BRPI0908165A8 - distribuidor setorizado para uma turbomáquina, turbina baixa-pressão de turbomáquina e turbomáquina tal como um turborreator ou um turbopropulsor de avião - Google Patents
distribuidor setorizado para uma turbomáquina, turbina baixa-pressão de turbomáquina e turbomáquina tal como um turborreator ou um turbopropulsor de aviãoInfo
- Publication number
- BRPI0908165A8 BRPI0908165A8 BRPI0908165A BRPI0908165A BRPI0908165A8 BR PI0908165 A8 BRPI0908165 A8 BR PI0908165A8 BR PI0908165 A BRPI0908165 A BR PI0908165A BR PI0908165 A BRPI0908165 A BR PI0908165A BR PI0908165 A8 BRPI0908165 A8 BR PI0908165A8
- Authority
- BR
- Brazil
- Prior art keywords
- turbocharger
- partition
- turbojet
- low
- airplane turboprop
- 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
- 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
- F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
-
- 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
- F01D11/001—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between stator blade and rotor
-
- 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
- F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
-
- 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
- F05D2230/00—Manufacture
- F05D2230/60—Assembly methods
-
- 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)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
distribuidor setorizado para uma turbomáquina, turbina baixa-pressão de turbomáquina e turbomáquina tal como um turborreator ou um turbopropulsor de avião distribuidor setorizado (112) para uma turbomáquina, compreendendo duas plataformas coaxiais ligadas entre si por lâminas radiais, a plataforma interna (130) sendo ligada a uma divisória anular (138) de suspensão de um suporte anular (140) portando elementos (136) de material sujeito à abrasão, este suporte deslizando circunferencialmente sobre a divisória e comportando meios cooperando com meios correspondentes da periferia interna da divisória para assegurar a retenção radial do suporte sobre esta divisória.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0801499A FR2928961B1 (fr) | 2008-03-19 | 2008-03-19 | Distributeur sectorise pour une turbomachine. |
PCT/FR2009/000277 WO2009125078A2 (fr) | 2008-03-19 | 2009-03-17 | Distributeur sectorisé pour une turbomachine |
Publications (3)
Publication Number | Publication Date |
---|---|
BRPI0908165A2 BRPI0908165A2 (pt) | 2015-12-15 |
BRPI0908165A8 true BRPI0908165A8 (pt) | 2019-01-29 |
BRPI0908165B1 BRPI0908165B1 (pt) | 2019-12-03 |
Family
ID=39832406
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BRPI0908165 BRPI0908165B1 (pt) | 2008-03-19 | 2009-03-17 | distribuidor setorizado para uma turbomáquina, turbina baixa-pressão de turbomáquina e turbomáquina tal como um turborreator ou um turbopropulsor de avião |
Country Status (9)
Country | Link |
---|---|
US (1) | US8602726B2 (pt) |
EP (1) | EP2252772B1 (pt) |
JP (1) | JP5759363B2 (pt) |
CN (1) | CN101970804B (pt) |
BR (1) | BRPI0908165B1 (pt) |
CA (1) | CA2715454C (pt) |
FR (1) | FR2928961B1 (pt) |
RU (1) | RU2494264C2 (pt) |
WO (1) | WO2009125078A2 (pt) |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2971022B1 (fr) * | 2011-02-02 | 2013-01-04 | Snecma | Etage redresseur de compresseur pour une turbomachine |
FR2979662B1 (fr) * | 2011-09-07 | 2013-09-27 | Snecma | Procede de fabrication d'un secteur de distributeur de turbine ou redresseur de compresseur en materiau composite pour turbomachine et turbine ou compresseur incorporant un distributeur ou un redresseur forme de tels secteurs |
FR2988429B1 (fr) * | 2012-03-26 | 2017-02-24 | Snecma | Aubage de turbomachine avec couronne interne rapportee et assemblage simplifie |
EP2722486B1 (de) * | 2012-10-17 | 2016-12-07 | MTU Aero Engines AG | Dichtungsträger für eine Leitschaufelanordnung |
FR3001252B1 (fr) * | 2013-01-23 | 2015-02-13 | Snecma | Aubage fixe de distribution de flux comprenant une plate-forme interne a renforts integres |
FR3036436B1 (fr) * | 2015-05-22 | 2020-01-24 | Safran Ceramics | Ensemble d'anneau de turbine avec maintien par brides |
EP3290642A1 (de) * | 2016-08-31 | 2018-03-07 | Siemens Aktiengesellschaft | Ringsegment für eine turbine und anordnung zur äusseren be-grenzung eines strömungspfades einer turbine |
DE102017209420A1 (de) * | 2017-06-02 | 2018-12-06 | MTU Aero Engines AG | Dichtungsanordnung mit angeschweißtem Dichtungsblech, Strömungsmaschine und Herstellungsverfahren |
FR3091311B1 (fr) * | 2018-12-31 | 2021-04-09 | Safran Aircraft Engines | Distributeur pour turbine, turbine de turbomachine équipée de ce distributeur et turbomachine équipée de cette turbine. |
IT201900013218A1 (it) * | 2019-07-29 | 2021-01-29 | Ge Avio Srl | Fascia interna per motore a turbina. |
CN111561473B (zh) * | 2020-05-25 | 2021-10-01 | 中国航发沈阳发动机研究所 | 一种风扇静子机匣结构 |
FR3113298B1 (fr) * | 2020-08-10 | 2023-09-01 | Safran Aircraft Engines | Porte-abradable d’un distributeur basse pression comprenant une unique tôle |
FR3120911A1 (fr) * | 2021-03-16 | 2022-09-23 | Safran Aircraft Engines | Aube comprenant un membre d’attache résistant au frottement et roue mobile comprenant une telle aube d’une turbine axiale de turbomachine |
Family Cites Families (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3941500A (en) * | 1974-06-10 | 1976-03-02 | Westinghouse Electric Corporation | Turbomachine interstage seal assembly |
FR2452590A1 (fr) * | 1979-03-27 | 1980-10-24 | Snecma | Garniture d'etancheite amovible pour segment de distributeur de turbomachine |
FR2524934B1 (fr) * | 1982-04-08 | 1986-12-26 | Snecma | Dispositif de butee de securite pour pivot d'aubes de stator a calage variable |
FR2556410B1 (fr) * | 1983-12-07 | 1986-09-12 | Snecma | Dispositif de centrage de l'anneau interieur d'un stator a ailettes a calage variable |
CN1006512B (zh) * | 1985-07-10 | 1990-01-17 | 阿尔斯汤姆大西洋有限公司 | 涡轮发电机转子励磁绕组-端的护环下面的一种冷却气体分配装置 |
US4767267A (en) * | 1986-12-03 | 1988-08-30 | General Electric Company | Seal assembly |
US4897021A (en) * | 1988-06-02 | 1990-01-30 | United Technologies Corporation | Stator vane asssembly for an axial flow rotary machine |
US5062767A (en) * | 1990-04-27 | 1991-11-05 | The United States Of America As Represented By The Secretary Of The Air Force | Segmented composite inner shrouds |
US5215435A (en) * | 1991-10-28 | 1993-06-01 | General Electric Company | Angled cooling air bypass slots in honeycomb seals |
FR2691749B1 (fr) * | 1992-05-27 | 1994-07-22 | Snecma | Dispositif d'etancheite entre des etages d'aubes et un tambour tournant notamment pour eviter les fuites autour des etages d'aubes de redresseur . |
US5346362A (en) * | 1993-04-26 | 1994-09-13 | United Technologies Corporation | Mechanical damper |
US5749701A (en) * | 1996-10-28 | 1998-05-12 | General Electric Company | Interstage seal assembly for a turbine |
US6139264A (en) * | 1998-12-07 | 2000-10-31 | General Electric Company | Compressor interstage seal |
ITMI991206A1 (it) * | 1999-05-31 | 2000-12-01 | Nuovo Pignone Spa | Dispositivo di supporto e bloccaggio per ugelli di uno stadio ad altapressione in turbine a gas |
FR2830873B1 (fr) * | 2001-10-16 | 2004-01-16 | Snecma Moteurs | Procede de protection par aluminisation de pieces metalliques constituees au moins en partie par une structure en nid d'abeilles |
US6901821B2 (en) * | 2001-11-20 | 2005-06-07 | United Technologies Corporation | Stator damper anti-rotation assembly |
FR2835563B1 (fr) * | 2002-02-07 | 2004-04-02 | Snecma Moteurs | Agencement d'accrochage de secteurs en arc de cercle de distributeur porteur d'aubes |
US6769865B2 (en) * | 2002-03-22 | 2004-08-03 | General Electric Company | Band cooled turbine nozzle |
US7033135B2 (en) * | 2003-11-10 | 2006-04-25 | General Electric Company | Method and apparatus for distributing fluid into a turbomachine |
FR2865002B1 (fr) * | 2004-01-12 | 2006-05-05 | Snecma Moteurs | Turboreacteur a double flux comprenant un support de distribution de servitudes et le support de distribution de servitudes. |
US7334983B2 (en) * | 2005-10-27 | 2008-02-26 | United Technologies Corporation | Integrated bladed fluid seal |
US7635251B2 (en) * | 2006-06-10 | 2009-12-22 | United Technologies Corporation | Stator assembly for a rotary machine |
US7837437B2 (en) * | 2007-03-07 | 2010-11-23 | General Electric Company | Turbine nozzle segment and repair method |
-
2008
- 2008-03-19 FR FR0801499A patent/FR2928961B1/fr active Active
-
2009
- 2009-03-17 CA CA2715454A patent/CA2715454C/fr active Active
- 2009-03-17 RU RU2010142483/06A patent/RU2494264C2/ru active
- 2009-03-17 JP JP2011500251A patent/JP5759363B2/ja active Active
- 2009-03-17 CN CN200980108026.5A patent/CN101970804B/zh active Active
- 2009-03-17 WO PCT/FR2009/000277 patent/WO2009125078A2/fr active Application Filing
- 2009-03-17 US US12/922,460 patent/US8602726B2/en active Active
- 2009-03-17 BR BRPI0908165 patent/BRPI0908165B1/pt active IP Right Grant
- 2009-03-17 EP EP09729986.1A patent/EP2252772B1/fr active Active
Also Published As
Publication number | Publication date |
---|---|
CA2715454C (fr) | 2016-09-06 |
RU2010142483A (ru) | 2012-04-27 |
CA2715454A1 (fr) | 2009-10-15 |
BRPI0908165B1 (pt) | 2019-12-03 |
FR2928961A1 (fr) | 2009-09-25 |
US8602726B2 (en) | 2013-12-10 |
BRPI0908165A2 (pt) | 2015-12-15 |
CN101970804B (zh) | 2014-01-29 |
JP2011515610A (ja) | 2011-05-19 |
RU2494264C2 (ru) | 2013-09-27 |
JP5759363B2 (ja) | 2015-08-05 |
FR2928961B1 (fr) | 2015-11-13 |
CN101970804A (zh) | 2011-02-09 |
US20110052380A1 (en) | 2011-03-03 |
WO2009125078A2 (fr) | 2009-10-15 |
WO2009125078A3 (fr) | 2009-11-26 |
EP2252772A2 (fr) | 2010-11-24 |
EP2252772B1 (fr) | 2013-08-07 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
B06F | Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette] | ||
B06T | Formal requirements before examination [chapter 6.20 patent gazette] | ||
B09A | Decision: intention to grant [chapter 9.1 patent gazette] | ||
B16A | Patent or certificate of addition of invention granted [chapter 16.1 patent gazette] |
Free format text: PRAZO DE VALIDADE: 10 (DEZ) ANOS CONTADOS A PARTIR DE 03/12/2019, OBSERVADAS AS CONDICOES LEGAIS. (CO) 10 (DEZ) ANOS CONTADOS A PARTIR DE 03/12/2019, OBSERVADAS AS CONDICOES LEGAIS |