JP2009500188A5 - - Google Patents

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Publication number
JP2009500188A5
JP2009500188A5 JP2008518742A JP2008518742A JP2009500188A5 JP 2009500188 A5 JP2009500188 A5 JP 2009500188A5 JP 2008518742 A JP2008518742 A JP 2008518742A JP 2008518742 A JP2008518742 A JP 2008518742A JP 2009500188 A5 JP2009500188 A5 JP 2009500188A5
Authority
JP
Japan
Prior art keywords
shell
doubler
reinforcing element
angle bracket
skin
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.)
Pending
Application number
JP2008518742A
Other languages
English (en)
Japanese (ja)
Other versions
JP2009500188A (ja
Filing date
Publication date
Priority claimed from DE102005030939A external-priority patent/DE102005030939A1/de
Application filed filed Critical
Publication of JP2009500188A publication Critical patent/JP2009500188A/ja
Publication of JP2009500188A5 publication Critical patent/JP2009500188A5/ja
Pending legal-status Critical Current

Links

JP2008518742A 2005-06-30 2006-06-30 ほぼシェル形の構成要素を製造する方法 Pending JP2009500188A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102005030939A DE102005030939A1 (de) 2005-06-30 2005-06-30 Verfahren zur Herstellung eines im Wesentlichen schalenförmigen Bauteils
PCT/EP2006/006384 WO2007003372A1 (en) 2005-06-30 2006-06-30 Process for producing a substantially shell-shaped component

Publications (2)

Publication Number Publication Date
JP2009500188A JP2009500188A (ja) 2009-01-08
JP2009500188A5 true JP2009500188A5 (enExample) 2012-01-05

Family

ID=36950577

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2008518742A Pending JP2009500188A (ja) 2005-06-30 2006-06-30 ほぼシェル形の構成要素を製造する方法

Country Status (9)

Country Link
US (1) US8580170B2 (enExample)
EP (1) EP1899149B1 (enExample)
JP (1) JP2009500188A (enExample)
CN (1) CN101203374B (enExample)
BR (1) BRPI0613477A2 (enExample)
CA (1) CA2611248A1 (enExample)
DE (2) DE102005030939A1 (enExample)
RU (1) RU2404059C2 (enExample)
WO (1) WO2007003372A1 (enExample)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
CN101870172B (zh) * 2010-06-09 2012-10-10 哈尔滨工业大学 飞机及航空器的碳纤维复合材料壳体的制备模具及其成形方法
CN101913250A (zh) * 2010-08-17 2010-12-15 沈阳飞机工业（集团）有限公司 方向舵壁板成型工艺
JP6403774B2 (ja) * 2013-08-09 2018-10-10 ザ・ボーイング・カンパニーＴｈｅ Ｂｏｅｉｎｇ Ｃｏｍｐａｎｙ 補強複合材パネル
ES2812608T3 (es) * 2015-04-30 2021-03-17 Airbus Operations Sl Método y molde para la fabricación de piezas de material compuesto
CN108995264B (zh) * 2018-05-28 2021-02-09 广西玉林华飞网络科技有限公司 一种epo无人机外壳加固方法及加固结构
CN108749028B (zh) * 2018-05-29 2019-10-08 沈阳飞机工业（集团）有限公司 一种常温固化耐高温辅助工装材料体系及其制造方法
US11446884B2 (en) * 2018-10-29 2022-09-20 Airbus Operations Gmbh Process for producing a component which is two-dimensional in regions from a fibre composite material
CN110524915A (zh) * 2019-09-05 2019-12-03 航天特种材料及工艺技术研究所 一种套接成型工装和套接成型方法
GB2615755A (en) * 2022-02-15 2023-08-23 Airbus Operations Ltd Fuel tank stringer with flow passage

Family Cites Families (16)

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Publication number Priority date Publication date Assignee Title
US1997718A (en) * 1934-08-03 1935-04-16 Claff Clarence Lloyd Folding box and method of making the same
GB884920A (en) * 1957-08-01 1961-12-20 Robert Frank Geiger Apparatus and method for metal adhesive bonding
US4331723A (en) * 1980-11-05 1982-05-25 The Boeing Company Advanced composite
US4813202A (en) * 1987-05-22 1989-03-21 Grumman Aerospace Corporation Structural members connected by interdigitating portions
CN1042692A (zh) * 1988-11-14 1990-06-06 通用电气公司 反转的飞机螺旋桨叶
JPH0310798A (ja) 1989-06-05 1991-01-18 Nec Corp 切断かしめ機構
JPH058316A (ja) 1991-07-05 1993-01-19 Mitsubishi Heavy Ind Ltd 複合材製構造体の製造方法
US5242523A (en) * 1992-05-14 1993-09-07 The Boeing Company Caul and method for bonding and curing intricate composite structures
FR2699499B1 (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 avec étape d'injection.
AU2001262912A1 (en) * 2000-02-25 2001-09-03 The Boeing Company Laminated composite radius filler
JP4318381B2 (ja) * 2000-04-27 2009-08-19 本田技研工業株式会社 繊維強化複合材からなる胴体構造体の製造方法、及びそれにより製造される胴体構造体
US6374570B1 (en) * 2000-08-25 2002-04-23 Lockheed Martin Corporation Apparatus and method for joining dissimilar materials to form a structural support member
RU2230406C2 (ru) * 2001-08-27 2004-06-10 Симонов Владимир Федорович Размеростабильное интегральное изделие из композиционных материалов, способ его изготовления и форма для осуществления способа
US6964723B2 (en) * 2002-10-04 2005-11-15 The Boeing Company Method for applying pressure to composite laminate areas masked by secondary features
MXPA06000874A (es) * 2003-07-24 2006-04-19 Tecomet Inc Espumas no aleatorias ensambladas.
US7052573B2 (en) * 2003-11-21 2006-05-30 The Boeing Company Method to eliminate undulations in a composite panel

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