JP2854722B2 - Steam turbine blade - Google Patents
Steam turbine bladeInfo
- Publication number
- JP2854722B2 JP2854722B2 JP3107873A JP10787391A JP2854722B2 JP 2854722 B2 JP2854722 B2 JP 2854722B2 JP 3107873 A JP3107873 A JP 3107873A JP 10787391 A JP10787391 A JP 10787391A JP 2854722 B2 JP2854722 B2 JP 2854722B2
- Authority
- JP
- Japan
- Prior art keywords
- blade
- shroud
- blade root
- steam turbine
- moving
- 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.)
- Expired - Fee Related
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
- F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
- F01D5/225—Blade-to-blade connections, e.g. for damping vibrations by shrouding
-
- 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
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
- F01D5/3023—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses
- F01D5/303—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses in a circumferential slot
-
- 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
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
- F01D5/3053—Fixing blades to rotors; Blade roots ; Blade spacers by means of pins
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Description
[発明の目的] [Object of the invention]
【0001】[0001]
【産業上の利用分野】本発明は蒸気タービンに係わり、
特に一体成型シュラウドを有する蒸気タービン動翼に関
する。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a steam turbine,
More particularly, it relates to a steam turbine blade having an integrally formed shroud.
【0002】[0002]
【従来の技術】従来の蒸気タービンは先端に一体に成型
されたシュラウドを持つ動翼を使用してきた。例えば、
図3(a)及び(b)に示す動翼は、翼根部12,翼部
13およびシュラウド14が一体成型されており、翼車
11と嵌合し固定されている。また図3(c)および
(d)に示すように、翼根部12とシュラウド14の円
周方向端面を、軸方向に対して同じ方向に傾斜させ、翼
根部12およびシュラウド14の双方の傾斜面16,1
7を隣接する動翼の相対する傾斜面と面圧8をもたせて
組立てる。さらに図4(a)及び(b)に示す他の動翼
は、翼根部12,翼部13およびシュラウド14が一体
成型されているが、翼車11とは結合ピン19により一
体に結合し固定されている。この動翼では図4(c)お
よび(d)に示すように、シュラウド14の一方の傾斜
面17に隣接するシュラウド14とは面圧8をもたせて
組立てる。そして、いずれの場合も、動翼を全周連続さ
せることにより動翼振動を抑制することを目的としてい
る。2. Description of the Related Art Conventional steam turbines have used blades having a shroud integrally molded at the tip. For example,
In the moving blade shown in FIGS. 3A and 3B, the blade root 12, the blade 13, and the shroud 14 are integrally formed, and are fitted and fixed to the impeller 11. Further, as shown in FIGS. 3C and 3D, the circumferential end faces of the blade root 12 and the shroud 14 are inclined in the same direction with respect to the axial direction, and the inclined surfaces of both the blade root 12 and the shroud 14 are formed. 16,1
7 is assembled with the opposing inclined surfaces of the adjacent moving blades and the surface pressure 8. 4 (a) and 4 (b), the blade root 12, the blade 13 and the shroud 14 are integrally formed, but are integrally connected to the impeller 11 by a connecting pin 19 and fixed. Have been. As shown in FIGS. 4C and 4D, the blade is assembled with the shroud 14 adjacent to one inclined surface 17 of the shroud 14 with a surface pressure 8. In any case, the object is to suppress the blade vibration by making the blade continuous all around.
【0003】[0003]
【発明が解決しようとする課題】ところで、図3(a)
及び(b)に示す動翼構造においては、同図(c)およ
び(d)に示すように、傾斜面17および傾斜面16に
それぞれ付与された面圧8により動翼を回転させる回転
モーメント9および10がそれぞれシュラウド14及び
翼根部12に発生するが、翼根部12と翼車11との接
触面18によりこの回転モーメント9および10を支持
している。また図4(a)及び(b)に示す動翼構造に
おいては、同図(c)および(d)に示すように傾斜面
17に付与された面圧8により動翼を回転させる回転モ
ーメント9が発生するが、翼車11との結合ピン19に
よりこの回転モーメント9を支持している。従って、こ
のような構造の動翼においては、シュラウド14と翼車
11との接触面18または翼根部12と翼車11を結合
する結合ピン19に付加的な過大な力が作用し、動翼変
形の発生や強度低下を引起こすという問題があった。FIG. 3 (a)
In the moving blade structure shown in FIGS. 1 and 2B, as shown in FIGS. 1C and 1D, a rotating moment 9 for rotating the moving blade by the surface pressure 8 applied to the inclined surfaces 17 and 16 respectively. And 10 are generated on the shroud 14 and the blade root 12, respectively, and are supported by the contact surfaces 18 between the blade root 12 and the impeller 11. In the moving blade structure shown in FIGS. 4A and 4B, as shown in FIGS. 4C and 4D, a rotational moment 9 for rotating the moving blade by the surface pressure 8 applied to the inclined surface 17 is used. Is generated, but the rotational moment 9 is supported by the connecting pin 19 with the impeller 11. Therefore, in the moving blade having such a structure, an excessively large additional force acts on the contact surface 18 between the shroud 14 and the impeller 11 or the connecting pin 19 connecting the blade root 12 and the impeller 11, and There is a problem that deformation occurs and strength is reduced.
【0004】本発明は上記事情に鑑みてなされたもの
で、その目的は動翼を回転させる回転モーメントを解消
し、翼車やピンに付加的な力が作用せずかつ強度低下の
ない一体成型されたシュラウドを持つ蒸気タービン動翼
を提供することにある。 [発明の構成]The present invention has been made in view of the above circumstances, and an object of the present invention is to eliminate a rotational moment for rotating a moving blade, and to integrally mold an impeller and a pin without applying an additional force and without reducing strength. To provide a steam turbine blade having a shroud. [Configuration of the Invention]
【0005】[0005]
【課題を解決するための手段】上記目的を達成するため
に、本発明は先端に動翼と一体に成型されたシュラウド
を有する蒸気タービン動翼において、前記動翼の翼根部
およびシュラウドの回転方向両端面の一部を、翼根部と
シュラウドで軸方向に対し互いに逆方向に傾いた傾斜面
とすることにより、隣合う動翼が傾斜面で面圧を持って
組立てられた際に発生する回転モーメントを、翼根部と
シュラウドとで互いに逆方向となるようにして相殺する
ように構成したことを特徴とする。SUMMARY OF THE INVENTION In order to achieve the above object, the present invention relates to a steam turbine blade having a shroud integrally formed with a blade at a tip thereof, wherein a blade root portion of the blade and a rotational direction of the shroud are provided. By forming a part of both end surfaces as inclined surfaces inclined in opposite directions to the axial direction at the blade root and shroud, rotation generated when adjacent blades are assembled with surface pressure on inclined surfaces The present invention is characterized in that the moment is offset in a direction opposite to each other between the blade root and the shroud.
【0006】[0006]
【作用】本発明によると、蒸気タービン動翼に作用する
回転モーメントは、翼根部およびシュラウドとで互いに
逆向きとなって打消し合い相殺される。したがって、従
来のように翼車やピンに何等付加的な力を与えないの
で、動翼の強度低下および振動抑制効果を損なうことが
ない。According to the present invention, the rotational moments acting on the steam turbine blades are mutually reversed at the blade root portion and the shroud, and cancel each other. Therefore, no additional force is applied to the impeller and the pin as in the prior art, so that the strength of the moving blade is not reduced and the effect of suppressing vibration is not impaired.
【0007】[0007]
【実施例】以下、本発明の実施例を図面を参照して説明
する。Embodiments of the present invention will be described below with reference to the drawings.
【0008】図1は本発明の一実施例である蒸気タービ
ン動翼の斜視図である。同図に示すように、動翼1は翼
根部2、翼部3、シュラウド4が一体に成型されてい
る。翼根部2の回転方向両端面5の蒸気入口側は、軸方
向に対し傾斜した傾斜面6となっている。一方、シュラ
ウド4の回転方向両端面の蒸気出口側には、翼根部2の
傾斜面6と軸方向に対し逆の傾斜面7を設けている。FIG. 1 is a perspective view of a steam turbine blade according to an embodiment of the present invention. As shown in FIG. 1, the blade 1 has a blade root 2, a blade 3, and a shroud 4 integrally formed. The steam inlet sides of both end surfaces 5 in the rotation direction of the blade root 2 are inclined surfaces 6 inclined with respect to the axial direction. On the other hand, on the steam outlet side of both ends in the rotation direction of the shroud 4, an inclined surface 7 opposite to the inclined surface 6 of the blade root portion 2 with respect to the axial direction is provided.
【0009】このように成型された動翼1を、図2
(a)に示すようにシュラウド4の傾斜面7が、隣接す
る動翼の相対する傾斜面と所定の面圧8を保つように組
立てる。また図2(b)に示すように翼根部2の傾斜面
6が、隣接する動翼の相対する傾斜面6と所定の面圧8
を保つように組立てる。さらに、動翼1は全周にわたり
連続する一つの動翼群を形成することにより、動翼の振
動を抑制するように構成されている。The rotor blade 1 molded in such a manner is shown in FIG.
As shown in (a), the shroud 4 is assembled so that the inclined surface 7 of the shroud 4 maintains a predetermined surface pressure 8 with the inclined surface of the adjacent moving blade. Further, as shown in FIG. 2B, the inclined surface 6 of the blade root portion 2 has a predetermined surface pressure 8
Assemble to keep Further, the moving blade 1 is configured to form one moving blade group that is continuous over the entire circumference, thereby suppressing vibration of the moving blade.
【0010】本実施例によれば、図2(a)および
(b)に示すように、面圧8によりシュラウド4に発生
する回転モーメント9と、面圧8により翼根部2に発生
する回転モーメント10とは互いに逆方向となるので、
両モーメントは打消し合って相殺される。したがって、
従来のように翼根部と翼車を結合する結合ピンに付加的
な力は一切作用しないので、結合ピンの強度低下は発生
しない。また翼車と動翼の接触面が変形するような付加
的な力も作用しない。本発明は上記実施例に限定される
ものではなく、その要旨を変更しない範囲で種々変形し
て実施することができる。According to this embodiment, as shown in FIGS. 2A and 2B, a rotational moment 9 generated in the shroud 4 by the surface pressure 8 and a rotational moment generated in the blade root 2 by the surface pressure 8 Since the directions are opposite to each other,
Both moments cancel each other out. Therefore,
As in the prior art, no additional force acts on the connecting pin connecting the blade root and the impeller, so that the strength of the connecting pin does not decrease. Also, no additional force acts on the contact surface between the impeller and the moving blade. The present invention is not limited to the above-described embodiment, and can be implemented with various modifications without departing from the scope of the invention.
【0011】[0011]
【発明の効果】以上説明したように、本発明によれば、
動翼の振動抑制効果を何等損なうことなく、しかも翼車
や結合ピンに付加的な力を与えることはないので、信頼
性の高い全周一群の蒸気タービン動翼を提供することが
できる。As described above, according to the present invention,
Since no additional force is applied to the impeller and the connecting pin without impairing the effect of suppressing the vibration of the moving blade at all, it is possible to provide a group of highly reliable steam turbine moving blades around the entire circumference.
【図1】本発明の一実施例の斜視図。FIG. 1 is a perspective view of one embodiment of the present invention.
【図2】同図(a)は図1のシュラウドに作用する圧力
および回転モーメントを模式的に示す図、同図(b)は
図1の翼根部に作用する圧力および回転モーメントを模
式的に示す図。2A is a diagram schematically showing the pressure and the rotational moment acting on the shroud of FIG. 1, and FIG. 2B is a diagram schematically showing the pressure and the rotational moment acting on the blade root of FIG. FIG.
【図3】同図(a)は従来の動翼の斜視図、同図(b)
は動翼を翼車に組立てた部分断面図、同図(c)はシュ
ラウドに作用する圧力および回転モーメントを模式的に
示す図、同図(d)は翼根部に作用する圧力および回転
モーメントを模式的に示す図。FIG. 3A is a perspective view of a conventional moving blade, and FIG.
Is a partial cross-sectional view in which a rotor blade is assembled to an impeller, FIG. 4C schematically shows pressure and rotational moment acting on a shroud, and FIG. 4D shows pressure and rotational moment acting on a blade root. The figure which shows typically.
【図4】同図(a)は従来の他の動翼の斜視図、同図
(b)は動翼を翼車に組立てた部分断面図、同図(c)
はシュラウドに作用する圧力および回転モーメントを模
式的に示す図、同図(d)は翼根部に作用する圧力およ
び回転モーメントを模式的に示す図。FIG. 4 (a) is a perspective view of another conventional moving blade, FIG. 4 (b) is a partial cross-sectional view of the moving blade assembled to the impeller, and FIG. 4 (c).
FIG. 3 is a diagram schematically showing a pressure and a rotational moment acting on a shroud, and FIG. 3 (d) is a diagram schematically showing a pressure and a rotational moment acting on a blade root.
1…動翼、2…翼根部、3…翼部、4…シュラウド、5
…翼根部回転方向端面、6…翼根部傾斜面、7…シュラ
ウド傾斜面、8…面圧、9…シュラウドに発生する回転
モーメント、10…翼根部に発生する回転モーメント、
11…翼車、18…動翼・翼車接触面、19…結合ピ
ン。DESCRIPTION OF SYMBOLS 1 ... Moving blade, 2 ... Blade root part, 3 ... Blade part, 4 ... Shroud, 5
... end face of blade root rotation direction, 6 ... blade root slope, 7 ... shroud slope, 8 ... surface pressure, 9 ... rotational moment generated in shroud, 10 ... rotational moment generated in blade root,
11 ... impeller, 18 ... rotor / wheel contact surface, 19 ... connecting pin.
Claims (1)
ドを有する蒸気タービン動翼において、前記動翼の翼根
部およびシュラウドの回転方向両端面の一部を、翼根部
とシュラウドで軸方向に対し互いに逆方向に傾いた傾斜
面とすることにより、隣合う動翼が傾斜面で面圧を持っ
て組立てられた際に発生する回転モーメントを、翼根部
とシュラウドとで互いに逆方向となるようにして相殺す
るように構成したことを特徴とする蒸気タービン動翼。1. A steam turbine blade having a shroud integrally formed with a moving blade at a tip thereof, a blade root portion of the moving blade and a part of both end surfaces in a rotational direction of the shroud are axially separated by the blade root portion and the shroud. On the other hand, by making the inclined surfaces inclined in opposite directions to each other, the rotating moment generated when the adjacent moving blades are assembled with the surface pressure on the inclined surface becomes opposite to each other at the blade root portion and the shroud. A steam turbine blade characterized by being configured to cancel each other.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP3107873A JP2854722B2 (en) | 1991-05-14 | 1991-05-14 | Steam turbine blade |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP3107873A JP2854722B2 (en) | 1991-05-14 | 1991-05-14 | Steam turbine blade |
Publications (2)
Publication Number | Publication Date |
---|---|
JPH04339102A JPH04339102A (en) | 1992-11-26 |
JP2854722B2 true JP2854722B2 (en) | 1999-02-03 |
Family
ID=14470256
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP3107873A Expired - Fee Related JP2854722B2 (en) | 1991-05-14 | 1991-05-14 | Steam turbine blade |
Country Status (1)
Country | Link |
---|---|
JP (1) | JP2854722B2 (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP3933130B2 (en) * | 2001-08-03 | 2007-06-20 | 株式会社日立製作所 | Turbine blade |
EP2918784A1 (en) * | 2014-03-13 | 2015-09-16 | Siemens Aktiengesellschaft | Blade foot for a turbine blade |
-
1991
- 1991-05-14 JP JP3107873A patent/JP2854722B2/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
JPH04339102A (en) | 1992-11-26 |
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