DK2459362T3 - Fremgangsmåde til fremstilling af en kerne med integrerede forbindende fibre til paneler af kompositmateriale, panel tilvejebragt derved, samt apparatur - Google Patents

Fremgangsmåde til fremstilling af en kerne med integrerede forbindende fibre til paneler af kompositmateriale, panel tilvejebragt derved, samt apparatur Download PDF

Info

Publication number
DK2459362T3
DK2459362T3 DK10752888.7T DK10752888T DK2459362T3 DK 2459362 T3 DK2459362 T3 DK 2459362T3 DK 10752888 T DK10752888 T DK 10752888T DK 2459362 T3 DK2459362 T3 DK 2459362T3
Authority
DK
Denmark
Prior art keywords
core
connecting fibers
station
fibers
fibres
Prior art date
Application number
DK10752888.7T
Other languages
English (en)
Inventor
Thierry Klethi
Frédéric Pinan
Original Assignee
Saertex France
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 Saertex France filed Critical Saertex France
Application granted granted Critical
Publication of DK2459362T3 publication Critical patent/DK2459362T3/da

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
    • D04H18/00—Needling machines
    • 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
    • B32B5/022—Non-woven fabric
    • 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
    • B32B5/16—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 features of a layer formed of particles, e.g. chips, powder or granules
    • 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
    • B32B5/18—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 features of a layer of foamed material
    • 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
    • B32B5/22—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 the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
    • 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
    • B32B5/22—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 the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
    • B32B5/24—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 the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
    • B32B5/245—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 the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it being a foam layer
    • 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
    • D04H1/00—Non-woven fabrics formed wholly or mainly of staple fibres or like relatively short fibres
    • D04H1/40—Non-woven fabrics formed wholly or mainly of staple fibres or like relatively short fibres from fleeces or layers composed of fibres without existing or potential cohesive properties
    • D04H1/44—Non-woven fabrics formed wholly or mainly of staple fibres or like relatively short fibres from fleeces or layers composed of fibres without existing or potential cohesive properties the fleeces or layers being consolidated by mechanical means, e.g. by rolling
    • D04H1/46—Non-woven fabrics formed wholly or mainly of staple fibres or like relatively short fibres from fleeces or layers composed of fibres without existing or potential cohesive properties the fleeces or layers being consolidated by mechanical means, e.g. by rolling by needling or like operations to cause entanglement of fibres
    • D04H1/48—Non-woven fabrics formed wholly or mainly of staple fibres or like relatively short fibres from fleeces or layers composed of fibres without existing or potential cohesive properties the fleeces or layers being consolidated by mechanical means, e.g. by rolling by needling or like operations to cause entanglement of fibres in combination with at least one other method of consolidation
    • 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
    • D04H13/00—Other non-woven fabrics
    • 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
    • D04H18/00—Needling machines
    • D04H18/02—Needling machines with needles
    • 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
    • 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
    • B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
    • B32B2260/02—Composition of the impregnated, bonded or embedded layer
    • B32B2260/021—Fibrous or filamentary layer
    • 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
    • B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
    • B32B2260/04—Impregnation, embedding, or binder material
    • B32B2260/046—Synthetic resin
    • 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
    • B32B2307/00—Properties of the layers or laminate
    • B32B2307/50—Properties of the layers or laminate having particular mechanical properties
    • 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
    • B32B2307/00—Properties of the layers or laminate
    • B32B2307/70—Other properties
    • B32B2307/72—Density
    • 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
    • Y10T156/12—Surface bonding means and/or assembly means with cutting, punching, piercing, severing or tearing
    • Y10T156/1304—Means making hole or aperture in part to be laminated
    • Y10T156/1309—Means making hole or aperture in part to be laminated and securing separate part over hole or aperture
    • 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
    • Y10T428/249924—Noninterengaged fiber-containing paper-free web or sheet which is not of specified porosity
    • Y10T428/24994—Fiber embedded in or on the surface of a polymeric matrix

Claims (14)

1. Fremgangsmåde til fremstilling af en kerne (11) med integrerede forbindende fibre (12), til fremstilling af kompositpaneler, kendetegnet ved, at den omfatter udførelse af følgende trin: tilvejebringelse af en blok (10) af letvægtsmateriale, anbringelse af forbindende fibre (12) i overskud på i det mindste én overflade (18, 20) af blokken (10), at bringe nogle af disse forbindende fibre (12) til at trænge ind i kernen, fjernelse af de ubrugte overskydende forbindende fibre (12).
2. Fremgangsmåde til fremstilling af en kerne (11) med forbindende fibre (12) i overensstemmelse med krav 1, kendetegnet ved, at nålestansning anvendes til at bringe de forbindende fibre (12) til at trænge ind i blokken (10).
3. Fremgangsmåde til fremstilling af en kerne (11) med forbindende fibre (12) i overensstemmelse med ethvert af de foregående krav, kendetegnet ved, at indtrængningen af de forbindende fibre (12) går helt igennem, således at hver forbindende fiber (12) er tilgængelig på begge sider af kernen.
4. Fremgangsmåde til fremstilling af en kerne (11) med forbindende fibre (12) i overensstemmelse med ethvert af de foregående krav, kendetegnet ved, at de forbindende fibre (12) er af forskellige typer.
5. Fremgangsmåde til fremstilling af en kerne (11) med forbindende fibre (12) i overensstemmelse med ethvert af kravene 1 til 4, kendetegnet ved, at de forbindende fibre (12) er dele af tråde, som omfatter bundter af omspundne filamenter.
6. Fremgangsmåde til fremstilling af en kerne (11) med forbindende fibre (12) i overensstemmelse med ethvert af kravene 1 til 5, kendetegnet ved, at de forbindende fibre (12) indføres med en hældning i forhold til overfladerne på blokken (10) af letvægtsmateriale.
7. Kerne (11) tilvejebragt ved implementering af fremgangsmåden i overensstemmelse med ethvert af de foregående krav, kendetegnet ved, at den kun omfatter én blok (10) af letvægtsmateriale og forbindende fibre (12), som er trængt ind i blokken, idet i det mindste nogle af fibrene, som er trængt ind, stikker ud på i det mindste en overflade af blokken (10).
8. Kerne (11) i overensstemmelse med krav 7, kendetegnet ved, at densiteten af de forbindende fibre (12) pr. overfladeenhed er kontrolleret.
9. Kerne (11) i overensstemmelse med krav 7 eller 8, kendetegnet ved, at fordelingsgeometrien for de forbindende fibre (12) pr. overfladeenhed er kontrolleret.
10. Panel (22) af kompositmateriale, omfattende en kerne (11), fremstillet ved anvendelse af en kerne i overensstemmelse med ethvert af kravene 7 til 9, kendetegnet ved, at den omfatter i det mindste overfladefibre (24), som er indlejrede i en harpiksmatrix, fastgjort til den nævnte kerne (11), idet harpiksen også er trængt ind i de forbindende fibre (12).
11. Panel (22) i overensstemmelse med krav 10, kendetegnet ved, at enderne af de forbindende fibre (12) er indlejrede i harpiksmatrixen sammen med overfladefibrene (24).
12. Panel (22) i overensstemmelse med krav 10 eller 11, kendetegnet ved, at de forbindende fibre (12) er skråtstillede i forhold til kernens plan.
13. Apparatur til fremstilling af en kerne i overensstemmelse med ethvert af kravene 10, 11 eller 12, kendetegnet ved, at det omfatter: en station (26) til at tilføre blokke (10) af letvægtsmateriale, en station (28) til at anbringe forbindende fibre på hver kerne, en nålestansningsstation (30), en station (32) til vinklet orientering af stationen (26) til at tilføre blokke i forhold til nålestansestationen, en station (36) til at afgive kernerne (11) med integrerede forbindende fibre.
14. Apparatur til fremstilling af en kerne i overensstemmelse med krav 13, kendetegnet ved, at det omfatter: en station (26) til at tilføre blokke (10) af letvægtsmateriale, en station (28) til at anbringe forbindende fibre på hver kerne, en nålestansestation (30), en station (32) til vinklet orientering af stationen til at tilføre blokke i forhold til nålestansestationen, en station (34) til at eliminere de ikke-nålestansede fibre, en station (36) til at afgive kernerne (11), som er tilvejebragt, med integrerede forbindende fibre.
DK10752888.7T 2009-07-28 2010-07-28 Fremgangsmåde til fremstilling af en kerne med integrerede forbindende fibre til paneler af kompositmateriale, panel tilvejebragt derved, samt apparatur DK2459362T3 (da)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0955260A FR2948693B1 (fr) 2009-07-28 2009-07-28 Procede de realisation d'une ame avec fibres de pontage integrees pour panneaux en materiaux composites, panneau obtenu et dispositif
PCT/FR2010/051601 WO2011015770A2 (fr) 2009-07-28 2010-07-28 Procede de realisation d'une ame avec fibres de pontage integrees pour panneaux en materiaux composites, panneau obtenu et dispositif

Publications (1)

Publication Number Publication Date
DK2459362T3 true DK2459362T3 (da) 2015-07-13

Family

ID=42116000

Family Applications (1)

Application Number Title Priority Date Filing Date
DK10752888.7T DK2459362T3 (da) 2009-07-28 2010-07-28 Fremgangsmåde til fremstilling af en kerne med integrerede forbindende fibre til paneler af kompositmateriale, panel tilvejebragt derved, samt apparatur

Country Status (22)

Country Link
US (1) US8914954B2 (da)
EP (1) EP2459362B1 (da)
JP (1) JP6008193B2 (da)
KR (1) KR101725296B1 (da)
CN (1) CN102497972B (da)
AU (1) AU2010280570B2 (da)
BR (1) BR112012001951A2 (da)
CA (1) CA2768870C (da)
DK (1) DK2459362T3 (da)
ES (1) ES2541837T3 (da)
FR (1) FR2948693B1 (da)
HR (1) HRP20150748T1 (da)
HU (1) HUE025043T2 (da)
MA (1) MA33443B1 (da)
MX (1) MX2012001184A (da)
PL (1) PL2459362T3 (da)
PT (1) PT2459362E (da)
RU (1) RU2543885C2 (da)
SI (1) SI2459362T1 (da)
TN (1) TN2012000041A1 (da)
WO (1) WO2011015770A2 (da)
ZA (1) ZA201200610B (da)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11059261B2 (en) * 2013-04-02 2021-07-13 Toray Industries, Inc. Sandwich laminate, sandwich structure and unified molded product using same and processes for producing both
US11173634B2 (en) 2018-02-01 2021-11-16 Ina Acquisition Corp Electromagnetic radiation curable pipe liner and method of making and installing the same
US10704728B2 (en) 2018-03-20 2020-07-07 Ina Acquisition Corp. Pipe liner and method of making same
RU2751171C1 (ru) * 2020-01-10 2021-07-09 Государственное предприятие "Запорожское машиностроительное конструкторское бюро "Прогресс" имени академика А.Г. Ивченко" Способ выполнения системы отверстий в многослойной заготовке
FR3107002B1 (fr) 2020-02-10 2024-03-01 Saertex France Procede de realisation d'une ame conformable pour la fabrication de produits en materiaux composites, ame conformable obtenue

Family Cites Families (33)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2132530A (en) * 1935-12-13 1938-10-11 Carthage Mills Inc Decorative needled fabric
US2840881A (en) * 1955-05-13 1958-07-01 Du Pont Article of manufacture and process of making same
US3059312A (en) * 1959-12-14 1962-10-23 Draper Brothers Company Composite laminated structures of high permeability
US3122141A (en) * 1962-03-29 1964-02-25 Johnson & Johnson Flexible absorbent sheet
US3451885A (en) * 1962-07-09 1969-06-24 Union Carbide Corp Needled composite web and method of making the same
BE668528A (da) * 1964-08-19 1900-01-01
US3395065A (en) * 1967-10-06 1968-07-30 Beacon Mfg Co Non-woven blanket fabric and method
AT296622B (de) * 1967-07-04 1972-02-25 Bayer Ag Hochbeanspruchbarer Schaumstoffkörper
US3839135A (en) * 1970-11-27 1974-10-01 Dow Badische Co Antistatic laminate filament and fabric prepared therefrom
US4047269A (en) * 1973-04-07 1977-09-13 Cikalon-Vliesstoff-Werke Gmbh Method and apparatus for producing ornamentally patterned, needled, nonwoven pile fabrics
US3976525A (en) * 1973-08-10 1976-08-24 Fiber Bond Corporation Method of making a needled scouring pad
US4053668A (en) * 1974-08-05 1977-10-11 Brunswick Corporation Tufted carpenting with unitary needlebonded backing and method of manufacturing the same
US3952126A (en) * 1975-03-20 1976-04-20 Dycks Christian C Resilient carpet padding sheet
DE3811778A1 (de) * 1987-04-08 1988-11-03 Sackner Prod Inc Waermeformbares integrales verbundmaterial und verfahren zu dessen herstellung
US4808461A (en) * 1987-12-14 1989-02-28 Foster-Miller, Inc. Composite structure reinforcement
FR2678547B1 (fr) * 1991-07-03 1995-03-10 Guy Leroy Procede et dispositif pour la realisation de nappes composites et composites obtenus.
FR2701665B1 (fr) * 1993-02-17 1995-05-19 Europ Propulsion Procédé de fabrication d'une pièce en matériau composite, notamment un panneau sandwich, à partir de plusieurs préformes assemblées.
EP0653984B1 (en) * 1993-05-04 2007-01-24 Foster-Miller, Inc. Truss reinforced foam core sandwich structure
US6027798A (en) * 1995-11-01 2000-02-22 The Boeing Company Pin-reinforced sandwich structure
JP3035649B2 (ja) * 1996-07-11 2000-04-24 双和化学産業株式会社 複合基材を使用した防水構造体
US6030907A (en) * 1996-07-29 2000-02-29 Sowa Chemical Co., Ltd. Composite substrate for plastic reinforcement, and fiber-reinforced plastic using such composite substrate
JP3113881B2 (ja) * 1996-07-29 2000-12-04 旭ファイバーグラス株式会社 樹脂強化用複合基材及び該複合基材を使用した繊維強化樹脂
US6105223A (en) * 1997-04-30 2000-08-22 The B. F. Goodrich Company Simplified process for making thick fibrous structures
US20020168503A1 (en) * 2000-12-11 2002-11-14 Daojie Dong Decorative and/or flame retardant laminates and/or polyolefin laminates and processes of manufacture thereof
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
JP2004060058A (ja) * 2002-07-24 2004-02-26 Mitsubishi Heavy Ind Ltd 複合材料用繊維基材
AU2003291688A1 (en) * 2002-11-01 2004-06-07 Bell Helicopter Textron Inc. Method and apparatus for z-direction reinforcement of composite laminates
US7622408B2 (en) * 2003-07-01 2009-11-24 Dzs, Llc Fabric-faced composites and methods for making same
FR2881442B1 (fr) * 2005-02-01 2007-08-10 Roy Guy Le Panneau composite, dispositif et procede pour fabriquer un tel panneau
US7493679B2 (en) * 2006-04-28 2009-02-24 Bgf Industries, Inc. Method for forming a relatively thick, lightweight, nonwoven insulating mat
JP2007301775A (ja) * 2006-05-09 2007-11-22 Kaneka Corp 自動車内装材用発泡積層シートおよび自動車内装材
FR2919879B1 (fr) * 2007-08-07 2010-09-17 Saint Gobain Vetrotex France S A Complexe aiguillete
FR2921076B1 (fr) 2007-09-18 2010-04-02 Roy Guy Le Panneau a forte resistance structurelle, dispositif et procede pour fabriquer un tel panneau

Also Published As

Publication number Publication date
WO2011015770A2 (fr) 2011-02-10
CN102497972A (zh) 2012-06-13
FR2948693A1 (fr) 2011-02-04
AU2010280570A1 (en) 2012-03-08
US8914954B2 (en) 2014-12-23
MX2012001184A (es) 2012-06-01
WO2011015770A3 (fr) 2011-03-31
RU2012106930A (ru) 2013-09-10
US20120121885A1 (en) 2012-05-17
KR20120052372A (ko) 2012-05-23
PT2459362E (pt) 2015-08-26
PL2459362T3 (pl) 2015-11-30
RU2543885C2 (ru) 2015-03-10
FR2948693B1 (fr) 2014-01-17
EP2459362B1 (fr) 2015-04-08
HUE025043T2 (en) 2016-01-28
AU2010280570B2 (en) 2016-11-03
HRP20150748T1 (hr) 2015-09-25
CA2768870A1 (fr) 2011-02-10
KR101725296B1 (ko) 2017-04-10
MA33443B1 (fr) 2012-07-03
JP2013500181A (ja) 2013-01-07
EP2459362A2 (fr) 2012-06-06
SI2459362T1 (sl) 2015-10-30
BR112012001951A2 (pt) 2016-03-15
ES2541837T3 (es) 2015-07-27
ZA201200610B (en) 2012-10-31
JP6008193B2 (ja) 2016-10-19
CN102497972B (zh) 2016-04-20
CA2768870C (fr) 2017-09-12
TN2012000041A1 (fr) 2013-09-19

Similar Documents

Publication Publication Date Title
WO2011012587A1 (en) Process for the production of a core with integrated bridging fibers for panels made of composite materials, panel that is obtained and device
DK2459362T3 (da) Fremgangsmåde til fremstilling af en kerne med integrerede forbindende fibre til paneler af kompositmateriale, panel tilvejebragt derved, samt apparatur
EP0030129B1 (en) Reinforcement board
EP2295235B1 (en) Fiber reinforced plastic-structure and a method to produce the fiber reinforced plastic-structure
CN109641409B (zh) 由带有基底的预制元件制成的带状物及其生产方法
CN102325646A (zh) 通过嵌入预固化纤维增强树脂层制造风轮机叶片的方法
WO2008057376A3 (en) Multi-layer process and apparatus for producing high strength fiber-reinforced structural cementitious panels with enhanced fiber content
MXPA06013109A (es) Estructura intercalada reforzada.
RU2552478C2 (ru) Способ изготовления композиционного материала, композиционный материал и конечный продукт
EP3548243B1 (en) Floor tile and process for manufacturing thereof
US20150317972A1 (en) Loudspeaker membrane and method for manufacturing such a membrane
CN106103068B (zh) 用于制造相互交叉的中空加固结构的方法
EP1937468B1 (en) Formable core material
CA1178411A (en) Manufacture of springs of fibre reinforced composite material
CN114536879A (zh) 一种微纳胶体纤维混凝结构及其加工方法
CN204566829U (zh) Frp管道
US20170225124A1 (en) Hollow-Fiber Membrane Device and Method For The Production Thereof
CN104401068A (zh) Frp管道及制作工艺
CN111566064B (zh) 具有改进的疲劳性能的纤维增强的材料
US8333340B2 (en) System and method for reinforcing a substrate
CN116459589B (zh) 一种ptfe乳液浸渍高精度耐高温滤料的生产方法
WO2012028619A1 (en) Method for producing a composite panel and composite panel
US20120012245A1 (en) Production method for a panel
EP2407304A1 (en) Production method for a panel
RU81551U1 (ru) Многослойное изолирующие изделие из минерального волокна