JP2007503533A5 - - Google Patents

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Publication number
JP2007503533A5
JP2007503533A5 JP2006524756A JP2006524756A JP2007503533A5 JP 2007503533 A5 JP2007503533 A5 JP 2007503533A5 JP 2006524756 A JP2006524756 A JP 2006524756A JP 2006524756 A JP2006524756 A JP 2006524756A JP 2007503533 A5 JP2007503533 A5 JP 2007503533A5
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JP
Japan
Prior art keywords
rotor blade
blade assembly
fibers
braided
longitudinal axis
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
JP2006524756A
Other languages
English (en)
Japanese (ja)
Other versions
JP4504374B2 (ja
JP2007503533A (ja
Filing date
Publication date
Priority claimed from US10/646,310 external-priority patent/US7165945B2/en
Application filed filed Critical
Publication of JP2007503533A publication Critical patent/JP2007503533A/ja
Publication of JP2007503533A5 publication Critical patent/JP2007503533A5/ja
Application granted granted Critical
Publication of JP4504374B2 publication Critical patent/JP4504374B2/ja
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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JP2006524756A 2003-08-22 2004-08-20 ロータブレードの編組翼桁とその製造方法 Expired - Fee Related JP4504374B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/646,310 US7165945B2 (en) 2003-08-22 2003-08-22 Braided spar for a rotor blade and method of manufacture thereof
PCT/US2004/027151 WO2005079184A2 (en) 2003-08-22 2004-08-20 Braided spar for a rotor blade and method of manufacture thereof

Publications (3)

Publication Number Publication Date
JP2007503533A JP2007503533A (ja) 2007-02-22
JP2007503533A5 true JP2007503533A5 (cg-RX-API-DMAC7.html) 2007-09-20
JP4504374B2 JP4504374B2 (ja) 2010-07-14

Family

ID=34194501

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2006524756A Expired - Fee Related JP4504374B2 (ja) 2003-08-22 2004-08-20 ロータブレードの編組翼桁とその製造方法

Country Status (5)

Country Link
US (1) US7165945B2 (cg-RX-API-DMAC7.html)
EP (1) EP1663779B1 (cg-RX-API-DMAC7.html)
JP (1) JP4504374B2 (cg-RX-API-DMAC7.html)
CA (1) CA2536668A1 (cg-RX-API-DMAC7.html)
WO (1) WO2005079184A2 (cg-RX-API-DMAC7.html)

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DE102011012675B4 (de) * 2011-02-28 2014-10-23 Munich Composites Gmbh Verfahren zum Herstellen einer Felge mit einer teilbaren Flechtvorrichtung
JP5738033B2 (ja) * 2011-03-28 2015-06-17 三菱重工業株式会社 複合材構造体の成形方法
WO2013037428A1 (de) 2011-09-14 2013-03-21 Bayerische Motoren Werke Aktiengesellschaft Fahrzeug-rad mit einer felge aus faserverstärktem kunststoffmaterial
JP6133307B2 (ja) 2011-10-17 2017-05-24 シークエント メディカル インコーポレイテッド 編組機及び使用方法
US8261648B1 (en) 2011-10-17 2012-09-11 Sequent Medical Inc. Braiding mechanism and methods of use
US9416668B2 (en) 2012-04-30 2016-08-16 United Technologies Corporation Hollow fan bladed with braided fabric tubes
EP2781734B1 (en) * 2013-03-20 2019-02-20 Siemens Aktiengesellschaft Rotor blade with a segmented supporting structure and method for manufacturing the rotor blade
GB201307066D0 (en) * 2013-04-18 2013-05-29 Airbus Operations Ltd Winglet and braided composite spar
US9745056B2 (en) * 2013-05-14 2017-08-29 Sikorsky Aircraft Corporation Main rotor blade with composite integral skin and cuff
KR20190058695A (ko) * 2014-02-21 2019-05-29 미쓰이금속광업주식회사 내장 캐패시터층 형성용 동장 적층판, 다층 프린트 배선판 및 다층 프린트 배선판의 제조 방법
US9890764B2 (en) * 2014-03-26 2018-02-13 General Electric Company Trailing edge cap for a rotor blade and method of manufacturing same
US10406763B2 (en) 2014-08-15 2019-09-10 Sikorsky Aircraft Corporation Rotor blade spar formation with automated fiber placement
US10589475B2 (en) 2014-09-23 2020-03-17 General Electric Company Braided blades and vanes having dovetail roots
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US10434687B2 (en) 2014-12-17 2019-10-08 Sikorsky Aircraft Corporation Composite laminate tooling and method of forming a composite part using the tooling
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US12232737B2 (en) 2016-03-17 2025-02-25 Eclipse Medical Limited Occluding anatomical structures
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KR20180031392A (ko) * 2016-09-20 2018-03-28 다이텍연구원 탄소섬유토우 프리프레그 브레이딩 튜브 프레임의 제조방법
FR3069185B1 (fr) * 2017-07-18 2020-07-24 Airbus Operations Sas Profil aerodynamique a noyau creux oblong arrondi en materiau composite renforce par un textile a fibres unidirectionnelles
EP3556544B1 (en) * 2018-04-17 2021-07-28 Ratier-Figeac SAS Propeller blade spar
GB2573285A (en) * 2018-04-27 2019-11-06 Airbus Operations Ltd Composite spar for a wing structure
CN112368134B (zh) * 2018-05-01 2023-05-02 通用电气公司 用于制造用于风力涡轮转子叶片的翼梁帽的方法
KR20220035104A (ko) * 2019-06-20 2022-03-21 갤럭틱 씨오., 엘엘씨 통합 인발 성형된 복합재 프로파일 및 이를 제조하기 위한 방법
EP3848488B1 (en) * 2020-01-08 2025-10-08 Ratier-Figeac SAS Propeller blade comprising a core and a braided cover of said core, bobbin and method for for braiding said braided cover
FR3111658B1 (fr) * 2020-06-18 2022-07-15 Safran Aircraft Engines Aube en matériau composite à renfort fibreux tissé tridimensionnel et peau tissée bidimensionnel et son procédé de fabrication
CN113459526B (zh) * 2021-06-30 2022-06-10 中国航空制造技术研究院 一种复合材料风扇叶片与金属包边的胶接成型方法
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