FR2852053B1 - Turbine haute pression pour turbomachine - Google Patents

Turbine haute pression pour turbomachine

Info

Publication number
FR2852053B1
FR2852053B1 FR0302783A FR0302783A FR2852053B1 FR 2852053 B1 FR2852053 B1 FR 2852053B1 FR 0302783 A FR0302783 A FR 0302783A FR 0302783 A FR0302783 A FR 0302783A FR 2852053 B1 FR2852053 B1 FR 2852053B1
Authority
FR
France
Prior art keywords
turbomachine
high pressure
pressure turbine
turbine
pressure
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 - Fee Related
Application number
FR0302783A
Other languages
English (en)
Other versions
FR2852053A1 (fr
Inventor
Marc Roger Marchi
Paul Rodrigues
Patrice Jean Marc Rosset
Jean Claude Christian Taillant
Jean Baptiste Arilla
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
Priority to FR0302783A priority Critical patent/FR2852053B1/fr
Priority to JP2004056027A priority patent/JP4129240B2/ja
Priority to US10/790,116 priority patent/US7011493B2/en
Priority to CA2459473A priority patent/CA2459473C/fr
Priority to DE602004017921T priority patent/DE602004017921D1/de
Priority to EP04100854A priority patent/EP1455055B1/fr
Priority to ES04100854T priority patent/ES2316922T3/es
Priority to RU2004106713/06A priority patent/RU2347079C2/ru
Priority to UA2004031654A priority patent/UA80536C2/uk
Publication of FR2852053A1 publication Critical patent/FR2852053A1/fr
Application granted granted Critical
Publication of FR2852053B1 publication Critical patent/FR2852053B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • 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
    • 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
    • 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
FR0302783A 2003-03-06 2003-03-06 Turbine haute pression pour turbomachine Expired - Fee Related FR2852053B1 (fr)

Priority Applications (9)

Application Number Priority Date Filing Date Title
FR0302783A FR2852053B1 (fr) 2003-03-06 2003-03-06 Turbine haute pression pour turbomachine
JP2004056027A JP4129240B2 (ja) 2003-03-06 2004-03-01 冷却リングセグメントを備えたターボマシン
US10/790,116 US7011493B2 (en) 2003-03-06 2004-03-02 Turbomachine with cooled ring segments
DE602004017921T DE602004017921D1 (de) 2003-03-06 2004-03-03 Turbomachine mit gekühlten Mantelringsegmenten
CA2459473A CA2459473C (fr) 2003-03-06 2004-03-03 Turbomachine a segments d'anneaux refroidis
EP04100854A EP1455055B1 (fr) 2003-03-06 2004-03-03 Turbomachine disposant de secteurs d'anneau refroidis
ES04100854T ES2316922T3 (es) 2003-03-06 2004-03-03 Turbomaquina que dispone de sectores de anillo refrigerados.
RU2004106713/06A RU2347079C2 (ru) 2003-03-06 2004-03-05 Турбомашина с охлаждаемыми кольцевыми сегментами
UA2004031654A UA80536C2 (en) 2003-03-06 2004-03-05 Turbo-machine with cooled ring segments

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0302783A FR2852053B1 (fr) 2003-03-06 2003-03-06 Turbine haute pression pour turbomachine

Publications (2)

Publication Number Publication Date
FR2852053A1 FR2852053A1 (fr) 2004-09-10
FR2852053B1 true FR2852053B1 (fr) 2007-12-28

Family

ID=32799640

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0302783A Expired - Fee Related FR2852053B1 (fr) 2003-03-06 2003-03-06 Turbine haute pression pour turbomachine

Country Status (9)

Country Link
US (1) US7011493B2 (fr)
EP (1) EP1455055B1 (fr)
JP (1) JP4129240B2 (fr)
CA (1) CA2459473C (fr)
DE (1) DE602004017921D1 (fr)
ES (1) ES2316922T3 (fr)
FR (1) FR2852053B1 (fr)
RU (1) RU2347079C2 (fr)
UA (1) UA80536C2 (fr)

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FR2931196B1 (fr) * 2008-05-16 2010-06-18 Snecma Organe de verrouillage de secteurs d'anneau sur un carter de turbomachine, comprenant des passages radiaux permettant sa prehension
FR2931197B1 (fr) * 2008-05-16 2010-06-18 Snecma Organe de verrouillage de secteurs d'anneau sur un carter de turbomachine, comprenant des passages axiaux pour sa prehension
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US9133724B2 (en) * 2012-01-09 2015-09-15 General Electric Company Turbomachine component including a cover plate
US9316117B2 (en) 2012-01-30 2016-04-19 United Technologies Corporation Internally cooled spoke
WO2013163581A1 (fr) * 2012-04-27 2013-10-31 General Electric Company Système et procédé pour limiter le mouvement axial entre un étrier et un ensemble carénage dans un ensemble turbine
GB201213039D0 (en) * 2012-07-23 2012-09-05 Rolls Royce Plc Fastener
US20140271154A1 (en) * 2013-03-14 2014-09-18 General Electric Company Casing for turbine engine having a cooling unit
BR112015028691A2 (pt) 2013-05-17 2017-07-25 Gen Electric sistema de sustentação de invólucro
WO2015088869A1 (fr) 2013-12-12 2015-06-18 General Electric Company Système de support de carénage cmc
FR3015554B1 (fr) * 2013-12-19 2016-01-29 Snecma Secteur d'anneau de turbine pour turbomachine d'aeronef, presentant des orifices de prehension ameliores
US10465558B2 (en) 2014-06-12 2019-11-05 General Electric Company Multi-piece shroud hanger assembly
JP6363232B2 (ja) 2014-06-12 2018-07-25 ゼネラル・エレクトリック・カンパニイ シュラウドハンガーアセンブリ
JP6775425B2 (ja) 2014-06-12 2020-10-28 ゼネラル・エレクトリック・カンパニイ シュラウドハンガーアセンブリ
EP3045674B1 (fr) * 2015-01-15 2018-11-21 Rolls-Royce Corporation Enveloppe de turbine avec inserts tubulaires de localisation de patins
US9856750B2 (en) * 2015-01-16 2018-01-02 United Technologies Corporation Cooling passages for a mid-turbine frame
US9874104B2 (en) 2015-02-27 2018-01-23 General Electric Company Method and system for a ceramic matrix composite shroud hanger assembly
US10422244B2 (en) * 2015-03-16 2019-09-24 General Electric Company System for cooling a turbine shroud
US10184352B2 (en) * 2015-06-29 2019-01-22 Rolls-Royce North American Technologies Inc. Turbine shroud segment with integrated cooling air distribution system
GB201518131D0 (en) * 2015-10-14 2015-11-25 Rolls Royce Plc Shroud assembly for a gas turbine engine
US10132194B2 (en) * 2015-12-16 2018-11-20 Rolls-Royce North American Technologies Inc. Seal segment low pressure cooling protection system
US20170248030A1 (en) * 2016-02-26 2017-08-31 General Electric Company Encapsulated Cooling for Turbine Shrouds
US10801354B2 (en) * 2016-04-25 2020-10-13 Raytheon Technologies Corporation Gas turbine engine having high pressure compressor case active clearance control system
US11021986B2 (en) * 2018-03-20 2021-06-01 Raytheon Technologies Corporation Seal assembly for gas turbine engine
US10774742B2 (en) * 2018-03-21 2020-09-15 Raytheon Technologies Corporation Flared anti-vortex tube rotor insert
US10753220B2 (en) * 2018-06-27 2020-08-25 Raytheon Technologies Corporation Gas turbine engine component
US10822986B2 (en) * 2019-01-31 2020-11-03 General Electric Company Unitary body turbine shrouds including internal cooling passages
US10927693B2 (en) 2019-01-31 2021-02-23 General Electric Company Unitary body turbine shroud for turbine systems
US10830050B2 (en) 2019-01-31 2020-11-10 General Electric Company Unitary body turbine shrouds including structural breakdown and collapsible features
US10927694B2 (en) * 2019-03-13 2021-02-23 Raytheon Technologies Corporation BOAS carrier with cooling supply
US11131215B2 (en) * 2019-11-19 2021-09-28 Rolls-Royce North American Technologies Inc. Turbine shroud cartridge assembly with sealing features
KR102299165B1 (ko) * 2020-03-31 2021-09-07 두산중공업 주식회사 터빈 블레이드의 팁 클리어런스 제어장치 및 이를 포함하는 가스 터빈
CN114278385A (zh) * 2021-12-16 2022-04-05 北京航空航天大学 一种带有遮热板和空气夹层的新型涡轮盘腔隔热结构

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Also Published As

Publication number Publication date
RU2004106713A (ru) 2005-08-10
EP1455055B1 (fr) 2008-11-26
CA2459473C (fr) 2011-11-08
US7011493B2 (en) 2006-03-14
EP1455055A1 (fr) 2004-09-08
JP4129240B2 (ja) 2008-08-06
DE602004017921D1 (de) 2009-01-08
JP2004270694A (ja) 2004-09-30
UA80536C2 (en) 2007-10-10
ES2316922T3 (es) 2009-04-16
RU2347079C2 (ru) 2009-02-20
FR2852053A1 (fr) 2004-09-10
CA2459473A1 (fr) 2004-09-06
US20040219009A1 (en) 2004-11-04

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Legal Events

Date Code Title Description
CD Change of name or company name
ST Notification of lapse

Effective date: 20101130