CN106560399B - 用于从复合非金属结构中的蒙皮紧固件转移雷电电流的方法 - Google Patents

用于从复合非金属结构中的蒙皮紧固件转移雷电电流的方法 Download PDF

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CN106560399B
CN106560399B CN201610653397.3A CN201610653397A CN106560399B CN 106560399 B CN106560399 B CN 106560399B CN 201610653397 A CN201610653397 A CN 201610653397A CN 106560399 B CN106560399 B CN 106560399B
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conductive layer
layer
conductive
holes
tapered
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CN106560399A (zh
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Q·勒
J·D·摩根
R·B·格雷戈尔
B·A·怀廷
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Boeing Co
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Boeing Co
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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
    • 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
    • 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
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    • 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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    • 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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    • 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
    • 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
    • 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
    • B32B37/12—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by using adhesives
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
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    • 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
    • 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
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    • B32B2260/02—Composition of the impregnated, bonded or embedded layer
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    • B—PERFORMING OPERATIONS; TRANSPORTING
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    • B32B2260/04—Impregnation, embedding, or binder material
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
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    • 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
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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
    • 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

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  • 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)
CN201610653397.3A 2015-10-05 2016-08-10 用于从复合非金属结构中的蒙皮紧固件转移雷电电流的方法 Active CN106560399B (zh)

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 (2)

Publication Number Publication Date
CN106560399A CN106560399A (zh) 2017-04-12
CN106560399B true CN106560399B (zh) 2021-08-24

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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)

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US10899468B2 (en) * 2018-09-27 2021-01-26 The Boeing Company Washer assembly with seal for lightning-protection fasteners and method of manufacture
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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

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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
EP3153410A1 (en) 2017-04-12
CN106560399A (zh) 2017-04-12
RU2711560C2 (ru) 2020-01-17
JP6941422B2 (ja) 2021-09-29

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