DE68907742D1 - Textile struktur fuer das verstaerken von bauelementen, wie balken, aus verbundwerkstoffen und verfahren zur herstellung derselben. - Google Patents

Textile struktur fuer das verstaerken von bauelementen, wie balken, aus verbundwerkstoffen und verfahren zur herstellung derselben.

Info

Publication number
DE68907742D1
DE68907742D1 DE8989301480T DE68907742T DE68907742D1 DE 68907742 D1 DE68907742 D1 DE 68907742D1 DE 8989301480 T DE8989301480 T DE 8989301480T DE 68907742 T DE68907742 T DE 68907742T DE 68907742 D1 DE68907742 D1 DE 68907742D1
Authority
DE
Germany
Prior art keywords
composites
reinforcement
bars
production
components
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 - Fee Related
Application number
DE8989301480T
Other languages
English (en)
Other versions
DE68907742T2 (de
Inventor
Yoshiaki C O Nagoya A Sakatani
Tetsuya C O Nagoya Ai Yamamoto
Shigeru C O Nagoya A Nishiyama
Tetsuro Hirokawa
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.)
Shikibo Ltd
Shikishima Boseki KK
Mitsubishi Heavy Industries Ltd
Original Assignee
Shikibo Ltd
Shikishima Boseki KK
Mitsubishi Heavy Industries Ltd
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 JP1011033A external-priority patent/JP2591814B2/ja
Application filed by Shikibo Ltd, Shikishima Boseki KK, Mitsubishi Heavy Industries Ltd filed Critical Shikibo Ltd
Application granted granted Critical
Publication of DE68907742D1 publication Critical patent/DE68907742D1/de
Publication of DE68907742T2 publication Critical patent/DE68907742T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • D—TEXTILES; PAPER
    • D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
    • D04H—MAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
    • D04H3/00—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length
    • D04H3/02—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of forming fleeces or layers, e.g. reorientation of yarns or filaments
    • D04H3/07—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of forming fleeces or layers, e.g. reorientation of yarns or filaments otherwise than in a plane, e.g. in a tubular way
    • 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
    • B29C70/22—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 two directions forming a two dimensional structure
    • B29C70/222—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 two directions forming a two dimensional structure the structure being shaped to form a three dimensional configuration
    • 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
    • D—TEXTILES; PAPER
    • D03—WEAVING
    • D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D41/00—Looms not otherwise provided for, e.g. for weaving chenille yarn; Details peculiar to these looms
    • D03D41/004—Looms for three-dimensional fabrics
    • 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
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S428/00—Stock material or miscellaneous articles
    • Y10S428/902—High modulus filament or fiber
    • 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]
    • Y10T442/3179—Woven fabric is characterized by a particular or differential weave other than fabric in which the strand denier or warp/weft pick count is specified
    • Y10T442/3195—Three-dimensional weave [e.g., x-y-z planes, multi-planar warps and/or wefts, etc.]

Landscapes

  • Engineering & Computer Science (AREA)
  • Textile Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Mechanical Engineering (AREA)
  • Woven Fabrics (AREA)
  • Moulding By Coating Moulds (AREA)
  • Laminated Bodies (AREA)
DE89301480T 1988-02-19 1989-02-16 Textile Struktur für das Verstärken von Bauelementen, wie Balken, aus Verbundwerkstoffen und Verfahren zur Herstellung derselben. Expired - Fee Related DE68907742T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
JP3829388 1988-02-19
JP1011033A JP2591814B2 (ja) 1988-02-19 1989-01-19 複合材製桁材の補強用繊維構造体およびその製造方法

Publications (2)

Publication Number Publication Date
DE68907742D1 true DE68907742D1 (de) 1993-09-02
DE68907742T2 DE68907742T2 (de) 1993-11-11

Family

ID=26346409

Family Applications (1)

Application Number Title Priority Date Filing Date
DE89301480T Expired - Fee Related DE68907742T2 (de) 1988-02-19 1989-02-16 Textile Struktur für das Verstärken von Bauelementen, wie Balken, aus Verbundwerkstoffen und Verfahren zur Herstellung derselben.

Country Status (3)

Country Link
US (2) US5121530A (de)
EP (1) EP0329434B1 (de)
DE (1) DE68907742T2 (de)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB8924590D0 (en) * 1989-11-01 1989-12-20 Maunsell Structural Plastics Reinforced composite structural members
US5211967A (en) * 1991-03-15 1993-05-18 Kabushiki Kaisha Toyoda Jidoshokki Seisakusho Three-dimensional fabric and method of producing the same
GB9117863D0 (en) * 1991-08-19 1991-10-09 Cambridge Consultants Fibre preforms for structural composite components
US5312670A (en) * 1992-01-06 1994-05-17 Wu Kuang Ming Fully isotropic laminates and quasi-homogeneous anisotropic laminates
FR2687174B1 (fr) * 1992-02-11 1995-09-22 Aerospatiale Procede pour la realisation d'une armature de fibres pour piece de matiere composite a parois non coplanaires, et piece composite comportant une telle armature.
US5327621A (en) * 1992-03-23 1994-07-12 Kabushiki Kaisha Toyoda Jidoshokki Seisakusho Method of producing fabric reinforcing matrix for composites
US5532040A (en) * 1994-04-15 1996-07-02 Wu; Kuang-Ming Multimaterial fully isotropic laminates and multimaterial quasi-homogeneous anisotropic laminates
GB2294709B (en) * 1994-11-04 1998-03-04 Rolls Royce Plc A method of manufacturing a porous material
JP3070428B2 (ja) * 1995-02-08 2000-07-31 株式会社豊田自動織機製作所 三次元繊維組織の製造装置
DE10018753A1 (de) * 2000-04-15 2001-10-25 Thyssenkrupp Technologies Ag Schweißzange
US6712099B2 (en) * 2001-06-15 2004-03-30 Lockheed Martin Corporation Three-dimensional weave architecture
US20030116267A1 (en) * 2001-12-21 2003-06-26 Sheahen Patrick D. Low-cost method of assembling structures with 3-D woven connectors
FR2869655B1 (fr) * 2004-04-28 2008-12-19 Airbus France Sas Procede d'assemblage de pieces structurales et assemblage obtenu.
US7964520B2 (en) * 2007-12-21 2011-06-21 Albany Engineered Composites, Inc. Method for weaving substrates with integral sidewalls
US7712488B2 (en) * 2008-03-31 2010-05-11 Albany Engineered Composites, Inc. Fiber architecture for Pi-preforms
FR2934562B1 (fr) * 2008-07-31 2011-04-22 Airbus France Panneau de protection et module de train d'atterissage le comportant.
JP5592672B2 (ja) * 2009-03-27 2014-09-17 ホンダ・パテンツ・アンド・テクノロジーズ・ノース・アメリカ・エルエルシー 航空機用スキッドレール及びその製造方法
BR112016003987B1 (pt) 2013-09-04 2021-10-05 Biteam Ab Artigo de tecido tridimensional, método para produção de um artigo de tecido tridimensional e aparelho para produzir um artigo de tecido tridimensional
EP3079951A4 (de) * 2013-12-10 2017-09-06 Continental Structural Plastics, Inc. I-träger mit verstärkter aussenhaut
WO2016025386A1 (en) * 2014-08-15 2016-02-18 Sikorsky Aircraft Corporation Rotor blade spar formation with automated fiber placement

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4336296A (en) * 1978-12-27 1982-06-22 Agency Of Industrial Science & Technology Three-dimensionally latticed flexible-structure composite
FR2497839A1 (fr) * 1981-01-12 1982-07-16 Brochier Fils J Tissu tridimensionnel pour le renforcement de materiaux stratifies et elements en forme obtenus a partir d'un tel tissu
FR2531459A1 (fr) * 1982-08-09 1984-02-10 Aerospatiale Procede et machine de realisation de pieces complexes par tissage multidirectionnel
US4526828A (en) * 1983-06-27 1985-07-02 Pioneer Industrial Products Company Protective apparel material and method for producing same
US4438173A (en) * 1983-07-21 1984-03-20 Barber-Colman Company Triaxial fabric
US4725485A (en) * 1984-03-13 1988-02-16 Shikishima Canvas Kabushiki Kaisha Textile structure for reinforced composite material
FR2564490B1 (fr) * 1984-05-15 1986-09-19 Aerospatiale Perfectionnements aux profiles composites tricotes en trois dimensions et procede pour leur fabrication
US4621980A (en) * 1984-09-19 1986-11-11 United Technologies Corporation Fiber reinforced composite spar for a rotary wing aircraft
US4606961A (en) * 1984-10-09 1986-08-19 The Boeing Company Discretely stiffened composite panel
JPS61179731A (ja) * 1984-12-29 1986-08-12 日本マイヤー株式会社 三次元構造材料
US4782864A (en) * 1984-12-31 1988-11-08 Edo Corporation Three dimensional woven fabric connector
JPS6221834A (ja) * 1985-07-15 1987-01-30 三菱重工業株式会社 複合材の強化部材用芯体及びその製造方法
JPS6221835A (ja) * 1985-07-15 1987-01-30 三菱重工業株式会社 複合材の強化部材用芯体及びその製造方法
US4671470A (en) * 1985-07-15 1987-06-09 Beech Aircraft Corporation Method for fastening aircraft frame elements to sandwich skin panels covering same using woven fiber connectors
DE3575746D1 (de) * 1985-09-13 1990-03-08 Shikishima Canvas Kk Faserstruktur zur verstaerkung von baumaterial.
FR2602248B1 (fr) * 1986-08-01 1989-11-24 Brochier Sa Structure textile multidimensionnelle pour le renforcement de materiaux stratifies et procede et metier a tisser permettant l'obtention d'une telle structure
JPH0778303B2 (ja) * 1987-02-03 1995-08-23 三菱重工業株式会社 複合材強化用の繊維構造体の製造方法

Also Published As

Publication number Publication date
EP0329434A3 (en) 1990-05-16
US5126190A (en) 1992-06-30
EP0329434B1 (de) 1993-07-28
EP0329434A2 (de) 1989-08-23
DE68907742T2 (de) 1993-11-11
US5121530A (en) 1992-06-16

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee