JPH08284607A - Steam turbine stationary blade - Google Patents

Steam turbine stationary blade

Info

Publication number
JPH08284607A
JPH08284607A JP8248395A JP8248395A JPH08284607A JP H08284607 A JPH08284607 A JP H08284607A JP 8248395 A JP8248395 A JP 8248395A JP 8248395 A JP8248395 A JP 8248395A JP H08284607 A JPH08284607 A JP H08284607A
Authority
JP
Japan
Prior art keywords
shroud
steam turbine
stationary blade
stationary blades
rubber
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Withdrawn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
JP8248395A
Other languages
Japanese (ja)
Inventor
Takeshi Eguchi
剛 江口
Takayuki Otsuka
隆幸 大塚
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.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries Ltd
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 Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP8248395A priority Critical patent/JPH08284607A/en
Publication of JPH08284607A publication Critical patent/JPH08284607A/en
Withdrawn legal-status Critical Current

Links

Abstract

PURPOSE: To obstruct occurrence of an unconformable event such as breakdown of stationary blades by constituting a shroud out of a first shroud secured on the inner circumferential end of maximum stationary blades and a secondary shroud elastically combined with the first shroud. CONSTITUTION: In maximum stationary blades 2 used in the low pressure stage of a steam turbine, a shroud fixing the stationary blades 2 is divided into two parts, a first shroud 3 and a second shroud 4, and the stationary blades 2 are in the condition of being fixed with rubber bolts 5 by fixing the shrouds through the rubber bolts 5. Hereby, the large damping effect of rubber itself of the rubber bolts 5 is applied to the stationary blades 2, and hence even if the stationary blades 2 are excited by steam flow at the low pressure stage and intended to vibrate, the vibration is restrained by the damping effect of the rubber itself, and the vibration is prevented from being enlarged.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】本発明は、蒸気タービンの低圧段
に設置される長大静翼の振動抑制を向上させた蒸気ター
ビン静翼に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a steam turbine stationary blade in which vibration suppression of a long stationary blade installed in a low pressure stage of a steam turbine is improved.

【0002】[0002]

【従来の技術】蒸気タービンは、一般的に高圧段又は高
圧段および中圧段と低圧段から構成されるが、低圧段と
なるほど通過する蒸気の密度が低下し、単位時間に通過
する体積、いわゆる体積流量が急激に大きくなる。した
がって、低圧段に設置される静翼は長大化し、静翼の剛
性が低下する傾向にある。
2. Description of the Related Art A steam turbine is generally composed of a high-pressure stage or a high-pressure stage and an intermediate-pressure stage and a low-pressure stage. The so-called volume flow rate increases rapidly. Therefore, the vanes installed in the low-pressure stage tend to be long and the rigidity of the vanes tends to decrease.

【0003】このような、蒸気タービンの低圧段に従来
使用されている長大静翼を具えた蒸気タービン静翼の一
例を図3及び図4に示す。図において、1は外周縁を蒸
気タービンのケーシング内周面に設けた溝に嵌合して、
静翼2を蒸気通路の所定位置に保持する翼根リング、3
aは回転するロータの外周面上に保持されるシール装置
を、その内周に設けるシュラウドを示し、それぞれ翼根
リング1の内周面と静翼2外径端、及び静翼2内径端と
シュラウド3a外周面は、肉盛溶接7で固着されてい
る。
An example of such a steam turbine vane having long vanes conventionally used in the low pressure stage of the steam turbine is shown in FIGS. 3 and 4. In the figure, 1 is an outer peripheral edge fitted into a groove provided on an inner peripheral surface of a casing of a steam turbine,
A blade root ring for holding the stationary blade 2 at a predetermined position in the steam passage, 3
Reference symbol a denotes a shroud provided on the inner periphery of a sealing device held on the outer peripheral surface of a rotating rotor, and the inner peripheral surface of the blade root ring 1, the outer diameter end of the stationary blade 2, and the inner diameter end of the stationary blade 2 respectively. The outer peripheral surface of the shroud 3a is fixed by overlay welding 7.

【0004】このように、従来の蒸気タービン静翼は、
静翼2の内周側をシュラウド3a、外周側を翼根リング
1と、それぞれ肉盛溶接7によって固着する剛体結合で
構成されているため、振動に対する減衰効果が非常に小
さかった。すなわち、このような構造の蒸気タービン静
翼においては、静翼2が長大静翼となり、その剛性が低
くなるため、通過する蒸気力によって、静翼2の振動が
大きくなり、しかも減衰効果が小さいために、静翼2が
破損するという不適合事象が生じることが考えられてい
る。
Thus, the conventional steam turbine vane is
Since the inner peripheral side of the stationary blade 2 is composed of the shroud 3a and the outer peripheral side is composed of the blade root ring 1 and rigid-body couplings fixed by the overlay welding 7, respectively, the damping effect on vibration is very small. That is, in the steam turbine stationary blade having such a structure, the stationary blade 2 becomes a large stationary blade and its rigidity becomes low, so that the vibration of the stationary blade 2 is increased by the passing steam force, and the damping effect is small. Therefore, it is considered that a nonconformity event occurs in which the stationary blade 2 is damaged.

【0005】[0005]

【発明が解決しようとする課題】本発明は、従来の蒸気
タービン静翼の、上述した不具合を解消するため、蒸気
力で静翼に発生する振動に対する減衰効果を高くして、
静翼が破損するという不適合事象が生じないようにした
蒸気タービン静翼を提供することを課題とする。
SUMMARY OF THE INVENTION In order to solve the above-mentioned problems of the conventional steam turbine stationary blade, the present invention enhances the damping effect on the vibration generated in the stationary blade by the steam force,
An object of the present invention is to provide a steam turbine stationary blade that does not cause a nonconformity event that the stationary blade is damaged.

【0006】[0006]

【課題を解決するための手段】このため、本発明の蒸気
タービン静翼は、次の手段とした。静翼の内周側に固着
されるシュラウドを、長大静翼の内周端に溶接等で固着
される第1のシュラウド、および第1のシュラウドと弾
性体を介装して結合される第2のシュラウドに分割して
設けることとした。なお、弾性体を介装して第1のシュ
ラウドおよび第2のシュラウドを結合する1つの手段と
してゴムボルトがある。すなわち、ゴム等の弾性体の一
方の側に一端を固着した、ボルトの他端側に設けた雄螺
を、静翼と溶接で固定している第1のシュラウドに設け
た雌螺にねじこみ、もう一方の側に一端を固着した、別
のボルトの他端側に設けた雄螺は、静翼に溶接で固定さ
れていない第2のシュラウドとナットにて固定して、結
合することができる。また、別の結合手段として、原動
軸と従動軸の連結に、従来使用されているゴム軸継手、
若しくは金属ばね軸継手等、いわゆる弾性体を介装した
継手を採用することもできる。
Therefore, the steam turbine vane of the present invention has the following means. A shroud fixed to the inner peripheral side of the stationary vane, a first shroud fixed to the inner peripheral end of the long stationary vane by welding or the like, and a second shroud coupled to the first shroud via an elastic body. It was decided to divide it into shrouds. There is a rubber bolt as one means for connecting the first shroud and the second shroud with an elastic body interposed. That is, a male screw provided on the other end side of the bolt, one end of which is fixed to one side of an elastic body such as rubber, is screwed into a female screw provided on the first shroud fixed to the stationary blade by welding, A male screw having one end fixed to the other side and provided on the other end side of another bolt can be fixed by a nut and a second shroud that is not fixed to the stationary blade by welding and can be connected. . Further, as another coupling means, a rubber shaft coupling conventionally used for connecting a driving shaft and a driven shaft,
Alternatively, a joint having a so-called elastic body interposed, such as a metal spring shaft joint, can be adopted.

【0007】[0007]

【作用】第2のシュラウドが弾性体を介して結合されて
いる第1のシュラウドは、その外周縁が静翼の内周縁と
溶接等にて固着されるが、第2のシュラウドは、弾性体
が介装されているために、静翼とは完全な剛体結合とは
ならず、弾性体がダンパーとして作用する。すなわち、
この構造によって静翼は、弾性体の上で固定されている
こととなり、従来の溶接のみによる結合と比べて、弾性
体自身の高い減衰効果が得られる。したがって、従来の
減衰効果が小さい剛体結合の蒸気タービン静翼の場合と
比べて、大きな減衰効果が得られ、静翼の振動が抑制さ
れる。これによって、体積流量の大きい蒸気の流れがあ
る中で、静翼が振動しても、弾性体の減衰効果によっ
て、剛性の小さい長大静翼においても、破損するような
ことがなくなり、信頼性が確保できる蒸気タービン静翼
とすることができる。
The outer peripheral edge of the first shroud, to which the second shroud is connected via the elastic body, is fixed to the inner peripheral edge of the vane by welding or the like, while the second shroud is made of the elastic body. Due to the interposition of, the rigid vanes are not completely rigidly coupled, and the elastic body acts as a damper. That is,
With this structure, the stationary blade is fixed on the elastic body, and a high damping effect of the elastic body itself can be obtained as compared with the conventional connection by only welding. Therefore, a large damping effect is obtained and vibration of the stationary blades is suppressed, as compared with the conventional case of a rigidly coupled steam turbine stationary blade having a small damping effect. As a result, even if the stationary blade vibrates in the presence of steam with a large volume flow rate, the damping effect of the elastic body will not damage even the large stationary blade with small rigidity, and reliability will be improved. It can be a steam turbine stationary blade that can be secured.

【0008】[0008]

【実施例】以下、本発明の蒸気タービン静翼の一実施例
を、図面を用いて具体的に説明する。図1は、本発明の
蒸気タービン静翼の一実施例としての蒸気タービン低圧
段静翼の断面図である。なお、本発明を示す実施例にお
いて、図3、図4で示す従来の蒸気タービン静翼と同一
部材については、同一符番を付して説明は省略した。
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS An embodiment of the steam turbine vane of the present invention will be specifically described below with reference to the drawings. FIG. 1 is a cross-sectional view of a steam turbine low-pressure stage vane as an example of the steam turbine vane of the present invention. In the embodiment showing the present invention, the same members as those of the conventional steam turbine vane shown in FIGS. 3 and 4 are designated by the same reference numerals and their description is omitted.

【0009】図において、静翼2の外周側には、翼根リ
ング1の内周側が肉盛溶接7によって固着されており、
一方、静翼2の内周側には、第1のシュラウド3の外周
側が溶接7によって固着されている。第2のシュラウド
4は、外周面に凹溝8が円周方向に形成されており、こ
れに遊嵌される第1のシュラウド3を、半径方向に移動
自在に支持できる構造にされている。また、ゴムボルト
5は、中央部分がゴム材等の弾性素材で形成され、ゴム
材に対向して2本の金属製のボルトが結合されている。
そして、ゴムボルト5の一方の側に結合されたボルト
は、第1のシュラウド3の内周に穿設された雌螺に螺合
されるとともに、他方の側に結合されたボルトは、第2
のシュラウド4の凹溝8の底部を貫通して、ナット6で
締め付けられ、第2のシュラウド4と連結される。
In the figure, the inner peripheral side of the blade root ring 1 is fixed to the outer peripheral side of the stationary blade 2 by overlay welding 7.
On the other hand, the outer peripheral side of the first shroud 3 is fixed to the inner peripheral side of the stationary blade 2 by welding 7. The second shroud 4 has a groove 8 formed in the outer peripheral surface in the circumferential direction, and has a structure capable of supporting the first shroud 3 loosely fitted therein in a freely movable manner in the radial direction. The rubber bolt 5 has a central portion formed of an elastic material such as a rubber material, and two metal bolts are joined to face the rubber material.
Then, the bolt connected to one side of the rubber bolt 5 is screwed into a female screw formed in the inner circumference of the first shroud 3, and the bolt connected to the other side is the second screw.
The shroud 4 penetrates the bottom of the groove 8 and is fastened with the nut 6 to be connected to the second shroud 4.

【0010】このように、蒸気タービンの低圧段に使用
される長大静翼において、静翼2を固定するシュラウド
を、2分割された第1のシュラウド3、および第2のシ
ュラウド4として、それらをゴムボルト5を介して固定
することによって、静翼2はゴムボルトで固定されてい
る状態となる。これにより、ゴムボルト5のゴム自体の
大きな減衰効果が、静翼2に作用することとなり、静翼
2が低圧段の蒸気の流れによって励振され、振動しよう
としても、ゴム自体の大きな減衰効果によって、その振
動が抑制され、振動が大きくなることが防止され、静翼
2が振動により破損するようなことはなくなり、信頼性
が向上する。
As described above, in the long and large stationary blade used in the low pressure stage of the steam turbine, the shroud for fixing the stationary blade 2 is divided into two, that is, the first shroud 3 and the second shroud 4, which are divided into two parts. By fixing via the rubber bolts 5, the stationary blade 2 is in a state of being fixed by the rubber bolts. As a result, the large damping effect of the rubber itself of the rubber bolt 5 acts on the stationary blade 2, and even if the stationary blade 2 is excited by the flow of steam in the low pressure stage and tries to vibrate, the large damping effect of the rubber itself causes The vibration is suppressed, the vibration is prevented from becoming large, the vane 2 is not damaged by the vibration, and the reliability is improved.

【0011】以上、本発明の蒸気タービン静翼の一実施
例について説明したが、本発明はこのような、実施例に
限定されるものではなく、特許請求の範囲に記載された
技術的範囲のものを含むものである。すなわち、上述し
た実施例において、第1のシュラウド3と第2のシュラ
ウド4の間に介装される弾性体をゴムボルト5とした
が、その他の弾性体、例えばゴム軸継手、又は金属ばね
継手と同様な、弾性を介装した継手で、第1のシュラウ
ド3と第2のシュラウド4を結合するようにしても良い
ものである。
Although one embodiment of the steam turbine stationary blade of the present invention has been described above, the present invention is not limited to such an embodiment, and is within the technical scope described in the claims. It includes things. That is, in the above-described embodiment, the elastic body interposed between the first shroud 3 and the second shroud 4 is the rubber bolt 5, but other elastic bodies such as a rubber shaft joint or a metal spring joint are used. It is also possible to connect the first shroud 3 and the second shroud 4 with a similar elastic joint.

【0012】[0012]

【発明の効果】以上説明したように、本発明の蒸気ター
ビン静翼によれば、特許請求の範囲に示す構成により、
蒸気タービンの低圧段に使用される剛性の小さい長大静
翼においても、蒸気力による振動を低減することがで
き、静翼が破損するという不適合事象を排除できる。ま
た、弾性体を介装することによる他の利点、例えば蒸気
タービン静翼の軸心の狂いが生じた場合においても、過
大な応力の発生を防止することができるものである。
As described above, according to the steam turbine vane of the present invention, the structure shown in the claims provides
Even in a large-sized stationary vane with low rigidity used in a low-pressure stage of a steam turbine, vibration due to steam force can be reduced, and a nonconforming event of vane damage can be eliminated. Further, it is possible to prevent the occurrence of excessive stress even when another advantage due to the elastic body being interposed, for example, when the axis of the steam turbine stationary blade is deviated.

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

【図1】本発明の蒸気タービン静翼の一実施例としての
蒸気タービン低圧段の静翼の断面図、
FIG. 1 is a cross-sectional view of a steam turbine low-pressure stage stator blade as an embodiment of a steam turbine stator blade of the present invention,

【図2】図1に示すシュラウドの詳細を示す斜視図、FIG. 2 is a perspective view showing details of the shroud shown in FIG.

【図3】従来の低圧段静翼を示す側面図、FIG. 3 is a side view showing a conventional low pressure stage stationary blade,

【図4】図3に示すシュラウド部の斜視図である。FIG. 4 is a perspective view of the shroud portion shown in FIG. 3.

【符号の説明】[Explanation of symbols]

1 翼根リング 2 静翼 3 第1のシュラウド 4 第2のシュラウド 5 ゴムボルト 6 ナット 7 肉盛溶接 8 凹溝 1 blade root ring 2 stationary blade 3 first shroud 4 second shroud 5 rubber bolt 6 nut 7 build-up welding 8 concave groove

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】 外周端が翼根リングに固定され、内周端
がシュラウドに固定され、蒸気タービンの低圧段に設置
された長大静翼を具える蒸気タービン静翼において、前
記シュラウドを前記長大静翼の内周端に固着する第1の
シュラウドと、前記第1のシュラウドと弾性体を介装し
て結合された第2のシュラウドで構成したことを特徴と
する蒸気タービン静翼。
1. A steam turbine stationary vane having an outer peripheral end fixed to a blade root ring, an inner peripheral end fixed to a shroud, and a long stationary vane installed in a low pressure stage of a steam turbine. A steam turbine stationary blade comprising a first shroud fixed to an inner peripheral end of the stationary blade and a second shroud coupled to the first shroud via an elastic body.
JP8248395A 1995-04-07 1995-04-07 Steam turbine stationary blade Withdrawn JPH08284607A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP8248395A JPH08284607A (en) 1995-04-07 1995-04-07 Steam turbine stationary blade

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP8248395A JPH08284607A (en) 1995-04-07 1995-04-07 Steam turbine stationary blade

Publications (1)

Publication Number Publication Date
JPH08284607A true JPH08284607A (en) 1996-10-29

Family

ID=13775768

Family Applications (1)

Application Number Title Priority Date Filing Date
JP8248395A Withdrawn JPH08284607A (en) 1995-04-07 1995-04-07 Steam turbine stationary blade

Country Status (1)

Country Link
JP (1) JPH08284607A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2002180802A (en) * 2000-12-11 2002-06-26 Mitsubishi Heavy Ind Ltd Stationary blade in steam turbine
JP2007255224A (en) * 2006-03-20 2007-10-04 Mitsubishi Heavy Ind Ltd Turbine blade and gas turbine
CN102207093A (en) * 2010-03-29 2011-10-05 株式会社日立制作所 Compressor
JP2014114734A (en) * 2012-12-07 2014-06-26 Mitsubishi Heavy Ind Ltd Turbine blade and turbine
JP2019055408A (en) * 2017-09-19 2019-04-11 三菱重工業株式会社 Member joining method and turbine component
KR20200040835A (en) * 2017-09-19 2020-04-20 미츠비시 히타치 파워 시스템즈 가부시키가이샤 Method for manufacturing turbine blade, and turbine blade

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2002180802A (en) * 2000-12-11 2002-06-26 Mitsubishi Heavy Ind Ltd Stationary blade in steam turbine
JP2007255224A (en) * 2006-03-20 2007-10-04 Mitsubishi Heavy Ind Ltd Turbine blade and gas turbine
CN102207093A (en) * 2010-03-29 2011-10-05 株式会社日立制作所 Compressor
US9534613B2 (en) 2010-03-29 2017-01-03 Mitsubishi Hitachi Power Systems, Ltd. Compressor
JP2014114734A (en) * 2012-12-07 2014-06-26 Mitsubishi Heavy Ind Ltd Turbine blade and turbine
JP2019055408A (en) * 2017-09-19 2019-04-11 三菱重工業株式会社 Member joining method and turbine component
KR20200040835A (en) * 2017-09-19 2020-04-20 미츠비시 히타치 파워 시스템즈 가부시키가이샤 Method for manufacturing turbine blade, and turbine blade
CN111094721A (en) * 2017-09-19 2020-05-01 三菱日立电力系统株式会社 Method for manufacturing turbine blade and turbine blade
US11371353B2 (en) 2017-09-19 2022-06-28 Mitsubishi Heavy Industries, Ltd. Manufacturing method for turbine blade, and turbine 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: 20020702