ATE456445T1 - Vorrichtung und verfahren zur herstellung von gekrümmten tragelementen aus verbundwerkstoff - Google Patents
Vorrichtung und verfahren zur herstellung von gekrümmten tragelementen aus verbundwerkstoffInfo
- Publication number
- ATE456445T1 ATE456445T1 AT06787029T AT06787029T ATE456445T1 AT E456445 T1 ATE456445 T1 AT E456445T1 AT 06787029 T AT06787029 T AT 06787029T AT 06787029 T AT06787029 T AT 06787029T AT E456445 T1 ATE456445 T1 AT E456445T1
- Authority
- AT
- Austria
- Prior art keywords
- web
- composite material
- support elements
- curved support
- compaction roller
- Prior art date
Links
- 239000002131 composite material Substances 0.000 title abstract 4
- 238000004519 manufacturing process Methods 0.000 title 1
- 238000005056 compaction Methods 0.000 abstract 3
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
- B29C70/34—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
- B29C70/38—Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
- B29C70/38—Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
- B29C70/382—Automated fiber placement [AFP]
- B29C70/384—Fiber placement heads, e.g. component parts, details or accessories
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
- B29D99/00—Subject matter not provided for in other groups of this subclass
- B29D99/0003—Producing profiled members, e.g. beams
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
- B29C70/545—Perforating, cutting or machining during or after moulding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/001—Profiled members, e.g. beams, sections
- B29L2031/003—Profiled members, e.g. beams, sections having a profiled transverse cross-section
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
- Y10T156/10—Methods of surface bonding and/or assembly therefor
- Y10T156/1089—Methods of surface bonding and/or assembly therefor of discrete laminae to single face of additional lamina
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
- Y10T156/17—Surface bonding means and/or assemblymeans with work feeding or handling means
- Y10T156/1788—Work traversing type and/or means applying work to wall or static structure
- Y10T156/1795—Implement carried web supply
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Robotics (AREA)
- Moulding By Coating Moulds (AREA)
- Rod-Shaped Construction Members (AREA)
- Aerials With Secondary Devices (AREA)
- Bending Of Plates, Rods, And Pipes (AREA)
- Treatment Of Fiber Materials (AREA)
- Enzymes And Modification Thereof (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US11/195,786 US7469735B2 (en) | 2005-08-03 | 2005-08-03 | Composite structural element fabricating device and method |
| PCT/US2006/027067 WO2007018935A1 (en) | 2005-08-03 | 2006-07-11 | Curved composite structural element fabricating device and method |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ATE456445T1 true ATE456445T1 (de) | 2010-02-15 |
Family
ID=37098596
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AT06787029T ATE456445T1 (de) | 2005-08-03 | 2006-07-11 | Vorrichtung und verfahren zur herstellung von gekrümmten tragelementen aus verbundwerkstoff |
Country Status (9)
| Country | Link |
|---|---|
| US (1) | US7469735B2 (de) |
| EP (1) | EP1910062B1 (de) |
| JP (1) | JP4987002B2 (de) |
| KR (1) | KR100945565B1 (de) |
| CN (1) | CN101277809B (de) |
| AT (1) | ATE456445T1 (de) |
| DE (1) | DE602006012055D1 (de) |
| ES (1) | ES2339878T3 (de) |
| WO (1) | WO2007018935A1 (de) |
Families Citing this family (67)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7249943B2 (en) | 2003-08-01 | 2007-07-31 | Alliant Techsystems Inc. | Apparatus for forming composite stiffeners and reinforcing structures |
| US8632653B2 (en) * | 2005-05-03 | 2014-01-21 | The Boeing Company | Method of manufacturing curved composite structural elements |
| US7943076B1 (en) * | 2005-05-03 | 2011-05-17 | The Boeing Company | Method of manufacturing curved composite structural elements |
| ES2357841T3 (es) * | 2005-10-17 | 2011-05-03 | Saab Ab | Procedimiento de fabricación para un objeto curvado de material compuesto y objeto curvado así obtenido. |
| US8449709B2 (en) | 2007-05-25 | 2013-05-28 | The Boeing Company | Method of fabricating fiber reinforced composite structure having stepped surface |
| GB0712549D0 (en) * | 2007-06-29 | 2007-08-08 | Airbus Uk Ltd | Improvements in elongate composite structural members |
| GB0712553D0 (en) * | 2007-06-29 | 2007-08-08 | Airbus Uk Ltd | Composite panel stiffener |
| GB0712552D0 (en) * | 2007-06-29 | 2007-08-08 | Airbus Uk Ltd | Elongate composite structural members and improvements therein |
| ITTO20070557A1 (it) * | 2007-07-27 | 2009-01-28 | Alenia Aeronautica Spa | Procedimento di fabbricazione di un elemento curvo in materiale composito |
| US7897239B2 (en) * | 2007-11-01 | 2011-03-01 | Lockheed Martin Corporation | Highly tailored stiffening for advanced composites |
| US7591294B2 (en) | 2007-11-29 | 2009-09-22 | Spirit Aerosystems, Inc. | Material placement method and apparatus |
| US7717151B2 (en) * | 2007-11-29 | 2010-05-18 | Spirit Aerosystems, Inc. | Material placement method and apparatus |
| US8152948B2 (en) * | 2008-01-09 | 2012-04-10 | The Boeing Company | Contoured composite parts |
| CN101910493B (zh) * | 2008-01-11 | 2013-07-24 | 东丽株式会社 | 弯曲形状强化纤维基材、及使用其的层合体、预成型体、纤维强化树脂复合材料和它们的制造方法 |
| US8088317B1 (en) | 2008-03-03 | 2012-01-03 | Abe Karem | Partially automated fabrication of composite parts |
| US7858012B2 (en) * | 2008-03-03 | 2010-12-28 | Abe Karem | Automated prototyping of a composite airframe |
| FR2928294B1 (fr) * | 2008-03-07 | 2016-12-30 | Duqueine Rhone Alpes | Procede et dispositif de realisation d'un profil courbe en materiau composite,et profil correspondant. |
| WO2009112694A2 (fr) * | 2008-03-07 | 2009-09-17 | Airbus France | Piece structurale courbe en materiau composite et procede de fabrication d'une telle piece |
| FR2928295B1 (fr) * | 2008-03-07 | 2017-12-08 | Duqueine Rhone Alpes | Procede et dispositif de moulage d'une piece courbe en materiau composite,et piece correspondante. |
| US9090028B2 (en) * | 2008-04-17 | 2015-07-28 | The Boeing Company | Method for producing contoured composite structures and structures produced thereby |
| US9278484B2 (en) * | 2008-04-17 | 2016-03-08 | The Boeing Company | Method and apparatus for producing contoured composite structures and structures produced thereby |
| US8932423B2 (en) * | 2008-04-17 | 2015-01-13 | The Boeing Company | Method for producing contoured composite structures and structures produced thereby |
| US8349105B2 (en) * | 2008-04-17 | 2013-01-08 | The Boeing Company | Curved composite frames and method of making the same |
| US8540833B2 (en) * | 2008-05-16 | 2013-09-24 | The Boeing Company | Reinforced stiffeners and method for making the same |
| DE102008028865B4 (de) * | 2008-06-19 | 2015-04-02 | Airbus Defence and Space GmbH | Verfahren zur Herstellung von Faserverbund-Profilbauteilen, sowie Verwendung derartig hergestellter Faserverbund-Profilbauteile |
| GB0813146D0 (en) * | 2008-07-18 | 2008-08-27 | Airbus Uk Ltd | Ramped stiffener and apparatus and method for forming the same |
| GB0813161D0 (en) * | 2008-07-18 | 2008-08-27 | Airbus Uk Ltd | Ramped stiffener and apparatus and method for forming the same |
| FR2934198B1 (fr) * | 2008-07-24 | 2012-12-21 | Eads Europ Aeronautic Defence | Pli et procede de metallisation d'une piece en materiau composite. |
| WO2010056164A1 (en) * | 2008-11-13 | 2010-05-20 | Saab Ab | Method of forming a composite article |
| WO2010087443A1 (ja) * | 2009-02-02 | 2010-08-05 | 東レ株式会社 | 円弧状部を有する帯状強化繊維基材の製造方法および製造装置、およびその基材を用いた積層体、プリフォームおよび繊維強化樹脂複合材料 |
| IT1395892B1 (it) * | 2009-09-15 | 2012-10-26 | Alenia Aeronautica Spa | Procedimento per la fabbricazione di un'ordinata di fusoliera in materiale composito |
| US8282757B2 (en) | 2009-11-10 | 2012-10-09 | Alliant Techsystems Inc. | Automated composite annular structure forming |
| US9662841B2 (en) * | 2009-11-10 | 2017-05-30 | Orbital Atk, Inc. | Radially extending composite structures |
| DE102010013713A1 (de) | 2010-04-02 | 2011-10-06 | Airbus Operations Gmbh | Verfahren und Vorrichtung zur Herstellung eines faserverstärkten thermoplastischen Verbundbauteils |
| US9266279B2 (en) | 2010-07-08 | 2016-02-23 | Orbital Atk, Inc. | Variable material stretch-forming apparatus and methods |
| US8795567B2 (en) | 2010-09-23 | 2014-08-05 | The Boeing Company | Method for fabricating highly contoured composite stiffeners with reduced wrinkling |
| US9387657B2 (en) | 2010-11-12 | 2016-07-12 | The Boeing Company | Method of fabricating a curved composite structure using composite prepreg tape |
| US8551380B2 (en) | 2010-11-12 | 2013-10-08 | The Boeing Company | Method of laying up prepreg plies on contoured tools using a deformable carrier film |
| US9701067B2 (en) | 2010-11-12 | 2017-07-11 | The Boeing Company | Method of laying up prepreg plies on contoured tools using a deformable carrier film |
| US9604417B2 (en) | 2011-04-05 | 2017-03-28 | The Boeing Company | Method for making contoured composite stiffeners |
| US9180960B2 (en) | 2011-06-10 | 2015-11-10 | The Boeing Company | Boron fiber reinforced structural components |
| US8900391B2 (en) | 2011-06-26 | 2014-12-02 | The Boeing Company | Automated resin and fiber deposition for resin infusion |
| US9308692B2 (en) * | 2011-09-28 | 2016-04-12 | The Boeing Company | Material placement system |
| US8721316B2 (en) | 2012-01-26 | 2014-05-13 | Alliant Techsystems Inc. | Automated material delivery system |
| FR2989619B1 (fr) * | 2012-04-23 | 2014-06-13 | Airbus Operations Sas | Procede de realisation d'un profile courbe en materiau composite a partir d'une preforme rectiligne de nappes de fibres |
| US8826957B2 (en) * | 2012-08-31 | 2014-09-09 | General Electric Company | Methods and systems for automated ply layup for composites |
| EP2808158A1 (de) * | 2013-05-31 | 2014-12-03 | Siemens Aktiengesellschaft | Verfahren und Vorrichtug zum Verlegen eines Fasermaterials auf einer Formoberfläche |
| DE102013017450A1 (de) * | 2013-10-22 | 2015-04-23 | Airbus Defence and Space GmbH | Verfahren zur Herstellung von Faserverbund-Halbzeugen |
| CN103692663B (zh) * | 2013-12-30 | 2015-09-23 | 中国科学院自动化研究所 | 一种对纤维丝束进行重送剪切导向压紧的方法 |
| US9579875B2 (en) | 2014-02-04 | 2017-02-28 | The Boeing Company | Bonded tab and tooling device |
| US10112349B2 (en) * | 2014-03-20 | 2018-10-30 | The Boeing Company | Placement of prepreg tows in high angle transition regions |
| WO2016018194A1 (en) * | 2014-08-01 | 2016-02-04 | Gök Gökhan Vargin | Fiber placement head having double roller system and a fiber placement head application method |
| US9545759B2 (en) * | 2015-01-30 | 2017-01-17 | CGTech | Automated fiber placement with course trajectory compensation |
| EP3597412B1 (de) * | 2017-03-17 | 2022-10-05 | Subaru Corporation | Formvorrichtung für fasermaterial und formverfahren für fasermaterial |
| WO2018181983A1 (ja) * | 2017-03-31 | 2018-10-04 | 三菱ケミカル株式会社 | プリプレグシート、その製造方法、表皮材付き単位層、繊維強化複合材料成形品の製造方法、及び繊維強化複合材料成形品 |
| EP3581306A1 (de) * | 2018-06-12 | 2019-12-18 | Siemens Gamesa Renewable Energy A/S | Führungswerkzeug für eine oberflächenschneidevorrichtung und schneideanordnung |
| JPWO2020067478A1 (ja) * | 2018-09-27 | 2021-08-30 | 三菱ケミカル株式会社 | テーププリプレグ、テーププリプレグの配置方法、繊維強化複合材料及び繊維強化複合材料の製造方法 |
| US11305498B2 (en) | 2018-12-21 | 2022-04-19 | The Boeing Company | System and method for fabricating a composite ply layup |
| US11318689B2 (en) | 2018-12-21 | 2022-05-03 | The Boeing Company | Ply transporting and compacting apparatus and method therefor |
| CN111203996B (zh) * | 2019-12-13 | 2022-04-19 | 中国航空工业集团公司基础技术研究院 | 一种带有弯折截面预制体的制备设备及方法 |
| WO2021171529A1 (ja) * | 2020-02-28 | 2021-09-02 | 三菱重工業株式会社 | 積層体および積層方法 |
| EP4000909A1 (de) * | 2020-11-18 | 2022-05-25 | The Boeing Company | Rahmenfertigungslinie |
| US11845566B2 (en) | 2020-11-18 | 2023-12-19 | The Boeing Company | Frame fabrication line |
| NL2027395B1 (en) * | 2021-01-26 | 2022-08-12 | Boeing Co | Frame fabrication line |
| US11577814B2 (en) | 2020-12-18 | 2023-02-14 | The Boeing Company | Composite structure and method of forming |
| US12553352B2 (en) * | 2024-03-20 | 2026-02-17 | General Electric Company | Method and system of forming a composite airfoil having a set of plies |
| FR3161594A1 (fr) * | 2024-04-25 | 2025-10-31 | Airbus | Système d’application de ruban de préimprégné pour recouvrir un bord de composite. |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| US3259021A (en) | 1961-05-05 | 1966-07-05 | North American Aviation Inc | Multiple purpose fabrication apparatus and method |
| JPS5839845U (ja) * | 1981-09-11 | 1983-03-16 | 東芝機械株式会社 | テ−プ自動貼付装置 |
| US4726924A (en) * | 1984-06-28 | 1988-02-23 | The Boeing Company | Method of planar forming of zero degree composite tape |
| US4720255A (en) * | 1984-06-28 | 1988-01-19 | The Boeing Company | Apparatus for planar forming of zero degree composite tape |
| FR2590069B1 (fr) * | 1985-11-14 | 1987-12-11 | Alsthom | Enrubanneuse pour l'enrubannage a chaud d'un conducteur electrique |
| US4867834A (en) | 1986-04-07 | 1989-09-19 | Hercules | Filament winding system |
| JPH0639133B2 (ja) * | 1990-06-27 | 1994-05-25 | 川崎重工業株式会社 | ロービング材自動積層装置 |
| JPH0483713U (de) * | 1990-11-30 | 1992-07-21 | ||
| JP2501497B2 (ja) * | 1991-08-27 | 1996-05-29 | 川崎重工業株式会社 | ロ―ビング材積層装置 |
| JP2001521839A (ja) * | 1997-11-05 | 2001-11-13 | シコルスキー エアクラフト コーポレイション | 繊維配置装置の供給制御システム |
| JP3999031B2 (ja) * | 2002-04-26 | 2007-10-31 | 東京特殊電線株式会社 | 角形断面マグネットワイヤの製造方法 |
| US7249943B2 (en) * | 2003-08-01 | 2007-07-31 | Alliant Techsystems Inc. | Apparatus for forming composite stiffeners and reinforcing structures |
| JP3742082B2 (ja) * | 2003-08-08 | 2006-02-01 | 株式会社ジャムコ | 曲率を有した繊維強化プラスチック部材の連続成形方法及び装置 |
| US7134629B2 (en) | 2004-04-06 | 2006-11-14 | The Boeing Company | Structural panels for use in aircraft fuselages and other structures |
-
2005
- 2005-08-03 US US11/195,786 patent/US7469735B2/en active Active
-
2006
- 2006-07-11 WO PCT/US2006/027067 patent/WO2007018935A1/en not_active Ceased
- 2006-07-11 AT AT06787029T patent/ATE456445T1/de not_active IP Right Cessation
- 2006-07-11 DE DE602006012055T patent/DE602006012055D1/de active Active
- 2006-07-11 CN CN2006800369058A patent/CN101277809B/zh not_active Expired - Fee Related
- 2006-07-11 ES ES06787029T patent/ES2339878T3/es active Active
- 2006-07-11 EP EP06787029A patent/EP1910062B1/de not_active Not-in-force
- 2006-07-11 KR KR1020087002950A patent/KR100945565B1/ko active Active
- 2006-07-11 JP JP2008524977A patent/JP4987002B2/ja not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| KR20080031942A (ko) | 2008-04-11 |
| EP1910062A1 (de) | 2008-04-16 |
| ES2339878T3 (es) | 2010-05-26 |
| KR100945565B1 (ko) | 2010-03-08 |
| WO2007018935A1 (en) | 2007-02-15 |
| JP2009502585A (ja) | 2009-01-29 |
| HK1109601A1 (en) | 2008-06-13 |
| US20070029038A1 (en) | 2007-02-08 |
| JP4987002B2 (ja) | 2012-07-25 |
| US7469735B2 (en) | 2008-12-30 |
| EP1910062B1 (de) | 2010-01-27 |
| CN101277809B (zh) | 2010-09-29 |
| DE602006012055D1 (de) | 2010-03-18 |
| CN101277809A (zh) | 2008-10-01 |
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