PT2871050T - Elemento de preenchimento de raios, compósito, laminado com elemento de preenchimento de forma geométrica e método de formação do mesmo - Google Patents
Elemento de preenchimento de raios, compósito, laminado com elemento de preenchimento de forma geométrica e método de formação do mesmoInfo
- Publication number
- PT2871050T PT2871050T PT141872416T PT14187241T PT2871050T PT 2871050 T PT2871050 T PT 2871050T PT 141872416 T PT141872416 T PT 141872416T PT 14187241 T PT14187241 T PT 14187241T PT 2871050 T PT2871050 T PT 2871050T
- Authority
- PT
- Portugal
- Prior art keywords
- forming
- same
- filler
- laminated composite
- geometric shaped
- Prior art date
Links
- 239000000945 filler Substances 0.000 title 2
- 239000002131 composite material 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
- B29C70/50—Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC]
- B29C70/52—Pultrusion, i.e. forming and compressing by continuously pulling through a die
-
- 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
- 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
- B29D99/0005—Producing noodles, i.e. composite gap fillers, characterised by their construction
-
- 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
- B29C70/543—Fixing the position or configuration of fibrous reinforcements before or during moulding
-
- 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
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
- B32B3/26—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer
- B32B3/266—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer characterised by an apertured layer, the apertures going through the whole thickness of the layer, e.g. expanded metal, perforated layer, slit layer regular cells B32B3/12
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
- B32B3/26—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer
- B32B3/28—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer characterised by a layer comprising a deformed thin sheet, i.e. the layer having its entire thickness deformed out of the plane, e.g. corrugated, crumpled
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B38/00—Ancillary operations in connection with laminating processes
- B32B38/0012—Mechanical treatment, e.g. roughening, deforming, stretching
-
- 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
- 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
- B64C1/12—Construction or attachment of skin panels
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/24—Moulded or cast structures
-
- 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
- B29C53/00—Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
- B29C53/14—Twisting
-
- 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
- B29L2031/3076—Aircrafts
- B29L2031/3082—Fuselages
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
- B32B5/10—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer characterised by a fibrous or filamentary layer reinforced with filaments
-
- 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
-
- 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
-
- 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
- Y10T156/1002—Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining 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
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24273—Structurally defined web or sheet [e.g., overall dimension, etc.] including aperture
- Y10T428/24298—Noncircular aperture [e.g., slit, diamond, rectangular, etc.]
- Y10T428/24314—Slit or elongated
-
- 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
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24479—Structurally defined web or sheet [e.g., overall dimension, etc.] including variation in thickness
- Y10T428/24521—Structurally defined web or sheet [e.g., overall dimension, etc.] including variation in thickness with component conforming to contour of nonplanar surface
- Y10T428/24529—Structurally defined web or sheet [e.g., overall dimension, etc.] including variation in thickness with component conforming to contour of nonplanar surface and conforming component on an opposite nonplanar surface
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Textile Engineering (AREA)
- Laminated Bodies (AREA)
- Moulding By Coating Moulds (AREA)
- Woven Fabrics (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US14/074,692 US9359060B2 (en) | 2013-11-07 | 2013-11-07 | Laminated composite radius filler with geometric shaped filler element and method of forming the same |
Publications (1)
Publication Number | Publication Date |
---|---|
PT2871050T true PT2871050T (pt) | 2017-04-05 |
Family
ID=51690823
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PT141872416T PT2871050T (pt) | 2013-11-07 | 2014-10-01 | Elemento de preenchimento de raios, compósito, laminado com elemento de preenchimento de forma geométrica e método de formação do mesmo |
Country Status (11)
Country | Link |
---|---|
US (1) | US9359060B2 (pt) |
EP (1) | EP2871050B1 (pt) |
JP (1) | JP6505997B2 (pt) |
KR (1) | KR101999577B1 (pt) |
CN (1) | CN104786525B (pt) |
AU (1) | AU2014203585B2 (pt) |
BR (1) | BR102014021244B1 (pt) |
CA (1) | CA2857783C (pt) |
ES (1) | ES2622357T3 (pt) |
PT (1) | PT2871050T (pt) |
RU (1) | RU2664524C9 (pt) |
Families Citing this family (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9566739B2 (en) | 2014-02-18 | 2017-02-14 | The Boeing Company | Composite filler |
US9475256B2 (en) * | 2014-07-10 | 2016-10-25 | The Boeing Company | Composite filler |
KR101722323B1 (ko) * | 2015-07-29 | 2017-03-31 | 경상대학교산학협력단 | 복합재료 성형용 필러 및 이를 이용한 복합재료 |
US9808988B2 (en) * | 2015-11-30 | 2017-11-07 | The Boeing Company | Carbon fiber reinforced plastic (CFRP) stringer termination softening with stacked CFRP noodle |
US10329030B2 (en) * | 2016-03-04 | 2019-06-25 | The Boeing Company | Conductive radius filler system and method |
US10046525B2 (en) | 2016-09-30 | 2018-08-14 | The Boeing Company | Advanced variable radius laminated composite radius filler |
DE102017102552A1 (de) * | 2017-02-09 | 2018-08-09 | CG Rail - Chinesisch-Deutsches Forschungs- und Entwicklungszentrum für Bahn- und Verkehrstechnik Dresden GmbH | Wagenkasten für ein Schienenfahrzeug |
RU2665001C1 (ru) * | 2017-03-06 | 2018-08-24 | Геннадий Алексеевич Павлов | Конструкционный материал, способ его изготовления и способ изготовления композиционного материала заполнителя трёхслойной оболочки несущей корпусной конструкции |
US10703053B2 (en) * | 2017-07-06 | 2020-07-07 | The Boeing Company | Method and system for manufacturing noodles of structural joints |
CN111051691A (zh) * | 2017-07-27 | 2020-04-21 | 维斯塔斯风力系统有限公司 | 抗剪腹板的腹板脚 |
US10723436B2 (en) * | 2017-08-14 | 2020-07-28 | The Boeing Company | Methods and apparatus to increase strength and toughness of aircraft structural components |
US10689085B2 (en) | 2017-08-14 | 2020-06-23 | The Boeing Company | Stringer stiffened composite panels having improved pull-off strength |
US10800128B2 (en) | 2018-01-24 | 2020-10-13 | General Electric Company | Composite components having T or L-joints and methods for forming same |
US11180238B2 (en) * | 2018-11-19 | 2021-11-23 | The Boeing Company | Shear ties for aircraft wing |
JP7249404B2 (ja) * | 2019-03-29 | 2023-03-30 | 川崎重工業株式会社 | 複合材料製パネル構造体およびその製造方法 |
JP2022528796A (ja) * | 2019-04-18 | 2022-06-15 | テイジン カーボン ユーロップ ゲー・エム・ベー・ハー | 楔状フィラープリフォーム |
US11420733B2 (en) | 2020-04-27 | 2022-08-23 | Textron Innovations Inc. | Additively manufactured flyaway tools for aircraft |
KR20210153312A (ko) | 2020-06-10 | 2021-12-17 | 한국항공우주산업 주식회사 | 복합소재 강화패널 제조 장치 및 제조 방법 |
US20240308159A1 (en) * | 2023-03-17 | 2024-09-19 | Spirit Aerosystems, Inc. | Composite parts, and methods of manufacturing |
Family Cites Families (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4238214A (en) * | 1975-03-25 | 1980-12-09 | Ashbee Kenneth H | Particle orientation method |
US4331723A (en) | 1980-11-05 | 1982-05-25 | The Boeing Company | Advanced composite |
JPH0436905Y2 (pt) * | 1987-02-03 | 1992-08-31 | ||
US4789594A (en) | 1987-04-15 | 1988-12-06 | The Boeing Company | Method of forming composite radius fillers |
JPH0790605B2 (ja) * | 1987-09-16 | 1995-10-04 | 三菱重工業株式会社 | 複合材製桁材のジョイント部補強用繊維構造体およびその製造方法 |
WO1993023236A1 (en) * | 1992-05-12 | 1993-11-25 | American Standard Inc. | Polyester backed acrylic composite molded structure and method of manufacturing thereof |
US5833786A (en) | 1996-05-16 | 1998-11-10 | The Boeing Company | Titanium radius filler for use in composite interfaces |
US5639535A (en) * | 1996-06-06 | 1997-06-17 | The Boeing Company | Composite interleaving for composite interfaces |
AU2001262912A1 (en) | 2000-02-25 | 2001-09-03 | The Boeing Company | Laminated composite radius filler |
US7531058B2 (en) | 2005-02-24 | 2009-05-12 | The Boeing Company | Reinforced rampdown for composite structural member and method for same |
US7823490B2 (en) | 2006-10-04 | 2010-11-02 | The Boeing Company | Cutting sequence for net trimming a composite layup at an oblique angle |
DE102007018052A1 (de) * | 2007-04-17 | 2008-10-23 | Airbus Deutschland Gmbh | Pultrusionsverfahren zur Herstellung eines endlosen Profils |
US7874829B2 (en) | 2007-11-09 | 2011-01-25 | Spirit Aerosystems, Inc. | Method and apparatus for forming adhesive strips |
US8216499B2 (en) | 2008-12-09 | 2012-07-10 | The Boeing Company | Extrusion of adhesives for composite structures |
GB201005308D0 (en) * | 2010-03-30 | 2010-05-12 | Airbus Operations Ltd | Composite structural member |
US8776375B2 (en) | 2011-05-19 | 2014-07-15 | The Boeing Company | Aircraft structure for high capacity pull off |
-
2013
- 2013-11-07 US US14/074,692 patent/US9359060B2/en active Active
-
2014
- 2014-06-30 AU AU2014203585A patent/AU2014203585B2/en active Active
- 2014-07-01 RU RU2014126644A patent/RU2664524C9/ru active
- 2014-07-24 KR KR1020140093867A patent/KR101999577B1/ko active IP Right Grant
- 2014-07-24 CA CA2857783A patent/CA2857783C/en active Active
- 2014-08-27 BR BR102014021244-2A patent/BR102014021244B1/pt active IP Right Grant
- 2014-08-29 JP JP2014175086A patent/JP6505997B2/ja active Active
- 2014-10-01 PT PT141872416T patent/PT2871050T/pt unknown
- 2014-10-01 EP EP14187241.6A patent/EP2871050B1/en active Active
- 2014-10-01 ES ES14187241.6T patent/ES2622357T3/es active Active
- 2014-10-31 CN CN201410602457.XA patent/CN104786525B/zh active Active
Also Published As
Publication number | Publication date |
---|---|
US9359060B2 (en) | 2016-06-07 |
BR102014021244A2 (pt) | 2016-09-27 |
EP2871050A1 (en) | 2015-05-13 |
RU2664524C9 (ru) | 2019-01-11 |
CN104786525A (zh) | 2015-07-22 |
BR102014021244B1 (pt) | 2020-08-04 |
AU2014203585B2 (en) | 2017-07-27 |
JP2015098166A (ja) | 2015-05-28 |
ES2622357T3 (es) | 2017-07-06 |
KR20150053222A (ko) | 2015-05-15 |
RU2664524C2 (ru) | 2018-08-20 |
RU2014126644A (ru) | 2016-01-27 |
US20150125655A1 (en) | 2015-05-07 |
CA2857783A1 (en) | 2015-05-07 |
CN104786525B (zh) | 2017-10-24 |
JP6505997B2 (ja) | 2019-04-24 |
EP2871050B1 (en) | 2017-01-11 |
AU2014203585A1 (en) | 2015-05-21 |
CA2857783C (en) | 2016-11-22 |
KR101999577B1 (ko) | 2019-10-01 |
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