EP1707745A3 - Aube de rotor pour une turbomachine et turbomachine - Google Patents
Aube de rotor pour une turbomachine et turbomachine Download PDFInfo
- Publication number
- EP1707745A3 EP1707745A3 EP06014569A EP06014569A EP1707745A3 EP 1707745 A3 EP1707745 A3 EP 1707745A3 EP 06014569 A EP06014569 A EP 06014569A EP 06014569 A EP06014569 A EP 06014569A EP 1707745 A3 EP1707745 A3 EP 1707745A3
- Authority
- EP
- European Patent Office
- Prior art keywords
- turbomachine
- blade
- proposed
- design
- rotor blade
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Withdrawn
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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/147—Construction, i.e. structural features, e.g. of weight-saving hollow 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F2998/00—Supplementary information concerning processes or compositions relating to powder metallurgy
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
- F05C2201/00—Metals
- F05C2201/04—Heavy metals
- F05C2201/0433—Iron group; Ferrous alloys, e.g. steel
- F05C2201/0463—Cobalt
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
- F05C2201/00—Metals
- F05C2201/04—Heavy metals
- F05C2201/0433—Iron group; Ferrous alloys, e.g. steel
- F05C2201/0466—Nickel
-
- 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
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/203—Heat transfer, e.g. cooling by transpiration cooling
-
- 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
- F05D2300/612—Foam
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Materials Engineering (AREA)
- Architecture (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Finish Polishing, Edge Sharpening, And Grinding By Specific Grinding Devices (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP06014569A EP1707745A3 (fr) | 2000-09-05 | 2001-08-23 | Aube de rotor pour une turbomachine et turbomachine |
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP00119203A EP1186748A1 (fr) | 2000-09-05 | 2000-09-05 | Aube de rotor pour une turbomachine et turbomachine |
EP01971957A EP1322838B1 (fr) | 2000-09-05 | 2001-08-23 | Aube de turbomachine et turbomachine |
EP06014569A EP1707745A3 (fr) | 2000-09-05 | 2001-08-23 | Aube de rotor pour une turbomachine et turbomachine |
Related Parent Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP01971957A Division EP1322838B1 (fr) | 2000-09-05 | 2001-08-23 | Aube de turbomachine et turbomachine |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1707745A2 EP1707745A2 (fr) | 2006-10-04 |
EP1707745A3 true EP1707745A3 (fr) | 2006-10-18 |
Family
ID=8169757
Family Applications (3)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP00119203A Withdrawn EP1186748A1 (fr) | 2000-09-05 | 2000-09-05 | Aube de rotor pour une turbomachine et turbomachine |
EP06014569A Withdrawn EP1707745A3 (fr) | 2000-09-05 | 2001-08-23 | Aube de rotor pour une turbomachine et turbomachine |
EP01971957A Expired - Lifetime EP1322838B1 (fr) | 2000-09-05 | 2001-08-23 | Aube de turbomachine et turbomachine |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP00119203A Withdrawn EP1186748A1 (fr) | 2000-09-05 | 2000-09-05 | Aube de rotor pour une turbomachine et turbomachine |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP01971957A Expired - Lifetime EP1322838B1 (fr) | 2000-09-05 | 2001-08-23 | Aube de turbomachine et turbomachine |
Country Status (6)
Country | Link |
---|---|
US (1) | US6827556B2 (fr) |
EP (3) | EP1186748A1 (fr) |
JP (1) | JP4499351B2 (fr) |
CN (1) | CN1325761C (fr) |
DE (1) | DE50111221D1 (fr) |
WO (1) | WO2002020948A1 (fr) |
Families Citing this family (54)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE10331599A1 (de) * | 2003-07-11 | 2005-02-03 | Mtu Aero Engines Gmbh | Bauteil für eine Gasturbine sowie Verfahren zur Herstellung desselben |
DE10357656A1 (de) * | 2003-12-10 | 2005-07-07 | Mtu Aero Engines Gmbh | Verfahren zur Herstellung von Gasturbinenbauteilen und Bauteil für eine Gasturbine |
DE10360164A1 (de) | 2003-12-20 | 2005-07-21 | Mtu Aero Engines Gmbh | Gasturbinenbauteil |
EP1566519A1 (fr) * | 2004-02-23 | 2005-08-24 | Siemens Aktiengesellschaft | Composant à haute température d'une turbomachine et turbomachine |
GB2418459B (en) * | 2004-09-22 | 2009-04-29 | Rolls Royce Plc | A method of manufacturing an aerofoil |
DE102006013557B4 (de) | 2005-03-30 | 2015-09-24 | Alstom Technology Ltd. | Rotor für eine Dampfturbine |
DE102005044470A1 (de) * | 2005-09-16 | 2007-03-22 | Orbiter Group Beteiligungs Gmbh | Verwendung eines Metallschaumes in Strömungsmaschinen, insbesondere in Turbinen, Lüftern und Pumpen |
GB0601220D0 (en) * | 2006-01-21 | 2006-03-01 | Rolls Royce Plc | Aerofoils for gas turbine engines |
DE102006022164B4 (de) * | 2006-05-12 | 2012-07-19 | Mtu Aero Engines Gmbh | Verfahren zum Aussteifen eines Rotorelements |
DE102007009468A1 (de) * | 2007-02-27 | 2008-08-28 | Mtu Aero Engines Gmbh | Verfahren zur Herstellung eines Strukturelements |
US7905016B2 (en) * | 2007-04-10 | 2011-03-15 | Siemens Energy, Inc. | System for forming a gas cooled airfoil for use in a turbine engine |
CN101078354B (zh) * | 2007-06-06 | 2013-03-27 | 北京航空航天大学 | 多孔金属叶片耦合设计方法 |
GB2450937B (en) * | 2007-07-13 | 2009-06-03 | Rolls Royce Plc | Component with tuned frequency response |
US7988412B2 (en) * | 2007-08-24 | 2011-08-02 | General Electric Company | Structures for damping of turbine components |
US7633175B1 (en) * | 2008-05-13 | 2009-12-15 | Florida Turbine Technologies, Inc. | Resonating blade for electric power generation |
US9938931B2 (en) | 2008-12-23 | 2018-04-10 | General Electric Company | Combined surface cooler and acoustic absorber for turbomachines |
US8333552B2 (en) * | 2008-06-20 | 2012-12-18 | General Electric Company | Combined acoustic absorber and heat exchanging outlet guide vanes |
DE102008058142A1 (de) * | 2008-11-20 | 2010-05-27 | Mtu Aero Engines Gmbh | Verfahren zum Herstellen und/oder Reparieren eines Rotors einer Strömungsmaschine und Rotor hierzu |
DE102008058141A1 (de) * | 2008-11-20 | 2010-05-27 | Mtu Aero Engines Gmbh | Verfahren zum Herstellen einer Schaufel für einen Rotor einer Strömungsmaschine |
US8246291B2 (en) * | 2009-05-21 | 2012-08-21 | Rolls-Royce Corporation | Thermal system for a working member of a power plant |
GB0912796D0 (en) | 2009-07-23 | 2009-08-26 | Cummins Turbo Tech Ltd | Compressor,turbine and turbocharger |
US9341118B2 (en) | 2009-12-29 | 2016-05-17 | Rolls-Royce Corporation | Various layered gas turbine engine component constructions |
CN103180617B (zh) * | 2010-10-18 | 2016-05-18 | 三菱日立电力系统株式会社 | 跨音速叶片 |
US8753093B2 (en) * | 2010-10-19 | 2014-06-17 | General Electric Company | Bonded turbine bucket tip shroud and related method |
US9004873B2 (en) * | 2010-12-27 | 2015-04-14 | Rolls-Royce Corporation | Airfoil, turbomachine and gas turbine engine |
US20120167572A1 (en) * | 2010-12-30 | 2012-07-05 | Edward Claude Rice | Gas turbine engine and diffuser |
US8807944B2 (en) | 2011-01-03 | 2014-08-19 | General Electric Company | Turbomachine airfoil component and cooling method therefor |
DE102011014292A1 (de) * | 2011-03-17 | 2012-09-20 | Rolls-Royce Deutschland Ltd & Co Kg | Zwischenstufendichtungsring sowie Verfahren zu dessen Herstellung |
WO2013141939A2 (fr) | 2011-12-30 | 2013-09-26 | Rolls-Royce North American Technologies Inc. | Procédé de fabrication de composant de turbomachine, de profil aérodynamique, et de turbine à gaz |
JP5555727B2 (ja) * | 2012-01-23 | 2014-07-23 | 川崎重工業株式会社 | 軸流圧縮機翼の製造方法 |
WO2014143340A2 (fr) * | 2013-03-03 | 2014-09-18 | Uskert Richard C | Élément de turbine à gaz doté d'un noyau en mousse et d'un revêtement composite, comprenant fente de refroidissement |
GB201414495D0 (en) * | 2014-08-15 | 2014-10-01 | Rolls Royce Plc | Blade |
US9789536B2 (en) | 2015-01-20 | 2017-10-17 | United Technologies Corporation | Dual investment technique for solid mold casting of reticulated metal foams |
US9737930B2 (en) | 2015-01-20 | 2017-08-22 | United Technologies Corporation | Dual investment shelled solid mold casting of reticulated metal foams |
US9789534B2 (en) | 2015-01-20 | 2017-10-17 | United Technologies Corporation | Investment technique for solid mold casting of reticulated metal foams |
US9884363B2 (en) | 2015-06-30 | 2018-02-06 | United Technologies Corporation | Variable diameter investment casting mold for casting of reticulated metal foams |
US9731342B2 (en) | 2015-07-07 | 2017-08-15 | United Technologies Corporation | Chill plate for equiax casting solidification control for solid mold casting of reticulated metal foams |
EP3147069A1 (fr) * | 2015-09-24 | 2017-03-29 | Siemens Aktiengesellschaft | Procédé de fabrication d'une aube hybride d'une turbomachine thermique par soudage de rechargement |
US10605117B2 (en) | 2015-10-08 | 2020-03-31 | General Electric Company | Fan platform for a gas turbine engine |
EP3222814A1 (fr) * | 2016-03-24 | 2017-09-27 | Siemens Aktiengesellschaft | Aube, procédé de fabrication associé et turbomachine associée |
EP3249159A1 (fr) * | 2016-05-23 | 2017-11-29 | Siemens Aktiengesellschaft | Aube de turbine et turbomachine associée |
GB201707836D0 (en) * | 2017-05-16 | 2017-06-28 | Oscar Propulsion Ltd | Outlet guide vanes |
US10808545B2 (en) * | 2017-07-14 | 2020-10-20 | United Technologies Corporation | Gas turbine engine fan blade, design, and fabrication |
DE102017214060A1 (de) * | 2017-08-11 | 2019-02-14 | Siemens Aktiengesellschaft | Funktionale Struktur und Komponente für eine Strömungsmaschine |
EP3480431A1 (fr) * | 2017-11-02 | 2019-05-08 | MTU Aero Engines GmbH | Composant pour une turbine à gaz doté d'une structure ayant un gradient dans le module d'élasticité et procédé de fabrication additive |
US11078795B2 (en) * | 2017-11-16 | 2021-08-03 | General Electric Company | OGV electroformed heat exchangers |
DE102018207444A1 (de) * | 2018-05-15 | 2019-11-21 | Bayerische Motoren Werke Aktiengesellschaft | Verfahren zur Herstellung eines Strukturbauteils |
GB201918777D0 (en) | 2019-12-19 | 2020-02-05 | Rolls Royce Plc | Shaft bearing arrangement |
GB201918780D0 (en) | 2019-12-19 | 2020-02-05 | Rolls Royce Plc | Shaft bearings for gas turbine engine |
GB201918779D0 (en) | 2019-12-19 | 2020-02-05 | Rolls Royce Plc | Shaft bearings |
GB201918781D0 (en) | 2019-12-19 | 2020-02-05 | Rolls Royce Plc | Improved shaft bearing positioning in a gas turbine engine |
GB201918783D0 (en) * | 2019-12-19 | 2020-02-05 | Rolls Royce Plc | Shaft with three bearings |
GB201918782D0 (en) | 2019-12-19 | 2020-02-05 | Rolls Royce Plc | Shaft bearing arrangement |
US11834956B2 (en) * | 2021-12-20 | 2023-12-05 | Rolls-Royce Plc | Gas turbine engine components with metallic and ceramic foam for improved cooling |
Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB885322A (en) * | 1957-01-31 | 1961-12-28 | Federal Mogul Bower Bearings | A process of fabricating transpiration cooled turbine blades and the blades producedthereby |
US3567333A (en) * | 1969-01-31 | 1971-03-02 | Curtiss Wright Corp | Gas turbine blade |
US3644059A (en) * | 1970-06-05 | 1972-02-22 | John K Bryan | Cooled airfoil |
US3656863A (en) * | 1970-07-27 | 1972-04-18 | Curtiss Wright Corp | Transpiration cooled turbine rotor blade |
DE2503285A1 (de) * | 1975-01-28 | 1976-07-29 | Motoren Turbinen Union | Thermisch hochbeanspruchtes, gekuehltes bauteil, insbesondere schaufel fuer turbinentriebwerke |
US5073459A (en) * | 1989-01-25 | 1991-12-17 | Mtu Motoren- Und Turbinen-Union Munchen Gmbh | Sintered light-weight structural material and method of its manufacture |
EP0764764A1 (fr) * | 1995-09-25 | 1997-03-26 | General Electric Company | Aube partialement métallique pour une turbine à gaz |
US5634189A (en) * | 1993-11-11 | 1997-05-27 | Mtu Motoren-Und Turbinen Union Munchen Gmbh | Structural component made of metal or ceramic having a solid outer shell and a porous core and its method of manufacture |
US5690473A (en) * | 1992-08-25 | 1997-11-25 | General Electric Company | Turbine blade having transpiration strip cooling and method of manufacture |
EP1063389A2 (fr) * | 1999-06-24 | 2000-12-27 | ABB Research Ltd. | Aube de turbine |
EP1155760A1 (fr) * | 2000-05-17 | 2001-11-21 | ALSTOM Power N.V. | Procédé de fabrication d'une pièce moulée à charge thermique élevée |
Family Cites Families (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1130285A (en) * | 1967-05-05 | 1968-10-16 | Rolls Royce | Method of making an aerofoil shaped blade for a fluid flow machine |
US3810286A (en) * | 1969-09-10 | 1974-05-14 | Universal Cyclops Specialty St | Methods for manufacturing hollow members |
US3695778A (en) * | 1970-09-18 | 1972-10-03 | Trw Inc | Turbine blade |
US3778188A (en) * | 1972-09-11 | 1973-12-11 | Gen Motors Corp | Cooled turbine rotor and its manufacture |
JPS5216841B2 (fr) * | 1974-06-18 | 1977-05-12 | ||
JPS5121010A (ja) * | 1974-08-14 | 1976-02-19 | Tokyo Shibaura Electric Co | Gasutaabinyoku |
JPS5519959A (en) * | 1978-07-29 | 1980-02-13 | Kawasaki Heavy Ind Ltd | Cooling wing |
GB2042648B (en) * | 1979-02-24 | 1983-05-05 | Rolls Royce | Gas turbine engine hollow blades |
JPS59153902A (ja) * | 1983-02-23 | 1984-09-01 | Hitachi Ltd | 冷却翼 |
JPH01127631A (ja) * | 1987-11-10 | 1989-05-19 | Agency Of Ind Science & Technol | 発泡金属の製造方法 |
JPH03230859A (ja) * | 1990-02-07 | 1991-10-14 | Mitsubishi Heavy Ind Ltd | 軽量アルミニウム鋳物の製造方法 |
JP3237115B2 (ja) * | 1990-05-29 | 2001-12-10 | スズキ株式会社 | Ti―Al系金属間化合物の発泡体製造方法と製品 |
FR2688264A1 (fr) * | 1992-03-04 | 1993-09-10 | Snecma | Redresseur de turbomachine a aubes ayant une face alveolee chargee en materiau composite. |
JPH07293204A (ja) * | 1994-04-27 | 1995-11-07 | Mitsubishi Heavy Ind Ltd | ガスタービン冷却翼 |
JP3352584B2 (ja) * | 1996-03-11 | 2002-12-03 | 神鋼鋼線工業株式会社 | 金属発泡体の製造方法 |
JPH1054204A (ja) * | 1996-05-20 | 1998-02-24 | General Electric Co <Ge> | ガスタービン用の多構成部翼 |
EP0884123B1 (fr) * | 1997-06-10 | 2003-03-26 | Goldschmidt AG | Corps métallique moussable |
JP3462750B2 (ja) * | 1998-05-14 | 2003-11-05 | 住友電気工業株式会社 | ディーゼルエンジン用パティキュレートトラップ |
US6544003B1 (en) * | 2000-11-08 | 2003-04-08 | General Electric Co. | Gas turbine blisk with ceramic foam blades and its preparation |
-
2000
- 2000-09-05 EP EP00119203A patent/EP1186748A1/fr not_active Withdrawn
-
2001
- 2001-08-23 EP EP06014569A patent/EP1707745A3/fr not_active Withdrawn
- 2001-08-23 WO PCT/EP2001/009759 patent/WO2002020948A1/fr active IP Right Grant
- 2001-08-23 DE DE50111221T patent/DE50111221D1/de not_active Expired - Lifetime
- 2001-08-23 EP EP01971957A patent/EP1322838B1/fr not_active Expired - Lifetime
- 2001-08-23 JP JP2002525339A patent/JP4499351B2/ja not_active Expired - Fee Related
- 2001-08-23 CN CNB018149537A patent/CN1325761C/zh not_active Expired - Fee Related
-
2003
- 2003-03-05 US US10/379,987 patent/US6827556B2/en not_active Expired - Fee Related
Patent Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB885322A (en) * | 1957-01-31 | 1961-12-28 | Federal Mogul Bower Bearings | A process of fabricating transpiration cooled turbine blades and the blades producedthereby |
US3567333A (en) * | 1969-01-31 | 1971-03-02 | Curtiss Wright Corp | Gas turbine blade |
US3644059A (en) * | 1970-06-05 | 1972-02-22 | John K Bryan | Cooled airfoil |
US3656863A (en) * | 1970-07-27 | 1972-04-18 | Curtiss Wright Corp | Transpiration cooled turbine rotor blade |
DE2503285A1 (de) * | 1975-01-28 | 1976-07-29 | Motoren Turbinen Union | Thermisch hochbeanspruchtes, gekuehltes bauteil, insbesondere schaufel fuer turbinentriebwerke |
US5073459A (en) * | 1989-01-25 | 1991-12-17 | Mtu Motoren- Und Turbinen-Union Munchen Gmbh | Sintered light-weight structural material and method of its manufacture |
US5690473A (en) * | 1992-08-25 | 1997-11-25 | General Electric Company | Turbine blade having transpiration strip cooling and method of manufacture |
US5634189A (en) * | 1993-11-11 | 1997-05-27 | Mtu Motoren-Und Turbinen Union Munchen Gmbh | Structural component made of metal or ceramic having a solid outer shell and a porous core and its method of manufacture |
EP0764764A1 (fr) * | 1995-09-25 | 1997-03-26 | General Electric Company | Aube partialement métallique pour une turbine à gaz |
EP1063389A2 (fr) * | 1999-06-24 | 2000-12-27 | ABB Research Ltd. | Aube de turbine |
EP1155760A1 (fr) * | 2000-05-17 | 2001-11-21 | ALSTOM Power N.V. | Procédé de fabrication d'une pièce moulée à charge thermique élevée |
Also Published As
Publication number | Publication date |
---|---|
EP1322838B1 (fr) | 2006-10-11 |
CN1449470A (zh) | 2003-10-15 |
CN1325761C (zh) | 2007-07-11 |
DE50111221D1 (de) | 2006-11-23 |
EP1707745A2 (fr) | 2006-10-04 |
EP1322838A1 (fr) | 2003-07-02 |
US20030185685A1 (en) | 2003-10-02 |
US6827556B2 (en) | 2004-12-07 |
JP4499351B2 (ja) | 2010-07-07 |
WO2002020948A1 (fr) | 2002-03-14 |
EP1186748A1 (fr) | 2002-03-13 |
JP2004508478A (ja) | 2004-03-18 |
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