PL2145080T3 - Silnik turbinowy do śmigłowca zawierający generator gazowy i turbinę swobodną - Google Patents
Silnik turbinowy do śmigłowca zawierający generator gazowy i turbinę swobodnąInfo
- Publication number
- PL2145080T3 PL2145080T3 PL08788124T PL08788124T PL2145080T3 PL 2145080 T3 PL2145080 T3 PL 2145080T3 PL 08788124 T PL08788124 T PL 08788124T PL 08788124 T PL08788124 T PL 08788124T PL 2145080 T3 PL2145080 T3 PL 2145080T3
- Authority
- PL
- Poland
- Prior art keywords
- gas
- helicoptere
- turbine
- free
- turbine engine
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/32—Arrangement, mounting, or driving, of auxiliaries
-
- 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
- F01D15/00—Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
- F01D15/08—Adaptations for driving, or combinations with, pumps
-
- 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
- F01D15/00—Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
- F01D15/10—Adaptations for driving, or combinations with, electric generators
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
- F02C3/10—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with another turbine driving an output shaft but not driving the compressor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/26—Starting; Ignition
-
- 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
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/32—Application in turbines in gas turbines
- F05D2220/329—Application in turbines in gas turbines in helicopters
-
- 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
- F05D2260/85—Starting
-
- 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
- F05D2260/90—Braking
-
- 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
- F05D2260/90—Braking
- F05D2260/903—Braking using electrical or magnetic forces
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
- Control Of Eletrric Generators (AREA)
- Supercharger (AREA)
- Arrangement Or Mounting Of Propulsion Units For Vehicles (AREA)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0754346A FR2914697B1 (fr) | 2007-04-06 | 2007-04-06 | Dispositif d'assistance aux phases transitoires d'acceleration et de deceleration |
EP08788124.9A EP2145080B1 (fr) | 2007-04-06 | 2008-04-04 | Turbomoteur pour hélicoptère comprenant un générateur de gaz et une turbine libre |
PCT/FR2008/050601 WO2008139096A2 (fr) | 2007-04-06 | 2008-04-04 | Turbomoteur de helicoptere comrpenant un generateur de gaz et une turbine libre |
Publications (1)
Publication Number | Publication Date |
---|---|
PL2145080T3 true PL2145080T3 (pl) | 2018-11-30 |
Family
ID=38780785
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PL08788124T PL2145080T3 (pl) | 2007-04-06 | 2008-04-04 | Silnik turbinowy do śmigłowca zawierający generator gazowy i turbinę swobodną |
Country Status (12)
Country | Link |
---|---|
US (1) | US8201414B2 (pl) |
EP (1) | EP2145080B1 (pl) |
JP (2) | JP2010523879A (pl) |
CN (1) | CN101652535B (pl) |
BR (1) | BRPI0810074B1 (pl) |
CA (1) | CA2683372C (pl) |
ES (1) | ES2687254T3 (pl) |
FR (1) | FR2914697B1 (pl) |
PL (1) | PL2145080T3 (pl) |
RU (1) | RU2462607C2 (pl) |
WO (1) | WO2008139096A2 (pl) |
ZA (1) | ZA200906886B (pl) |
Families Citing this family (74)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2941492B1 (fr) * | 2009-01-23 | 2011-09-09 | Snecma | Turbomachine a turbine de puissance equipee d'un generateur electronique de puissance centre sur l'axe de la turbomachine |
FR2942077B1 (fr) * | 2009-02-06 | 2013-08-16 | Turbomeca | Generation thermoelectrique pour turbine a gaz |
FR2947006B1 (fr) * | 2009-06-17 | 2014-10-17 | Eurocopter France | Dispositif et procede pour le demarrage d'un moteur a turbine equipant un helicoptere,mettant en oeuvre une source d'energie electrique comprenant des organes d'appoint a decharge |
FR2952907B1 (fr) | 2009-11-26 | 2011-12-09 | Eurocopter France | Installation motrice, helicoptere comportant une telle installation motrice, et procede mis en oeuvre par cette installation motrice |
FR2962488B1 (fr) * | 2010-07-06 | 2014-05-02 | Turbomeca | Procede et architecture de recombinaison de puissance de turbomachine |
FR2964155B1 (fr) * | 2010-08-25 | 2014-03-28 | Turbomeca | Procede d'optimisation de regulation d'un groupe de puissance a turbine libre pour aeronef et commande de regulation de mise en oeuvre |
FR2964087B1 (fr) * | 2010-08-25 | 2013-06-14 | Turbomeca | Procede d'optimisation de l'operabilite de motorisation d'un aeronef et groupe de puissance autonome de mise en oeuvre |
FR2968716B1 (fr) * | 2010-12-13 | 2012-12-28 | Turbomeca | Procede de controle de la generation electrique appliquee a une turbine a gaz d'aeronef et turbomoteur mettant en oeuvre un tel procede |
FR2978124B1 (fr) | 2011-07-18 | 2013-08-02 | Eurocopter France | Procede de controle d'un groupe de moteurs et aeronef |
US9267438B2 (en) | 2011-10-11 | 2016-02-23 | Pratt & Whitney Canada Corp. | Starting of aircraft engine |
US9429077B2 (en) * | 2011-12-06 | 2016-08-30 | Pratt & Whitney Canada Corp. | Multiple turboshaft engine control method and system for helicopters |
US20130147192A1 (en) * | 2011-12-13 | 2013-06-13 | Honeywell International Inc. | Gas turbine engine transient assist using a starter-generator |
FR2986040B1 (fr) * | 2012-01-20 | 2016-03-25 | Turbomeca | Support de palier de turbomachine |
FR2986570B1 (fr) | 2012-02-06 | 2014-02-28 | Eurocopter France | Dispositif et procede de regulation d'une installation motrice comportant au moins un turbomoteur, et aeronef |
FR2990004B1 (fr) * | 2012-04-27 | 2014-04-18 | Turbomeca | Procede et systeme de demarrage d'urgence d'architecture generatrice d'energie |
FR2993243B1 (fr) | 2012-07-12 | 2014-07-11 | Eurocopter France | Architecture d'alimentation hybride en puissance mecanique d'un rotor, geree a partir du reseau de bord d'un giravion |
FR2997382B1 (fr) | 2012-10-29 | 2014-11-21 | Eurocopter France | Procede de gestion d'une panne moteur sur un aeronef multimoteur muni d'une installation motrice hybride |
US9045996B2 (en) | 2012-11-20 | 2015-06-02 | Honeywell International Inc. | Gas turbine engine optimization by electric power transfer |
JP6130131B2 (ja) * | 2012-12-06 | 2017-05-17 | 三菱日立パワーシステムズ株式会社 | 2軸式ガスタービンの制御装置及びそれを備えた2軸式ガスタービン |
ITFI20120292A1 (it) | 2012-12-24 | 2014-06-25 | Nuovo Pignone Srl | "gas turbines in mechanical drive applications and operating methods" |
JP5899133B2 (ja) | 2013-02-01 | 2016-04-06 | 株式会社日立製作所 | 2軸ガスタービン |
DE112013006847T5 (de) * | 2013-03-19 | 2015-12-03 | Hitachi, Ltd. | Gasturbinenstromerzeugungssystem |
DE102013209538B4 (de) * | 2013-05-23 | 2020-12-03 | Robert Bosch Gmbh | Hybridantrieb für kraftgetriebenes Luftfahrzeug, kraftgetriebenes Luftfahrzeug mit Hybridantrieb und zugehöriges Betriebsverfahren |
DE102013213263B4 (de) * | 2013-07-05 | 2023-03-30 | Siemens Energy Global GmbH & Co. KG | Stromrichter mit wenigstens einem elektrischen Energieverbraucher |
US10113487B2 (en) | 2013-10-24 | 2018-10-30 | United Technologies Corporation | Cascaded multi-variable control system for a turboshaft engine |
FR3015574B1 (fr) * | 2013-12-20 | 2019-05-03 | Safran Helicopter Engines | Procede de commande automatique du regime de fonctionnement d'un turbomoteur d'un helicoptere, dispositif de commande correspondant et helicoptere equipe d'un tel dispositif |
EP2889452B1 (en) | 2013-12-30 | 2020-07-22 | Rolls-Royce Corporation | System and method for coordinated control of a power system |
US9394002B2 (en) | 2014-03-20 | 2016-07-19 | Ford Global Technologies, Llc | Extruded metal sub-frame for a vehicle |
FR3019214B1 (fr) | 2014-03-27 | 2019-05-31 | Safran Helicopter Engines | Dispositif d'assistance pour une turbomachine a turbine libre d'aeronef |
FR3019224B1 (fr) * | 2014-03-27 | 2016-03-18 | Turbomeca | Procede d'assistance d'un turbomoteur en veille d'un helicoptere multi-moteur et architecture d'un systeme propulsif d'un helicoptere comprenant au moins un turbomoteur pouvant etre en veille |
FR3019215B1 (fr) * | 2014-03-27 | 2019-05-31 | Safran Helicopter Engines | Dispositif d'assistance pour une turbomachine a turbine libre d'un aeronef comprenant au moins deux turbomachines a turbine libre |
FR3019217B1 (fr) * | 2014-03-27 | 2018-07-27 | Safran Helicopter Engines | Procede et systeme de reactivation rapide de turbomachine |
FR3019221B1 (fr) * | 2014-03-27 | 2018-10-12 | Safran Helicopter Engines | Dispositif hydraulique de demarrage d'urgence d'un turbomoteur, architecture d'un systeme propulsif d'un helicoptere multi-moteur equipe d'un tel dispositif et helicoptere correspondant |
FR3019218B1 (fr) * | 2014-03-27 | 2016-03-18 | Turbomeca | Architecture d'un systeme propulsif d'un helicoptere multi-moteur et helicoptere correspondant |
EP2930335B1 (en) * | 2014-04-10 | 2019-09-18 | Rolls-Royce North American Technologies, Inc. | Fuel-air ratio control of gas turbine engines |
FR3020658B1 (fr) * | 2014-04-30 | 2020-05-15 | Safran Aircraft Engines | Capot de recuperation d'huile de lubrification pour un equipement de turbomachine |
FR3024180B1 (fr) * | 2014-07-28 | 2016-07-22 | Turbomeca | Dispositif pneumatique de reactivation rapide d'un turbomoteur, architecture d'un systeme propulsif d'un helicoptere multi-moteur equipe d'un tel dispositif et helicoptere correspondant |
FR3024707B1 (fr) * | 2014-08-07 | 2018-03-23 | Turbomeca | Dispositif d'assistance rapide pour une turbomachine a turbine libre d'un aeronef |
FR3024755B1 (fr) * | 2014-08-08 | 2019-06-21 | Safran Aircraft Engines | Hybridation des compresseurs d'un turboreacteur |
FR3039614B1 (fr) * | 2015-07-31 | 2018-05-04 | Airbus Helicopters | Installation motrice hybride pour aeronef a voilure tournante bimoteur |
US20170044989A1 (en) * | 2015-08-14 | 2017-02-16 | General Electric Company | Gas turbine engine stall margin management |
KR101695374B1 (ko) * | 2016-07-05 | 2017-01-17 | 김민수 | 폐열을 이용한 소형 발전터빈 |
JP6288529B2 (ja) * | 2016-07-22 | 2018-03-07 | 三菱日立パワーシステムズ株式会社 | 二軸ガスタービン発電設備、及びその制御方法 |
FR3056558B1 (fr) * | 2016-09-26 | 2021-06-04 | Safran | Procede d'optimisation de l'operabilite de la motorisation d'un aeronef |
CN106762138A (zh) * | 2017-01-21 | 2017-05-31 | 袁新友 | 一种并轴式航空燃气发动机 |
US10934935B2 (en) * | 2017-01-30 | 2021-03-02 | Ge Aviation Systems Llc | Engine core assistance |
US11230385B2 (en) * | 2017-06-08 | 2022-01-25 | General Electric Company | Hybrid-electric propulsion system for an aircraft |
US11008111B2 (en) * | 2017-06-26 | 2021-05-18 | General Electric Company | Propulsion system for an aircraft |
US10006375B1 (en) * | 2017-07-11 | 2018-06-26 | General Electric Company | Propulsion system for an aircraft |
FR3081150B1 (fr) | 2018-05-18 | 2020-06-12 | Safran Helicopter Engines | Architecture de puissance d'un aeronef |
US11097849B2 (en) | 2018-09-10 | 2021-08-24 | General Electric Company | Aircraft having an aft engine |
US10961921B2 (en) | 2018-09-19 | 2021-03-30 | Pratt & Whitney Canada Corp. | Model-based control system and method for a turboprop engine |
JP7021054B2 (ja) * | 2018-11-08 | 2022-02-16 | 本田技研工業株式会社 | ハイブリッド飛行体 |
JP7049234B2 (ja) * | 2018-11-15 | 2022-04-06 | 本田技研工業株式会社 | ハイブリッド飛行体 |
US11274599B2 (en) | 2019-03-27 | 2022-03-15 | Pratt & Whitney Canada Corp. | Air system switching system to allow aero-engines to operate in standby mode |
US11391219B2 (en) | 2019-04-18 | 2022-07-19 | Pratt & Whitney Canada Corp. | Health monitor for air switching system |
CN110259582A (zh) * | 2019-05-23 | 2019-09-20 | 贵州航天天马机电科技有限公司 | 一种涡轮轴发动机动力输出机构 |
US11274611B2 (en) | 2019-05-31 | 2022-03-15 | Pratt & Whitney Canada Corp. | Control logic for gas turbine engine fuel economy |
EP3744959B1 (en) * | 2019-05-31 | 2023-06-28 | Pratt & Whitney Canada Corp. | Control logic for gas turbine engine fuel economy |
US11859563B2 (en) | 2019-05-31 | 2024-01-02 | Pratt & Whitney Canada Corp. | Air system of multi-engine aircraft |
FR3097012B1 (fr) * | 2019-06-06 | 2022-01-21 | Safran Aircraft Engines | Procédé de régulation d’une accélération d’une turbomachine |
RU2730691C1 (ru) * | 2019-09-13 | 2020-08-25 | Владимир Игоревич Лаврентьев | Газотурбинный двигатель лаврентьева |
US11326525B2 (en) | 2019-10-11 | 2022-05-10 | Pratt & Whitney Canada Corp. | Aircraft bleed air systems and methods |
GB201915310D0 (en) | 2019-10-23 | 2019-12-04 | Rolls Royce Plc | Turboelectric generator system |
EP3832096A1 (en) * | 2019-12-03 | 2021-06-09 | Airbus SAS | Electrical assistance system for a turbomachine of an aircraft, method of operating a turbomachine of an aircraft, and aircraft |
US11428171B2 (en) | 2019-12-06 | 2022-08-30 | General Electric Company | Electric machine assistance for multi-spool turbomachine operation and control |
FR3115825A1 (fr) * | 2020-11-04 | 2022-05-06 | Airbus Helicopters | Procédé de pilotage d’une installation motrice d’un giravion comprenant au moins deux turbomoteurs |
JP7365325B2 (ja) * | 2020-12-22 | 2023-10-19 | 本田技研工業株式会社 | ガスタービンシステム |
JP7558093B2 (ja) | 2021-03-12 | 2024-09-30 | 本田技研工業株式会社 | 航空機用推進システム |
CN113062801B (zh) * | 2021-04-19 | 2022-07-22 | 中国航发湖南动力机械研究所 | 功率后输出式涡轮螺旋桨发动机及飞机 |
CN113006940B (zh) * | 2021-05-06 | 2022-03-29 | 中国航发湖南动力机械研究所 | 一种无需外部减速器的微小型涡桨发动机 |
US11845388B2 (en) | 2021-05-20 | 2023-12-19 | General Electric Company | AC electrical power system for a vehicle |
FR3138116A1 (fr) | 2022-07-20 | 2024-01-26 | Airbus Helicopters | Aéronef comportant au moins deux turbomoteurs et un dispositif configuré pour être relié à un des turbomoteurs et procédé de contrôle d’un tel aéronef |
FR3142510A1 (fr) * | 2022-11-24 | 2024-05-31 | Safran Aircraft Engines | dispositif et procédé de contrôle de maintien en régime de ralenti |
Family Cites Families (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1530430A (fr) * | 1966-01-22 | 1968-06-28 | Productions Ind Et De Distrib | Turbo-machine à gaz ou analogue et ses diverses applications |
US4062185A (en) * | 1976-05-13 | 1977-12-13 | General Electric Company | Method and apparatus for windmill starts in gas turbine engines |
US4927329A (en) * | 1988-10-21 | 1990-05-22 | General Electric Company | Aircraft engine unducted fan blade pitch control system |
JPH0687640U (ja) * | 1993-06-04 | 1994-12-22 | 石川島播磨重工業株式会社 | ガスタービンエンジン |
RU2224352C2 (ru) * | 1996-12-03 | 2004-02-20 | Эллиотт Энерджи Системс, Инк. | Электрическая система для турбины/генератора переменного тока на общем валу |
US5929537A (en) * | 1997-06-30 | 1999-07-27 | Sundstrand Corporation | PMG main engine starter/generator system |
US6107693A (en) * | 1997-09-19 | 2000-08-22 | Solo Energy Corporation | Self-contained energy center for producing mechanical, electrical, and heat energy |
US6145296A (en) * | 1998-09-25 | 2000-11-14 | Alm Development, Inc. | Gas turbine engine having counter rotating turbines and a controller for controlling the load driven by one of the turbines |
JP4300682B2 (ja) * | 2000-05-30 | 2009-07-22 | 株式会社島津製作所 | 走行体 |
AU2002220089A1 (en) * | 2000-11-14 | 2002-05-27 | Capstone Turbine Corporation | Method and apparatus for turbogenerator anti-surge control |
RU2188960C1 (ru) * | 2001-08-20 | 2002-09-10 | Кондрашов Борис Михайлович | Способ преобразования энергии в силовой установке (варианты), струйно-адаптивном двигателе и газогенераторе |
US20040080165A1 (en) * | 2001-12-31 | 2004-04-29 | Capstone Turbine Corporation | Turbogenerator/motor controller with ancillary energy storage/discharge |
US20040160061A1 (en) * | 2003-01-31 | 2004-08-19 | Capstone Turbine Corporation | Gas-turbine engine with catalytic reactor |
US6931856B2 (en) * | 2003-09-12 | 2005-08-23 | Mes International, Inc. | Multi-spool turbogenerator system and control method |
US7188475B2 (en) * | 2003-12-18 | 2007-03-13 | Honeywell International, Inc. | Starting and controlling speed of a two spool gas turbine engine |
US7513120B2 (en) * | 2005-04-08 | 2009-04-07 | United Technologies Corporation | Electrically coupled supercharger for a gas turbine engine |
US7802757B2 (en) * | 2005-11-09 | 2010-09-28 | Pratt & Whitney Canada Corp. | Method and system for taxiing an aircraft |
US8584464B2 (en) * | 2005-12-20 | 2013-11-19 | General Electric Company | Gas turbine engine assembly and method of assembling same |
US7793505B2 (en) * | 2006-05-04 | 2010-09-14 | Pratt & Whitney Canada Corp | Gas turbine engine oil system operation |
US7942079B2 (en) * | 2007-02-16 | 2011-05-17 | Hamilton Sundstrand Corporation | Multi-speed gearbox for low spool driven auxiliary component |
US7926287B2 (en) * | 2007-05-08 | 2011-04-19 | Pratt & Whitney Canada Corp. | Method of operating a gas turbine engine |
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2007
- 2007-04-06 FR FR0754346A patent/FR2914697B1/fr active Active
-
2008
- 2008-04-04 ES ES08788124.9T patent/ES2687254T3/es active Active
- 2008-04-04 RU RU2009140975/06A patent/RU2462607C2/ru active
- 2008-04-04 WO PCT/FR2008/050601 patent/WO2008139096A2/fr active Application Filing
- 2008-04-04 PL PL08788124T patent/PL2145080T3/pl unknown
- 2008-04-04 US US12/594,826 patent/US8201414B2/en active Active
- 2008-04-04 BR BRPI0810074A patent/BRPI0810074B1/pt not_active IP Right Cessation
- 2008-04-04 CN CN2008800114518A patent/CN101652535B/zh active Active
- 2008-04-04 JP JP2010501572A patent/JP2010523879A/ja active Pending
- 2008-04-04 CA CA2683372A patent/CA2683372C/fr active Active
- 2008-04-04 EP EP08788124.9A patent/EP2145080B1/fr active Active
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2009
- 2009-10-02 ZA ZA200906886A patent/ZA200906886B/xx unknown
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2013
- 2013-04-17 JP JP2013086292A patent/JP2013174242A/ja active Pending
Also Published As
Publication number | Publication date |
---|---|
US8201414B2 (en) | 2012-06-19 |
BRPI0810074A2 (pt) | 2014-10-21 |
ZA200906886B (en) | 2010-06-30 |
CN101652535B (zh) | 2013-08-21 |
US20100058731A1 (en) | 2010-03-11 |
FR2914697B1 (fr) | 2012-11-30 |
FR2914697A1 (fr) | 2008-10-10 |
WO2008139096A4 (fr) | 2009-05-07 |
RU2009140975A (ru) | 2011-05-20 |
ES2687254T3 (es) | 2018-10-24 |
WO2008139096A3 (fr) | 2009-03-26 |
JP2010523879A (ja) | 2010-07-15 |
EP2145080A2 (fr) | 2010-01-20 |
WO2008139096A2 (fr) | 2008-11-20 |
RU2462607C2 (ru) | 2012-09-27 |
EP2145080B1 (fr) | 2018-08-01 |
CA2683372C (fr) | 2015-07-07 |
JP2013174242A (ja) | 2013-09-05 |
CN101652535A (zh) | 2010-02-17 |
CA2683372A1 (fr) | 2008-11-20 |
BRPI0810074B1 (pt) | 2020-02-04 |
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