EP1574674A1 - Procédé et dispositif pour la détection d'impuretés sur des composants de turbine - Google Patents
Procédé et dispositif pour la détection d'impuretés sur des composants de turbine Download PDFInfo
- Publication number
- EP1574674A1 EP1574674A1 EP04004981A EP04004981A EP1574674A1 EP 1574674 A1 EP1574674 A1 EP 1574674A1 EP 04004981 A EP04004981 A EP 04004981A EP 04004981 A EP04004981 A EP 04004981A EP 1574674 A1 EP1574674 A1 EP 1574674A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- turbine
- characteristic value
- vibration
- vibration characteristic
- component
- 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- Withdrawn
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/002—Cleaning of turbomachines
Definitions
- the invention relates to a method and a device for the detection of impurities in turbine components a turbine, in particular a gas turbine for generating of electrical energy.
- a turbine for generating electrical energy In a turbine for generating electrical energy is the energy contained in a working medium is converted into Rotational energy of the turbine, so that a coupled to the turbine Generator is powered and electric power provides.
- Hot gas usually generated in a combustion chamber, wherein as fuel for the burner, for example heavy fuel oil or Naphtha can be used.
- the hot gas is supplied to the turbine blades of the turbine and thereby generates a rotation of the turbine blade ring.
- All turbine components which come into contact with the hot gas are at risk of polluting, since at contact of the contaminated hot gas with the turbine components at least a portion of the dirt particles deposited on the turbine components. Particularly affected are the turbine blades.
- the impurities usually form undesirable deposits on the affected turbine components, the used Fuel, the ambient conditions or the operating mode of Turbine affects how strong and / or how quickly these deposits form.
- the coverings need to be cleaned by cleaning the affected turbine components be removed.
- the visual inspection may, for example, reveal that a cleaning actually not yet necessary or that on the other hand maybe even damage to turbine components is present.
- the invention is therefore based on the object, an improved Method and device for detecting Indicate impurities in turbine components of a turbine, by means of which in particular a disassembly of the turbine is avoided.
- the invention is achieved by a Method for detecting impurities in turbine components a turbine, wherein during operation of the turbine at least one current vibration characteristic at least a turbine component is determined.
- the invention is based on the consideration that, in particular the rotating components of a turbine due to the forces acting on them perform a vibration.
- This vibration can be more or less severe their amplitude and / or attenuation be pronounced and of a fast decaying shock up to an undamped harmonic Range vibration.
- the vibration characteristic value during operation the turbine determined.
- the components in a Operating turbine forces, causing the affected Components in response with a more or less strong vibration.
- the nature of this excited vibration depends on the degree of contamination of the component. For example, as a result of changes the pollution the mass of the component. This is the result during operation adjusting vibration of this component compared to a non-contaminated component more damped and / or has a different frequency. If now such a vibration characteristic of the in operation located turbine component determined, so you can from this, deduce impurities from the turbine component and set a cleaning schedule.
- the natural frequency shifts with one Impurities occupied component compared to a non-contaminated component.
- this can be detected, for example be excited by the component directly or indirectly is, for example by means of a shock, and the adjusting component vibration is measured.
- the vibration characteristic value becomes advantageous with a vibration reference value which corresponds to a corresponding, not contaminated turbine component is assigned.
- a vibration reference value which corresponds to a corresponding, not contaminated turbine component is assigned.
- For example can be the natural frequency of the polluted and one corresponding similar, not polluted turbine component be determined and compared with each other.
- the turbine component a turbine blade.
- the turbine blades are those turbine components which are in the most intensive contact during operation the hot gas. Therefore, it is expected that pads with Form impurities especially on the turbine blades and thereby the operation of the turbine is impaired. Therefore, it is particularly advantageous to have one, several or all turbine blades of the turbine in terms of their current Vibration characteristic to examine in time contaminants to be able to determine.
- the turbine component leads Hot gas.
- Such turbine components not only include the aforementioned Turbine blades, but also other components, which come into contact with the hot gas, such as Henfingaszu- and / or hot gas lines.
- the invention may also include such turbine components be examined for impurities.
- the vibration characteristic value comprises a natural frequency and / or a vibration frequency and / or a Vibration amplitude and / or a damping characteristic and / or a vibration decay behavior of the turbine component.
- vibration characteristics can during operation or be determined during a turbine standstill. While of the establishment must be used to determine these characteristics turbine components usually not excited separately as they occur during operation as a result of they act on forces (for example, centrifugal forces and / or slight imbalances) are excited to vibrate anyway. With respect to this vibration or vibrations then the corresponding vibration characteristic determined.
- the invention further leads to a device for detection contaminants on turbine components of a turbine, wherein at least one sensor unit for determining at least a current vibration characteristic of at least one Turbine component is provided.
- FIG. 3 shows a device according to the invention for detecting.
- the turbine 3 is preferably a gas turbine, whose turbine blades are driven by hot gas.
- the turbine 3 is on a generator 5 coupled.
- a sensor unit 7 For detecting a vibration characteristic of the turbine blades a sensor unit 7 is provided.
- This sensor unit may be attached to the outside of the turbine housing and, for example, sound frequencies at the sensor unit Take up 7 passing turbine blades.
- the sensor unit 7 in the interior of the turbine housing be arranged and, for example, on inductive Record measured values of passing turbine blades.
- the sensor unit 7 is highly integrated is executed and, for example, in the manner of a film is applied to at least one turbine blade.
- One Reading the detected measured values can be and / or done wirelessly.
- the arithmetic unit 9 comprises a memory 11, in which a Vibration reference value is stored, which to a Turbine blade corresponds that is not contaminated, So has no coverings.
- the vibration characteristic value or the vibration reference value can a natural frequency and / or a vibration frequency and / or a vibration amplitude and / or a damping characteristic value and / or a vibration decay behavior of the turbine component include.
- the turbine component is one or more turbine blades.
- the determination of the vibration characteristic value takes place during the Operation of the turbine 3 or alternatively or in combination during a turbine shutdown.
- the arithmetic unit 9 can, for example, by means of a digital computer be realized, in which an evaluation program is used, which the one or more vibration characteristics with respect to the turbine blade accordingly an evaluation algorithm balances with the stored one or more Vibration reference values.
- an evaluation program is used, which the one or more vibration characteristics with respect to the turbine blade accordingly an evaluation algorithm balances with the stored one or more Vibration reference values.
- a Maintenance instructions 13 are generated, for example, based on methods of artificial intelligence.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Measurement Of Mechanical Vibrations Or Ultrasonic Waves (AREA)
- Control Of Turbines (AREA)
- Investigating Or Analyzing Materials By The Use Of Electric Means (AREA)
Priority Applications (8)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP04004981A EP1574674A1 (fr) | 2004-03-03 | 2004-03-03 | Procédé et dispositif pour la détection d'impuretés sur des composants de turbine |
US10/591,511 US20070194773A1 (en) | 2004-03-03 | 2005-03-01 | Method and device for detecting contaminants on turbine components |
PCT/EP2005/050881 WO2005085602A1 (fr) | 2004-03-03 | 2005-03-01 | Procede et dispositif pour detecter des impuretes sur des composants d'une turbine |
CNB2005800063955A CN100404797C (zh) | 2004-03-03 | 2005-03-01 | 检测透平的透平构件上污染物的方法和设备 |
DE502005000794T DE502005000794D1 (de) | 2004-03-03 | 2005-03-01 | Verfahren und vorrichtung zur detektierung von verunreinigungen an turbinenbauteilen |
ES05716854T ES2284155T3 (es) | 2004-03-03 | 2005-03-01 | Procedimiento y dispositivo para detectar suciedad en componentes de una turbina. |
EP05716854A EP1725743B1 (fr) | 2004-03-03 | 2005-03-01 | Procede et dispositif pour detecter des impuretes sur des composants d'une turbine |
JP2007501279A JP4474459B2 (ja) | 2004-03-03 | 2005-03-01 | タービンのタービン部品の汚れを検出する方法とその装置 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP04004981A EP1574674A1 (fr) | 2004-03-03 | 2004-03-03 | Procédé et dispositif pour la détection d'impuretés sur des composants de turbine |
Publications (1)
Publication Number | Publication Date |
---|---|
EP1574674A1 true EP1574674A1 (fr) | 2005-09-14 |
Family
ID=34814246
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP04004981A Withdrawn EP1574674A1 (fr) | 2004-03-03 | 2004-03-03 | Procédé et dispositif pour la détection d'impuretés sur des composants de turbine |
EP05716854A Not-in-force EP1725743B1 (fr) | 2004-03-03 | 2005-03-01 | Procede et dispositif pour detecter des impuretes sur des composants d'une turbine |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP05716854A Not-in-force EP1725743B1 (fr) | 2004-03-03 | 2005-03-01 | Procede et dispositif pour detecter des impuretes sur des composants d'une turbine |
Country Status (7)
Country | Link |
---|---|
US (1) | US20070194773A1 (fr) |
EP (2) | EP1574674A1 (fr) |
JP (1) | JP4474459B2 (fr) |
CN (1) | CN100404797C (fr) |
DE (1) | DE502005000794D1 (fr) |
ES (1) | ES2284155T3 (fr) |
WO (1) | WO2005085602A1 (fr) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8685176B2 (en) * | 2006-10-16 | 2014-04-01 | Ecoservices, Llc | System and method for optimized gas turbine compressor cleaning and performance measurement |
JP5448597B2 (ja) * | 2009-06-19 | 2014-03-19 | 三菱重工業株式会社 | ガスタービン及びこの運転方法 |
FR2956159B1 (fr) * | 2010-02-08 | 2012-02-10 | Snecma | Methode de detection automatisee de l'ingestion d'au moins un corps etranger par un moteur a turbine a gaz |
CN108916017B (zh) * | 2018-06-01 | 2019-08-23 | 武汉船用机械有限责任公司 | 一种船用透平货油泵故障诊断*** |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4548040A (en) * | 1984-05-11 | 1985-10-22 | Elliott Turbomachinery Company, Inc. | Method and apparatus for determining when to initiate cleaning of turbocharger turbine blades |
DE19801804A1 (de) * | 1998-01-19 | 1999-07-22 | Siemens Ag | Turbinenschaufel sowie Verfahren zur Inspektion und/oder Reinigung einer Turbinenschaufel |
US20030085203A1 (en) * | 2001-10-18 | 2003-05-08 | Nair N. Kutty | Method and apparatus for cleaning generator and turbine components |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2657525C3 (de) * | 1976-12-18 | 1981-02-12 | Teldix Gmbh, 6900 Heidelberg | Vorrichtung zum Überwachen des abgezogenen Fadens eines OE-Spinnrotors |
US4339719A (en) * | 1980-07-30 | 1982-07-13 | Electric Power Research Institute, Inc. | Conductivity sensor for monitoring corrodents being deposited in a steam turbine |
US4335600A (en) * | 1980-11-13 | 1982-06-22 | General Electric Company | Detecting internal abnormalities in turbines |
US4588885A (en) * | 1984-02-07 | 1986-05-13 | International Technical Associates | Method of and apparatus for the removal of paint and the like from a substrate |
US5365663A (en) * | 1992-04-28 | 1994-11-22 | Westinghouse Electric Corporation | Method of attaching a monitor target to a shrouded blade |
US5507306A (en) * | 1993-12-23 | 1996-04-16 | Howmet Corporation | Cleaning apparatus and method for cleaning internal airfoil cooling passages |
US5696324A (en) * | 1995-05-11 | 1997-12-09 | Iwatsu Electric Co., Ltd. | Method and apparatus for predicting the life of an object to be measured using longitudinal waves |
US5986234A (en) * | 1997-03-28 | 1999-11-16 | The Regents Of The University Of California | High removal rate laser-based coating removal system |
US6668655B2 (en) * | 2001-09-27 | 2003-12-30 | Siemens Westinghouse Power Corporation | Acoustic monitoring of foreign objects in combustion turbines during operation |
EP1646864B1 (fr) * | 2003-07-18 | 2018-11-07 | Rosemount Inc. | Diagnostic de procede |
-
2004
- 2004-03-03 EP EP04004981A patent/EP1574674A1/fr not_active Withdrawn
-
2005
- 2005-03-01 US US10/591,511 patent/US20070194773A1/en not_active Abandoned
- 2005-03-01 EP EP05716854A patent/EP1725743B1/fr not_active Not-in-force
- 2005-03-01 WO PCT/EP2005/050881 patent/WO2005085602A1/fr active IP Right Grant
- 2005-03-01 JP JP2007501279A patent/JP4474459B2/ja not_active Expired - Fee Related
- 2005-03-01 ES ES05716854T patent/ES2284155T3/es active Active
- 2005-03-01 CN CNB2005800063955A patent/CN100404797C/zh not_active Expired - Fee Related
- 2005-03-01 DE DE502005000794T patent/DE502005000794D1/de active Active
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4548040A (en) * | 1984-05-11 | 1985-10-22 | Elliott Turbomachinery Company, Inc. | Method and apparatus for determining when to initiate cleaning of turbocharger turbine blades |
DE19801804A1 (de) * | 1998-01-19 | 1999-07-22 | Siemens Ag | Turbinenschaufel sowie Verfahren zur Inspektion und/oder Reinigung einer Turbinenschaufel |
US20030085203A1 (en) * | 2001-10-18 | 2003-05-08 | Nair N. Kutty | Method and apparatus for cleaning generator and turbine components |
Also Published As
Publication number | Publication date |
---|---|
US20070194773A1 (en) | 2007-08-23 |
EP1725743A1 (fr) | 2006-11-29 |
JP4474459B2 (ja) | 2010-06-02 |
EP1725743B1 (fr) | 2007-05-30 |
WO2005085602A1 (fr) | 2005-09-15 |
ES2284155T3 (es) | 2007-11-01 |
JP2007526421A (ja) | 2007-09-13 |
DE502005000794D1 (de) | 2007-07-12 |
CN1926309A (zh) | 2007-03-07 |
CN100404797C (zh) | 2008-07-23 |
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