ES528087A0 - Procedimiento para la fabricacion de modulos de capas de plastico reforzado con fibra. - Google Patents

Procedimiento para la fabricacion de modulos de capas de plastico reforzado con fibra.

Info

Publication number
ES528087A0
ES528087A0 ES528087A ES528087A ES528087A0 ES 528087 A0 ES528087 A0 ES 528087A0 ES 528087 A ES528087 A ES 528087A ES 528087 A ES528087 A ES 528087A ES 528087 A0 ES528087 A0 ES 528087A0
Authority
ES
Spain
Prior art keywords
modules
fiber
procedure
manufacture
plastic layers
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.)
Granted
Application number
ES528087A
Other languages
English (en)
Other versions
ES8505583A1 (es
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 GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
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 Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of ES528087A0 publication Critical patent/ES528087A0/es
Publication of ES8505583A1 publication Critical patent/ES8505583A1/es
Expired 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
    • B29C70/10—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
    • B29C70/28—Shaping operations therefor
    • B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/543—Fixing the position or configuration of fibrous reinforcements before or during moulding
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
    • B32B5/06—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer characterised by a fibrous or filamentary layer mechanically connected, e.g. by needling to another layer, e.g. of fibres, of paper
    • 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
    • D04H3/002—Inorganic yarns or filaments
    • 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
    • D04H3/002—Inorganic yarns or filaments
    • D04H3/004—Glass yarns or filaments
    • 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
    • D04H3/08—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating
    • D04H3/10—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating with bonds between yarns or filaments made mechanically
    • D04H3/105—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating with bonds between yarns or filaments made mechanically by needling
    • 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
    • D04H3/08—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating
    • D04H3/10—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating with bonds between yarns or filaments made mechanically
    • D04H3/115—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating with bonds between yarns or filaments made mechanically by applying or inserting filamentary binding elements
    • 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
    • B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/56—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using mechanical means or mechanical connections, e.g. form-fits
    • B29C65/562—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using mechanical means or mechanical connections, e.g. form-fits using extra joining elements, i.e. which are not integral with the parts to be joined
    • B29C65/564—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using mechanical means or mechanical connections, e.g. form-fits using extra joining elements, i.e. which are not integral with the parts to be joined hidden in the joint, e.g. dowels or Z-pins
    • 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
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/01—General aspects dealing with the joint area or with the area to be joined
    • B29C66/05—Particular design of joint configurations
    • B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
    • B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
    • B29C66/112—Single lapped joints
    • B29C66/1122—Single lap to lap joints, i.e. overlap joints
    • 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
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/01—General aspects dealing with the joint area or with the area to be joined
    • B29C66/05—Particular design of joint configurations
    • B29C66/303—Particular design of joint configurations the joint involving an anchoring effect
    • B29C66/3034—Particular design of joint configurations the joint involving an anchoring effect making use of additional elements, e.g. meshes
    • B29C66/30341—Particular design of joint configurations the joint involving an anchoring effect making use of additional elements, e.g. meshes non-integral with the parts to be joined, e.g. making use of extra elements
    • 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
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/40—General aspects of joining substantially flat articles, e.g. plates, sheets or web-like materials; Making flat seams in tubular or hollow articles; Joining single elements to substantially flat surfaces
    • B29C66/41—Joining substantially flat articles ; Making flat seams in tubular or hollow articles
    • B29C66/45—Joining of substantially the whole surface of the articles
    • 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
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
    • B29C66/721—Fibre-reinforced materials
    • 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
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
    • B29C66/721—Fibre-reinforced materials
    • B29C66/7212—Fibre-reinforced materials characterised by the composition of the fibres
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2305/00—Condition, form or state of the layers or laminate
    • B32B2305/07—Parts immersed or impregnated in a matrix
    • B32B2305/076—Prepregs
    • 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
    • Y10T428/249921—Web or sheet containing structurally defined element or component
    • Y10T428/249923—Including interlaminar mechanical fastener
    • 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
    • Y10T428/30—Self-sustaining carbon mass or layer with impregnant or other 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
    • Y10T442/00—Fabric [woven, knitted, or nonwoven textile or cloth, etc.]
    • Y10T442/60—Nonwoven fabric [i.e., nonwoven strand or fiber material]
    • Y10T442/654—Including a free metal or alloy constituent
ES528087A 1982-12-17 1983-12-15 Procedimiento para la fabricacion de modulos de capas de plastico reforzado con fibra. Expired ES8505583A1 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19823246803 DE3246803A1 (de) 1982-12-17 1982-12-17 Verfahren zum herstellen von bauteilen aus lagen von faserverstaerktem kunststoff

Publications (2)

Publication Number Publication Date
ES528087A0 true ES528087A0 (es) 1985-06-01
ES8505583A1 ES8505583A1 (es) 1985-06-01

Family

ID=6180989

Family Applications (1)

Application Number Title Priority Date Filing Date
ES528087A Expired ES8505583A1 (es) 1982-12-17 1983-12-15 Procedimiento para la fabricacion de modulos de capas de plastico reforzado con fibra.

Country Status (5)

Country Link
US (1) US4528051A (es)
DE (1) DE3246803A1 (es)
ES (1) ES8505583A1 (es)
FR (1) FR2537916B1 (es)
GB (1) GB2132134B (es)

Families Citing this family (54)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3302337C2 (de) * 1983-01-25 1986-08-07 Deutsche Fibrit Gesellschaft Ebers & Dr. Müller mbH, 4150 Krefeld Verfahren und Vorrichtung zum Kaschieren von Verkleidungen
US4740257A (en) * 1985-03-04 1988-04-26 Acoustic Industries, Inc. Ceiling tile covering system
GB8618727D0 (en) * 1986-07-31 1986-09-10 Wiggins Teape Group Ltd Thermoplastic sheets
US4808461A (en) * 1987-12-14 1989-02-28 Foster-Miller, Inc. Composite structure reinforcement
GB8927734D0 (en) * 1989-12-07 1990-02-07 Short Brothers Plc A composite material
US5186776A (en) * 1990-05-07 1993-02-16 Foster-Miller, Inc. Composite laminate translaminar reinforcement apparatus and method
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
FR2687389B1 (fr) * 1992-02-17 1994-05-06 Aerospatiale Ste Nationale Indle Dispositif et procede pour realiser une piece de structure complexe par depose au contact de fil ou ruban.
US5466506A (en) * 1992-10-27 1995-11-14 Foster-Miller, Inc. Translaminar reinforcement system for Z-direction reinforcement of a fiber matrix structure
DE69431909T2 (de) * 1993-04-30 2003-11-06 Foster Miller Inc Ein verstärktes verbindungselement von verbundstrukturen und verfahren zum verbinden von verbundteilen
EP0653984B1 (en) * 1993-05-04 2007-01-24 Foster-Miller, Inc. Truss reinforced foam core sandwich structure
EP0646454B1 (en) * 1993-09-25 1998-03-18 Symalit Ag Fibre reinforced thermoplastic sheet
EP0725728B1 (en) * 1993-10-29 2007-09-12 Foster-Miller, Inc. Translaminar reinforcement system for z-direction reinforcement of a fiber matrix structure
JPH09508079A (ja) * 1994-01-24 1997-08-19 ケムファブ コーポレイション フルオロポリマーと熱的非粘着性非フルオロポリマーとの複合物及びその製造方法
US5720143A (en) * 1994-03-01 1998-02-24 The United States Of America As Represented By The Secretary Of Agriculture Localized notch reinforcement for wooden beams
US5756973A (en) * 1995-06-07 1998-05-26 The Boeing Company Barbed susceptor for improviing pulloff strength in welded thermoplastic composite structures
WO1997039886A1 (fr) * 1996-04-19 1997-10-30 Gennady Ashotovich Amiryants Panneau elastomere arme et cellule
US5876540A (en) * 1996-05-31 1999-03-02 The Boeing Company Joining composites using Z-pinned precured strips
US5980665A (en) * 1996-05-31 1999-11-09 The Boeing Company Z-pin reinforced bonds for connecting composite structures
US5759924A (en) * 1996-10-18 1998-06-02 Chemfab Corporation Translucent polymeric composite for use in an architectural load-bearing structure
US6051089A (en) * 1997-02-07 2000-04-18 Mcdonnell Douglas Corporation Reinforcing member for composite workpieces and associated methods
US6291049B1 (en) 1998-10-20 2001-09-18 Aztex, Inc. Sandwich structure and method of making same
DE19935518A1 (de) * 1999-07-28 2001-02-01 Bayerische Motoren Werke Ag Verbundteil mit übereinander angeordneten Schichten
US6267175B1 (en) * 2000-02-08 2001-07-31 Honeywell International Inc. Composite heat exchanger having strengthened joints
US7105071B2 (en) * 2001-04-06 2006-09-12 Ebert Composites Corporation Method of inserting z-axis reinforcing fibers into a composite laminate
US7731046B2 (en) * 2001-04-06 2010-06-08 Ebert Composites Corporation Composite sandwich panel and method of making same
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
US7785693B2 (en) 2001-04-06 2010-08-31 Ebert Composites Corporation Composite laminate structure
US20050025948A1 (en) * 2001-04-06 2005-02-03 Johnson David W. Composite laminate reinforced with curvilinear 3-D fiber and method of making the same
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
US20050118448A1 (en) * 2002-12-05 2005-06-02 Olin Corporation, A Corporation Of The Commonwealth Of Virginia Laser ablation resistant copper foil
DE102005012496B3 (de) * 2005-03-16 2006-10-26 Technische Universität Berlin Vorrichtung mit einem auf einem Montageteil montierten elektronischen Bauteil und Verfahren
DE102005035681A1 (de) * 2005-07-27 2007-02-08 Röhm Gmbh Fertigungsverfahren zur Armierung von Kernmaterialien für Kernverbunde sowie von Kernverbund-Strukturen
US8709584B2 (en) * 2006-01-31 2014-04-29 Sikorsky Aircraft Corporation Composite aircraft floor system
US20100021682A1 (en) * 2008-07-25 2010-01-28 Florida State University Research Foundation Composite material and method for increasing z-axis thermal conductivity of composite sheet material
DE102008043314B4 (de) * 2008-10-30 2010-12-09 Airbus Deutschland Gmbh Verfahren und Vorrichtung zum Verstärken eines Substrats oder eines Textils einer Kernstruktur eines Bauelementes, beispielsweise eines Luft- oder Raumfahrzeugs
JP5405584B2 (ja) * 2008-11-19 2014-02-05 ビ−エイイ− システムズ パブリック リミテッド カンパニ− 繊維強化複合材料
DE102009010292A1 (de) * 2009-02-24 2010-08-26 Bayerische Motoren Werke Aktiengesellschaft Verfahren zur Herstellung eines faserverstärkten Kunststoffbauteils
WO2010141984A1 (en) * 2009-06-12 2010-12-16 Quickstep Technologies Pty Ltd Method of producing advanced composite components
DE102009047671A1 (de) * 2009-12-08 2011-06-09 Airbus Operations Gmbh Verfahren zum Anbinden eines Faserverbundbauteils an ein Strukturbauteil eines Luft- und Raumfahrzeuges und eine entsprechende Anordnung
FR2959442B1 (fr) * 2010-04-30 2012-09-28 Eads Europ Aeronautic Defence Procede et dispositif d'assemblage de preformes en composites thermoplastiques
DE102011101456A1 (de) * 2011-05-13 2012-11-15 Airbus Operations Gmbh Verbindungsvorrichtung, Baugruppe und Verfahren zur Herstellung einer Baugruppe
DE102011115406A1 (de) * 2011-10-06 2013-04-11 Airbus Operations Gmbh Verfahren zum Verbinden von faserverstärkten Zwischenprodukten und Strukturbauteil mit faserverstärkten Zwischenprodukten sowie Verfahren und Vorrichtung zur Herstellung einer Adhäsionsschicht
GB201117467D0 (en) * 2011-10-11 2011-11-23 Rolls Royce Plc A method of providing through-thickness reinforcement of a laminated material
FR2998210B1 (fr) * 2012-11-20 2017-03-10 Plastic Omnium Cie Ensemble d'un insert metallique et d'une nappe de materiau composite, procede d'incorporation d'un tel insert dans une telle nappe et piece obtenue par moulage d'une telle nappe
JP6286022B2 (ja) 2013-03-15 2018-02-28 セリフォージ インコーポレイテッド 複合材プリフォームの三次元製織方法及び漸変断面トポロジーを備えた製品
DE102014209815A1 (de) * 2014-03-07 2015-09-10 Leichtbau-Zentrum Sachsen Gmbh Verfahren zur Verbindung von faserverstärkten Kunststoffbauteilen mit duroplastischer Matrix
EP3034278B1 (de) * 2014-12-19 2020-02-12 Airbus Defence and Space GmbH Bauteil mit stoffschlüssiger Verbindung und ein Fügeverfahren
EP3034276B1 (de) 2014-12-19 2021-06-30 Airbus Defence and Space GmbH Bauteil mit stoffschlüssiger Verbindung und ein Fügeverfahren
CN108778728A (zh) 2016-03-21 2018-11-09 美国圣戈班性能塑料公司 建筑膜
US10543646B2 (en) 2018-01-12 2020-01-28 Arevo, Inc. Structural sewing and overmolding
US11549391B2 (en) * 2021-03-22 2023-01-10 General Electric Company Component formed from hybrid material

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1657979A (en) * 1926-05-03 1928-01-31 Thomas Frederick William Roofing material
FR950104A (fr) * 1943-01-30 1949-09-19 Procédé de fixation d'éléments d'assemblage
GB891121A (en) * 1957-05-07 1962-03-14 Dracone Developments Ltd Improvements in or relating to flexible barges or storage vessels
US3451884A (en) * 1964-08-05 1969-06-24 Mitsubishi Petrochemical Co Waterproof pile coated sheet for laminating
US3464348A (en) * 1967-06-02 1969-09-02 Arthur E Mcglinchey Apparatus for fabricating wooden structures
GB1310355A (en) * 1969-07-03 1973-03-21 Foseco Trading Ag Fibre containing compositions
GB1244893A (en) * 1969-07-21 1971-09-02 Carol Ann Franiel Improvements in laminates
CH526012A (de) * 1970-04-07 1972-07-31 Ver Drahtwerke Ag Verfahren zur Herstellung von Nagelplatten und Einrichtung zur Durchführung des Verfahrens
US3769142A (en) * 1970-12-04 1973-10-30 Mc Donnell Douglas Corp Non-woven locked ply composite structure
GB1411379A (en) * 1971-12-21 1975-10-22 Rolls Royce Fibre reinforced composite structures
US3837985A (en) * 1972-02-24 1974-09-24 Whittaker Corp Multi-directional reinforced composite and method of making the same
US4218276A (en) * 1972-03-31 1980-08-19 Avco Corporation Method for making 3-D structures
US4032383A (en) * 1975-11-04 1977-06-28 Mcdonnell Douglas Corporation Fiber insertion device for continuous 3d foaming machine and method
SU545483A2 (ru) * 1975-12-24 1977-02-05 Предприятие П/Я 7332 Способ изготовлени силового элемента из стеклопластика
DE2606666C2 (de) * 1976-02-19 1982-03-18 Greimbau-Lizenz-Gmbh, 3200 Hildesheim Nagelplatte zum Verbinden von Holzbauteilen
FR2433003A1 (fr) * 1978-08-08 1980-03-07 Commissariat Energie Atomique Procede de fabrication d'un materiau renforce par une structure textile tridimensionnelle
FR2446175A1 (fr) * 1979-01-09 1980-08-08 Europ Propulsion Texture stratifiee renforcee
US4350728A (en) * 1980-10-02 1982-09-21 The United States Of America As Represented By The Secretary Of The Navy Cross reinforcement in a graphite-epoxy laminate

Also Published As

Publication number Publication date
FR2537916A1 (fr) 1984-06-22
US4528051A (en) 1985-07-09
FR2537916B1 (fr) 1987-02-20
GB2132134B (en) 1986-12-10
GB2132134A (en) 1984-07-04
DE3246803C2 (es) 1990-04-19
ES8505583A1 (es) 1985-06-01
DE3246803A1 (de) 1984-06-20

Similar Documents

Publication Publication Date Title
ES528087A0 (es) Procedimiento para la fabricacion de modulos de capas de plastico reforzado con fibra.
ES521916A0 (es) Un metodo para la fabricacion de articulos con refuerzo de fibra.
ES530453A0 (es) Un procedimiento para fabricar un material compuesto reforzado con fibra
DE3370635D1 (de) Polyamino-bis-imide resin
IT8322159A0 (it) Materiali compositi rinforzati con fibre.
DK72283D0 (da) Krympefolier af polyethylen
ES533882A0 (es) Procedimiento para la preparacion de polimero vulcanizados fluoro-elastomericos.
DE3772704D1 (de) Thermoplastisches harzlaminat.
ES522230A0 (es) Procedimiento para la fabricacion de laminados multicapa de vidrio-termoplastico.
ATA119183A (de) Herstellung
IT8748660A0 (it) Laminato in polipropilene reticolato rinforzato con fibre per la produzione di circuiti stampati
ES498220A0 (es) Procedimiento para la fabricacion de un material laminar plastico reforzado con fibra de vidrio
IT8304834A0 (it) Aerodina ad ala rigida.
ES522663A0 (es) Procedimiento para preparar acidos imidazolinbenzoicos con propiedades herbicidas.
ES524711A0 (es) Procedimiento para la obtencion de composiciones de moldeo termoplasticas.
ES524501A0 (es) Procedimiento de obtencion de una composicion de polimero termoplastico reforzada con fibra
ES489207A0 (es) Procedimiento para la fabricacion de una estructura laminada de piel fina reforzada con espuma polimerica.
ES522229A0 (es) Procedimiento para la fabricacion de un laminado curvo de vidrio-plastico.
ES519862A0 (es) Un procedimiento para fabricar fibra de vidrio.
ES530721A0 (es) Procedimiento para preparar una composicion polimidica reforzada con fibra de vidrio
ES524710A0 (es) Procedimiento para la obtencion de composiciones de moldeo termoplasticas.
ES528234A0 (es) Procedimiento para la fabricacion de laminados de vidrionplastico
ES536689A0 (es) Un metodo para la fabricacion de cuerpos compuestos de plastico reforzado con fibra de vidrio
NO832605L (no) Ekstruderingsinnretning
KR840001342U (ko) 조립식 합성수지 관