RU2009102192A - Способ изготовления конструктивного компонента для авиационно-космических летательных аппаратов - Google Patents

Способ изготовления конструктивного компонента для авиационно-космических летательных аппаратов Download PDF

Info

Publication number
RU2009102192A
RU2009102192A RU2009102192/05A RU2009102192A RU2009102192A RU 2009102192 A RU2009102192 A RU 2009102192A RU 2009102192/05 A RU2009102192/05 A RU 2009102192/05A RU 2009102192 A RU2009102192 A RU 2009102192A RU 2009102192 A RU2009102192 A RU 2009102192A
Authority
RU
Russia
Prior art keywords
reinforcing elements
arrangement
web
tape
biaxial
Prior art date
Application number
RU2009102192/05A
Other languages
English (en)
Other versions
RU2438876C2 (ru
Inventor
Олаф РОКЕР (DE)
Олаф РОКЕР
Мануэль ЮНГ (DE)
Мануэль ЮНГ
Торстен БЛЕК (DE)
Торстен БЛЕК
Original Assignee
Эйрбас Дойчланд Гмбх (De)
Эйрбас Дойчланд Гмбх
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Эйрбас Дойчланд Гмбх (De), Эйрбас Дойчланд Гмбх filed Critical Эйрбас Дойчланд Гмбх (De)
Publication of RU2009102192A publication Critical patent/RU2009102192A/ru
Application granted granted Critical
Publication of RU2438876C2 publication Critical patent/RU2438876C2/ru

Links

Classifications

    • 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
    • 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
    • B32B27/00—Layered products comprising a layer of synthetic resin
    • B32B27/04—Layered products comprising a layer of synthetic resin as impregnant, bonding, or embedding substance
    • 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
    • B32B5/28—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 impregnated with or embedded in a plastic substance
    • D—TEXTILES; PAPER
    • D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
    • D04H—MAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
    • D04H13/00—Other non-woven fabrics
    • D—TEXTILES; PAPER
    • D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
    • D04H—MAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
    • D04H3/00—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length
    • D04H3/002—Inorganic yarns or filaments
    • D04H3/004—Glass yarns or filaments
    • D—TEXTILES; PAPER
    • D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
    • D04H—MAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
    • D04H3/00—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length
    • D04H3/02—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of forming fleeces or layers, e.g. reorientation of yarns or filaments
    • D04H3/04—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of forming fleeces or layers, e.g. reorientation of yarns or filaments in rectilinear paths, e.g. crossing at right angles
    • D—TEXTILES; PAPER
    • D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
    • D04H—MAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
    • D04H3/00—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length
    • D04H3/02—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of forming fleeces or layers, e.g. reorientation of yarns or filaments
    • D04H3/04—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of forming fleeces or layers, e.g. reorientation of yarns or filaments in rectilinear paths, e.g. crossing at right angles
    • D04H3/045—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of forming fleeces or layers, e.g. reorientation of yarns or filaments in rectilinear paths, e.g. crossing at right angles for net manufacturing
    • 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
    • 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
    • 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
    • Y10T156/12—Surface bonding means and/or assembly means with cutting, punching, piercing, severing or tearing
    • Y10T156/1348—Work traversing type
    • 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
    • Y10T156/17—Surface bonding means and/or assemblymeans with work feeding or handling means
    • Y10T156/1788—Work traversing type and/or means applying work to wall or static 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
    • Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/17—Surface bonding means and/or assemblymeans with work feeding or handling means
    • Y10T156/1788—Work traversing type and/or means applying work to wall or static structure
    • Y10T156/1795—Implement carried web supply
    • 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
    • Y10T428/31504—Composite [nonstructural laminate]
    • Y10T428/31678—Of metal

Landscapes

  • Engineering & Computer Science (AREA)
  • Textile Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Mechanical Engineering (AREA)
  • Inorganic Chemistry (AREA)
  • Robotics (AREA)
  • Moulding By Coating Moulds (AREA)
  • Laminated Bodies (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)

Abstract

1. Способ изготовления конструктивного компонента для аэрокосмической техники, содержащий следующие этапы, на которых: ! производят подачу полотна с двухосным расположением армирующих элементов, содержащего структуру, выполненную из металла и предварительно пропитанную смоляной матрицей; ! выкладывают полотно с двухосным расположением армирующих элементов на ламинаторе посредством лентоукладочной машины; и ! производят отверждение полотна с двухосным расположением армирующих элементов для формирования конструктивного компонента. ! 2. Способ по п.1, отличающийся тем, что производят перемещение укладчика лентоукладочной машины вдоль нескольких осей, в частности, способом числового программного управления. ! 3. Способ по п.1 или 2, отличающийся тем, что выкладку полотна с двухосным расположением армирующих элементов производят в направлениях различных осей относительно ламинатора. ! 4. Способ по п.1, отличающийся тем, что выкладывают друг на друга несколько слоев полотна с одноосным расположением армирующих элементов и/или с двухосным расположением армирующих элементов. ! 5. Способ по п.4, отличающийся тем, что поверх, между и/или снизу полотен с одноосным расположением армирующих элементов и/или с двухосным расположением армирующих элементов укладывают, по меньшей мере, один слой CFRP препрега, в частности, при помощи лентоукладочной машины и/или дополнительной лентоукладочной машины. ! 6. Способ по п.1, отличающийся тем, что производят, посредством лентоукладочной машины, выкладку полотна с одноосным расположением армирующих элементов на конструктивный компонент, в частности, выполненный из алюминия. ! 7. Сп

Claims (8)

1. Способ изготовления конструктивного компонента для аэрокосмической техники, содержащий следующие этапы, на которых:
производят подачу полотна с двухосным расположением армирующих элементов, содержащего структуру, выполненную из металла и предварительно пропитанную смоляной матрицей;
выкладывают полотно с двухосным расположением армирующих элементов на ламинаторе посредством лентоукладочной машины; и
производят отверждение полотна с двухосным расположением армирующих элементов для формирования конструктивного компонента.
2. Способ по п.1, отличающийся тем, что производят перемещение укладчика лентоукладочной машины вдоль нескольких осей, в частности, способом числового программного управления.
3. Способ по п.1 или 2, отличающийся тем, что выкладку полотна с двухосным расположением армирующих элементов производят в направлениях различных осей относительно ламинатора.
4. Способ по п.1, отличающийся тем, что выкладывают друг на друга несколько слоев полотна с одноосным расположением армирующих элементов и/или с двухосным расположением армирующих элементов.
5. Способ по п.4, отличающийся тем, что поверх, между и/или снизу полотен с одноосным расположением армирующих элементов и/или с двухосным расположением армирующих элементов укладывают, по меньшей мере, один слой CFRP препрега, в частности, при помощи лентоукладочной машины и/или дополнительной лентоукладочной машины.
6. Способ по п.1, отличающийся тем, что производят, посредством лентоукладочной машины, выкладку полотна с одноосным расположением армирующих элементов на конструктивный компонент, в частности, выполненный из алюминия.
7. Способ по п.5, отличающийся тем, что подачу полотна с одноосным расположением армирующих элементов и/или с двухосным расположением армирующих элементов и/или слоя CFRP препрега в лентоукладочную машину осуществляют посредством питателя в соответствии с потребностью.
8. Способ по одному из пп.4-7, отличающийся тем, что подачу полотна с одноосным расположением армирующих элементов и/или с двухосным расположением армирующих элементов осуществляют из рулонов.
RU2009102192A 2006-08-01 2007-07-10 Способ изготовления конструктивного компонента для авиационно-космических летательных аппаратов RU2438876C2 (ru)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
US83465006P 2006-08-01 2006-08-01
DE200610035847 DE102006035847B4 (de) 2006-08-01 2006-08-01 Strukturanordnung sowie Verfahren zum Herstellen eines Bauteils für die Luft-und Raumfahrt
DE102006035847.3 2006-08-01
US60/834,650 2006-08-01

Publications (2)

Publication Number Publication Date
RU2009102192A true RU2009102192A (ru) 2010-09-10
RU2438876C2 RU2438876C2 (ru) 2012-01-10

Family

ID=38921848

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2009102192A RU2438876C2 (ru) 2006-08-01 2007-07-10 Способ изготовления конструктивного компонента для авиационно-космических летательных аппаратов

Country Status (9)

Country Link
US (1) US8709188B2 (ru)
EP (1) EP2046570B1 (ru)
JP (1) JP4940301B2 (ru)
CN (1) CN101500796B (ru)
BR (1) BRPI0715080A2 (ru)
CA (1) CA2654248A1 (ru)
DE (1) DE102006035847B4 (ru)
RU (1) RU2438876C2 (ru)
WO (1) WO2008015082A1 (ru)

Families Citing this family (33)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8206823B2 (en) * 2008-04-14 2012-06-26 The Boeing Company System and method for fabrication of integrated lightning strike protection material
FR2934198B1 (fr) * 2008-07-24 2012-12-21 Eads Europ Aeronautic Defence Pli et procede de metallisation d'une piece en materiau composite.
ES2568778T3 (es) 2009-04-17 2016-05-04 3M Innovative Properties Company Lámina de protección contra rayos con conductor estampado
BRPI1006590B1 (pt) 2009-04-17 2020-04-14 3M Innovative Properties Co revestimento de proteção contra raios
WO2010135318A2 (en) 2009-05-19 2010-11-25 Adc Acquisition Company Methods for forming a structure having a lightning strike protection
DE102009049668A1 (de) 2009-10-16 2011-04-21 Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. Ablegekopf und Verfahren zum gesteuerten Ablegen von abgelenkten Fasersträngen
GB2474897B (en) * 2009-11-02 2015-09-16 Hexcel Composites Ltd Electromagnetic hazard protector for composite materials
GB2475041A (en) * 2009-11-02 2011-05-11 Hexcel Composites Ltd Electromagnetic hazard protector for composite materials
DE102009055912A1 (de) 2009-11-27 2011-06-09 Thüringisches Institut für Textil- und Kunststoff-Forschung e.V. Verfahren zur kontinuierlichen Herstellung von Stapelfasergelegen aus endlich langen Verstärkungsfasern mit gerichteter Faserorientierung
DE102010015027B4 (de) * 2010-04-13 2011-11-24 Deutsches Zentrum für Luft- und Raumfahrt e.V. Faser-Legevorrichtung
FR2958575B1 (fr) * 2010-04-13 2013-03-15 Airbus Operations Sas Procede et dispositif pour la fabrication automatisee de preformes seche.
GB201018706D0 (en) 2010-11-05 2010-12-22 Hexcel Composites Ltd Improvements in composite materials
GB2487050A (en) 2011-01-04 2012-07-11 Vestas Wind Sys As Automated techniques for manufacturing fibrous panels
DE102011107444A1 (de) * 2011-07-08 2013-01-10 Institut Für Verbundwerkstoffe Gmbh Verbundwerkstoff, sowie Bauteil aus einem solchen Verbundwerkstoff
UA99418C2 (en) * 2011-10-26 2012-08-10 Владимир Владимирович Князев Multilayered lightning protection material
DE102011086101A1 (de) * 2011-11-10 2013-05-16 Airbus Operations Gmbh Verfahren zur automatisierten Herstellung eines Faserverbundbauteils mit integriertem Blitzschutz sowie Faserverbundbauteil
FR2985215B1 (fr) 2011-12-28 2014-09-19 Saint Gobain Performance Plast Revetements polymeres deposes sur des substrats par des techniques de projection thermique
GB2503864B (en) * 2012-03-08 2014-09-03 Hexcel Composites Ltd Composite material for automated lay-up
EP2832773A4 (en) * 2012-03-27 2015-11-18 Mitsubishi Heavy Ind Ltd STRUCTURAL MATERIAL FOR STRUCTURE
US9205605B2 (en) * 2012-04-25 2015-12-08 Textron Innovations Inc. Multi-function detection liner for manufacturing of composites
EP2743064B1 (en) 2012-12-14 2016-09-14 Airbus Operations GmbH Lightning strike protection means and fibre composite component
DE102013021672A1 (de) * 2013-12-19 2015-06-25 Audi Ag Verfahren zur Herstellung eines Hybridbauteils
CN104108187B (zh) * 2014-06-18 2016-08-24 际华三五零二职业装有限公司 一种由防弹头盔自动铺片机的取送大料片装置和模具组成的机构
CN104097333B (zh) * 2014-06-18 2016-06-22 际华三五零二职业装有限公司 一种由防弹头盔自动铺片机的取送小料片装置和模具组成的机构
RU2600057C1 (ru) * 2015-07-01 2016-10-20 Наби Магомедаминович Абдулов Способ контактного формирования изделия из композиционного материала
US10059067B2 (en) * 2016-01-18 2018-08-28 Fives Machining Systems, Inc. Small 4-axis fiber placement machine
GB2549113A (en) 2016-04-05 2017-10-11 Rolls Royce Plc Composite bodies and their manufacture
CN106181408B (zh) * 2016-08-25 2019-04-12 西安爱邦电磁技术有限责任公司 一种一体成型防雷网及其制备装置及制备方法
JP7161989B2 (ja) 2016-09-27 2022-10-27 スリーエム イノベイティブ プロパティズ カンパニー 保護フィルム
DE102017215153B4 (de) 2017-08-30 2021-08-26 M & A - Dieterle GmbH Maschinen- und Apparatebau Handführungsvorrichtung
EP3480008B1 (de) * 2017-11-03 2022-01-05 Bucher Leichtbau AG Leichtbauteil
EP3862170B1 (en) * 2018-10-05 2023-09-27 Fukui Prefectural Government Automatic layering method and device for thin tape
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

Family Cites Families (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3577297A (en) * 1969-01-27 1971-05-04 Rohr Corp Taping apparatus and method
SU956286A1 (ru) 1981-03-23 1982-09-07 Экспериментальное Проектно-Конструкторское И Технологическое Бюро "Стройпластик" Устройство дл изготовлени армированных пленочных изделий из полимерных материалов
US4556592A (en) 1981-09-25 1985-12-03 The Boeing Company Conductive joint seals for composite aircraft
US4707212A (en) 1986-04-28 1987-11-17 The United States Of America As Represented By The Secretary Of The Air Force Automated tape laying machine for composite structures
IL96489A0 (en) 1989-12-06 1991-08-16 Du Pont Method for laying down tapes
US6086975A (en) 1991-01-16 2000-07-11 The Boeing Company Lighting protection for electrically conductive or insulating skin and core for honeycomb structure
US5370921A (en) * 1991-07-11 1994-12-06 The Dexter Corporation Lightning strike composite and process
US5352306A (en) 1993-05-27 1994-10-04 Cincinnati Milacron Inc. Tape laying apparatus and method
JPH08161883A (ja) 1994-11-30 1996-06-21 Mitsubishi Electric Corp 半導体記憶装置
DE19649617A1 (de) 1996-11-29 1998-06-04 Henniges Elastomer Kunststoff Verfahren zur Herstellung einer Verbindung eines Bauteils mit einem Bauelement
DE19737966A1 (de) 1997-08-30 1998-08-06 Daimler Benz Ag Klebverbindung zwischen zwei Bauteilen
NL1007018C2 (nl) 1997-09-11 1999-03-12 Hollandse Signaalapparaten Bv Vezel-kunststof composiet lichaam voor electromagnetische afscherming, voorzien van een elektrische contactstrip.
US5968445A (en) * 1998-01-05 1999-10-19 The Boeing Company Method and apparatus for curing large composite panels
DE60144380D1 (de) * 2000-07-28 2011-05-19 Hypercar Inc Verfahren und ausrüstung zur herstellung fortschrittlicher kompositstrukturen
US6992027B1 (en) * 2000-11-13 2006-01-31 Hexcel Composites Ltd Composite panel with fire resistant face sheets
US7014143B2 (en) * 2002-10-11 2006-03-21 The Boeing Company Aircraft lightning strike protection and grounding technique
US7867621B2 (en) * 2003-09-30 2011-01-11 The Boeing Company Wide area lightning diverter overlay
US7063118B2 (en) * 2003-11-20 2006-06-20 Adc Acquisition Company Composite tape laying apparatus and method
US7527222B2 (en) * 2004-04-06 2009-05-05 The Boeing Company Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections
US20050238892A1 (en) * 2004-04-22 2005-10-27 The Boeing Company Backing film and method for ply materials
EP1756206A2 (en) * 2004-05-14 2007-02-28 Cytec Technology Corp. Self-adhesive prepreg
CA2581042C (en) * 2004-09-24 2013-11-19 Itochu Corporation Thin ply laminates
GB2421926B (en) * 2005-01-10 2010-03-10 Short Brothers Plc Fibre metal reinforced composite structure
JP2006219078A (ja) * 2005-02-14 2006-08-24 Honda Motor Co Ltd 航空機用複合体及び航空機の複合体構造部の製造方法
US20070141927A1 (en) 2005-12-21 2007-06-21 Brown Arlene M Method and system for exterior protection of an aircraft
US8206823B2 (en) * 2008-04-14 2012-06-26 The Boeing Company System and method for fabrication of integrated lightning strike protection material

Also Published As

Publication number Publication date
CA2654248A1 (en) 2008-02-07
EP2046570B1 (en) 2018-09-05
WO2008015082A1 (en) 2008-02-07
CN101500796B (zh) 2016-04-27
US8709188B2 (en) 2014-04-29
US20090269596A1 (en) 2009-10-29
EP2046570A1 (en) 2009-04-15
BRPI0715080A2 (pt) 2013-04-09
DE102006035847A1 (de) 2008-02-14
CN101500796A (zh) 2009-08-05
DE102006035847B4 (de) 2009-11-19
RU2438876C2 (ru) 2012-01-10
JP4940301B2 (ja) 2012-05-30
JP2009545468A (ja) 2009-12-24

Similar Documents

Publication Publication Date Title
RU2009102192A (ru) Способ изготовления конструктивного компонента для авиационно-космических летательных аппаратов
Hou et al. 3D printed continuous fibre reinforced composite corrugated structure
Mills Automation of carbon fibre preform manufacture for affordable aerospace applications
US11260566B2 (en) Methods to increase structural performance, strength and durability of fabric-reinforced composite materials by pre-stressing
US8535784B2 (en) Contoured composite parts
KR101699523B1 (ko) 복합재료의 다차원 직물 성형기
RU2388599C2 (ru) Устройство для изготовления с использованием tfp-технологии волокнистой заготовки, имеющей, по существу, произвольную геометрию поверхности
EP1342544B1 (en) Moulding material
US7261930B2 (en) Moulding materials
US8771567B2 (en) Process for producing fibre preforms
Kim et al. Limitations of fibre placement techniques for variable angle tow composites and their process-induced defects
WO1998010128A1 (en) Improved warp/knit reinforced structural fabric
US11286592B2 (en) Method for producing unidirectional hybrid-braided fabrics
CN105431286A (zh) 具有通过受控纤维铺放生产的孔图案的复合材料层压板
Shang et al. Controllable inter-line bonding performance and fracture patterns of continuous fiber reinforced composites by sinusoidal-path 3D printing
US20100316857A1 (en) Reinforcing Material for the Local Reinforcement of a Component Formed With a Composite Material, and Method
JP2013512351A (ja) 指向性の繊維配向を有する有限長補強繊維からステープルファイバレイドファブリックを連続式に製造する方法
US20180044849A1 (en) Method and Apparatus of Making Pipes and Panels Using a Treated Fiber Thread to Weave, Braid or Spin Products
CN202115036U (zh) 一种多轴向线束增强的热塑性预固结片材
JP5847033B2 (ja) 炭素繊維ステッチ基材、およびそれを用いたウエット・プリプレグ
EP3126133A1 (en) Systems and methods of producing a structural and non-structural homogeneous and hybrid composite panels, prepregs, hand layup panels with "basalt" fiber, various composite materials, and additives
JP2020525587A (ja) 形状記憶合金ワイヤを含む材料及びこの材料の製造方法
JP2015030950A (ja) ステッチ基材およびそれを用いた繊維強化プラスチック
JP2007152672A (ja) ３次元繊維強化樹脂複合材及び３次元織物
CN102555316B (zh) 具有高抗屈曲能力的纤维织物及具有高抗屈曲能力的纤维复合材料制件的制备方法

Legal Events

Date Code Title Description
TK4A Correction to the publication in the bulletin (patent)

Free format text: AMENDMENT TO CHAPTER -FG4A- IN JOURNAL: 1-2012

MM4A The patent is invalid due to non-payment of fees

Effective date: 20150711