DK1907193T3 - Fremstillingsfremgangsmåde til armering af kernematerialer til kernesamlinger - Google Patents

Fremstillingsfremgangsmåde til armering af kernematerialer til kernesamlinger

Info

Publication number
DK1907193T3
DK1907193T3 DK06724058.0T DK06724058T DK1907193T3 DK 1907193 T3 DK1907193 T3 DK 1907193T3 DK 06724058 T DK06724058 T DK 06724058T DK 1907193 T3 DK1907193 T3 DK 1907193T3
Authority
DK
Denmark
Prior art keywords
core
reinforcing
hole
manufacturing
reinforcing structure
Prior art date
Application number
DK06724058.0T
Other languages
English (en)
Inventor
Matthias Alexander Roth
Original Assignee
Evonik Roehm Gmbh
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 Evonik Roehm Gmbh filed Critical Evonik Roehm Gmbh
Application granted granted Critical
Publication of DK1907193T3 publication Critical patent/DK1907193T3/da

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
    • B29C70/086—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 pure plastics material, e.g. foam 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
    • B29C70/04—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
    • B29C70/04—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 [3D] 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
    • Y10T156/1052—Methods of surface bonding and/or assembly therefor with cutting, punching, tearing or severing
    • Y10T156/1062—Prior to assembly
    • 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
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49801—Shaping fiber or fibered material
    • 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
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49826—Assembling or joining
    • Y10T29/49833—Punching, piercing or reaming part by surface of second part
    • 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
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49826—Assembling or joining
    • Y10T29/49833—Punching, piercing or reaming part by surface of second part
    • Y10T29/49835—Punching, piercing or reaming part by surface of second part with shaping
    • 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
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49826—Assembling or joining
    • Y10T29/49838—Assembling or joining by stringing
    • 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.]
    • Y10T428/24479—Structurally defined web or sheet [e.g., overall dimension, etc.] including variation in thickness
    • Y10T428/24612—Composite web or sheet

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Mechanical Engineering (AREA)
  • Textile Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Laminated Bodies (AREA)
  • Panels For Use In Building Construction (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Woven Fabrics (AREA)
  • Molds, Cores, And Manufacturing Methods Thereof (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
DK06724058.0T 2005-07-27 2006-04-05 Fremstillingsfremgangsmåde til armering af kernematerialer til kernesamlinger DK1907193T3 (da)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102005035681A DE102005035681A1 (de) 2005-07-27 2005-07-27 Fertigungsverfahren zur Armierung von Kernmaterialien für Kernverbunde sowie von Kernverbund-Strukturen
PCT/EP2006/003110 WO2007012353A1 (de) 2005-07-27 2006-04-05 Fertigungsverfahren zur armierung von kernmaterialien für kernverbunde sowie von kernverbund-strukturen

Publications (1)

Publication Number Publication Date
DK1907193T3 true DK1907193T3 (da) 2011-06-14

Family

ID=36609036

Family Applications (1)

Application Number Title Priority Date Filing Date
DK06724058.0T DK1907193T3 (da) 2005-07-27 2006-04-05 Fremstillingsfremgangsmåde til armering af kernematerialer til kernesamlinger

Country Status (19)

Country Link
US (1) US20080226876A1 (da)
EP (1) EP1907193B8 (da)
JP (1) JP4751448B2 (da)
KR (1) KR101319703B1 (da)
CN (1) CN101198459B (da)
AT (1) ATE500049T1 (da)
AU (1) AU2006274270B2 (da)
BR (1) BRPI0613882A2 (da)
CA (1) CA2616655C (da)
DE (2) DE102005035681A1 (da)
DK (1) DK1907193T3 (da)
ES (1) ES2361617T3 (da)
IL (1) IL186761A (da)
NZ (1) NZ563572A (da)
PL (1) PL1907193T3 (da)
RU (1) RU2419543C2 (da)
TW (1) TWI388429B (da)
WO (1) WO2007012353A1 (da)
ZA (1) ZA200800782B (da)

Families Citing this family (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7861969B2 (en) 2007-05-24 2011-01-04 The Boeing Company Shaped composite stringers and methods of making
DE102007033120A1 (de) * 2007-07-13 2009-01-15 Evonik Röhm Gmbh Verbesserte Stumpfstoßverbindungen für Kernwerkstoffe
DE102007051422A1 (de) * 2007-10-25 2009-04-30 Evonik Röhm Gmbh Zweiseiten-Einnadel-Unterfaden-Nähtechnik
US7879276B2 (en) * 2007-11-08 2011-02-01 The Boeing Company Foam stiffened hollow composite stringer
DE102007055684A1 (de) * 2007-11-21 2009-06-10 Airbus Deutschland Gmbh Vorrichtung zur Herstellung eines verstärkten Schaumwerkstoffes
DE102008006981B3 (de) * 2008-01-31 2009-06-10 Airbus Deutschland Gmbh Verfahren zum Herstellen eines Kernverbundes, insbesondere eines Kernverbundes im Luft- und Raumfahrtbereich
US8127450B2 (en) * 2008-01-31 2012-03-06 Airbus Operations Gmbh Method for producing a sandwich construction, in particular a sandwich construction for the aeronautical and aerospace fields
DE102008001826B3 (de) * 2008-05-16 2009-09-17 Airbus Deutschland Gmbh Ausschnittverstärkung für Kernverbunde sowie ein Verfahren zum Herstellen einer Ausschnittverstärkung für Kernverbunde
DE102008041788A1 (de) 2008-09-03 2010-03-11 Airbus Deutschland Gmbh Sandwichplatte mit integrierter Verstärkungsstruktur sowie Verfahren zu deren Herstellung
US8540921B2 (en) 2008-11-25 2013-09-24 The Boeing Company Method of forming a reinforced foam-filled composite stringer
US8500066B2 (en) 2009-06-12 2013-08-06 The Boeing Company Method and apparatus for wireless aircraft communications and power system using fuselage stringers
US8570152B2 (en) 2009-07-23 2013-10-29 The Boeing Company Method and apparatus for wireless sensing with power harvesting of a wireless signal
US8617687B2 (en) 2009-08-03 2013-12-31 The Boeing Company Multi-functional aircraft structures
DE102010054935B4 (de) * 2010-12-17 2013-11-28 Daimler Ag Karosseriemodulbauteil
AU2013295249B2 (en) 2012-07-24 2016-03-31 Evonik Operations Gmbh Novel shaping process for PMI foam materials and/or composite components produced therefrom
GB2510133B (en) * 2013-01-24 2017-08-30 Bae Systems Plc Conductive bonded composites
DE102013223347A1 (de) 2013-11-15 2015-05-21 Evonik Industries Ag Mit Poly(meth)acrylimid-Schaum gefüllte Wabenstrukturen
DE102013018158A1 (de) 2013-12-05 2015-06-11 Airbus Defence and Space GmbH Verfahren zur Herstellung von verstärkten Materialien und Material erhältlich aus diesem Verfahren
DE102014014961A1 (de) * 2014-10-14 2016-04-14 Airbus Defence and Space GmbH Vorrichtung sowie Verfahren
EP3237508B1 (de) * 2014-12-22 2020-04-22 Basf Se Faserverstärkung von schaumstoffen aus miteinander verbundenen segmenten
DE102015202035B4 (de) * 2015-02-05 2025-06-26 Bayerische Motoren Werke Aktiengesellschaft Verfahren zur Herstellung eines Faser-Kunststoff-Verbund-Bauteils und Faser-Kunststoff-Verbund-Bauteil
DE102015110855B4 (de) 2015-07-06 2019-12-05 Technische Universität Chemnitz Verfahren zur Fertigung von komplexen 3D-Preformen
EP3263321B1 (de) * 2016-06-29 2021-07-28 Airbus Defence and Space GmbH Verfahren zur herstellung eines sandwich-paneels mit einem verstärkten schaumstoffkern
RU2678021C1 (ru) * 2017-09-11 2019-01-22 Государственное бюджетное образовательное учреждение высшего образования Московской области "Технологический университет" Способ изготовления объемно армированного композиционного материала
GB201903190D0 (en) * 2019-03-09 2019-04-24 Rolls Royce Plc An apparatus for gripping a plurality of reinforcement rods
DE102019114433A1 (de) 2019-05-29 2020-12-03 Airbus Operations Gmbh Verfahren und ein System zum Herstellen eines Bauteils oder Halbzeugs mit einem faserverstärkten Schaumkern
FR3098444B1 (fr) * 2019-07-08 2021-10-01 Soc Internationale Pour Le Commerce Et Lindustrie Procédé de renforcement d’un panneau et un procédé de fabrication de panneau composite mettant en œuvre un tel procédé

Family Cites Families (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2996330A (en) * 1959-11-12 1961-08-15 Edwin L Hutto Remotely operated manipulator
DE3246803A1 (de) * 1982-12-17 1984-06-20 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Verfahren zum herstellen von bauteilen aus lagen von faserverstaerktem kunststoff
GB9014770D0 (en) * 1990-07-03 1990-08-22 Short Brothers Plc Manufacture of a composite material
DE4030989A1 (de) * 1990-10-01 1992-04-09 Airbus Gmbh Verfahren und vorrichtung zum verstaerken von bauteilen aus lagen von faserverstaerktem thermoplastischem kunststoff
IT1245753B (it) * 1991-05-29 1994-10-14 Metalleido Srl Procedimento per la realizzazione di una struttura composita con tessuto intermedio tridimensionale ,e struttura realizzata mediante il procedimento stesso
DE4200855A1 (de) * 1992-01-15 1993-07-22 Mst Draenbedarf Schutzabdeckung fuer erdboeden
CA2138775C (en) * 1993-05-04 2000-03-14 Glenn A. Freitas Truss reinforced foam core sandwich structure
FR2718670B1 (fr) * 1994-04-18 1996-06-14 Aerospatiale Pièce comportant au moins une plaque de revêtement de matière composite et procédé pour réaliser ladite pièce.
JP2986220B2 (ja) * 1995-08-21 1999-12-06 フォスター−ミラー インク 複合構造内に部材を挿入するためのシステム
US6027798A (en) * 1995-11-01 2000-02-22 The Boeing Company Pin-reinforced sandwich structure
US5876652A (en) * 1996-04-05 1999-03-02 The Boeing Company Method for improving pulloff strength in pin-reinforced sandwich structure
US6722842B1 (en) * 1998-01-13 2004-04-20 Btm Corporation End arm manipulator
US6367856B1 (en) * 1999-04-15 2002-04-09 Thomas J. Jasperse Transfer apparatus for automated parts movement
DE10018035A1 (de) * 2000-04-03 2001-10-18 Nils Helbig Kernwerkstoff für Sandwichkonstruktionen
US7105071B2 (en) * 2001-04-06 2006-09-12 Ebert Composites Corporation Method of inserting z-axis reinforcing fibers into a composite laminate
US6676785B2 (en) * 2001-04-06 2004-01-13 Ebert Composites Corporation Method of clinching the top and bottom ends of Z-axis fibers into the respective top and bottom surfaces of a composite laminate
US7056576B2 (en) * 2001-04-06 2006-06-06 Ebert Composites, Inc. 3D fiber elements with high moment of inertia characteristics in composite sandwich laminates
US6645333B2 (en) * 2001-04-06 2003-11-11 Ebert Composites Corporation Method of inserting z-axis reinforcing fibers into a composite laminate
US6984277B2 (en) * 2003-07-31 2006-01-10 Siemens Westinghouse Power Corporation Bond enhancement for thermally insulated ceramic matrix composite materials
KR101111993B1 (ko) * 2003-09-08 2012-02-15 에보니크 룀 게엠베하 코어 복합체에서의 힘 도입 포인트 및 코어 복합체의 두께 방향으로 삽입되는 보강 부재를 사용하여 힘 도입 포인트를 제조하는 방법
US20060006023A1 (en) * 2004-07-08 2006-01-12 The United States Of America As Represented By Secretary Of The Army Combination rear impact guard, ladder, and ramp for military cargo vehicles
US7563497B2 (en) * 2004-12-27 2009-07-21 Mkp Structural Design Associates, Inc. Lightweight, rigid composite structures
DE102005024408A1 (de) * 2005-05-27 2006-11-30 Airbus Deutschland Gmbh Verstärkung von Schaumwerkstoffen
DE102007055684A1 (de) * 2007-11-21 2009-06-10 Airbus Deutschland Gmbh Vorrichtung zur Herstellung eines verstärkten Schaumwerkstoffes

Also Published As

Publication number Publication date
JP4751448B2 (ja) 2011-08-17
KR20080031908A (ko) 2008-04-11
RU2008106981A (ru) 2009-09-10
DE102005035681A1 (de) 2007-02-08
US20080226876A1 (en) 2008-09-18
WO2007012353A1 (de) 2007-02-01
CA2616655C (en) 2014-01-07
KR101319703B1 (ko) 2013-10-17
ZA200800782B (en) 2008-12-31
JP2009502562A (ja) 2009-01-29
PL1907193T3 (pl) 2011-08-31
EP1907193B1 (de) 2011-03-02
CA2616655A1 (en) 2007-02-01
AU2006274270B2 (en) 2011-06-16
EP1907193B8 (de) 2011-10-12
TWI388429B (zh) 2013-03-11
DE502006009011D1 (de) 2011-04-14
CN101198459B (zh) 2012-02-22
HK1120768A1 (en) 2009-04-09
BRPI0613882A2 (pt) 2011-02-15
RU2419543C2 (ru) 2011-05-27
ES2361617T3 (es) 2011-06-20
AU2006274270A1 (en) 2007-02-01
ATE500049T1 (de) 2011-03-15
IL186761A (en) 2011-01-31
TW200709929A (en) 2007-03-16
CN101198459A (zh) 2008-06-11
NZ563572A (en) 2010-08-27
EP1907193A1 (de) 2008-04-09
IL186761A0 (en) 2008-02-09

Similar Documents

Publication Publication Date Title
IL186761A0 (en) Method for producing a core material reinforcement for sandwich structures and said sandwich structures
Partridge et al. Delamination resistant laminates by Z-Fiber® pinning: Part I manufacture and fracture performance
CA2604572A1 (en) Reinforcement of cellular materials
EP1707702A3 (en) Composite structural members and methods for forming the same
FR2893683B1 (fr) Procede de fabrication d'une bielle en materiau composite
US10232558B2 (en) Component with a fastening region for a threaded connection, together with a moulded part and a fastening part
FI3758923T3 (fi) Tikattu moniaksiaalinen lujite ja menetelmä sen valmistamiseksi
An et al. Static strength of RTM composite joint with I-fiber stitching process
ATE463631T1 (de) Bewehrungskörper aus faserverstärktem kunststoff
JP2013241753A (ja) 繊維強化プラスチック製矢板
Zhang et al. A comprehensive study on the effect of reinforcing methods on the flexural behaviour of Concrete-RUHTCC composite beams
CN101046031B (zh) 制造塑料成圈工具梳栉的方法和塑料成圈工具梳栉
ATE556166T1 (de) Hochfestes verbindungssystem für faserverstärkte verbundwerkstoffe
Weimer et al. Approach to net-shape preforming using textile technologies. Part I: edges
WO2012175208A1 (de) Behälter, insbesondere selbsttragender behälter, verfahren zur herstellung desselben
RU2007111602A (ru) Конструкция каркасов солнечных батарей и способ изготовления каркаса
ES2387095T8 (es) Procedimiento de fabricación de tubos compuestos mediante pultrusión y tubos obtenidos
Hawkins et al. Embedding Micromachines in Materials
ATE536302T1 (de) Metallverstärkte hybridstruktur
Heidrich et al. Correlations between injection molding and welding of microcellular materials
DE102007054280B3 (de) Holzverbundwerkstoff und Verfahren zur Herstellung von Holzverbundwerkstoffen
Peng et al. Shear strength analysis of concrete beam-column joints reinforced with FRP.
INTERLAMINAR et al. FOR ENGINEERING-DOCTORATE
PL381993A1 (pl) Rura, zwłaszcza do zastosowań przemysłowych i sposób wytwarzania rury, zwłaszcza do zastosowań przemysłowych
Noda et al. Tensile Strength of CFRP Cross-Ply Laminate with Transverse Crack.