JP4681272B2 - タービンシュラウド用のばね質量ダンパシステム - Google Patents
タービンシュラウド用のばね質量ダンパシステム Download PDFInfo
- Publication number
- JP4681272B2 JP4681272B2 JP2004320157A JP2004320157A JP4681272B2 JP 4681272 B2 JP4681272 B2 JP 4681272B2 JP 2004320157 A JP2004320157 A JP 2004320157A JP 2004320157 A JP2004320157 A JP 2004320157A JP 4681272 B2 JP4681272 B2 JP 4681272B2
- Authority
- JP
- Japan
- Prior art keywords
- shroud
- damper
- spring
- damper block
- piston
- 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.)
- Expired - Lifetime
Links
Images
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
- F01D25/005—Selecting particular materials
-
- 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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/04—Antivibration arrangements
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Materials Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Springs (AREA)
- Pistons, Piston Rings, And Cylinders (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US10/700,251 US6942203B2 (en) | 2003-11-04 | 2003-11-04 | Spring mass damper system for turbine shrouds |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2005140114A JP2005140114A (ja) | 2005-06-02 |
| JP2005140114A5 JP2005140114A5 (enExample) | 2007-12-20 |
| JP4681272B2 true JP4681272B2 (ja) | 2011-05-11 |
Family
ID=34435517
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2004320157A Expired - Lifetime JP4681272B2 (ja) | 2003-11-04 | 2004-11-04 | タービンシュラウド用のばね質量ダンパシステム |
Country Status (4)
| Country | Link |
|---|---|
| US (3) | US6942203B2 (enExample) |
| EP (1) | EP1529926B1 (enExample) |
| JP (1) | JP4681272B2 (enExample) |
| CN (1) | CN100430574C (enExample) |
Families Citing this family (103)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2005106634A (ja) * | 2003-09-30 | 2005-04-21 | Takata Corp | シート重量計測装置 |
| US6942203B2 (en) * | 2003-11-04 | 2005-09-13 | General Electric Company | Spring mass damper system for turbine shrouds |
| US7494317B2 (en) | 2005-06-23 | 2009-02-24 | Siemens Energy, Inc. | Ring seal attachment system |
| US7278820B2 (en) * | 2005-10-04 | 2007-10-09 | Siemens Power Generation, Inc. | Ring seal system with reduced cooling requirements |
| US7238002B2 (en) * | 2005-11-03 | 2007-07-03 | General Electric Company | Damper seal system and method |
| US20080096819A1 (en) * | 2006-05-02 | 2008-04-24 | Allozyne, Inc. | Amino acid substituted molecules |
| US7665960B2 (en) | 2006-08-10 | 2010-02-23 | United Technologies Corporation | Turbine shroud thermal distortion control |
| US7771160B2 (en) * | 2006-08-10 | 2010-08-10 | United Technologies Corporation | Ceramic shroud assembly |
| US7950234B2 (en) * | 2006-10-13 | 2011-05-31 | Siemens Energy, Inc. | Ceramic matrix composite turbine engine components with unitary stiffening frame |
| US7771159B2 (en) * | 2006-10-16 | 2010-08-10 | General Electric Company | High temperature seals and high temperature sealing systems |
| US7811054B2 (en) * | 2007-05-30 | 2010-10-12 | General Electric Company | Shroud configuration having sloped seal |
| US8047773B2 (en) * | 2007-08-23 | 2011-11-01 | General Electric Company | Gas turbine shroud support apparatus |
| US20090165945A1 (en) * | 2007-12-27 | 2009-07-02 | General Electric Company | Tool for use in the manufacture of turbine bucket shroud and related method |
| US8240988B2 (en) * | 2008-03-26 | 2012-08-14 | Siemens Energy, Inc. | Fastener assembly with cyclone cooling |
| US9127565B2 (en) * | 2008-04-16 | 2015-09-08 | Siemens Energy, Inc. | Apparatus comprising a CMC-comprising body and compliant porous element preloaded within an outer metal shell |
| US8118546B2 (en) * | 2008-08-20 | 2012-02-21 | Siemens Energy, Inc. | Grid ceramic matrix composite structure for gas turbine shroud ring segment |
| US8973375B2 (en) * | 2008-12-31 | 2015-03-10 | Rolls-Royce North American Technologies, Inc. | Shielding for a gas turbine engine component |
| US8382436B2 (en) | 2009-01-06 | 2013-02-26 | General Electric Company | Non-integral turbine blade platforms and systems |
| ATE537333T1 (de) * | 2009-01-28 | 2011-12-15 | Alstom Technology Ltd | Streifendichtung und verfahren zum entwurf einer streifendichtung |
| US8262345B2 (en) | 2009-02-06 | 2012-09-11 | General Electric Company | Ceramic matrix composite turbine engine |
| ES2542159T3 (es) | 2009-03-09 | 2015-07-31 | Ge Avio S.R.L. | Rotor para turbomáquinas |
| US8393858B2 (en) * | 2009-03-13 | 2013-03-12 | Honeywell International Inc. | Turbine shroud support coupling assembly |
| US8142138B2 (en) * | 2009-05-01 | 2012-03-27 | General Electric Company | Turbine engine having cooling pin |
| US20100284810A1 (en) * | 2009-05-07 | 2010-11-11 | General Electric Company | Process for inhibiting delamination in a bend of a continuous fiber-reinforced composite article |
| DE102009039184A1 (de) * | 2009-08-28 | 2011-03-17 | Man Diesel & Turbo Se | Turbomaschine |
| US8167546B2 (en) * | 2009-09-01 | 2012-05-01 | United Technologies Corporation | Ceramic turbine shroud support |
| FR2952965B1 (fr) * | 2009-11-25 | 2012-03-09 | Snecma | Isolation d'un rebord circonferentiel d'un carter externe de turbomachine vis-a-vis d'un secteur d'anneau correspondant |
| US8529201B2 (en) * | 2009-12-17 | 2013-09-10 | United Technologies Corporation | Blade outer air seal formed of stacked panels |
| JP5569194B2 (ja) | 2010-07-02 | 2014-08-13 | 株式会社Ihi | シュラウドセグメントの製造方法 |
| US8807885B2 (en) * | 2010-10-07 | 2014-08-19 | General Electric Company | Method and apparatus for machining a shroud block |
| US8790067B2 (en) | 2011-04-27 | 2014-07-29 | United Technologies Corporation | Blade clearance control using high-CTE and low-CTE ring members |
| US8864492B2 (en) | 2011-06-23 | 2014-10-21 | United Technologies Corporation | Reverse flow combustor duct attachment |
| US8739547B2 (en) * | 2011-06-23 | 2014-06-03 | United Technologies Corporation | Gas turbine engine joint having a metallic member, a CMC member, and a ceramic key |
| US9335051B2 (en) | 2011-07-13 | 2016-05-10 | United Technologies Corporation | Ceramic matrix composite combustor vane ring assembly |
| US8920127B2 (en) | 2011-07-18 | 2014-12-30 | United Technologies Corporation | Turbine rotor non-metallic blade attachment |
| US9328623B2 (en) * | 2011-10-05 | 2016-05-03 | General Electric Company | Turbine system |
| US8920116B2 (en) * | 2011-10-07 | 2014-12-30 | Siemens Energy, Inc. | Wear prevention system for securing compressor airfoils within a turbine engine |
| US9726043B2 (en) | 2011-12-15 | 2017-08-08 | General Electric Company | Mounting apparatus for low-ductility turbine shroud |
| US8899914B2 (en) | 2012-01-05 | 2014-12-02 | United Technologies Corporation | Stator vane integrated attachment liner and spring damper |
| FR2989140B1 (fr) * | 2012-04-06 | 2014-09-05 | Snecma | Systeme de transmission de puissance pour une turbomachine |
| US9527262B2 (en) | 2012-09-28 | 2016-12-27 | General Electric Company | Layered arrangement, hot-gas path component, and process of producing a layered arrangement |
| US9416671B2 (en) | 2012-10-04 | 2016-08-16 | General Electric Company | Bimetallic turbine shroud and method of fabricating |
| US20140223919A1 (en) * | 2013-02-14 | 2014-08-14 | United Technologies Corporation | Flexible liner hanger |
| CA2900687C (en) | 2013-03-05 | 2019-06-18 | Rolls-Royce Corporation | Structure and method for providing compliance and sealing between ceramic and metallic structures |
| EP2971587B1 (en) | 2013-03-12 | 2020-02-05 | Rolls-Royce Corporation | Turbine blade track assembly |
| US9458731B2 (en) | 2013-03-13 | 2016-10-04 | General Electric Company | Turbine shroud cooling system |
| EP2971588A1 (en) | 2013-03-13 | 2016-01-20 | Rolls-Royce Corporation | Dovetail retention system for blade tracks |
| JP6114878B2 (ja) | 2013-05-17 | 2017-04-12 | ゼネラル・エレクトリック・カンパニイ | Cmcシュラウド支持システム |
| EP3044514B1 (en) | 2013-09-11 | 2019-04-24 | General Electric Company | Spring loaded and sealed ceramic matrix composite combustor liner |
| JP6529013B2 (ja) | 2013-12-12 | 2019-06-12 | ゼネラル・エレクトリック・カンパニイ | Cmcシュラウド支持システム |
| US9464530B2 (en) * | 2014-02-20 | 2016-10-11 | General Electric Company | Turbine bucket and method for balancing a tip shroud of a turbine bucket |
| US10400619B2 (en) | 2014-06-12 | 2019-09-03 | General Electric Company | Shroud hanger assembly |
| US11668207B2 (en) | 2014-06-12 | 2023-06-06 | General Electric Company | Shroud hanger assembly |
| CA2951431C (en) | 2014-06-12 | 2019-03-26 | General Electric Company | Multi-piece shroud hanger assembly |
| US10982564B2 (en) | 2014-12-15 | 2021-04-20 | General Electric Company | Apparatus and system for ceramic matrix composite attachment |
| US10100659B2 (en) | 2014-12-16 | 2018-10-16 | Rolls-Royce North American Technologies Inc. | Hanger system for a turbine engine component |
| US9874104B2 (en) | 2015-02-27 | 2018-01-23 | General Electric Company | Method and system for a ceramic matrix composite shroud hanger assembly |
| US10100649B2 (en) | 2015-03-31 | 2018-10-16 | Rolls-Royce North American Technologies Inc. | Compliant rail hanger |
| FR3036435B1 (fr) * | 2015-05-22 | 2020-01-24 | Safran Ceramics | Ensemble d'anneau de turbine |
| US10370997B2 (en) | 2015-05-26 | 2019-08-06 | Rolls-Royce Corporation | Turbine shroud having ceramic matrix composite seal segment |
| US9963990B2 (en) | 2015-05-26 | 2018-05-08 | Rolls-Royce North American Technologies, Inc. | Ceramic matrix composite seal segment for a gas turbine engine |
| US10221713B2 (en) | 2015-05-26 | 2019-03-05 | Rolls-Royce Corporation | Shroud cartridge having a ceramic matrix composite seal segment |
| US10370998B2 (en) | 2015-05-26 | 2019-08-06 | Rolls-Royce Corporation | Flexibly mounted ceramic matrix composite seal segments |
| US10087770B2 (en) | 2015-05-26 | 2018-10-02 | Rolls-Royce Corporation | Shroud cartridge having a ceramic matrix composite seal segment |
| US10094234B2 (en) | 2015-06-29 | 2018-10-09 | Rolls-Royce North America Technologies Inc. | Turbine shroud segment with buffer air seal system |
| US10047624B2 (en) | 2015-06-29 | 2018-08-14 | Rolls-Royce North American Technologies Inc. | Turbine shroud segment with flange-facing perimeter seal |
| US10196919B2 (en) | 2015-06-29 | 2019-02-05 | Rolls-Royce North American Technologies Inc. | Turbine shroud segment with load distribution springs |
| US10132186B2 (en) * | 2015-08-13 | 2018-11-20 | General Electric Company | System and method for supporting a turbine shroud |
| US9903218B2 (en) * | 2015-08-17 | 2018-02-27 | General Electric Company | Turbine shroud assembly |
| US10443417B2 (en) | 2015-09-18 | 2019-10-15 | General Electric Company | Ceramic matrix composite ring shroud retention methods-finger seals with stepped shroud interface |
| US10094244B2 (en) | 2015-09-18 | 2018-10-09 | General Electric Company | Ceramic matrix composite ring shroud retention methods-wiggle strip spring seal |
| US9945257B2 (en) * | 2015-09-18 | 2018-04-17 | General Electric Company | Ceramic matrix composite ring shroud retention methods-CMC pin-head |
| US10138750B2 (en) * | 2016-03-16 | 2018-11-27 | United Technologies Corporation | Boas segmented heat shield |
| DE102016211613A1 (de) * | 2016-06-28 | 2017-12-28 | Siemens Aktiengesellschaft | Hitzeschildanordnung einer Brennkammer mit Tellerfederpaket |
| FR3056636B1 (fr) * | 2016-09-27 | 2020-06-05 | Safran Aircraft Engines | Ensemble d'anneau de turbine sans jeu de montage a froid |
| US10533581B2 (en) | 2016-12-09 | 2020-01-14 | United Technologies Corporation | Stator with support structure feature for tuned airfoil |
| US10371611B2 (en) | 2017-01-12 | 2019-08-06 | Rolls-Royce North American Technologies Inc. | Material testing system and method of use |
| US10480337B2 (en) | 2017-04-18 | 2019-11-19 | Rolls-Royce North American Technologies Inc. | Turbine shroud assembly with multi-piece seals |
| US10669895B2 (en) | 2017-06-15 | 2020-06-02 | General Electric Company | Shroud dampening pin and turbine shroud assembly |
| US10544701B2 (en) * | 2017-06-15 | 2020-01-28 | General Electric Company | Turbine shroud assembly |
| US10526921B2 (en) | 2017-06-15 | 2020-01-07 | General Electric Company | Anti-rotation shroud dampening pin and turbine shroud assembly |
| US10876417B2 (en) | 2017-08-17 | 2020-12-29 | Raytheon Technologies Corporation | Tuned airfoil assembly |
| US10557365B2 (en) | 2017-10-05 | 2020-02-11 | Rolls-Royce Corporation | Ceramic matrix composite blade track with mounting system having reaction load distribution features |
| US10392957B2 (en) | 2017-10-05 | 2019-08-27 | Rolls-Royce Corporation | Ceramic matrix composite blade track with mounting system having load distribution features |
| US10619514B2 (en) | 2017-10-18 | 2020-04-14 | Rolls-Royce Corporation | Ceramic matrix composite assembly with compliant pin attachment features |
| CN107882599B (zh) * | 2017-11-01 | 2021-02-09 | 中国航发湖南动力机械研究所 | 整体式涡轮外环连接结构及涡轮发动机 |
| US11021986B2 (en) | 2018-03-20 | 2021-06-01 | Raytheon Technologies Corporation | Seal assembly for gas turbine engine |
| US10711630B2 (en) | 2018-03-20 | 2020-07-14 | Honeywell International Inc. | Retention and control system for turbine shroud ring |
| US10801351B2 (en) | 2018-04-17 | 2020-10-13 | Raytheon Technologies Corporation | Seal assembly for gas turbine engine |
| US10689997B2 (en) | 2018-04-17 | 2020-06-23 | Raytheon Technologies Corporation | Seal assembly for gas turbine engine |
| US11047250B2 (en) * | 2019-04-05 | 2021-06-29 | Raytheon Technologies Corporation | CMC BOAS transverse hook arrangement |
| US11536454B2 (en) * | 2019-05-09 | 2022-12-27 | Pratt & Whitney Canada Corp. | Combustor wall assembly for gas turbine engine |
| US11174739B2 (en) | 2019-08-27 | 2021-11-16 | Solar Turbines Incorporated | Damped turbine blade assembly |
| US11352897B2 (en) | 2019-09-26 | 2022-06-07 | Raytheon Technologies Corporation | Double box composite seal assembly for gas turbine engine |
| US11220924B2 (en) | 2019-09-26 | 2022-01-11 | Raytheon Technologies Corporation | Double box composite seal assembly with insert for gas turbine engine |
| US11359507B2 (en) | 2019-09-26 | 2022-06-14 | Raytheon Technologies Corporation | Double box composite seal assembly with fiber density arrangement for gas turbine engine |
| 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 |
| US11041399B2 (en) * | 2019-11-01 | 2021-06-22 | Raytheon Technologies Corporation | CMC heat shield |
| US11187098B2 (en) | 2019-12-20 | 2021-11-30 | Rolls-Royce Corporation | Turbine shroud assembly with hangers for ceramic matrix composite material seal segments |
| KR20220156559A (ko) * | 2020-03-31 | 2022-11-25 | 마큐 에이비 | 공구 어셈블리용 공구 홀더 및 공구 홀더를 포함하는 공구 어셈블리 |
| US12055058B2 (en) * | 2022-05-31 | 2024-08-06 | Pratt & Whitney Canada Corp. | Joint between gas turbine engine components with a spring element |
| CN115013079B (zh) * | 2022-07-08 | 2024-10-29 | 泰安凯顺机电工程有限公司 | 一种汽轮机 |
| US12091980B1 (en) | 2023-12-13 | 2024-09-17 | Honeywell International Inc. | Spring biased shroud retention system for gas turbine engine |
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| US3864056A (en) * | 1973-07-27 | 1975-02-04 | Westinghouse Electric Corp | Cooled turbine blade ring assembly |
| US4087199A (en) * | 1976-11-22 | 1978-05-02 | General Electric Company | Ceramic turbine shroud assembly |
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| CA1156844A (en) * | 1980-08-27 | 1983-11-15 | Westinghouse Canada Inc. | Blade tip clearance control for an industrial gas turbine engine |
| US4621976A (en) * | 1985-04-23 | 1986-11-11 | United Technologies Corporation | Integrally cast vane and shroud stator with damper |
| FR2597921A1 (fr) * | 1986-04-24 | 1987-10-30 | Snecma | Anneau de turbine sectorise |
| US5346362A (en) * | 1993-04-26 | 1994-09-13 | United Technologies Corporation | Mechanical damper |
| DE4329014C1 (de) * | 1993-08-28 | 1995-01-05 | Mtu Muenchen Gmbh | Rotorgehäuse, insbesondere Gehäuse für Turbotriebwerke |
| US5618161A (en) * | 1995-10-17 | 1997-04-08 | Westinghouse Electric Corporation | Apparatus for restraining motion of a turbo-machine stationary vane |
| US5639211A (en) * | 1995-11-30 | 1997-06-17 | United Technology Corporation | Brush seal for stator of a gas turbine engine case |
| US6024898A (en) | 1996-12-30 | 2000-02-15 | General Electric Company | Article and method for making complex shaped preform and silicon carbide composite by melt infiltration |
| US5952100A (en) | 1997-05-21 | 1999-09-14 | General Electric Company | Silicon-doped boron nitride coated fibers in silicon melt infiltrated composites |
| DE19740990C2 (de) * | 1997-09-18 | 2001-11-29 | Enidine Gmbh | Kolben-Zylinder-Anordnung |
| FR2780443B1 (fr) * | 1998-06-25 | 2000-08-04 | Snecma | Anneau de stator de turbine haute pression d'une turbomachine |
| US6126389A (en) * | 1998-09-02 | 2000-10-03 | General Electric Co. | Impingement cooling for the shroud of a gas turbine |
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| US6435824B1 (en) | 2000-11-08 | 2002-08-20 | General Electric Co. | Gas turbine stationary shroud made of a ceramic foam material, and its preparation |
| US6503441B2 (en) | 2001-05-30 | 2003-01-07 | General Electric Company | Method for producing melt-infiltrated ceramic composites using formed supports |
| US6726448B2 (en) * | 2002-05-15 | 2004-04-27 | General Electric Company | Ceramic turbine shroud |
| JP2004036443A (ja) * | 2002-07-02 | 2004-02-05 | Ishikawajima Harima Heavy Ind Co Ltd | ガスタービンシュラウド構造 |
| US6814538B2 (en) * | 2003-01-22 | 2004-11-09 | General Electric Company | Turbine stage one shroud configuration and method for service enhancement |
| US6942203B2 (en) * | 2003-11-04 | 2005-09-13 | General Electric Company | Spring mass damper system for turbine shrouds |
-
2003
- 2003-11-04 US US10/700,251 patent/US6942203B2/en not_active Expired - Lifetime
-
2004
- 2004-03-05 US US10/793,051 patent/US7117983B2/en not_active Expired - Lifetime
- 2004-11-04 CN CNB2004100903739A patent/CN100430574C/zh not_active Expired - Lifetime
- 2004-11-04 EP EP04256829.5A patent/EP1529926B1/en not_active Expired - Lifetime
- 2004-11-04 JP JP2004320157A patent/JP4681272B2/ja not_active Expired - Lifetime
-
2006
- 2006-08-16 US US11/504,673 patent/US7434670B2/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| US20050092566A1 (en) | 2005-05-05 |
| US20080202877A1 (en) | 2008-08-28 |
| US7434670B2 (en) | 2008-10-14 |
| CN100430574C (zh) | 2008-11-05 |
| EP1529926A2 (en) | 2005-05-11 |
| JP2005140114A (ja) | 2005-06-02 |
| US7117983B2 (en) | 2006-10-10 |
| EP1529926B1 (en) | 2014-09-17 |
| EP1529926A3 (en) | 2012-08-22 |
| US20050093214A1 (en) | 2005-05-05 |
| US6942203B2 (en) | 2005-09-13 |
| CN1614199A (zh) | 2005-05-11 |
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