BR112012012393A2 - isolamento de uma borda circunferencial de um cárter externo de turbomáquina de um setor de anel correspondente - Google Patents
isolamento de uma borda circunferencial de um cárter externo de turbomáquina de um setor de anel correspondenteInfo
- Publication number
- BR112012012393A2 BR112012012393A2 BR112012012393A BR112012012393A BR112012012393A2 BR 112012012393 A2 BR112012012393 A2 BR 112012012393A2 BR 112012012393 A BR112012012393 A BR 112012012393A BR 112012012393 A BR112012012393 A BR 112012012393A BR 112012012393 A2 BR112012012393 A2 BR 112012012393A2
- Authority
- BR
- Brazil
- Prior art keywords
- circumferential edge
- ring sector
- isolation
- external
- corresponding ring
- Prior art date
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
- F01D11/005—Sealing means between non relatively rotating elements
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Supercharger (AREA)
Abstract
isolamento de uma borda circunferencial de um cárter externo de turbomáquina de um setor de anel correspondente a invenção refere-se a um estágio de turbina de uma turbomáquina, compreendendo uma roda de rotor montada no interior de um anel setorizado portado por um cárter externo (4), o cárter externo (4) comportando pelo menos uma borda circunferencial (22) alojada nesta cavidade para fixação da extremidade a jusante (13) do setor de anel (6), caracterizado pelo fota de que a parede de fundo (16) da cavidade anular do setor de anel (6) permanece afastada radialmente da borda circunferencial (22) do cárter externo (4), de modo a dispor um espaço termicamente isolante entre as duas e comporta meios de posicionamento radial (24) sobre esta borda circunferencial (22).
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR09/05657 | 2009-11-25 | ||
FR0905657A FR2952965B1 (fr) | 2009-11-25 | 2009-11-25 | Isolation d'un rebord circonferentiel d'un carter externe de turbomachine vis-a-vis d'un secteur d'anneau correspondant |
PCT/FR2010/052495 WO2011064496A1 (fr) | 2009-11-25 | 2010-11-24 | Isolation d'un rebord circonférentiel d'un carter externe de turbomachine vis-à-vis d'un secteur d'anneau correspondant |
Publications (2)
Publication Number | Publication Date |
---|---|
BR112012012393A2 true BR112012012393A2 (pt) | 2016-04-12 |
BR112012012393B1 BR112012012393B1 (pt) | 2020-11-10 |
Family
ID=42312955
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112012012393-9A BR112012012393B1 (pt) | 2009-11-25 | 2010-11-24 | estágio de turbina de uma turbomáquina, e, turbomáquina |
Country Status (9)
Country | Link |
---|---|
US (1) | US8961117B2 (pt) |
EP (1) | EP2504529B1 (pt) |
JP (1) | JP5771217B2 (pt) |
CN (1) | CN102630268B (pt) |
BR (1) | BR112012012393B1 (pt) |
CA (1) | CA2781936C (pt) |
FR (1) | FR2952965B1 (pt) |
RU (1) | RU2548535C2 (pt) |
WO (1) | WO2011064496A1 (pt) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA2870765C (en) * | 2012-04-27 | 2017-03-28 | General Electric Company | System and method of limiting axial movement between a hanger and a fairing assembly in a turbine assembly |
EP2696037B1 (de) * | 2012-08-09 | 2017-03-01 | MTU Aero Engines AG | Abdichtung des Strömungskanals einer Strömungsmaschine |
JP6233578B2 (ja) * | 2013-12-05 | 2017-11-22 | 株式会社Ihi | タービン |
US10648362B2 (en) | 2017-02-24 | 2020-05-12 | General Electric Company | Spline for a turbine engine |
US10655495B2 (en) | 2017-02-24 | 2020-05-19 | General Electric Company | Spline for a turbine engine |
US20180347399A1 (en) * | 2017-06-01 | 2018-12-06 | Pratt & Whitney Canada Corp. | Turbine shroud with integrated heat shield |
FR3071273B1 (fr) * | 2017-09-21 | 2019-08-30 | Safran Aircraft Engines | Ensemble d'etancheite de turbine pour turbomachine |
US10982559B2 (en) * | 2018-08-24 | 2021-04-20 | General Electric Company | Spline seal with cooling features for turbine engines |
FR3096395B1 (fr) * | 2019-05-21 | 2021-04-23 | Safran Aircraft Engines | Turbine pour une turbomachine, telle qu’un turboréacteur ou un turbopropulseur d’avion |
FR3100838B1 (fr) * | 2019-09-13 | 2021-10-01 | Safran Aircraft Engines | Anneau d’etancheite de turbomachine |
FR3109402B1 (fr) * | 2020-04-15 | 2022-07-15 | Safran Aircraft Engines | Turbine pour une turbomachine |
Family Cites Families (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4687413A (en) * | 1985-07-31 | 1987-08-18 | United Technologies Corporation | Gas turbine engine assembly |
FR2635562B1 (fr) * | 1988-08-18 | 1993-12-24 | Snecma | Anneau de stator de turbine associe a un support de liaison au carter de turbine |
US5553999A (en) * | 1995-06-06 | 1996-09-10 | General Electric Company | Sealable turbine shroud hanger |
US5641267A (en) * | 1995-06-06 | 1997-06-24 | General Electric Company | Controlled leakage shroud panel |
JP3592932B2 (ja) * | 1998-05-22 | 2004-11-24 | 三菱重工業株式会社 | ガスタービン静翼と翼環の接触構造 |
DE19938443A1 (de) | 1999-08-13 | 2001-02-15 | Abb Alstom Power Ch Ag | Befestigungs- und Fixierungsvorrichtung |
US6435820B1 (en) * | 1999-08-25 | 2002-08-20 | General Electric Company | Shroud assembly having C-clip retainer |
FR2800797B1 (fr) * | 1999-11-10 | 2001-12-07 | Snecma | Assemblage d'un anneau bordant une turbine a la structure de turbine |
DE10122464C1 (de) * | 2001-05-09 | 2002-03-07 | Mtu Aero Engines Gmbh | Mantelring |
US6733235B2 (en) * | 2002-03-28 | 2004-05-11 | General Electric Company | Shroud segment and assembly for a turbine engine |
US6902371B2 (en) * | 2002-07-26 | 2005-06-07 | General Electric Company | Internal low pressure turbine case cooling |
US20040219011A1 (en) | 2003-05-02 | 2004-11-04 | General Electric Company | High pressure turbine elastic clearance control system and method |
US7186078B2 (en) * | 2003-07-04 | 2007-03-06 | Ishikawajima-Harima Heavy Industries Co., Ltd. | Turbine shroud segment |
JP4269829B2 (ja) * | 2003-07-04 | 2009-05-27 | 株式会社Ihi | シュラウドセグメント |
JP4200846B2 (ja) * | 2003-07-04 | 2008-12-24 | 株式会社Ihi | シュラウドセグメント |
US6942203B2 (en) * | 2003-11-04 | 2005-09-13 | General Electric Company | Spring mass damper system for turbine shrouds |
FR2867224B1 (fr) * | 2004-03-04 | 2006-05-19 | Snecma Moteurs | Dispositif de maintien axial de secteur d'entretoise pour anneau d'une turbine haute-pression de turbomachine |
US7217089B2 (en) * | 2005-01-14 | 2007-05-15 | Pratt & Whitney Canada Corp. | Gas turbine engine shroud sealing arrangement |
FR2887920B1 (fr) * | 2005-06-29 | 2010-09-10 | Snecma | Dispositif de fixation de secteurs d'anneau sur un carter de turbine |
FR2899273B1 (fr) * | 2006-03-30 | 2012-08-17 | Snecma | Dispositif de fixation de secteurs d'anneau sur un carter de turbine d'une turbomachine |
FR2899275A1 (fr) * | 2006-03-30 | 2007-10-05 | Snecma Sa | Dispositif de fixation de secteurs d'anneau sur un carter de turbine d'une turbomachine |
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 |
-
2009
- 2009-11-25 FR FR0905657A patent/FR2952965B1/fr not_active Expired - Fee Related
-
2010
- 2010-11-24 WO PCT/FR2010/052495 patent/WO2011064496A1/fr active Application Filing
- 2010-11-24 EP EP10805261.4A patent/EP2504529B1/fr active Active
- 2010-11-24 JP JP2012540478A patent/JP5771217B2/ja active Active
- 2010-11-24 RU RU2012126095/06A patent/RU2548535C2/ru active
- 2010-11-24 CN CN201080053721.9A patent/CN102630268B/zh active Active
- 2010-11-24 US US13/511,021 patent/US8961117B2/en active Active
- 2010-11-24 BR BR112012012393-9A patent/BR112012012393B1/pt active IP Right Grant
- 2010-11-24 CA CA2781936A patent/CA2781936C/fr active Active
Also Published As
Publication number | Publication date |
---|---|
EP2504529A1 (fr) | 2012-10-03 |
RU2012126095A (ru) | 2013-12-27 |
US20120288362A1 (en) | 2012-11-15 |
RU2548535C2 (ru) | 2015-04-20 |
CA2781936A1 (fr) | 2011-06-03 |
CN102630268A (zh) | 2012-08-08 |
WO2011064496A1 (fr) | 2011-06-03 |
CN102630268B (zh) | 2015-07-08 |
US8961117B2 (en) | 2015-02-24 |
CA2781936C (fr) | 2017-12-12 |
JP2013512382A (ja) | 2013-04-11 |
FR2952965B1 (fr) | 2012-03-09 |
EP2504529B1 (fr) | 2013-10-09 |
FR2952965A1 (fr) | 2011-05-27 |
JP5771217B2 (ja) | 2015-08-26 |
BR112012012393B1 (pt) | 2020-11-10 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
B06F | Objections, documents and/or translations needed after an examination request according art. 34 industrial property law | ||
B06U | Preliminary requirement: requests with searches performed by other patent offices: suspension of the patent application procedure | ||
B09A | Decision: intention to grant | ||
B16A | Patent or certificate of addition of invention granted |
Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 24/11/2010, OBSERVADAS AS CONDICOES LEGAIS. |