JP2012527375A - 落雷保護を有する構造物の形成方法 - Google Patents

落雷保護を有する構造物の形成方法 Download PDF

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Publication number
JP2012527375A
JP2012527375A JP2012511960A JP2012511960A JP2012527375A JP 2012527375 A JP2012527375 A JP 2012527375A JP 2012511960 A JP2012511960 A JP 2012511960A JP 2012511960 A JP2012511960 A JP 2012511960A JP 2012527375 A JP2012527375 A JP 2012527375A
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JP
Japan
Prior art keywords
lightning protection
reinforcing layer
layer
strip
protection strip
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Pending
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JP2012511960A
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English (en)
Japanese (ja)
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JP2012527375A5 (enExample
Inventor
ロバート ジェー． ランゴーン
ロバート ディー． ベッカー
Original Assignee
エーディーシー アクイジション カンパニー
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Application filed by エーディーシー アクイジション カンパニー filed Critical エーディーシー アクイジション カンパニー
Publication of JP2012527375A publication Critical patent/JP2012527375A/ja
Publication of JP2012527375A5 publication Critical patent/JP2012527375A5/ja
Pending legal-status Critical Current

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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
    • 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
    • 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
    • B29C70/38—Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
    • B29C70/386—Automated tape laying [ATL]
    • 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
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D45/02—Lightning protectors; Static dischargers
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Robotics (AREA)
  • Laminated Bodies (AREA)
  • Moulding By Coating Moulds (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
JP2012511960A 2009-05-19 2010-05-18 落雷保護を有する構造物の形成方法 Pending JP2012527375A (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US17953909P 2009-05-19 2009-05-19
US61/179,539 2009-05-19
PCT/US2010/035243 WO2010135318A2 (en) 2009-05-19 2010-05-18 Methods for forming a structure having a lightning strike protection

Publications (2)

Publication Number Publication Date
JP2012527375A true JP2012527375A (ja) 2012-11-08
JP2012527375A5 JP2012527375A5 (enExample) 2013-07-18

Family

ID=42478459

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2012511960A Pending JP2012527375A (ja) 2009-05-19 2010-05-18 落雷保護を有する構造物の形成方法

Country Status (7)

Country Link
US (1) US8947847B2 (enExample)
EP (1) EP2432634B1 (enExample)
JP (1) JP2012527375A (enExample)
BR (1) BRPI1010934A2 (enExample)
CA (1) CA2762520C (enExample)
ES (1) ES2439648T3 (enExample)
WO (1) WO2010135318A2 (enExample)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8947847B2 (en) 2009-05-19 2015-02-03 Adc Acquisition Company Methods for forming a structure having a lightning strike protection
WO2015040951A1 (ja) * 2013-09-18 2015-03-26 株式会社Ihi ジェットエンジンのための導電構造
WO2016103841A1 (ja) * 2014-12-26 2016-06-30 株式会社Ihi 円筒状ケース及びジェットエンジン

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WO2012091897A1 (en) * 2010-12-31 2012-07-05 Cytec Technology Corp. Method of fabricating a composite structure with a conductive surface
EP2686244B1 (en) 2011-03-16 2016-05-18 Airbus Operations Limited Aircraft bonding network
DE102011112518B4 (de) * 2011-05-27 2020-01-09 Airbus Defence and Space GmbH Verfahren zur Herstellung einer Oberflächenstruktur mit Blitzschutz sowie Fahrzeugbauteilherstellverfahren
CN104115580A (zh) * 2011-08-25 2014-10-22 洛德公司 雷击防护系统
DE102011086101A1 (de) * 2011-11-10 2013-05-16 Airbus Operations Gmbh Verfahren zur automatisierten Herstellung eines Faserverbundbauteils mit integriertem Blitzschutz sowie Faserverbundbauteil
EP2743064B1 (en) 2012-12-14 2016-09-14 Airbus Operations GmbH Lightning strike protection means and fibre composite component
US9643734B2 (en) * 2013-03-18 2017-05-09 The Boeing Company Electromagnetic energy surface protection
JP6150054B2 (ja) * 2013-07-02 2017-06-21 株式会社Ihi 静翼構造及びこれを用いたターボファンジェットエンジン
DE102014004118A1 (de) 2014-03-24 2015-09-24 Airbus Operations Gmbh Neuartiges blitzschutzmaterial für faerverbundbauteile
GB2531045B (en) * 2014-10-08 2019-04-24 Hexcel Composites Ltd Electrically conductive surfacing material
FR3028205B1 (fr) * 2014-11-10 2018-01-05 Airbus Operations Procede de fabrication d'un panneau en materiau composite integrant une protection contre la foudre et panneau en materiau composite fabrique selon ledit procede
DE102014017198A1 (de) * 2014-11-21 2016-05-25 Airbus Defence and Space GmbH Strukturelement
BR112018010824B1 (pt) * 2015-11-30 2022-02-01 Cytec Industries Inc Material de superfície integrado eletricamente condutivo, estrutura compósita, e, método para formar uma estrutura compósita
GB201522539D0 (en) 2015-12-21 2016-02-03 Hexcel Composites Ltd Improvements in or relating to electrically conducting materials
WO2018063970A1 (en) 2016-09-27 2018-04-05 3M Innovative Properties Company Protection film
CN111070722B (zh) * 2018-10-19 2021-10-22 哈尔滨工业大学 一种基于隔热和绝缘机理的雷电防护复合材料的制备方法
US12134238B2 (en) 2018-12-21 2024-11-05 3M Innovative Properties Company Fiber-reinforced composite layup
US12257817B2 (en) * 2019-03-29 2025-03-25 Kawasaki Jukogyo Kabushiki Kaisha Composite panel structure and method of manufacturing
US11053020B2 (en) * 2019-08-13 2021-07-06 The Boeing Company Electrically conductive patch for indicating a compromised electrical discharge point in an aircraft
DE102019133418A1 (de) * 2019-12-06 2021-06-10 Deutsches Zentrum für Luft- und Raumfahrt e.V. Blitzschutzwerkstoff und Verfahren zur Herstellung eines Faserverbundbauteils
US11872774B2 (en) * 2020-09-29 2024-01-16 Ford Global Technologies, Llc Independent conductive tape dispensing system for manufacturing of electrical distribution circuits in vehicles
US12043003B2 (en) 2022-01-18 2024-07-23 Rohr, Inc. Assemblies and methods for forming fiber reinforced thermoplastic structures
US12115738B2 (en) * 2022-01-18 2024-10-15 Rohr, Inc. Assemblies and methods for forming fiber-reinforced thermoplastic structures with lightning strike protection
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
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
US12350915B2 (en) 2022-03-30 2025-07-08 The Boeing Company Co-cured UV/visible light-resistant composite material for structural aircraft 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
GB2632100A (en) 2023-07-18 2025-01-29 Hexcel Composites Ltd Lightning strike surfacing material

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4352142A (en) * 1981-04-15 1982-09-28 The Boeing Company Composite aircraft structure having lightning protection
JPH027399A (ja) * 1987-10-30 1990-01-11 Ppg Ind Inc 航空機窓に静電荷が集積されるのを減少させる方法及び装置
US5370921A (en) * 1991-07-11 1994-12-06 The Dexter Corporation Lightning strike composite and process
DE10252909A1 (de) * 2002-11-12 2004-05-19 Cargolifter Ag I.Ins. Anordnung zum Blitzschutz membraner Strukturen von Luftfahrzeugen
US20050041362A1 (en) * 2003-08-18 2005-02-24 Hall Allen L. Current diverter strip and methods
US20070141927A1 (en) * 2005-12-21 2007-06-21 Brown Arlene M Method and system for exterior protection of an aircraft
WO2008015082A1 (en) * 2006-08-01 2008-02-07 Airbus Deutschland Gmbh Lay-up arrangement and structural arrangement and method for producing a component for aerospace
JP2011524265A (ja) * 2008-04-14 2011-09-01 ザ・ボーイング・カンパニー 一体型落雷防護材料の作成システムおよび方法

Family Cites Families (6)

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US3755713A (en) 1972-07-25 1973-08-28 Boeing Co Electrically conductive surface for aircraft
US6692681B1 (en) 1997-01-29 2004-02-17 Raytheon Aircraft Company Method and apparatus for manufacturing composite structures
US7063118B2 (en) 2003-11-20 2006-06-20 Adc Acquisition Company Composite tape laying apparatus and method
WO2006093553A2 (en) * 2004-12-17 2006-09-08 Hexcel Corporation Anodized aluminum foil sheets and expanded aluminum foil (eaf) sheets and methods of making and using the same
US8312827B1 (en) * 2007-01-08 2012-11-20 James J Free Inter/pre-cured layer/pre-cured embroidered composite laminate and method of producing same
CA2762520C (en) 2009-05-19 2017-03-21 Adc Acquisition Company Methods for forming a structure having a lightning strike protection

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4352142A (en) * 1981-04-15 1982-09-28 The Boeing Company Composite aircraft structure having lightning protection
JPH027399A (ja) * 1987-10-30 1990-01-11 Ppg Ind Inc 航空機窓に静電荷が集積されるのを減少させる方法及び装置
US5370921A (en) * 1991-07-11 1994-12-06 The Dexter Corporation Lightning strike composite and process
DE10252909A1 (de) * 2002-11-12 2004-05-19 Cargolifter Ag I.Ins. Anordnung zum Blitzschutz membraner Strukturen von Luftfahrzeugen
US20050041362A1 (en) * 2003-08-18 2005-02-24 Hall Allen L. Current diverter strip and methods
US20070141927A1 (en) * 2005-12-21 2007-06-21 Brown Arlene M Method and system for exterior protection of an aircraft
WO2008015082A1 (en) * 2006-08-01 2008-02-07 Airbus Deutschland Gmbh Lay-up arrangement and structural arrangement and method for producing a component for aerospace
JP2009545468A (ja) * 2006-08-01 2009-12-24 エアバス ドイッチュラント ゲゼルシャフト ミット ベシュレンクテル ハフツング レイアップ配列及び構造配列並びに航空宇宙産業用構成部品の製造方法
JP2011524265A (ja) * 2008-04-14 2011-09-01 ザ・ボーイング・カンパニー 一体型落雷防護材料の作成システムおよび方法

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8947847B2 (en) 2009-05-19 2015-02-03 Adc Acquisition Company Methods for forming a structure having a lightning strike protection
WO2015040951A1 (ja) * 2013-09-18 2015-03-26 株式会社Ihi ジェットエンジンのための導電構造
JP2015059460A (ja) * 2013-09-18 2015-03-30 株式会社Ihi ジェットエンジンのための導電構造
US10421557B2 (en) 2013-09-18 2019-09-24 Ihi Corporation Electric conduction structure for jet engine
WO2016103841A1 (ja) * 2014-12-26 2016-06-30 株式会社Ihi 円筒状ケース及びジェットエンジン
JP2016125357A (ja) * 2014-12-26 2016-07-11 株式会社Ihi 円筒状ケース及びジェットエンジン
CN107076054A (zh) * 2014-12-26 2017-08-18 株式会社Ihi 圆筒状壳体以及喷气发动机
CN107076054B (zh) * 2014-12-26 2018-11-30 株式会社Ihi 圆筒状壳体以及喷气发动机
US10843811B2 (en) 2014-12-26 2020-11-24 Ihi Corporation Cylindrical case and jet engine

Also Published As

Publication number Publication date
ES2439648T3 (es) 2014-01-24
WO2010135318A3 (en) 2011-01-20
CA2762520A1 (en) 2010-11-25
US20120063050A1 (en) 2012-03-15
WO2010135318A2 (en) 2010-11-25
EP2432634B1 (en) 2013-12-04
US8947847B2 (en) 2015-02-03
EP2432634A2 (en) 2012-03-28
BRPI1010934A2 (pt) 2016-04-05
CA2762520C (en) 2017-03-21

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