JP6941422B2 - 落雷防護相互接続を有する多層複合材構造体及び外板留め具から雷電流をそらす方法 - Google Patents
落雷防護相互接続を有する多層複合材構造体及び外板留め具から雷電流をそらす方法 Download PDFInfo
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- JP6941422B2 JP6941422B2 JP2016193484A JP2016193484A JP6941422B2 JP 6941422 B2 JP6941422 B2 JP 6941422B2 JP 2016193484 A JP2016193484 A JP 2016193484A JP 2016193484 A JP2016193484 A JP 2016193484A JP 6941422 B2 JP6941422 B2 JP 6941422B2
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- layer
- conductive layer
- conductive
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- fastener
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D45/02—Lightning protectors; Static dischargers
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02G—INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINED OPTICAL AND ELECTRIC CABLES OR LINES
- H02G13/00—Installations of lightning conductors; Fastening thereof to supporting structure
- H02G13/80—Discharge by conduction or dissipation, e.g. rods, arresters, spark gaps
-
- 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
- B29C70/88—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced
-
- 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
- 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
- B29C70/88—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced
- B29C70/882—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced partly or totally electrically conductive, e.g. for EMI shielding
-
- 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
- B29C70/88—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced
- B29C70/882—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced partly or totally electrically conductive, e.g. for EMI shielding
- B29C70/885—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced partly or totally electrically conductive, e.g. for EMI shielding with incorporated metallic wires, nets, films or plates
-
- 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
- B32B15/00—Layered products comprising a layer of metal
- B32B15/02—Layer formed of wires, e.g. mesh
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- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
- B32B15/08—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
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- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/06—Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material
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- 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
- B32B3/08—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 characterised by added members at particular parts
- B32B3/085—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 characterised by added members at particular parts spaced apart pieces on the surface of a layer
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- 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
- B32B3/10—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 discontinuous layer, i.e. formed of separate pieces of material
- B32B3/12—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 discontinuous layer, i.e. formed of separate pieces of material characterised by a layer of regularly- arranged cells, e.g. a honeycomb structure
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- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B33/00—Layered products characterised by particular properties or particular surface features, e.g. particular surface coatings; Layered products designed for particular purposes not covered by another single class
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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
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/02—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by a sequence of laminating steps, e.g. by adding new layers at consecutive laminating stations
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/12—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by using adhesives
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- 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
- 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
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D37/00—Arrangements in connection with fuel supply for power plant
- B64D37/32—Safety measures not otherwise provided for, e.g. preventing explosive conditions
-
- 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
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B37/00—Nuts or like thread-engaging members
- F16B37/14—Cap nuts; Nut caps or bolt caps
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02G—INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINED OPTICAL AND ELECTRIC CABLES OR LINES
- H02G13/00—Installations of lightning conductors; Fastening thereof to supporting structure
-
- 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
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- 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
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/20—Properties of the layers or laminate having particular electrical or magnetic properties, e.g. piezoelectric
- B32B2307/202—Conductive
-
- 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
-
- 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)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Laminated Bodies (AREA)
- Moulding By Coating Moulds (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US14/875,297 US9912137B2 (en) | 2015-10-05 | 2015-10-05 | Methods for diverting lightning current from skin fasteners in composite, non-metallic structures |
| US14/875,297 | 2015-10-05 |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2017071388A JP2017071388A (ja) | 2017-04-13 |
| JP2017071388A5 JP2017071388A5 (enExample) | 2019-10-24 |
| JP6941422B2 true JP6941422B2 (ja) | 2021-09-29 |
Family
ID=57137806
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2016193484A Active JP6941422B2 (ja) | 2015-10-05 | 2016-09-30 | 落雷防護相互接続を有する多層複合材構造体及び外板留め具から雷電流をそらす方法 |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US9912137B2 (enExample) |
| EP (1) | EP3153410B1 (enExample) |
| JP (1) | JP6941422B2 (enExample) |
| CN (1) | CN106560399B (enExample) |
| AU (1) | AU2016204482B2 (enExample) |
| BR (1) | BR102016018329B1 (enExample) |
| CA (1) | CA2934731C (enExample) |
| RU (1) | RU2711560C2 (enExample) |
Families Citing this family (24)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US10878139B2 (en) * | 2015-07-27 | 2020-12-29 | The Boeing Company | Composite joint optimization |
| CN107323648A (zh) * | 2017-06-22 | 2017-11-07 | 中国航空工业集团公司沈阳飞机设计研究所 | 复合材料飞机的传导金属网络 |
| US10710352B2 (en) * | 2017-07-11 | 2020-07-14 | The Boeing Company | Structural pre-cured repair patch for repair to highly loaded primary and secondary structural components |
| US10875663B2 (en) | 2017-12-11 | 2020-12-29 | The Boeing Company | Lightning protection in aircrafts constructed with carbon fiber reinforced plastic |
| JP6778221B2 (ja) | 2018-01-15 | 2020-10-28 | 株式会社Subaru | 締結構造 |
| US11338899B2 (en) * | 2018-04-05 | 2022-05-24 | The Boeing Company | Joint for a metal airplane skin using metal matrix composite |
| US10899468B2 (en) * | 2018-09-27 | 2021-01-26 | The Boeing Company | Washer assembly with seal for lightning-protection fasteners and method of manufacture |
| US11001393B2 (en) | 2018-09-27 | 2021-05-11 | The Boeing Company | Washer assembly with seal for lightning-protection fasteners and method of use |
| CN109783849B (zh) * | 2018-12-06 | 2021-11-23 | 西安交通大学 | 单一快上升雷电流分量作用下碳纤维复合材料损伤计算方法 |
| CN109783848B (zh) * | 2018-12-06 | 2022-04-05 | 西安交通大学 | 单一缓上升雷电流分量作用下碳纤维复合材料损伤计算方法 |
| CN109605783A (zh) * | 2018-12-10 | 2019-04-12 | 河北汉光重工有限责任公司 | 一种解决复合材料结构件导电连续性的方法 |
| CN110065620A (zh) * | 2019-04-12 | 2019-07-30 | 西安飞机工业(集团)有限责任公司 | 一种复合材料壁板连接结构 |
| US11396900B2 (en) * | 2019-05-10 | 2022-07-26 | The Boeing Company | Fastener and methods of manufacturing and use |
| GB2596322B (en) * | 2020-06-24 | 2024-06-05 | Stalcom Automotive Tech Limited | Sheet Material |
| CN112072335B (zh) * | 2020-09-25 | 2022-06-24 | 中国直升机设计研究所 | 一种复合材料结构件之间导电结构及导电处理方法 |
| CH718028B1 (fr) * | 2020-11-02 | 2023-06-30 | Projets Et Realisations Sarl | Fuselage d'aéronef configuré pour offrir aux passagers une vue totalement panoramique de l'extérieur. |
| CN113928576B (zh) * | 2021-11-19 | 2023-09-01 | 中国直升机设计研究所 | 一种直升机复合材料雷电防护能力修复方法 |
| US12350915B2 (en) | 2022-03-30 | 2025-07-08 | The Boeing Company | Co-cured UV/visible light-resistant composite material for structural aircraft assembly |
| US12350892B2 (en) | 2022-03-30 | 2025-07-08 | The Boeing Company | Co-cured UV/visible light-resistant fiberglass coated composite material for aircraft fuselage assembly |
| US12377949B2 (en) | 2022-03-30 | 2025-08-05 | The Boeing Company | Co-cured UV/visible light-resistant coated composite material for aircraft fuselage assembly |
| US12466574B2 (en) | 2022-03-30 | 2025-11-11 | The Boeing Company | Co-cured UV-resistant fiberglass coated composite material for aircraft wing fuel tank assembly |
| GB2620563A (en) * | 2022-07-07 | 2024-01-17 | Airbus Operations Ltd | Structure with lightning-strike protection layer |
| CN115648668B (zh) * | 2022-10-26 | 2025-08-29 | 河北中电华拓科技有限公司 | 一种实现碳纤维复合材料电导通结构及其制造方法 |
| CN116053812A (zh) * | 2022-12-19 | 2023-05-02 | 中国直升机设计研究所 | 复合材料活动罩与机体固定结构之间导电方法及结构 |
Family Cites Families (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3755713A (en) | 1972-07-25 | 1973-08-28 | Boeing Co | Electrically conductive surface for aircraft |
| FR2765066B1 (fr) | 1997-06-20 | 1999-08-20 | Aerospatiale | Structure anti-etincelage, notamment pour aeronef |
| ES2264299B1 (es) | 2003-06-06 | 2007-11-16 | Airbus España S.L. | Sistema de proteccion contra rayos para depositos de combustible fabricados en materiales compuestos de pobre conductividad electrica. |
| US7686905B2 (en) * | 2005-09-06 | 2010-03-30 | The Boeing Company | Copper grid repair technique for lightning strike protection |
| US8246770B2 (en) * | 2005-09-06 | 2012-08-21 | The Boeing Company | Copper grid repair technique for lightning strike protection |
| US7599164B2 (en) | 2006-12-07 | 2009-10-06 | The Boeing Company | Lightning protection system for aircraft composite structure |
| US7898785B2 (en) * | 2006-12-07 | 2011-03-01 | The Boeing Company | Lightning protection system for an aircraft composite structure |
| JP4719203B2 (ja) * | 2007-09-28 | 2011-07-06 | 三菱重工業株式会社 | 耐雷ファスナ |
| FR2924685B1 (fr) * | 2007-12-11 | 2010-03-19 | Airbus France | Systeme parafoudre et aeronef comportant un tel systeme. |
| JP5055178B2 (ja) * | 2008-03-24 | 2012-10-24 | 三菱重工業株式会社 | 航空機組立品 |
| US8206823B2 (en) | 2008-04-14 | 2012-06-26 | The Boeing Company | System and method for fabrication of integrated lightning strike protection material |
| EP2331320B1 (en) | 2008-10-03 | 2013-03-13 | Short Brothers Plc | Fibre reinforced composite structures and method of manufacture |
| KR101711226B1 (ko) * | 2009-04-17 | 2017-02-28 | 쓰리엠 이노베이티브 프로퍼티즈 컴파니 | 패턴화된 전도체를 갖는 낙뢰 보호 시트 |
| US8475102B2 (en) * | 2009-10-22 | 2013-07-02 | Alcoa Inc. | Enhanced conductivity sleeved fastener and method for making same |
| EP2501975B1 (en) * | 2009-11-20 | 2015-01-07 | Alcoa Inc. | Lockwireless anti-rotation fitting |
| RU2466912C1 (ru) * | 2011-07-01 | 2012-11-20 | Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Национальный исследовательский университет "МЭИ" | Устройство для молниезащиты носового обтекателя самолета и находящейся под ним антенны |
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2015
- 2015-10-05 US US14/875,297 patent/US9912137B2/en active Active
-
2016
- 2016-06-28 RU RU2016125789A patent/RU2711560C2/ru active
- 2016-06-29 CA CA2934731A patent/CA2934731C/en active Active
- 2016-06-29 AU AU2016204482A patent/AU2016204482B2/en active Active
- 2016-08-09 BR BR102016018329-4A patent/BR102016018329B1/pt active IP Right Grant
- 2016-08-10 CN CN201610653397.3A patent/CN106560399B/zh active Active
- 2016-09-16 EP EP16189302.9A patent/EP3153410B1/en active Active
- 2016-09-30 JP JP2016193484A patent/JP6941422B2/ja active Active
Also Published As
| Publication number | Publication date |
|---|---|
| US9912137B2 (en) | 2018-03-06 |
| AU2016204482B2 (en) | 2020-10-08 |
| US20170098930A1 (en) | 2017-04-06 |
| CA2934731A1 (en) | 2017-04-05 |
| RU2016125789A (ru) | 2018-01-10 |
| BR102016018329A2 (pt) | 2017-07-25 |
| CA2934731C (en) | 2021-03-09 |
| AU2016204482A1 (en) | 2017-04-20 |
| EP3153410B1 (en) | 2020-06-17 |
| JP2017071388A (ja) | 2017-04-13 |
| BR102016018329B1 (pt) | 2021-10-26 |
| CN106560399B (zh) | 2021-08-24 |
| EP3153410A1 (en) | 2017-04-12 |
| CN106560399A (zh) | 2017-04-12 |
| RU2711560C2 (ru) | 2020-01-17 |
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