GR3002178T3 - Laminate of metal sheets and continuous glass filaments-reinforced synthetic material - Google Patents

Laminate of metal sheets and continuous glass filaments-reinforced synthetic material

Info

Publication number
GR3002178T3
GR3002178T3 GR91400862T GR910400862T GR3002178T3 GR 3002178 T3 GR3002178 T3 GR 3002178T3 GR 91400862 T GR91400862 T GR 91400862T GR 910400862 T GR910400862 T GR 910400862T GR 3002178 T3 GR3002178 T3 GR 3002178T3
Authority
GR
Greece
Prior art keywords
glass filaments
poly
laminate
continuous glass
synthetic material
Prior art date
Application number
GR91400862T
Other languages
English (en)
Inventor
Laurens Boudewijn Vogelesang
Gerardus Hubertus Jo Roebroeks
Original Assignee
Akzo Nv
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 Akzo Nv filed Critical Akzo Nv
Publication of GR3002178T3 publication Critical patent/GR3002178T3/el

Links

Classifications

    • 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
    • B32B15/14—Layered products comprising a layer of metal next to a fibrous or filamentary layer
    • 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
    • B32B15/04—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
    • 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
    • B32B15/18—Layered products comprising a layer of metal comprising iron or steel
    • 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
    • B32B15/20—Layered products comprising a layer of metal comprising aluminium or copper
    • 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
    • C—CHEMISTRY; METALLURGY
    • C03—GLASS; MINERAL OR SLAG WOOL
    • C03C—CHEMICAL COMPOSITION OF GLASSES, GLAZES OR VITREOUS ENAMELS; SURFACE TREATMENT OF GLASS; SURFACE TREATMENT OF FIBRES OR FILAMENTS MADE FROM GLASS, MINERALS OR SLAGS; JOINING GLASS TO GLASS OR OTHER MATERIALS
    • C03C13/00—Fibre or filament compositions
    • 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
    • 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
    • B32B2260/04—Impregnation, embedding, or binder material
    • B32B2260/046—Synthetic resin
    • 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
    • B32B2307/00—Properties of the layers or laminate
    • B32B2307/50—Properties of the layers or laminate having particular mechanical properties
    • B32B2307/51—Elastic
    • 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
    • B32B2307/00—Properties of the layers or laminate
    • B32B2307/50—Properties of the layers or laminate having particular mechanical properties
    • B32B2307/54—Yield strength; Tensile strength
    • 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
    • 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
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
    • 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
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0081—Fuselage structures substantially made from particular materials from metallic materials
    • 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
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24942—Structurally defined web or sheet [e.g., overall dimension, etc.] including components having same physical characteristic in differing degree
    • Y10T428/2495—Thickness [relative or absolute]
    • 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
    • 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
    • Y10T428/31681—Next to polyester, polyamide or polyimide [e.g., alkyd, glue, or nylon, etc.]
    • 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
    • Y10T442/00—Fabric [woven, knitted, or nonwoven textile or cloth, etc.]
    • Y10T442/60—Nonwoven fabric [i.e., nonwoven strand or fiber material]
    • Y10T442/654—Including a free metal or alloy constituent
    • Y10T442/656—Preformed metallic film or foil or sheet [film or foil or sheet had structural integrity prior to association with the nonwoven fabric]

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • General Chemical & Material Sciences (AREA)
  • Geochemistry & Mineralogy (AREA)
  • Materials Engineering (AREA)
  • Organic Chemistry (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Laminated Bodies (AREA)
GR91400862T 1987-10-14 1991-06-25 Laminate of metal sheets and continuous glass filaments-reinforced synthetic material GR3002178T3 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
NL8702453 1987-10-14

Publications (1)

Publication Number Publication Date
GR3002178T3 true GR3002178T3 (en) 1992-12-30

Family

ID=19850766

Family Applications (1)

Application Number Title Priority Date Filing Date
GR91400862T GR3002178T3 (en) 1987-10-14 1991-06-25 Laminate of metal sheets and continuous glass filaments-reinforced synthetic material

Country Status (8)

Country Link
US (1) US5039571A (el)
EP (1) EP0312151B1 (el)
JP (1) JP2660563B2 (el)
AT (1) ATE61970T1 (el)
CA (1) CA1306936C (el)
DE (1) DE3862185D1 (el)
ES (1) ES2022602B3 (el)
GR (1) GR3002178T3 (el)

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US5733390A (en) * 1993-10-18 1998-03-31 Ticomp, Inc. Carbon-titanium composites
US5906550A (en) * 1993-10-18 1999-05-25 Ticomp, Inc. Sports bat having multilayered shell
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US5651850A (en) * 1996-01-11 1997-07-29 The Boeing Company Method of fabricating hybrid composite structures
US5866272A (en) * 1996-01-11 1999-02-02 The Boeing Company Titanium-polymer hybrid laminates
JP4262782B2 (ja) 1997-05-28 2009-05-13 ストラクチユアル・ラミネイツ・カンパニー ラミネートの製造方法およびその方法によって得られるラミネート
US6039832A (en) * 1998-02-27 2000-03-21 The Boeing Company Thermoplastic titanium honeycomb panel
EP1244544A4 (en) * 1999-10-25 2003-01-29 Rolls Royce Corp EROSION-RESISTANT COATINGS FOR ORGANIC MATRIX COMPOSITES
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US6648273B2 (en) 2001-10-30 2003-11-18 The Boeing Company Light weight and high strength fuselage
NL1019601C2 (nl) * 2001-12-18 2003-06-30 Fokker Aerostructures Bv Werkwijze voor het vervaardigen van een laminaat alsmede gekromd product bestaande uit laminaat.
US6758924B1 (en) 2002-04-15 2004-07-06 The United States Of America As Represented By The Secretary Of The Air Force Method of repairing cracked aircraft structures
FR2844742B1 (fr) * 2002-09-25 2005-04-29 Pechiney Rhenalu Feuilles composites stratifiees aluminium-fibres de verre
US7192501B2 (en) * 2002-10-29 2007-03-20 The Boeing Company Method for improving crack resistance in fiber-metal-laminate structures
DE10330341B4 (de) * 2003-07-05 2005-09-15 Airbus Deutschland Gmbh Metallischer Schichtwerkstoff, verstärkt mit langen Basaltfasern sowie dessen Erzeugnisse
DE10360808B4 (de) * 2003-12-19 2005-10-27 Airbus Deutschland Gmbh Faserverstärkter metallischer Verbundwerkstoff
US20050142968A1 (en) * 2003-12-24 2005-06-30 The Boeing Company Translucent, flame resistant composite materials
RU2270098C1 (ru) * 2004-07-14 2006-02-20 Федеральное государственное унитарное предприятие "Всероссийский научно-исследовательский институт авиационных материалов" (ФГУП "ВИАМ") Слоистый композиционный материал и изделие, выполненное из него
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US7255916B2 (en) 2005-01-04 2007-08-14 Airbus Deutschland Gmbh Metallic layer material, reinforced with basalt fibers, as well as products made thereof
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NL1030066C2 (nl) * 2005-09-29 2007-03-30 Gtm Consulting B V Werkwijze voor het vervaardigen van een vormdeel uit een samengesteld materiaal.
EP2021238A2 (en) * 2006-05-15 2009-02-11 Alcoa Inc. Reinforced hybrid structures and methods thereof
NL2000100C2 (nl) 2006-06-13 2007-12-14 Gtm Consulting B V Laminaat uit metaalplaten en kunststof.
NL2000232C2 (nl) * 2006-09-12 2008-03-13 Gtm Consulting B V Huidpaneel voor een vliegtuigromp.
US7690164B2 (en) * 2006-12-05 2010-04-06 Lockheed Martin Corporation System, method, and apparatus for structural lug formed from a combination of metal and composite laminate materials
US20090211697A1 (en) * 2007-05-15 2009-08-27 Heinimann Markus B Reinforced hybrid structures and methods thereof
EP2085215B1 (en) * 2008-01-29 2013-03-27 GTM Holding B.V. High-toughness fiber-metal laminate
JP5392465B2 (ja) * 2008-11-25 2014-01-22 住友電気工業株式会社 マグネシウム合金部材
JP4902025B2 (ja) 2009-07-31 2012-03-21 新日本製鐵株式会社 積層鋼板
US20130316148A1 (en) 2010-11-29 2013-11-28 Gtm-Advanced Products B.V. Metal sheet-fiber reinforced composite laminate
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WO2013124001A1 (en) 2012-02-25 2013-08-29 Adamco Ag Self stabilizing halloysite aluminum metal matrix compound
EP2821226B1 (en) 2012-03-02 2018-12-26 Avic Composite Corporation Ltd. Composite material containing plant fibre fabrics and preparation method thereof
CN102991009B (zh) * 2012-11-16 2015-02-11 中国航空工业集团公司北京航空材料研究院 一种层间增韧的碳纤维-金属层合板
KR101455834B1 (ko) * 2013-04-01 2014-11-03 채경남 그래핀의 피에조 저항 특성을 이용한 스마트 복합재
CN105522788B (zh) 2014-11-24 2017-11-21 比亚迪股份有限公司 一种纤维金属层合板及其制备方法
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US11273622B2 (en) 2016-12-14 2022-03-15 The Boeing Company Stiffening elements that comprise integral current flowpaths
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Also Published As

Publication number Publication date
EP0312151A1 (en) 1989-04-19
DE3862185D1 (de) 1991-05-02
CA1306936C (en) 1992-09-01
JPH01136736A (ja) 1989-05-30
EP0312151B1 (en) 1991-03-27
JP2660563B2 (ja) 1997-10-08
ATE61970T1 (de) 1991-04-15
US5039571A (en) 1991-08-13
ES2022602B3 (es) 1991-12-01

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