JPS6198927A - Automatic inspector for gas turbine generator - Google Patents

Automatic inspector for gas turbine generator

Info

Publication number
JPS6198927A
JPS6198927A JP59218559A JP21855984A JPS6198927A JP S6198927 A JPS6198927 A JP S6198927A JP 59218559 A JP59218559 A JP 59218559A JP 21855984 A JP21855984 A JP 21855984A JP S6198927 A JPS6198927 A JP S6198927A
Authority
JP
Japan
Prior art keywords
gas turbine
lubricating oil
detector
output
temperature
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.)
Pending
Application number
JP59218559A
Other languages
Japanese (ja)
Inventor
Hideya Uno
宇野 秀也
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 Electric Corp
Original Assignee
Mitsubishi Electric Corp
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 Electric Corp filed Critical Mitsubishi Electric Corp
Priority to JP59218559A priority Critical patent/JPS6198927A/en
Publication of JPS6198927A publication Critical patent/JPS6198927A/en
Pending legal-status Critical Current

Links

Classifications

    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K9/00Arrangements for cooling or ventilating
    • H02K9/24Protection against failure of cooling arrangements, e.g. due to loss of cooling medium or due to interruption of the circulation of cooling medium
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16NLUBRICATING
    • F16N29/00Special means in lubricating arrangements or systems providing for the indication or detection of undesired conditions; Use of devices responsive to conditions in lubricating arrangements or systems
    • F16N29/04Special means in lubricating arrangements or systems providing for the indication or detection of undesired conditions; Use of devices responsive to conditions in lubricating arrangements or systems enabling a warning to be given; enabling moving parts to be stopped
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16NLUBRICATING
    • F16N39/00Arrangements for conditioning of lubricants in the lubricating system
    • F16N39/02Arrangements for conditioning of lubricants in the lubricating system by cooling

Abstract

PURPOSE:To continue monitoring under abnormal operation of cooling unit by detecting the abnormality of lubricant cooler in gas turbine generator through comparison between the inlet/outlet temperature of lubricant to be fed to the bearing and a referential level. CONSTITUTION:A gas turbine 1 to be coupled coaxially, inlet temperature thetaI detector 9 of lubricant to be fed to the bearings of reduction gear 2 and generator 3 and outlet temperature thetaO detector 10 of lubricant discharged from the bearing are provided. The outputs from said detectors 9, 10 are fed together with the signals from gas turbine output KW detector 11, room temperature thetaA detector 12 and a gas turbine operating condition contact signal 13 to an operational controller 16 through an input unit 14. Said controller 16 will operate the degree (alpha) (=thetaI-thetaA/thetaO-thetaI) of performance degradation under abnormality and compare with the degree (alphan) under normal condition, and if alpha>alphan, it is decided that the lubricant cooler 5 is abnormal. Said degree (alpha) is set while being corrected by gas turbine output KW.

Description

【発明の詳細な説明】 〔産業上の利用分野〕 この発明はガスタービン(以下GTと略す)を潤滑油に
よって冷却する場合の冷却器以上を検出するガスタービ
ン発電装置の自動点検装置に関するものである。
[Detailed Description of the Invention] [Industrial Application Field] The present invention relates to an automatic inspection device for a gas turbine power generator that detects a cooler or higher temperature when a gas turbine (hereinafter abbreviated as GT) is cooled by lubricating oil. be.

〔従来の技術〕[Conventional technology]

従来この種の装置として実施例は見当らなく、かつ、こ
の発明の如く冷却器の性能低下を直接、定量的に把握す
ること自動点検は実施されていない。
Conventionally, no examples of this type of device have been found, and automatic inspection to directly and quantitatively grasp the deterioration in the performance of the cooler as in the present invention has not been carried out.

〔発明が解決しようとする問題点〕[Problem that the invention seeks to solve]

従来は潤滑油冷却器の異常を定量的に検出する手段がな
かったために冷却器フィンの汚損や冷却ファン、換気フ
ァン等が性能の低下を来たすとそれが原因となって冷却
器の性能低下を招きガスタービン発電装置の各軸受部に
供給する潤滑油の油温か上昇する。そのため軸受部は温
度が上昇し、軸受の性能に悪い影響を与える他、軸受保
護装置が誤動作するという問題点があった。
Previously, there was no way to quantitatively detect abnormalities in the lubricating oil cooler, so if the cooler fins were dirty or the performance of the cooling fan, ventilation fan, etc. deteriorated, this could cause a decline in the cooler's performance. As a result, the temperature of the lubricating oil supplied to each bearing of the gas turbine generator increases. As a result, the temperature of the bearing increases, which has a negative effect on the performance of the bearing, and also causes the bearing protection device to malfunction.

この発明はかかる問題点を解決するためになされたもの
で、ガスタービン発電装置の各部軸受に供給される潤滑
油の入口側温度と出口側温度、あるいは、室内温度やガ
スタービン出力等から発電器動作中の冷却器の実際の性
能と理論上得られた正電時の性能とを演算し比較するこ
とによシ潤滑油冷却器に異常が発生すると直ちにこれを
捕え、事故発生前にガスタービン発電装置の潤滑油冷却
器異常を予見することができるガスタービン発電装置の
自動点検装置を提供することを目的としている。
This invention was made to solve this problem, and the generator is based on the inlet and outlet temperatures of the lubricating oil supplied to the bearings of each part of the gas turbine generator, or the indoor temperature and gas turbine output. By calculating and comparing the actual performance of the operating cooler with the theoretically obtained performance at positive voltage, we can immediately catch any abnormality in the lubricating oil cooler and prevent it from occurring in the gas turbine before an accident occurs. It is an object of the present invention to provide an automatic inspection device for a gas turbine power generation device that can predict abnormalities in the lubricating oil cooler of the power generation device.

〔問題点を解決するだめの手段〕[Failure to solve the problem]

この発明に係るガスタービン発電装置の自動点検装置は
ガスタービン発電装置の各軸受部に供給される潤滑油の
入口温度検出器と出口温度検出器1ガスタービン出力検
出器及び室内温度検出器等からの各検出データ、並びに
ガスタービン運転状態の接点信号とを入力信号として入
力装置に与え、記憶装置と演算装置とによって正常値と
比較演算したガスタービン発電装置の各潤滑油冷却器の
自動点検結果を出力装置を介して外部に出力し補助リレ
ー、表示装置等を作動させるようにしたものである。
The automatic inspection device for a gas turbine power generator according to the present invention includes an inlet temperature detector and an outlet temperature detector for lubricating oil supplied to each bearing of the gas turbine power generator, a gas turbine output detector, an indoor temperature detector, etc. The automatic inspection results of each lubricating oil cooler of the gas turbine power generator are calculated by applying the detected data and the contact signal of the gas turbine operating state to the input device as input signals, and comparing and calculating the normal values with the storage device and the calculation device. is output to the outside via an output device to operate an auxiliary relay, display device, etc.

〔作用〕[Effect]

この発明においては正常運転時のガスタービン発電装置
の各軸受部に供給される潤滑油の入出力温度を予め計測
し、被比較データとして記憶装置に格納しであるので、
−潤滑油冷却器異常の運転中の監視は連続的に行われ、
かつ、前記記憶データに上下限の判定幅を持たせること
によシ異常の判定格成を任意に設定できるものである。
In this invention, the input and output temperatures of the lubricating oil supplied to each bearing part of the gas turbine generator during normal operation are measured in advance and stored in the storage device as data to be compared.
- Monitoring of lubricating oil cooler abnormalities during operation is carried out continuously;
Moreover, by providing upper and lower judgment limits to the stored data, the judgment criteria for abnormality can be arbitrarily set.

〔実施例〕〔Example〕

以下この発明の一実施例を図について説明する。 An embodiment of the present invention will be described below with reference to the drawings.

第1図はガスタービン発電装置の潤滑油供給系銃声 図を示したもので、図において1はガスタービン、2は
そのガスタービン1の回転を減速して発電機3に動力を
伝達する減速機、4はガスタービン1゜減速機22発信
1機3を機械的に接続する出力軸、5は潤滑油冷却器、
6は潤滑油槽、7は潤滑油配管、8は潤滑油冷却器用冷
却ファン、9は軸受への潤滑油入口温度(θ■)検出器
、10は軸受からのτ岡滑油出口温度(eo)検出器、
11はガスタービン出力(席)検出器、12は室内温度
(θA)検出器である。また、第2図は自動点検装置の
構成を示したもので、13はガスタービン運転状態接点
信号、14は入力装置、15は第3図に示す論理判断や
演算を実行するためのプログラムや入力データ。
FIG. 1 shows a gunshot diagram of the lubricating oil supply system of a gas turbine power generator. In the figure, 1 is a gas turbine, and 2 is a speed reducer that reduces the rotation of the gas turbine 1 and transmits power to the generator 3. , 4 is an output shaft that mechanically connects the gas turbine 1° reducer 22 transmitter 3, 5 is a lubricating oil cooler,
6 is a lubricating oil tank, 7 is a lubricating oil pipe, 8 is a cooling fan for a lubricating oil cooler, 9 is a lubricating oil inlet temperature to the bearing (θ■) detector, 10 is a τOka oil outlet temperature from the bearing (eo) Detector,
11 is a gas turbine output (seat) detector, and 12 is an indoor temperature (θA) detector. In addition, Fig. 2 shows the configuration of the automatic inspection device, in which 13 is a gas turbine operating state contact signal, 14 is an input device, and 15 is a program and input for executing the logical judgments and calculations shown in Fig. 3. data.

演算結果等のデータを記憶する記憶装置、16は前記記
憶装置15に内蔵されたプログラムに従って先の入力装
置14からのデータを取入れ、論理判断や演算を実行し
、その結果を記憶装置15や出力装置1Tに出力する演
算制御装置、1Tは前記の演算制御装置16によシ判断
されるガスタービン発電装置潤滑油冷却器異常の点検結
果を外部の補助リレー18や表示装置19へ出力可能な
信号に変換する出力装置、18は出力装置17の出力内
容に従って動作し、他の装置へ点検結果を伝達するだめ
の補助リレー、19は出力装置1γの出力内容に従って
点検結果を表示するための表示装置である。
A storage device 16 for storing data such as calculation results takes in data from the input device 14 according to a program built in the storage device 15, executes logical judgments and calculations, and stores the results in the storage device 15 or output. An arithmetic and control device that outputs to the device 1T, 1T is a signal capable of outputting the inspection result of the gas turbine generator lubricating oil cooler abnormality determined by the arithmetic and control device 16 to the external auxiliary relay 18 and display device 19. 18 is an auxiliary relay that operates according to the output contents of the output device 17 and transmits the inspection results to other devices; 19 is a display device for displaying the inspection results according to the output contents of the output device 1γ It is.

次に動作について説明する。まず潤滑油冷却器5のフィ
ンの汚損や潤滑油冷却用ファン8の能力低下等が発奮す
るとそれが原因となって潤滑油冷却器5の性能が低下す
る。この異常時の性能低下の度合αは各軸受に供給する
潤滑油入口温度(θl)検出器9と各軸受からの潤滑油
出口温度(θ0)検出θl−θA 器10及び室内温度(θA>検出器とよシ、α=e。−
01で表わすことができる。従って、これを正常時の性
能低下の度合αnと比較し、α〉αnで゛あると潤滑油
冷却器5に異常があることが判別できる。しかし、正常
時の性能低下の度合αnはガスタービン出力(席)検出
器11によってその値が異なシガスタービン出力(KW
)が大きい時には前記αnは小さく、また小さい時には
性能低下の度合αnは大きくなるため、αn = −A
 −’lli+ Bによシ補正される。但し、A、Bは
各ガスタービン発電装置ごとに各々異なった値となる定
数で、理論と実機テストによシ決定されるものである。
Next, the operation will be explained. First, when the fins of the lubricating oil cooler 5 become dirty or the performance of the lubricating oil cooling fan 8 deteriorates, the performance of the lubricating oil cooler 5 deteriorates. The degree of performance decline α during this abnormality is determined by the lubricant inlet temperature (θl) supplied to each bearing, the lubricant outlet temperature (θ0) detected from each bearing θl−θA, and the indoor temperature (θA>detected). Vessel toyoshi, α=e.−
It can be represented by 01. Therefore, this is compared with the degree of performance deterioration αn under normal conditions, and if α>αn, it can be determined that there is an abnormality in the lubricating oil cooler 5. However, the degree of performance deterioration αn during normal operation varies depending on the gas turbine output (KW) detector 11.
) is large, the above αn is small, and when it is small, the degree of performance deterioration αn is large, so αn = −A
-'lli+B is corrected. However, A and B are constants that have different values for each gas turbine generator, and are determined by theory and actual tests.

第3図は本装置の点検処理フローチャートを示したもの
で、点検処理はGT運転21により開始され、以下GT
運転終了27又は異常25発生(YES )まで周期的
に繰返される。
Figure 3 shows a flowchart of the inspection process of this device.The inspection process is started by GT operation 21, and hereinafter,
This is repeated periodically until the operation ends 27 or an abnormality 25 occurs (YES).

点検中は周期的に各種データを計測22し各軸受の潤滑
油入口温度(θI)検出器9.潤滑油出口温度(θ0)
検出器10.室内温度(θA)検出器12.ガスタービ
ン出力(猫)検出器11t−計測して基準値の算出23
にて性能低下の度合αの理論値αnを算出し、異常点検
処理24にて前記αを算出し、αとαnの比較を各軸受
対応に実施し、α〉αnであれば潤滑油冷却器5に異常
があると4−II断し、またα≦αnであれば正常であ
ると判断する。
During inspection, various data are periodically measured 22 and each bearing's lubricating oil inlet temperature (θI) detector 9. Lubricating oil outlet temperature (θ0)
Detector 10. Indoor temperature (θA) detector 12. Gas turbine output (cat) detector 11t - Measure and calculate reference value 23
The theoretical value αn of the degree of performance deterioration α is calculated at If 5 is abnormal, it is judged as 4-II, and if α≦αn, it is judged to be normal.

異常25発生(YES)の場合は異常内容を出力26で
処理を行い点検処理をし2γでGT運転終了とする。
If an abnormality 25 has occurred (YES), the contents of the abnormality are processed at the output 26, an inspection process is performed, and the GT operation is terminated at 2γ.

なお、上記実施例はガスタービン発電装置潤滑油冷却器
に関してのものであったが、ガスタービン発電装置以外
の各種回転機器潤滑油冷却器異常の自動点検においても
同様の効果を秦するものである。
Although the above embodiment was related to a lubricating oil cooler for a gas turbine power generator, the same effect can be achieved in automatic inspection of abnormalities in lubricating oil coolers of various rotating equipment other than gas turbine power generators. .

〔発明の効果〕〔Effect of the invention〕

以上のようにこの発明によればガスタービン発電装置潤
滑油冷却器の異常を軸受に供給される潤滑油の入口、出
口温度及び室内温度等を定号的に捕え、ガスタービンの
出力容量に応じて補正、fT。
As described above, according to the present invention, an abnormality in the lubricating oil cooler of a gas turbine power generation device can be detected based on the inlet and outlet temperatures, indoor temperature, etc. of the lubricating oil supplied to the bearings, and the abnormality can be determined according to the output capacity of the gas turbine. Correction, fT.

出した基準値と比較することにより潤滑油冷却器の異常
を点検するようにシステムを惜敗したので、ガスタービ
ン運転状態に対応して点検が可能となる他、自動化並び
にガスタービン発電装置の安定運転化が可能となる効果
がある。
The system was designed to check for abnormalities in the lubricating oil cooler by comparing it with the established standard values, which not only makes it possible to perform inspections according to the operating status of the gas turbine, but also improves automation and stable operation of the gas turbine generator. This has the effect of making it possible to

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

第1図はガスタービン発!装置の゛潤滑油供給系統図、
第2図は本発明の一実施例によるガスタービン発電装置
潤滑油冷却器異常自動点検装置の構成図、第3図は自動
点検゛処理フローチャートを示す。 1はガスタービン、2は減速機、3は発電機、5は潤滑
油冷却器、9は潤滑油入口温度(θI)検出器、10は
潤滑油出力温度(θ0)検出器、11はガスタービン出
力(曹)検出器、12は室内温度(0人)検出器、13
はガスタービン運転状態接点信号、14は入力装置、1
5は記憶装置、16は演算制御装置、17は出力装置、
18は補助リレー、19は表示装置。
Figure 1 is from the gas turbine! Equipment lubricating oil supply system diagram,
FIG. 2 is a block diagram of an automatic inspection system for abnormalities in a lubricating oil cooler of a gas turbine power generator according to an embodiment of the present invention, and FIG. 3 is a flowchart of automatic inspection processing. 1 is a gas turbine, 2 is a speed reducer, 3 is a generator, 5 is a lubricating oil cooler, 9 is a lubricating oil inlet temperature (θI) detector, 10 is a lubricating oil output temperature (θ0) detector, 11 is a gas turbine Output (Cold) detector, 12 is indoor temperature (0 person) detector, 13
is a gas turbine operating state contact signal, 14 is an input device, 1
5 is a storage device, 16 is an arithmetic control device, 17 is an output device,
18 is an auxiliary relay, and 19 is a display device.

Claims (3)

【特許請求の範囲】[Claims] (1)ガスタービン発電装置の要部軸受に供給される潤
滑油出、入口温度を検出する潤滑油出、入口温度検出器
と、前記ガスタービン発電装置のガスタービン出力を検
出するガスタービン出力検出器と、前記ガスタービン発
電装置の室内温度を検出する室内温度検出器と、前記潤
滑油出、入口温度検出器の出力信号、ガスタービン出力
検出器の出力信号、前記室内温度検出器の出力信号、並
びにガスタービン運転信号とを入力とする入力装置と、
前記入力装置への入力信号を収集しガスタービン発電装
置の要部軸受の正常、異常を所定の演算式に基いて自動
点検し判断する演算制御装置と、前記演算制御装置を介
して得た正常運転時の被比較データを格納する記憶装置
と、前記自動点検の結果を出力する出力装置と、前記出
力装置から出力される潤滑油温度を介した潤滑油冷却器
異常の有無を出力する補助リレー、及び表示装置とを備
えたガスタービン発電装置の自動点検装置。
(1) A lubricating oil outlet and an inlet temperature detector that detect the lubricating oil outlet and inlet temperature supplied to the main bearings of the gas turbine power generator, and a gas turbine output detector that detects the gas turbine output of the gas turbine power generator. an indoor temperature detector for detecting the indoor temperature of the gas turbine power generator, an output signal of the lubricating oil outlet and inlet temperature detector, an output signal of the gas turbine output detector, and an output signal of the indoor temperature detector. , and a gas turbine operation signal as inputs;
an arithmetic and control device that collects input signals to the input device and automatically inspects and determines whether the main bearings of the gas turbine generator are normal or abnormal based on a predetermined arithmetic formula; A storage device that stores comparison data during operation, an output device that outputs the results of the automatic inspection, and an auxiliary relay that outputs whether or not there is an abnormality in the lubricating oil cooler through the lubricating oil temperature output from the output device. , and a display device.
(2)前記演算制御装置におけるタービン発電装置の冷
却器異常判別の演算式を各軸受に供給する潤滑油入口温
度をΘ_I、同様に出力温度をΘ_O、室内温度をΘ_
Aとしたとき、Θ_I−Θ_A/Θ_O−Θ_I=αで
表わし、前記性能低下度合αの値を正常値と異常値とで
比較判別するようにしたことを特徴とする特許請求の範
囲第1項記載のガスタービン発電装置の自動点検装置。
(2) The arithmetic formula for determining abnormality in the cooler of the turbine generator in the arithmetic and control unit is Θ_I, the output temperature is Θ_O, and the indoor temperature is Θ_I, which is the lubricating oil inlet temperature supplied to each bearing.
Claim 1, characterized in that when A, Θ_I - Θ_A/Θ_O - Θ_I = α, and the value of the degree of performance decline α is compared and determined between a normal value and an abnormal value. An automatic inspection device for the gas turbine power generator described above.
(3)前記冷却器異常に伴う潤滑油の温度監視対象軸受
をガスタービン、減速機、及び発電機としたことを特徴
とする特許請求の範囲第1項記載のガスタービン発電装
置の自動点検装置。
(3) An automatic inspection device for a gas turbine power generation device according to claim 1, characterized in that the bearings to be monitored for the temperature of lubricating oil due to the cooler abnormality are gas turbines, speed reducers, and generators. .
JP59218559A 1984-10-19 1984-10-19 Automatic inspector for gas turbine generator Pending JPS6198927A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP59218559A JPS6198927A (en) 1984-10-19 1984-10-19 Automatic inspector for gas turbine generator

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP59218559A JPS6198927A (en) 1984-10-19 1984-10-19 Automatic inspector for gas turbine generator

Publications (1)

Publication Number Publication Date
JPS6198927A true JPS6198927A (en) 1986-05-17

Family

ID=16721840

Family Applications (1)

Application Number Title Priority Date Filing Date
JP59218559A Pending JPS6198927A (en) 1984-10-19 1984-10-19 Automatic inspector for gas turbine generator

Country Status (1)

Country Link
JP (1) JPS6198927A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH04313636A (en) * 1991-04-10 1992-11-05 Zexel Corp Blow-off duct of local cooling and heating device
JP2018080694A (en) * 2016-10-03 2018-05-24 ゼネラル・エレクトリック・カンパニイ System and method for detecting lubricated bearing condition

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH04313636A (en) * 1991-04-10 1992-11-05 Zexel Corp Blow-off duct of local cooling and heating device
JP2018080694A (en) * 2016-10-03 2018-05-24 ゼネラル・エレクトリック・カンパニイ System and method for detecting lubricated bearing condition

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