AU2001261508A1 - Self-adhesive prepreg face sheets for sandwich panels - Google Patents

Self-adhesive prepreg face sheets for sandwich panels

Info

Publication number
AU2001261508A1
AU2001261508A1 AU2001261508A AU6150801A AU2001261508A1 AU 2001261508 A1 AU2001261508 A1 AU 2001261508A1 AU 2001261508 A AU2001261508 A AU 2001261508A AU 6150801 A AU6150801 A AU 6150801A AU 2001261508 A1 AU2001261508 A1 AU 2001261508A1
Authority
AU
Australia
Prior art keywords
prepreg
resin
self
sandwich panels
face sheets
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.)
Abandoned
Application number
AU2001261508A
Inventor
Philippe D. Christou
Ligui Zhou
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hexcel Corp
Original Assignee
Hexcel Corp
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
Priority claimed from US09/573,760 external-priority patent/US6440257B1/en
Application filed by Hexcel Corp filed Critical Hexcel Corp
Publication of AU2001261508A1 publication Critical patent/AU2001261508A1/en
Abandoned legal-status Critical Current

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
    • B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/14—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers
    • B32B37/146—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers whereby one or more of the layers is a honeycomb structure
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D24/00—Producing articles with hollow walls
    • B29D24/002—Producing articles with hollow walls formed with structures, e.g. cores placed between two plates or sheets, e.g. partially filled
    • B29D24/005—Producing articles with hollow walls formed with structures, e.g. cores placed between two plates or sheets, e.g. partially filled the structure having joined ribs, e.g. honeycomb
    • 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
    • B32B3/00—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
    • 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
    • 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
    • Y10T156/1002—Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina
    • Y10T156/1025—Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina to form undulated to corrugated sheet and securing to base with parts of shaped areas out of contact
    • 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.]
    • Y10T442/30—Woven fabric [i.e., woven strand or strip material]

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Laminated Bodies (AREA)
  • Reinforced Plastic Materials (AREA)

Abstract

Resin compositions are provided which are used in combination with fibers to form self-adhesive prepreg sheets that are applied to core materials to form sandwich panels. The prepreg resin includes a thermoset resin, a curing agent and a viscosity control agent. The prepreg resin further includes certain thermoplastic particles which are used to control the flow characteristics of the prepreg resin and the formation of fillets during bonding of the prepreg to the core material.
AU2001261508A 2000-05-18 2001-05-11 Self-adhesive prepreg face sheets for sandwich panels Abandoned AU2001261508A1 (en)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
US09573760 2000-05-18
US09/573,760 US6440257B1 (en) 2000-05-18 2000-05-18 Self-adhesive prepreg face sheets for sandwich panels
US09/795,177 US6508910B2 (en) 2000-05-18 2001-02-27 Self-adhesive prepreg face sheet for sandwich panels
US09795177 2001-02-27
PCT/US2001/015389 WO2001087583A2 (en) 2000-05-18 2001-05-11 Self-adhesive prepreg facesheets for sandwich panels

Publications (1)

Publication Number Publication Date
AU2001261508A1 true AU2001261508A1 (en) 2001-11-26

Family

ID=27076189

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2001261508A Abandoned AU2001261508A1 (en) 2000-05-18 2001-05-11 Self-adhesive prepreg face sheets for sandwich panels

Country Status (7)

Country Link
US (2) US6508910B2 (en)
EP (1) EP1303570B1 (en)
AT (1) ATE357332T1 (en)
AU (1) AU2001261508A1 (en)
DE (1) DE60127411T2 (en)
ES (1) ES2284649T3 (en)
WO (1) WO2001087583A2 (en)

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JP4175894B2 (en) * 2001-02-27 2008-11-05 ヘクセル コーポレイション Adhesive prepreg sheet for sandwich panels
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TW561102B (en) * 2001-10-22 2003-11-11 Hrl Lab Llc Preparing composites by using resins
US20050123717A1 (en) * 2003-12-08 2005-06-09 Shen Shyan B. Sealing of honeycomb core and the honeycomb core assembly made with the same
FR2866905B1 (en) * 2004-02-27 2008-04-04 Eurocopter France FABRIC PREIMPREGNATED BY TWO DISTINCT THERMOSETTING MATRICES
EP1724306A4 (en) * 2004-03-02 2009-04-01 Toray Industries Epoxy resin composition for fiber-reinforced composite material, prepreg and fiber-reinforced composite material
US7988809B2 (en) * 2004-09-01 2011-08-02 Hexcel Corporation Aircraft floor and interior panels using edge coated honeycomb
US7581366B2 (en) 2004-09-01 2009-09-01 Hexcel Corporation Aircraft floor panels using edge coated honeycomb
US7550190B2 (en) * 2004-09-01 2009-06-23 Hexcel Corporation Rubber-modified edge coating for honeycomb used in panels with composite face sheets
US7938922B2 (en) * 2004-09-01 2011-05-10 Hexcel Corporation Edge coating for honeycomb used in panels with composite face sheets
US7507461B2 (en) * 2004-09-01 2009-03-24 Hexcel Corporation Edge coating for honeycomb used in panels with composite face sheets
US20060182949A1 (en) 2005-02-17 2006-08-17 3M Innovative Properties Company Surfacing and/or joining method
US20060292375A1 (en) * 2005-06-28 2006-12-28 Martin Cary J Resin compositions with high thermoplatic loading
DE102005048156B9 (en) * 2005-10-06 2010-08-12 Dorma Gmbh + Co. Kg Mobile partition
GB2436106B (en) * 2006-01-21 2011-10-19 Advanced Composites Group Ltd Resinous materials, articles made therewith and methods of producing same
US7695797B2 (en) * 2006-06-27 2010-04-13 Hexcel Corporation Corrosion resistant honeycomb
GB0619401D0 (en) * 2006-10-02 2006-11-08 Hexcel Composites Ltd Composite materials with improved performance
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GB2464539B (en) * 2008-10-20 2014-01-08 Hexcel Composites Ltd Composite Materials with Improved Sandability
ITMI20071448A1 (en) * 2007-07-18 2009-01-19 Alenia Aermacchi Spa PROCEDURE FOR THE REALIZATION OF A SOUND ABSORBING PANEL FOR VEHICLES
US8946322B2 (en) 2008-04-14 2015-02-03 Hexcel Composites Ltd Thermosetting resin containing irradiated thermoplastic toughening agent
EP2287236B1 (en) * 2008-05-21 2017-07-26 Toray Industries, Inc. Method for producing polymer fine particle
WO2013055968A1 (en) 2011-10-12 2013-04-18 Hunter Douglas Industries Switzerland Gmbh Resin panels with embedded structured-cores and methods of making the same
CA2761878A1 (en) * 2009-05-13 2010-11-18 3Form, Inc. Structured-core laminate panels and methods of forming the same
US9074091B2 (en) 2009-09-25 2015-07-07 The Yokohama Rubber Co., Ltd. Thermosetting resin composition, thermosetting resin composition for fiber-reinforced composite material, prepared using the same, and honeycomb sandwich panel
US8597455B1 (en) * 2009-10-02 2013-12-03 Metacomb, Inc. Translucent building material comprising corrugated cardboard
WO2012046088A1 (en) * 2009-10-07 2012-04-12 Hexcel Composites, Ltd. Thermosetting resin adhesive containing irradiated thermoplastic toughening agent
DE102009059805A1 (en) * 2009-12-21 2011-06-22 Daimler AG, 70327 Motor vehicle component with a sandwich structure and method for its production
GB2477091A (en) * 2010-01-20 2011-07-27 Hexcel Composites Ltd Structureal laminate comprising face sheets, core and open-structured sheet
CN102741045B (en) * 2010-02-04 2015-12-02 贝尔直升机泰克斯特龙公司 Composite core material and preparation method thereof
US8453793B1 (en) 2012-04-12 2013-06-04 M.C. Gill Corporation Accoustic fabrication system
US9187636B2 (en) 2012-08-26 2015-11-17 Hexcel Corporation Composite material with polyamide particle mixtures
US9072184B2 (en) * 2012-10-24 2015-06-30 The Boeing Company Carbon fiber spacecraft panel with integral metallic foil power return
US20150028247A1 (en) 2013-07-23 2015-01-29 Sabic Innovative Plastics Ip B.V. Rigid foam and associated article and method
US9175160B2 (en) 2013-08-28 2015-11-03 Sabic Global Technologies B.V. Blend of poly(phenylene ether) particles and polyoxymethylene, article thereof, and method of preparation
US9447227B2 (en) 2013-10-03 2016-09-20 Sabic Global Technologies B.V. Flexible polyurethane foam and associated method and article
US10272619B2 (en) 2014-05-19 2019-04-30 The Boeing Company Manufacture of a resin infused one-piece composite truss structure
US10316443B2 (en) * 2015-04-17 2019-06-11 Auburn University Composite braided open structure without inter-yarn bonding, and structures made therefrom
GB2543572A (en) * 2015-10-23 2017-04-26 Gordon Murray Design Ltd A component for a vehicle
CN105548214B (en) * 2015-12-04 2021-06-01 中航复合材料有限责任公司 Defect discrimination method for honeycomb core-skin connection quality optical imaging detection
US9738764B2 (en) * 2016-01-05 2017-08-22 The Boeing Company Methods, systems and apparatuses for curing epoxy-containing prepreg composite assembly
US10800129B2 (en) 2017-01-24 2020-10-13 Bell Textron Inc. Honeycomb core sandwich panels
WO2018174217A1 (en) * 2017-03-23 2018-09-27 東邦テナックス株式会社 Self-adhesive prepreg and method for producing same
US10391735B2 (en) 2017-04-07 2019-08-27 Hexcel Corporation Use of fibrous veils to reduce core crush in honeycomb sandwich structures
US11339569B2 (en) * 2017-04-18 2022-05-24 Nexgen Composites Llc Unitized construction panel
US11104113B2 (en) * 2017-04-19 2021-08-31 The Boeing Company Systems and methods for assembling elongate composite structures
CN107175837B (en) * 2017-06-22 2019-03-19 哈尔滨哈飞航空工业有限责任公司 A kind of honeycomb cladding spicing forming type method
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WO2020262483A1 (en) * 2019-06-28 2020-12-30 株式会社イノアックコーポレーション Honeycomb layered body and production method therefor

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Also Published As

Publication number Publication date
WO2001087583A3 (en) 2002-03-21
US6508910B2 (en) 2003-01-21
EP1303570A2 (en) 2003-04-23
EP1303570B1 (en) 2007-03-21
EP1303570A4 (en) 2004-05-12
DE60127411D1 (en) 2007-05-03
ATE357332T1 (en) 2007-04-15
ES2284649T3 (en) 2007-11-16
DE60127411T2 (en) 2007-11-29
US20010042593A1 (en) 2001-11-22
WO2001087583A2 (en) 2001-11-22
US20020079052A1 (en) 2002-06-27

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