NO20073931L - Fremgangsmate for fremstilling av en fiberforsterket sammenfoyning samt den oppnadde fiberforsterkede sammenfoyning - Google Patents
Fremgangsmate for fremstilling av en fiberforsterket sammenfoyning samt den oppnadde fiberforsterkede sammenfoyningInfo
- Publication number
- NO20073931L NO20073931L NO20073931A NO20073931A NO20073931L NO 20073931 L NO20073931 L NO 20073931L NO 20073931 A NO20073931 A NO 20073931A NO 20073931 A NO20073931 A NO 20073931A NO 20073931 L NO20073931 L NO 20073931L
- Authority
- NO
- Norway
- Prior art keywords
- laminate
- fiber
- fibers
- reinforced joint
- relates
- Prior art date
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
- B29C70/28—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
-
- 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
- B29C37/00—Component parts, details, accessories or auxiliary operations, not covered by group B29C33/00 or B29C35/00
- B29C37/0078—Measures or configurations for obtaining anchoring effects in the contact areas between layers
- B29C37/0082—Mechanical anchoring
-
- 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
- B29C70/40—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
- B29C70/44—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
- B29C70/443—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding and impregnating by vacuum or injection
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/08—Blades for rotors, stators, fans, turbines or the like, e.g. screw propellers
- B29L2031/082—Blades, e.g. for helicopters
- B29L2031/085—Wind turbine blades
-
- 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
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P70/00—Climate change mitigation technologies in the production process for final industrial or consumer products
- Y02P70/50—Manufacturing or production processes characterised by the final manufactured product
-
- 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
-
- 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
- Y10T428/23907—Pile or nap type surface or component
- Y10T428/23914—Interlaminar
-
- 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
- Y10T428/24124—Fibers
-
- 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
Abstract
Den foreliggende oppfinnelsen vedrører en fremgangsmåte for tilvirkning av et fiberarmert laminat (101), hvilke laminat innbefatter minst et området på overflaten av laminatet konfigurert med utragende fibere for skjoting til ett eller flere andre elementer. Dette blir oppnådd ved å anordne en hybridmatte (505) lengst ut i laminatet som innbefatter minst to lag med fibere (105) på tvers over skjøtoverflaten (402) til lagene. Det ytterste laget (301) til hybridmatten blir fjernet før skjoting, mens det innerste laget (506) av hybridmatten forblir en bestanddel av laminatet (101). Oppfinnelsen vedrører ulike fremgangsmåter for å fibere til å rage ut fra overflaten til laminatet, hvilke fibere således har en forsterkningseffekt på skjøtene. Oppfinnelsen vedrører også et laminat tilvirket ved hjelp av de beskrevne fremgangsmåter og et blad for et vindkraftanlegg innbefattende et slikt laminat.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DK200402014A DK176564B1 (da) | 2004-12-29 | 2004-12-29 | Fiberforstærket samling |
PCT/DK2005/000833 WO2006069581A1 (en) | 2004-12-29 | 2005-12-29 | Method of producing a fibre reinforced joint and fibre reinforced joint obtained thereby |
Publications (1)
Publication Number | Publication Date |
---|---|
NO20073931L true NO20073931L (no) | 2007-09-28 |
Family
ID=36054833
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
NO20073931A NO20073931L (no) | 2004-12-29 | 2007-07-26 | Fremgangsmate for fremstilling av en fiberforsterket sammenfoyning samt den oppnadde fiberforsterkede sammenfoyning |
Country Status (10)
Country | Link |
---|---|
US (1) | US8168027B2 (no) |
EP (1) | EP1841580B1 (no) |
CN (1) | CN100572025C (no) |
AU (1) | AU2005321685B2 (no) |
BR (1) | BRPI0519417B1 (no) |
CA (1) | CA2589144C (no) |
DK (2) | DK176564B1 (no) |
MX (1) | MX2007007953A (no) |
NO (1) | NO20073931L (no) |
WO (1) | WO2006069581A1 (no) |
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CN101168926A (zh) * | 2006-10-27 | 2008-04-30 | 韩楠林 | 一种纤维制品及其制造和应用方法 |
US7981495B2 (en) * | 2006-10-31 | 2011-07-19 | Invensys Systems, Inc. | Materials methodology to improve the delamination strength of laminar composites |
US8337163B2 (en) * | 2007-12-05 | 2012-12-25 | General Electric Company | Fiber composite half-product with integrated elements, manufacturing method therefor and use thereof |
FR2932410B1 (fr) * | 2008-06-11 | 2010-05-28 | Aircelle Sa | Procede de fabrication d'une piece a corps creux en materiau composite |
CN101391488B (zh) * | 2008-08-22 | 2010-06-09 | 成都飞机工业(集团)有限责任公司 | 非平板复合材料制件的固化成型方法与成型模 |
CN102216058B (zh) * | 2008-11-12 | 2014-02-26 | Lm玻璃纤维制品有限公司 | 涂敷凝胶涂层的方法及执行所述方法的设备 |
US8079820B2 (en) | 2008-12-18 | 2011-12-20 | General Electric Company | Blade module, a modular rotor blade and a method for assembling a modular rotor blade |
US8404162B2 (en) * | 2008-12-22 | 2013-03-26 | Florida State University Research Foundation | Composite materials and methods for selective placement of nano-particulates within composites |
EP2496534A1 (en) * | 2009-11-02 | 2012-09-12 | Dror Selivansky | Fiber-reinforced structures and processes for their manufacture |
CN101718250B (zh) * | 2010-01-11 | 2011-11-09 | 华锐风电科技(集团)股份有限公司 | 风力发电机组分段式风轮叶片及其装配方法 |
DE102010025068B4 (de) * | 2010-06-25 | 2016-07-28 | Airbus Defence and Space GmbH | Vorrichtung und Verfahren zur Herstellung von faserverstärkten Bauteilen |
DE102011006977A1 (de) * | 2011-04-07 | 2012-10-11 | Airbus Operations Gmbh | Verfahren zur Herstellung eines Faserverbundbauteils, Verstärkungselement sowie Faserverbundbauteil |
WO2012140049A2 (en) * | 2011-04-11 | 2012-10-18 | Lm Wind Power A/S | Wind turbine blade comprising cylindrical metal inserts in a root region thereof |
DK2697046T3 (en) * | 2011-04-11 | 2016-05-23 | Lm Wp Patent Holding As | Windmill blade with tapered root bushings |
US8834117B2 (en) * | 2011-09-09 | 2014-09-16 | General Electric Company | Integrated lightning receptor system and trailing edge noise reducer for a wind turbine rotor blade |
US10046528B2 (en) * | 2012-02-20 | 2018-08-14 | The Boeing Company | Composite layers with exposed reinforcement |
US9254622B2 (en) * | 2012-04-23 | 2016-02-09 | University Of Washington | Bond ply for adhesive bonding of composites and associated systems and methods |
US9297357B2 (en) | 2013-04-04 | 2016-03-29 | General Electric Company | Blade insert for a wind turbine rotor blade |
US9506452B2 (en) | 2013-08-28 | 2016-11-29 | General Electric Company | Method for installing a shear web insert within a segmented rotor blade assembly |
US20150258765A1 (en) * | 2014-03-17 | 2015-09-17 | The Boeing Company | Composite Structure and Method for Inspecting a Pre-bond Surface of a Composite Structure |
CN104552994B (zh) * | 2015-01-23 | 2017-01-11 | 南京航空航天大学 | Z-pin增强复合材料风电叶片及其制造方法 |
US9897065B2 (en) | 2015-06-29 | 2018-02-20 | General Electric Company | Modular wind turbine rotor blades and methods of assembling same |
US10337490B2 (en) | 2015-06-29 | 2019-07-02 | General Electric Company | Structural component for a modular rotor blade |
US10077758B2 (en) | 2015-06-30 | 2018-09-18 | General Electric Company | Corrugated pre-cured laminate plates for use within wind turbine rotor blades |
US10072632B2 (en) | 2015-06-30 | 2018-09-11 | General Electric Company | Spar cap for a wind turbine rotor blade formed from pre-cured laminate plates of varying thicknesses |
DE102015217310A1 (de) | 2015-09-10 | 2017-03-16 | Tesa Se | Verfahren zum Verbinden zweier faserverstärkter Kunststoffbauteile |
DE102015217312A1 (de) | 2015-09-10 | 2017-03-16 | Tesa Se | Klebeband, das insbesondere in einem Verfahren zum Verbinden zweier faserverstärkter Kunststoffbauteile eingesetzt werden kann |
US10107257B2 (en) | 2015-09-23 | 2018-10-23 | General Electric Company | Wind turbine rotor blade components formed from pultruded hybrid-resin fiber-reinforced composites |
US10113532B2 (en) | 2015-10-23 | 2018-10-30 | General Electric Company | Pre-cured composites for rotor blade components |
DE102015225467B4 (de) * | 2015-12-16 | 2019-12-19 | Airbus Defence and Space GmbH | Beschichtetes Verbundbauteil und Verfahren zum Herstellen eines beschichteten Verbundbauteils |
DE102016009640A1 (de) * | 2016-08-10 | 2018-02-15 | Senvion Gmbh | Gurt aus vorgefertigten Elementen mit Gelege und ein Verfahren zu seiner Fertigung |
US10422316B2 (en) | 2016-08-30 | 2019-09-24 | General Electric Company | Pre-cured rotor blade components having areas of variable stiffness |
FR3056438B1 (fr) | 2016-09-27 | 2019-11-01 | Coriolis Group | Procede de realisation de pieces en materiau composite par impregnation d'une preforme particuliere. |
GB2565350A (en) | 2017-08-11 | 2019-02-13 | Airbus Operations Ltd | Panel assembly |
FR3070623B1 (fr) * | 2017-09-04 | 2020-10-09 | Coriolis Composites | Procede de realisation d’une piece en materiau composite par aiguilletage oriente d’une preforme |
US10677216B2 (en) | 2017-10-24 | 2020-06-09 | General Electric Company | Wind turbine rotor blade components formed using pultruded rods |
US11738530B2 (en) | 2018-03-22 | 2023-08-29 | General Electric Company | Methods for manufacturing wind turbine rotor blade components |
DE102019115357B8 (de) * | 2019-06-06 | 2023-06-22 | Airbus Defence and Space GmbH | Fügeverfahren zum Zusammenfügen faserverstärkter Werkstücke sowie Bauteil und Luftfahrzeug |
GB201910566D0 (en) * | 2019-07-24 | 2019-09-04 | Blade Dynamics Ltd | Part element for a wind turbine blade and method for manufacturing a part element for a wind turbine blade |
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US5980665A (en) * | 1996-05-31 | 1999-11-09 | The Boeing Company | Z-pin reinforced bonds for connecting composite structures |
US5879492A (en) * | 1998-04-17 | 1999-03-09 | Northrop Grumman Corporation | Z-peel sheets |
US6645333B2 (en) * | 2001-04-06 | 2003-11-11 | Ebert Composites Corporation | Method of inserting z-axis reinforcing fibers into a composite laminate |
US20030041948A1 (en) * | 2001-08-31 | 2003-03-06 | Bersuch Larry R. | Co-cured joint with Z-pins |
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JP4908266B2 (ja) * | 2007-03-05 | 2012-04-04 | 株式会社ジャムコ | 段階状の断面厚さを有する複合材の連続成形方法 |
JP2009221390A (ja) * | 2008-03-18 | 2009-10-01 | Jamco Corp | 複合材連続成形用プリプレグピールプライ |
WO2010144159A1 (en) * | 2009-02-25 | 2010-12-16 | Templar Protection Group, Llc | Ballistic armor panel system |
-
2004
- 2004-12-29 DK DK200402014A patent/DK176564B1/da not_active IP Right Cessation
-
2005
- 2005-03-22 MX MX2007007953A patent/MX2007007953A/es active IP Right Grant
- 2005-12-29 EP EP20050822907 patent/EP1841580B1/en active Active
- 2005-12-29 DK DK05822907.1T patent/DK1841580T3/en active
- 2005-12-29 CA CA 2589144 patent/CA2589144C/en not_active Expired - Fee Related
- 2005-12-29 AU AU2005321685A patent/AU2005321685B2/en not_active Ceased
- 2005-12-29 CN CNB2005800453212A patent/CN100572025C/zh active Active
- 2005-12-29 BR BRPI0519417A patent/BRPI0519417B1/pt active IP Right Grant
- 2005-12-29 US US11/793,952 patent/US8168027B2/en active Active
- 2005-12-29 WO PCT/DK2005/000833 patent/WO2006069581A1/en active Application Filing
-
2007
- 2007-07-26 NO NO20073931A patent/NO20073931L/no not_active Application Discontinuation
Also Published As
Publication number | Publication date |
---|---|
CN100572025C (zh) | 2009-12-23 |
CA2589144C (en) | 2013-03-05 |
US20080160248A1 (en) | 2008-07-03 |
BRPI0519417B1 (pt) | 2017-04-11 |
CA2589144A1 (en) | 2006-07-06 |
MX2007007953A (es) | 2007-08-23 |
BRPI0519417A2 (pt) | 2009-01-20 |
DK176564B1 (da) | 2008-09-01 |
EP1841580B1 (en) | 2013-12-04 |
AU2005321685A1 (en) | 2006-07-06 |
CN101094753A (zh) | 2007-12-26 |
US8168027B2 (en) | 2012-05-01 |
DK1841580T3 (en) | 2014-03-03 |
EP1841580A1 (en) | 2007-10-10 |
WO2006069581A1 (en) | 2006-07-06 |
DK200402014A (da) | 2006-06-30 |
AU2005321685B2 (en) | 2011-11-17 |
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Legal Events
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