RU2014118504A - Состав тканей, включающий в себя эластичные волокна - Google Patents
Состав тканей, включающий в себя эластичные волокна Download PDFInfo
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- RU2014118504A RU2014118504A RU2014118504/12A RU2014118504A RU2014118504A RU 2014118504 A RU2014118504 A RU 2014118504A RU 2014118504/12 A RU2014118504/12 A RU 2014118504/12A RU 2014118504 A RU2014118504 A RU 2014118504A RU 2014118504 A RU2014118504 A RU 2014118504A
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- fabric
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- threads
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- 239000004744 fabric Substances 0.000 title claims abstract 18
- 210000004177 elastic tissue Anatomy 0.000 title 1
- 239000000835 fiber Substances 0.000 claims abstract 8
- 230000003014 reinforcing effect Effects 0.000 claims abstract 5
- 238000009941 weaving Methods 0.000 claims abstract 5
- 239000012783 reinforcing fiber Substances 0.000 claims abstract 3
- 239000011347 resin Substances 0.000 claims abstract 2
- 229920005989 resin Polymers 0.000 claims abstract 2
- 238000000034 method Methods 0.000 claims 2
- 239000002131 composite material Substances 0.000 claims 1
- 238000004519 manufacturing process Methods 0.000 claims 1
Classifications
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- 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
- B32B3/02—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 features of form at particular places, e.g. in edge regions
- B32B3/06—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 features of form at particular places, e.g. in edge regions for securing layers together; for attaching the product to another member, e.g. to a support, or to another product, e.g. groove/tongue, interlocking
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- D—TEXTILES; PAPER
- D01—NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
- D01D—MECHANICAL METHODS OR APPARATUS IN THE MANUFACTURE OF ARTIFICIAL FILAMENTS, THREADS, FIBRES, BRISTLES OR RIBBONS
- D01D5/00—Formation of filaments, threads, or the like
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- 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
- B29C37/00—Component parts, details, accessories or auxiliary operations, not covered by group B29C33/00 or B29C35/00
- B29C37/0078—Measures or configurations for obtaining anchoring effects in the contact areas between layers
- B29C37/0082—Mechanical anchoring
-
- 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
- B29C70/06—Fibrous reinforcements only
- B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
- B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
- B29C70/22—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least two directions forming a two dimensional structure
-
- 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
- B29C70/304—In-plane lamination by juxtaposing or interleaving of plies, e.g. scarf joining
-
- 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
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- 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
- B29C73/00—Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D
- B29C73/04—Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D using preformed elements
- B29C73/10—Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D using preformed elements using patches sealing on the surface of the article
-
- 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
- B32B43/00—Operations specially adapted for layered products and not otherwise provided for, e.g. repairing; Apparatus therefor
-
- 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
- B32B5/22—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 the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
- B32B5/24—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 the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
- B32B5/26—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 the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
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- 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
- B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
- B32B7/04—Interconnection of layers
- B32B7/12—Interconnection of layers using interposed adhesives or interposed materials with bonding properties
-
- 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
-
- 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
- B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
- B32B2260/02—Composition of the impregnated, bonded or embedded layer
- B32B2260/021—Fibrous or filamentary layer
-
- 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
- B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
- B32B2260/04—Impregnation, embedding, or binder material
- B32B2260/046—Synthetic resin
-
- 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
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/10—Inorganic fibres
- B32B2262/101—Glass fibres
-
- 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
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/10—Inorganic fibres
- B32B2262/106—Carbon fibres, e.g. graphite fibres
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- 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
- B32B2556/00—Patches, e.g. medical patches, repair patches
-
- 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
- B32B2605/00—Vehicles
- B32B2605/18—Aircraft
-
- 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
- B64C1/061—Frames
- B64C1/062—Frames specially adapted to absorb crash loads
-
- 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
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- 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
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/20—Patched hole or depression
-
- 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
- Y10T428/21—Circular sheet or circular blank
- Y10T428/219—Edge structure
-
- 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.]
- Y10T428/24752—Laterally noncoextensive components
- Y10T428/2476—Fabric, cloth or textile component
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Textile Engineering (AREA)
- Moulding By Coating Moulds (AREA)
- Woven Fabrics (AREA)
- Laminated Bodies (AREA)
- Reinforced Plastic Materials (AREA)
- Aviation & Aerospace Engineering (AREA)
Abstract
1. Изделие, содержащее многонаправленную ткань из первых усиливающих прядей волокна, проходящих в первом направлении, и вторых усиливающих прядей волокна, проходящих во втором направлении, причем части нитей в первых прядях волокна проходят за пределы границы ткани и являются распределенными, а пряди внедрены в смолу.2. Изделие по п. 1, в котором нити во вторых прядях также проходят за пределы границы ткани и являются распределенными.3. Изделие по п. 1, в котором нити в пределах границы ткани обеспечивают структурную прочность вдоль первого и второго направлений, причем нити, проходящие за пределы границы, обеспечивают структурную прочность в только первом направлении.4. Изделие по п. 1, в котором ткань содержит несколько рядов связанных нитей, причем распределенные нити находятся в меньшем числе рядов.5. Изделие по п. 1, в котором ткань имеет ткацкое переплетение прядей.6. Изделие по п. 5, в котором нити, проходящие за пределы границы, разрежены таким образом, что не поддерживаются поперечными волокнами.7. Изделие по п. 1, в котором ткань имеет плетение прядей, проходящих в первом, втором и третьем направлениях.8. Изделие по п. 1, в котором ткань имеет круглую границу, причем нити, проходящие за пределы границы, являются перпендикулярными по отношению к границе.9. Изделие по п. 1, в котором концы распределенных нитей имеют плоскостную волнистость.10. Изделие по п. 1, в котором нити, проходящие за пределы границы, имеют концы различной длины.11. Укладка, содержащая множество слоев усиливающих волокон и наружный слой, содержащий изделие по п. 1.12. Структура, содержащая первую и вторую части, соединенные вместе, причем первая часть соде�
Claims (20)
1. Изделие, содержащее многонаправленную ткань из первых усиливающих прядей волокна, проходящих в первом направлении, и вторых усиливающих прядей волокна, проходящих во втором направлении, причем части нитей в первых прядях волокна проходят за пределы границы ткани и являются распределенными, а пряди внедрены в смолу.
2. Изделие по п. 1, в котором нити во вторых прядях также проходят за пределы границы ткани и являются распределенными.
3. Изделие по п. 1, в котором нити в пределах границы ткани обеспечивают структурную прочность вдоль первого и второго направлений, причем нити, проходящие за пределы границы, обеспечивают структурную прочность в только первом направлении.
4. Изделие по п. 1, в котором ткань содержит несколько рядов связанных нитей, причем распределенные нити находятся в меньшем числе рядов.
5. Изделие по п. 1, в котором ткань имеет ткацкое переплетение прядей.
6. Изделие по п. 5, в котором нити, проходящие за пределы границы, разрежены таким образом, что не поддерживаются поперечными волокнами.
7. Изделие по п. 1, в котором ткань имеет плетение прядей, проходящих в первом, втором и третьем направлениях.
8. Изделие по п. 1, в котором ткань имеет круглую границу, причем нити, проходящие за пределы границы, являются перпендикулярными по отношению к границе.
9. Изделие по п. 1, в котором концы распределенных нитей имеют плоскостную волнистость.
10. Изделие по п. 1, в котором нити, проходящие за пределы границы, имеют концы различной длины.
11. Укладка, содержащая множество слоев усиливающих волокон и наружный слой, содержащий изделие по п. 1.
12. Структура, содержащая первую и вторую части, соединенные вместе, причем первая часть содержит множественные слои усиливающих волокон, при этом наружный слой из числа слоев содержит многомерную ткань усиливающих прядей, имеющих распределенные нити, которые соединены с поверхностью второй части.
13. Структура по п. 12, в которой первая и вторая части являются дискретными.
14. Структура по п. 13, в которой дискретные части являются элементами конструкции самолета.
15. Структура по п. 12, в которой первой частью является заплата для второй части.
16. Структура по п. 15, в которой вторая часть расположена в области самолета, которая подвержена ударному повреждению.
17. Структура по п. 12, в которой концы нитей являются волнистыми.
18. Способ изготовления композитной структуры, содержащий этапы, согласно которым:
соединяют первую и вторую части, причем первая часть содержит наружный слой, имеющий ткацкое переплетение первых прядей, проходящих в первом направлении, и вторых прядей, проходящих во втором направлении,
распределяют концы прядей на отдельные нити и
соединяют распределенные нити с поверхностью второй части.
19. Способ по п. 18, согласно которому первая и вторая части являются элементами конструкции самолета.
20. Способ по п. 18, согласно которому первой частью является заплата для второй части, которая в свою очередь является элементом конструкции самолета.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US14/034,456 US10035323B2 (en) | 2013-09-23 | 2013-09-23 | Composite textiles including spread filaments |
US14/034,456 | 2013-09-23 |
Publications (3)
Publication Number | Publication Date |
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RU2014118504A true RU2014118504A (ru) | 2015-11-20 |
RU2619647C2 RU2619647C2 (ru) | 2017-05-17 |
RU2619647C9 RU2619647C9 (ru) | 2017-09-18 |
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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RU2014118504A RU2619647C9 (ru) | 2013-09-23 | 2014-05-07 | Композитные ткани, содержащие распределенные нити |
Country Status (10)
Country | Link |
---|---|
US (1) | US10035323B2 (ru) |
EP (1) | EP2853380B1 (ru) |
JP (1) | JP6468761B2 (ru) |
CN (1) | CN104448877B (ru) |
AU (1) | AU2014202672B2 (ru) |
BR (1) | BR102014021942B1 (ru) |
CA (1) | CA2851497C (ru) |
ES (1) | ES2799180T3 (ru) |
PT (1) | PT2853380T (ru) |
RU (1) | RU2619647C9 (ru) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9919791B2 (en) * | 2015-04-15 | 2018-03-20 | Gulfstream Aerospace Corporation | Stiffening structures, wing structures, and methods for manufacturing stiffening structures |
CN107848163B (zh) * | 2015-07-08 | 2019-08-09 | 三菱化学株式会社 | 纤维增强复合材料的制造方法及纤维增强复合材料 |
GB201519877D0 (en) * | 2015-11-11 | 2015-12-23 | Short Brothers Plc | Methods and patches for repairing composite laminates |
US9827688B2 (en) * | 2016-01-12 | 2017-11-28 | The Boeing Company | Patch fabrication system |
CN106182749A (zh) * | 2016-07-13 | 2016-12-07 | 道生天合材料科技(上海)有限公司 | 玻璃纤维布粘接方法 |
EP3969685A4 (en) * | 2019-05-15 | 2022-06-29 | Dap Products Inc. | Layered apparatus and method |
Family Cites Families (30)
Publication number | Priority date | Publication date | Assignee | Title |
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-
2013
- 2013-09-23 US US14/034,456 patent/US10035323B2/en active Active
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2014
- 2014-05-07 RU RU2014118504A patent/RU2619647C9/ru active
- 2014-05-07 CA CA2851497A patent/CA2851497C/en active Active
- 2014-05-16 AU AU2014202672A patent/AU2014202672B2/en active Active
- 2014-08-26 CN CN201410423099.6A patent/CN104448877B/zh active Active
- 2014-09-04 JP JP2014179758A patent/JP6468761B2/ja active Active
- 2014-09-04 BR BR102014021942-0A patent/BR102014021942B1/pt active IP Right Grant
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AU2014202672B2 (en) | 2017-06-29 |
JP6468761B2 (ja) | 2019-02-13 |
ES2799180T3 (es) | 2020-12-15 |
PT2853380T (pt) | 2020-05-06 |
CA2851497A1 (en) | 2015-03-23 |
JP2015071300A (ja) | 2015-04-16 |
CN104448877A (zh) | 2015-03-25 |
CN104448877B (zh) | 2018-09-28 |
EP2853380B1 (en) | 2020-04-15 |
BR102014021942B1 (pt) | 2020-09-08 |
AU2014202672A1 (en) | 2015-04-09 |
BR102014021942A2 (pt) | 2015-09-15 |
US10035323B2 (en) | 2018-07-31 |
EP2853380A1 (en) | 2015-04-01 |
US20150086745A1 (en) | 2015-03-26 |
RU2619647C2 (ru) | 2017-05-17 |
CA2851497C (en) | 2016-08-30 |
RU2619647C9 (ru) | 2017-09-18 |
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