DE102010016890A1 - Aktives Regelungssystem und Verfahren zur Gehäuseausrichtung - Google Patents

Aktives Regelungssystem und Verfahren zur Gehäuseausrichtung Download PDF

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Publication number
DE102010016890A1
DE102010016890A1 DE102010016890A DE102010016890A DE102010016890A1 DE 102010016890 A1 DE102010016890 A1 DE 102010016890A1 DE 102010016890 A DE102010016890 A DE 102010016890A DE 102010016890 A DE102010016890 A DE 102010016890A DE 102010016890 A1 DE102010016890 A1 DE 102010016890A1
Authority
DE
Germany
Prior art keywords
rotor
shroud
sensors
housing
actuators
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Withdrawn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
DE102010016890A
Other languages
German (de)
English (en)
Inventor
Martel Alexander Mccallum
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of DE102010016890A1 publication Critical patent/DE102010016890A1/de
Withdrawn legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/14Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
    • F01D11/20Actively adjusting tip-clearance
    • F01D11/22Actively adjusting tip-clearance by mechanically actuating the stator or rotor components, e.g. moving shroud sections relative to the rotor

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
DE102010016890A 2009-05-22 2010-05-11 Aktives Regelungssystem und Verfahren zur Gehäuseausrichtung Withdrawn DE102010016890A1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US12/470,929 2009-05-22
US12/470,929 US8177483B2 (en) 2009-05-22 2009-05-22 Active casing alignment control system and method

Publications (1)

Publication Number Publication Date
DE102010016890A1 true DE102010016890A1 (de) 2010-11-25

Family

ID=42993757

Family Applications (1)

Application Number Title Priority Date Filing Date
DE102010016890A Withdrawn DE102010016890A1 (de) 2009-05-22 2010-05-11 Aktives Regelungssystem und Verfahren zur Gehäuseausrichtung

Country Status (5)

Country Link
US (1) US8177483B2 (enExample)
JP (1) JP5583473B2 (enExample)
CN (1) CN101892875B (enExample)
CH (1) CH701143B1 (enExample)
DE (1) DE102010016890A1 (enExample)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109931182A (zh) * 2019-04-25 2019-06-25 西安航空学院 偏心滑片式燃气轮机

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US8593296B2 (en) * 2010-10-19 2013-11-26 General Electric Company System and method for turbine bucket tip shroud deflection measurement
US8388314B2 (en) 2011-04-21 2013-03-05 General Electric Company Turbine inlet casing with integral bearing housing
US9228447B2 (en) 2012-02-14 2016-01-05 United Technologies Corporation Adjustable blade outer air seal apparatus
US20130326875A1 (en) * 2012-06-08 2013-12-12 General Electric Company Method and apparatus for roll-in and alignment of a casing shell of a gas turbine
US20130330187A1 (en) * 2012-06-11 2013-12-12 General Electric Company Method and apparatus for mitigating out of roundness effects at a turbine
US9476318B2 (en) 2013-09-03 2016-10-25 General Electric Company Systems and methods to monitor a rotating component
US9593589B2 (en) * 2014-02-28 2017-03-14 General Electric Company System and method for thrust bearing actuation to actively control clearance in a turbo machine
US10584609B2 (en) 2016-06-22 2020-03-10 Rolls-Royce Corporation Gas turbine engine frame alignment tool
EP3361099A1 (en) * 2017-02-10 2018-08-15 Entecnia Consulting, S.L.U. Method of manufacturing and assembling a pump and vacuum pump
US10753223B2 (en) * 2017-10-04 2020-08-25 General Electric Company Active centering control for static annular turbine flowpath structures
KR102036191B1 (ko) * 2017-11-20 2019-10-24 두산중공업 주식회사 블레이드 팁 간극 조절 수단을 구비한 가스 터빈
US10920605B2 (en) * 2017-12-21 2021-02-16 General Electric Company System and method for measuring eccentricity of turbine shell relative to turbine rotor
US10976220B2 (en) 2019-06-11 2021-04-13 General Electric Company Wireless antenna system for sensors on circumferential interior surface of turbomachine casing
US11179820B2 (en) 2019-06-11 2021-11-23 General Electric Company Mounting system for tool for machining circumferential interior surface of turbomachine casing
US11519298B2 (en) 2019-06-11 2022-12-06 General Electric Company Sensor mounting for circumferential interior surface of turbomachine casing
US11952907B2 (en) 2019-06-11 2024-04-09 Ge Infrastructure Technology Llc Systems and methods for sensors on only part of circumferential interior surface of turbomachine casing
US11248495B2 (en) * 2019-06-11 2022-02-15 General Electric Company Systems and methods for sensors on circumferential interior surface of turbomachine casing
US11635750B2 (en) 2019-10-30 2023-04-25 General Electric Company System and method for removably inserting a sensor assembly into a compressor casing
US11060847B2 (en) 2019-10-30 2021-07-13 General Electric Company System and method for optical measurements in a rotary machine
US11400527B2 (en) 2019-10-30 2022-08-02 General Electric Company System and method for machining a slot in an inner surface of a casing for a gas turbine engine
US11409022B2 (en) 2019-10-30 2022-08-09 General Electric Company System and method for optical measurements in a rotary machine
JP2023100250A (ja) * 2022-01-05 2023-07-18 ゼネラル・エレクトリック・カンパニイ 排気フレーム差動冷却システム
US11668206B1 (en) 2022-03-09 2023-06-06 General Electric Company Temperature gradient control system for a compressor casing

Citations (1)

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Publication number Priority date Publication date Assignee Title
US6126390A (en) 1997-12-19 2000-10-03 Rolls-Royce Deutschland Gmbh Passive clearance control system for a gas turbine

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US5263816A (en) 1991-09-03 1993-11-23 General Motors Corporation Turbomachine with active tip clearance control
JPH0711908A (ja) * 1993-06-25 1995-01-13 Mitsubishi Heavy Ind Ltd 蒸気タービン動翼のフラッタ防止装置
US5545007A (en) * 1994-11-25 1996-08-13 United Technologies Corp. Engine blade clearance control system with piezoelectric actuator
US5658125A (en) * 1995-02-28 1997-08-19 Allison Engine Company, Inc. Magnetic bearings as actuation for active compressor stability control
JPH1150809A (ja) * 1997-08-01 1999-02-23 Mitsubishi Heavy Ind Ltd 回転体の伸び量調整装置
ES2286054T3 (es) * 2001-04-12 2007-12-01 Siemens Aktiengesellschaft Turbina de gas con piezas de la carcasa axialmente desplazables.
KR100546349B1 (ko) 2003-07-23 2006-01-26 삼성전자주식회사 광 디스크 서보 시스템에서 디스크 편심 보상 장치 및 그방법
US7079957B2 (en) * 2003-12-30 2006-07-18 General Electric Company Method and system for active tip clearance control in turbines
JP2005344874A (ja) 2004-06-04 2005-12-15 Shimadzu Corp 磁気軸受装置
US7341426B2 (en) 2004-12-29 2008-03-11 United Technologies Corporation Gas turbine engine blade tip clearance apparatus and method
GB0513654D0 (en) * 2005-07-02 2005-08-10 Rolls Royce Plc Variable displacement turbine liner
US20090031802A1 (en) 2007-08-03 2009-02-05 General Electric Company Rotor alignment system and method
US20090053042A1 (en) 2007-08-22 2009-02-26 General Electric Company Method and apparatus for clearance control of turbine blade tip
US8152446B2 (en) * 2007-08-23 2012-04-10 General Electric Company Apparatus and method for reducing eccentricity and out-of-roundness in turbines

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6126390A (en) 1997-12-19 2000-10-03 Rolls-Royce Deutschland Gmbh Passive clearance control system for a gas turbine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109931182A (zh) * 2019-04-25 2019-06-25 西安航空学院 偏心滑片式燃气轮机
CN109931182B (zh) * 2019-04-25 2024-02-20 西安航空学院 偏心滑片式燃气轮机

Also Published As

Publication number Publication date
CN101892875A (zh) 2010-11-24
US8177483B2 (en) 2012-05-15
JP5583473B2 (ja) 2014-09-03
JP2010270755A (ja) 2010-12-02
US20100296911A1 (en) 2010-11-25
CH701143A2 (de) 2010-11-30
CN101892875B (zh) 2014-04-02
CH701143B1 (de) 2015-08-14

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R119 Application deemed withdrawn, or ip right lapsed, due to non-payment of renewal fee