JPH0674001A - Governor stage nozzle of steam turbine - Google Patents
Governor stage nozzle of steam turbineInfo
- Publication number
- JPH0674001A JPH0674001A JP25060992A JP25060992A JPH0674001A JP H0674001 A JPH0674001 A JP H0674001A JP 25060992 A JP25060992 A JP 25060992A JP 25060992 A JP25060992 A JP 25060992A JP H0674001 A JPH0674001 A JP H0674001A
- Authority
- JP
- Japan
- Prior art keywords
- nozzle
- blade width
- pieces
- steam turbine
- piece
- 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- Withdrawn
Links
Landscapes
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Description
【0001】[0001]
【産業上の利用分野】本発明は、蒸気タービンの調速段
ノズルに関する。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a speed control nozzle for a steam turbine.
【0002】[0002]
【従来の技術】蒸気タービンの調速段ノズルとして、従
来、組立式ノズルと溶接式ノズルとがある。2. Description of the Related Art Conventionally, there are an assembly type nozzle and a welding type nozzle as a speed control nozzle of a steam turbine.
【0003】図2は従来の組立式ノズルを示す縦断面図
であり、ノズルを構成する複数のノズル片1は外壁2と
内壁3とにそれぞれ嵌め込まれ、まだノズル片列の上流
側には補強用の支柱4が複数配置されて外壁2と内壁3
とに溶接されている。そして、図3の横断面図に示すよ
うに、蒸気5は複数のノズル片1で限定される流路内を
通過することにより膨張し、図示していない動翼翼列へ
流入する。FIG. 2 is a vertical cross-sectional view showing a conventional assembly type nozzle. A plurality of nozzle pieces 1 constituting the nozzle are fitted into an outer wall 2 and an inner wall 3, respectively, and a reinforcement is still provided on the upstream side of the nozzle piece row. A plurality of supporting columns 4 are arranged to form an outer wall 2 and an inner wall 3.
It is welded to. Then, as shown in the cross-sectional view of FIG. 3, the steam 5 expands by passing through the flow passage defined by the plurality of nozzle pieces 1, and flows into a blade row (not shown).
【0004】次に、図4は従来の溶接式ノズルを示す縦
断面図であり、ノズルを構成する複数のノズル片11は
外壁12と内壁13とにそれぞれ溶接され、ノズル片1
1は翼幅を大きくされて、支柱の役割を兼ねている。そ
して、図5の横断面図に示すように、蒸気14は複数の
ノズル片11で限定される流路内を通過することにより
膨張し、図示していない動翼翼列へ流入する。Next, FIG. 4 is a longitudinal sectional view showing a conventional welding type nozzle. A plurality of nozzle pieces 11 constituting the nozzle are welded to an outer wall 12 and an inner wall 13, respectively, and the nozzle piece 1 is formed.
1 has a large wing width and also serves as a pillar. Then, as shown in the cross-sectional view of FIG. 5, the steam 14 expands by passing through the flow passage defined by the plurality of nozzle pieces 11, and flows into a blade row (not shown).
【0005】[0005]
【発明が解決しようとする課題】ところで、以上述べた
従来の蒸気タービン調速段ノズルにおいて、図2,図3
に示した従来の組立式ノズルでは、ノズル片1は翼の断
面積が小さいために、外壁2と内壁3との支えとなるに
は強度が弱いことから、ノズル片1とは別に支柱4を設
けているが、この支柱4が蒸気流れ5の妨げとなり、圧
損の原因となる他、ノズル片列に流入する蒸気流れ5を
乱し、損失の原因となる問題があった。By the way, in the conventional steam turbine speed control stage nozzle described above, as shown in FIGS.
In the conventional assembly type nozzle shown in FIG. 2, since the nozzle piece 1 has a small blade cross-sectional area, it is weak in strength to support the outer wall 2 and the inner wall 3. Therefore, the column 4 is provided separately from the nozzle piece 1. However, the column 4 obstructs the steam flow 5 and causes pressure loss, and also disturbs the steam flow 5 flowing into the nozzle piece row, which causes a problem of loss.
【0006】一方、図4,図5に示した従来の溶接式ノ
ズルでは、ノズル片11に外壁12と内壁13とを支え
る支柱としての役目も持たせるため、その翼幅を大きく
することによって翼の断面積を増し、強度を増加させて
いることから、この溶接式ノズル片11は前述した組立
式ノズル片1に比べて翼幅が大きくなり、このため2次
流れ損失が大きくなる問題があった。On the other hand, in the conventional welding type nozzle shown in FIGS. 4 and 5, the blade is enlarged by increasing the blade width so that the nozzle piece 11 also has a function as a support for supporting the outer wall 12 and the inner wall 13. Since the welded nozzle piece 11 has a larger blade width than the above-described assembled nozzle piece 1 due to the increased cross-sectional area and the increased strength, there is a problem that the secondary flow loss increases. It was
【0007】本発明は、このような従来技術の課題を解
決するためになされたもので、ノズル片列の上流側に支
柱を設置することを止めて圧損や蒸気流れの乱れを無く
し、かつノズル片間に発生する2次流れ損失を小さくす
るようにした蒸気タービンの調速段ノズルを提供するこ
とを目的とする。The present invention has been made in order to solve the above-mentioned problems of the prior art, and stops the installation of the column on the upstream side of the nozzle piece row to eliminate pressure loss and turbulence of the steam flow, and It is an object of the present invention to provide a speed-control stage nozzle for a steam turbine in which the secondary flow loss generated between the one side is reduced.
【0008】[0008]
【課題を解決するための手段】上記の課題を解決するた
めに、本発明は、複数のノズル片から成る蒸気タービン
の調速段ノズルにおいて、前記ノズル片を、翼幅の小さ
い複数のノズル片と、上流側前半部の曲率を小さくし
た、翼幅の大きい複数のノズル片とで構成し、翼幅の大
きいノズル片間に少なくとも1枚の翼幅の小さいノズル
片を配置したものである。In order to solve the above problems, the present invention provides a speed control nozzle for a steam turbine comprising a plurality of nozzle pieces, wherein the nozzle pieces are a plurality of nozzle pieces having a small blade width. And a plurality of nozzle pieces each having a large blade width and having a small curvature in the upstream front half portion, and at least one nozzle piece having a small blade width is arranged between the nozzle pieces having a large blade width.
【0009】[0009]
【作用】上記の手段によれば、ノズル片とは別の支柱が
存在しないため、支柱による圧損や蒸気流れの乱れが無
くなり、損失が減少する。また、翼幅の大きいノズル片
の間隔が大きくなるため、翼幅の大きいノズル間に発生
する2次流れ損失が減少する。According to the above means, since there is no column other than the nozzle piece, pressure loss and turbulence of the steam flow due to the column are eliminated, and the loss is reduced. Further, since the interval between the nozzle pieces having the large blade width becomes large, the secondary flow loss generated between the nozzles having the large blade width is reduced.
【0010】そして、翼幅の大きいノズル片の上流側前
半部の曲率が小さいことから、翼幅の大きいノズル片の
上流側前半部の背面側及び腹面側での蒸気流れの加速は
低く抑えられ、ノズル片の後半部では全ての流路でほぼ
同じ流入条件となるため、形状の異なるノズル片を混在
させたことによる蒸気流れの不均一性は低く抑えられ
る。Further, since the upstream half of the nozzle piece having a large blade width has a small curvature, the acceleration of the steam flow on the back side and the ventral side of the upstream half of the nozzle piece having a large blade width can be suppressed to a low level. In the latter half of the nozzle piece, all the flow paths have substantially the same inflow condition, so that the nonuniformity of the vapor flow due to the mixture of the nozzle pieces having different shapes can be suppressed to a low level.
【0011】[0011]
【実施例】以下、図1を参照して本発明の一実施例につ
いて詳細に説明する。図1は、本発明に係る蒸気タービ
ン調速段ノズルの一実施例を示す横断面図である。An embodiment of the present invention will be described in detail below with reference to FIG. FIG. 1 is a cross-sectional view showing an embodiment of a steam turbine speed control stage nozzle according to the present invention.
【0012】図1において、蒸気タービンの調速段ノズ
ルは、翼幅の小さい複数のノズル片21と、翼幅の大き
い、例えばノズル片21の翼幅の約2倍の翼幅を有する
複数のノズル片22とで構成され、この翼幅の大きいノ
ズル片22の上流側前半部の曲率は小さくされている。
そして、翼幅の大きいノズル片22間には、少なくとも
1枚(本実施例では2枚)の翼幅の小さいノズル片21
が配置されている。In FIG. 1, the speed-control stage nozzle of the steam turbine has a plurality of nozzle pieces 21 having a small blade width and a plurality of blade pieces having a large blade width, for example, about twice the blade width of the nozzle piece 21. The nozzle piece 22 has a large blade width, and the upstream half of the nozzle piece 22 has a small curvature.
At least one (two in this embodiment) nozzle piece 21 having a small blade width is provided between the nozzle pieces 22 having a large blade width.
Are arranged.
【0013】なお、翼幅の小さいノズル片21は組立
式、翼幅の大きいノズル片22は溶接式とすることがで
きるが、必ずしもこれに限られるものではない。Although the nozzle piece 21 having a small blade width may be of the assembly type and the nozzle piece 22 having a large blade width may be of the welding type, the invention is not limited to this.
【0014】以上述べた蒸気タービン調速段ノズルの構
成によれば、ノズル片21,22とは別の支柱が存在し
ないため、図2,図3に示した従来の組立式ノズルと比
較すれば、支柱による圧損や蒸気流れの乱れが無い分、
損失が減少する。また、翼幅の大きいノズル片22の間
隔が大きくなるため、翼幅の大きいノズル片22間に発
生する2次流れ損失が減少する。According to the structure of the steam turbine speed control stage nozzle described above, since there is no support column different from the nozzle pieces 21 and 22, a comparison with the conventional assembly type nozzle shown in FIGS. Since there is no pressure loss or steam flow disturbance due to the columns,
Loss is reduced. Moreover, since the interval between the nozzle pieces 22 having a large blade width becomes large, the secondary flow loss generated between the nozzle pieces 22 having a large blade width is reduced.
【0015】そして、翼幅の大きいノズル片22の上流
側前半部の曲率が小さいことから、翼幅の大きいノズル
片22の上流側前半部の背面側及び腹面側での蒸気流れ
23の加速は低く抑えられ、ノズル片の後半部では全て
の流路でほぼ同じ流入条件となるため、形状の異なるノ
ズル片を混在させたことによる蒸気流れの不均一性は低
く抑えられる。Since the upstream front half of the nozzle piece 22 having a large blade width has a small curvature, the steam flow 23 is accelerated on the back side and ventral side of the upstream front half of the nozzle piece 22 having a large blade width. Since the flow rate is suppressed to a low level, and in the latter half of the nozzle piece, all the flow paths have substantially the same inflow condition, so that the nonuniformity of the vapor flow due to the mixture of nozzle pieces having different shapes can be suppressed to a low level.
【0016】[0016]
【発明の効果】以上述べたように、本発明によれば、複
数のノズル片から成る蒸気タービンの調速段ノズルにお
いて、前記ノズル片を、翼幅の小さい複数のノズル片
と、上流側前半部の曲率を小さくした、翼幅の大きい複
数のノズル片とで構成し、翼幅の大きいノズル片間に少
なくとも1枚の翼幅の小さいノズル片を配置した構成と
したことにより、支柱の設置を止めて圧損や蒸気流れの
乱れを無くし、かつ翼幅の大きいノズル片間に発生する
2次流れ損失を小さくすることができる。そして、形状
の異なるノズル片を混在させたことによる蒸気流れの不
均一性も、翼幅の大きいノズル片の上流側前半部の曲率
を小さくしたことによって低く抑えることができる。As described above, according to the present invention, in a speed control stage nozzle of a steam turbine comprising a plurality of nozzle pieces, the nozzle piece is composed of a plurality of nozzle pieces having a small blade width and an upstream first half. Installation of stanchions by configuring with a plurality of nozzle pieces with large blade width with a small curvature of part, and arranging at least one nozzle piece with small blade width between nozzle pieces with large blade width It is possible to stop the pressure loss and the turbulence of the steam flow, and reduce the secondary flow loss generated between the nozzle pieces having a large blade width. Further, the nonuniformity of the steam flow due to the mixing of nozzle pieces having different shapes can be suppressed to a low level by reducing the curvature of the upstream front half of the nozzle piece having a large blade width.
【図1】本発明に係る蒸気タービン調速段ノズルの一実
施例を示す横断面図である。FIG. 1 is a cross-sectional view showing an embodiment of a steam turbine speed control stage nozzle according to the present invention.
【図2】従来の蒸気タービン調速段ノズルの一例を示す
縦断面図である。FIG. 2 is a vertical cross-sectional view showing an example of a conventional steam turbine speed control stage nozzle.
【図3】図2の調速段ノズルの横断面図である。3 is a cross-sectional view of the speed control stage nozzle of FIG.
【図4】従来の蒸気タービン調速段ノズルの他の例を示
す縦断面図である。FIG. 4 is a vertical cross-sectional view showing another example of a conventional steam turbine speed control stage nozzle.
【図5】図4の調速段ノズルの横断面図である。5 is a cross-sectional view of the speed control stage nozzle of FIG.
21 翼幅の小さいノズル片 22 翼幅の大きいノズル片 23 蒸気流れ 21 Nozzle piece with small blade width 22 Nozzle piece with large blade width 23 Steam flow
Claims (1)
速段ノズルにおいて、前記ノズル片を、翼幅の小さい複
数のノズル片と、上流側前半部の曲率を小さくした、翼
幅の大きい複数のノズル片とで構成し、翼幅の大きいノ
ズル片間に少なくとも1枚の翼幅の小さいノズル片を配
置したことを特徴とする蒸気タービンの調速段ノズル。1. A steam turbine speed-control stage nozzle comprising a plurality of nozzle pieces, the nozzle pieces comprising a plurality of nozzle pieces having a small blade width, and a plurality of blade pieces having a small upstream side half and a large blade width. And a nozzle piece having a small blade width, and at least one nozzle piece having a small blade width is disposed between the nozzle pieces having a large blade width.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP25060992A JPH0674001A (en) | 1992-08-26 | 1992-08-26 | Governor stage nozzle of steam turbine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP25060992A JPH0674001A (en) | 1992-08-26 | 1992-08-26 | Governor stage nozzle of steam turbine |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH0674001A true JPH0674001A (en) | 1994-03-15 |
Family
ID=17210411
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP25060992A Withdrawn JPH0674001A (en) | 1992-08-26 | 1992-08-26 | Governor stage nozzle of steam turbine |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH0674001A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2005103465A1 (en) * | 2004-04-26 | 2005-11-03 | Ishikawajima-Harima Heavy Industries Co., Ltd. | Turbine nozzle segment, turbine nozzle, turbine, and gas turbine engine |
JP2009215897A (en) * | 2008-03-07 | 2009-09-24 | Mitsubishi Heavy Ind Ltd | Gas turbine engine |
US9091174B2 (en) | 2011-05-13 | 2015-07-28 | Rolls-Royce Plc | Method of reducing asymmetric fluid flow effects in a passage |
-
1992
- 1992-08-26 JP JP25060992A patent/JPH0674001A/en not_active Withdrawn
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2005103465A1 (en) * | 2004-04-26 | 2005-11-03 | Ishikawajima-Harima Heavy Industries Co., Ltd. | Turbine nozzle segment, turbine nozzle, turbine, and gas turbine engine |
JP2009215897A (en) * | 2008-03-07 | 2009-09-24 | Mitsubishi Heavy Ind Ltd | Gas turbine engine |
US9091174B2 (en) | 2011-05-13 | 2015-07-28 | Rolls-Royce Plc | Method of reducing asymmetric fluid flow effects in a passage |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
A300 | Withdrawal of application because of no request for examination |
Free format text: JAPANESE INTERMEDIATE CODE: A300 Effective date: 19991102 |