FR2292868A1 - Systeme de joints a labyrinthe pour turbine a gaz - Google Patents

Systeme de joints a labyrinthe pour turbine a gaz

Info

Publication number
FR2292868A1
FR2292868A1 FR7536283A FR7536283A FR2292868A1 FR 2292868 A1 FR2292868 A1 FR 2292868A1 FR 7536283 A FR7536283 A FR 7536283A FR 7536283 A FR7536283 A FR 7536283A FR 2292868 A1 FR2292868 A1 FR 2292868A1
Authority
FR
France
Prior art keywords
gas turbine
sealing system
labyrinth sealing
labyrinth
turbine
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
FR7536283A
Other languages
English (en)
Other versions
FR2292868B1 (fr
Inventor
Bartolomeo Joseph Ferrari
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 FR2292868A1 publication Critical patent/FR2292868A1/fr
Application granted granted Critical
Publication of FR2292868B1 publication Critical patent/FR2292868B1/fr
Granted 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
    • F01D3/00—Machines or engines with axial-thrust balancing effected by working-fluid
    • 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
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/08—Heating, heat-insulating or cooling means
    • F01D5/081—Cooling fluid being directed on the side of the rotor disc or at the roots of the blades

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)
FR7536283A 1974-11-27 1975-11-27 Systeme de joints a labyrinthe pour turbine a gaz Granted FR2292868A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/527,748 US3989410A (en) 1974-11-27 1974-11-27 Labyrinth seal system

Publications (2)

Publication Number Publication Date
FR2292868A1 true FR2292868A1 (fr) 1976-06-25
FR2292868B1 FR2292868B1 (fr) 1982-08-13

Family

ID=24102768

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7536283A Granted FR2292868A1 (fr) 1974-11-27 1975-11-27 Systeme de joints a labyrinthe pour turbine a gaz

Country Status (7)

Country Link
US (1) US3989410A (fr)
JP (1) JPS5854249B2 (fr)
BE (1) BE835964A (fr)
DE (1) DE2552695A1 (fr)
FR (1) FR2292868A1 (fr)
GB (1) GB1525746A (fr)
IT (1) IT1049802B (fr)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2449789A1 (fr) * 1979-02-26 1980-09-19 Gen Electric Turbomachine a structure de refroidissement de joint d'etancheite perfectionnee
FR2570764A1 (fr) * 1984-09-27 1986-03-28 Snecma Dispositif de controle automatique du jeu d'un joint a labyrinthe de turbomachine
FR2648866A1 (fr) * 1989-06-23 1990-12-28 United Technologies Corp Dispositif de controle d'un flux d'air de fuite dans un turbomoteur
EP0501066A1 (fr) * 1991-02-28 1992-09-02 General Electric Company Disque de moteur de turbine avec rainures et ailettes intégrales pour le pompage d'air de refroidissement
EP0785338A1 (fr) * 1996-01-18 1997-07-23 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Dispositif de refroidissement d'un disque de turbine
EP2213836A3 (fr) * 2009-01-30 2014-02-19 General Electric Company Élément de recouvrement de chambre de rotor doté d'une ouverture pour la séparation des déchets et turbine associée
WO2019168590A1 (fr) * 2018-02-27 2019-09-06 Siemens Aktiengesellschaft Moteur à turbine à gaz avec système de distribution d'air de refroidissement de turbine

Families Citing this family (93)

* Cited by examiner, † Cited by third party
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US4103899A (en) * 1975-10-01 1978-08-01 United Technologies Corporation Rotary seal with pressurized air directed at fluid approaching the seal
DE2610783C3 (de) * 1976-03-15 1978-08-31 Kraftwerk Union Ag, 4330 Muelheim Einrichtung zur Stabilisierung der Strömung durch Radialbohrungen in rotierenden Hohlzylindern, insbesondere in Hohlwellen von Gasturbinen
US4173120A (en) * 1977-09-09 1979-11-06 International Harvester Company Turbine nozzle and rotor cooling systems
US4190397A (en) * 1977-11-23 1980-02-26 General Electric Company Windage shield
US4265590A (en) * 1978-05-20 1981-05-05 Rolls-Royce Limited Cooling air supply arrangement for a gas turbine engine
FR2437544A1 (fr) * 1978-09-27 1980-04-25 Snecma Perfectionnements aux joints a labyrinthe
US4348157A (en) * 1978-10-26 1982-09-07 Rolls-Royce Limited Air cooled turbine for a gas turbine engine
US4309145A (en) * 1978-10-30 1982-01-05 General Electric Company Cooling air seal
US4217755A (en) * 1978-12-04 1980-08-19 General Motors Corporation Cooling air control valve
US4554789A (en) * 1979-02-26 1985-11-26 General Electric Company Seal cooling apparatus
DE3003469A1 (de) * 1980-01-31 1981-08-06 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Einrichtung zur verbindung einander rotationssymmetrisch zugeordneter bauteile fuer stroemungsmaschinen, insbesondere gasturbinentriebwerke
US4397471A (en) * 1981-09-02 1983-08-09 General Electric Company Rotary pressure seal structure and method for reducing thermal stresses therein
FR2732405B1 (fr) * 1982-03-23 1997-05-30 Snecma Dispositif pour refroidir le rotor d'une turbine a gaz
US4435123A (en) * 1982-04-19 1984-03-06 United Technologies Corporation Cooling system for turbines
US4466239A (en) * 1983-02-22 1984-08-21 General Electric Company Gas turbine engine with improved air cooling circuit
US4541775A (en) * 1983-03-30 1985-09-17 United Technologies Corporation Clearance control in turbine seals
US4557664A (en) * 1983-04-13 1985-12-10 Dresser Industries, Inc. Control of steam turbine shaft thrust loads
US4463956A (en) * 1983-07-21 1984-08-07 General Motors Corporation Shield for labyrinth seal
FR2570763B1 (fr) * 1984-09-27 1986-11-28 Snecma Dispositif de controle automatique du jeu d'un joint a labyrinthe de turbomachine
US4747750A (en) * 1986-01-17 1988-05-31 United Technologies Corporation Transition duct seal
US4730977A (en) * 1986-12-31 1988-03-15 General Electric Company Thrust bearing loading arrangement for gas turbine engines
US4822244A (en) * 1987-10-15 1989-04-18 United Technologies Corporation Tobi
US5134265A (en) * 1990-02-16 1992-07-28 Metcal, Inc. Rapid heating, uniform, highly efficient griddle
DE59102139D1 (de) * 1990-03-23 1994-08-18 Asea Brown Boveri Axialdurchströmte Gasturbine.
US5142859A (en) * 1991-02-22 1992-09-01 Solar Turbines, Incorporated Turbine cooling system
US5224713A (en) * 1991-08-28 1993-07-06 General Electric Company Labyrinth seal with recirculating means for reducing or eliminating parasitic leakage through the seal
CA2076120A1 (fr) * 1991-09-11 1993-03-12 Adam Nelson Pope Systeme et methode permettant d'ameliorer le refroidissement d'un moteur
US5402636A (en) * 1993-12-06 1995-04-04 United Technologies Corporation Anti-contamination thrust balancing system for gas turbine engines
US5503528A (en) * 1993-12-27 1996-04-02 Solar Turbines Incorporated Rim seal for turbine wheel
US5800124A (en) * 1996-04-12 1998-09-01 United Technologies Corporation Cooled rotor assembly for a turbine engine
JP3327814B2 (ja) * 1997-06-18 2002-09-24 三菱重工業株式会社 ガスタービンのシール装置
US6000701A (en) * 1997-12-15 1999-12-14 Dresser-Rand Company Labyrinth seal assembly and method
US5984636A (en) * 1997-12-17 1999-11-16 Pratt & Whitney Canada Inc. Cooling arrangement for turbine rotor
US5984630A (en) * 1997-12-24 1999-11-16 General Electric Company Reduced windage high pressure turbine forward outer seal
US6095750A (en) * 1998-12-21 2000-08-01 General Electric Company Turbine nozzle assembly
US6394459B1 (en) 2000-06-16 2002-05-28 General Electric Company Multi-clearance labyrinth seal design and related process
US6276896B1 (en) 2000-07-25 2001-08-21 Joseph C. Burge Apparatus and method for cooling Axi-Centrifugal impeller
US6735956B2 (en) * 2001-10-26 2004-05-18 Pratt & Whitney Canada Corp. High pressure turbine blade cooling scoop
FR2831918B1 (fr) * 2001-11-08 2004-05-28 Snecma Moteurs Stator pour turbomachine
JP2005513329A (ja) * 2001-12-13 2005-05-12 アルストム テクノロジー リミテッド タービンエンジンの構成部品用密閉構造体
US6773225B2 (en) * 2002-05-30 2004-08-10 Mitsubishi Heavy Industries, Ltd. Gas turbine and method of bleeding gas therefrom
US6887039B2 (en) * 2002-07-10 2005-05-03 Mitsubishi Heavy Industries, Ltd. Stationary blade in gas turbine and gas turbine comprising the same
US6837676B2 (en) * 2002-09-11 2005-01-04 Mitsubishi Heavy Industries, Ltd. Gas turbine
FR2867223B1 (fr) * 2004-03-03 2006-07-28 Snecma Moteurs Turbomachine comme par exemple un turboreacteur pour avion
GB2426289B (en) * 2005-04-01 2007-07-04 Rolls Royce Plc Cooling system for a gas turbine engine
DE102005025244A1 (de) * 2005-05-31 2006-12-07 Rolls-Royce Deutschland Ltd & Co Kg Luftführungssystem zwischen Verdichter und Turbine eines Gasturbinentriebwerks
GB0513468D0 (en) * 2005-07-01 2005-08-10 Rolls Royce Plc A mounting arrangement for turbine blades
GB2435909A (en) * 2006-03-07 2007-09-12 Rolls Royce Plc Turbine blade arrangement
US20080041064A1 (en) * 2006-08-17 2008-02-21 United Technologies Corporation Preswirl pollution air handling with tangential on-board injector for turbine rotor cooling
GB0620430D0 (en) * 2006-10-14 2006-11-22 Rolls Royce Plc A flow cavity arrangement
FR2908153B1 (fr) * 2006-11-07 2011-05-13 Snecma Dispositif d'accrochage d'un distributeur (8) d'une turbine, turbine les comportant, et moteur d'aeronef en etant equipe
US9127770B2 (en) * 2006-12-19 2015-09-08 Rolls-Royce Corporation Tuned fluid seal
EP2011963B1 (fr) * 2007-07-04 2018-04-04 Ansaldo Energia Switzerland AG Procédé de fonctionnement d'une turbine à gaz à poussée axiale compensée
FR2920525B1 (fr) * 2007-08-31 2014-06-13 Snecma Separateur pour alimentation de l'air de refroidissement d'une turbine
US20090072487A1 (en) * 2007-09-18 2009-03-19 Honeywell International, Inc. Notched tooth labyrinth seals and methods of manufacture
DE102009016803A1 (de) * 2009-04-09 2010-10-14 Rolls-Royce Deutschland Ltd & Co Kg Labyrinth-Anstreifdichtung für eine Strömungsmaschine
US8381533B2 (en) * 2009-04-30 2013-02-26 Honeywell International Inc. Direct transfer axial tangential onboard injector system (TOBI) with self-supporting seal plate
JP5326894B2 (ja) * 2009-07-15 2013-10-30 株式会社Ｉｈｉ ガスタービンの動翼冷却構造
GB201012719D0 (en) 2010-07-29 2010-09-15 Rolls Royce Plc Labyrinth seal
US9074609B2 (en) * 2011-02-15 2015-07-07 Siemens Energy, Inc. Gas turbine engine
US9353647B2 (en) 2012-04-27 2016-05-31 General Electric Company Wide discourager tooth
US9567908B2 (en) * 2012-04-27 2017-02-14 General Electric Company Mitigating vortex pumping effect upstream of oil seal
US9228436B2 (en) * 2012-07-03 2016-01-05 Solar Turbines Incorporated Preswirler configured for improved sealing
US9435206B2 (en) * 2012-09-11 2016-09-06 General Electric Company Flow inducer for a gas turbine system
US10012087B2 (en) * 2012-09-12 2018-07-03 Mitsubishi Hitachi Power Systems, Ltd. Gas turbine including a contoured end wall section of a rotor blade
US10060279B2 (en) 2012-12-29 2018-08-28 United Technologies Corporation Seal support disk and assembly
GB201305432D0 (en) * 2013-03-26 2013-05-08 Rolls Royce Plc A gas turbine engine cooling arrangement
CN103206270A (zh) * 2013-04-25 2013-07-17 北京华清燃气轮机与煤气化联合循环工程技术有限公司 一种冷却燃气轮机涡轮盘及动叶片的方法
US9388698B2 (en) * 2013-11-13 2016-07-12 General Electric Company Rotor cooling
EP3009613B1 (fr) * 2014-08-19 2019-01-30 United Technologies Corporation Joints sans contact pour moteurs à turbine à gaz
EP3130750B1 (fr) * 2015-08-14 2018-03-28 Ansaldo Energia Switzerland AG Système de refroidissement de turbines à gaz
RU2602029C1 (ru) * 2015-09-21 2016-11-10 Акционерное общество "Климов"(АО"Климов") Газогенератор газотурбинного двигателя
RU2603699C1 (ru) * 2015-10-06 2016-11-27 Открытое акционерное общество "Уфимское моторостроительное производственное объединение" ОАО "УМПО" Охлаждаемая турбина газотурбинного двигателя
US10107109B2 (en) 2015-12-10 2018-10-23 United Technologies Corporation Gas turbine engine component cooling assembly
RU2614453C1 (ru) * 2015-12-24 2017-03-28 Открытое акционерное общество "Уфимское моторостроительное производственное объединение" ОАО "УМПО" Охлаждаемая турбина высокого давления
US10655480B2 (en) * 2016-01-18 2020-05-19 United Technologies Corporation Mini-disk for gas turbine engine
RU2623622C1 (ru) * 2016-05-12 2017-06-28 Публичное акционерное общество "Уфимское моторостроительное производственное объединение" ПАО "УМПО" Охлаждаемая турбина высокого давления
US10344869B2 (en) * 2016-05-31 2019-07-09 Rolls-Royce Corporation Labyrinth seal with lubricant directing projection
FR3054606B1 (fr) * 2016-07-29 2020-04-17 Safran Aircraft Engines Turbine comprenant un systeme de ventilation entre rotor et stator
US11053797B2 (en) * 2017-01-23 2021-07-06 General Electric Company Rotor thrust balanced turbine engine
US10400618B2 (en) * 2017-05-02 2019-09-03 Rolls-Royce Corporation Shaft seal crack obviation
US10774746B2 (en) * 2017-07-10 2020-09-15 Dresser-Rand Company Systems and methods for cooling components of a gas turbine
US10598038B2 (en) 2017-11-21 2020-03-24 Honeywell International Inc. Labyrinth seal with variable tooth heights
CN108060979B (zh) * 2017-12-19 2024-04-26 中国联合重型燃气轮机技术有限公司 燃气轮机及其旋流装置
KR101888466B1 (ko) * 2018-02-12 2018-08-16 황재은 형상측정기
JP6966354B2 (ja) 2018-02-28 2021-11-17 三菱パワー株式会社 ガスタービン燃焼器
US11293295B2 (en) 2019-09-13 2022-04-05 Pratt & Whitney Canada Corp. Labyrinth seal with angled fins
CN112523813B (zh) * 2019-09-19 2022-09-16 中国航发商用航空发动机有限责任公司 航空发动机涡轮轮缘封严结构
CN111255522B (zh) * 2020-01-19 2022-02-11 中国科学院工程热物理研究所 一种用于调节发动机高压转子系统轴向力的平衡盘结构
US11428160B2 (en) 2020-12-31 2022-08-30 General Electric Company Gas turbine engine with interdigitated turbine and gear assembly
US20220213802A1 (en) * 2021-01-06 2022-07-07 General Electric Company System for controlling blade clearances within a gas turbine engine
US11859550B2 (en) 2021-04-01 2024-01-02 General Electric Company Compound angle accelerator
CN118128603B (zh) * 2024-05-10 2024-07-02 中国航发四川燃气涡轮研究院 一种涡轮盘系冷却封严结构

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US3532399A (en) * 1968-10-28 1970-10-06 Avco Corp Labyrinth-sling seal
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Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2449789A1 (fr) * 1979-02-26 1980-09-19 Gen Electric Turbomachine a structure de refroidissement de joint d'etancheite perfectionnee
FR2570764A1 (fr) * 1984-09-27 1986-03-28 Snecma Dispositif de controle automatique du jeu d'un joint a labyrinthe de turbomachine
EP0176447A1 (fr) * 1984-09-27 1986-04-02 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Dispositif de contrôle automatique du jeu d'un joint à labyrinthe de turbomachine
US4662821A (en) * 1984-09-27 1987-05-05 Societe Nationale D'etude Et De Construction De Moteur D'aviation S.N.E.C.M.A. Automatic control device of a labyrinth seal clearance in a turbo jet engine
FR2648866A1 (fr) * 1989-06-23 1990-12-28 United Technologies Corp Dispositif de controle d'un flux d'air de fuite dans un turbomoteur
EP0501066A1 (fr) * 1991-02-28 1992-09-02 General Electric Company Disque de moteur de turbine avec rainures et ailettes intégrales pour le pompage d'air de refroidissement
EP0785338A1 (fr) * 1996-01-18 1997-07-23 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Dispositif de refroidissement d'un disque de turbine
FR2743844A1 (fr) * 1996-01-18 1997-07-25 Snecma Dispositif de refroidissement d'un disque de turbine
US5800125A (en) * 1996-01-18 1998-09-01 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Turbine disk cooling device
EP2213836A3 (fr) * 2009-01-30 2014-02-19 General Electric Company Élément de recouvrement de chambre de rotor doté d'une ouverture pour la séparation des déchets et turbine associée
WO2019168590A1 (fr) * 2018-02-27 2019-09-06 Siemens Aktiengesellschaft Moteur à turbine à gaz avec système de distribution d'air de refroidissement de turbine

Also Published As

Publication number Publication date
BE835964A (fr) 1976-03-16
GB1525746A (en) 1978-09-20
IT1049802B (it) 1981-02-10
JPS5177708A (en) 1976-07-06
US3989410A (en) 1976-11-02
JPS5854249B2 (ja) 1983-12-03
FR2292868B1 (fr) 1982-08-13
DE2552695A1 (de) 1976-08-12

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