CN101818661B - 悬链式涡轮密封系统 - Google Patents

悬链式涡轮密封系统 Download PDF

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Publication number
CN101818661B
CN101818661B CN201010122270.1A CN201010122270A CN101818661B CN 101818661 B CN101818661 B CN 101818661B CN 201010122270 A CN201010122270 A CN 201010122270A CN 101818661 B CN101818661 B CN 101818661B
Authority
CN
China
Prior art keywords
rotor
impeller
chain type
sealing configuration
type sealing
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
CN201010122270.1A
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English (en)
Chinese (zh)
Other versions
CN101818661A (zh
Inventor
I·威尔逊
K·布莱克
J·S·卡明斯
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 CN101818661A publication Critical patent/CN101818661A/zh
Application granted granted Critical
Publication of CN101818661B publication Critical patent/CN101818661B/zh
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/001—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between stator blade and rotor
    • 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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/005—Sealing means between non relatively rotating elements
    • 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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/02—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Sealing Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)
  • Rolls And Other Rotary Bodies (AREA)
  • Sealing Devices (AREA)
CN201010122270.1A 2009-02-13 2010-02-10 悬链式涡轮密封系统 Expired - Fee Related CN101818661B (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US12/370960 2009-02-13
US12/370,960 US8235656B2 (en) 2009-02-13 2009-02-13 Catenary turbine seal systems

Publications (2)

Publication Number Publication Date
CN101818661A CN101818661A (zh) 2010-09-01
CN101818661B true CN101818661B (zh) 2015-06-24

Family

ID=41847705

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201010122270.1A Expired - Fee Related CN101818661B (zh) 2009-02-13 2010-02-10 悬链式涡轮密封系统

Country Status (4)

Country Link
US (1) US8235656B2 (enExample)
EP (1) EP2218879A3 (enExample)
JP (1) JP5484942B2 (enExample)
CN (1) CN101818661B (enExample)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9080456B2 (en) * 2012-01-20 2015-07-14 General Electric Company Near flow path seal with axially flexible arms
US9540940B2 (en) * 2012-03-12 2017-01-10 General Electric Company Turbine interstage seal system
US9404376B2 (en) * 2013-10-28 2016-08-02 General Electric Company Sealing component for reducing secondary airflow in a turbine system
US10662793B2 (en) * 2014-12-01 2020-05-26 General Electric Company Turbine wheel cover-plate mounted gas turbine interstage seal
US10337345B2 (en) * 2015-02-20 2019-07-02 General Electric Company Bucket mounted multi-stage turbine interstage seal and method of assembly
US10502080B2 (en) * 2015-04-10 2019-12-10 United Technologies Corporation Rotating labyrinth M-seal
US10400618B2 (en) * 2017-05-02 2019-09-03 Rolls-Royce Corporation Shaft seal crack obviation
US10584599B2 (en) 2017-07-14 2020-03-10 United Technologies Corporation Compressor rotor stack assembly for gas turbine engine
US11952708B1 (en) 2021-08-27 2024-04-09 Equine Performance Consulting, LLC Method and apparatus for drying gloves and other objects

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2973938A (en) * 1958-08-18 1961-03-07 Gen Electric Cooling means for a multi-stage turbine
US4655683A (en) * 1984-12-24 1987-04-07 United Technologies Corporation Stator seal land structure
US5660526A (en) * 1995-06-05 1997-08-26 Allison Engine Company, Inc. Gas turbine rotor with remote support rings
US6464453B2 (en) * 2000-12-04 2002-10-15 General Electric Company Turbine interstage sealing ring
CN1690389A (zh) * 2004-04-15 2005-11-02 通用电气公司 用于涡轮机叶片冷却回路的旋转式密封装置

Family Cites Families (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2623357A (en) * 1945-09-06 1952-12-30 Birmann Rudolph Gas turbine power plant having means to cool and means to compress combustion products passing through the turbine
DE950100C (de) * 1955-04-10 1956-10-04 Maschf Augsburg Nuernberg Ag Zusammengesetzter Trommellaeufer fuer Kreiselmaschinen, insbesondere fuer Gasturbinen mit axialer Durchstroemrichtung
US2948060A (en) * 1955-05-06 1960-08-09 Manning Maxwell & Moore Inc Method of assembling a limp diaphragm actuator
US3018085A (en) * 1957-03-25 1962-01-23 Gen Motors Corp Floating labyrinth seal
US3056579A (en) * 1959-04-13 1962-10-02 Gen Electric Rotor construction
US3258067A (en) * 1964-06-01 1966-06-28 Fleur Corp Heat exchanger
US3433020A (en) * 1966-09-26 1969-03-18 Gen Electric Gas turbine engine rotors
DE2555911A1 (de) * 1975-12-12 1977-06-23 Motoren Turbinen Union Rotor fuer stroemungsmaschinen, insbesondere gasturbinenstrahltriebwerke
US5236302A (en) * 1991-10-30 1993-08-17 General Electric Company Turbine disk interstage seal system
US5472313A (en) * 1991-10-30 1995-12-05 General Electric Company Turbine disk cooling system
US5275534A (en) * 1991-10-30 1994-01-04 General Electric Company Turbine disk forward seal assembly
US5288210A (en) * 1991-10-30 1994-02-22 General Electric Company Turbine disk attachment system
US5318405A (en) * 1993-03-17 1994-06-07 General Electric Company Turbine disk interstage seal anti-rotation key through disk dovetail slot
US5338154A (en) * 1993-03-17 1994-08-16 General Electric Company Turbine disk interstage seal axial retaining ring
US5535585A (en) * 1994-12-13 1996-07-16 Eichhorn; Gunther Slotted exhaust liner
US5630703A (en) * 1995-12-15 1997-05-20 General Electric Company Rotor disk post cooling system
US5749701A (en) * 1996-10-28 1998-05-12 General Electric Company Interstage seal assembly for a turbine
US6267553B1 (en) * 1999-06-01 2001-07-31 Joseph C. Burge Gas turbine compressor spool with structural and thermal upgrades
DE19940525A1 (de) * 1999-08-26 2001-03-01 Asea Brown Boveri Wärmestaueinheit für eine Rotoranordnung
FR2825748B1 (fr) * 2001-06-07 2003-11-07 Snecma Moteurs Agencement de rotor de turbomachine a deux disques aubages separes par une entretoise
US6899520B2 (en) * 2003-09-02 2005-05-31 General Electric Company Methods and apparatus to reduce seal rubbing within gas turbine engines
US7309210B2 (en) * 2004-12-17 2007-12-18 United Technologies Corporation Turbine engine rotor stack
DE102005059084A1 (de) * 2005-12-10 2007-06-14 Mtu Aero Engines Gmbh Turbomaschine, insbesondere Gasturbine

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2973938A (en) * 1958-08-18 1961-03-07 Gen Electric Cooling means for a multi-stage turbine
US4655683A (en) * 1984-12-24 1987-04-07 United Technologies Corporation Stator seal land structure
US5660526A (en) * 1995-06-05 1997-08-26 Allison Engine Company, Inc. Gas turbine rotor with remote support rings
US6464453B2 (en) * 2000-12-04 2002-10-15 General Electric Company Turbine interstage sealing ring
CN1690389A (zh) * 2004-04-15 2005-11-02 通用电气公司 用于涡轮机叶片冷却回路的旋转式密封装置

Also Published As

Publication number Publication date
US20100209233A1 (en) 2010-08-19
JP5484942B2 (ja) 2014-05-07
CN101818661A (zh) 2010-09-01
EP2218879A2 (en) 2010-08-18
US8235656B2 (en) 2012-08-07
JP2010190215A (ja) 2010-09-02
EP2218879A3 (en) 2012-12-05

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C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20150624

Termination date: 20220210

CF01 Termination of patent right due to non-payment of annual fee