ITTO20040410A1 - Procedimento per la fabbricazione di travi strutturali in composito per aeromobili. - Google Patents

Procedimento per la fabbricazione di travi strutturali in composito per aeromobili.

Info

Publication number
ITTO20040410A1
ITTO20040410A1 IT000410A ITTO20040410A ITTO20040410A1 IT TO20040410 A1 ITTO20040410 A1 IT TO20040410A1 IT 000410 A IT000410 A IT 000410A IT TO20040410 A ITTO20040410 A IT TO20040410A IT TO20040410 A1 ITTO20040410 A1 IT TO20040410A1
Authority
IT
Italy
Prior art keywords
aircrafts
composite
procedure
manufacture
structural beams
Prior art date
Application number
IT000410A
Other languages
English (en)
Inventor
Carmine Suriano
Original Assignee
Alenia Aeronautica Spa
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 Alenia Aeronautica Spa filed Critical Alenia Aeronautica Spa
Priority to IT000410A priority Critical patent/ITTO20040410A1/it
Publication of ITTO20040410A1 publication Critical patent/ITTO20040410A1/it
Priority to DE602005002300T priority patent/DE602005002300T2/de
Priority to EP05102276A priority patent/EP1609584B1/en
Priority to ES05102276T priority patent/ES2289653T3/es
Priority to US11/154,461 priority patent/US20060011289A1/en

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
    • B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/34—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
    • B29C70/345—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation using matched moulds
    • 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
    • B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/34—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
    • B29C70/342—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation using isostatic pressure

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)
IT000410A 2004-06-21 2004-06-21 Procedimento per la fabbricazione di travi strutturali in composito per aeromobili. ITTO20040410A1 (it)

Priority Applications (5)

Application Number Priority Date Filing Date Title
IT000410A ITTO20040410A1 (it) 2004-06-21 2004-06-21 Procedimento per la fabbricazione di travi strutturali in composito per aeromobili.
DE602005002300T DE602005002300T2 (de) 2004-06-21 2005-03-22 Ein Verfahren zur Herstellung eines strukturellen Verbundträgers für Flugzeuge
EP05102276A EP1609584B1 (en) 2004-06-21 2005-03-22 A method of manufacturing composite structural beams for aircraft
ES05102276T ES2289653T3 (es) 2004-06-21 2005-03-22 Metodo para fabricar vigas estructurales de material compuesto para aviones.
US11/154,461 US20060011289A1 (en) 2004-06-21 2005-06-16 Method of manufacturing composite structural beams for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT000410A ITTO20040410A1 (it) 2004-06-21 2004-06-21 Procedimento per la fabbricazione di travi strutturali in composito per aeromobili.

Publications (1)

Publication Number Publication Date
ITTO20040410A1 true ITTO20040410A1 (it) 2004-09-21

Family

ID=34939033

Family Applications (1)

Application Number Title Priority Date Filing Date
IT000410A ITTO20040410A1 (it) 2004-06-21 2004-06-21 Procedimento per la fabbricazione di travi strutturali in composito per aeromobili.

Country Status (5)

Country Link
US (1) US20060011289A1 (it)
EP (1) EP1609584B1 (it)
DE (1) DE602005002300T2 (it)
ES (1) ES2289653T3 (it)
IT (1) ITTO20040410A1 (it)

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Publication number Priority date Publication date Assignee Title
US7237506B2 (en) * 2005-05-04 2007-07-03 Dietz Dan L Multiple function animal bed
US20060249087A1 (en) * 2005-05-04 2006-11-09 Dietz Dan L Multiple function animal training system with extendable ramp
US7234415B2 (en) * 2005-05-04 2007-06-26 Dietz Dan L Multiple function animal furniture system
US7807005B2 (en) * 2006-02-02 2010-10-05 The Boeing Company Fabrication process for thermoplastic composite parts
US10449736B2 (en) 2006-02-02 2019-10-22 The Boeing Company Apparatus for fabricating thermoplastic composite parts
US8333858B2 (en) * 2006-02-02 2012-12-18 The Boeing Company Method for fabricating curved thermoplastic composite parts
US8491745B2 (en) * 2007-02-03 2013-07-23 The Boeing Company Method and material efficient tooling for continuous compression molding
US8691137B2 (en) * 2009-03-04 2014-04-08 The Boeing Company Method of molding partus using a tool sleeve for mold die
US9102103B2 (en) * 2006-02-02 2015-08-11 The Boeing Company Thermoplastic composite parts having integrated metal fittings and method of making the same
US10232532B1 (en) 2006-02-02 2019-03-19 The Boeing Company Method for fabricating tapered thermoplastic composite parts
DE102007015518A1 (de) * 2007-03-30 2008-10-02 Airbus Deutschland Gmbh Verfahren zur Herstellung von Profilteilen
ES2611033T3 (es) * 2007-04-30 2017-05-04 Airbus Operations S.L. Cajón de torsión multilargero integrado de material compuesto
ITTO20070434A1 (it) * 2007-06-18 2008-12-19 Alenia Aeronautica Spa Procedimento e attrezzo per la formatura e l'assemblaggio di longheroni non polimerizzati per gli stabilizzatori orizzontali di aeromobili
US7968169B2 (en) * 2007-08-07 2011-06-28 The Boeing Company Compound contoured composite beams and fabrication methods
ES2443917T3 (es) 2007-10-09 2014-02-21 Saab Ab Procedimiento y dispositivo para conformar un material compuesto
DE102007058727A1 (de) 2007-12-06 2009-06-10 Airbus Deutschland Gmbh Verfahren zur Herstellung eines FVW-Vorformlings aus einem Laminat mit zumindest zwei Prepreg-Lagen sowie Herstellungsvorrichtung für ein derartiges Verfahren
DE102008046991A1 (de) † 2008-09-12 2010-03-25 Mt Aerospace Ag Lasttragendes dickwandiges Faserverbundstrukturbauteil und Verfahren zu dessen Herstellung
DE102008042574B4 (de) 2008-10-02 2010-06-10 Airbus Deutschland Gmbh Vorrichtung zum Ablegen und Drapieren von Abschnitten einer Verstärkungsfaserstruktur zur Herstellung eines Profilvorformlings sowie Verfahren
DE102008057708B4 (de) * 2008-11-17 2012-09-13 Airbus Operations Gmbh Faserverbundvorformling, Faserverbundwerkstück und Verfahren zur Herstellung eines Faserverbundwerkstücks
DE102009060706B4 (de) * 2009-12-29 2014-12-04 Airbus Operations Gmbh Verfahren sowie Vorrichtung zur Herstellung einer Versteifungsstruktur für ein Flugzeugrumpfsegment sowie eine Versteifungsstruktur
US10821653B2 (en) * 2010-02-24 2020-11-03 Alexander M. Rubin Continuous molding of thermoplastic laminates
EP2415573B1 (en) * 2010-08-05 2012-10-31 Eurocopter Deutschland GmbH Method to produce a tapered composite preform
ES2432090B2 (es) * 2012-03-26 2015-04-27 Airbus Operations, S.L. Procedimiento de fabricación de piezas realizadas en material compuesto y dispositivo empleado.
CN103320770A (zh) * 2013-06-21 2013-09-25 光垒光电科技（上海）有限公司 气体喷淋头以及气相沉积反应腔
CA2966239C (en) * 2014-10-30 2022-08-16 Lm Wp Patent Holding A/S A shear web mould system comprising variable moulding plates
DE102015201349A1 (de) * 2015-01-27 2016-07-28 Bayerische Motoren Werke Aktiengesellschaft Formgebungswerkzeug und Verfahren zum Bearbeiten eines Vorformlings eines Faserverbundbauteils
HK1250693A1 (zh) * 2015-04-10 2019-01-11 Leonardo S.P.A. 用於借助共固化制造复合材料的强化面板的方法
JP6477720B2 (ja) * 2015-08-04 2019-03-06 三菱ケミカル株式会社 繊維強化プラスチック及びその製造方法
FR3081369B1 (fr) 2018-05-28 2020-05-08 Stelia Aerospace Dispositif et procede de mise en forme d'une piece d'ebauche pour la formation d'une piece thermoplastique structurelle
EP3822068B1 (en) * 2019-11-13 2023-07-19 Airbus Operations, S.L.U. Device and method for forming a composite laminate for obtaining a z-shaped profile

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2268704B (en) * 1992-07-16 1996-01-10 British Aerospace Layup preparation for fibre reinforced composites
US5954898A (en) * 1994-05-13 1999-09-21 Lockheed Fort Worth Company Method and system for fabricating parts from composite materials
US5538589A (en) * 1994-08-31 1996-07-23 The Boeing Company Composite stringer assembly machine
US6217000B1 (en) * 1996-10-25 2001-04-17 The Boeing Company Composite fabrication method and tooling to improve part consolidation
JP4363741B2 (ja) * 2000-04-14 2009-11-11 本田技研工業株式会社 繊維強化複合材からなる中間成形物品の製造方法

Also Published As

Publication number Publication date
ES2289653T3 (es) 2008-02-01
EP1609584B1 (en) 2007-09-05
EP1609584A1 (en) 2005-12-28
DE602005002300T2 (de) 2008-05-29
DE602005002300D1 (de) 2007-10-18
US20060011289A1 (en) 2006-01-19

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