CN1854486B - 对转式涡轮机引擎及其组装方法 - Google Patents
对转式涡轮机引擎及其组装方法 Download PDFInfo
- Publication number
- CN1854486B CN1854486B CN200510097640XA CN200510097640A CN1854486B CN 1854486 B CN1854486 B CN 1854486B CN 200510097640X A CN200510097640X A CN 200510097640XA CN 200510097640 A CN200510097640 A CN 200510097640A CN 1854486 B CN1854486 B CN 1854486B
- Authority
- CN
- China
- Prior art keywords
- foil bearing
- rotor
- external rotor
- pressure turbine
- foil
- 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 - Fee Related
Links
- 238000000034 method Methods 0.000 title abstract description 20
- 239000011888 foil Substances 0.000 claims abstract description 115
- 230000002093 peripheral effect Effects 0.000 claims description 5
- 229920003266 Leaf® Polymers 0.000 claims 6
- 230000008878 coupling Effects 0.000 abstract 1
- 238000010168 coupling process Methods 0.000 abstract 1
- 238000005859 coupling reaction Methods 0.000 abstract 1
- 239000007789 gas Substances 0.000 description 40
- 239000000567 combustion gas Substances 0.000 description 6
- 238000004519 manufacturing process Methods 0.000 description 5
- 238000007789 sealing Methods 0.000 description 4
- 238000011144 upstream manufacturing Methods 0.000 description 4
- 239000000284 extract Substances 0.000 description 2
- 239000012530 fluid Substances 0.000 description 2
- 230000001970 hydrokinetic effect Effects 0.000 description 2
- 230000000007 visual effect Effects 0.000 description 2
- 241000239290 Araneae Species 0.000 description 1
- 206010033307 Overweight Diseases 0.000 description 1
- 238000007664 blowing Methods 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 238000002955 isolation Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000008041 oiling agent Substances 0.000 description 1
- 238000005457 optimization Methods 0.000 description 1
- 235000020825 overweight Nutrition 0.000 description 1
- 238000012827 research and development Methods 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C17/00—Sliding-contact bearings for exclusively rotary movement
- F16C17/02—Sliding-contact bearings for exclusively rotary movement for radial load only
- F16C17/024—Sliding-contact bearings for exclusively rotary movement for radial load only with flexible leaves to create hydrodynamic wedge, e.g. radial foil bearings
-
- 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
- F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
- F01D1/24—Non-positive-displacement machines or engines, e.g. steam turbines characterised by counter-rotating rotors subjected to same working fluid stream without intermediate stator blades or the like
-
- 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
- F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
-
- 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
- F02C3/06—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages
- F02C3/067—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages having counter-rotating rotors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
- F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
- F02K3/072—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with counter-rotating, e.g. fan rotors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C17/00—Sliding-contact bearings for exclusively rotary movement
- F16C17/12—Sliding-contact bearings for exclusively rotary movement characterised by features not related to the direction of the load
- F16C17/18—Sliding-contact bearings for exclusively rotary movement characterised by features not related to the direction of the load with floating brasses or brushing, rotatable at a reduced speed
-
- 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
- F05D2240/50—Bearings
- F05D2240/53—Hydrodynamic or hydrostatic bearings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2360/00—Engines or pumps
- F16C2360/23—Gas turbine engines
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Support Of The Bearing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US10/976,496 US7195446B2 (en) | 2004-10-29 | 2004-10-29 | Counter-rotating turbine engine and method of assembling same |
| US10/976496 | 2004-10-29 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN1854486A CN1854486A (zh) | 2006-11-01 |
| CN1854486B true CN1854486B (zh) | 2011-08-24 |
Family
ID=35033621
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN200510097640XA Expired - Fee Related CN1854486B (zh) | 2004-10-29 | 2005-08-29 | 对转式涡轮机引擎及其组装方法 |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US7195446B2 (enExample) |
| EP (1) | EP1655475B1 (enExample) |
| JP (1) | JP4693551B2 (enExample) |
| CN (1) | CN1854486B (enExample) |
| DE (1) | DE602005003759T2 (enExample) |
Families Citing this family (70)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7269938B2 (en) * | 2004-10-29 | 2007-09-18 | General Electric Company | Counter-rotating gas turbine engine and method of assembling same |
| FR2908452A1 (fr) * | 2006-11-15 | 2008-05-16 | Snecma Sa | Dispositif de fixation de stator de turbine libre par double centrage. |
| EP2123884B1 (en) * | 2008-05-13 | 2015-03-04 | Rolls-Royce Corporation | Dual clutch arrangement |
| US20140174056A1 (en) | 2008-06-02 | 2014-06-26 | United Technologies Corporation | Gas turbine engine with low stage count low pressure turbine |
| US8128021B2 (en) | 2008-06-02 | 2012-03-06 | United Technologies Corporation | Engine mount system for a turbofan gas turbine engine |
| US20100005810A1 (en) * | 2008-07-11 | 2010-01-14 | Rob Jarrell | Power transmission among shafts in a turbine engine |
| US8480527B2 (en) * | 2008-08-27 | 2013-07-09 | Rolls-Royce Corporation | Gearing arrangement |
| FR2938013B1 (fr) * | 2008-11-04 | 2015-08-07 | Microturbo | Turbomachine a paliers mixtes de support d'arbres. |
| US8011877B2 (en) * | 2008-11-24 | 2011-09-06 | General Electric Company | Fiber composite reinforced aircraft gas turbine engine drums with radially inwardly extending blades |
| US8021267B2 (en) * | 2008-12-11 | 2011-09-20 | Rolls-Royce Corporation | Coupling assembly |
| US8075438B2 (en) * | 2008-12-11 | 2011-12-13 | Rolls-Royce Corporation | Apparatus and method for transmitting a rotary input into counter-rotating outputs |
| CN101963073B (zh) * | 2009-07-22 | 2012-05-23 | 中国科学院工程热物理研究所 | 具有悬垂转子叶片结构的对转涡轮 |
| US8739513B2 (en) * | 2009-08-17 | 2014-06-03 | Pratt & Whitney Canada Corp. | Gas turbine engine exhaust mixer |
| FR2976024B1 (fr) * | 2011-05-31 | 2015-10-30 | Snecma | Moteur a turbine a gaz comportant trois corps rotatifs |
| US9239012B2 (en) | 2011-06-08 | 2016-01-19 | United Technologies Corporation | Flexible support structure for a geared architecture gas turbine engine |
| US9410608B2 (en) | 2011-06-08 | 2016-08-09 | United Technologies Corporation | Flexible support structure for a geared architecture gas turbine engine |
| US9631558B2 (en) | 2012-01-03 | 2017-04-25 | United Technologies Corporation | Geared architecture for high speed and small volume fan drive turbine |
| US8973373B2 (en) | 2011-10-31 | 2015-03-10 | General Electric Company | Active clearance control system and method for gas turbine |
| US20130192256A1 (en) * | 2012-01-31 | 2013-08-01 | Gabriel L. Suciu | Geared turbofan engine with counter-rotating shafts |
| US10287914B2 (en) | 2012-01-31 | 2019-05-14 | United Technologies Corporation | Gas turbine engine with high speed low pressure turbine section and bearing support features |
| US9028200B2 (en) * | 2012-02-29 | 2015-05-12 | United Technologies Corporation | Counter rotating low pressure turbine with splitter gear system |
| US10125693B2 (en) | 2012-04-02 | 2018-11-13 | United Technologies Corporation | Geared turbofan engine with power density range |
| US20150308351A1 (en) | 2012-05-31 | 2015-10-29 | United Technologies Corporation | Fundamental gear system architecture |
| US8572943B1 (en) | 2012-05-31 | 2013-11-05 | United Technologies Corporation | Fundamental gear system architecture |
| US8756908B2 (en) | 2012-05-31 | 2014-06-24 | United Technologies Corporation | Fundamental gear system architecture |
| FR3005099B1 (fr) * | 2013-04-30 | 2017-08-25 | Snecma | Structure de turbomachine comportant une bague de ventilation |
| US9410430B2 (en) | 2014-06-19 | 2016-08-09 | Jay HASKIN | Turbine apparatus with counter-rotating blades |
| BE1022364B1 (fr) * | 2014-10-27 | 2016-03-17 | Techspace Aero S.A. | Compresseur de turbomachine axiale avec double rotors contrarotatifs |
| GB201512494D0 (en) * | 2015-07-17 | 2015-08-19 | Rolls Royce Plc And Rolls Royce Deutschland Ltd & Co Kg | Gas turbine engine |
| US10392970B2 (en) * | 2016-11-02 | 2019-08-27 | General Electric Company | Rotor shaft architectures for a gas turbine engine and methods of assembly thereof |
| US9745860B1 (en) * | 2016-11-02 | 2017-08-29 | Jay HASKIN | Power transmission system for turbine or compressor having counter-rotating blades |
| US10260367B2 (en) | 2016-11-02 | 2019-04-16 | Jay HASKIN | Power transmission system for turbines or compressors having counter-rotating blades |
| US10190436B2 (en) * | 2016-11-02 | 2019-01-29 | Jay HASKIN | Power transmission system for turbine, a turbocharger, a compressor, or a pump |
| US11053797B2 (en) * | 2017-01-23 | 2021-07-06 | General Electric Company | Rotor thrust balanced turbine engine |
| US10823114B2 (en) | 2017-02-08 | 2020-11-03 | General Electric Company | Counter rotating turbine with reversing reduction gearbox |
| US10465606B2 (en) | 2017-02-08 | 2019-11-05 | General Electric Company | Counter rotating turbine with reversing reduction gearbox |
| US10801442B2 (en) | 2017-02-08 | 2020-10-13 | General Electric Company | Counter rotating turbine with reversing reduction gear assembly |
| US10876407B2 (en) * | 2017-02-16 | 2020-12-29 | General Electric Company | Thermal structure for outer diameter mounted turbine blades |
| GB201704502D0 (en) * | 2017-03-22 | 2017-05-03 | Rolls Royce Plc | Gas turbine engine |
| US10294821B2 (en) * | 2017-04-12 | 2019-05-21 | General Electric Company | Interturbine frame for gas turbine engine |
| CN106988882B (zh) * | 2017-04-13 | 2019-03-01 | 深圳福世达动力科技有限公司 | 双级对转燃气轮机 |
| US10605168B2 (en) | 2017-05-25 | 2020-03-31 | General Electric Company | Interdigitated turbine engine air bearing cooling structure and method of thermal management |
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| US10914194B2 (en) | 2017-09-20 | 2021-02-09 | General Electric Company | Turbomachine with alternatingly spaced turbine rotor blades |
| US10458267B2 (en) * | 2017-09-20 | 2019-10-29 | General Electric Company | Seal assembly for counter rotating turbine assembly |
| US10781717B2 (en) | 2017-09-20 | 2020-09-22 | General Electric Company | Turbomachine with alternatingly spaced turbine rotor blades |
| US10823001B2 (en) * | 2017-09-20 | 2020-11-03 | General Electric Company | Turbomachine with alternatingly spaced turbine rotor blades |
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| US10480322B2 (en) | 2018-01-12 | 2019-11-19 | General Electric Company | Turbine engine with annular cavity |
| EP3578763A1 (en) | 2018-06-07 | 2019-12-11 | Haskin, Jay | Power transmission system for turbine, a turbocharger, a compressor, or a pump |
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| US11753939B2 (en) | 2019-02-20 | 2023-09-12 | General Electric Company | Turbomachine with alternatingly spaced rotor blades |
| US11085515B2 (en) | 2019-02-20 | 2021-08-10 | General Electric Company | Gearbox coupling in a turbomachine |
| US11021970B2 (en) | 2019-02-20 | 2021-06-01 | General Electric Company | Turbomachine with alternatingly spaced rotor blades |
| US11118535B2 (en) | 2019-03-05 | 2021-09-14 | General Electric Company | Reversing gear assembly for a turbo machine |
| FR3095670B1 (fr) * | 2019-04-30 | 2021-12-03 | Safran Aircraft Engines | Architecture améliorée de turbomachine à turbine contrarotative |
| GB201910009D0 (en) * | 2019-07-12 | 2019-08-28 | Rolls Royce Plc | Gas turbine engine electrical generator |
| US11280219B2 (en) * | 2019-11-27 | 2022-03-22 | General Electric Company | Rotor support structures for rotating drum rotors of gas turbine engines |
| US11274557B2 (en) * | 2019-11-27 | 2022-03-15 | General Electric Company | Damper assemblies for rotating drum rotors of gas turbine engines |
| FR3111377B1 (fr) | 2020-06-10 | 2022-07-15 | Safran Aircraft Engines | Architecture améliorée de turbomachine à turbine contrarotative |
| US11512637B2 (en) | 2020-11-12 | 2022-11-29 | General Electric Company | Turbine engine bearing arrangement |
| US11428160B2 (en) | 2020-12-31 | 2022-08-30 | General Electric Company | Gas turbine engine with interdigitated turbine and gear assembly |
| CN115492681B (zh) * | 2021-06-18 | 2025-07-22 | 中国航发商用航空发动机有限责任公司 | 三转子涡扇发动机 |
| US12247516B2 (en) * | 2022-09-29 | 2025-03-11 | General Electric Company | Counter-rotating gas turbine engines including turbine sections with separable torque frames |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4950089A (en) * | 1988-05-12 | 1990-08-21 | Williams International Corporation | Compliant foil bearing |
| US5307622A (en) * | 1993-08-02 | 1994-05-03 | General Electric Company | Counterrotating turbine support assembly |
| US6286303B1 (en) * | 1999-11-18 | 2001-09-11 | Allied Signal, Inc. | Impingement cooled foil bearings in a gas turbine engine |
| US6619030B1 (en) * | 2002-03-01 | 2003-09-16 | General Electric Company | Aircraft engine with inter-turbine engine frame supported counter rotating low pressure turbine rotors |
| US6725643B1 (en) * | 2001-06-19 | 2004-04-27 | Marius Paul | High efficiency gas turbine power generator systems |
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|---|---|---|---|---|
| US3861139A (en) * | 1973-02-12 | 1975-01-21 | Gen Electric | Turbofan engine having counterrotating compressor and turbine elements and unique fan disposition |
| US5450719A (en) * | 1993-11-17 | 1995-09-19 | Alliedsignal, Inc. | Gas turbine engine rear magnetic or foil bearing cooling using exhaust eductor |
| US5806303A (en) * | 1996-03-29 | 1998-09-15 | General Electric Company | Turbofan engine with a core driven supercharged bypass duct and fixed geometry nozzle |
| US5809772A (en) * | 1996-03-29 | 1998-09-22 | General Electric Company | Turbofan engine with a core driven supercharged bypass duct |
| US5867980A (en) * | 1996-12-17 | 1999-02-09 | General Electric Company | Turbofan engine with a low pressure turbine driven supercharger in a bypass duct operated by a fuel rich combustor and an afterburner |
| US5813214A (en) * | 1997-01-03 | 1998-09-29 | General Electric Company | Bearing lubrication configuration in a turbine engine |
| FR2759734B1 (fr) * | 1997-02-20 | 1999-04-09 | Snecma | Turbomachine a systeme de compression optimise |
| US20020067872A1 (en) | 2000-12-01 | 2002-06-06 | Capstone Turbine Corporation | Hydrodynamic compliant foil thrust bearing |
| US6732502B2 (en) * | 2002-03-01 | 2004-05-11 | General Electric Company | Counter rotating aircraft gas turbine engine with high overall pressure ratio compressor |
| US6739120B2 (en) * | 2002-04-29 | 2004-05-25 | General Electric Company | Counterrotatable booster compressor assembly for a gas turbine engine |
| US6684626B1 (en) * | 2002-07-30 | 2004-02-03 | General Electric Company | Aircraft gas turbine engine with control vanes for counter rotating low pressure turbines |
| US6711887B2 (en) * | 2002-08-19 | 2004-03-30 | General Electric Co. | Aircraft gas turbine engine with tandem non-interdigitated counter rotating low pressure turbines |
| JP2004084877A (ja) * | 2002-08-28 | 2004-03-18 | Honda Motor Co Ltd | フォイル軸受け |
| US6763653B2 (en) * | 2002-09-24 | 2004-07-20 | General Electric Company | Counter rotating fan aircraft gas turbine engine with aft booster |
| US6763652B2 (en) | 2002-09-24 | 2004-07-20 | General Electric Company | Variable torque split aircraft gas turbine engine counter rotating low pressure turbines |
| US6763654B2 (en) * | 2002-09-30 | 2004-07-20 | General Electric Co. | Aircraft gas turbine engine having variable torque split counter rotating low pressure turbines and booster aft of counter rotating fans |
-
2004
- 2004-10-29 US US10/976,496 patent/US7195446B2/en not_active Expired - Lifetime
-
2005
- 2005-08-25 DE DE602005003759T patent/DE602005003759T2/de not_active Expired - Lifetime
- 2005-08-25 EP EP05255228A patent/EP1655475B1/en not_active Ceased
- 2005-08-26 JP JP2005245340A patent/JP4693551B2/ja not_active Expired - Lifetime
- 2005-08-29 CN CN200510097640XA patent/CN1854486B/zh not_active Expired - Fee Related
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4950089A (en) * | 1988-05-12 | 1990-08-21 | Williams International Corporation | Compliant foil bearing |
| US5307622A (en) * | 1993-08-02 | 1994-05-03 | General Electric Company | Counterrotating turbine support assembly |
| US6286303B1 (en) * | 1999-11-18 | 2001-09-11 | Allied Signal, Inc. | Impingement cooled foil bearings in a gas turbine engine |
| US6725643B1 (en) * | 2001-06-19 | 2004-04-27 | Marius Paul | High efficiency gas turbine power generator systems |
| US6619030B1 (en) * | 2002-03-01 | 2003-09-16 | General Electric Company | Aircraft engine with inter-turbine engine frame supported counter rotating low pressure turbine rotors |
Also Published As
| Publication number | Publication date |
|---|---|
| EP1655475A1 (en) | 2006-05-10 |
| DE602005003759D1 (de) | 2008-01-24 |
| JP4693551B2 (ja) | 2011-06-01 |
| CN1854486A (zh) | 2006-11-01 |
| US7195446B2 (en) | 2007-03-27 |
| DE602005003759T2 (de) | 2008-12-04 |
| US20060093466A1 (en) | 2006-05-04 |
| EP1655475B1 (en) | 2007-12-12 |
| JP2006125387A (ja) | 2006-05-18 |
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