ES2196792T3 - Juntas unidas mediante adhesivo en estructuras de materiales compuestos de fibra de carbono. - Google Patents
Juntas unidas mediante adhesivo en estructuras de materiales compuestos de fibra de carbono.Info
- Publication number
- ES2196792T3 ES2196792T3 ES99913513T ES99913513T ES2196792T3 ES 2196792 T3 ES2196792 T3 ES 2196792T3 ES 99913513 T ES99913513 T ES 99913513T ES 99913513 T ES99913513 T ES 99913513T ES 2196792 T3 ES2196792 T3 ES 2196792T3
- Authority
- ES
- Spain
- Prior art keywords
- adhesive
- carbon fiber
- composite material
- fiber composite
- material structures
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 229920000049 Carbon (fiber) Polymers 0.000 title abstract 5
- 239000004917 carbon fiber Substances 0.000 title abstract 5
- 239000000853 adhesive Substances 0.000 title abstract 4
- 230000001070 adhesive effect Effects 0.000 title abstract 4
- 239000002131 composite material Substances 0.000 title abstract 4
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 title abstract 4
- 230000005540 biological transmission Effects 0.000 abstract 1
Classifications
-
- 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
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
- B29C65/4855—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding characterised by their physical properties, e.g. being electrically-conductive
-
- 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
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
- B29C65/4865—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding containing additives
- B29C65/487—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding containing additives characterised by their shape, e.g. being fibres or being spherical
- B29C65/488—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding containing additives characterised by their shape, e.g. being fibres or being spherical being longitudinal, e.g. fibres
-
- 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
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
- B29C65/4865—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding containing additives
- B29C65/4885—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding containing additives characterised by their composition being non-plastics
-
- 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
- B29C65/56—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using mechanical means or mechanical connections, e.g. form-fits
- B29C65/562—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using mechanical means or mechanical connections, e.g. form-fits using extra joining elements, i.e. which are not integral with the parts to be joined
-
- 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
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
- B29C66/112—Single lapped joints
-
- 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
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/13—Single flanged joints; Fin-type joints; Single hem joints; Edge joints; Interpenetrating fingered joints; Other specific particular designs of joint cross-sections not provided for in groups B29C66/11 - B29C66/12
- B29C66/131—Single flanged joints, i.e. one of the parts to be joined being rigid and flanged in the joint area
-
- 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
- B29C66/70—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
- B29C66/7212—Fibre-reinforced materials characterised by the composition of the fibres
-
- 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
- B29C66/7214—Fibre-reinforced materials characterised by the length of the fibres
- B29C66/72143—Fibres of discontinuous lengths
-
- 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
- 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
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
- B29C65/4805—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding characterised by the type of adhesives
- B29C65/483—Reactive adhesives, e.g. chemically curing adhesives
-
- 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
- B29C66/41—Joining substantially flat articles ; Making flat seams in tubular or hollow articles
- B29C66/43—Joining a relatively small portion of the surface of said articles
- B29C66/434—Joining substantially flat articles for forming corner connections, fork connections or cross connections
- B29C66/4344—Joining substantially flat articles for forming fork connections, e.g. for making Y-shaped pieces
- B29C66/43441—Joining substantially flat articles for forming fork connections, e.g. for making Y-shaped pieces with two right angles, e.g. for making T-shaped pieces, H-shaped pieces
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
- B29K2105/06—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2307/00—Use of elements other than metals as reinforcement
-
- 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
- B29L2031/712—Containers; Packaging elements or accessories, Packages
- B29L2031/7172—Fuel tanks, jerry cans
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Adhesives Or Adhesive Processes (AREA)
- Laminated Bodies (AREA)
- Lining Or Joining Of Plastics Or The Like (AREA)
Abstract
Una unión estructural para la transmisión y control de grandes flujos de corriente en una estructura de material compuesto de fibra de carbono o híbrido de fibra de carbono, comprendiendo dicha unión: al menos dos estructuras de material compuesto (1, 2) que comprenden una multiplicidad de capas de fibra de carbono unidas con resina, un adhesivo (3) aplicado entremedias y capaz de conducir grandes corrientes a través y fuera de la unión, incluyendo dicho adhesivo (3) una película portadora conductora que comprende fibras de carbono, en la que la conductividad eléctrica del adhesivo es comparable con la de las estructuras de material compuesto contiguas.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GBGB9807198.8A GB9807198D0 (en) | 1998-04-04 | 1998-04-04 | Adhesively bonded joints in carbon fibre composite structures |
Publications (1)
Publication Number | Publication Date |
---|---|
ES2196792T3 true ES2196792T3 (es) | 2003-12-16 |
Family
ID=10829818
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES99913513T Expired - Lifetime ES2196792T3 (es) | 1998-04-04 | 1999-04-01 | Juntas unidas mediante adhesivo en estructuras de materiales compuestos de fibra de carbono. |
Country Status (8)
Country | Link |
---|---|
US (1) | US6320118B1 (es) |
EP (1) | EP1068130B1 (es) |
JP (1) | JP3391467B2 (es) |
AU (1) | AU758909B2 (es) |
DE (1) | DE69908924D1 (es) |
ES (1) | ES2196792T3 (es) |
GB (1) | GB9807198D0 (es) |
WO (1) | WO1999051494A1 (es) |
Families Citing this family (49)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7115323B2 (en) * | 2003-08-28 | 2006-10-03 | The Boeing Company | Titanium foil ply replacement in layup of composite skin |
US20050055180A1 (en) * | 2003-09-08 | 2005-03-10 | Pischke Gina C. | Method and system for seat placement |
US7194391B2 (en) * | 2003-09-30 | 2007-03-20 | The Boeing Company | Method and system for seat placement |
US7052573B2 (en) * | 2003-11-21 | 2006-05-30 | The Boeing Company | Method to eliminate undulations in a composite panel |
FR2866991B1 (fr) * | 2004-02-26 | 2006-05-19 | Airbus France | Dispositif de retour d'alimentation electrique pour equipements avioniques |
GB0417473D0 (en) * | 2004-08-05 | 2004-09-08 | Airbus Uk Ltd | Fuel tank |
GB0417472D0 (en) * | 2004-08-05 | 2004-09-08 | Airbus Uk Ltd | Fuel tank system |
EP1826402B1 (en) * | 2004-11-11 | 2016-08-24 | Gamesa Innovation & Technology, S.L. | Lightning conductor system for wind generator blades comprising carbon fibre laminates |
US7721495B2 (en) * | 2005-03-31 | 2010-05-25 | The Boeing Company | Composite structural members and methods for forming the same |
US7467763B2 (en) * | 2005-06-03 | 2008-12-23 | Kismarton Max U | Composite landing gear apparatus and methods |
US8444087B2 (en) * | 2005-04-28 | 2013-05-21 | The Boeing Company | Composite skin and stringer structure and method for forming the same |
US20060222837A1 (en) * | 2005-03-31 | 2006-10-05 | The Boeing Company | Multi-axial laminate composite structures and methods of forming the same |
US7740932B2 (en) | 2005-03-31 | 2010-06-22 | The Boeing Company | Hybrid fiberglass composite structures and methods of forming the same |
US8720825B2 (en) | 2005-03-31 | 2014-05-13 | The Boeing Company | Composite stiffeners for aerospace vehicles |
US7748119B2 (en) * | 2005-06-03 | 2010-07-06 | The Boeing Company | Method for manufacturing composite components |
US20070052554A1 (en) * | 2005-08-24 | 2007-03-08 | The Boeing Company | Methods and systems for logistics health status display |
US20070050104A1 (en) * | 2005-08-24 | 2007-03-01 | The Boeing Company | Methods and systems for logistics health status reasoner |
DE102006003160A1 (de) * | 2006-01-24 | 2007-09-06 | Airbus Deutschland Gmbh | Flächendichtung sowie Verfahren zur Herstellung von abgedichteten Fügeverbindungen mit der Flächendichtung |
DK200600653A (da) * | 2006-05-09 | 2007-11-10 | Vestas Wind Sys As | Lynbeskyttelsesanlæg til en vindmöllevinge, og fremgangsmåde til fremstilling af en vindmöllevinge med et lynbeskyttelsessystem |
FR2914622B1 (fr) | 2007-04-04 | 2009-05-15 | Airbus France Sas | Aeronef comprenant une structure assurant les fonctions structurale et electrique |
US7628879B2 (en) * | 2007-08-23 | 2009-12-08 | The Boeing Company | Conductive scrim embedded structural adhesive films |
FR2924685B1 (fr) * | 2007-12-11 | 2010-03-19 | Airbus France | Systeme parafoudre et aeronef comportant un tel systeme. |
GB0802938D0 (en) * | 2008-02-19 | 2008-03-26 | Airbus Uk Ltd | Clamped friction joint |
GB0805640D0 (en) | 2008-03-28 | 2008-04-30 | Hexcel Composites Ltd | Improved composite materials |
ATE535711T1 (de) * | 2008-07-02 | 2011-12-15 | Siemens Ag | Windturbinenschaufel mit blitzrezeptor und verfahren zum schutz der oberfläche einer windturbinenschaufel |
GB0819159D0 (en) | 2008-10-20 | 2008-11-26 | Airbus Uk Ltd | Joint between aircraft components |
US8382413B2 (en) | 2008-11-17 | 2013-02-26 | The Boeing Company | Conductive sleeved fastener assembly |
US8231080B2 (en) * | 2009-02-26 | 2012-07-31 | The Boeing Company | Distributing power in systems having a composite structure |
US11407199B2 (en) * | 2009-04-15 | 2022-08-09 | The Boeing Company | Metal-coated fabrics for fiber-metal laminates |
JP5924934B2 (ja) * | 2011-12-28 | 2016-05-25 | 三菱重工業株式会社 | 複合材の継手構造 |
WO2013146335A1 (ja) * | 2012-03-26 | 2013-10-03 | 三菱重工業株式会社 | 燃料タンク、主翼、航空機胴体、航空機及び移動体 |
US8937254B2 (en) * | 2012-05-29 | 2015-01-20 | Aurora Flight Sciences Corporation | Apparatus and method for an aircraft conductor sandwich assembly embedded to an aircraft structure |
US20140117022A1 (en) * | 2012-10-30 | 2014-05-01 | The Boeing Company | Composite Structures Having Bondlines with Matched Electrical Conductivity |
US9878773B2 (en) | 2012-12-03 | 2018-01-30 | The Boeing Company | Split resistant composite laminate |
GB2510133B (en) | 2013-01-24 | 2017-08-30 | Bae Systems Plc | Conductive bonded composites |
US9331402B2 (en) | 2013-02-04 | 2016-05-03 | The Boeing Company | Conductive sleeved fastener assembly |
US9343824B2 (en) | 2013-02-04 | 2016-05-17 | The Boeing Company | Sleeved fastener assembly |
JP6071686B2 (ja) | 2013-03-26 | 2017-02-01 | 三菱重工業株式会社 | 燃料タンク、主翼、航空機胴体、航空機及び移動体 |
JP6113544B2 (ja) * | 2013-03-26 | 2017-04-12 | 三菱重工業株式会社 | 燃料タンク、主翼、航空機胴体、航空機及び移動体 |
ES2674659T3 (es) | 2013-09-23 | 2018-07-03 | Airbus Operations S.L. | Método para fabricar una caja de torsión aeronáutica, caja de torsión y herramienta para fabricar una caja de torsión aeronáutica |
US10368401B2 (en) | 2014-06-03 | 2019-07-30 | Aurora Flight Sciences Corporation | Multi-functional composite structures |
US10167550B2 (en) | 2014-06-03 | 2019-01-01 | Aurora Flight Sciences Corporation | Multi-functional composite structures |
GB2529634B (en) * | 2014-08-26 | 2017-04-19 | Kwikbolt Ltd | Removable blind fastener for joining components |
US10285219B2 (en) * | 2014-09-25 | 2019-05-07 | Aurora Flight Sciences Corporation | Electrical curing of composite structures |
US10329030B2 (en) | 2016-03-04 | 2019-06-25 | The Boeing Company | Conductive radius filler system and method |
JP6778221B2 (ja) | 2018-01-15 | 2020-10-28 | 株式会社Subaru | 締結構造 |
US11685508B2 (en) * | 2020-04-08 | 2023-06-27 | The Boeing Company | Systems and methods for constructing a bonded structure |
US11725632B2 (en) | 2020-10-08 | 2023-08-15 | Arctura, Inc. | Surface coating for enhanced lightning protection of wind turbine blades and other composite structures |
US11162475B1 (en) * | 2020-10-08 | 2021-11-02 | Ardura, Inc. | Surface coating for enhanced lightning protection of wind turbine blades and other composite structures |
Family Cites Families (14)
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US3347978A (en) * | 1963-06-03 | 1967-10-17 | Lockheed Aircraft Corp | Electrically conductive joints and gaskets |
DE2362801C3 (de) | 1973-12-18 | 1979-02-08 | Hoechst Ag, 6000 Frankfurt | Verfahren zum Aufbringen von metallischen Kontaktstreifen auf Flächenheizelemente |
US4556591A (en) * | 1981-09-25 | 1985-12-03 | The Boeing Company | Conductive bonded/bolted joint seals for composite aircraft |
WO1984001487A1 (en) * | 1982-09-30 | 1984-04-12 | Boeing Co | Integral lightning protection system for composite aircraft skins |
DE3606464A1 (de) * | 1986-02-28 | 1987-09-03 | Licentia Gmbh | Einrichtung an solargeneratoren zur verhinderung statischer aufladungen |
GB8628555D0 (en) * | 1986-11-28 | 1987-01-07 | British Aerospace | Anti lightning strike fasteners |
JPH0764962B2 (ja) * | 1986-12-05 | 1995-07-12 | 日本ユニカ−株式会社 | 耐熱導電性接着性樹脂組成物 |
US5127601A (en) * | 1989-01-23 | 1992-07-07 | Lightning Diversion Systems | Conformal lightning shield and method of making |
FR2668580B1 (fr) * | 1990-10-30 | 1993-01-22 | Aerospatiale | Structure anti-etincelage, notamment pour aeronef. |
WO1992009992A1 (de) * | 1990-12-01 | 1992-06-11 | Henkel Kommanditgesellschaft Auf Aktien | Zusammensetzung aus elektrisch isolierenden polymeren und elektrisch leitfähigen füllstoffen |
US5613862A (en) * | 1992-07-18 | 1997-03-25 | Central Research Laboratories Limited | Anisotropic electrical connection |
GB9411006D0 (en) * | 1994-06-02 | 1994-07-20 | British Aerospace | Method of fastening composite aircraft skins |
US5686703A (en) | 1994-12-16 | 1997-11-11 | Minnesota Mining And Manufacturing Company | Anisotropic, electrically conductive adhesive film |
US5698316A (en) * | 1996-10-07 | 1997-12-16 | The Boeing Company | Apparatus and methods of providing corrosion resistant conductive path across non conductive joints or gaps |
-
1998
- 1998-04-04 GB GBGB9807198.8A patent/GB9807198D0/en not_active Ceased
-
1999
- 1999-04-01 EP EP99913513A patent/EP1068130B1/en not_active Expired - Lifetime
- 1999-04-01 DE DE69908924T patent/DE69908924D1/de not_active Expired - Lifetime
- 1999-04-01 WO PCT/GB1999/001032 patent/WO1999051494A1/en active IP Right Grant
- 1999-04-01 AU AU31624/99A patent/AU758909B2/en not_active Ceased
- 1999-04-01 ES ES99913513T patent/ES2196792T3/es not_active Expired - Lifetime
- 1999-04-01 JP JP55018599A patent/JP3391467B2/ja not_active Expired - Fee Related
- 1999-09-17 US US09/397,867 patent/US6320118B1/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
EP1068130A1 (en) | 2001-01-17 |
WO1999051494A1 (en) | 1999-10-14 |
DE69908924D1 (de) | 2003-07-24 |
AU758909B2 (en) | 2003-04-03 |
JP2001510422A (ja) | 2001-07-31 |
US6320118B1 (en) | 2001-11-20 |
JP3391467B2 (ja) | 2003-03-31 |
AU3162499A (en) | 1999-10-25 |
GB9807198D0 (en) | 1998-06-03 |
EP1068130B1 (en) | 2003-06-18 |
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