FR2857406B1 - Refroidissement des anneaux de turbine - Google Patents

Refroidissement des anneaux de turbine

Info

Publication number
FR2857406B1
FR2857406B1 FR0308483A FR0308483A FR2857406B1 FR 2857406 B1 FR2857406 B1 FR 2857406B1 FR 0308483 A FR0308483 A FR 0308483A FR 0308483 A FR0308483 A FR 0308483A FR 2857406 B1 FR2857406 B1 FR 2857406B1
Authority
FR
France
Prior art keywords
cooling
turbine rings
turbine
rings
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
FR0308483A
Other languages
English (en)
Other versions
FR2857406A1 (fr
Inventor
Stephane Camus
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
Priority to FR0308483A priority Critical patent/FR2857406B1/fr
Application filed by SNECMA Moteurs SA filed Critical SNECMA Moteurs SA
Priority to RU2005141577/06A priority patent/RU2348817C2/ru
Priority to PCT/FR2004/001785 priority patent/WO2005008033A1/fr
Priority to CA2531519A priority patent/CA2531519C/fr
Priority to JP2006518296A priority patent/JP4536723B2/ja
Priority to US10/557,203 priority patent/US7517189B2/en
Priority to EP04767617.6A priority patent/EP1644615B1/fr
Priority to UAA200600154A priority patent/UA83835C2/ru
Publication of FR2857406A1 publication Critical patent/FR2857406A1/fr
Application granted granted Critical
Publication of FR2857406B1 publication Critical patent/FR2857406B1/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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • 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
    • 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
    • F01D25/08—Cooling; Heating; Heat-insulation
    • F01D25/12—Cooling
    • 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
    • F05D2260/202—Heat transfer, e.g. cooling by film cooling

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR0308483A 2003-07-10 2003-07-10 Refroidissement des anneaux de turbine Expired - Lifetime FR2857406B1 (fr)

Priority Applications (8)

Application Number Priority Date Filing Date Title
FR0308483A FR2857406B1 (fr) 2003-07-10 2003-07-10 Refroidissement des anneaux de turbine
PCT/FR2004/001785 WO2005008033A1 (fr) 2003-07-10 2004-07-08 Circuits de refroidissement pour anneau fixe de turbine a gaz
CA2531519A CA2531519C (fr) 2003-07-10 2004-07-08 Circuits de refroidissement pour anneau fixe de turbine a gaz
JP2006518296A JP4536723B2 (ja) 2003-07-10 2004-07-08 ガスタービンの静止リングのための冷却回路
RU2005141577/06A RU2348817C2 (ru) 2003-07-10 2004-07-08 Система охлаждения неподвижно установленного стяжного кольца газовой турбины
US10/557,203 US7517189B2 (en) 2003-07-10 2004-07-08 Cooling circuit for gas turbine fixed ring
EP04767617.6A EP1644615B1 (fr) 2003-07-10 2004-07-08 Circuits de refroidissement pour anneau fixe de turbine a gaz
UAA200600154A UA83835C2 (ru) 2003-07-10 2004-07-08 Система охлаждения неподвижно установленного стяжного кольца газовой турбины

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0308483A FR2857406B1 (fr) 2003-07-10 2003-07-10 Refroidissement des anneaux de turbine

Publications (2)

Publication Number Publication Date
FR2857406A1 FR2857406A1 (fr) 2005-01-14
FR2857406B1 true FR2857406B1 (fr) 2005-09-30

Family

ID=33522945

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0308483A Expired - Lifetime FR2857406B1 (fr) 2003-07-10 2003-07-10 Refroidissement des anneaux de turbine

Country Status (8)

Country Link
US (1) US7517189B2 (fr)
EP (1) EP1644615B1 (fr)
JP (1) JP4536723B2 (fr)
CA (1) CA2531519C (fr)
FR (1) FR2857406B1 (fr)
RU (1) RU2348817C2 (fr)
UA (1) UA83835C2 (fr)
WO (1) WO2005008033A1 (fr)

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US7650926B2 (en) * 2006-09-28 2010-01-26 United Technologies Corporation Blade outer air seals, cores, and manufacture methods
US7665953B2 (en) * 2006-11-30 2010-02-23 General Electric Company Methods and system for recuperated cooling of integral turbine nozzle and shroud assemblies
US7722315B2 (en) * 2006-11-30 2010-05-25 General Electric Company Method and system to facilitate preferentially distributed recuperated film cooling of turbine shroud assembly
US8123466B2 (en) * 2007-03-01 2012-02-28 United Technologies Corporation Blade outer air seal
US8128348B2 (en) * 2007-09-26 2012-03-06 United Technologies Corporation Segmented cooling air cavity for turbine component
US8061979B1 (en) * 2007-10-19 2011-11-22 Florida Turbine Technologies, Inc. Turbine BOAS with edge cooling
US8177492B2 (en) * 2008-03-04 2012-05-15 United Technologies Corporation Passage obstruction for improved inlet coolant filling
EP2159381A1 (fr) * 2008-08-27 2010-03-03 Siemens Aktiengesellschaft Support d'aube directrice de turbine pour une turbine à gaz
EP2405103B1 (fr) 2009-08-24 2016-05-04 Mitsubishi Heavy Industries, Ltd. Anneaux fendus avec structure de refroidissement
JP4634528B1 (ja) * 2010-01-26 2011-02-23 三菱重工業株式会社 分割環冷却構造およびガスタービン
JP5791232B2 (ja) * 2010-02-24 2015-10-07 三菱重工航空エンジン株式会社 航空用ガスタービン
KR20140015564A (ko) * 2010-04-20 2014-02-06 미츠비시 쥬고교 가부시키가이샤 분할 링 냉각 구조
US8727704B2 (en) 2010-09-07 2014-05-20 Siemens Energy, Inc. Ring segment with serpentine cooling passages
US8845272B2 (en) 2011-02-25 2014-09-30 General Electric Company Turbine shroud and a method for manufacturing the turbine shroud
US9151179B2 (en) * 2011-04-13 2015-10-06 General Electric Company Turbine shroud segment cooling system and method
FR2974839B1 (fr) * 2011-05-04 2015-08-14 Snecma Anneau sectorise de turbine a orifices de ventilation, et turbomachine equipee d'un tel anneau
US9127549B2 (en) * 2012-04-26 2015-09-08 General Electric Company Turbine shroud cooling assembly for a gas turbine system
GB201308602D0 (en) * 2013-05-14 2013-06-19 Rolls Royce Plc A Shroud Arrangement for a Gas Turbine Engine
GB201308605D0 (en) 2013-05-14 2013-06-19 Rolls Royce Plc A shroud arrangement for a gas turbine engine
EP2894301A1 (fr) * 2014-01-14 2015-07-15 Alstom Technology Ltd Segment de bouclier thermique de stator
US20150198063A1 (en) * 2014-01-14 2015-07-16 Alstom Technology Ltd Cooled stator heat shield
US9416675B2 (en) 2014-01-27 2016-08-16 General Electric Company Sealing device for providing a seal in a turbomachine
US9963996B2 (en) 2014-08-22 2018-05-08 Siemens Aktiengesellschaft Shroud cooling system for shrouds adjacent to airfoils within gas turbine engines
US10329934B2 (en) 2014-12-15 2019-06-25 United Technologies Corporation Reversible flow blade outer air seal
US10099290B2 (en) 2014-12-18 2018-10-16 General Electric Company Hybrid additive manufacturing methods using hybrid additively manufactured features for hybrid components
GB201508551D0 (en) * 2015-05-19 2015-07-01 Rolls Royce Plc A heat exchanger for a gas turbine engine
US10641120B2 (en) 2015-07-24 2020-05-05 Rolls-Royce Corporation Seal segment for a gas turbine engine
US10107128B2 (en) * 2015-08-20 2018-10-23 United Technologies Corporation Cooling channels for gas turbine engine component
US9926799B2 (en) * 2015-10-12 2018-03-27 United Technologies Corporation Gas turbine engine components, blade outer air seal assemblies, and blade outer air seal segments thereof
US10145257B2 (en) * 2015-10-16 2018-12-04 United Technologies Corporation Blade outer air seal
GB201612646D0 (en) * 2016-07-21 2016-09-07 Rolls Royce Plc An air cooled component for a gas turbine engine
US10544683B2 (en) 2016-08-30 2020-01-28 Rolls-Royce Corporation Air-film cooled component for a gas turbine engine
JP6925862B2 (ja) * 2017-05-16 2021-08-25 三菱パワー株式会社 ガスタービン、及び翼環部の製造方法
GB201720121D0 (en) * 2017-12-04 2018-01-17 Siemens Ag Heatshield for a gas turbine engine
US10533454B2 (en) 2017-12-13 2020-01-14 Pratt & Whitney Canada Corp. Turbine shroud cooling
US11274569B2 (en) * 2017-12-13 2022-03-15 Pratt & Whitney Canada Corp. Turbine shroud cooling
US10570773B2 (en) * 2017-12-13 2020-02-25 Pratt & Whitney Canada Corp. Turbine shroud cooling
US10502093B2 (en) * 2017-12-13 2019-12-10 Pratt & Whitney Canada Corp. Turbine shroud cooling
US10989068B2 (en) * 2018-07-19 2021-04-27 General Electric Company Turbine shroud including plurality of cooling passages
US10815828B2 (en) * 2018-11-30 2020-10-27 General Electric Company Hot gas path components including plurality of nozzles and venturi
US11098608B2 (en) * 2019-03-13 2021-08-24 Raytheon Technologies Corporation CMC BOAS with internal support structure
JP6666500B1 (ja) * 2019-03-29 2020-03-13 三菱重工業株式会社 高温部品及び高温部品の製造方法
GB201907545D0 (en) * 2019-05-29 2019-07-10 Siemens Ag Heatshield for a gas turbine engine
KR102226741B1 (ko) 2019-06-25 2021-03-12 두산중공업 주식회사 링 세그먼트, 및 이를 포함하는 터빈
FR3101915B1 (fr) 2019-10-11 2022-10-28 Safran Helicoptere Engines Anneau de turbine de turbomachine comprenant des conduites internes de refroidissement
KR102291801B1 (ko) * 2020-02-11 2021-08-24 두산중공업 주식회사 링 세그먼트 및 이를 포함하는 가스터빈
KR102299164B1 (ko) * 2020-03-31 2021-09-07 두산중공업 주식회사 터빈 블레이드의 팁 클리어런스 제어장치 및 이를 포함하는 가스 터빈
US11365645B2 (en) 2020-10-07 2022-06-21 Pratt & Whitney Canada Corp. Turbine shroud cooling
KR102510535B1 (ko) 2021-02-23 2023-03-15 두산에너빌리티 주식회사 링 세그먼트 및 이를 포함하는 터보머신
KR102510537B1 (ko) * 2021-02-24 2023-03-15 두산에너빌리티 주식회사 링 세그먼트 및 이를 포함하는 터보머신
KR102636366B1 (ko) * 2021-09-15 2024-02-13 두산에너빌리티 주식회사 링 세그먼트, 이를 포함하는 회전 기계

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FR2416345A1 (fr) * 1978-01-31 1979-08-31 Snecma Dispositif de refroidissement par impact des segments d'etancheite de turbine d'un turboreacteur
FR2438165A1 (fr) * 1978-10-06 1980-04-30 Snecma Dispositif de regulation de temperature pour turbines a gaz
FR2516597A1 (fr) * 1981-11-16 1983-05-20 Snecma Dispositif annulaire de joint d'usure et d'etancheite refroidi par l'air pour aubage de roue de turbine a gaz ou de compresseur
FR2540937B1 (fr) * 1983-02-10 1987-05-22 Snecma Anneau pour un rotor de turbine d'une turbomachine
US4573866A (en) * 1983-05-02 1986-03-04 United Technologies Corporation Sealed shroud for rotating body
FR2574473B1 (fr) * 1984-11-22 1987-03-20 Snecma Anneau de turbine pour une turbomachine a gaz
US4650395A (en) * 1984-12-21 1987-03-17 United Technologies Corporation Coolable seal segment for a rotary machine
US4668164A (en) * 1984-12-21 1987-05-26 United Technologies Corporation Coolable stator assembly for a gas turbine engine
US5098257A (en) * 1990-09-10 1992-03-24 Westinghouse Electric Corp. Apparatus and method for minimizing differential thermal expansion of gas turbine vane structures
US5165847A (en) * 1991-05-20 1992-11-24 General Electric Company Tapered enlargement metering inlet channel for a shroud cooling assembly of gas turbine engines
US5486090A (en) * 1994-03-30 1996-01-23 United Technologies Corporation Turbine shroud segment with serpentine cooling channels
US5584651A (en) * 1994-10-31 1996-12-17 General Electric Company Cooled shroud
US5538393A (en) * 1995-01-31 1996-07-23 United Technologies Corporation Turbine shroud segment with serpentine cooling channels having a bend passage
US5536143A (en) * 1995-03-31 1996-07-16 General Electric Co. Closed circuit steam cooled bucket
US5993150A (en) * 1998-01-16 1999-11-30 General Electric Company Dual cooled shroud
JP3631898B2 (ja) * 1998-03-03 2005-03-23 三菱重工業株式会社 ガスタービンにおける分割環の冷却構造
US6139257A (en) * 1998-03-23 2000-10-31 General Electric Company Shroud cooling assembly for gas turbine engine
FR2803871B1 (fr) * 2000-01-13 2002-06-07 Snecma Moteurs Agencement de reglage de diametre d'un stator de turbine a gaz

Also Published As

Publication number Publication date
FR2857406A1 (fr) 2005-01-14
JP4536723B2 (ja) 2010-09-01
CA2531519A1 (fr) 2005-01-27
WO2005008033A1 (fr) 2005-01-27
EP1644615B1 (fr) 2015-04-01
JP2007516375A (ja) 2007-06-21
RU2005141577A (ru) 2006-06-27
UA83835C2 (ru) 2008-08-26
US7517189B2 (en) 2009-04-14
EP1644615A1 (fr) 2006-04-12
US20070041827A1 (en) 2007-02-22
RU2348817C2 (ru) 2009-03-10
CA2531519C (fr) 2011-08-30

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Legal Events

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Year of fee payment: 14

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Owner name: SAFRAN AIRCRAFT ENGINES, FR

Effective date: 20170719

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