位差に基づく腐蝕を防止するようにした蒸気ター
ビンに関する。
[Detailed Description of the Invention] (Technical Field of the Invention) The present invention relates to a steam turbine having turbine rotor blades made of titanium alloy, and in particular to a steam turbine having turbine rotor blades made of a titanium alloy, and in particular, a method for preventing corrosion due to a potential difference generated between the turbine rotor blades and a wheel. related to steam turbines.

(発明の技術的背景およびその問題点〕最近、蒸気ター
ビンにおいては、その大容吊化に伴いタービンロータに
設けられているホイールの外周に取付けられたタービン
動翼が大型化し、その回転周速度も増加し、動翼に作用
する遠心力も大きくなっている。特に低圧タービンの最
終段ではその遠心力が最大となり、タービン動翼のホイ
ールへの植込部の応力の増大により上記植込部が破壊し
、タービンfiJ+ ’HAが飛散する危険性がある。
(Technical background of the invention and its problems) Recently, in steam turbines, the turbine rotor blades attached to the outer periphery of the wheel provided on the turbine rotor have become larger as the capacity of the steam turbine has increased, and the peripheral speed of rotation has increased. The centrifugal force acting on the rotor blades has also increased.Especially in the final stage of a low-pressure turbine, the centrifugal force is at its maximum, and the stress at the implanted part of the turbine rotor blade in the wheel increases, causing the aforementioned implanted part to There is a risk of destruction and the turbine fiJ+'HA flying off.

そこで、近年大型の蒸気タービンでは、低圧タービンの
最終段タービン動翼に従来の120r基鋼からチタン合
金を採用する傾向にある。すなわち、チタン合金の機械
的性質は12Crli鋼と同等であるのに対し、比重は
12CrW鋼の7.7に対してチタン合金は4.54と
軽く、12Or基鋼の約6割程度であることから、植込
部の応力を低減できるとともにさらに大型化にも対応で
きるようにするため、タービン動翼にチタン合金の採用
が行なわれている。
Therefore, in recent years, there has been a trend in large steam turbines to adopt titanium alloys instead of the conventional 120R base steel for the final stage turbine rotor blades of low-pressure turbines. In other words, the mechanical properties of titanium alloy are equivalent to those of 12Crli steel, while the specific gravity of titanium alloy is lighter at 4.54 compared to 7.7 of 12CrW steel, which is about 60% of that of 12Or base steel. Therefore, titanium alloys are being used for turbine rotor blades in order to reduce the stress at the implanted part and also to accommodate larger sizes.

一方、低圧タービン最終段における蒸気は、タービンの
各段落で熱エネルギーから運動エネルギーに変化するに
したがって圧力および温度が低下するため、通常8〜1
2%に及7S湿り度を有している。しかして、このよう
な環境中ではタービン動翼、ホイールとも濡れた状態に
あり、また水分の電導率も給水処理薬品として添加され
ているアンモニアにより約8μS / cyrと^いた
め、タービン動翼とホイールとの間には電気的な回路が
形成されている。
On the other hand, the pressure and temperature of the steam in the final stage of the low-pressure turbine decrease as it changes from thermal energy to kinetic energy in each stage of the turbine, so it is usually 8 to 1
It has a 7S wetness of up to 2%. However, in such an environment, both the turbine blades and wheels are wet, and the conductivity of water is approximately 8μS/cyr due to the ammonia added as a water treatment chemical, so the turbine blades and wheels are wet. An electrical circuit is formed between them.

ところで、一般的に金属は水中で固有のlS蝕電位を有
しており、チタン合金製タービン翼と低合金製ホイール
の上述の如き環境中でのrrj4M1電位はそれぞれ約
−50mV、−400mV (飽和甘こう電極基準)で
、両者の電位差は約3507FLVである。したがって
、このような腐蝕電位の異なった金属の間で電気的な回
路が形成されると、電位の真な金属すなわちタービン動
翼はカソードとなり、卑な金属すなわちホイールはアノ
ードとなって、両者間には2者のg節電位差に応じた腐
蝕電流が流れ、アノードであるホイールに腐蝕が発生す
る。すなわち、従来のようにタービン動翼とホイールが
ほぼ同等で電位差が100mV以内ではこの影響を無視
できたが、タービン動翼をチタン合金に変えたことによ
り、電位差に基づく新たな腐蝕の問題が生じ、これによ
りタービン動翼とホイールの間に隙間が生じ、蒸気ター
ビンの運転時にアンバランス、ひいては振動発生の原因
となり、長期連続運転に際して信頼性が損なわれる等の
問題がある。
By the way, metals generally have a unique lS corrosion potential in water, and the rrj4M1 potentials of a titanium alloy turbine blade and a low alloy wheel in the above environment are approximately -50 mV and -400 mV (saturated), respectively. The potential difference between the two is approximately 3,507 FLV (based on a sweet tooth electrode). Therefore, when an electrical circuit is formed between metals with different corrosion potentials, the metal with the true potential, that is, the turbine rotor blade, becomes the cathode, and the base metal, that is, the wheel, becomes the anode, and there is no connection between the two. A corrosive current flows in accordance with the g-node potential difference between the two, and corrosion occurs in the wheel, which is the anode. In other words, as in the past, this effect could be ignored if the turbine rotor blades and wheels were almost the same and the potential difference was within 100 mV, but by changing the turbine rotor blades to titanium alloy, a new corrosion problem based on the potential difference has arisen. As a result, a gap is created between the turbine rotor blade and the wheel, causing imbalance during operation of the steam turbine, which in turn causes vibration, resulting in problems such as loss of reliability during long-term continuous operation.

〔発明の目的〕[Purpose of the invention]

本発明はこのような点に鑑み、蒸気タービン運転中にホ
イールの腐蝕が発生することを防止し、振動発生を防止
できるようにした蒸気タービンを得ることを目的とする
In view of these points, it is an object of the present invention to provide a steam turbine that can prevent corrosion of wheels and vibration during operation of the steam turbine.

〔発明の概要〕[Summary of the invention]

本発明は、低合金鋼製のホイールにチタン合金製のター
ビン動翼が植込まれている蒸気タービンにおいて、上記
タービン動翼とホイールとが接している部分に、タービ
ン動翼とホイールが示す腐蝕電位の中間値を示す単層ま
たは複層の金属を介在させたことを特徴とするものであ
って、タービン動翼とホイールとの間の腐蝕電位差を順
次変化させ、両者間の腐蝕電流を極小ならしめるように
したものである。
The present invention provides a steam turbine in which a titanium alloy turbine blade is embedded in a low-alloy steel wheel, and the corrosion caused by the turbine blade and the wheel is prevented at a portion where the turbine blade and the wheel are in contact with each other. It is characterized by interposing a single layer or multiple layers of metal that exhibit an intermediate potential value, and it sequentially changes the corrosion potential difference between the turbine rotor blade and the wheel, minimizing the corrosion current between them. It was designed to help you get used to it.

〔発明の実施例〕[Embodiments of the invention]

以下、第1図を秦照して本発明の実施例について説明す
る。
Hereinafter, embodiments of the present invention will be described with reference to FIG.

第1図において、符号1はタービンロータにおけるホイ
ールであって、そのホイール1の外周部には複数段の凹
部を有するタービン動翼取付部1aが形成されており、
そのタービン動翼取付部1aに、タービン動翼2の植込
部2aが係合装着されている。
In FIG. 1, reference numeral 1 denotes a wheel in a turbine rotor, and a turbine rotor blade mounting portion 1a having multiple stages of recesses is formed on the outer circumference of the wheel 1.
An implanted portion 2a of a turbine rotor blade 2 is engaged with and attached to the turbine rotor blade attachment portion 1a.

ところで、上記タービンホイール2の植込部2aにはホ
イール1のタービン動翼取付部1aと接する面に、ター
ビン動翼2およびホイール1の腐蝕電位の中間に相当す
る腐蝕電位を右する純金属3が複数層にわたってメッキ
により層着されている。
By the way, in the implanted part 2a of the turbine wheel 2, a pure metal 3 is provided on the surface in contact with the turbine rotor blade attachment part 1a of the wheel 1, which has a corrosion potential corresponding to the middle of the corrosion potential of the turbine rotor blade 2 and the wheel 1. is layered by plating over multiple layers.

そして、各部の腐蝕電位が、タービンホイール1、第1
のメッキ金屈層3a1第2のメッキ金属層3b、第3の
メッキ金属)M2C,タービン動翼2の順に順次負とな
るように構成されている。
Then, the corrosion potential of each part of the turbine wheel 1,
The plating metal layer 3a1, the second plating metal layer 3b, the third plating metal) M2C, and the turbine rotor blade 2 are configured to have negative values in this order.

しかして、タービン運転中に蒸気中の水分は第1のメッ
キ金属層3aとタービンホイール1との間隙に浸入し、
ここで腐蝕電池を構成するが、前記構成によって互いに
接する部分間の腐蝕電位差が小さいため、使用中実質的
に問題となるような腐蝕反応を生ずるようなことはない
。また蒸気中の水分がタービン動翼2と第3のメッキ金
属層3Cとの間に浸入することによって腐蝕電池を構成
しても、前記ホイールと第1のメッキ金属層3aとの間
に形成される腐蝕電池と同様に腐蝕電位差が小さく、さ
らにこのような現象が生じる確率は、ホイール1と第1
のメッキ金属層3a間に腐蝕電池が形成される確率に比
較して甚しく小であり、タービンの運転に支障を来すよ
うな腐蝕反応が生ずるようなことはない。
Therefore, during turbine operation, moisture in the steam enters the gap between the first plated metal layer 3a and the turbine wheel 1,
Although a corrosion battery is constructed here, because the corrosion potential difference between the parts that are in contact with each other is small due to the above-mentioned construction, no corrosion reaction that would cause a problem will occur during use. Furthermore, even if moisture in the steam infiltrates between the turbine rotor blade 2 and the third plated metal layer 3C to form a corrosion cell, no moisture is formed between the wheel and the first plated metal layer 3a. Similar to a corrosion battery, the corrosion potential difference is small, and the probability that such a phenomenon will occur is
The probability of a corrosion battery being formed between the plated metal layers 3a is extremely small compared to the probability that a corrosion cell will be formed between the plated metal layers 3a, and there is no possibility that a corrosion reaction that would impede the operation of the turbine will occur.

なお、上記実施例においてはタービン動翼2の植込部2
aの表面にメッキ層を設けたものを示したが、ホイール
側にメッキ層を設けてもよく、また複数層でなく単層に
してもよい。
In addition, in the above embodiment, the implanted portion 2 of the turbine rotor blade 2
Although a plated layer is provided on the surface of a, a plated layer may be provided on the wheel side, or a single layer may be provided instead of multiple layers.

さらに、タービン動翼の植込部2aおよびホイールの互
いに接する面のいずれか一方に、タービン動翼とホイー
ルが示す腐蝕電位の中間値、約−270mV、−200
mV、−130mVを示す合金として、Ni10%、C
u90%の合金、Ni30%、Cu70%の合金、およ
びNi90%、Cu10%の合金を順次コーティングし
ても同様の効果を得ることができる。
Further, on one of the mutually contacting surfaces of the implanted part 2a of the turbine rotor blade and the wheel, the intermediate value of the corrosion potential exhibited by the turbine rotor blade and the wheel is approximately -270 mV, -200 mV.
As an alloy showing mV, -130mV, Ni10%, C
A similar effect can be obtained by sequentially coating an alloy of 90% U, 30% Ni and 70% Cu, and an alloy of 90% Ni and 10% Cu.

〔発明の効果〕〔Effect of the invention〕

以上説明したように、本発明においては腐蝕電位差の大
きいチタン合金製のタービン動翼と低合金製のホイール
の間に、両者の中間電位を示す金属層を介在させたので
、蒸気タービンの運転中にホイールの腐蝕が発生するこ
とを防止することができ、振動発生によるプラント停止
もなく、発電プラントを高効率で運転させることができ
る等の効果を奏する。
As explained above, in the present invention, a metal layer exhibiting an intermediate potential is interposed between the titanium alloy turbine rotor blade, which has a large corrosion potential difference, and the low alloy wheel. It is possible to prevent corrosion of the wheels, and there is no need to stop the plant due to vibration, and the power generation plant can be operated with high efficiency.

【図面の簡単な説明】[Brief explanation of drawings]

第1図は本発明の蒸気タービンの正面部分図、第2図は
第1図のA矢印部の拡大図である。 1・・・ホイール、1a・・・タービン動翼取付部、2
・・・タービン動翼、2a・・・植込部、3a、3b。 3C・・・メッキ金属層。 出願人代理人  Fi、   藤  −雄第1図 第2図
FIG. 1 is a partial front view of the steam turbine of the present invention, and FIG. 2 is an enlarged view of the portion indicated by arrow A in FIG. 1...Wheel, 1a...Turbine rotor blade attachment part, 2
...Turbine rotor blade, 2a... Implanted part, 3a, 3b. 3C...Plated metal layer. Applicant's Representative Fi, Yu Fuji Figure 1 Figure 2

Claims (1)

【特許請求の範囲】 1、低合金鋼製のホイールにチタン合金製のタービン動
翼が植め込まれている蒸気タービンにおいて、上記ター
ビン動翼とホイールとが接している部分に、タービン動
翼とホイールが示す腐蝕電位の中間値を示す単層または
複層の金属を介在させたことを特徴とする、蒸気タービ
ン。 2、上記金属はタービン動翼およびホイールのいずれか
一方にメッキされてい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。 3、上記金属はタービン動翼およびホイールのいずれか
一方にコーティングされてい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。 4、金属は純金属であることを特徴とする特許請求の範
囲第2項または第3項記載の蒸気タービン。 5、金属は合金であることを特徴とする、特許請求の範
囲第2項または第3項記載の蒸気タービン。 6、合金はNi−Cu系合金であることを特徴とする、
特許請求の範囲第5項記載の蒸気タービン。 7、金属の層は、タービンホイール側からタービン動翼
側に順次腐蝕電位が負となるように構成されていること
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。
[Claims] 1. In a steam turbine in which a titanium alloy turbine rotor blade is embedded in a low alloy steel wheel, a turbine rotor blade is provided at a portion where the turbine rotor blade and the wheel are in contact with each other. A steam turbine characterized in that a single layer or multiple layers of metal exhibiting an intermediate value of corrosion potential are interposed between the wheels and the wheels. 2. The steam turbine according to claim 1, wherein the metal is plated on either one of the turbine rotor blades and the wheel. 3. The steam turbine according to claim 1, wherein the metal is coated on either one of the turbine rotor blades and the wheel. 4. The steam turbine according to claim 2 or 3, wherein the metal is a pure metal. 5. The steam turbine according to claim 2 or 3, wherein the metal is an alloy. 6. The alloy is a Ni-Cu alloy,
A steam turbine according to claim 5. 7. The steam turbine according to claim 1, wherein the metal layer is configured such that the corrosion potential becomes negative sequentially from the turbine wheel side to the turbine rotor blade side.
JP25405485A 1985-11-13 1985-11-13 Steam turbine Pending JPS62113804A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP25405485A JPS62113804A (en) 1985-11-13 1985-11-13 Steam turbine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP25405485A JPS62113804A (en) 1985-11-13 1985-11-13 Steam turbine

Publications (1)

Publication Number Publication Date
JPS62113804A true JPS62113804A (en) 1987-05-25

Family

ID=17259588

Family Applications (1)

Application Number Title Priority Date Filing Date
JP25405485A Pending JPS62113804A (en) 1985-11-13 1985-11-13 Steam turbine

Country Status (1)

Country Link
JP (1) JPS62113804A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5024582A (en) * 1990-08-14 1991-06-18 Westinghouse Electric Corp. Steam turbine rotor having graded weldments
US5240375A (en) * 1992-01-10 1993-08-31 General Electric Company Wear protection system for turbine engine rotor and blade
US5704765A (en) * 1995-08-07 1998-01-06 Westinghouse Electric Corporation High chromium content welding material to improve resistance of corrosion method and device
US5746579A (en) * 1996-12-27 1998-05-05 Westinghouse Electric Corporation Stress corrosion resistant rims and discs for steam turbine rotors device and method
JP2009019630A (en) * 2007-07-13 2009-01-29 Snecma Rotor assembly of turbo machine
JP2009019629A (en) * 2007-07-13 2009-01-29 Snecma Shim for blade of turbo machine

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5024582A (en) * 1990-08-14 1991-06-18 Westinghouse Electric Corp. Steam turbine rotor having graded weldments
DE4126443C2 (en) * 1990-08-14 1999-12-09 Westinghouse Electric Corp Turbine impeller layered welds
US5240375A (en) * 1992-01-10 1993-08-31 General Electric Company Wear protection system for turbine engine rotor and blade
US5704765A (en) * 1995-08-07 1998-01-06 Westinghouse Electric Corporation High chromium content welding material to improve resistance of corrosion method and device
US5746579A (en) * 1996-12-27 1998-05-05 Westinghouse Electric Corporation Stress corrosion resistant rims and discs for steam turbine rotors device and method
JP2009019630A (en) * 2007-07-13 2009-01-29 Snecma Rotor assembly of turbo machine
JP2009019629A (en) * 2007-07-13 2009-01-29 Snecma Shim for blade of turbo machine

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