JP2008523264A5 - - Google Patents

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Publication number
JP2008523264A5
JP2008523264A5 JP2007545485A JP2007545485A JP2008523264A5 JP 2008523264 A5 JP2008523264 A5 JP 2008523264A5 JP 2007545485 A JP2007545485 A JP 2007545485A JP 2007545485 A JP2007545485 A JP 2007545485A JP 2008523264 A5 JP2008523264 A5 JP 2008523264A5
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JP
Japan
Prior art keywords
woven fabric
woven
integrally
preform
fabric
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
JP2007545485A
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English (en)
Japanese (ja)
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JP2008523264A (ja
JP4944790B2 (ja
Filing date
Publication date
Priority claimed from US11/007,600 external-priority patent/US7713893B2/en
Application filed filed Critical
Publication of JP2008523264A publication Critical patent/JP2008523264A/ja
Publication of JP2008523264A5 publication Critical patent/JP2008523264A5/ja
Application granted granted Critical
Publication of JP4944790B2 publication Critical patent/JP4944790B2/ja
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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JP2007545485A 2004-12-08 2005-11-10 ３次元で一体的に織成された強化パネル Expired - Fee Related JP4944790B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US11/007,600 2004-12-08
US11/007,600 US7713893B2 (en) 2004-12-08 2004-12-08 Three-dimensional woven integrally stiffened panel
PCT/US2005/040755 WO2006062670A1 (en) 2004-12-08 2005-11-10 Three-dimensional woven integrally stiffened panel

Publications (3)

Publication Number Publication Date
JP2008523264A JP2008523264A (ja) 2008-07-03
JP2008523264A5 true JP2008523264A5 (enExample) 2008-12-25
JP4944790B2 JP4944790B2 (ja) 2012-06-06

Family

ID=36574935

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2007545485A Expired - Fee Related JP4944790B2 (ja) 2004-12-08 2005-11-10 ３次元で一体的に織成された強化パネル

Country Status (19)

Country Link
US (1) US7713893B2 (enExample)
EP (1) EP1828455B1 (enExample)
JP (1) JP4944790B2 (enExample)
KR (1) KR101240922B1 (enExample)
CN (1) CN101087909B (enExample)
AT (1) ATE460520T1 (enExample)
AU (1) AU2005314504B2 (enExample)
BR (1) BRPI0517154B1 (enExample)
CA (1) CA2589557C (enExample)
DE (1) DE602005019915D1 (enExample)
ES (1) ES2341269T3 (enExample)
MX (1) MX2007006835A (enExample)
NO (1) NO20073509L (enExample)
PL (1) PL1828455T3 (enExample)
PT (1) PT1828455E (enExample)
RU (1) RU2386733C2 (enExample)
TW (1) TWI356858B (enExample)
WO (1) WO2006062670A1 (enExample)
ZA (1) ZA200704810B (enExample)

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CN102677318A (zh) * 2012-05-29 2012-09-19 蔡紫林 一种纺织面料
US9833930B2 (en) * 2012-10-23 2017-12-05 Albany Engineered Composites, Inc. Circumferential stiffeners for composite fancases
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US9290865B2 (en) * 2012-12-26 2016-03-22 Albany Engineered Composites, Inc. Three-dimensional woven corner fitting with lap joint preforms
FR3009315B1 (fr) * 2013-07-30 2015-12-18 Aircelle Sa Procede de fabrication d'une preforme tissee pour une poutre en materiaux composites disposant de renforts interieurs transversaux
CA2922198C (en) * 2013-09-04 2021-06-15 Biteam Ab Method and means for weaving a 3d fabric, 3d fabric items thereof and their use
KR102085893B1 (ko) * 2016-01-04 2020-03-06 알바니 엔지니어드 콤포짓스, 인크. 일체화된 틈 충전재를 갖는 예비성형체
US11131289B2 (en) * 2016-06-28 2021-09-28 Vestas Wind Systems A/S Manufacture of a wind turbine blade
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US10994468B2 (en) 2018-04-11 2021-05-04 Clemson University Research Foundation Foldable composite structures
CN109208155A (zh) * 2018-09-27 2019-01-15 西安工程大学 一种制备混纺纱线和三维织物预制件的方法
JP7439451B2 (ja) * 2019-10-28 2024-02-28 ウシオ電機株式会社 炭素繊維強化プラスチック構造体、その製造方法および測定器
US11492733B2 (en) * 2020-02-21 2022-11-08 Raytheon Technologies Corporation Weave control grid
GB202210823D0 (en) 2022-07-25 2022-09-07 Rolls Royce Plc Woven structure and method of manufacture
FR3141872A1 (fr) * 2022-11-10 2024-05-17 Safran Aircraft Engines Texture fibreuse comprenant deux portions de déploiement
FR3141873A1 (fr) * 2022-11-10 2024-05-17 Safran Aircraft Engines Texture fibreuse comprenant deux portions de déploiement
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US20250242557A1 (en) * 2024-01-30 2025-07-31 General Electric Company Composite structure for a turbine engine

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