DE602005025589D1 - Verfahren zur Herstellung einer monolithischen Lüfterhaube - Google Patents

Verfahren zur Herstellung einer monolithischen Lüfterhaube

Info

Publication number
DE602005025589D1
DE602005025589D1 DE602005025589T DE602005025589T DE602005025589D1 DE 602005025589 D1 DE602005025589 D1 DE 602005025589D1 DE 602005025589 T DE602005025589 T DE 602005025589T DE 602005025589 T DE602005025589 T DE 602005025589T DE 602005025589 D1 DE602005025589 D1 DE 602005025589D1
Authority
DE
Germany
Prior art keywords
skin
frames
longitudinal
hat frames
hat
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.)
Active
Application number
DE602005025589T
Other languages
English (en)
Inventor
Pleite Joaquin Gallego
Duque Jose Luis Fauste
Garcia Luis Rubio
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Defence and Space SA
Original Assignee
EADS Construcciones Aeronauticas SA
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by EADS Construcciones Aeronauticas SA filed Critical EADS Construcciones Aeronauticas SA
Publication of DE602005025589D1 publication Critical patent/DE602005025589D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/40—Shaping or impregnating by compression not applied
    • B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/44—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Composite Materials (AREA)
  • Mechanical Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Body Structure For Vehicles (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)
DE602005025589T 2005-03-30 2005-03-30 Verfahren zur Herstellung einer monolithischen Lüfterhaube Active DE602005025589D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP05381016A EP1707344B1 (de) 2005-03-30 2005-03-30 Verfahren zur Herstellung einer monolithischen Lüfterhaube

Publications (1)

Publication Number Publication Date
DE602005025589D1 true DE602005025589D1 (de) 2011-02-10

Family

ID=34942809

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602005025589T Active DE602005025589D1 (de) 2005-03-30 2005-03-30 Verfahren zur Herstellung einer monolithischen Lüfterhaube

Country Status (5)

Country Link
US (1) US20060290028A1 (de)
EP (1) EP1707344B1 (de)
AT (1) ATE493253T1 (de)
DE (1) DE602005025589D1 (de)
ES (1) ES2356319T3 (de)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9359061B2 (en) * 2005-10-31 2016-06-07 The Boeing Company Compliant stiffener for aircraft fuselage
DE102007004313B4 (de) * 2007-01-29 2015-01-15 Airbus Operations Gmbh Verfahren zur Herstellung eines Bauteils für ein Luft- oder Raumfahrzeug
US20080302912A1 (en) * 2007-06-08 2008-12-11 The Boeing Company Bladderless Mold Line Conformal Hat Stringer
US8043554B2 (en) * 2007-06-08 2011-10-25 The Boeing Company Manufacturing process using bladderless mold line conformal hat stringer
US8778117B2 (en) 2008-12-11 2014-07-15 Airbus Operations Gmbh Method for producing an integral, reinforced fibre composite component as well as a hollow fibre composite component
DE102008054540B4 (de) * 2008-12-11 2014-07-10 Airbus Operations Gmbh Verfahren zur Herstellung eines integralen, versteiften Faserverbundbauteils
ES2635122T3 (es) 2013-03-04 2017-10-02 Airbus Defence And Space Sa Capot monolítico mejorado de un motor de aeronave y método de fabricación
CN104875398A (zh) * 2015-06-17 2015-09-02 沈阳飞机工业（集团）有限公司 大曲率夹层结构复合材料异形零件的制作方法
EP3659774B1 (de) * 2017-07-25 2023-05-31 Subaru Corporation Verbundstoffmaterialformgestell und verbundstoffmaterialformverfahren

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3614618A1 (de) * 1986-04-30 1987-11-05 Messerschmitt Boelkow Blohm Schalenstruktur aus faserverstaerktem kunststoff
US5484277A (en) * 1989-12-26 1996-01-16 Mcdonnell Douglas Corporation Mandreless molding system
US5242523A (en) * 1992-05-14 1993-09-07 The Boeing Company Caul and method for bonding and curing intricate composite structures
US5664518A (en) * 1994-01-14 1997-09-09 Compsys, Inc. Composite structures and method of making composite structures
FR2771330B1 (fr) 1997-11-26 2004-02-27 Aerospatiale Procede de fabrication d'un panneau composite monolithique articule avec des moyens raidisseurs integres, panneau articule obtenu et capot articule dans un aeronef
US6458309B1 (en) * 1998-06-01 2002-10-01 Rohr, Inc. Method for fabricating an advanced composite aerostructure article having an integral co-cured fly away hollow mandrel
US6110567A (en) * 1999-01-27 2000-08-29 Scaled Composites, Inc. Composite structural panel having a face sheet reinforced with a channel stiffener grid
ES2185443B1 (es) * 2000-03-07 2004-09-01 Airbus España S.L. Procedimiento de fabricacion de piezas precuradas en material compuesto con rigidizadores aplicados en estado fresco.
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
ES2205961B2 (es) * 2001-02-13 2005-03-01 Eads Construcciones Aeronauticas, S.A. Procedimiento de fabricacion de elementos de material compuesto mediante la tecnoclogia del coencolado.

Also Published As

Publication number Publication date
ES2356319T3 (es) 2011-04-06
ATE493253T1 (de) 2011-01-15
EP1707344A1 (de) 2006-10-04
US20060290028A1 (en) 2006-12-28
EP1707344B1 (de) 2010-12-29

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