DE60009259D1 - Verfahren zur Herstellung von vorgehärteten Teilen aus Verbundwerkstoff mit in frischem Zustand angewandten Versteifern - Google Patents

Verfahren zur Herstellung von vorgehärteten Teilen aus Verbundwerkstoff mit in frischem Zustand angewandten Versteifern

Info

Publication number
DE60009259D1
DE60009259D1 DE60009259T DE60009259T DE60009259D1 DE 60009259 D1 DE60009259 D1 DE 60009259D1 DE 60009259 T DE60009259 T DE 60009259T DE 60009259 T DE60009259 T DE 60009259T DE 60009259 D1 DE60009259 D1 DE 60009259D1
Authority
DE
Germany
Prior art keywords
composite material
base part
production
fresh state
hardened parts
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.)
Expired - Lifetime
Application number
DE60009259T
Other languages
English (en)
Other versions
DE60009259T2 (de
Inventor
Pancorbo Carlos Cerezo
Casado Rafael Dominguez
Castro Nodal Manuel De
Pastor Augusto Perez
Garcia Aquilino Garcia
Garcia Manuel Huertas
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 Operations SL
Original Assignee
Airbus Espana SL
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 Airbus Espana SL filed Critical Airbus Espana SL
Application granted granted Critical
Publication of DE60009259D1 publication Critical patent/DE60009259D1/de
Publication of DE60009259T2 publication Critical patent/DE60009259T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/18—Spars; Ribs; Stringers
    • B64C3/182—Stringers, longerons
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/18—Spars; Ribs; Stringers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/24—Moulded or cast structures
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/24—Condition, form or state of moulded material or of the material to be shaped crosslinked or vulcanised
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/24—Condition, form or state of moulded material or of the material to be shaped crosslinked or vulcanised
    • B29K2105/246—Uncured, e.g. green
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/001—Profiled members, e.g. beams, sections
    • B29L2031/003—Profiled members, e.g. beams, sections having a profiled transverse cross-section
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S264/00—Plastic and nonmetallic article shaping or treating: processes
    • Y10S264/42—Processes of molding involving cross linking
DE60009259T 2000-03-07 2000-07-26 Verfahren zur Herstellung von vorgehärteten Teilen aus Verbundwerkstoff mit in frischem Zustand angewandten Versteifern Expired - Lifetime DE60009259T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
ES200000551 2000-03-07
ES200000551A ES2185443B1 (es) 2000-03-07 2000-03-07 Procedimiento de fabricacion de piezas precuradas en material compuesto con rigidizadores aplicados en estado fresco.

Publications (2)

Publication Number Publication Date
DE60009259D1 true DE60009259D1 (de) 2004-04-29
DE60009259T2 DE60009259T2 (de) 2004-12-30

Family

ID=8492610

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60009259T Expired - Lifetime DE60009259T2 (de) 2000-03-07 2000-07-26 Verfahren zur Herstellung von vorgehärteten Teilen aus Verbundwerkstoff mit in frischem Zustand angewandten Versteifern

Country Status (6)

Country Link
US (1) US6508909B1 (de)
EP (1) EP1134070B1 (de)
AT (1) ATE262408T1 (de)
CA (1) CA2315541C (de)
DE (1) DE60009259T2 (de)
ES (1) ES2185443B1 (de)

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US7527222B2 (en) 2004-04-06 2009-05-05 The Boeing Company Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections
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US8016970B2 (en) * 2007-08-02 2011-09-13 The Boeing Company Method for applying a pre-cured composite strip to a composite component to minimize inconsistencies appearing on a surface of the composite component
US8042767B2 (en) * 2007-09-04 2011-10-25 The Boeing Company Composite fabric with rigid member structure
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ES2397727B1 (es) * 2010-10-28 2014-01-17 Airbus Operations, S.L. Retenedores reutilizables para coencolado de larguerillos no curados.
ITTO20110421A1 (it) * 2011-05-12 2012-11-13 Alenia Aeronautica Spa Elemento strutturale con ala avente bordo netto, e suo processo di fabbricazione
ES2400129B1 (es) * 2011-05-30 2014-06-18 Airbus Operations, S.L. Método de fabricación de larguerillos con forma de "t" con un ángulo diferente de 90� entre el alma y el pie
DE102011079943A1 (de) * 2011-07-27 2013-01-31 Airbus Operations Gmbh Vorrichtung zur Herstellung eines Klebebauteils mit Faserverbundkunststoffen sowie Verfahren
ES2415773B1 (es) * 2011-12-29 2014-09-02 Airbus Operations S.L. Método de fabricación de piezas de material compuesto con cambios de espesor
EP2889211B1 (de) * 2013-12-31 2018-10-24 Airbus Operations S.L. Flugzeugstruktur aus Verbundmaterial
GB2528080A (en) * 2014-07-08 2016-01-13 Airbus Operations Ltd Structure
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ES2926668T3 (es) * 2015-04-30 2022-10-27 Airbus Operations Sl Método de fabricación de estructuras de material compuesto con útiles de curado por fuera de la bolsa de vacío
EP3098585B1 (de) * 2015-05-28 2018-02-28 Airbus Operations, S.L. Inspektionsverfahren und -systeme zur detektion von lecks in vakuumbeutelanordnungen
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Also Published As

Publication number Publication date
EP1134070A1 (de) 2001-09-19
US6508909B1 (en) 2003-01-21
CA2315541A1 (en) 2001-09-07
DE60009259T2 (de) 2004-12-30
CA2315541C (en) 2007-10-23
EP1134070B1 (de) 2004-03-24
ATE262408T1 (de) 2004-04-15
ES2185443B1 (es) 2004-09-01
ES2185443A1 (es) 2003-04-16

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