DE50106206D1 - TURBINE PLANT - Google Patents

TURBINE PLANT

Info

Publication number
DE50106206D1
DE50106206D1 DE50106206T DE50106206T DE50106206D1 DE 50106206 D1 DE50106206 D1 DE 50106206D1 DE 50106206 T DE50106206 T DE 50106206T DE 50106206 T DE50106206 T DE 50106206T DE 50106206 D1 DE50106206 D1 DE 50106206D1
Authority
DE
Germany
Prior art keywords
turbine plant
turbine
plant
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 - Lifetime
Application number
DE50106206T
Other languages
German (de)
Inventor
Peter Tiemann
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.)
Siemens AG
Original Assignee
Siemens AG
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 Siemens AG filed Critical Siemens AG
Application granted granted Critical
Publication of DE50106206D1 publication Critical patent/DE50106206D1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

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
    • F01D11/005—Sealing means between non relatively rotating elements
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/002—Wall structures
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/205—Cooling fluid recirculation, i.e. after cooling one or more components is the cooling fluid recovered and used elsewhere for other purposes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/232—Heat transfer, e.g. cooling characterized by the cooling medium
    • F05D2260/2322—Heat transfer, e.g. cooling characterized by the cooling medium steam
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23M—CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
    • F23M2900/00—Special features of, or arrangements for combustion chambers
    • F23M2900/05005—Sealing means between wall tiles or panels
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00012—Details of sealing devices
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/03044—Impingement cooled combustion chamber walls or subassemblies
DE50106206T 2000-03-02 2001-02-23 TURBINE PLANT Expired - Lifetime DE50106206D1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
EP00104346A EP1130219A1 (en) 2000-03-02 2000-03-02 Turbine engine with sealing means between panels
PCT/EP2001/002094 WO2001065073A1 (en) 2000-03-02 2001-02-23 Turbine installation

Publications (1)

Publication Number Publication Date
DE50106206D1 true DE50106206D1 (en) 2005-06-16

Family

ID=8168008

Family Applications (1)

Application Number Title Priority Date Filing Date
DE50106206T Expired - Lifetime DE50106206D1 (en) 2000-03-02 2001-02-23 TURBINE PLANT

Country Status (5)

Country Link
EP (2) EP1130219A1 (en)
JP (1) JP4637435B2 (en)
CN (1) CN1272525C (en)
DE (1) DE50106206D1 (en)
WO (1) WO2001065073A1 (en)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1302723A1 (en) 2001-10-15 2003-04-16 Siemens Aktiengesellschaft Lining for combustion chamber inside walls
DE10155420A1 (en) 2001-11-12 2003-05-22 Rolls Royce Deutschland Heat shield arrangement with sealing element
FR2868119B1 (en) * 2004-03-26 2006-06-16 Snecma Moteurs Sa SEAL SEAL BETWEEN THE INTERIOR AND EXTERIOR HOUSINGS OF A TURBOJET SECTION
US7870738B2 (en) 2006-09-29 2011-01-18 Siemens Energy, Inc. Gas turbine: seal between adjacent can annular combustors
DE102010031124A1 (en) * 2010-07-08 2012-01-12 Man Diesel & Turbo Se flow machine
CH704185A1 (en) * 2010-12-06 2012-06-15 Alstom Technology Ltd GAS TURBINE AND METHOD FOR recondition SUCH GAS TURBINE.
DE102010063594A1 (en) 2010-12-20 2012-06-21 Mtu Aero Engines Gmbh Sealing arrangement for use in airplane thruster to prevent leakage in gap between e.g. guide vanes, has high temperature-fixed sealing web arranged between component portions of two static components to seal gap between component portions
US8544852B2 (en) 2011-06-03 2013-10-01 General Electric Company Torsion seal
CN104379877B (en) * 2012-06-18 2016-06-15 通用电器技术有限公司 Sealing member between static turbine part
DE102015201782A1 (en) * 2015-02-02 2016-08-18 MTU Aero Engines AG Guide vane ring for a turbomachine
DE102017207667A1 (en) 2017-05-08 2018-11-08 Siemens Aktiengesellschaft Method for servicing a turbomachine
CN109653816A (en) * 2019-01-23 2019-04-19 江苏核电有限公司 It is a kind of for steam turbine from the support tool and its support method of integral blade

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2991045A (en) * 1958-07-10 1961-07-04 Westinghouse Electric Corp Sealing arrangement for a divided tubular casing
US2999631A (en) * 1958-09-05 1961-09-12 Gen Electric Dual airfoil
US4199151A (en) * 1978-08-14 1980-04-22 General Electric Company Method and apparatus for retaining seals
CA2031085A1 (en) * 1990-01-16 1991-07-17 Michael P. Hagle Arrangement for sealing gaps between adjacent circumferential segments of turbine nozzles and shrouds
US5158305A (en) * 1992-01-31 1992-10-27 Eg&G Pressure Science, Inc. Pressure-energized two-element seal
GB9305012D0 (en) * 1993-03-11 1993-04-28 Rolls Royce Plc Sealing structures for gas turbine engines
US5735671A (en) * 1996-11-29 1998-04-07 General Electric Company Shielded turbine rotor
US6076835A (en) * 1997-05-21 2000-06-20 Allison Advanced Development Company Interstage van seal apparatus
JPH1150805A (en) * 1997-08-06 1999-02-23 Mitsubishi Heavy Ind Ltd Sealing structure for gas turbine stator blade shroud
GB2335470B (en) * 1998-03-18 2002-02-13 Rolls Royce Plc A seal

Also Published As

Publication number Publication date
CN1272525C (en) 2006-08-30
EP1130219A1 (en) 2001-09-05
JP2003525381A (en) 2003-08-26
CN1408048A (en) 2003-04-02
JP4637435B2 (en) 2011-02-23
EP1268981B1 (en) 2005-05-11
WO2001065073A1 (en) 2001-09-07
EP1268981A1 (en) 2003-01-02

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition