DE69610666D1 - Faserverstärktes Bauteil und Verfahren zu seiner Herstellung - Google Patents

Faserverstärktes Bauteil und Verfahren zu seiner Herstellung

Info

Publication number
DE69610666D1
DE69610666D1 DE69610666T DE69610666T DE69610666D1 DE 69610666 D1 DE69610666 D1 DE 69610666D1 DE 69610666 T DE69610666 T DE 69610666T DE 69610666 T DE69610666 T DE 69610666T DE 69610666 D1 DE69610666 D1 DE 69610666D1
Authority
DE
Germany
Prior art keywords
fiber
production
reinforced component
reinforced
component
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
DE69610666T
Other languages
English (en)
Other versions
DE69610666T2 (de
Inventor
Tozuka Shoichiro
Nishimoto Mitsuo
Masugi Kyoichi
Amaoka Kazuaki
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.)
Japan Aircraft Development Corp
Subaru Corp
Original Assignee
Japan Aircraft Development Corp
Fuji Jukogyo KK
Fuji 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
Application filed by Japan Aircraft Development Corp, Fuji Jukogyo KK, Fuji Heavy Industries Ltd filed Critical Japan Aircraft Development Corp
Application granted granted Critical
Publication of DE69610666D1 publication Critical patent/DE69610666D1/de
Publication of DE69610666T2 publication Critical patent/DE69610666T2/de
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
    • B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00—Subject matter not provided for in other groups of this subclass
    • B29D99/0003—Producing profiled members, e.g. beams
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29B—PREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
    • B29B11/00—Making preforms
    • B29B11/14—Making preforms characterised by structure or composition
    • B29B11/16—Making preforms characterised by structure or composition comprising fillers or reinforcement
    • 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
    • B29D99/00—Subject matter not provided for in other groups of this subclass
    • B29D99/001—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings
    • B29D99/0014—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings provided with ridges or ribs, e.g. joined ribs
    • 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
    • B29C2793/00—Shaping techniques involving a cutting or machining operation
    • 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
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24058—Structurally defined web or sheet [e.g., overall dimension, etc.] including grain, strips, or filamentary elements in respective layers or components in angular relation
    • 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.]
    • Y10T428/24058—Structurally defined web or sheet [e.g., overall dimension, etc.] including grain, strips, or filamentary elements in respective layers or components in angular relation
    • Y10T428/24074—Strand or strand-portions
    • Y10T428/24083—Nonlinear strands or strand-portions
    • 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.]
    • Y10T428/24058—Structurally defined web or sheet [e.g., overall dimension, etc.] including grain, strips, or filamentary elements in respective layers or components in angular relation
    • Y10T428/24074—Strand or strand-portions
    • Y10T428/24091—Strand or strand-portions with additional layer[s]
    • 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.]
    • Y10T428/24058—Structurally defined web or sheet [e.g., overall dimension, etc.] including grain, strips, or filamentary elements in respective layers or components in angular relation
    • Y10T428/24074—Strand or strand-portions
    • Y10T428/24091—Strand or strand-portions with additional layer[s]
    • Y10T428/24099—On each side of strands or strand-portions
    • Y10T428/24107—On each side of strands or strand-portions including mechanically interengaged strands, strand-portions or strand-like strips
DE69610666T 1995-06-21 1996-06-19 Faserverstärktes Bauteil und Verfahren zu seiner Herstellung Expired - Lifetime DE69610666T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP15475695A JP3839080B2 (ja) 1995-06-21 1995-06-21 繊維強化複合材の構造体及びその製造方法

Publications (2)

Publication Number Publication Date
DE69610666D1 true DE69610666D1 (de) 2000-11-23
DE69610666T2 DE69610666T2 (de) 2001-05-03

Family

ID=15591222

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69610666T Expired - Lifetime DE69610666T2 (de) 1995-06-21 1996-06-19 Faserverstärktes Bauteil und Verfahren zu seiner Herstellung

Country Status (4)

Country Link
US (1) US5981023A (de)
EP (1) EP0749825B1 (de)
JP (1) JP3839080B2 (de)
DE (1) DE69610666T2 (de)

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FR2803899B1 (fr) * 2000-01-17 2002-04-05 Ecia Equip Composants Ind Auto Element structurel comprenant un corps et des nervures de renfort et vehicule automobile correspondant
JP3615714B2 (ja) * 2001-04-03 2005-02-02 太陽パーツ株式会社 樹脂構造材の製造方法
JP4856327B2 (ja) * 2001-07-03 2012-01-18 富士重工業株式会社 複合材パネルの製造方法
US7138028B2 (en) * 2001-07-26 2006-11-21 The Boeing Company Vacuum assisted resin transfer method for co-bonding composite laminate structures
US20030019567A1 (en) * 2001-07-26 2003-01-30 Burpo Steven J. Vacuum assisted resin transfer method for co-bonding composite laminate structures
JP4574086B2 (ja) * 2001-09-03 2010-11-04 富士重工業株式会社 複合材翼の製造方法および複合材翼
AT410656B (de) * 2001-10-24 2003-06-25 Fischer Adv Components Gmbh Trag- bzw. führungsvorrichtung für flugzeugkomponenten
DE10161773A1 (de) * 2001-12-15 2003-06-26 Bayerische Motoren Werke Ag Verfahren zur Herstellung eines dreidimensional geformten Faserverbundkunststoffbauteils
FR2835854B1 (fr) * 2002-02-14 2005-12-30 Jean Dessinges Preformes fibreuses et leur procede de fabrication
GB0205498D0 (en) * 2002-03-08 2002-04-24 Structural Polymer Systems Ltd Moulding material
EP1342554B1 (de) * 2002-03-08 2010-02-03 Airbus Deutschland GmbH Verfahren zum Herstellen textiler Vorformlinge aus textilen Halbzeugen
EP1342553B1 (de) 2002-03-08 2016-05-18 Airbus Operations GmbH Verfahren zum Herstellen eines Fensterrahmens für Flugzeuge aus faserverstärktem Kunststoff und Vorrichtung zur Durchführung des Verfahrens
DE10251580B4 (de) * 2002-03-08 2013-01-10 Airbus Operations Gmbh Verfahren zum Herstellen eines Bauelementes aus faserverstärktem Kunststoff
EP1473131A3 (de) * 2003-04-30 2007-01-03 Airbus Deutschland GmbH Verfahren zum herstellen textiler vorformlinge aus textilen halbzeugen
US7563497B2 (en) * 2004-12-27 2009-07-21 Mkp Structural Design Associates, Inc. Lightweight, rigid composite structures
US7490539B2 (en) 2005-07-22 2009-02-17 Mkp Structural Design Associates, Inc. Lightweight composite armor
US7694621B1 (en) 2005-07-22 2010-04-13 Mkp Structural Design Associates, Inc. Lightweight composite armor
DE102005057907B4 (de) * 2005-12-02 2012-03-22 Eurocopter Deutschland Gmbh Luftfahrzeug-Druckkabinentür aus Faserverbundwerkstoff
GB0619512D0 (en) * 2006-10-03 2006-11-15 Airbus Uk Ltd Fitting
DE102006051457B4 (de) * 2006-10-31 2012-04-12 Airbus Operations Gmbh Versteifungselement für ein Luft- oder Raumfahrzeug und Verfahren zum Herstellen desselben
FR2913910B1 (fr) * 2007-03-19 2009-05-29 Skf Aerospace France Soc Par A Ensemble fibreux pour piece composite,piece composite et procede de fabrication d'une telle piece composite
DE102007015518A1 (de) * 2007-03-30 2008-10-02 Airbus Deutschland Gmbh Verfahren zur Herstellung von Profilteilen
GB0708333D0 (en) 2007-04-30 2007-06-06 Airbus Uk Ltd Composite structure
FR2921899B1 (fr) * 2007-10-04 2011-04-15 Airbus France Procede de renforcement local d'un element en materiau composite, et caisson central de voilure pour aeronef renforce
US8006605B2 (en) * 2007-10-10 2011-08-30 Hardware, LLC Armor panel system
US8181909B2 (en) * 2008-03-31 2012-05-22 Honda Motor Co., Ltd. Pressure bulkhead for aircraft
FR2932410B1 (fr) * 2008-06-11 2010-05-28 Aircelle Sa Procede de fabrication d'une piece a corps creux en materiau composite
GB0813785D0 (en) * 2008-07-29 2008-09-03 Airbus Uk Ltd Method of manufacturing a composite element
ES2384349B1 (es) * 2009-12-30 2013-05-16 Airbus Operations, S.L. Cuaderna de fuselaje de aeronave en material compuesto con costillas estabilizadoras.
US8616104B2 (en) 2010-07-12 2013-12-31 Robert Bosch Gmbh Portable table saw
WO2012117593A1 (ja) * 2011-02-28 2012-09-07 帝人株式会社 繊維強化複合材料からなる成形体
EP2511078B1 (de) 2011-04-14 2018-05-30 Siemens Aktiengesellschaft Verfahren zur Herstellung einer faserverstärkten Struktur
GB201114997D0 (en) * 2011-08-31 2011-10-12 Airbus Operations Ltd A curable assembly and a filler component
EP2762520B1 (de) * 2011-09-30 2020-11-11 Subaru Corporation Faserverstärktes harzverbundmaterial und herstellungsverfahren dafür
EP2814732B1 (de) * 2012-02-17 2017-04-05 Saab Ab Verfahren und formsystem zur netzformung einer cogehärteten, integrierten struktur
FR2990187B1 (fr) * 2012-05-07 2015-01-30 Airbus Operations Sas Poutre en materiau composite integrant un renfort a section fermee
JP2015127121A (ja) * 2013-12-27 2015-07-09 三菱重工業株式会社 アイソグリッドパネル構造体およびアイソグリッドパネル構造体製造方法
CN105172165A (zh) * 2015-09-14 2015-12-23 江西洪都航空工业集团有限责任公司 一种毫米波天线罩的厚度修正方法
EP3415297B1 (de) * 2016-04-07 2019-11-06 Mitsubishi Heavy Industries, Ltd. Verfahren zur herstellung eines verbundstoffmaterials
US10207471B2 (en) * 2016-05-04 2019-02-19 General Electric Company Perforated ceramic matrix composite ply, ceramic matrix composite article, and method for forming ceramic matrix composite article
DE102017212860B4 (de) * 2017-07-26 2020-07-09 Premium Aerotec Gmbh Vorrichtung und Verfahren zur Herstellung eines gekrümmten Faservorformlings aus einem bi- oder multidirektionalen Faserhalbzeug
DE102018222431B4 (de) * 2018-12-20 2023-12-07 Premium Aerotec Gmbh Rumpfbauteil für ein Luftfahrzeug, Verfahren zur Herstellung eines Rumpfbauteils sowie Luftfahrzeug
US11155056B2 (en) * 2019-04-08 2021-10-26 The Boeing Company Methods of making laminated metallic structures
CN216301443U (zh) * 2021-09-24 2022-04-15 深圳市道通智能航空技术股份有限公司 一种无人机
CN115107299B (zh) * 2022-07-05 2024-02-09 江西昌兴航空装备股份有限公司 一种垂尾整体梁铺贴方法

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FR2687173B1 (fr) * 1992-02-11 1995-09-08 Aerospatiale Procede pour la realisation d'une armature de fibres pour piece de matiere composite, et piece composite comportant une telle armature.
FR2699449B1 (fr) * 1992-12-17 1995-03-24 Eurocopter France Procédé de fabrication de liaisons en matériau composite de structures en forme de treillis ou d'éléments de treillis, et treillis obtenus par ce procédé.

Also Published As

Publication number Publication date
EP0749825A3 (de) 1997-04-02
DE69610666T2 (de) 2001-05-03
EP0749825A2 (de) 1996-12-27
JP3839080B2 (ja) 2006-11-01
EP0749825B1 (de) 2000-10-18
US5981023A (en) 1999-11-09
JPH091681A (ja) 1997-01-07

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