JPH0861007A - Stator blade device for steam turbine - Google Patents
Stator blade device for steam turbineInfo
- Publication number
- JPH0861007A JPH0861007A JP19244894A JP19244894A JPH0861007A JP H0861007 A JPH0861007 A JP H0861007A JP 19244894 A JP19244894 A JP 19244894A JP 19244894 A JP19244894 A JP 19244894A JP H0861007 A JPH0861007 A JP H0861007A
- Authority
- JP
- Japan
- Prior art keywords
- divided
- stator blade
- diameter side
- dividing surface
- steam turbine
- 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- Withdrawn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
Abstract
Description
【0001】[0001]
【産業上の利用分野】本発明は蒸気タービンの静翼装置
に関し、特にその静翼輪の分割構造に関する。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a steam turbine stationary blade device, and more particularly to a divided structure of a stationary blade ring.
【0002】[0002]
【従来の技術】蒸気タービンの静翼装置における静翼輪
は上下に分割されているが、従来の静翼輪の分割部は図
3〜図6に示す構造となっていた。従来の静翼輪の上下
分割部の構造には、大きく分けて2種類ある。2. Description of the Related Art A stationary vane ring in a stationary vane device of a steam turbine is divided into upper and lower parts, but the conventional vane ring has a structure shown in FIGS. There are roughly two types of conventional structures of the upper and lower divided portions of the stationary vane wheel.
【0003】すなわち、その一つは、図3,図4に示す
ように、静翼のプロフィル11に沿って斜めに分割する
ものであり、もう一つは図5,図6に示すように、静翼
輪12を水平に分割してその分割面に当る静翼を半翼1
3とし、これをピン14などで補強するものである。That is, one is to divide the stator blade obliquely along the profile 11 of the vane as shown in FIGS. 3 and 4, and the other is to divide it as shown in FIGS. The vane ring 12 is divided horizontally, and the vane that hits the divided surface is the half-blade 1.
3, which is reinforced with pins 14 and the like.
【0004】[0004]
【発明が解決しようとする課題】従来の静翼輪の上下分
割部の構造は前述の通りであるが、図3,図4に示すも
のについては、斜め分割部の上下に加工精度、加工技術
の都合上、通常1.6mm程度の隙間を設ける必要がある
ことから、この隙間を通って蒸気が洩れるという欠点が
ある。The structure of the conventional upper and lower split portions of the stationary vane ring is as described above. However, in the structures shown in FIG. 3 and FIG. For this reason, it is usually necessary to provide a gap of about 1.6 mm, and there is a drawback that steam leaks through this gap.
【0005】また図5,図6に示すものについては、上
下分割部はその水平面を隙間なしに合せることができる
が、図に示す如く、水平分割面に当る静翼が分割されて
半翼となるため分割された静翼をピンで補強するなどの
対応が必要となり、それらの補強構造のため、蒸気に対
する円滑な流路を形成することができず、性能を犠牲に
しなければならないという欠点がある。5 and 6, the upper and lower split parts can be aligned in the horizontal plane without any gap, but as shown in the figure, the stationary blades that hit the horizontal split surface are divided into half blades. Therefore, it is necessary to take measures such as reinforcing the divided stationary blades with pins, and due to these reinforcing structures, it is not possible to form a smooth flow path for steam, and there is the disadvantage that performance must be sacrificed. is there.
【0006】本発明はこれらの欠点を解消するためにな
されたもので、静翼輪の上下分割部に蒸気洩れを起こす
隙間と、補強を必要とする半翼を発生させない構造の蒸
気タービンの静翼装置を提供することを課題としてい
る。The present invention has been made in order to eliminate these drawbacks, and a static turbine of a steam turbine having a structure that does not generate a gap that causes steam leakage in the upper and lower split portions of the stationary vane ring and a half blade that requires reinforcement. An object is to provide a wing device.
【0007】[0007]
【課題を解決するための手段】本発明は、上下に分割し
た静翼輪をもつ蒸気タービンの静翼装置における前記課
題を解決するため、静翼輪の分割面の内径側部を翼間を
通る斜めの分割面とするとともに外径側部を水平分割面
とした複合分割面とする。SUMMARY OF THE INVENTION In order to solve the above-mentioned problems in a steam turbine stator vane device having vertically divided stator vanes, the present invention is designed so that the inner diameter side portion of the split surface of the stator vane is placed between the blades. A diagonal dividing surface that passes through and a composite dividing surface in which the outer diameter side portion is a horizontal dividing surface.
【0008】そして、その斜め分割面は対向する斜め分
割面との間に隙間を有し、水平分割面は対向する水平分
割面と密着する構造とする。Further, the diagonal dividing surface has a gap between the facing diagonal dividing surface, and the horizontal dividing surface is in close contact with the facing horizontal dividing surface.
【0009】[0009]
【作用】本発明による静翼装置では、その静翼輪の上下
分割面を内径側部の斜め分割面と外径側部の水平分割面
とを組合せた複合分割面で構成したことにより、斜め分
割面の隙間を通る蒸気洩れは、外径側部の水平分割面で
閉塞される。In the stator vane device according to the present invention, since the upper and lower split faces of the stator vane ring are composed of the complex split faces in which the diagonal split faces on the inner diameter side and the horizontal split faces on the outer diameter side are combined, Leakage of steam passing through the gap between the dividing surfaces is blocked by the horizontal dividing surface on the outer diameter side.
【0010】また内径側部の分割面は翼間を通る斜めの
分割面としているので静翼は、分割面に当って半翼とな
ることを避けることができる。そのためピンによる静翼
の補強などが不要となる。従ってこれまでの静翼装置が
有していた欠点を解消することができる。Further, since the dividing surface on the inner diameter side is an oblique dividing surface that passes between the blades, it is possible to prevent the stationary blade from hitting the dividing surface and becoming a half blade. Therefore, it is not necessary to reinforce the vane with pins. Therefore, it is possible to eliminate the drawbacks that the conventional vane devices have.
【0011】[0011]
【実施例】以下、本発明を図1,図2に示した一実施例
に基づいて具体的に説明する。図1は静翼輪の分割部に
おける内径側の側面図である。図2は、その分割された
静翼輪の下側部の斜視図である。静翼輪1の内径側部2
は静翼4の間を斜めに分割して分割面Aを形成させてあ
る。静翼輪1の外径側部3は、水平に分割してあり分割
面Bを形成させてある。DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS The present invention will be specifically described below based on an embodiment shown in FIGS. FIG. 1 is a side view of the divided portion of the stationary vane ring on the inner diameter side. FIG. 2 is a perspective view of a lower side portion of the divided stationary vane ring. Inner diameter side part 2 of vane wheel 1
Divides the stator vanes 4 obliquely to form a dividing surface A. The outer diameter side portion 3 of the stationary vane wheel 1 is horizontally divided to form a dividing surface B.
【0012】このように静翼輪1の上下分割部を斜めの
分割面Aと水平な分割面Bとからなる複合分割面とした
ことにより、隙間を通る蒸気洩れは水平分割面Bが閉塞
されて防止されるとともに、静翼4は翼間を通る斜めの
分割面Aによって半翼になることを避けることができ、
そのため、従来のものに見られたピンによる静翼の補強
などが不要となる。As described above, the upper and lower divided portions of the stationary vane ring 1 are formed as the compound divided surfaces composed of the diagonal divided surface A and the horizontal divided surface B, so that the horizontal divided surface B is blocked by the steam leakage passing through the gap. And the stationary blade 4 can be prevented from becoming a half blade due to the slanted dividing surface A passing between the blades.
Therefore, it is not necessary to reinforce the stationary blade with the pin, which is seen in the conventional one.
【0013】[0013]
【発明の効果】本発明の静翼装置では、その静翼輪の分
割面を、内径側部の斜め分割面と外径側部の水平分割面
とからなる複合分割面で構成してあるので、従来の斜め
分割において生じていた隙間からの蒸気の洩れや水平分
割における半翼の発生とその補強等の欠点が解消され
る。In the stator vane device of the present invention, the stator vane ring is divided by a compound dividing face composed of an oblique dividing face on the inner diameter side and a horizontal dividing face on the outer diameter side. The problems such as steam leakage from the gap, generation of half blades in horizontal division, and reinforcement thereof, which have occurred in conventional diagonal division, are eliminated.
【0014】そのため本発明による静翼装置ではその性
能が向上するうえ、翼の強度も確保されるので蒸気ター
ビンの品質向上に寄与する効果は極めて大きい。Therefore, in the stationary blade device according to the present invention, not only the performance is improved but also the strength of the blade is secured, so that the effect of improving the quality of the steam turbine is extremely large.
【図1】本発明の一実施例に係る静翼装置における複合
分割面部分を内径側から見た側面図。FIG. 1 is a side view of a composite divided surface portion of a stationary blade device according to an embodiment of the present invention as viewed from an inner diameter side.
【図2】図1に示した静翼装置における複合分割面の下
側部分の斜視図。FIG. 2 is a perspective view of a lower portion of a composite dividing surface in the stationary blade device shown in FIG.
【図3】従来の静翼装置における斜め分割面部分の側面
図。FIG. 3 is a side view of an oblique dividing surface portion in a conventional vane device.
【図4】従来の静翼装置における別の斜め分割面部分の
側面図。FIG. 4 is a side view of another oblique division surface portion in the conventional vane device.
【図5】従来の静翼装置における水平分割面部分の側面
図。FIG. 5 is a side view of a horizontal split surface portion of a conventional vane device.
【図6】従来の静翼装置における別の水平分割面部分の
側面図。FIG. 6 is a side view of another horizontal division surface portion in the conventional vane device.
1 静翼輪 2 内径側部 3 外径側部 4 静翼 A 斜めの分割面 B 水平分割面 1 stationary vane ring 2 inner diameter side part 3 outer diameter side part 4 stationary vane A diagonal dividing surface B horizontal dividing surface
Claims (1)
ビンの静翼装置において、前記静翼輪の分割面が、内径
側部は翼間を通り互いに隙間を有する斜めの分割面、外
径側部は互いに密着する水平な分割面とした複合分割面
からなることを特徴とする蒸気タービンの静翼装置。1. A steam turbine stationary vane device having vertically divided stationary vanes, wherein a dividing surface of the stationary vane is an oblique dividing surface having an inner diameter side portion between the blades and a gap therebetween, and an outer portion. A stationary vane device for a steam turbine, characterized in that the radial side portion is composed of a composite dividing surface which is a horizontal dividing surface in close contact with each other.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP19244894A JPH0861007A (en) | 1994-08-16 | 1994-08-16 | Stator blade device for steam turbine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP19244894A JPH0861007A (en) | 1994-08-16 | 1994-08-16 | Stator blade device for steam turbine |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH0861007A true JPH0861007A (en) | 1996-03-05 |
Family
ID=16291478
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP19244894A Withdrawn JPH0861007A (en) | 1994-08-16 | 1994-08-16 | Stator blade device for steam turbine |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH0861007A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109356669A (en) * | 2018-10-19 | 2019-02-19 | 杭州中能汽轮动力有限公司 | The arc of impulse turbine divides whole stator blade |
-
1994
- 1994-08-16 JP JP19244894A patent/JPH0861007A/en not_active Withdrawn
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109356669A (en) * | 2018-10-19 | 2019-02-19 | 杭州中能汽轮动力有限公司 | The arc of impulse turbine divides whole stator blade |
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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: 20011106 |