BRPI0920928A2 - setor de pás de distribuidor de turbina destinado a ser levado por um cárter de turbina de uma turbomáquina aeronáutica, módulo de turbina e motor aeronáutico - Google Patents
setor de pás de distribuidor de turbina destinado a ser levado por um cárter de turbina de uma turbomáquina aeronáutica, módulo de turbina e motor aeronáuticoInfo
- Publication number
- BRPI0920928A2 BRPI0920928A2 BRPI0920928A BRPI0920928A BRPI0920928A2 BR PI0920928 A2 BRPI0920928 A2 BR PI0920928A2 BR PI0920928 A BRPI0920928 A BR PI0920928A BR PI0920928 A BRPI0920928 A BR PI0920928A BR PI0920928 A2 BRPI0920928 A2 BR PI0920928A2
- Authority
- BR
- Brazil
- Prior art keywords
- turbine
- aeronautical
- turbocharger
- carried
- crankcase
- 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
- 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
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
- F01D5/3092—Protective layers between blade root and rotor disc surfaces, e.g. anti-friction layers
-
- 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
- F05D2230/50—Building or constructing in particular ways
- F05D2230/54—Building or constructing in particular ways by sheet metal manufacturing
-
- 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
- F05D2300/509—Self lubricating materials; Solid lubricants
-
- 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)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0858028A FR2938872B1 (fr) | 2008-11-26 | 2008-11-26 | Dispositif anti-usure pour aubes d'un distributeur de turbine d'une turbomachine aeronautique |
| PCT/EP2009/065860 WO2010060938A1 (fr) | 2008-11-26 | 2009-11-25 | Dispositif anti-usure pour aubes d'un distributeur de turbine d'une turbomachine aeronautique |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| BRPI0920928A2 true BRPI0920928A2 (pt) | 2015-12-29 |
| BRPI0920928B1 BRPI0920928B1 (pt) | 2020-04-07 |
Family
ID=40897324
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BRPI0920928A BRPI0920928B1 (pt) | 2008-11-26 | 2009-11-25 | setor de pás de distribuidor de turbina destinado a ser levado por um cárter de turbina de uma turbomáquina aeronáutica, módulo de turbina e motor aeronáutico |
Country Status (9)
| Country | Link |
|---|---|
| US (1) | US9062553B2 (pt) |
| EP (1) | EP2368016B1 (pt) |
| JP (1) | JP5466244B2 (pt) |
| CN (1) | CN102227546B (pt) |
| BR (1) | BRPI0920928B1 (pt) |
| CA (1) | CA2744297C (pt) |
| FR (1) | FR2938872B1 (pt) |
| RU (1) | RU2506432C2 (pt) |
| WO (1) | WO2010060938A1 (pt) |
Families Citing this family (43)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2477825B (en) * | 2010-09-23 | 2015-04-01 | Rolls Royce Plc | Anti fret liner assembly |
| FR2967730B1 (fr) * | 2010-11-24 | 2015-05-15 | Snecma | Etage de compresseur dans une turbomachine |
| US8926270B2 (en) * | 2010-12-17 | 2015-01-06 | General Electric Company | Low-ductility turbine shroud flowpath and mounting arrangement therefor |
| US8899914B2 (en) * | 2012-01-05 | 2014-12-02 | United Technologies Corporation | Stator vane integrated attachment liner and spring damper |
| FR2986836B1 (fr) * | 2012-02-09 | 2016-01-01 | Snecma | Tole annulaire anti-usure pour une turbomachine |
| US9051849B2 (en) * | 2012-02-13 | 2015-06-09 | United Technologies Corporation | Anti-rotation stator segments |
| US10240467B2 (en) * | 2012-08-03 | 2019-03-26 | United Technologies Corporation | Anti-rotation lug for a gas turbine engine stator assembly |
| FR2995340B1 (fr) * | 2012-09-12 | 2026-03-06 | Snecma | Tole de protection thermique avec butee radiale, notamment pour distributeur de turbomachine |
| US9353649B2 (en) * | 2013-01-08 | 2016-05-31 | United Technologies Corporation | Wear liner spring seal |
| US9796055B2 (en) * | 2013-02-17 | 2017-10-24 | United Technologies Corporation | Turbine case retention hook with insert |
| CA2897965C (en) * | 2013-03-11 | 2020-02-25 | Rolls-Royce Corporation | Compliant intermediate component of a gas turbine engine |
| FR3024883B1 (fr) * | 2014-08-14 | 2016-08-05 | Snecma | Module de turbomachine |
| FR3027071B1 (fr) * | 2014-10-13 | 2019-08-23 | Safran Aircraft Engines | Procede d'intervention sur un rotor et clinquant associe |
| US10309257B2 (en) | 2015-03-02 | 2019-06-04 | Rolls-Royce North American Technologies Inc. | Turbine assembly with load pads |
| FR3036432B1 (fr) * | 2015-05-22 | 2019-04-19 | Safran Ceramics | Ensemble d'anneau de turbine avec maintien axial |
| EP3147457B1 (en) * | 2015-09-22 | 2019-01-30 | Ansaldo Energia Switzerland AG | Gas turbine comprising a guide vane and a guide vane carrier |
| US10294813B2 (en) | 2016-03-24 | 2019-05-21 | United Technologies Corporation | Geared unison ring for variable vane actuation |
| US10329946B2 (en) | 2016-03-24 | 2019-06-25 | United Technologies Corporation | Sliding gear actuation for variable vanes |
| US10301962B2 (en) | 2016-03-24 | 2019-05-28 | United Technologies Corporation | Harmonic drive for shaft driving multiple stages of vanes via gears |
| US10443430B2 (en) | 2016-03-24 | 2019-10-15 | United Technologies Corporation | Variable vane actuation with rotating ring and sliding links |
| US10443431B2 (en) | 2016-03-24 | 2019-10-15 | United Technologies Corporation | Idler gear connection for multi-stage variable vane actuation |
| US10458271B2 (en) | 2016-03-24 | 2019-10-29 | United Technologies Corporation | Cable drive system for variable vane operation |
| US10329947B2 (en) | 2016-03-24 | 2019-06-25 | United Technologies Corporation | 35Geared unison ring for multi-stage variable vane actuation |
| US10107130B2 (en) | 2016-03-24 | 2018-10-23 | United Technologies Corporation | Concentric shafts for remote independent variable vane actuation |
| US10190599B2 (en) | 2016-03-24 | 2019-01-29 | United Technologies Corporation | Drive shaft for remote variable vane actuation |
| US10415596B2 (en) | 2016-03-24 | 2019-09-17 | United Technologies Corporation | Electric actuation for variable vanes |
| US10288087B2 (en) | 2016-03-24 | 2019-05-14 | United Technologies Corporation | Off-axis electric actuation for variable vanes |
| US11066951B2 (en) | 2016-04-21 | 2021-07-20 | Raytheon Technologies Corporation | Wear liner for fixed stator vanes |
| FR3060051B1 (fr) * | 2016-12-14 | 2018-12-07 | Safran Aircraft Engines | Turbine pour turbomachine |
| FR3061511B1 (fr) * | 2017-01-05 | 2020-12-25 | Safran Aircraft Engines | Turbine pour turbomachine |
| US10316861B2 (en) * | 2017-01-19 | 2019-06-11 | United Technologies Corporation | Two-piece multi-surface wear liner |
| US20180355741A1 (en) * | 2017-02-24 | 2018-12-13 | General Electric Company | Spline for a turbine engine |
| US11466700B2 (en) * | 2017-02-28 | 2022-10-11 | Unison Industries, Llc | Fan casing and mount bracket for oil cooler |
| FR3066780B1 (fr) * | 2017-05-24 | 2019-07-19 | Safran Aircraft Engines | Piece amovible anti-usure pour talon d'aube |
| FR3076852B1 (fr) * | 2018-01-16 | 2020-01-31 | Safran Aircraft Engines | Anneau de turbomachine |
| FR3085412B1 (fr) * | 2018-08-31 | 2020-12-04 | Safran Aircraft Engines | Secteur de distributeur d'une turbomachine comprenant une encoche anti-rotation a insert d'usure |
| DE102020200073A1 (de) * | 2020-01-07 | 2021-07-08 | Siemens Aktiengesellschaft | Leitschaufelkranz |
| FR3113923B1 (fr) | 2020-09-04 | 2023-12-15 | Safran Aircraft Engines | Turbine pour turbomachine comprenant des clinquants de protection thermique |
| FR3116860B1 (fr) | 2020-11-27 | 2026-01-30 | Safran Aircraft Engines | Installation et procede pour l’assemblage des distributeurs d’une turbine |
| FR3116746B1 (fr) | 2020-11-27 | 2023-12-22 | Safran Aircraft Engines | Dispositif automatise d’insertion de plaquettes d’etancheite dans un secteur d’un distributeur de turbine |
| FR3116861B1 (fr) | 2020-11-27 | 2022-10-21 | Safran Aircraft Engines | Dispositif et procede de controle des secteurs pour l’assemblage de distributeurs d’une turbine |
| CN114718758B (zh) * | 2021-01-05 | 2023-10-31 | 中国航发商用航空发动机有限责任公司 | 反推装置、滑动配合件及其成形方法 |
| US12492640B2 (en) | 2024-05-30 | 2025-12-09 | General Electric Company | Turbine engine including a vane support and a vane |
Family Cites Families (26)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4078922A (en) * | 1975-12-08 | 1978-03-14 | United Technologies Corporation | Oxidation resistant cobalt base alloy |
| US4314792A (en) * | 1978-12-20 | 1982-02-09 | United Technologies Corporation | Turbine seal and vane damper |
| GB2249356B (en) * | 1990-11-01 | 1995-01-18 | Rolls Royce Plc | Shroud liners |
| US5240375A (en) * | 1992-01-10 | 1993-08-31 | General Electric Company | Wear protection system for turbine engine rotor and blade |
| GB9204791D0 (en) * | 1992-03-05 | 1992-04-22 | Rolls Royce Plc | A coated article |
| US5232340A (en) * | 1992-09-28 | 1993-08-03 | General Electric Company | Gas turbine engine stator assembly |
| JPH07247804A (ja) * | 1993-01-07 | 1995-09-26 | General Electric Co <Ge> | ガスタービンエンジン用のロータ及び動翼アセンブリ、並びに多層被覆シム |
| US5333995A (en) * | 1993-08-09 | 1994-08-02 | General Electric Company | Wear shim for a turbine engine |
| EP0750689B1 (en) * | 1994-03-17 | 2002-09-04 | The Westaim Corporation | Low friction cobalt-based coatings for titanium |
| US5738490A (en) * | 1996-05-20 | 1998-04-14 | Pratt & Whitney Canada, Inc. | Gas turbine engine shroud seals |
| GB9815611D0 (en) * | 1998-07-18 | 1998-09-16 | Rolls Royce Plc | Improvements in or relating to turbine cooling |
| RU2171381C2 (ru) * | 1999-05-25 | 2001-07-27 | Открытое акционерное общество "Авиадвигатель" | Сопловой аппарат турбомашины |
| US6431835B1 (en) * | 2000-10-17 | 2002-08-13 | Honeywell International, Inc. | Fan blade compliant shim |
| US6431820B1 (en) * | 2001-02-28 | 2002-08-13 | General Electric Company | Methods and apparatus for cooling gas turbine engine blade tips |
| US6537022B1 (en) * | 2001-10-05 | 2003-03-25 | General Electric Company | Nozzle lock for gas turbine engines |
| US6860722B2 (en) * | 2003-01-31 | 2005-03-01 | General Electric Company | Snap on blade shim |
| US20040261265A1 (en) * | 2003-06-25 | 2004-12-30 | General Electric Company | Method for improving the wear resistance of a support region between a turbine outer case and a supported turbine vane |
| US7040857B2 (en) * | 2004-04-14 | 2006-05-09 | General Electric Company | Flexible seal assembly between gas turbine components and methods of installation |
| US7094026B2 (en) * | 2004-04-29 | 2006-08-22 | General Electric Company | System for sealing an inner retainer segment and support ring in a gas turbine and methods therefor |
| US7172388B2 (en) * | 2004-08-24 | 2007-02-06 | Pratt & Whitney Canada Corp. | Multi-point seal |
| US7360990B2 (en) * | 2004-10-13 | 2008-04-22 | General Electric Company | Methods and apparatus for assembling gas turbine engines |
| US7278821B1 (en) * | 2004-11-04 | 2007-10-09 | General Electric Company | Methods and apparatus for assembling gas turbine engines |
| JP4234107B2 (ja) * | 2005-02-10 | 2009-03-04 | 三菱重工業株式会社 | 可変容量型排気ターボ過給機及び可変ノズル機構構成部材の製造方法 |
| FR2885168A1 (fr) * | 2005-04-27 | 2006-11-03 | Snecma Moteurs Sa | Dispositif d'etancheite pour une enceinte d'une turbomachine, et moteur d'aeronef equipe de celui-ci |
| US8038389B2 (en) * | 2006-01-04 | 2011-10-18 | General Electric Company | Method and apparatus for assembling turbine nozzle assembly |
| US7500824B2 (en) * | 2006-08-22 | 2009-03-10 | General Electric Company | Angel wing abradable seal and sealing method |
-
2008
- 2008-11-26 FR FR0858028A patent/FR2938872B1/fr active Active
-
2009
- 2009-11-25 EP EP09756529.5A patent/EP2368016B1/fr active Active
- 2009-11-25 CN CN200980147572.XA patent/CN102227546B/zh active Active
- 2009-11-25 BR BRPI0920928A patent/BRPI0920928B1/pt active IP Right Grant
- 2009-11-25 US US13/131,036 patent/US9062553B2/en active Active
- 2009-11-25 RU RU2011126208/06A patent/RU2506432C2/ru active
- 2009-11-25 CA CA2744297A patent/CA2744297C/fr active Active
- 2009-11-25 JP JP2011537972A patent/JP5466244B2/ja active Active
- 2009-11-25 WO PCT/EP2009/065860 patent/WO2010060938A1/fr not_active Ceased
Also Published As
| Publication number | Publication date |
|---|---|
| EP2368016A1 (fr) | 2011-09-28 |
| BRPI0920928B1 (pt) | 2020-04-07 |
| RU2011126208A (ru) | 2013-01-10 |
| JP2012510027A (ja) | 2012-04-26 |
| CN102227546B (zh) | 2014-02-19 |
| FR2938872A1 (fr) | 2010-05-28 |
| EP2368016B1 (fr) | 2016-10-12 |
| US9062553B2 (en) | 2015-06-23 |
| RU2506432C2 (ru) | 2014-02-10 |
| US20120128481A1 (en) | 2012-05-24 |
| JP5466244B2 (ja) | 2014-04-09 |
| CN102227546A (zh) | 2011-10-26 |
| WO2010060938A1 (fr) | 2010-06-03 |
| FR2938872B1 (fr) | 2015-11-27 |
| CA2744297C (fr) | 2016-10-11 |
| CA2744297A1 (fr) | 2010-06-03 |
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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 07/04/2020, OBSERVADAS AS CONDICOES LEGAIS. |