DE602008002070D1 - Turbinenringanordnung für eine gasturbine - Google Patents

Turbinenringanordnung für eine gasturbine

Info

Publication number
DE602008002070D1
DE602008002070D1 DE602008002070T DE602008002070T DE602008002070D1 DE 602008002070 D1 DE602008002070 D1 DE 602008002070D1 DE 602008002070 T DE602008002070 T DE 602008002070T DE 602008002070 T DE602008002070 T DE 602008002070T DE 602008002070 D1 DE602008002070 D1 DE 602008002070D1
Authority
DE
Germany
Prior art keywords
ring
cmc
turbine
split
contact
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.)
Active
Application number
DE602008002070T
Other languages
English (en)
Inventor
Georges Habarou
Julien Mateo
Eric Bouillon
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 Ceramics SA
Original Assignee
SNECMA Propulsion Solide 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 Propulsion Solide SA filed Critical SNECMA Propulsion Solide SA
Publication of DE602008002070D1 publication Critical patent/DE602008002070D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • 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
    • F01D11/12—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
    • F01D11/122—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part with erodable or abradable material
    • F01D11/125—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part with erodable or abradable material with a reinforcing structure
    • 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
    • F05D2250/00—Geometry
    • F05D2250/20—Three-dimensional
    • F05D2250/23—Three-dimensional prismatic
    • F05D2250/232—Three-dimensional prismatic conical
    • 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
    • F05D2260/30—Retaining components in desired mutual position
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/50—Intrinsic material properties or characteristics
    • F05D2300/502—Thermal properties
    • F05D2300/5021—Expansivity
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/603—Composites; e.g. fibre-reinforced
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/614—Fibres or filaments
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
DE602008002070T 2007-03-15 2008-03-14 Turbinenringanordnung für eine gasturbine Active DE602008002070D1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0753842A FR2913718B1 (fr) 2007-03-15 2007-03-15 Ensemble d'anneau de turbine pour turbine a gaz
PCT/FR2008/050445 WO2008132364A1 (fr) 2007-03-15 2008-03-14 Ensemble d'anneau de turbine pour turbine a gaz

Publications (1)

Publication Number Publication Date
DE602008002070D1 true DE602008002070D1 (de) 2010-09-16

Family

ID=38670627

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602008002070T Active DE602008002070D1 (de) 2007-03-15 2008-03-14 Turbinenringanordnung für eine gasturbine

Country Status (8)

Country Link
US (1) US8257029B2 (de)
EP (1) EP2137384B1 (de)
CN (1) CN101627184A (de)
AT (1) ATE476585T1 (de)
CA (1) CA2679093C (de)
DE (1) DE602008002070D1 (de)
FR (1) FR2913718B1 (de)
WO (1) WO2008132364A1 (de)

Families Citing this family (48)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2913718B1 (fr) * 2007-03-15 2009-06-05 Snecma Propulsion Solide Sa Ensemble d'anneau de turbine pour turbine a gaz
FR2913717A1 (fr) * 2007-03-15 2008-09-19 Snecma Propulsion Solide Sa Ensemble d'anneau de turbine pour turbine a gaz
JP5569194B2 (ja) 2010-07-02 2014-08-13 株式会社Ｉｈｉ シュラウドセグメントの製造方法
US8696311B2 (en) 2011-03-29 2014-04-15 Pratt & Whitney Canada Corp. Apparatus and method for gas turbine engine vane retention
US9803868B2 (en) * 2011-05-20 2017-10-31 Siemens Energy, Inc. Thermally compliant support for a combustion system
US9039364B2 (en) * 2011-06-29 2015-05-26 United Technologies Corporation Integrated case and stator
WO2013102171A2 (en) 2011-12-31 2013-07-04 Rolls-Royce Corporation Blade track assembly, components, and methods
US20130186304A1 (en) * 2012-01-20 2013-07-25 General Electric Company Process of fabricating a thermal barrier coating and an article having a cold sprayed thermal barrier coating
RU2615292C2 (ru) 2012-01-26 2017-04-04 АНСАЛДО ЭНЕРДЖИА АйПи ЮКей ЛИМИТЕД Деталь статора с сегментированным внутренним кольцом для турбомашины
WO2014120334A1 (en) 2013-01-29 2014-08-07 Sippel Aaron D Turbine shroud
WO2014158276A2 (en) * 2013-03-05 2014-10-02 Rolls-Royce Corporation Structure and method for providing compliance and sealing between ceramic and metallic structures
US10094233B2 (en) 2013-03-13 2018-10-09 Rolls-Royce Corporation Turbine shroud
US9757920B2 (en) * 2013-03-15 2017-09-12 Rolls-Royce Corporation Flexible ceramic matrix composite seal
EP2789803A1 (de) * 2013-04-09 2014-10-15 Siemens Aktiengesellschaft Aufprallringelementbefestigung und -abdichtung
WO2014186001A2 (en) * 2013-04-12 2014-11-20 United Technologies Corporation Flexible feather seal for blade outer air seal gas turbine engine rapid response clearance control system
US9040138B2 (en) * 2013-04-29 2015-05-26 General Electric Company Composite article including composite to metal interlock and method of fabrication
FR3011271B1 (fr) * 2013-10-01 2018-01-19 Safran Aircraft Engines Dispositif de connexion d'une partie fixe de turbomachine et d'un pied de distributeur d'une turbine de turbomachine
US10443423B2 (en) * 2014-09-22 2019-10-15 United Technologies Corporation Gas turbine engine blade outer air seal assembly
US9945243B2 (en) 2014-10-14 2018-04-17 Rolls-Royce Corporation Turbine shroud with biased blade track
US10190434B2 (en) 2014-10-29 2019-01-29 Rolls-Royce North American Technologies Inc. Turbine shroud with locating inserts
CA2915370A1 (en) 2014-12-23 2016-06-23 Rolls-Royce Corporation Full hoop blade track with axially keyed features
CA2915246A1 (en) 2014-12-23 2016-06-23 Rolls-Royce Corporation Turbine shroud
EP3045674B1 (de) 2015-01-15 2018-11-21 Rolls-Royce Corporation Turbinenummantelung mit rohrförmigen laufradpositionierungseinsätzen
US10100649B2 (en) 2015-03-31 2018-10-16 Rolls-Royce North American Technologies Inc. Compliant rail hanger
CA2924855A1 (en) 2015-04-29 2016-10-29 Rolls-Royce Corporation Keystoned blade track
CA2925588A1 (en) 2015-04-29 2016-10-29 Rolls-Royce Corporation Brazed blade track for a gas turbine engine
EP3298249A1 (de) * 2015-05-07 2018-03-28 Nuovo Pignone Tecnologie Srl Turbomaschinendichtung und turbomaschine mit solch einer dichtung
US10370994B2 (en) * 2015-05-28 2019-08-06 Rolls-Royce North American Technologies Inc. Pressure activated seals for a gas turbine engine
US10215056B2 (en) 2015-06-30 2019-02-26 Rolls-Royce Corporation Turbine shroud with movable attachment features
US10233763B2 (en) * 2015-09-09 2019-03-19 United Technologies Corporation Seal assembly for turbine engine component
US10240476B2 (en) 2016-01-19 2019-03-26 Rolls-Royce North American Technologies Inc. Full hoop blade track with interstage cooling air
US10215037B2 (en) * 2016-05-13 2019-02-26 United Technologies Corporation Contoured retaining ring
US10415415B2 (en) 2016-07-22 2019-09-17 Rolls-Royce North American Technologies Inc. Turbine shroud with forward case and full hoop blade track
US10287906B2 (en) 2016-05-24 2019-05-14 Rolls-Royce North American Technologies Inc. Turbine shroud with full hoop ceramic matrix composite blade track and seal system
US10677260B2 (en) * 2017-02-21 2020-06-09 General Electric Company Turbine engine and method of manufacturing
US10655491B2 (en) * 2017-02-22 2020-05-19 Rolls-Royce Corporation Turbine shroud ring for a gas turbine engine with radial retention features
CN106988784A (zh) * 2017-03-24 2017-07-28 中国北方发动机研究所(天津) 一种径流式增压器涡轮转轴结构及其成型工艺
US10392957B2 (en) 2017-10-05 2019-08-27 Rolls-Royce Corporation Ceramic matrix composite blade track with mounting system having load distribution features
CN108050913B (zh) * 2017-12-14 2020-04-14 中国航发沈阳发动机研究所 一种用于涡轮转子外径的测量装置
US10934877B2 (en) 2018-10-31 2021-03-02 Raytheon Technologies Corporation CMC laminate pocket BOAS with axial attachment scheme
US11008894B2 (en) 2018-10-31 2021-05-18 Raytheon Technologies Corporation BOAS spring clip
US11078802B2 (en) * 2019-05-10 2021-08-03 Rolls-Royce Plc Turbine engine assembly with ceramic matrix composite components and end face seals
FR3100048B1 (fr) * 2019-08-23 2023-02-24 Safran Ceram Anneau de turbine en CMC avec revêtement de protection à épaisseur variable et procédé de fabrication d’un tel anneau
EP3789638A1 (de) * 2019-09-05 2021-03-10 Siemens Aktiengesellschaft Dichtung für verbrennungsvorrichtung
FR3101114B1 (fr) * 2019-09-23 2021-08-27 Safran Aircraft Engines Ensemble pour une turbomachine
US11149563B2 (en) * 2019-10-04 2021-10-19 Rolls-Royce Corporation Ceramic matrix composite blade track with mounting system having axial reaction load distribution features
CN114542292A (zh) * 2022-02-22 2022-05-27 中国联合重型燃气轮机技术有限公司 一种缸体支撑装置
US20240011410A1 (en) * 2022-07-05 2024-01-11 General Electric Company Variable flowpath casings for blade tip clearance control

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3126149A (en) * 1964-03-24 Foamed aluminum honeycomb motor
FR2724973B1 (fr) * 1982-12-31 1996-12-13 Snecma Dispositif d'etancheite d'aubages mobiles de turbomachine avec controle actif des jeux en temps reel et methode de determination dudit dispositif
FR2559834B1 (fr) * 1984-02-22 1988-04-08 Snecma Anneau de turbine
US4589666A (en) * 1985-07-25 1986-05-20 Pressure Science Incorporated Slip joint assembly for a split ring seal
US5088775A (en) * 1990-07-27 1992-02-18 General Electric Company Seal ring with flanged end portions
GB0108398D0 (en) * 2001-04-04 2001-05-23 Siemens Ag Seal element for sealing a gap and combustion turbine having a seal element
US6997673B2 (en) * 2003-12-11 2006-02-14 Honeywell International, Inc. Gas turbine high temperature turbine blade outer air seal assembly
US20060082074A1 (en) * 2004-10-18 2006-04-20 Pratt & Whitney Canada Corp. Circumferential feather seal
US7771160B2 (en) * 2006-08-10 2010-08-10 United Technologies Corporation Ceramic shroud assembly
FR2913718B1 (fr) * 2007-03-15 2009-06-05 Snecma Propulsion Solide Sa Ensemble d'anneau de turbine pour turbine a gaz
FR2913717A1 (fr) * 2007-03-15 2008-09-19 Snecma Propulsion Solide Sa Ensemble d'anneau de turbine pour turbine a gaz
US8186692B2 (en) * 2009-03-17 2012-05-29 Pratt & Whitney Canada Corp. Split ring seal with spring element

Also Published As

Publication number Publication date
US20100092281A1 (en) 2010-04-15
FR2913718A1 (fr) 2008-09-19
CA2679093C (en) 2015-01-27
WO2008132364A1 (fr) 2008-11-06
CN101627184A (zh) 2010-01-13
CA2679093A1 (en) 2008-11-06
EP2137384A1 (de) 2009-12-30
US8257029B2 (en) 2012-09-04
ATE476585T1 (de) 2010-08-15
EP2137384B1 (de) 2010-08-04
FR2913718B1 (fr) 2009-06-05

Similar Documents

Publication Publication Date Title
ATE476585T1 (de) Turbinenringanordnung für eine gasturbine
ATE541121T1 (de) Windturbine, nabe für eine windturbine und verwendung davon
UA100438C2 (en) Flexible abutment links for attaching a part made of cmc
DE502005007638D1 (de) Lamellendichtung, insbesondere für eine gasturbine
FR2891242B1 (fr) Turboreacteur pour aeronef, aeronef muni d'un tel turboreacteur, et procede de montage d'un tel turboreacteur sur un aeronef
TR200201649T2 (tr) Düz rulman ve böyle bir düz rulmana sahip rüzgar enerjisi tesisi
MX2009013424A (es) Elemento mezclador estatico.
ATE478237T1 (de) Turbinenringanordnung für eine gasturbine
EP2290199A3 (de) Gehäuseanordnung für eine Strömungsmaschine
WO2009135120A3 (en) Thrust bearing assembly
EP2028343A3 (de) Turbinenummantelung für Gasturbinenbaugruppen und Verfahren zum Bilden der Ummantelung
RU2008141809A (ru) Контроль зазора у вершины лопаток в турбине высокого давления турбомашины
ATE549244T1 (de) Gondel für ein flugzeugtriebwerk
WO2009106763A3 (fr) Structure 12 heures pour inverseur de poussée notamment à grilles
WO2008039216A3 (en) Turbocharger turbine and shaft assembly
BR112012013131A2 (pt) estrutura de suporte para uma nacela de motor turbojato, nacela de aeronaves.
EP1801390A3 (de) Enteisungsstruktur eines Gasturbinenbauteils
BR112012001965B8 (pt) viga para a suspensão de um turbomotor na estrutura de uma aeronave, utilização de uma viga, e, aeronave
RU2012104645A (ru) Компоновка маслоотделения
US9932831B2 (en) High temperature compliant metallic elements for low contact stress ceramic support
EP2080920A3 (de) Lageranordnung
DE502006008609D1 (de) Hitzeschildanordnung, insbesondere für eine Gasturbine
DE502006003514D1 (de) Lageranordnung
BRPI0814906A2 (pt) "vedação"
SG130114A1 (en) Turbine airfoil platform platypus for low buttress stress