JPH04134605U - steam turbine rotor blades - Google Patents

steam turbine rotor blades

Info

Publication number
JPH04134605U
JPH04134605U JP4273691U JP4273691U JPH04134605U JP H04134605 U JPH04134605 U JP H04134605U JP 4273691 U JP4273691 U JP 4273691U JP 4273691 U JP4273691 U JP 4273691U JP H04134605 U JPH04134605 U JP H04134605U
Authority
JP
Japan
Prior art keywords
blade
rotor
steam turbine
blade root
root
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.)
Withdrawn
Application number
JP4273691U
Other languages
Japanese (ja)
Inventor
宏治 大山
Original Assignee
三菱重工業株式会社
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 三菱重工業株式会社 filed Critical 三菱重工業株式会社
Priority to JP4273691U priority Critical patent/JPH04134605U/en
Publication of JPH04134605U publication Critical patent/JPH04134605U/en
Withdrawn legal-status Critical Current

Links

Abstract

(57)【要約】 【目的】 翼根部における損傷が軽減されることを目的
とする。 【構成】 翼根部を介してロータの溝に固定される蒸気
タービンの動翼における翼根部の翼出口腹側の面にレリ
ーフを形成して構成する。
(57) [Summary] [Purpose] The purpose is to reduce damage to the blade root. [Structure] A relief is formed on the ventral surface of the blade outlet of the blade root of a rotor blade of a steam turbine that is fixed to a groove of a rotor via the blade root.

Description

【考案の詳細な説明】[Detailed explanation of the idea]

【0001】0001

【産業上の利用分野】[Industrial application field]

本考案は、火力発電などに適用される蒸気タービンの動翼に関する。 The present invention relates to rotor blades for steam turbines applied to thermal power generation and the like.

【0002】0002

【従来の技術】[Conventional technology]

蒸気タービンの動翼は羽根に作用する遠心力によってクリスマスツリー形、T 字形、ダブテイル形、鋸歯形等の各種形状の翼根部が使い分けられている。図2 は従来の蒸気タービンの動翼の構造説明図である。図において、本動翼はクリス マスツリー形の翼根部1を有しており、この翼根部1を介して図示しないロータ の溝に固定されている。蒸気は矢印dにより示す方向に翼プロフィル部2を流れ る。 The rotor blades of a steam turbine are shaped like a Christmas tree due to centrifugal force acting on the blades. Various types of blade root shapes are used, including letter-shaped, dovetail-shaped, and sawtooth-shaped. Figure 2 1 is a structural explanatory diagram of a rotor blade of a conventional steam turbine. In the figure, the main rotor blade is It has a mass tree-shaped blade root 1, and a rotor (not shown) is connected via this blade root 1. is fixed in the groove. Steam flows through the blade profile 2 in the direction indicated by arrow d. Ru.

【0003】0003

【考案が解決しようとする課題】[Problem that the idea aims to solve]

上記のような従来の蒸気タービンの動翼において、動翼には回転による遠心力 と蒸気による曲げ力が作用し、これらの力は翼根部1を介してロータに伝達され る。このため、翼根部1には静応力とともに周期的に変化する振動応力が発生す る。また、一般に蒸気タービンの動翼は図に示すように翼プロフィル部2が出口 端腹側に向かって弯曲し、その遠心力はプラットフォーム3上の翼プロフィル部 2後縁側に偏心する。この偏心した遠心力はプラットフォーム3上では矢印eに より示すようなモーメントとなり、翼根部1における翼出口腹側の面圧を増大さ せる。そして、この局部的な面圧が過大すると翼根部1の翼出口腹側が損傷する 。 In the rotor blades of conventional steam turbines as described above, the rotor blades are subject to centrifugal force due to rotation. and the bending force caused by the steam acts, and these forces are transmitted to the rotor via the blade root 1. Ru. Therefore, vibration stress that changes periodically along with static stress is generated in the blade root 1. Ru. In general, as shown in the figure, the rotor blades of a steam turbine have a blade profile section 2 at the outlet. The blade is curved toward the ventral side, and its centrifugal force is applied to the wing profile on platform 3. 2 Eccentric to the trailing edge side. This eccentric centrifugal force is caused by arrow e on platform 3. The moment becomes as shown below, increasing the surface pressure on the ventral side of the blade outlet at the blade root 1. let If this local surface pressure becomes excessive, the ventral side of the blade outlet of the blade root 1 will be damaged. .

【0004】0004

【課題を解決するための手段】[Means to solve the problem]

本考案に係る蒸発タービンの動翼は上記課題の解決を目的にしており、翼根部 を介してロータの溝に固定される蒸気タービンの動翼において、上記翼根部の翼 出口腹側の面にレリーフを形成した構成を特徴とする。 The purpose of the rotor blade of the evaporator turbine according to the present invention is to solve the above problems. In steam turbine rotor blades that are fixed to the grooves of the rotor through It is characterized by a relief formed on the ventral side of the outlet.

【0005】[0005]

【作用】[Effect]

即ち、本考案に係る蒸気タービンの動翼においては、翼根部を介してロータの 溝に固定される蒸気タービンの動翼における翼根部の翼出口腹側の面にレリーフ が形成されており、ロータの溝に圧接される動翼の翼根部が外力によって圧縮さ れて弾性変形し翼根部の翼出口腹側の面に局部的に過大な応力が作用するが、レ リーフによりこの局部的に過大な応力が除去されて翼根部全幅に対してほぼ均一 になる。 That is, in the steam turbine rotor blade according to the present invention, the rotor is connected to the rotor through the blade root. Relief on the ventral side of the blade outlet of the blade root of a steam turbine rotor blade that is fixed in a groove. is formed, and the blade root of the rotor blade, which is in pressure contact with the rotor groove, is compressed by external force. The blade is elastically deformed and excessive stress is applied locally to the surface of the blade root on the ventral side of the blade outlet. The leaves remove this locally excessive stress, making it almost uniform over the entire width of the blade root. become.

【0006】[0006]

【実施例】【Example】

図1は本考案の一実施例に係る蒸気タービンの動翼の構造説明図である。図に おいて本実施例に係る蒸気タービンの動翼は火力発電に使用される蒸気タービン の動翼で、図に示すようにクリスマスツリー形の翼根部1を有しており、この翼 根部1を介して図示しないロータの溝に固定されている。蒸気は矢印dにより示 す方向に翼プロフィル部2を流れる。本動翼には回転による遠心力と蒸気による 曲げ力が作用し、これらの力は翼根部1を介してロータに伝達される。このため 、翼根部1には静応力とともに周期的に変化する振動応力が発生する。また、一 般に蒸気タービンの動翼は図に示すように翼プロフィル部2が出口端腹側に向か って弯曲し、その遠心力はプラットフォーム3上の翼プロフィル部2後縁側に偏 心する。この偏心した遠心力はプラットフォーム3上では矢印eで示すようなモ ーメントとなり、翼根部1の翼出口腹側の面Aの面圧を増大させる。この局部的 な面圧が過大となると翼根部1の翼出口腹側が損傷するため、本動翼においては この局部的に面圧が増大する翼根部1の翼出口腹側の面Aを薄く切削して盗み、 過大な面圧を逃がすようにレリーフを形成している。このレリーフが形成される 幅bは翼根部1の全幅Bの1/5以下で、その深さはレリーフを形成しない面C との境界から始まって直線的に増加し、翼根部1の端縁では10/100〜20 /100mmとなっている。 FIG. 1 is a structural explanatory diagram of a rotor blade of a steam turbine according to an embodiment of the present invention. In the figure The rotor blades of the steam turbine according to this embodiment are steam turbines used for thermal power generation. This rotor blade has a Christmas tree-shaped blade root 1 as shown in the figure. It is fixed to a groove of a rotor (not shown) via the root 1. Steam is indicated by arrow d. flow through the blade profile 2 in the direction of the flow. The rotor blades are caused by centrifugal force due to rotation and steam Bending forces act and these forces are transmitted via the blade root 1 to the rotor. For this reason , a periodically changing vibration stress is generated in the blade root portion 1 along with static stress. Also, one Generally speaking, the rotor blades of a steam turbine have a blade profile portion 2 facing toward the ventral side of the outlet end, as shown in the figure. The centrifugal force is biased toward the trailing edge of the blade profile 2 on the platform 3. I care. This eccentric centrifugal force is generated by a motor as shown by arrow e on platform 3. This increases the surface pressure on the surface A of the blade root 1 on the ventral side of the blade outlet. This local If the surface pressure becomes excessive, the ventral side of the blade outlet of the blade root 1 will be damaged, so in this rotor blade, The surface A on the ventral side of the blade outlet of the blade root 1 where the surface pressure locally increases is cut thinly and removed. A relief is formed to release excessive surface pressure. This relief is formed The width b is 1/5 or less of the total width B of the blade root 1, and its depth is the surface C where no relief is formed. It increases linearly starting from the boundary with 10/100 to 20 at the edge of blade root 1. /100mm.

【0007】 このようにして翼根部1の翼出口腹側の面Aにレリーフを形成することにより 、翼根部1の翼出口腹側の面Aに局部的に作用する面圧が逃がされ、過大な応力 が除去されて翼根部1の全幅Bに対してほぼ均一に作用するようになるので、翼 根部1における損傷が軽減されて動翼の寿命が増大する。[0007] By forming a relief on the surface A of the blade outlet ventral side of the blade root 1 in this way, , the surface pressure acting locally on the surface A on the ventral side of the blade outlet of the blade root 1 is released, causing excessive stress. is removed and acts almost uniformly over the entire width B of the blade root 1, so the blade Damage at the root 1 is reduced and the life of the rotor blade is increased.

【0008】[0008]

【考案の効果】[Effect of the idea]

本考案に係る蒸気タービンの動翼は前記のように構成されており、翼根部に作 用する応力が翼根部の全幅に対してほぼ均一になるので、翼根部における損傷が 軽減される。 The rotor blades of the steam turbine according to the present invention are constructed as described above, and the rotor blades are formed at the blade roots. Since the applied stress is almost uniform across the entire width of the blade root, damage to the blade root is minimized. Reduced.

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

【図1】図1は本考案の一実施例に係る蒸気タービンの
動翼の斜視図である。
FIG. 1 is a perspective view of a rotor blade of a steam turbine according to an embodiment of the present invention.

【図2】図2は従来の蒸気タービンの動翼の斜視図であ
る。
FIG. 2 is a perspective view of a rotor blade of a conventional steam turbine.

【符号の説明】[Explanation of symbols]

1 翼根部 2 翼プロフィル部 3 プラットフォーム A 翼根部の翼出口腹側の面 B 翼根部の全幅 b レリーフを形成する幅 C レリーフを形成しない面 1 Wing root 2 Wing profile part 3 Platform A Ventral surface of the blade outlet at the blade root B Total width of wing root b Width forming relief C Surface that does not form relief

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 【請求項1】 翼根部を介してロータの溝に固定される
蒸気タービンの動翼において、上記翼根部の翼出口腹側
の面にレリーフを形成したことを特徴とする蒸気タービ
ンの動翼。
1. A rotor blade for a steam turbine fixed to a groove of a rotor via a blade root, wherein a relief is formed on a surface of the blade root on the ventral side of a blade outlet.
JP4273691U 1991-06-07 1991-06-07 steam turbine rotor blades Withdrawn JPH04134605U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP4273691U JPH04134605U (en) 1991-06-07 1991-06-07 steam turbine rotor blades

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP4273691U JPH04134605U (en) 1991-06-07 1991-06-07 steam turbine rotor blades

Publications (1)

Publication Number Publication Date
JPH04134605U true JPH04134605U (en) 1992-12-15

Family

ID=31923185

Family Applications (1)

Application Number Title Priority Date Filing Date
JP4273691U Withdrawn JPH04134605U (en) 1991-06-07 1991-06-07 steam turbine rotor blades

Country Status (1)

Country Link
JP (1) JPH04134605U (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2008540921A (en) * 2005-05-12 2008-11-20 ゼネラル・エレクトリック・カンパニイ Rotor blade / disc dovetail backcut to reduce stress on rotor blade / disk (7FA + e, 2nd stage)
JP2009536994A (en) * 2006-05-12 2009-10-22 ゼネラル・エレクトリック・カンパニイ Blade / disk dovetail backcut for stress reduction in blade / disk (6FA + e, 2nd stage)
JP2010190199A (en) * 2009-02-20 2010-09-02 Mitsubishi Heavy Ind Ltd Moving blade for axial flow compressor
JP2013164068A (en) * 2012-02-10 2013-08-22 General Electric Co <Ge> Turbine assembly
EP3274561B1 (en) * 2015-05-28 2022-03-09 Siemens Energy Global GmbH & Co. KG Rotor blade for a gas turbine, manufacturing process and post production process

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2008540921A (en) * 2005-05-12 2008-11-20 ゼネラル・エレクトリック・カンパニイ Rotor blade / disc dovetail backcut to reduce stress on rotor blade / disk (7FA + e, 2nd stage)
JP2009536994A (en) * 2006-05-12 2009-10-22 ゼネラル・エレクトリック・カンパニイ Blade / disk dovetail backcut for stress reduction in blade / disk (6FA + e, 2nd stage)
JP2010190199A (en) * 2009-02-20 2010-09-02 Mitsubishi Heavy Ind Ltd Moving blade for axial flow compressor
JP2013164068A (en) * 2012-02-10 2013-08-22 General Electric Co <Ge> Turbine assembly
EP3274561B1 (en) * 2015-05-28 2022-03-09 Siemens Energy Global GmbH & Co. KG Rotor blade for a gas turbine, manufacturing process and post production process

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A300 Application deemed to be withdrawn because no request for examination was validly filed

Free format text: JAPANESE INTERMEDIATE CODE: A300

Effective date: 19950907