JPH0523014U - Blade turbine shroud clearance determination device for steam turbine - Google Patents

Blade turbine shroud clearance determination device for steam turbine

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Publication number
JPH0523014U
JPH0523014U JP077093U JP7709391U JPH0523014U JP H0523014 U JPH0523014 U JP H0523014U JP 077093 U JP077093 U JP 077093U JP 7709391 U JP7709391 U JP 7709391U JP H0523014 U JPH0523014 U JP H0523014U
Authority
JP
Japan
Prior art keywords
gap
laser
light
steam turbine
value
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Withdrawn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
JP077093U
Other languages
Japanese (ja)
Inventor
朝春 松尾
慎也 井上
善幸 後藤
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 JP077093U priority Critical patent/JPH0523014U/en
Publication of JPH0523014U publication Critical patent/JPH0523014U/en
Withdrawn legal-status Critical Current

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Abstract

(57)【要約】 【目的】 3/100mm未満の間隙値でも計測可能と
し、また間隙の適、不適の判定を容易かつ確実に行い、
これにより人的検査による計測差を生ずる等の不都合を
除去する。 【構成】 蒸気タービン動翼10のシュラウド11間の
間隙Cに対向して投光器3を配置し、レーザ発振装置1
のレーザダイオード2(発振用電力を供給する電源装置
4に接続されている)からのレーザ光を該投光器3から
投光Aとして照射する。その反射光Bをレーザ検出装置
5のフォトダイオード6により受光して起電力として捉
え、該フォトダイオード6に設定しておいた設定値以上
の場合には表示器7の判定部9のランプを点灯させると
共に、表示部8で数値表示等を行なうことにより、間隙
の存在の把握及びその間隙値の適、不適を判定する。
(57) [Summary] [Purpose] It is possible to measure even gap values of less than 3/100 mm, and it is possible to easily and reliably determine whether the gap is suitable or not.
This eliminates inconveniences such as a measurement difference caused by a human inspection. A laser projector 1 is provided with a projector 3 arranged to face a gap C between shrouds 11 of a steam turbine rotor blade 10.
The laser light from the laser diode 2 (connected to the power supply device 4 for supplying the oscillation power) is emitted from the light projector 3 as the light projection A. The reflected light B is received by the photodiode 6 of the laser detection device 5 and is regarded as an electromotive force. The presence of the gap is grasped and whether the gap value is suitable or not is determined by displaying the numerical value or the like on the display unit 8.

Description

【考案の詳細な説明】[Detailed description of the device]

【0001】[0001]

【産業上の利用分野】[Industrial applications]

本考案は、蒸気タービンの動翼外径部側に設けられるシュラウド間の間隙値を 計測し、その間隙値の適、不適を判定する蒸気タービンの翼シュラウド間隙判定 装置に関する。 The present invention relates to a blade shroud clearance determination device for a steam turbine, which measures a clearance value between shrouds provided on the outer diameter side of a moving blade of a steam turbine and determines whether the clearance value is appropriate or not.

【0002】[0002]

【従来の技術】[Prior Art]

一般に、蒸気タービンの動翼外径部側には、各翼間の間隙を正しく保持すると ともに、動翼が遠心力で飛出すのを防止し、かつ固有振動数を高めて耐震強度を 増すために、シュラウドが取付けられる。 Generally, on the outer diameter side of the moving blades of a steam turbine, the clearance between the blades is properly maintained, the rotating blades are prevented from flying out by centrifugal force, and the natural frequency is increased to increase the seismic strength. A shroud is attached to the.

【0003】 このシュラウドとしては、例えば、複数個の動翼を一組として、その動翼の頂 部に設けた断面円形又は長方形の突起(テノンと称されている)を介して取付け た後、かしめて結合したものや、インテグラルシュラウド翼のように、動翼と一 体に削り出してテノンを省略したものなどがある。As this shroud, for example, a plurality of moving blades are set as a set, and after being attached through a projection (referred to as Tenon) having a circular or rectangular cross section provided at the top of the moving blades, There are those that are caulked and combined, and those that have been machined together with the rotor blade and have the tenon omitted, such as integral shroud blades.

【0004】 このようなシュラウドにおいて、互いに隣接するシュラウド間に形成される間 隙は、強度上極めて重要であり、大きすぎても、小さすぎても翼に何等かの影響 を与えて翼損傷等の事故を惹起するものである。従来は、このように重要なシュ ラウド間の間隙を、検査員がスキミゲージを該間隙に入れて計測するのが一般的 である。In such a shroud, the gap formed between the shrouds adjacent to each other is extremely important in terms of strength, and even if it is too large or too small, it has some influence on the blade to cause blade damage or the like. Cause an accident. Conventionally, it is common for an inspector to measure a gap between such important shrouds by inserting a skim gauge into the gap.

【0005】[0005]

【考案が解決しようとする課題】[Problems to be solved by the device]

ところが、このようなスキミゲージによる検査では、間隙値が3/100mm以 上の場合には検出可能であるが、3/100mm未満であると、人間の手によって は計測できず、記録の採取もできない。したがって、従来は、3/100mm未満 の間隙にあっては、定量的に把握することができず、間隙の適、不適の判定が行 なえない。また、人的検査であるため検査員毎に計測差が生じ、信頼性に欠ける 不具合がある。 However, in the inspection using such a skim gauge, it is possible to detect when the gap value is 3/100 mm or more, but when it is less than 3/100 mm, it is not possible to measure it by human hands and it is not possible to collect records. .. Therefore, conventionally, if the gap is less than 3/100 mm, it cannot be quantitatively grasped, and it cannot be judged whether the gap is suitable or not. In addition, since it is a human inspection, there is a problem of lack of reliability due to measurement differences between inspectors.

【0006】 本考案は、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、3/ 100mm未満の間隙値でも計測可能であり、また間隙の適、不適の判定が容易か つ確実に行え、これにより人的検査による計測差を生ずる等の不都合を除去して 、計測値の信頼性を高めてタービン品質の向上に寄与することができる蒸気ター ビンの翼シュラウド間隙判定装置を提供することを目的とする。The present invention has been made in order to solve the problems of the prior art, and can measure a gap value of less than 3/100 mm, and it is easy and reliable to determine whether the gap is suitable or not. A blade turbine shroud clearance determination device for steam turbines that can improve the reliability of measurement values and contribute to the improvement of turbine quality by eliminating inconveniences such as measurement differences due to human inspection. The purpose is to do.

【0007】[0007]

【課題を解決するための手段】[Means for Solving the Problems]

上記の課題を解決するために、本考案に係る蒸気タービンの翼シュラウド間隙 判定装置は、蒸気タービンの動翼外径部側に設けられるシュラウド間の間隙にレ ーザ光を照射するレーザ発振装置と、前記シュラウドからの反射光又は通過光を 受光するレーザ検出装置とを備え、該レーザ検出装置は、受光した光量を電力に 変換して前記シュラウド間の間隙値を表示する表示部と、その検出した間隙値の 、設定値に対応する適、不適をランプ表示するランプ判定部とを有してなる。 In order to solve the above-mentioned problems, a blade shroud clearance determination device for a steam turbine according to the present invention is a laser oscillator that irradiates laser light to the clearance between shrouds provided on the outer diameter side of a moving blade of a steam turbine. And a laser detecting device for receiving reflected light or passing light from the shroud, the laser detecting device converting the received light amount into electric power and displaying the gap value between the shrouds, and A lamp determination unit that lamp-displays whether the detected gap value is suitable or not corresponding to the set value.

【0008】[0008]

【作用】[Action]

レーザ光は周波数が高く、小さな反射効果等を拡大して測定することができる とともに、波長が短く極めて高い分解能の測定ができ、しかも波長が可視光領域 にある。 Laser light has a high frequency and can be used to magnify small reflection effects and other measurements, and also has a short wavelength for extremely high resolution measurement, and its wavelength is in the visible light range.

【0009】 したがって、上記の手段のように、レーザダイオード等のレーザ発振装置でシ ュラウド間の間隙にレーザ光を投光するとともに、フォトダイオード等のレーザ 検出装置によりその反射光又は間隙通過光を受光して起電力として捉えるように すれば、例えばフォトダイオードに設定しておいた設定値以上の場合には判定部 のランプを点灯させるなどによって間隙の存在の把握及びその間隙値の適、不適 の判定が可能となる。Therefore, as in the above means, a laser oscillator such as a laser diode projects laser light into the gap between the shrouds, and a laser detector such as a photodiode detects reflected light or light passing through the gap. If it is detected as an electromotive force by receiving light, for example, when the value is above the preset value set for the photodiode, the lamp in the judgment unit is turned on to detect the existence of the gap and determine whether the gap value is appropriate or not. Can be determined.

【0010】 よって、このような手段によれば、従来定量的に計測できなかった3/100 mm未満の間隙もレーザ光の利用によって計測可能となり、また間隙の適性判定も 容易に行えるようになる。しかも、人的検査による検査員の計測差を生ずる等の 不具合も除去でき、計測値の信頼性を一段と高めることができ、タービン品質の 向上に寄与できるようになる。なお、設定値を変えることにより間隙の大きさを 判定させることができる。Therefore, with such a means, it becomes possible to measure a gap of less than 3/100 mm, which could not be quantitatively measured in the past, by using laser light, and it is possible to easily determine the suitability of the gap. .. In addition, it is possible to eliminate problems such as measurement differences among inspectors due to human inspection, further improve the reliability of measured values, and contribute to the improvement of turbine quality. The size of the gap can be determined by changing the set value.

【0011】[0011]

【実施例】【Example】

以下、図1を参照して本考案の一実施例について詳細に説明する。本実施例で は、レーザ光を照射するレーザ発振装置1が、単光色の可干渉性で強力な細いレ ーザ光線を発振するレーザダイオード(半導体レーザ発振器)2と、このレーザ ダイオード2に接続された投光器3とを備えた構成とされている。レーザダイオ ード2は、電源装置4に接続され、この電源装置4から発振用電力の供給を受け るようになっている。また、投光器3は、自身からの投光Aの反射光Bを受光す る受光機能を兼備しており、その反射光Bはレーザ検出装置5に入光するように なっている。 Hereinafter, an embodiment of the present invention will be described in detail with reference to FIG. In this embodiment, a laser oscillating device 1 for irradiating a laser beam is composed of a laser diode (semiconductor laser oscillator) 2 for oscillating a thin laser beam having a single-color coherent and strong power, and the laser diode 2. The projector 3 is connected to the projector 3. The laser diode 2 is connected to a power supply device 4 and receives power for oscillation from the power supply device 4. The projector 3 also has a light receiving function of receiving the reflected light B of the projected light A from itself, and the reflected light B enters the laser detection device 5.

【0012】 このレーザ検出装置5は、受光した光量を電力に変換するフォトダイオード( 半導体ダイオード検出器)6と、このフォトダイオード6に接続された表示器7 とを有し、表示器7は、検出電力に応じてシュラウド間の間隙値を演算する演算 部と、その間隙値を表示する表示部8と、その検出した間隙値の、設定値に対応 する適、不適をランプ表示するランプ判定部9とを有する構成とされている。な お、フォトダイオード6の設定値を変えることによって、計測する間隙の大きさ の判定値を調整できるようになっている。This laser detection device 5 has a photodiode (semiconductor diode detector) 6 for converting the amount of received light into electric power, and a display 7 connected to this photodiode 6, and the display 7 is A calculation unit that calculates the gap value between the shrouds according to the detected power, a display unit 8 that displays the gap value, and a lamp determination unit that lamp-displays whether the detected gap value corresponds to the set value or not. 9 and 9. The judgment value of the size of the gap to be measured can be adjusted by changing the set value of the photodiode 6.

【0013】 さて、蒸気タービン動翼10のシュラウド11間の間隙Cを計測する場合には 、図1に示すように、該間隙Cに対向して投光器3を配置して投光Aを出射し、 その反射光Bをフォトダイオード6に入射させる。レーザ光は周波数が高く、小 さな反射効果等を拡大して測定することができるとともに、波長が短く極めて高 い分解能の測定ができ、しかも波長が可視光領域にある。When measuring the clearance C between the shrouds 11 of the steam turbine rotor blade 10, as shown in FIG. 1, the projector 3 is arranged so as to face the clearance C, and the projection A is emitted. The reflected light B is incident on the photodiode 6. Laser light has a high frequency and can be used to magnify small reflection effects and other measurements. It also has a short wavelength and enables measurement with extremely high resolution, and the wavelength is in the visible light range.

【0014】 本実施例によれば、レーザダイオード2から投光器3を介してシュラウド11 間の間隙Cにレーザ光の投光Aを出射するとともに、フォトダイオード6により 反射光Bを受光して起電力として捉えるようにしたので、フォトダイオード6に 設定しておいた設定値以上の場合にはランプ判定部9のランプを点灯させるとと もに、表示部8で数値表示等を行なうことにより、間隙の存在の把握及びその間 隙値の適、不適の判定が可能となる。According to this embodiment, the laser diode 2 emits the laser light projection A through the projector 3 to the gap C between the shrouds 11, and the photodiode 6 receives the reflected light B to generate an electromotive force. Therefore, when the value is equal to or more than the set value set in the photodiode 6, the lamp of the lamp determination unit 9 is turned on, and the numerical value is displayed on the display unit 8 to display the gap. It becomes possible to grasp the existence of the and the appropriateness of the space value.

【0015】 したがって、従来定量的に計測できなかった3/100mm未満の間隙もレーザ 光の利用によって計測可能となり、また間隙の適性判定も容易に行えるようにな る。しかも、人的検査による検査員の計測差を生ずる等の不具合も除去でき、計 測値の信頼性を一段と高めることができ、タービン品質の向上に寄与できるよう になる。Therefore, it becomes possible to measure the gap of less than 3/100 mm, which could not be quantitatively measured in the past, by using the laser beam, and the suitability of the gap can be easily determined. In addition, it is possible to eliminate problems such as differences in measurement by inspectors due to human inspection, further improve reliability of measurement values, and contribute to improvement of turbine quality.

【0016】 なお、上記の実施例では、反射光を検出するようにしたが、通過光を検出する ようにしてもよい。In the above embodiment, the reflected light is detected, but the passing light may be detected.

【0017】[0017]

【考案の効果】[Effect of the device]

以上述べたように、本考案によれば、従来定量的に計測できなかった3/10 0mm未満の間隙もレーザ光の利用によって計測可能となり、また間隙の適性判定 も容易に行えるようになり、しかも人的検査による検査員の計測差を生ずる等の 不具合も除去でき、計測値の信頼性を一段と高めることができ、タービン品質の 向上に寄与できるようになる等、優れた効果が奏される。 As described above, according to the present invention, it becomes possible to measure a gap of less than 3/100 mm, which could not be quantitatively measured in the past, by using laser light, and it becomes possible to easily determine the suitability of the gap. Moreover, it is possible to eliminate defects such as measurement differences among inspectors due to human inspection, further improve the reliability of measurement values, and contribute to the improvement of turbine quality. ..

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

【図1】本考案の一実施例に係る蒸気タービンの翼シュ
ラウド間隙判定装置を示す構成図である。
FIG. 1 is a configuration diagram showing a blade shroud clearance determining device for a steam turbine according to an embodiment of the present invention.

【符号の説明】 1 レーザ発振装置 2 レーザダイオード 3 投光器 4 電源装置 5 レーザ検出装置 6 フォトダイオード 7 表示器 8 表示部 9 ランプ判定部 10 蒸気タービン動翼 11 シュラウド A 投光 B 反射光 C 間隙[Explanation of Codes] 1 laser oscillation device 2 laser diode 3 light projector 4 power supply device 5 laser detection device 6 photo diode 7 display device 8 display unit 9 lamp determination unit 10 steam turbine blade 11 shroud A light projection B reflected light C gap

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 【請求項1】蒸気タービンの動翼外径部側に設けられる
シュラウド間の間隙にレーザ光を照射するレーザ発振装
置と、前記シュラウドからの反射光又は通過光を受光す
るレーザ検出装置とを備え、該レーザ検出装置は、受光
した光量を電力に変換して前記シュラウド間の間隙値を
表示する表示部と、その検出した間隙値の、設定値に対
応する適、不適をランプ表示するランプ判定部とを有す
ることを特徴とする蒸気タービンの翼シュラウド間隙判
定装置。
1. A laser oscillating device for irradiating a gap between shrouds provided on the outer diameter side of a moving blade of a steam turbine with laser light, and a laser detecting device for receiving reflected light or passing light from the shroud. The laser detecting device converts an amount of received light into electric power to display a gap value between the shrouds, and a lamp determination for indicating whether or not the detected gap value corresponds to a set value by a lamp. And a blade shroud clearance determining device for a steam turbine.
JP077093U 1991-08-30 1991-08-30 Blade turbine shroud clearance determination device for steam turbine Withdrawn JPH0523014U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP077093U JPH0523014U (en) 1991-08-30 1991-08-30 Blade turbine shroud clearance determination device for steam turbine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP077093U JPH0523014U (en) 1991-08-30 1991-08-30 Blade turbine shroud clearance determination device for steam turbine

Publications (1)

Publication Number Publication Date
JPH0523014U true JPH0523014U (en) 1993-03-26

Family

ID=13624172

Family Applications (1)

Application Number Title Priority Date Filing Date
JP077093U Withdrawn JPH0523014U (en) 1991-08-30 1991-08-30 Blade turbine shroud clearance determination device for steam turbine

Country Status (1)

Country Link
JP (1) JPH0523014U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2007010656A (en) * 2005-06-27 2007-01-18 General Electric Co <Ge> Clearance measurement system and operation method
WO2020202363A1 (en) * 2019-03-29 2020-10-08 平田機工株式会社 Mounting device

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2007010656A (en) * 2005-06-27 2007-01-18 General Electric Co <Ge> Clearance measurement system and operation method
WO2020202363A1 (en) * 2019-03-29 2020-10-08 平田機工株式会社 Mounting device
JPWO2020202363A1 (en) * 2019-03-29 2020-10-08
US11491591B2 (en) 2019-03-29 2022-11-08 Hirata Corporation Attachment device

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