JP2006168718A5 - - Google Patents

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Publication number
JP2006168718A5
JP2006168718A5 JP2005353122A JP2005353122A JP2006168718A5 JP 2006168718 A5 JP2006168718 A5 JP 2006168718A5 JP 2005353122 A JP2005353122 A JP 2005353122A JP 2005353122 A JP2005353122 A JP 2005353122A JP 2006168718 A5 JP2006168718 A5 JP 2006168718A5
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JP
Japan
Prior art keywords
preform
integrated
sidewall
mold
preforms
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Application number
JP2005353122A
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English (en)
Japanese (ja)
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JP4236661B2 (ja
JP2006168718A (ja
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Publication date
Priority claimed from FR0413397A external-priority patent/FR2879496B1/fr
Application filed filed Critical
Publication of JP2006168718A publication Critical patent/JP2006168718A/ja
Publication of JP2006168718A5 publication Critical patent/JP2006168718A5/ja
Application granted granted Critical
Publication of JP4236661B2 publication Critical patent/JP4236661B2/ja
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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JP2005353122A 2004-12-16 2005-12-07 ヘリコプター回転翼フェアリングを製造するための方法及び装置、並びにそれによって得られたフェアリング Expired - Fee Related JP4236661B2 (ja)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0413397A FR2879496B1 (fr) 2004-12-16 2004-12-16 Procede et dispositif de fabrication d'une carene de rotor d'helicoptere, et carene obtenue

Publications (3)

Publication Number Publication Date
JP2006168718A JP2006168718A (ja) 2006-06-29
JP2006168718A5 true JP2006168718A5 (enExample) 2008-12-25
JP4236661B2 JP4236661B2 (ja) 2009-03-11

Family

ID=34951807

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2005353122A Expired - Fee Related JP4236661B2 (ja) 2004-12-16 2005-12-07 ヘリコプター回転翼フェアリングを製造するための方法及び装置、並びにそれによって得られたフェアリング

Country Status (5)

Country Link
US (1) US7676923B2 (enExample)
EP (1) EP1676775B1 (enExample)
JP (1) JP4236661B2 (enExample)
CN (1) CN100410144C (enExample)
FR (1) FR2879496B1 (enExample)

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2924378B1 (fr) * 2007-03-29 2010-01-01 Carbone Forge Procede de fabrication par moulage d'une piece composite thermoplastique.
DE102007015909A1 (de) * 2007-04-02 2008-10-09 Mt Aerospace Ag Verfahren zur Herstellung faserverstärkter Hohlkörper
GB2449907B (en) * 2007-06-07 2010-02-10 Gkn Aerospace Services Ltd Composite flange and method of making such flange
US8936695B2 (en) * 2007-07-28 2015-01-20 The Boeing Company Method for forming and applying composite layups having complex geometries
US20100279806A1 (en) * 2008-01-03 2010-11-04 Aling Lai Transmission structure improvement for bending tail pipe
CN102019592B (zh) * 2009-09-10 2012-07-04 中国航空工业集团公司北京航空制造工程研究所 一种大尺寸复合材料加筋壁板成形的定位装置
CN101791821B (zh) * 2010-04-08 2011-09-14 中国航空工业集团公司北京航空制造工程研究所 一种大尺寸复合材料长桁的成形装置
US8939395B2 (en) * 2010-09-09 2015-01-27 Groen Brothers Aviation, Inc. Tail fan apparatus and method for low speed yaw control of a rotorcraft
FR2968272B1 (fr) * 2010-12-06 2013-07-12 Eurocopter France Element de structure ameliore d'un giravion pour diminuer la trainee aerodynamique.
ITRM20110626A1 (it) * 2011-11-25 2013-05-26 Aeronautical Service S R L Metodo per la realizzazione di supporti di sostegno per l'avionica.
EP2706009B1 (en) 2012-09-07 2016-04-27 AIRBUS HELICOPTERS DEUTSCHLAND GmbH An empennage of a helicopter
EP2914488A4 (en) 2012-11-01 2016-06-29 Israel Aerospace Ind Ltd MANUFACTURE OF INTEGRATED STRUCTURES MADE FROM COMPOSITE MATERIALS
US8983171B2 (en) 2012-12-26 2015-03-17 Israel Aerospace Industries Ltd. System and method for inspecting structures formed of composite materials during the fabrication thereof
EP2878433B1 (en) * 2013-11-29 2016-04-20 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Shrouded rotary assembly from segmented composite for aircraft and method for its manufacture
PL3061689T3 (pl) * 2015-02-27 2018-01-31 Airbus Helicopters Deutschland GmbH Zespół ogonowy do wiropłatu, wiropłat i sposób wytwarzania wzmocnionego zespołu ogonowego
EP3199455B1 (en) * 2016-01-29 2020-04-22 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Rotary aircraft with an interface frame joining the fuselage tail boom and the tail cone
US10814971B2 (en) * 2018-04-10 2020-10-27 Textron Innovations Inc. Tail rotor housing
CN109130247B (zh) * 2018-07-20 2021-02-26 菲舍尔航空部件（镇江）有限公司 航空复材c型盒体零件成型方法
KR102215966B1 (ko) * 2019-08-21 2021-02-16 한국항공우주산업 주식회사 헬리콥터용 에프터 콘 핀 제조 장치
GB202020714D0 (en) * 2020-12-30 2021-02-10 Gen Electric Method of joining blade segments using an internal bladder
US20220315212A1 (en) * 2021-04-06 2022-10-06 Bell Textron Inc. Distributed propulsion structure
CN113977984B (zh) * 2021-10-15 2023-07-04 江西洪都航空工业集团有限责任公司 一种管状双曲面复合材料结构件的制备方法
CN115723949B (zh) * 2022-12-09 2025-08-19 哈尔滨飞机工业集团有限责任公司 一种高置涵道式尾部结构及其成型方法
US12097975B1 (en) * 2023-04-26 2024-09-24 James P Gross Tail boom support stand assembly
CN117140995B (zh) * 2023-08-23 2025-06-27 江苏新扬新材料股份有限公司 一种聚酰亚胺复合材料机尾罩的成型方法

Family Cites Families (16)

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Publication number Priority date Publication date Assignee Title
FR2542695B1 (fr) * 1983-03-18 1985-07-26 Aerospatiale Helice multipale a pas variable a pale s en materiaux composites demontables individuellement, procede de fabrication de telles pales et pales ainsi realisees
FR2556650B1 (fr) * 1983-12-14 1986-05-23 Matra Procede et dispositif de fabrication de corps structural creux en materiau composite, notamment pour missiles
US4594761A (en) * 1984-02-13 1986-06-17 General Electric Company Method of fabricating hollow composite airfoils
US4986949A (en) * 1986-05-12 1991-01-22 Trimble Brent J Method of making composite bicycle frames
FR2683504A1 (fr) * 1991-11-07 1993-05-14 Aerospatiale Systeme anticouple a rotor arriere pour helicoptere.
FR2699498B1 (fr) * 1992-12-23 1995-03-10 Eurocopter France Pale en composite thermoplastique, notamment pour rotor arrière caréné d'hélicoptère, et son procédé de fabrication.
FR2719553B1 (fr) * 1994-05-04 1996-07-26 Eurocopter France Dispositif anti-couple à rotor arrière et stator redresseur carénés pour hélicoptère.
WO1996009159A1 (en) * 1994-09-20 1996-03-28 Viatech, Inc. Method of making internally reinforced composite tubes
FR2740380B1 (fr) * 1995-10-30 1998-01-02 Eurocopter France Procede de fabrication d'une pale a pas variable en materiau composite pour rotor d'helicoptere
FR2740378B1 (fr) * 1995-10-30 1998-01-02 Eurocopter France Procede de fabrication d'une pale a pas variable en materiau composite pour rotor d'helicoptere, et pale a pas variable pouvant etre obtenue par un tel procede
FR2766407B1 (fr) * 1997-07-22 1999-10-15 Aerospatiale Procede de fabrication de pieces de grandes dimensions en materiau composite a matrice thermoplastique, telles que des troncons de fuselage d'aeronefs
US6372176B1 (en) * 1999-03-01 2002-04-16 Kiefel Technologies Inc. System and method for twin sheet forming
US6889937B2 (en) * 1999-11-18 2005-05-10 Rocky Mountain Composites, Inc. Single piece co-cure composite wing
DE10153875A1 (de) * 2001-11-02 2003-05-15 Bpw Bergische Achsen Kg Bauteil in langgestreckter Bauweise aus einem Faser-Kunststoff-Verbund
US7204951B2 (en) * 2002-07-30 2007-04-17 Rocky Mountain Composites, Inc. Method of assembling a single piece co-cured structure
EP1473131A3 (de) * 2003-04-30 2007-01-03 Airbus Deutschland GmbH Verfahren zum herstellen textiler vorformlinge aus textilen halbzeugen

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