EP1134360A3 - Agencement de réglage de diamètre d'un stator de turbine à gaz - Google Patents

Agencement de réglage de diamètre d'un stator de turbine à gaz Download PDF

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Publication number
EP1134360A3
EP1134360A3 EP01400059A EP01400059A EP1134360A3 EP 1134360 A3 EP1134360 A3 EP 1134360A3 EP 01400059 A EP01400059 A EP 01400059A EP 01400059 A EP01400059 A EP 01400059A EP 1134360 A3 EP1134360 A3 EP 1134360A3
Authority
EP
European Patent Office
Prior art keywords
stator
adjusting
diameter
gas turbine
turbine engine
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
EP01400059A
Other languages
German (de)
English (en)
Other versions
EP1134360A2 (fr
EP1134360B1 (fr
Inventor
Jean-Baptiste Arilla
Anne-Marie Arraitz
Alain Dominique Gendraud
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.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA Moteurs 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 SNECMA Moteurs SA filed Critical SNECMA Moteurs SA
Publication of EP1134360A2 publication Critical patent/EP1134360A2/fr
Publication of EP1134360A3 publication Critical patent/EP1134360A3/fr
Application granted granted Critical
Publication of EP1134360B1 publication Critical patent/EP1134360B1/fr
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
    • F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/14—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
    • F01D11/20—Actively adjusting tip-clearance
    • F01D11/24—Actively adjusting tip-clearance by selectively cooling-heating stator or rotor components
    • 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/246—Fastening of diaphragms or stator-rings
    • 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
    • F05D2240/00—Components
    • F05D2240/10—Stators
    • F05D2240/11—Shroud seal segments

Landscapes

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

Abstract

Du gaz de ventilation est soufflé vers un anneau de stator (3) pour régler sa distance du bout d'aubes mobiles (5) et diminuer les fuites dans une turbine de machine. On propose d'opérer des communications entre chambres successives (18, 19, 20) à travers des crochets (26, 27, 28 et 29) de fixation d'une entretoise (10) de support de l'anneau (3) au carter (2), afin de réduire les concentrations de contrainte dans cette entretoise (10).
EP01400059A 2000-01-13 2001-01-11 Agencement de réglage de diamètre d'un stator de turbine à gaz Expired - Lifetime EP1134360B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0000371A FR2803871B1 (fr) 2000-01-13 2000-01-13 Agencement de reglage de diametre d'un stator de turbine a gaz
FR0000371 2000-01-13

Publications (3)

Publication Number Publication Date
EP1134360A2 EP1134360A2 (fr) 2001-09-19
EP1134360A3 true EP1134360A3 (fr) 2002-07-31
EP1134360B1 EP1134360B1 (fr) 2005-11-16

Family

ID=8845853

Family Applications (1)

Application Number Title Priority Date Filing Date
EP01400059A Expired - Lifetime EP1134360B1 (fr) 2000-01-13 2001-01-11 Agencement de réglage de diamètre d'un stator de turbine à gaz

Country Status (10)

Country Link
US (1) US6666645B1 (fr)
EP (1) EP1134360B1 (fr)
JP (1) JP4248785B2 (fr)
CA (1) CA2366363C (fr)
DE (1) DE60114910T2 (fr)
ES (1) ES2248248T3 (fr)
FR (1) FR2803871B1 (fr)
RU (1) RU2292466C2 (fr)
UA (1) UA70353C2 (fr)
WO (1) WO2001051771A2 (fr)

Families Citing this family (52)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2816352B1 (fr) * 2000-11-09 2003-01-31 Snecma Moteurs Ensemble de ventilation d'un anneau de stator
US6893217B2 (en) * 2002-12-20 2005-05-17 General Electric Company Methods and apparatus for assembling gas turbine nozzles
US6892931B2 (en) * 2002-12-27 2005-05-17 General Electric Company Methods for replacing portions of turbine shroud supports
FR2857406B1 (fr) * 2003-07-10 2005-09-30 Snecma Moteurs Refroidissement des anneaux de turbine
DE102005013796A1 (de) * 2005-03-24 2006-09-28 Alstom Technology Ltd. Wärmestausegment
DE102005013797A1 (de) * 2005-03-24 2006-09-28 Alstom Technology Ltd. Wärmestausegment
US7600967B2 (en) * 2005-07-30 2009-10-13 United Technologies Corporation Stator assembly, module and method for forming a rotary machine
FR2899281B1 (fr) 2006-03-30 2012-08-10 Snecma Dispositif de refroidissement d'un carter de turbine d'une turbomachine
US20070249823A1 (en) * 2006-04-20 2007-10-25 Chemagis Ltd. Process for preparing gemcitabine and associated intermediates
US7785063B2 (en) * 2006-12-15 2010-08-31 Siemens Energy, Inc. Tip clearance control
US7597533B1 (en) 2007-01-26 2009-10-06 Florida Turbine Technologies, Inc. BOAS with multi-metering diffusion cooling
US7665962B1 (en) 2007-01-26 2010-02-23 Florida Turbine Technologies, Inc. Segmented ring for an industrial gas turbine
AU2009216831B2 (en) * 2008-02-20 2014-11-20 General Electric Technology Gmbh Gas turbine
US8123473B2 (en) * 2008-10-31 2012-02-28 General Electric Company Shroud hanger with diffused cooling passage
JP5254774B2 (ja) * 2008-12-22 2013-08-07 三菱重工業株式会社 熱機関の流体シール構造
EP2415969A1 (fr) 2010-08-05 2012-02-08 Siemens Aktiengesellschaft Composant d'une turbine avec des joints lamelles et procédé d'étanchéification contre les fuites entre une pale et un élément porteur
RU2465466C1 (ru) * 2011-05-05 2012-10-27 Открытое акционерное общество "Авиадвигатель" Высокотемпературная турбина газотурбинного двигателя
US8826668B2 (en) * 2011-08-02 2014-09-09 Siemens Energy, Inc. Two stage serial impingement cooling for isogrid structures
US9080458B2 (en) 2011-08-23 2015-07-14 United Technologies Corporation Blade outer air seal with multi impingement plate assembly
BR112014026803A2 (pt) 2012-04-27 2017-06-27 Gen Electric montagem de invólucro para um motor de turbina a gás
ES2531468T3 (es) * 2012-10-12 2015-03-16 Mtu Aero Engines Gmbh Estructura de caja con obturación y refrigeración mejoradas
EP2728255A1 (fr) * 2012-10-31 2014-05-07 Alstom Technology Ltd Agencement de segment de gaz chaud
US9752451B2 (en) * 2012-12-19 2017-09-05 United Technologies Corporation Active clearance control system with zone controls
FR3002971B1 (fr) * 2013-03-06 2015-04-17 Snecma Dispositif de ventilation d'un carter de stator d'une turbomachine, comprenant un ajustement sur des circonferences
FR3002972B1 (fr) * 2013-03-06 2015-04-17 Snecma Dispositif de ventilation d'un carter de stator d'une turbomachine comprenant un ajustement en direction axiale
DE102013212501A1 (de) * 2013-06-27 2014-12-31 MTU Aero Engines AG Leitschaufelsegment mit stirnseitiger Ausnehmung
US9464538B2 (en) * 2013-07-08 2016-10-11 General Electric Company Shroud block segment for a gas turbine
FR3009579B1 (fr) * 2013-08-07 2015-09-25 Snecma Carter de turbine en deux materiaux
US10329939B2 (en) 2013-09-12 2019-06-25 United Technologies Corporation Blade tip clearance control system including BOAS support
US10364706B2 (en) 2013-12-17 2019-07-30 United Technologies Corporation Meter plate for blade outer air seal
EP3183431B1 (fr) 2014-08-22 2018-10-10 Siemens Aktiengesellschaft Système de refroidissement de carénage pour des carénages adjacents à des surfaces portantes dans des moteurs à turbine à gaz
EP3034803A1 (fr) * 2014-12-16 2016-06-22 Rolls-Royce Corporation Système de suspension d'un composant de moteur à turbine
US20170248030A1 (en) * 2016-02-26 2017-08-31 General Electric Company Encapsulated Cooling for Turbine Shrouds
FR3049003B1 (fr) * 2016-03-21 2018-04-06 Safran Aircraft Engines Ensemble d'anneau de turbine sans jeu de montage a froid
US10815814B2 (en) * 2017-05-08 2020-10-27 Raytheon Technologies Corporation Re-use and modulated cooling from tip clearance control system for gas turbine engine
GB201708744D0 (en) * 2017-06-01 2017-07-19 Rolls Royce Plc Clearance control arrangement
US10900378B2 (en) 2017-06-16 2021-01-26 Honeywell International Inc. Turbine tip shroud assembly with plural shroud segments having internal cooling passages
US10677084B2 (en) 2017-06-16 2020-06-09 Honeywell International Inc. Turbine tip shroud assembly with plural shroud segments having inter-segment seal arrangement
US20190218928A1 (en) * 2018-01-17 2019-07-18 United Technologies Corporation Blade outer air seal for gas turbine engine
FR3082872B1 (fr) * 2018-06-25 2021-06-04 Safran Aircraft Engines Dispositif de refroidissement d'un carter de turbomachine
US10634010B2 (en) * 2018-09-05 2020-04-28 United Technologies Corporation CMC BOAS axial retaining clip
US10830050B2 (en) * 2019-01-31 2020-11-10 General Electric Company Unitary body turbine shrouds including structural breakdown and collapsible features
US11761343B2 (en) * 2019-03-13 2023-09-19 Rtx Corporation BOAS carrier with dovetail attachments
US10995626B2 (en) * 2019-03-15 2021-05-04 Raytheon Technologies Corporation BOAS and methods of making a BOAS having fatigue resistant cooling inlets
FR3109406B1 (fr) * 2020-04-17 2022-10-07 Safran Aircraft Engines Dispositif de refroidissement d’un carter de turbine
FR3127981B1 (fr) * 2021-10-08 2025-07-11 Safran Aircraft Engines Virole annulaire de turbine
US11788425B2 (en) * 2021-11-05 2023-10-17 General Electric Company Gas turbine engine with clearance control system
CN116085067A (zh) 2021-11-05 2023-05-09 通用电气公司 具有流体导管系统的燃气涡轮发动机及其操作方法
EP4332351A1 (fr) * 2022-09-05 2024-03-06 General Electric Company Polska Sp. Z o.o Ensemble boîtier externe de rotor de turbine
US12188359B2 (en) 2022-09-30 2025-01-07 Rtx Corporation Blade outer air seal with retainer ring
US12421870B1 (en) 2024-04-30 2025-09-23 Rolls-Royce Corporation Pin mounted ceramic matrix composite heat shields with impingement cooling
US20250389200A1 (en) * 2024-06-19 2025-12-25 Rtx Corporation Center Tie Rotor Annular Seal

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1604778A (fr) * 1966-11-02 1972-01-31
US4177004A (en) * 1977-10-31 1979-12-04 General Electric Company Combined turbine shroud and vane support structure
US4573866A (en) * 1983-05-02 1986-03-04 United Technologies Corporation Sealed shroud for rotating body
WO1994012775A1 (fr) * 1992-11-24 1994-06-09 United Technologies Corporation Ensemble d'etancheite d'air externe a refroidissement pour turbine

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4650394A (en) * 1984-11-13 1987-03-17 United Technologies Corporation Coolable seal assembly for a gas turbine engine
US5169287A (en) * 1991-05-20 1992-12-08 General Electric Company Shroud cooling assembly for gas turbine engine
US5205708A (en) * 1992-02-07 1993-04-27 General Electric Company High pressure turbine component interference fit up
US5273396A (en) * 1992-06-22 1993-12-28 General Electric Company Arrangement for defining improved cooling airflow supply path through clearance control ring and shroud
RU2086792C1 (ru) * 1994-11-24 1997-08-10 Акционерное общество "Авиадвигатель" Газотурбинный двигатель
RU2136896C1 (ru) * 1997-05-28 1999-09-10 Акционерное общество "Турбомоторный завод" Турбина

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1604778A (fr) * 1966-11-02 1972-01-31
US4177004A (en) * 1977-10-31 1979-12-04 General Electric Company Combined turbine shroud and vane support structure
US4573866A (en) * 1983-05-02 1986-03-04 United Technologies Corporation Sealed shroud for rotating body
WO1994012775A1 (fr) * 1992-11-24 1994-06-09 United Technologies Corporation Ensemble d'etancheite d'air externe a refroidissement pour turbine

Also Published As

Publication number Publication date
WO2001051771A2 (fr) 2001-07-19
DE60114910T2 (de) 2006-08-10
WO2001051771A3 (fr) 2002-01-17
FR2803871A1 (fr) 2001-07-20
FR2803871B1 (fr) 2002-06-07
RU2292466C2 (ru) 2007-01-27
CA2366363C (fr) 2008-12-09
UA70353C2 (uk) 2004-10-15
US6666645B1 (en) 2003-12-23
JP2003519742A (ja) 2003-06-24
CA2366363A1 (fr) 2001-07-19
ES2248248T3 (es) 2006-03-16
EP1134360A2 (fr) 2001-09-19
EP1134360B1 (fr) 2005-11-16
JP4248785B2 (ja) 2009-04-02
DE60114910D1 (de) 2005-12-22

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