BRPI0511162A - método para fazer moldura de janela - Google Patents

método para fazer moldura de janela

Info

Publication number
BRPI0511162A
BRPI0511162A BRPI0511162-5A BRPI0511162A BRPI0511162A BR PI0511162 A BRPI0511162 A BR PI0511162A BR PI0511162 A BRPI0511162 A BR PI0511162A BR PI0511162 A BRPI0511162 A BR PI0511162A
Authority
BR
Brazil
Prior art keywords
window frame
semi
fiber bundles
molding tool
mesh material
Prior art date
Application number
BRPI0511162-5A
Other languages
English (en)
Inventor
Jens Bold
Original Assignee
Airbus Gmbh
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 Gmbh filed Critical Airbus Gmbh
Publication of BRPI0511162A publication Critical patent/BRPI0511162A/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/14—Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
    • B64C1/1476—Canopies; Windscreens or similar transparent elements
    • B64C1/1492—Structure and mounting of the transparent elements in the window or windscreen
    • 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
    • B29C70/46—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
    • B29C70/48—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs and impregnating the reinforcements in the closed mould, e.g. resin transfer moulding [RTM], e.g. by vacuum
    • 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
    • B29L2031/005—Profiled members, e.g. beams, sections having a profiled transverse cross-section for making window frames
    • 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
    • B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
    • B29L2031/3076—Aircrafts
    • B29L2031/3082—Fuselages
    • 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
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24058—Structurally defined web or sheet [e.g., overall dimension, etc.] including grain, strips, or filamentary elements in respective layers or components in angular relation
    • 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
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24058—Structurally defined web or sheet [e.g., overall dimension, etc.] including grain, strips, or filamentary elements in respective layers or components in angular relation
    • Y10T428/24124—Fibers
    • 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
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24174—Structurally defined web or sheet [e.g., overall dimension, etc.] including sheet or component perpendicular to plane of web or sheet

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Moulding By Coating Moulds (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Wing Frames And Configurations (AREA)
  • Injection Moulding Of Plastics Or The Like (AREA)
  • Woven Fabrics (AREA)
  • Laminated Bodies (AREA)

Abstract

MéTODO PARA FAZER MOLDURA DE JANELA Um método para fazer uma moldura de janela para instalação na carcaça exterior de uma aeronave, que compreende pelo menos um flange externo, um flange interno e um flange vertical dispostos perpendiculares a e entre esses dois flanges, contempla que primeiro uma parte semi-acabada compreendendo subestruturas individuais, múltiplas é feita, que em seguida é inserida em uma ferramenta de moldagem, dentro da qual, sob pressão e temperatura, resina é injetada, e que o componente feito desta maneira subseqüentemente é endurecido na ferramenta de moldagem. A parte semi-acabada tem uma estrutura de camada, que compreende um material de rede, feixes de fibra ou uma combinação de feixes de fibra e material de rede.
BRPI0511162-5A 2004-05-24 2005-05-24 método para fazer moldura de janela BRPI0511162A (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE102004025381.1A DE102004025381B4 (de) 2004-05-24 2004-05-24 Fensterrahmen für Flugzeuge
US60010304P 2004-08-09 2004-08-09
PCT/EP2005/005606 WO2005115728A1 (en) 2004-05-24 2005-05-24 Method for making window frame

Publications (1)

Publication Number Publication Date
BRPI0511162A true BRPI0511162A (pt) 2007-12-04

Family

ID=35433006

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0511162-5A BRPI0511162A (pt) 2004-05-24 2005-05-24 método para fazer moldura de janela

Country Status (9)

Country Link
US (1) US8096506B2 (pt)
EP (1) EP1748879A1 (pt)
JP (1) JP2008500233A (pt)
CN (1) CN1956837B (pt)
BR (1) BRPI0511162A (pt)
CA (1) CA2563574A1 (pt)
DE (1) DE102004025381B4 (pt)
RU (1) RU2006140137A (pt)
WO (1) WO2005115728A1 (pt)

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US20080060755A1 (en) * 2006-09-13 2008-03-13 General Electric Corporation composite corner and method for making composite corner
US20100096063A1 (en) * 2006-11-13 2010-04-22 Friddell S Douglas Inspectability of composite items
US7871486B2 (en) * 2006-11-21 2011-01-18 General Electric Company Methods for making structures having mounting flanges
FR2911111B1 (fr) * 2007-01-05 2009-02-13 Airbus France Sas Procede d'assemblage d'un hublot pour aeronef
CA2675206A1 (en) 2007-01-12 2008-07-24 The Nordam Group, Inc. Composite aircraft window frame
WO2008104614A1 (es) * 2007-02-28 2008-09-04 Airbus España, S.L. Utillaje y método de fabricación de cuadernas de aeronave en material compuesto
FR2913910B1 (fr) * 2007-03-19 2009-05-29 Skf Aerospace France Soc Par A Ensemble fibreux pour piece composite,piece composite et procede de fabrication d'une telle piece composite
US8449709B2 (en) 2007-05-25 2013-05-28 The Boeing Company Method of fabricating fiber reinforced composite structure having stepped surface
DE102007049347B8 (de) * 2007-10-12 2011-02-03 Eads Deutschland Gmbh Verfahren zur Herstellung eines Vorformlings aus Halbzeug, zur Herstellung eines ringförmigen Rahmenprofils, Verwendung des Vefahrens, sowie Rahmenprofil
FR2928343B1 (fr) 2008-03-10 2010-08-20 Airbus France Panneau du hublot et procede de fabrication d'un tel panneau aeronef comprenant un panneau de hublot
DE102008001826B3 (de) * 2008-05-16 2009-09-17 Airbus Deutschland Gmbh Ausschnittverstärkung für Kernverbunde sowie ein Verfahren zum Herstellen einer Ausschnittverstärkung für Kernverbunde
CN102666050B (zh) 2009-10-01 2015-09-16 奥尔巴尼工程两合公司 编织预制件、复合材料、及其制造方法
MX2012003670A (es) 2009-10-01 2012-06-27 Albany Eng Composites Inc Preformacion tejida, material compuesto y metodo de elaboracion de los mismos.
ES2568934T3 (es) 2010-01-18 2016-05-05 Airbus Helicopters Deutschland GmbH Un método de fabricación de una pieza de material compuesto reforzado
EP2384884A1 (en) * 2010-05-07 2011-11-09 Eurocopter Deutschland GmbH A method of fabricating a reinforced composite part and a reinforced composite part obtained with said method
CN102041954B (zh) * 2010-11-15 2012-06-20 陕西飞机工业（集团）有限公司 一种飞机舱内观察窗装饰罩装饰层的粘贴方法
EP2640919A4 (en) 2010-11-16 2018-01-10 The Nordam Group, Inc. Hybrid frame co-mold manufacture
FR2988324B1 (fr) * 2012-03-23 2014-04-25 Daher Aerospace Procede pour la fabrication d'un cadre de hublot en materiau composite a renfort fibreux et hublot obtenu par un tel procede
US9074408B2 (en) * 2012-06-06 2015-07-07 University Of Southern California Window assembly and construction module assembly using thermobimetals
US10239289B2 (en) * 2013-04-12 2019-03-26 Hexcel Corporation Multi-component composite structures
FR3040014B1 (fr) * 2015-08-14 2017-09-08 Conseil & Technique Procede de fabrication d’un cadre de forme annulaire
DE102016210891A1 (de) * 2016-06-17 2017-12-21 Zf Friedrichshafen Ag Verfahren und Anlage zur Herstellung eines Faserkunststoffverbundbauteils unter Verwendung von Sub-Preforms
DE102017221048A1 (de) * 2017-11-24 2019-05-29 Airbus Operations Gmbh Verfahren zur herstellung eines rahmenbauteils für eine türrahmenstruktur eines luftfahrzeugs, rahmenbauteil sowie türrahmenstruktur
US12358605B2 (en) * 2022-03-09 2025-07-15 The Boeing Company Vehicle window assembly
FR3143542A1 (fr) * 2022-12-15 2024-06-21 Airbus Operations (S.A.S.) Procédé de fabrication d’un cadre de hublot d’aéronef comportant une couche barrière, cadre de hublot obtenu à partir de ce procédé et aéronef comprenant au moins un tel cadre de hublot

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4046933A (en) * 1975-09-16 1977-09-06 Ppg Industries, Inc. Laminated window structure and its method of fabrication
GB2225227A (en) 1988-07-14 1990-05-30 Kiw International Limited Work platform and connector therefor
GB2225277B (en) * 1988-11-21 1992-11-18 United Technologies Corp Method of fabricating fiber reinforced composite articles by resin transfer molding
US6641893B1 (en) * 1997-03-14 2003-11-04 Massachusetts Institute Of Technology Functionally-graded materials and the engineering of tribological resistance at surfaces
FR2807737B1 (fr) * 2000-04-14 2002-07-12 Aerospatiale Matra Airbus Dispositif de prise de pression et son procede d'implantation sur un panneau de fuselage d'aeronef
US7014806B2 (en) * 2002-03-08 2006-03-21 Airbus Deutschland Gmbh Method for producing a three-dimensional fiber reinforced ring frame component
EP1342553B1 (de) * 2002-03-08 2016-05-18 Airbus Operations GmbH Verfahren zum Herstellen eines Fensterrahmens für Flugzeuge aus faserverstärktem Kunststoff und Vorrichtung zur Durchführung des Verfahrens
DE10251580B4 (de) * 2002-03-08 2013-01-10 Airbus Operations Gmbh Verfahren zum Herstellen eines Bauelementes aus faserverstärktem Kunststoff
US6736352B2 (en) * 2002-06-25 2004-05-18 The Boeing Company Aircraft windows and associated methods for installation
JP3943572B2 (ja) * 2002-08-12 2007-07-11 シキボウ株式会社 繊維強化複合材料用プリフォーム前駆体、繊維強化複合材料用プリフォームおよびその製造方法
JP4304948B2 (ja) * 2002-09-27 2009-07-29 東レ株式会社 強化繊維基材、プリフォームおよびそれよりなる繊維強化樹脂成形体ならびに繊維強化樹脂成形体の製造方法

Also Published As

Publication number Publication date
US20080197237A1 (en) 2008-08-21
DE102004025381B4 (de) 2014-01-23
CN1956837B (zh) 2011-04-27
RU2006140137A (ru) 2008-05-20
CN1956837A (zh) 2007-05-02
US8096506B2 (en) 2012-01-17
DE102004025381A1 (de) 2005-12-22
JP2008500233A (ja) 2008-01-10
EP1748879A1 (en) 2007-02-07
WO2005115728A1 (en) 2005-12-08
CA2563574A1 (en) 2005-12-08

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Legal Events

Date Code Title Description
B25D Requested change of name of applicant approved

Owner name: AIRBUS OPERATIONS GMBH (DE)

Free format text: NOME ALTERADO DE: AIRBUS DEUTSCHLAND GMBH

B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]

Free format text: REFERENTE A 8A ANUIDADE.

B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]

Free format text: REFERENTE AO DESPACHO 8.6 PUBLICADO NA RPI 2204 DE 02/04/2013.