FR2510220B1 - Joint d'etancheite - Google Patents

Joint d'etancheite

Info

Publication number
FR2510220B1
FR2510220B1 FR8212915A FR8212915A FR2510220B1 FR 2510220 B1 FR2510220 B1 FR 2510220B1 FR 8212915 A FR8212915 A FR 8212915A FR 8212915 A FR8212915 A FR 8212915A FR 2510220 B1 FR2510220 B1 FR 2510220B1
Authority
FR
France
Prior art keywords
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
Application number
FR8212915A
Other languages
English (en)
Other versions
FR2510220A1 (fr
Inventor
James Leonard Thompson
Edward Ivan Stamm
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 FR2510220A1 publication Critical patent/FR2510220A1/fr
Application granted granted Critical
Publication of FR2510220B1 publication Critical patent/FR2510220B1/fr
Expired 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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/023—Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
    • 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
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16J—PISTONS; CYLINDERS; SEALINGS
    • F16J15/00—Sealings
    • F16J15/02—Sealings between relatively-stationary surfaces
    • F16J15/021—Sealings between relatively-stationary surfaces with elastic packing
    • F16J15/022—Sealings between relatively-stationary surfaces with elastic packing characterised by structure or material
    • F16J15/024—Sealings between relatively-stationary surfaces with elastic packing characterised by structure or material the packing being locally weakened in order to increase elasticity
    • F16J15/025—Sealings between relatively-stationary surfaces with elastic packing characterised by structure or material the packing being locally weakened in order to increase elasticity and with at least one flexible lip
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16J—PISTONS; CYLINDERS; SEALINGS
    • F16J15/00—Sealings
    • F16J15/02—Sealings between relatively-stationary surfaces
    • F16J15/06—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces
    • F16J15/08—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with exclusively metal packing
    • F16J15/0887—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with exclusively metal packing the sealing effect being obtained by elastic deformation of the packing
    • 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
FR8212915A 1981-07-27 1982-07-23 Joint d'etancheite Expired FR2510220B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US28700981A 1981-07-27 1981-07-27

Publications (2)

Publication Number Publication Date
FR2510220A1 FR2510220A1 (fr) 1983-01-28
FR2510220B1 true FR2510220B1 (fr) 1987-01-16

Family

ID=23101084

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8212915A Expired FR2510220B1 (fr) 1981-07-27 1982-07-23 Joint d'etancheite

Country Status (5)

Country Link
JP (1) JPS5831226A (fr)
DE (1) DE3224563A1 (fr)
FR (1) FR2510220B1 (fr)
GB (1) GB2102897B (fr)
IT (1) IT1198380B (fr)

Families Citing this family (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4566851A (en) * 1984-05-11 1986-01-28 United Technologies Corporation First stage turbine vane support structure
IT1216611B (it) * 1988-04-21 1990-03-08 Nuovo Pignone Spa Dispositivo per mantenere la bocca anulare di uscita del convogliatore dei gas sempre centrata rispetto al gruppo ugelli di una turbina agas.
GB9305012D0 (en) * 1993-03-11 1993-04-28 Rolls Royce Plc Sealing structures for gas turbine engines
GB9304994D0 (en) * 1993-03-11 1993-04-28 Rolls Royce Plc Improvements in or relating to gas turbine engines
US6334298B1 (en) * 2000-07-14 2002-01-01 General Electric Company Gas turbine combustor having dome-to-liner joint
WO2002027148A1 (fr) * 2000-09-28 2002-04-04 Siemens Westinghouse Power Corporation Joint de transition souple a verrouillage pour chambre de combustion
EP1245790A1 (fr) * 2001-03-26 2002-10-02 Siemens Aktiengesellschaft Turbine à gaz
DE60102217T2 (de) * 2001-05-30 2005-01-13 Techspace Aero, Milmort Dichtende Verbindungsplatte
JP3600912B2 (ja) * 2001-09-12 2004-12-15 川崎重工業株式会社 燃焼器ライナのシール構造
EP1371814A1 (fr) * 2002-06-11 2003-12-17 ALSTOM (Switzerland) Ltd Arrangement des joints d'étanchéité dans le rotor d'une turbine à gaz
FR2840974B1 (fr) 2002-06-13 2005-12-30 Snecma Propulsion Solide Anneau d'etancheite pour cahmbre de combustion et chambre de combustion comportant un tel anneau
US7000406B2 (en) * 2003-12-03 2006-02-21 Pratt & Whitney Canada Corp. Gas turbine combustor sliding joint
GB2418966B (en) * 2004-10-11 2006-11-15 Rolls Royce Plc A sealing arrangement
JP4476152B2 (ja) 2005-04-01 2010-06-09 三菱重工業株式会社 ガスタービン燃焼器
US20070134087A1 (en) 2005-12-08 2007-06-14 General Electric Company Methods and apparatus for assembling turbine engines
US7836702B2 (en) 2006-09-15 2010-11-23 Pratt & Whitney Canada Corp. Gas turbine combustor exit duct and HP vane interface
JP2009197633A (ja) * 2008-02-20 2009-09-03 Ihi Corp ターボチャージャ
ES2400197T3 (es) 2009-09-04 2013-04-08 Alstom Technology Ltd Turbina de gas
EP2525047A1 (fr) * 2011-05-20 2012-11-21 Siemens Aktiengesellschaft Dispositif d'étanchéité pour l'étanchéification de deux pièces limitrophes
RU2597350C2 (ru) * 2011-10-24 2016-09-10 Дженерал Электрик Текнолоджи Гмбх Газотурбинный двигатель, внутренняя оболочка камеры сгорания для газотурбинного двигателя и роторный кожух для газотурбинного двигателя
US9115808B2 (en) * 2012-02-13 2015-08-25 General Electric Company Transition piece seal assembly for a turbomachine
DE102013007443A1 (de) 2013-04-30 2014-10-30 Rolls-Royce Deutschland Ltd & Co Kg Brennerdichtung für Gasturbinen-Brennkammerkopf und Hitzeschild
US10001022B2 (en) * 2013-06-21 2018-06-19 United Technologies Corporation Seals for gas turbine engine
WO2016010556A1 (fr) * 2014-07-18 2016-01-21 Siemens Aktiengesellschaft Joint utilisable entre une transition et un ensemble d'aubes de turbine dans un moteur à turbine
US10612403B2 (en) 2014-08-07 2020-04-07 Pratt & Whitney Canada Corp. Combustor sliding joint
US20160131045A1 (en) * 2014-11-12 2016-05-12 Siemens Energy, Inc. Emissions control system for a gas turbine engine
US10837637B2 (en) * 2016-03-22 2020-11-17 Raytheon Technologies Corporation Gas turbine engine having a heat shield
JP6650849B2 (ja) * 2016-08-25 2020-02-19 三菱日立パワーシステムズ株式会社 ガスタービン
GB201614711D0 (en) * 2016-08-31 2016-10-12 Rolls Royce Plc Axial flow machine
FR3063117B1 (fr) 2017-02-23 2021-07-02 Safran Aircraft Engines Raccordement entre une virole circulaire et un bras radial de structure d'une turbomachine, comprenant un joint d'etancheite et son support

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3042364A (en) * 1960-12-12 1962-07-03 Gen Electric Sealing mechanism
US3965066A (en) * 1974-03-15 1976-06-22 General Electric Company Combustor-turbine nozzle interconnection
CH594836A5 (fr) * 1975-12-19 1978-01-31 Bbc Brown Boveri & Cie
FR2422037A1 (fr) * 1977-12-13 1979-11-02 Alsthom Atlantique Turbine a gaz
US4184689A (en) * 1978-10-02 1980-01-22 United Technologies Corporation Seal structure for an axial flow rotary machine
CH633351A5 (de) * 1978-11-09 1982-11-30 Sulzer Ag Waermedehnungen nachgebende abdichtung einer ringbrennkammer fuer eine gasturbine.
US4251986A (en) * 1978-12-05 1981-02-24 General Electric Company Seal vibration-reducing apparatus

Also Published As

Publication number Publication date
IT1198380B (it) 1988-12-21
GB2102897A (en) 1983-02-09
DE3224563A1 (de) 1983-02-10
JPS5831226A (ja) 1983-02-23
GB2102897B (en) 1985-06-19
IT8222204A0 (it) 1982-07-02
FR2510220A1 (fr) 1983-01-28

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Legal Events

Date Code Title Description
ST Notification of lapse