NO20065282L - Fremgangsmate og anordning for deteksjon av rubbing mellom en turbomaskins stator og rotor - Google Patents

Fremgangsmate og anordning for deteksjon av rubbing mellom en turbomaskins stator og rotor

Info

Publication number
NO20065282L
NO20065282L NO20065282A NO20065282A NO20065282L NO 20065282 L NO20065282 L NO 20065282L NO 20065282 A NO20065282 A NO 20065282A NO 20065282 A NO20065282 A NO 20065282A NO 20065282 L NO20065282 L NO 20065282L
Authority
NO
Norway
Prior art keywords
turbo machine
stator
rotor
rubbing
detecting
Prior art date
Application number
NO20065282A
Other languages
English (en)
Inventor
Lyder Moen
Original Assignee
Dynatrend As
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 Dynatrend As filed Critical Dynatrend As
Priority to NO20065282A priority Critical patent/NO20065282L/no
Priority to PCT/NO2007/000403 priority patent/WO2008060164A1/en
Publication of NO20065282L publication Critical patent/NO20065282L/no

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01HMEASUREMENT OF MECHANICAL VIBRATIONS OR ULTRASONIC, SONIC OR INFRASONIC WAVES
    • G01H1/00Measuring characteristics of vibrations in solids by using direct conduction to the detector
    • G01H1/003Measuring characteristics of vibrations in solids by using direct conduction to the detector of rotating machines
    • G01H1/006Measuring characteristics of vibrations in solids by using direct conduction to the detector of rotating machines of the rotor of turbo machines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/20Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
    • F02C3/22Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products the fuel or oxidant being gaseous at standard temperature and pressure
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C6/00Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/18Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use using the waste heat of gas-turbine plants outside the plants themselves, e.g. gas-turbine power heat plants
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/08Heating air supply before combustion, e.g. by exhaust gases

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
  • Measurement Of Mechanical Vibrations Or Ultrasonic Waves (AREA)

Abstract

Fremgangsmåte for deteksjon av rubbing mellom en turbomaskins (1) stator (2) og rotor (4) hvor en giver (16, 18) i form av et akselaerometer, en sensor for måling av vibrasjon ved ultrahøye frekvenser eller en mikrofon anbringes ved turbomaskinen (1), hvoretter signalet fra giveren (16, 18) i det minste frekvens- eller amplitudeanalyseres og sammenlignes med i det minste forutbestemte eller adaptive verdier fra gruppen som omfatter måleverdier og frekvensmønstre, og hvor det ut fra den nevnte sammenligning og forutbestemte grenseverdier bestemmes om rubbing er til stede eller har vært til stede.
NO20065282A 2006-11-17 2006-11-17 Fremgangsmate og anordning for deteksjon av rubbing mellom en turbomaskins stator og rotor NO20065282L (no)

Priority Applications (2)

Application Number Priority Date Filing Date Title
NO20065282A NO20065282L (no) 2006-11-17 2006-11-17 Fremgangsmate og anordning for deteksjon av rubbing mellom en turbomaskins stator og rotor
PCT/NO2007/000403 WO2008060164A1 (en) 2006-11-17 2007-11-16 A method and a device for detection of rubbing between a stator and a rotor of a turbo-machine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
NO20065282A NO20065282L (no) 2006-11-17 2006-11-17 Fremgangsmate og anordning for deteksjon av rubbing mellom en turbomaskins stator og rotor

Publications (1)

Publication Number Publication Date
NO20065282L true NO20065282L (no) 2008-05-19

Family

ID=39401894

Family Applications (1)

Application Number Title Priority Date Filing Date
NO20065282A NO20065282L (no) 2006-11-17 2006-11-17 Fremgangsmate og anordning for deteksjon av rubbing mellom en turbomaskins stator og rotor

Country Status (2)

Country Link
NO (1) NO20065282L (no)
WO (1) WO2008060164A1 (no)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102012213016A1 (de) * 2012-07-25 2014-01-30 Siemens Aktiengesellschaft Verfahren zur Minimierung des Spalts zwischen einem Läufer und einem Gehäuse
CZ306833B6 (cs) * 2012-12-20 2017-08-02 Doosan Ĺ koda Power s.r.o. Způsob detekce a lokalizace částečného kontaktu rotor-stator při provozu turbíny
CN104634526B (zh) * 2015-01-27 2017-06-30 西安交通大学 一种基于非线性压缩变换的转子碰摩故障检测方法及系统
DE102019116954A1 (de) * 2019-06-24 2020-12-24 Rolls-Royce Deutschland Ltd & Co Kg Vorrichtung und Verfahren zur Einstellung einer Spalthöhe
CN110926745B (zh) * 2019-11-22 2020-11-17 华中科技大学 一种航空发动机低压涡轮转静子叶片碰摩试验台架

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4335600A (en) * 1980-11-13 1982-06-22 General Electric Company Detecting internal abnormalities in turbines
JPS5834326A (ja) * 1981-08-26 1983-02-28 Hitachi Ltd 回転機のラビング検出装置
US4543830A (en) * 1983-12-09 1985-10-01 Stephens James O Gas turbine rub detector
JPH0782035A (ja) * 1993-06-22 1995-03-28 Nippon Cement Co Ltd サイアロン・窒化アルミニウム複合粉末の製造方法
GB2396438B (en) * 2002-12-20 2006-03-22 Rolls Royce Plc Rotor system

Also Published As

Publication number Publication date
WO2008060164A1 (en) 2008-05-22

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