ES2188490T3 - Procedimiento de fabricacion de un panel sandwich de material compuesto y el panel obtenido por el mismo. - Google Patents

Procedimiento de fabricacion de un panel sandwich de material compuesto y el panel obtenido por el mismo.

Info

Publication number
ES2188490T3
ES2188490T3 ES00402567T ES00402567T ES2188490T3 ES 2188490 T3 ES2188490 T3 ES 2188490T3 ES 00402567 T ES00402567 T ES 00402567T ES 00402567 T ES00402567 T ES 00402567T ES 2188490 T3 ES2188490 T3 ES 2188490T3
Authority
ES
Spain
Prior art keywords
mold
dry
panel
barrier
covers
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
Application number
ES00402567T
Other languages
English (en)
Inventor
Alain Fournier
Nathalie Duret
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.)
Airbus Operations SAS
Original Assignee
Airbus Operations SAS
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 Airbus Operations SAS filed Critical Airbus Operations SAS
Application granted granted Critical
Publication of ES2188490T3 publication Critical patent/ES2188490T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • B29C70/06—Fibrous reinforcements only
    • B29C70/08—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers
    • B29C70/088—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers and with one or more layers of non-plastics material or non-specified material, e.g. supports
    • 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
    • B29C70/40—Shaping or impregnating by compression not applied
    • B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/46—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
    • B29C70/48—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs and impregnating the reinforcements in the closed mould, e.g. resin transfer moulding [RTM], e.g. by vacuum
    • 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
    • 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
    • Y10T428/23—Sheet including cover or casing
    • Y10T428/233—Foamed or expanded material encased
    • 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
    • Y10T428/23—Sheet including cover or casing
    • Y10T428/234—Sheet including cover or casing including elements cooperating to form cells
    • Y10T428/236—Honeycomb type cells extend perpendicularly to nonthickness layer
    • 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.]
    • Y10T428/24149—Honeycomb-like
    • Y10T428/24157—Filled honeycomb cells [e.g., solid substance in cavities, etc.]

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Laminated Bodies (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)

Abstract

Procedimiento de fabricación de un panel sándwich de material compuesto, que se caracteriza porque comprende las etapas siguientes: - colocación, en un molde, de un conjunto que comprende un alma (10) de celdas abiertas, una película (12) de material intumescente que recubre cada una de las caras del alma, un tejido barrera seco (14) que recubre cada una de las películas (12), y un revestimiento (16) de fibras secas que recubre cada uno de los tejidos barrera, siendo los citados tejidos barrera estancos a una espuma (12a) susceptible de ser obtenida durante la polimerización de las citadas películas (12), y mojables por una resina susceptible de ser inyectada en el molde; - cierre del molde; - puesta bajo presión y calentamiento del molde, según un ciclo de expansión y de polimerización del material intumescente (12), con el fin de formar la citada espuma (12), obturando las celdas del alma (10) por cada una de sus caras, sin impregnar los tejidos barrera secos (14); - puesta bajo vacío delmolde, e inyección de la citada resina en éste, con el fin de impregnar los revestimientos (16) de fibras secas y los tejidos barrera secos (14); - ejecución de un ciclo de polimerización de la resina; - desmoldeo del panel así obtenido.
ES00402567T 1999-09-21 2000-09-18 Procedimiento de fabricacion de un panel sandwich de material compuesto y el panel obtenido por el mismo. Expired - Lifetime ES2188490T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9911766A FR2798618B1 (fr) 1999-09-21 1999-09-21 Procede de fabrication d'un panneau sandwich en materiau composite, et panneau ainsi obtenu

Publications (1)

Publication Number Publication Date
ES2188490T3 true ES2188490T3 (es) 2003-07-01

Family

ID=9550062

Family Applications (1)

Application Number Title Priority Date Filing Date
ES00402567T Expired - Lifetime ES2188490T3 (es) 1999-09-21 2000-09-18 Procedimiento de fabricacion de un panel sandwich de material compuesto y el panel obtenido por el mismo.

Country Status (5)

Country Link
US (2) US6679969B1 (es)
EP (1) EP1086801B1 (es)
DE (1) DE60001033T2 (es)
ES (1) ES2188490T3 (es)
FR (1) FR2798618B1 (es)

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US6557702B1 (en) * 2001-10-31 2003-05-06 Skb Corporation Golf club travel bag
US7226559B2 (en) * 2000-12-08 2007-06-05 Toyota Motor Sales, U.S.A., Inc. Method for molding structures
JP4663174B2 (ja) * 2001-08-03 2011-03-30 富士重工業株式会社 ハニカムサンドイッチ構造複合材の成形方法
FR2839986B1 (fr) * 2002-05-21 2004-08-20 Chomarat Composites Renfort fibreux a fonction de barriere pour la realisation de pieces composites et pieces composites en faisant application
GB2401900B (en) * 2003-05-23 2005-03-30 Acell Holdings Ltd Precursors
US7294220B2 (en) * 2003-10-16 2007-11-13 Toyota Motor Sales, U.S.A., Inc. Methods of stabilizing and/or sealing core material and stabilized and/or sealed core material
US7284726B2 (en) * 2004-02-17 2007-10-23 Sikorsky Aircraft Corporation Self extinguishing composite primary structure
US8070994B2 (en) * 2004-06-18 2011-12-06 Zephyros, Inc. Panel structure
US7416401B2 (en) * 2005-06-13 2008-08-26 The Boeing Company Lightweight composite fairing bar and method for manufacturing the same
US8034989B2 (en) * 2005-08-26 2011-10-11 Knupp Stephen L Energy generation process
DE102005048156B9 (de) * 2005-10-06 2010-08-12 Dorma Gmbh + Co. Kg Mobile Trennwand
ES2317436T3 (es) * 2006-09-07 2009-04-16 Euro-Composites S.A. Procedimiento para fabricar un componente de sandwich con un nucleo de nido de abeja.
US20080086965A1 (en) * 2006-10-16 2008-04-17 Metz Timothy W Composite structural panel
US20110223372A1 (en) * 2006-10-16 2011-09-15 Csp Systems, Inc. Non-Planar Composite Structural Panel
US20090155524A1 (en) 2007-12-13 2009-06-18 Rapp Robert A Composite panel and method of manufacturing the same
US8215585B2 (en) * 2008-05-13 2012-07-10 The Boeing Company Impact resistant core
US8286919B2 (en) * 2008-05-13 2012-10-16 The Boeing Company Impact resistant composite structures
RU2402663C2 (ru) * 2008-11-17 2010-10-27 Александр Александрович Артёменко Многослойный конструкционный материал и способ его получения
AU2009245873A1 (en) * 2008-12-10 2010-07-01 Ig6 Pty Ltd Fire containment devices and components therefor
US20120153242A1 (en) * 2009-06-24 2012-06-21 Zephyros, Inc. Insulation materials
IT1396049B1 (it) * 2009-09-24 2012-11-09 Magaldi Ind Srl Sistema di estrazione e trasporto di ceneri leggere mediante trasportatore a nastro in acciaio.
DE102010035493A1 (de) * 2010-08-26 2012-03-01 Airbus Operations Gmbh Verfahren sowie Herstellvorrichtung zur Herstellung eines Faserverbund-Sandwichbauteils
JP5972376B2 (ja) * 2011-08-17 2016-08-17 ビー イー エアロスペイス，インク． 埋込みインサートを備えた高強度航空機インテリアパネル
DE202012006756U1 (de) 2012-07-15 2012-08-09 Gunter Tannhäuser Brandschutz-Leichtbauplatte
WO2014055991A1 (en) * 2012-10-05 2014-04-10 Leonard Michael R Layered insulation system
US9597826B2 (en) 2012-10-30 2017-03-21 Bell Helicopter Textron Inc. Method of repairing, splicing, joining, machining, and stabilizing honeycomb core using pourable structural foam and a structure incorporating the same
US9015941B2 (en) 2012-10-30 2015-04-28 Bell Helicopter Textron Inc. Method of repairing honeycomb core using pourable structural foam
US9149999B2 (en) * 2012-10-30 2015-10-06 Bell Helicopter Textron Inc. Method of repairing, splicing, joining, machining, and stabilizing honeycomb core using pourable structural foam and a structure incorporating the same
US9333684B2 (en) 2012-10-30 2016-05-10 Bell Helicopter Textron Inc. Method of repairing, splicing, joining, machining, and stabilizing honeycomb core using pourable structural foam and a structure incorporating the same
EP3024642B1 (en) 2013-07-26 2020-04-22 Learjet Inc. Composite material incorporating water ingress barrier
EP2894136B1 (en) 2014-01-08 2019-12-04 The Boeing Company Improved method of making fire resistant sustainable aircraft interior panels
GB2533306A (en) * 2014-12-15 2016-06-22 Airbus Operations Ltd Sandwich Panel
BR112017016240A2 (pt) 2015-01-30 2018-03-27 Zephyros Inc composição
WO2016126595A1 (en) 2015-02-03 2016-08-11 Zephyros, Inc. One part epoxy-based composition
FR3032908A1 (fr) * 2015-02-24 2016-08-26 Airbus Defence & Space Sas Panneau composite renforce
US9845596B2 (en) 2015-09-29 2017-12-19 Awi Licensing Llc Ceiling system
GB2554870A (en) * 2016-10-06 2018-04-18 Forward Composites Fabricating a composite article
FR3089854B1 (fr) 2018-12-18 2022-02-04 Saint Gobain Performance Plastics France Procede de preparation d’un materiau composite sous forme de sandwich
CN114072280A (zh) * 2019-06-28 2022-02-18 井上株式会社 蜂窝层叠体及其制造方法
EP4122693A1 (en) * 2021-07-21 2023-01-25 Airbus Operations, S.L.U. Method for manufacturing a sandwich panel with improved impact and damping behaviours
US11623428B2 (en) 2021-07-30 2023-04-11 United States Government As Represented By The Secretary Of The Army Load-bearing composite platform

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WO1984004727A1 (en) * 1983-05-27 1984-12-06 Boeing Co Lightweight, fire-retardant structural panel
US5338594A (en) * 1992-02-07 1994-08-16 Hexcel Corporation Foam filled honeycomb and methods for their production
US5569508A (en) * 1995-01-03 1996-10-29 The Boeing Company Resin transfer molding with honeycomb core and core filler
US5567499A (en) 1995-01-03 1996-10-22 The Boeing Company Resin transfer molding in combination with honeycomb core
FR2740383B1 (fr) 1995-10-27 1998-01-16 Aerospatiale Procede de fabrication d'un panneau en materiau composite avec moulage par transfert de resine
US5604010A (en) * 1996-01-11 1997-02-18 Hartz; Dale E. Composite honeycomb sandwich structure

Also Published As

Publication number Publication date
FR2798618B1 (fr) 2002-05-03
EP1086801B1 (fr) 2002-12-18
DE60001033D1 (de) 2003-01-30
EP1086801A1 (fr) 2001-03-28
FR2798618A1 (fr) 2001-03-23
DE60001033T2 (de) 2003-09-25
US6679969B1 (en) 2004-01-20
US20040146687A1 (en) 2004-07-29

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