BRPI1013342A8 - Conjunto de anel de turbina - Google Patents
Conjunto de anel de turbinaInfo
- Publication number
- BRPI1013342A8 BRPI1013342A8 BRPI1013342A BRPI1013342A BRPI1013342A8 BR PI1013342 A8 BRPI1013342 A8 BR PI1013342A8 BR PI1013342 A BRPI1013342 A BR PI1013342A BR PI1013342 A BRPI1013342 A BR PI1013342A BR PI1013342 A8 BRPI1013342 A8 BR PI1013342A8
- Authority
- BR
- Brazil
- Prior art keywords
- ring
- flanges
- support structure
- turbine
- ring assembly
- Prior art date
Links
Classifications
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- 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
-
- D—TEXTILES; PAPER
- D03—WEAVING
- D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
- D03D25/00—Woven fabrics not otherwise provided for
- D03D25/005—Three-dimensional woven fabrics
-
- 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
-
- 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
- F05D2230/64—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins
- F05D2230/642—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins using maintaining alignment while permitting differential dilatation
-
- 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
- F05D2240/00—Components
- F05D2240/10—Stators
- F05D2240/11—Shroud seal segments
-
- 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
- F05D2300/20—Oxide or non-oxide ceramics
- F05D2300/21—Oxide ceramics
-
- 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
-
- 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)
- Textile Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Saccharide Compounds (AREA)
- Gasket Seals (AREA)
Abstract
CONJUNTO DE ANEL DE TURBINA O conjunto de anel de turbina compreende uma pluralidadede setores de anel (10) em uma única peça de material compósito de matriz cerâmica e uma estrutura de suporte de anel, cada setor de anel tendo uma primeira parte (12) formando base anular com uma face interna definindo a face interna do anel da turbina e uma face externa a partir da qual se estendem duas partes formandoflanges (14, 16), cujas extremidades são encaixadas nos alojamentos da estrutura de suporte de anel. Os setores de anel (10) são de seção sensivelmente em forma de pi e as extremidades (14a, 16a) dos flanges (14, 16) são mantidas sem jogo radial pela estrutura de suporte de anel. Preferivelmente, os flanges (14, 16) têm, em seção meridiana, um comprimento livre pelo menos igual a 3 vezes sua largura média.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0951446A FR2942845B1 (fr) | 2009-03-09 | 2009-03-09 | Ensemble d'anneau de turbine |
FR0951445A FR2942844B1 (fr) | 2009-03-09 | 2009-03-09 | Ensemble d'anneau de turbine avec arret axial |
PCT/FR2010/050342 WO2010103213A1 (fr) | 2009-03-09 | 2010-03-01 | Ensemble d'anneau de turbine |
Publications (2)
Publication Number | Publication Date |
---|---|
BRPI1013342A2 BRPI1013342A2 (pt) | 2016-03-29 |
BRPI1013342A8 true BRPI1013342A8 (pt) | 2016-09-20 |
Family
ID=42237201
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BRPI1013342A BRPI1013342A8 (pt) | 2009-03-09 | 2010-03-01 | Conjunto de anel de turbina |
Country Status (9)
Country | Link |
---|---|
US (1) | US9080463B2 (pt) |
EP (1) | EP2406466B1 (pt) |
JP (1) | JP5646517B2 (pt) |
CN (1) | CN102272419A (pt) |
BR (1) | BRPI1013342A8 (pt) |
CA (1) | CA2750938A1 (pt) |
ES (1) | ES2398727T3 (pt) |
RU (1) | RU2522264C2 (pt) |
WO (1) | WO2010103213A1 (pt) |
Families Citing this family (87)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2957093B1 (fr) * | 2010-03-02 | 2012-03-23 | Snecma | Preforme fibreuse pour un secteur d'anneau de turbine et son procede de fabrication. |
FR2970897B1 (fr) * | 2011-01-28 | 2014-09-19 | Snecma | Structure fibreuse formant une bride et une contre-bride |
FR2972483B1 (fr) * | 2011-03-07 | 2013-04-19 | Snecma | Carter de turbine comportant des moyens de fixation de secteurs d'anneau |
FR2972760B1 (fr) * | 2011-03-16 | 2015-10-30 | Snecma | Anneau de carter de turbomachine |
FR2973434A1 (fr) * | 2011-03-30 | 2012-10-05 | Snecma | Distributeur de turbine en cmc adapte au support d'un carter interne de turbine metallique par un contact radial |
FR2973435B1 (fr) * | 2011-03-30 | 2016-03-04 | Snecma | Distributeur de turbine en cmc adapte au support d'un carter interne de turbine metallique par un contact axial |
FR2976968B1 (fr) | 2011-06-21 | 2015-06-05 | Snecma | Piece de turbomachine formant redresseur de compresseur ou distributeur de turbine et procede pour sa fabrication |
CA2858320C (fr) | 2011-12-14 | 2019-04-16 | Snecma | Structure fibreuse tissee en une seule piece par tissage 3d et application a la fabrication de piece en materiau composite. |
US20130272870A1 (en) * | 2012-04-17 | 2013-10-17 | General Electric Company | Mica-based seals for gas turbine shroud retaining clip |
GB201305702D0 (en) * | 2013-03-28 | 2013-05-15 | Rolls Royce Plc | Seal segment |
ES2935815T3 (es) * | 2013-09-06 | 2023-03-10 | MTU Aero Engines AG | (Des)montaje de un rotor de una turbina de gas, en particular delantero |
EP3044442B1 (en) | 2013-09-11 | 2020-03-04 | United Technologies Corporation | Ceramic liner for a turbine exhaust case |
DE102013223585A1 (de) | 2013-11-19 | 2015-06-03 | MTU Aero Engines AG | Einlaufbelag auf Basis von Metallfasern |
US10309244B2 (en) * | 2013-12-12 | 2019-06-04 | General Electric Company | CMC shroud support system |
EP2886802B1 (fr) * | 2013-12-20 | 2019-04-10 | Safran Aero Boosters SA | Joint de virole interne de dernier étage de compresseur de turbomachine axiale |
FR3018473B1 (fr) * | 2014-03-17 | 2016-04-08 | Snecma | Procede de fabrication d'une plate-forme d'aube en materiau composite a joints integres pour soufflante de turbomachine |
US9869196B2 (en) * | 2014-06-24 | 2018-01-16 | General Electric Company | Gas turbine engine spring mounted manifold |
EP2963250B1 (en) | 2014-06-30 | 2019-08-07 | Rolls-Royce Corporation | Coating for isolating metallic components from composite components |
FR3025830B1 (fr) * | 2014-09-15 | 2020-07-03 | Safran Aircraft Engines | Anneau d'etancheite de turbomachine |
US10443435B2 (en) * | 2014-12-15 | 2019-10-15 | United Technologies Corporation | Slots for turbomachine structures |
US10100659B2 (en) * | 2014-12-16 | 2018-10-16 | Rolls-Royce North American Technologies Inc. | Hanger system for a turbine engine component |
US10054008B2 (en) * | 2015-02-09 | 2018-08-21 | United Technologies Corporation | Turbomachine accessory gearbox bracket |
FR3033825B1 (fr) | 2015-03-16 | 2018-09-07 | Safran Aircraft Engines | Ensemble d'anneau de turbine en materiau composite a matrice ceramique |
FR3033826B1 (fr) | 2015-03-16 | 2018-11-23 | Safran Ceramics | Ensemble d'anneau de turbine comprenant une pluralite de secteurs d'anneau en materiau composite a matrice ceramique |
FR3034132B1 (fr) | 2015-03-23 | 2018-06-15 | Safran Ceramics | Ensemble d'anneau de turbine comprenant une pluralite de secteurs d'anneau en materiau composite a matrice ceramique |
US10100649B2 (en) | 2015-03-31 | 2018-10-16 | Rolls-Royce North American Technologies Inc. | Compliant rail hanger |
FR3034454B1 (fr) | 2015-04-01 | 2018-04-20 | Safran Ceramics | Ensemble d'anneau de turbine avec liaison inter-secteurs |
FR3034453B1 (fr) | 2015-04-01 | 2017-04-28 | Herakles | Ensemble d'anneau de turbine avec etancheite |
FR3036436B1 (fr) | 2015-05-22 | 2020-01-24 | Safran Ceramics | Ensemble d'anneau de turbine avec maintien par brides |
FR3036433B1 (fr) | 2015-05-22 | 2019-09-13 | Safran Ceramics | Ensemble d'anneau de turbine avec maintien par crabotage |
FR3036435B1 (fr) | 2015-05-22 | 2020-01-24 | Safran Ceramics | Ensemble d'anneau de turbine |
FR3036432B1 (fr) * | 2015-05-22 | 2019-04-19 | Safran Ceramics | Ensemble d'anneau de turbine avec maintien axial |
JP6614407B2 (ja) * | 2015-06-10 | 2019-12-04 | 株式会社Ihi | タービン |
EP3118420A1 (en) * | 2015-07-15 | 2017-01-18 | Siemens Aktiengesellschaft | Coolable wall element with impingement plate |
US10309240B2 (en) | 2015-07-24 | 2019-06-04 | General Electric Company | Method and system for interfacing a ceramic matrix composite component to a metallic component |
FR3041993B1 (fr) * | 2015-10-05 | 2019-06-21 | Safran Aircraft Engines | Ensemble d'anneau de turbine avec maintien axial |
US10822972B2 (en) | 2015-12-08 | 2020-11-03 | General Electric Company | Compliant shroud for gas turbine engine clearance control |
FR3045716B1 (fr) | 2015-12-18 | 2018-01-26 | Safran Aircraft Engines | Ensemble d'anneau de turbine avec maintien elastique a froid |
FR3045715B1 (fr) * | 2015-12-18 | 2018-01-26 | Safran Aircraft Engines | Ensemble d'anneau de turbine avec maintien a froid et a chaud |
FR3049003B1 (fr) * | 2016-03-21 | 2018-04-06 | Safran Aircraft Engines | Ensemble d'anneau de turbine sans jeu de montage a froid |
FR3051017B1 (fr) * | 2016-05-09 | 2018-05-25 | Safran Aircraft Engines | Ensemble d'anneau de turbine avec calage a froid |
FR3055146B1 (fr) | 2016-08-19 | 2020-05-29 | Safran Aircraft Engines | Ensemble d'anneau de turbine |
FR3055148B1 (fr) | 2016-08-19 | 2020-06-05 | Safran Aircraft Engines | Ensemble d'anneau de turbine |
FR3055147B1 (fr) | 2016-08-19 | 2020-05-29 | Safran Aircraft Engines | Ensemble d'anneau de turbine |
FR3055625B1 (fr) * | 2016-09-08 | 2019-11-29 | Safran Ceramics | Preforme fibreuse pour fabriquer une piece en materiau composite et procede associe |
FR3055624B1 (fr) * | 2016-09-08 | 2019-11-22 | Safran Ceramics | Preforme fibreuse pour fabriquer une piece en materiau composite et procede associe |
FR3056632B1 (fr) | 2016-09-27 | 2020-06-05 | Safran Aircraft Engines | Ensemble d'anneau turbine comprenant un element de repartition de l'air de refroidissement |
FR3056637B1 (fr) * | 2016-09-27 | 2018-10-19 | Safran Aircraft Engines | Ensemble d'anneau de turbine avec calage a froid |
US10697314B2 (en) | 2016-10-14 | 2020-06-30 | Rolls-Royce Corporation | Turbine shroud with I-beam construction |
FR3061738B1 (fr) | 2017-01-12 | 2019-05-31 | Safran Aircraft Engines | Ensemble d'anneau de turbine |
FR3064022B1 (fr) | 2017-03-16 | 2019-09-13 | Safran Aircraft Engines | Ensemble d'anneau de turbine |
FR3064024B1 (fr) * | 2017-03-16 | 2019-09-13 | Safran Aircraft Engines | Ensemble d'anneau de turbine |
FR3064023B1 (fr) | 2017-03-16 | 2019-09-13 | Safran Aircraft Engines | Ensemble d'anneau de turbine |
GB201708746D0 (en) * | 2017-06-01 | 2017-07-19 | Rolls Royce Plc | Clearance control arrangement |
US20190093512A1 (en) * | 2017-09-01 | 2019-03-28 | Rolls-Royce Corporation | Ceramic matrix composite blade track for a gas turbine engine |
FR3071247B1 (fr) * | 2017-09-21 | 2019-09-20 | Safran Ceramics | Procede de fabrication d'une piece en cmc |
US10392957B2 (en) | 2017-10-05 | 2019-08-27 | Rolls-Royce Corporation | Ceramic matrix composite blade track with mounting system having load distribution features |
US10557365B2 (en) | 2017-10-05 | 2020-02-11 | Rolls-Royce Corporation | Ceramic matrix composite blade track with mounting system having reaction load distribution features |
FR3072711B1 (fr) | 2017-10-19 | 2021-07-16 | Safran Aircraft Engines | Element de repartition d'un fluide de refroidissement et ensemble d'anneau de turbine associe |
FR3076578B1 (fr) | 2018-01-09 | 2020-01-31 | Safran Aircraft Engines | Ensemble d'anneau de turbine |
FR3082765B1 (fr) | 2018-06-25 | 2021-04-30 | Safran Aircraft Engines | Procede de fabrication d'une couche abradable |
US10907501B2 (en) * | 2018-08-21 | 2021-02-02 | General Electric Company | Shroud hanger assembly cooling |
US10634010B2 (en) | 2018-09-05 | 2020-04-28 | United Technologies Corporation | CMC BOAS axial retaining clip |
FR3086327B1 (fr) | 2018-09-25 | 2020-12-04 | Safran Aircraft Engines | Ensemble pour une turbine de turbomachine |
GB201820224D0 (en) * | 2018-12-12 | 2019-01-23 | Rolls Royce Plc | Seal segment for shroud ring of a gas turbine engine |
FR3090732B1 (fr) | 2018-12-19 | 2021-01-08 | Safran Aircraft Engines | Ensemble d’anneau de turbine avec flasques indexés. |
FR3090731B1 (fr) | 2018-12-19 | 2021-01-08 | Safran Aircraft Engines | Ensemble d’anneau de turbine à appuis rectilignes bombés. |
US11021990B2 (en) | 2018-12-19 | 2021-06-01 | General Electric Company | Shroud sealing for a gas turbine engine |
FR3091550B1 (fr) | 2019-01-08 | 2021-01-22 | Safran Aircraft Engines | Procédé de montage et de démontage d’un ensemble d’anneau de turbine |
FR3093536B1 (fr) * | 2019-03-08 | 2021-02-19 | Safran Aircraft Engines | Rotor pour une turbine contrarotative de turbomachine |
FR3095668B1 (fr) | 2019-05-03 | 2021-04-09 | Safran Aircraft Engines | Ensemble d’anneau de turbine monté sur entretoise |
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 |
FR3100838B1 (fr) * | 2019-09-13 | 2021-10-01 | Safran Aircraft Engines | Anneau d’etancheite de 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 |
US11187098B2 (en) | 2019-12-20 | 2021-11-30 | Rolls-Royce Corporation | Turbine shroud assembly with hangers for ceramic matrix composite material seal segments |
FR3106152B1 (fr) | 2020-01-09 | 2022-01-21 | Safran Aircraft Engines | Ensemble d’anneau de turbine avec flasques indexés |
FR3108367B1 (fr) | 2020-03-20 | 2023-07-21 | Safran Aircraft Engines | Ensemble de turbine et turbomachine munie d’un tel ensemble |
FR3108672B1 (fr) * | 2020-03-24 | 2023-06-02 | Safran Aircraft Engines | Ensemble d'anneau de turbine |
FR3113696B1 (fr) * | 2020-09-03 | 2023-02-24 | Safran Aircraft Engines | Pièce de turbomachine avec bord de liaison en matériau composite à matrice céramique et à fibres courtes et son procédé de fabrication |
FR3123236B1 (fr) | 2021-05-25 | 2023-10-27 | Safran Aircraft Engines | Procédé de fabrication d’une couche abradable. |
US11674396B2 (en) | 2021-07-30 | 2023-06-13 | General Electric Company | Cooling air delivery assembly |
US11674405B2 (en) | 2021-08-30 | 2023-06-13 | General Electric Company | Abradable insert with lattice structure |
FR3134135B1 (fr) | 2022-04-04 | 2024-03-29 | Safran Aircraft Engines | Ensemble d’anneau de turbine à dispositif de refroidissement amélioré |
FR3136782B1 (fr) | 2022-06-21 | 2024-06-21 | Safran Ceram | Procédé de tissage tridimensionnel d’une structure fibreuse avec orientation des colonnes de trame dans une portion de déploiement et structure fibreuse résultante |
FR3139292B1 (fr) | 2022-09-01 | 2024-08-30 | Safran Aircraft Engines | Ensemble d’anneau de turbine à rattrapage de jeux intégré |
US20240199498A1 (en) * | 2022-12-20 | 2024-06-20 | Raytheon Technologies Corporation | Boron nitride aerogel interface coating precursor for ceramic matrix composites |
FR3146821A1 (fr) * | 2023-03-21 | 2024-09-27 | Safran Ceramics | Procédé de fabrication d’un secteur d’anneau de turbine |
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FR2540939A1 (fr) * | 1983-02-10 | 1984-08-17 | Snecma | Anneau d'etancheite pour un rotor de turbine d'une turbomachine et installation de turbomachine munie de tels anneaux |
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FR2887601B1 (fr) | 2005-06-24 | 2007-10-05 | Snecma Moteurs Sa | Piece mecanique et procede de fabrication d'une telle piece |
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US7811054B2 (en) * | 2007-05-30 | 2010-10-12 | General Electric Company | Shroud configuration having sloped seal |
FR2919345B1 (fr) | 2007-07-26 | 2013-08-30 | Snecma | Anneau pour une roue de turbine de turbomachine. |
-
2010
- 2010-03-01 BR BRPI1013342A patent/BRPI1013342A8/pt not_active IP Right Cessation
- 2010-03-01 CN CN201080004094XA patent/CN102272419A/zh active Pending
- 2010-03-01 JP JP2011553489A patent/JP5646517B2/ja active Active
- 2010-03-01 ES ES10715282T patent/ES2398727T3/es active Active
- 2010-03-01 RU RU2011140942/06A patent/RU2522264C2/ru active
- 2010-03-01 CA CA2750938A patent/CA2750938A1/fr not_active Abandoned
- 2010-03-01 US US13/255,436 patent/US9080463B2/en active Active
- 2010-03-01 WO PCT/FR2010/050342 patent/WO2010103213A1/fr active Application Filing
- 2010-03-01 EP EP10715282A patent/EP2406466B1/fr active Active
Also Published As
Publication number | Publication date |
---|---|
BRPI1013342A2 (pt) | 2016-03-29 |
US20120027572A1 (en) | 2012-02-02 |
CN102272419A (zh) | 2011-12-07 |
US9080463B2 (en) | 2015-07-14 |
JP2012519803A (ja) | 2012-08-30 |
CA2750938A1 (fr) | 2010-09-16 |
EP2406466B1 (fr) | 2012-11-07 |
RU2522264C2 (ru) | 2014-07-10 |
RU2011140942A (ru) | 2013-04-20 |
EP2406466A1 (fr) | 2012-01-18 |
WO2010103213A1 (fr) | 2010-09-16 |
ES2398727T3 (es) | 2013-03-21 |
JP5646517B2 (ja) | 2014-12-24 |
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