PT2585287E - Estruturas compósitas que têm endurecedores integrados e método para o seu fabrico - Google Patents
Estruturas compósitas que têm endurecedores integrados e método para o seu fabrico Download PDFInfo
- Publication number
- PT2585287E PT2585287E PT117219055T PT11721905T PT2585287E PT 2585287 E PT2585287 E PT 2585287E PT 117219055 T PT117219055 T PT 117219055T PT 11721905 T PT11721905 T PT 11721905T PT 2585287 E PT2585287 E PT 2585287E
- Authority
- PT
- Portugal
- Prior art keywords
- making
- same
- composite structures
- integrated stiffeners
- stiffeners
- Prior art date
Links
- 239000002131 composite material Substances 0.000 title 1
- 238000004519 manufacturing process Methods 0.000 title 1
- 239000003351 stiffener Substances 0.000 title 1
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
- B29C70/40—Shaping or impregnating by compression not applied
-
- 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
- B29D99/001—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings
- B29D99/0014—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings provided with ridges or ribs, e.g. joined ribs
- B29D99/0017—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings provided with ridges or ribs, e.g. joined ribs with filled hollow ridges
-
- 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
- B29C35/00—Heating, cooling or curing, e.g. crosslinking or vulcanising; Apparatus therefor
- B29C35/02—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould
- B29C35/0288—Controlling heating or curing of polymers during moulding, e.g. by measuring temperatures or properties of the polymer and regulating the process
-
- 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
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
- B29C66/721—Fibre-reinforced materials
-
- 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
- B29C70/40—Shaping or impregnating by compression not applied
- B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
- B29C70/44—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
- B29C70/443—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding and impregnating by vacuum or injection
-
- 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
- B29C70/68—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
- B29C70/86—Incorporated in coherent impregnated reinforcing layers, e.g. by winding
- B29C70/865—Incorporated in coherent impregnated reinforcing layers, e.g. by winding completely encapsulated
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/064—Stringers; Longerons
-
- 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
- B29C35/00—Heating, cooling or curing, e.g. crosslinking or vulcanising; Apparatus therefor
- B29C35/02—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould
-
- 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
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/78—Means for handling the parts to be joined, e.g. for making containers or hollow articles, e.g. means for handling sheets, plates, web-like materials, tubular articles, hollow articles or elements to be joined therewith; Means for discharging the joined articles from the joining apparatus
- B29C65/7841—Holding or clamping means for handling purposes
-
- 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
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/301—Three-dimensional joints, i.e. the joined area being substantially non-flat
-
- 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
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/40—General aspects of joining substantially flat articles, e.g. plates, sheets or web-like materials; Making flat seams in tubular or hollow articles; Joining single elements to substantially flat surfaces
- B29C66/47—Joining single elements to sheets, plates or other substantially flat surfaces
- B29C66/474—Joining single elements to sheets, plates or other substantially flat surfaces said single elements being substantially non-flat
-
- 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
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/50—General aspects of joining tubular articles; General aspects of joining long products, i.e. bars or profiled elements; General aspects of joining single elements to tubular articles, hollow articles or bars; General aspects of joining several hollow-preforms to form hollow or tubular articles
- B29C66/51—Joining tubular articles, profiled elements or bars; Joining single elements to tubular articles, hollow articles or bars; Joining several hollow-preforms to form hollow or tubular articles
- B29C66/52—Joining tubular articles, bars or profiled elements
- B29C66/524—Joining profiled elements
-
- 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
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/80—General aspects of machine operations or constructions and parts thereof
- B29C66/81—General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps
- B29C66/814—General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the design of the pressing elements, e.g. of the welding jaws or clamps
- B29C66/8145—General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the design of the pressing elements, e.g. of the welding jaws or clamps characterised by the constructional aspects of the pressing elements, e.g. of the welding jaws or clamps
- B29C66/81455—General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the design of the pressing elements, e.g. of the welding jaws or clamps characterised by the constructional aspects of the pressing elements, e.g. of the welding jaws or clamps being a fluid inflatable bag or bladder, a diaphragm or a vacuum bag for applying isostatic pressure
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C2001/0054—Fuselage structures substantially made from particular materials
- B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Composite Materials (AREA)
- Chemical & Material Sciences (AREA)
- Aviation & Aerospace Engineering (AREA)
- Architecture (AREA)
- Structural Engineering (AREA)
- Civil Engineering (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Oral & Maxillofacial Surgery (AREA)
- Health & Medical Sciences (AREA)
- Moulding By Coating Moulds (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
- Compositions Of Macromolecular Compounds (AREA)
- Reinforced Plastic Materials (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US12/823,414 US8628717B2 (en) | 2010-06-25 | 2010-06-25 | Composite structures having integrated stiffeners and method of making the same |
Publications (1)
Publication Number | Publication Date |
---|---|
PT2585287E true PT2585287E (pt) | 2014-12-09 |
Family
ID=44520552
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PT117219055T PT2585287E (pt) | 2010-06-25 | 2011-05-12 | Estruturas compósitas que têm endurecedores integrados e método para o seu fabrico |
Country Status (8)
Country | Link |
---|---|
US (1) | US8628717B2 (pt) |
EP (1) | EP2585287B1 (pt) |
JP (1) | JP5801885B2 (pt) |
KR (1) | KR101837217B1 (pt) |
AU (1) | AU2011269749B2 (pt) |
ES (1) | ES2513542T3 (pt) |
PT (1) | PT2585287E (pt) |
WO (1) | WO2011162884A1 (pt) |
Families Citing this family (48)
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US9586699B1 (en) | 1999-08-16 | 2017-03-07 | Smart Drilling And Completion, Inc. | Methods and apparatus for monitoring and fixing holes in composite aircraft |
US9625361B1 (en) | 2001-08-19 | 2017-04-18 | Smart Drilling And Completion, Inc. | Methods and apparatus to prevent failures of fiber-reinforced composite materials under compressive stresses caused by fluids and gases invading microfractures in the materials |
US8636252B2 (en) | 2010-06-25 | 2014-01-28 | The Boeing Company | Composite structures having integrated stiffeners with smooth runouts and method of making the same |
US8940213B2 (en) * | 2010-06-25 | 2015-01-27 | The Boeing Company | Resin infusion of composite parts using a perforated caul sheet |
US8628717B2 (en) | 2010-06-25 | 2014-01-14 | The Boeing Company | Composite structures having integrated stiffeners and method of making the same |
US9682514B2 (en) | 2010-06-25 | 2017-06-20 | The Boeing Company | Method of manufacturing resin infused composite parts using a perforated caul sheet |
GB201020152D0 (en) * | 2010-11-29 | 2011-01-12 | Airbus Uk Ltd | Aircraft panel structure and aircraft panel structure manufacturing method for alleviation of stress |
US9957713B2 (en) * | 2011-05-11 | 2018-05-01 | Composite Technologies Corporation | Load transfer device |
SE537320C2 (sv) * | 2011-06-16 | 2015-04-07 | Bassoe Technology Ab | Borrtorn med förstyvat skal samt havsplattform |
US8651419B2 (en) | 2011-07-18 | 2014-02-18 | The Boeing Company | Flexible truss frame and method of making the same |
US8703269B2 (en) * | 2012-02-14 | 2014-04-22 | Gulfstream Aerospace Corporation | Reinforced composite structures for aircrafts and methods for making the same |
FR2990187B1 (fr) * | 2012-05-07 | 2015-01-30 | Airbus Operations Sas | Poutre en materiau composite integrant un renfort a section fermee |
US20130299073A1 (en) * | 2012-05-08 | 2013-11-14 | Lockheed Martin Corporation | Contour caul with expansion region |
US9145203B2 (en) * | 2012-10-31 | 2015-09-29 | The Boeing Company | Natural laminar flow wingtip |
ES2566168T3 (es) * | 2012-12-28 | 2016-04-11 | Airbus Operations, S.L. | Estructura aeronáutica con elementos de refuerzo integrados |
EP2989001B1 (en) * | 2013-04-25 | 2020-01-15 | Saab Ab | A method for production and an airfoil with a torsion-box type skin composite structure |
US20150142149A1 (en) * | 2013-11-15 | 2015-05-21 | Collier Research and Development Corporation | Method and computer-based tool for composite-structure fabrication design |
US10086922B2 (en) * | 2013-11-15 | 2018-10-02 | The Boeing Company | Low stress stiffener runout in Pi bonded structure |
DE102013224233A1 (de) * | 2013-11-27 | 2015-05-28 | Airbus Operations Gmbh | Druckschott für ein Flugzeug und Vorrichtung sowie Verfahren zur Herstellung eines Flugzeugstrukturbauteils |
JP6281865B2 (ja) * | 2014-01-31 | 2018-02-21 | 三菱重工業株式会社 | Frp成形治具及びfrp構造体の成形方法 |
KR102119909B1 (ko) * | 2014-03-07 | 2020-06-05 | 주식회사 포스코 | 타워모듈과, 이를 구비하는 모듈러 풍력타워 및, 풍력타워구조물 |
US10272619B2 (en) | 2014-05-19 | 2019-04-30 | The Boeing Company | Manufacture of a resin infused one-piece composite truss structure |
US10086534B2 (en) | 2014-10-17 | 2018-10-02 | The Boeing Company | Multifunctional mandrel end cap and method |
JP6501511B2 (ja) * | 2014-12-15 | 2019-04-17 | 三菱重工業株式会社 | コーナーフィレット部の設計方法及び航空機 |
US10040537B2 (en) * | 2015-01-15 | 2018-08-07 | The Boeing Company | Laminate composite wing structures |
AT516904A1 (de) * | 2015-03-05 | 2016-09-15 | Engel Austria Gmbh | Faserverbundbauteil und Verfahren zur Herstellung |
US9809297B2 (en) * | 2015-08-26 | 2017-11-07 | The Boeing Company | Structures containing stiffeners having transition portions |
US10766211B2 (en) | 2015-09-14 | 2020-09-08 | Textron Innovations Inc. | Method of forming pressure pad or other flexible element for use during cure of composite materials |
EP3205491B1 (en) * | 2016-02-09 | 2020-07-08 | Airbus Defence and Space SA | Method for manufacturing a stiffened panel made from composite material |
CN107784144A (zh) * | 2016-08-31 | 2018-03-09 | 新黎明科技股份有限公司 | 一种防爆壳体的加强筋结构以及设计方法 |
US10248158B2 (en) * | 2016-10-21 | 2019-04-02 | Microsoft Technology Licensing, Llc | Enclosure assembly and monitor device including same |
WO2018085038A1 (en) * | 2016-11-03 | 2018-05-11 | Dupont Anthony A | Isogrid stiffening elements |
US11014644B2 (en) * | 2017-10-25 | 2021-05-25 | The Boeing Company | Stiffened-cavity for modular wrap ply assembly for hat stringer |
CN108248824B (zh) * | 2017-12-29 | 2021-12-21 | 南京航空航天大学 | 一种微小型无人机翼面前缘结构、成型模具及其制备方法 |
FR3081828B1 (fr) * | 2018-06-02 | 2021-04-16 | Latecoere | Porte de cabine pressurisee d'aeronef a structure formee de poutres |
US11485468B2 (en) * | 2018-09-27 | 2022-11-01 | The Boeing Company | Thermoplastic multi-grid overmolded/co-consolidated aircraft fuselage structure |
FR3087188B1 (fr) | 2018-10-12 | 2021-05-21 | Airbus Operations Sas | Panneau structural raidi pour aeronef, presentant une conception amelioree |
KR102129997B1 (ko) | 2019-01-11 | 2020-07-03 | 한국항공우주산업 주식회사 | 응력 집중 회피를 위한 하중 전달경로 분산 패턴구조를 포함하는 패널 |
US11660830B2 (en) * | 2019-01-18 | 2023-05-30 | The Boeing Company | Contoured composite stringers |
EP3698955B1 (en) * | 2019-02-19 | 2021-10-27 | Muelles Y Ballestas Hispano-Alemanas Projects, S.L. | Stiffened panel made of composite material and method for manufacturing the said panel |
US11352124B2 (en) * | 2019-11-01 | 2022-06-07 | The Boeing Company | Continuous skin leading edge slats |
US11840362B2 (en) * | 2020-03-19 | 2023-12-12 | Mitsubishi Heavy Industries, Ltd. | Support body and support body mounting method |
US11242127B2 (en) * | 2020-04-22 | 2022-02-08 | The Boeing Company | Composite stringer assembly and methods for transmitting a load through a composite stringer assembly |
KR102343337B1 (ko) * | 2020-06-23 | 2021-12-23 | 한국항공대학교산학협력단 | 제로 포아송 비를 갖는 신축성 형상기억 폴리머 복합재 스킨 |
RU2751505C1 (ru) * | 2020-09-21 | 2021-07-14 | Федеральное государственное унитарное предприятие "Крыловский государственный научный центр" | Стыковое формованное соединение листовых элементов связей корпусных конструкций из полимерных композиционных материалов |
CN113977983B (zh) * | 2021-10-15 | 2023-06-30 | 江西洪都航空工业集团有限责任公司 | 一种复合材料壁板结构件的筋条定位装置及方法 |
GB2612957A (en) * | 2021-11-08 | 2023-05-24 | Airbus Operations Ltd | Stiffener with core and shell |
CN114248468A (zh) * | 2021-12-20 | 2022-03-29 | 山东广域科技有限责任公司 | 一种纤维增强复合材料和纤维增强复合材料的制备方法 |
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-
2010
- 2010-06-25 US US12/823,414 patent/US8628717B2/en active Active
-
2011
- 2011-05-12 ES ES11721905.5T patent/ES2513542T3/es active Active
- 2011-05-12 AU AU2011269749A patent/AU2011269749B2/en active Active
- 2011-05-12 WO PCT/US2011/036191 patent/WO2011162884A1/en active Application Filing
- 2011-05-12 KR KR1020127031079A patent/KR101837217B1/ko active IP Right Grant
- 2011-05-12 JP JP2013516576A patent/JP5801885B2/ja active Active
- 2011-05-12 PT PT117219055T patent/PT2585287E/pt unknown
- 2011-05-12 EP EP11721905.5A patent/EP2585287B1/en active Active
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Publication number | Publication date |
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AU2011269749B2 (en) | 2016-02-25 |
ES2513542T3 (es) | 2014-10-27 |
KR20130089148A (ko) | 2013-08-09 |
KR101837217B1 (ko) | 2018-04-19 |
EP2585287A1 (en) | 2013-05-01 |
WO2011162884A1 (en) | 2011-12-29 |
JP2013534478A (ja) | 2013-09-05 |
EP2585287B1 (en) | 2014-10-01 |
US8628717B2 (en) | 2014-01-14 |
US20110315824A1 (en) | 2011-12-29 |
JP5801885B2 (ja) | 2015-10-28 |
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