EP0995881A3 - Dichtungsanordnung - Google Patents

Dichtungsanordnung Download PDF

Info

Publication number
EP0995881A3
EP0995881A3 EP99810907A EP99810907A EP0995881A3 EP 0995881 A3 EP0995881 A3 EP 0995881A3 EP 99810907 A EP99810907 A EP 99810907A EP 99810907 A EP99810907 A EP 99810907A EP 0995881 A3 EP0995881 A3 EP 0995881A3
Authority
EP
European Patent Office
Prior art keywords
guide
rotor
sealing arrangement
blade
blades
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.)
Granted
Application number
EP99810907A
Other languages
English (en)
French (fr)
Other versions
EP0995881A2 (de
EP0995881B1 (de
Inventor
Alexander Dr. Beeck
Mohamed Dr. Nazmy
Bernhard Dr. Weigand
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.)
Alstom SA
Original Assignee
Alstom SA
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 Alstom SA filed Critical Alstom SA
Publication of EP0995881A2 publication Critical patent/EP0995881A2/de
Publication of EP0995881A3 publication Critical patent/EP0995881A3/de
Application granted granted Critical
Publication of EP0995881B1 publication Critical patent/EP0995881B1/de
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • F01D11/005Sealing means between non relatively rotating elements
    • F01D11/006Sealing the gap between rotor blades or blades and rotor
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Gasket Seals (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

Beschrieben wird eine Dichtungsanordnung zur Reduzierung von Leckströmen innerhalb einer Strömungsrotationsmaschine, vorzugsweise einer axialen Turbomaschine, mit Lauf- und Leitschaufeln, die jeweils in wenigstens einer Lauf- bzw. Leitschaufelreihe angeordnet sind und Schaufelfüsse aufweisen, über die die einzelnen Lauf- und Leitschaufeln mit Befestigungskonturen verbunden sind.
Die Erfindung zeichnet sich dadurch aus, daß zwischen wenigstens zwei benachbarten Schaufelfüßen innerhalb einer Leit- oder Laufschaufelreihe oder zwischen Leit- und/oder Laufschaufeln und benachbarten Komponenten der Strömungsmaschine ein filzartiges Material aufweisendes Dichtelement vorgesehen ist.
EP99810907A 1998-10-19 1999-10-06 Dichtungsanordnung Expired - Lifetime EP0995881B1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19848103 1998-10-19
DE19848103A DE19848103A1 (de) 1998-10-19 1998-10-19 Dichtungsanordnung

Publications (3)

Publication Number Publication Date
EP0995881A2 EP0995881A2 (de) 2000-04-26
EP0995881A3 true EP0995881A3 (de) 2002-03-13
EP0995881B1 EP0995881B1 (de) 2004-01-07

Family

ID=7884914

Family Applications (1)

Application Number Title Priority Date Filing Date
EP99810907A Expired - Lifetime EP0995881B1 (de) 1998-10-19 1999-10-06 Dichtungsanordnung

Country Status (4)

Country Link
US (1) US6312218B1 (de)
EP (1) EP0995881B1 (de)
JP (1) JP4465067B2 (de)
DE (2) DE19848103A1 (de)

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19937577A1 (de) * 1999-08-09 2001-02-15 Abb Alstom Power Ch Ag Reibungsbehaftete Gasturbinenkomponente
DE10047307A1 (de) 2000-09-25 2002-08-01 Alstom Switzerland Ltd Dichtungsanordnung
JP2003035105A (ja) * 2001-07-19 2003-02-07 Mitsubishi Heavy Ind Ltd ガスタービン分割壁
EP1448874B1 (de) 2001-09-25 2007-12-26 ALSTOM Technology Ltd Dichtungsanordnung zur dichtspaltreduzierung innerhalb einer strömungsrotationsmaschine
US6854960B2 (en) * 2002-06-24 2005-02-15 Electric Boat Corporation Segmented composite impeller/propeller arrangement and manufacturing method
EP1529123B1 (de) * 2002-08-16 2011-10-05 Alstom Technology Ltd Intermetallisches material und verwendung dieses materials
US6883807B2 (en) 2002-09-13 2005-04-26 Seimens Westinghouse Power Corporation Multidirectional turbine shim seal
US6733234B2 (en) 2002-09-13 2004-05-11 Siemens Westinghouse Power Corporation Biased wear resistant turbine seal assembly
US6893217B2 (en) * 2002-12-20 2005-05-17 General Electric Company Methods and apparatus for assembling gas turbine nozzles
US20070048140A1 (en) * 2005-08-24 2007-03-01 General Electric Company Methods and apparatus for assembling gas turbine engines
EP1914389A1 (de) * 2006-10-20 2008-04-23 Siemens Aktiengesellschaft Turbinenschaufel mit separatem Abdichtelement
US9133720B2 (en) * 2007-12-28 2015-09-15 United Technologies Corporation Integrally bladed rotor with slotted outer rim
US9273563B2 (en) 2007-12-28 2016-03-01 United Technologies Corporation Integrally bladed rotor with slotted outer rim
US8206087B2 (en) 2008-04-11 2012-06-26 Siemens Energy, Inc. Sealing arrangement for turbine engine having ceramic components
GB2462810B (en) * 2008-08-18 2010-07-21 Rolls Royce Plc Sealing means
US8322977B2 (en) * 2009-07-22 2012-12-04 Siemens Energy, Inc. Seal structure for preventing leakage of gases across a gap between two components in a turbine engine
FR2998610B1 (fr) * 2012-11-29 2019-04-05 Safran Aircraft Engines Roue de redresseurs a plateformes espacees
US9926790B2 (en) * 2014-07-21 2018-03-27 Rolls-Royce Corporation Composite turbine components adapted for use with strip seals
US10107127B2 (en) * 2014-07-31 2018-10-23 United Technologies Corporation Gas turbine engine with axial compressor having improved air sealing
US9759079B2 (en) 2015-05-28 2017-09-12 Rolls-Royce Corporation Split line flow path seals
US10890078B1 (en) 2017-06-12 2021-01-12 Technetics Group Llc Flexible seal assembly
EP3438410B1 (de) 2017-08-01 2021-09-29 General Electric Company Dichtungssystem für eine rotationsmaschine
US10718226B2 (en) 2017-11-21 2020-07-21 Rolls-Royce Corporation Ceramic matrix composite component assembly and seal
FR3092867B1 (fr) * 2019-02-19 2021-08-13 Safran Aircraft Engines Partie de turbomachine pour aeronef a languettes d’etancheite
CN113252246B (zh) * 2021-06-18 2021-11-05 中国科学院武汉岩土力学研究所 一种可回收的地下连续墙接缝处渗漏检测装置

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1580884A (en) * 1977-08-03 1980-12-10 Rolls Royce Sealing means
GB2189253A (en) * 1986-04-17 1987-10-21 Central Electr Generat Board Method of sealing joints and jointing compound therefor
EP0357984A1 (de) * 1988-08-31 1990-03-14 Westinghouse Electric Corporation Gasturbine mit einem gekühlten Leitschaufeldeckring
US5385760A (en) * 1992-12-09 1995-01-31 Mtu Motoren- Und Turbinen-Union Munchen Gmbh Process for the production of a composite coating of a functional substance in a metal matrix on the surface of an article
US5421704A (en) * 1993-06-10 1995-06-06 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Inter-blade platform for a bladed disc of a turbomachine rotor
EP1013974A2 (de) * 1998-12-25 2000-06-28 Nichias Corporation Dichtungsanordnung für die Verbindung von drei Elementen

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2108176A1 (de) * 1971-02-20 1972-08-31 Motoren Turbinen Union Befestigung von keramischen Turbinenschaufeln
US4422827A (en) * 1982-02-18 1983-12-27 United Technologies Corporation Blade root seal
US5104286A (en) * 1991-02-08 1992-04-14 Westinghouse Electric Corp. Recirculation seal for a gas turbine exhaust diffuser
US5149250A (en) 1991-02-28 1992-09-22 General Electric Company Gas turbine vane assembly seal and support system
FR2691749B1 (fr) * 1992-05-27 1994-07-22 Snecma Dispositif d'etancheite entre des etages d'aubes et un tambour tournant notamment pour eviter les fuites autour des etages d'aubes de redresseur .
DE4432685C1 (de) * 1994-09-14 1995-11-23 Mtu Muenchen Gmbh Anlaufbelaf für das Gehäuse einer Turbomaschine und Verfahren zur Herstellung
US5531457A (en) * 1994-12-07 1996-07-02 Pratt & Whitney Canada, Inc. Gas turbine engine feather seal arrangement
DE19520268A1 (de) 1995-06-02 1996-12-05 Abb Management Ag Dichtung
US5509669A (en) * 1995-06-19 1996-04-23 General Electric Company Gas-path leakage seal for a gas turbine
US5586773A (en) * 1995-06-19 1996-12-24 General Electric Company Gas-path leakage seal for a gas turbine made from metallic mesh
JP2941698B2 (ja) * 1995-11-10 1999-08-25 三菱重工業株式会社 ガスタービンロータ
US5820338A (en) * 1997-04-24 1998-10-13 United Technologies Corporation Fan blade interplatform seal

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1580884A (en) * 1977-08-03 1980-12-10 Rolls Royce Sealing means
GB2189253A (en) * 1986-04-17 1987-10-21 Central Electr Generat Board Method of sealing joints and jointing compound therefor
EP0357984A1 (de) * 1988-08-31 1990-03-14 Westinghouse Electric Corporation Gasturbine mit einem gekühlten Leitschaufeldeckring
US5385760A (en) * 1992-12-09 1995-01-31 Mtu Motoren- Und Turbinen-Union Munchen Gmbh Process for the production of a composite coating of a functional substance in a metal matrix on the surface of an article
US5421704A (en) * 1993-06-10 1995-06-06 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Inter-blade platform for a bladed disc of a turbomachine rotor
EP1013974A2 (de) * 1998-12-25 2000-06-28 Nichias Corporation Dichtungsanordnung für die Verbindung von drei Elementen

Also Published As

Publication number Publication date
JP2000120401A (ja) 2000-04-25
US6312218B1 (en) 2001-11-06
EP0995881A2 (de) 2000-04-26
EP0995881B1 (de) 2004-01-07
DE59908238D1 (de) 2004-02-12
JP4465067B2 (ja) 2010-05-19
DE19848103A1 (de) 2000-04-20

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