DE602005021390D1 - Hren dafür sowie verfahren zur herstellung einer sandwich-struktur mit dem einsatz - Google Patents

Hren dafür sowie verfahren zur herstellung einer sandwich-struktur mit dem einsatz

Info

Publication number
DE602005021390D1
DE602005021390D1 DE602005021390T DE602005021390T DE602005021390D1 DE 602005021390 D1 DE602005021390 D1 DE 602005021390D1 DE 602005021390 T DE602005021390 T DE 602005021390T DE 602005021390 T DE602005021390 T DE 602005021390T DE 602005021390 D1 DE602005021390 D1 DE 602005021390D1
Authority
DE
Germany
Prior art keywords
producing
sandwich structure
sandwich
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.)
Active
Application number
DE602005021390T
Other languages
English (en)
Inventor
Georges Cahuzac
Jack Gauthier
Eric Chocheyras
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 Defence and Space SAS
Original Assignee
Astrium 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 Astrium SAS filed Critical Astrium SAS
Publication of DE602005021390D1 publication Critical patent/DE602005021390D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
    • B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
    • B29C70/24—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least three directions forming a three dimensional structure
    • 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
    • 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
    • B29C70/68—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
    • B29C70/86—Incorporated in coherent impregnated reinforcing layers, e.g. by winding
    • 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
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24033—Structurally defined web or sheet [e.g., overall dimension, etc.] including stitching and discrete fastener[s], coating or bond
DE602005021390T 2004-10-27 2005-10-21 Hren dafür sowie verfahren zur herstellung einer sandwich-struktur mit dem einsatz Active DE602005021390D1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0452462A FR2876946B1 (fr) 2004-10-27 2004-10-27 Insert en materiau composite et son procede de fabrication, et procede de realisation d'une structure sandwich comportant un tel insert
PCT/FR2005/050886 WO2006045976A1 (fr) 2004-10-27 2005-10-21 Insert en matériau composite et son procédé de fabrication, et procédé de réalisation d'une structure sandwich comportant un tel insert

Publications (1)

Publication Number Publication Date
DE602005021390D1 true DE602005021390D1 (de) 2010-07-01

Family

ID=34954136

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602005021390T Active DE602005021390D1 (de) 2004-10-27 2005-10-21 Hren dafür sowie verfahren zur herstellung einer sandwich-struktur mit dem einsatz

Country Status (8)

Country Link
US (1) US8137491B2 (de)
EP (1) EP1812224B1 (de)
JP (1) JP4769252B2 (de)
CA (1) CA2585338A1 (de)
DE (1) DE602005021390D1 (de)
ES (1) ES2346334T3 (de)
FR (1) FR2876946B1 (de)
WO (1) WO2006045976A1 (de)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102014012915A1 (de) * 2014-09-05 2016-03-10 Airbus Defence and Space GmbH Faserverbundbauteil, Klebeanordnung für Faserverbundbauteile, sowie Verfahren zur Herstellung eines Faserverbundbauteils und einer Klebeanordnung
JP2018514417A (ja) 2015-05-08 2018-06-07 ムベア カルボ テック ゲーエムベーハーＭｕｂｅａ Ｃａｒｂｏ Ｔｅｃｈ Ｇｍｂｈ 荷重適用要素および荷重適用要素の製造方法
DE102017220331A1 (de) * 2017-11-15 2019-05-16 Siemens Aktiengesellschaft Verfahren zur Herstellung eines Sandwichelements und Sandwichelement
US10968620B2 (en) 2018-10-10 2021-04-06 Raytheon Company Sandwich structure with lattice having hard points
EP4201653A1 (de) 2021-12-16 2023-06-28 Rolls-Royce plc Z-stift zur erhöhung der delaminationsresistenz

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3855174A (en) 1971-03-19 1974-12-17 Commissariat Energie Atomique Method of manufacture of composite materials consisting of carbon fibers and resin and materials thus obtained
JPS5841950A (ja) * 1981-08-31 1983-03-11 東レ株式会社 繊維強化樹脂用補強基材
FR2610951B1 (fr) 1987-02-17 1989-05-05 Aerospatiale Armature tissee pour materiau composite
US5079055A (en) * 1989-09-21 1992-01-07 Doyle Brian P Reinforcement for laminate synthetic materials
FR2753993B1 (fr) 1996-10-01 1998-11-27 Aerospatiale Structure tubulaire tressee pour piece composite, sa realisation et ses applications
FR2768076B1 (fr) * 1997-09-10 2000-08-04 Peguform France Procede de realisation d'une zone rigidifiee formant insert dans un panneau composite du type sandwich, et panneau comprenant une telle zone
DE19834772C2 (de) * 1998-08-01 2002-10-17 Inst Verbundwerkstoffe Gmbh Faser-Kunststoff-Verbund-Bauteile mit Inserts
US6450450B1 (en) * 2000-11-06 2002-09-17 The United States Of America As Represented By The Secretary Of The Navy Low cost structural fabrication that resists catastrophic failure under rapid thermal loading
FR2832738B1 (fr) * 2001-11-27 2004-02-13 Eads Launch Vehicles Dispositif de tramage pour la realisation d'armatures textiles epaisses et armatures ainsi obtenues
DE10235509A1 (de) * 2002-07-29 2004-02-12 Brucker, Andreas Faserverbund und Verfahren zur Herstellung eines Faserverbundes
DE20314187U1 (de) * 2003-09-08 2003-12-18 Roth, Matthias Alexander, Dipl.-Ing. Krafteinleitungsstelle in Kernverbunden mit in Dickenrichtung des Kernverbundes durchsetzenden Armierungselementen

Also Published As

Publication number Publication date
FR2876946A1 (fr) 2006-04-28
US20090301644A1 (en) 2009-12-10
US8137491B2 (en) 2012-03-20
EP1812224A1 (de) 2007-08-01
JP4769252B2 (ja) 2011-09-07
JP2008517808A (ja) 2008-05-29
WO2006045976A1 (fr) 2006-05-04
CA2585338A1 (fr) 2006-05-04
FR2876946B1 (fr) 2007-02-02
EP1812224B1 (de) 2010-05-19
ES2346334T3 (es) 2010-10-14

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