CN101092884B - 用于装配涡轮机的方法和系统 - Google Patents

用于装配涡轮机的方法和系统 Download PDF

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Publication number
CN101092884B
CN101092884B CN2007101262105A CN200710126210A CN101092884B CN 101092884 B CN101092884 B CN 101092884B CN 2007101262105 A CN2007101262105 A CN 2007101262105A CN 200710126210 A CN200710126210 A CN 200710126210A CN 101092884 B CN101092884 B CN 101092884B
Authority
CN
China
Prior art keywords
housing
seat
turbine
annular
nozzle
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.)
Expired - Fee Related
Application number
CN2007101262105A
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English (en)
Chinese (zh)
Other versions
CN101092884A (zh
Inventor
S·S·伯奇克
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 CN101092884A publication Critical patent/CN101092884A/zh
Application granted granted Critical
Publication of CN101092884B publication Critical patent/CN101092884B/zh
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • F01D11/12Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
    • 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
    • F01D17/00Regulating or controlling by varying flow
    • F01D17/10Final actuators
    • 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
    • F01D11/005Sealing means between non relatively rotating elements
    • 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
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24Casings; Casing parts, e.g. diaphragms, casing fastenings
    • 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
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/246Fastening of diaphragms or stator-rings
    • 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
    • F01D9/00Stators
    • F01D9/02Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • 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
    • F01D9/00Stators
    • F01D9/06Fluid supply conduits to nozzles or the like
    • 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
    • F02C7/28Arrangement of seals
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00Application
    • F05D2220/30Application in turbines
    • F05D2220/31Application in turbines in steam turbines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00Components
    • F05D2240/55Seals
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49316Impeller making
    • Y10T29/4932Turbomachine making
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49316Impeller making
    • Y10T29/4932Turbomachine making
    • Y10T29/49323Assembling fluid flow directing devices, e.g., stators, diaphragms, nozzles

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Gasket Seals (AREA)
CN2007101262105A 2006-06-22 2007-06-22 用于装配涡轮机的方法和系统 Expired - Fee Related CN101092884B (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US11/425,782 US7722314B2 (en) 2006-06-22 2006-06-22 Methods and systems for assembling a turbine
US11/425782 2006-06-22

Publications (2)

Publication Number Publication Date
CN101092884A CN101092884A (zh) 2007-12-26
CN101092884B true CN101092884B (zh) 2011-07-06

Family

ID=38873732

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2007101262105A Expired - Fee Related CN101092884B (zh) 2006-06-22 2007-06-22 用于装配涡轮机的方法和系统

Country Status (4)

Country Link
US (1) US7722314B2 (enExample)
JP (1) JP5085987B2 (enExample)
KR (1) KR20070121584A (enExample)
CN (1) CN101092884B (enExample)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8887390B2 (en) 2008-08-15 2014-11-18 Dresser-Rand Company Method for correcting downstream deflection in gas turbine nozzles
GB0815879D0 (en) * 2008-09-02 2008-10-08 Rolls Royce Plc A method of joining articles
US8123474B2 (en) * 2009-05-12 2012-02-28 Dresser-Rand Company Repair of industrial gas turbine nozzle diaphragm packing
US20110164965A1 (en) * 2010-01-06 2011-07-07 General Electric Company Steam turbine stationary component seal
JP5675411B2 (ja) * 2011-02-10 2015-02-25 三菱重工業株式会社 蒸気転向装置の支持構造
US8834113B2 (en) * 2011-07-19 2014-09-16 General Electric Company Alignment member for steam turbine nozzle assembly
US9140136B2 (en) 2012-05-31 2015-09-22 United Technologies Corporation Stress-relieved wire seal assembly for gas turbine engines
US9541006B2 (en) * 2012-12-29 2017-01-10 United Technologies Corporation Inter-module flow discourager
US9359913B2 (en) * 2013-02-27 2016-06-07 General Electric Company Steam turbine inner shell assembly with common grooves
JP6382019B2 (ja) * 2014-08-08 2018-08-29 三菱航空機株式会社 航空機
EP3009604B1 (en) 2014-09-19 2018-08-08 United Technologies Corporation Radially fastened fixed-variable vane system
US10287903B2 (en) 2016-04-06 2019-05-14 General Electric Company Steam turbine drum nozzle having alignment feature, related assembly, steam turbine and storage medium

Citations (3)

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Publication number Priority date Publication date Assignee Title
US5655876A (en) * 1996-01-02 1997-08-12 General Electric Company Low leakage turbine nozzle
JP2003301702A (ja) * 2002-03-22 2003-10-24 General Electric Co <Ge> バンド冷却式タービンノズル
EP1382801A2 (en) * 2002-07-16 2004-01-21 General Electric Company Cradle mounted turbine nozzle

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GB961588A (en) * 1960-02-05 1964-06-24 Licentia Gmbh A stationary-blade carrier for axial-flow turbines
JPS4026641Y1 (enExample) * 1964-04-13 1965-09-10
US3360189A (en) * 1965-10-11 1967-12-26 United Aircraft Canada Bleed arrangement for gas turbine engines
US3724969A (en) 1971-11-01 1973-04-03 Carrier Corp Turbine construction
DE2218500B2 (de) * 1972-04-17 1974-01-31 Kraftwerk Union AG, 4330 Mülheim Mehrschaliges gehaeuse einer dampfturbine fuer hohe dampfdruecke und dampftemperaturen
US3937589A (en) * 1973-05-23 1976-02-10 Kraftwerkunion Ag High pressure double flow turbine construction
DE2635980C2 (de) * 1976-08-10 1977-12-15 Kraftwerk Union AG, 4330 Mülheim Anordnung zur Zentrierung des Innengehäuses einer Dampfturbine
US4274805A (en) * 1978-10-02 1981-06-23 United Technologies Corporation Floating vane support
US4379560A (en) * 1981-08-13 1983-04-12 Fern Engineering Turbine seal
IN162366B (enExample) * 1984-03-23 1988-05-14 Westinghouse Electric Corp
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ITMI20012584A1 (it) 2001-12-10 2003-06-10 Nuovo Pignone Spa Struttura di separazione dei turboespansori diaalta e bassa pressionedi una turbina a gas
US6752592B2 (en) * 2001-12-28 2004-06-22 General Electric Company Supplemental seal for the chordal hinge seals in a gas turbine
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Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5655876A (en) * 1996-01-02 1997-08-12 General Electric Company Low leakage turbine nozzle
JP2003301702A (ja) * 2002-03-22 2003-10-24 General Electric Co <Ge> バンド冷却式タービンノズル
CN1461873A (zh) * 2002-03-22 2003-12-17 通用电气公司 界壁受冷却的涡轮喷管
EP1382801A2 (en) * 2002-07-16 2004-01-21 General Electric Company Cradle mounted turbine nozzle

Also Published As

Publication number Publication date
KR20070121584A (ko) 2007-12-27
CN101092884A (zh) 2007-12-26
JP2008002467A (ja) 2008-01-10
US20070297899A1 (en) 2007-12-27
US7722314B2 (en) 2010-05-25
JP5085987B2 (ja) 2012-11-28

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C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
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GR01 Patent grant
C17 Cessation of patent right
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20110706

Termination date: 20130622