JP2006192904A5 - - Google Patents

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Publication number
JP2006192904A5
JP2006192904A5 JP2006057025A JP2006057025A JP2006192904A5 JP 2006192904 A5 JP2006192904 A5 JP 2006192904A5 JP 2006057025 A JP2006057025 A JP 2006057025A JP 2006057025 A JP2006057025 A JP 2006057025A JP 2006192904 A5 JP2006192904 A5 JP 2006192904A5
Authority
JP
Japan
Prior art keywords
skin
structure according
composite
laminated structure
composite laminate
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
JP2006057025A
Other languages
English (en)
Japanese (ja)
Other versions
JP2006192904A (ja
JP4266990B2 (ja
Filing date
Publication date
Priority claimed from US09/922,053 external-priority patent/US6645333B2/en
Priority claimed from US10/059,956 external-priority patent/US6676785B2/en
Application filed filed Critical
Publication of JP2006192904A publication Critical patent/JP2006192904A/ja
Publication of JP2006192904A5 publication Critical patent/JP2006192904A5/ja
Application granted granted Critical
Publication of JP4266990B2 publication Critical patent/JP4266990B2/ja
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

JP2006057025A 2001-08-02 2006-03-02 Ｚ軸繊維の頂部端部および底部端部を、複合積層体の頂部表面および底部表面それぞれに締め付ける方法 Expired - Fee Related JP4266990B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/922,053 US6645333B2 (en) 2001-04-06 2001-08-02 Method of inserting z-axis reinforcing fibers into a composite laminate
US10/059,956 US6676785B2 (en) 2001-04-06 2001-11-19 Method of clinching the top and bottom ends of Z-axis fibers into the respective top and bottom surfaces of a composite laminate

Related Parent Applications (1)

Application Number Title Priority Date Filing Date
JP2003516790A Division JP4510446B2 (ja) 2001-08-02 2002-08-02 Ｚ軸繊維の頂部端部および底部端部を、複合積層体の頂部表面および底部表面それぞれに締め付ける方法

Publications (3)

Publication Number Publication Date
JP2006192904A JP2006192904A (ja) 2006-07-27
JP2006192904A5 true JP2006192904A5 (enExample) 2007-07-26
JP4266990B2 JP4266990B2 (ja) 2009-05-27

Family

ID=26739403

Family Applications (2)

Application Number Title Priority Date Filing Date
JP2003516790A Expired - Fee Related JP4510446B2 (ja) 2001-08-02 2002-08-02 Ｚ軸繊維の頂部端部および底部端部を、複合積層体の頂部表面および底部表面それぞれに締め付ける方法
JP2006057025A Expired - Fee Related JP4266990B2 (ja) 2001-08-02 2006-03-02 Ｚ軸繊維の頂部端部および底部端部を、複合積層体の頂部表面および底部表面それぞれに締め付ける方法

Family Applications Before (1)

Application Number Title Priority Date Filing Date
JP2003516790A Expired - Fee Related JP4510446B2 (ja) 2001-08-02 2002-08-02 Ｚ軸繊維の頂部端部および底部端部を、複合積層体の頂部表面および底部表面それぞれに締め付ける方法

Country Status (7)

Country Link
EP (2) EP1412164B1 (enExample)
JP (2) JP4510446B2 (enExample)
AT (1) ATE509755T1 (enExample)
AU (1) AU2002319748B2 (enExample)
CA (1) CA2456017C (enExample)
MX (1) MXPA04000950A (enExample)
WO (1) WO2003011577A1 (enExample)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7105071B2 (en) 2001-04-06 2006-09-12 Ebert Composites Corporation Method of inserting z-axis reinforcing fibers into a composite laminate
US7785693B2 (en) * 2001-04-06 2010-08-31 Ebert Composites Corporation Composite laminate structure
US7056576B2 (en) * 2001-04-06 2006-06-06 Ebert Composites, Inc. 3D fiber elements with high moment of inertia characteristics in composite sandwich laminates
AU2004270389B2 (en) * 2003-09-08 2009-07-30 Evonik Rohm Gmbh Force-introduction point in core composites and method for producing said point using reinforcement elements that traverse the thickness of the core composite
DE20314187U1 (de) * 2003-09-08 2003-12-18 Roth, Matthias Alexander, Dipl.-Ing. Krafteinleitungsstelle in Kernverbunden mit in Dickenrichtung des Kernverbundes durchsetzenden Armierungselementen
US9511571B2 (en) * 2007-01-23 2016-12-06 The Boeing Company Composite laminate having a damping interlayer and method of making the same
EP2329939B1 (en) * 2009-12-07 2013-03-20 Groep Stevens International Sandwich panel and method for its manufacture
US20130330496A1 (en) * 2012-06-06 2013-12-12 General Electric Company Composite structure with low density core and composite stitching reinforcement
FR3029834B1 (fr) * 2014-12-10 2019-06-07 Doyen Entreprises Procede pour l'insertion et la mise en place de fils individuels au travers d'un panneau
JP6808946B2 (ja) * 2016-02-23 2021-01-06 三菱ケミカル株式会社 繊維強化複合材料成形品の製造方法
DE102016209140A1 (de) 2016-05-25 2017-11-30 Airbus Operations Gmbh Reparaturkonzept mit präimprägniertem gepinntem Schaumkern für Sandwich-Strukturkomponenten
DE102018216535A1 (de) * 2018-09-27 2020-04-02 AUNDE Achter & Ebels GmbH Verfahren zur Herstellung eines Sitzbezugs für einen Fahrzeugsitz gebildet aus einem Formstrickteil

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2762739A (en) * 1953-11-19 1956-09-11 Alexander C H Weiss Fiber-reinforced structural panel and method of making same
US2954001A (en) * 1957-05-03 1960-09-27 Luxenburg Julius Automatic eyelet attachment
FR1359354A (fr) * 1963-03-15 1964-04-24 Rhodiaceta Appareil pour la couture d'éléments plats à base de fils thermoplastiques
US3647606A (en) * 1969-11-21 1972-03-07 Union Carbide Corp Semirigid multilayer thermal insulation and method of making same
JPH01110944A (ja) * 1987-10-26 1989-04-27 Toyota Motor Corp Ｆｒｐ構造体
GB9014770D0 (en) * 1990-07-03 1990-08-22 Short Brothers Plc Manufacture of a composite material
JPH05138743A (ja) * 1991-11-25 1993-06-08 Sekisui Chem Co Ltd 軽量構造体及びその接続部の構造

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