BRPI0511162A - método para fazer moldura de janela - Google Patents
método para fazer moldura de janelaInfo
- 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
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)
- Laminated Bodies (AREA)
- Woven Fabrics (AREA)
- Injection Moulding Of Plastics Or The Like (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.
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) |
Families Citing this family (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
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 |
BRPI0806560A2 (pt) | 2007-01-12 | 2014-04-29 | Nordam Group Inc | Quadro de janela de aeronave composto. |
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 |
BR112012006935B1 (pt) | 2009-10-01 | 2020-01-14 | Albany Eng Composites Inc | pré-forma tecida tridimensional, compósito reforçado de fibra, métodos de formação de pré-forma tecida tridimensional e de compósito reforçado com fibra |
RU2550860C2 (ru) | 2009-10-01 | 2015-05-20 | Олбани Энджиниэрд Композитс, Инк. | Тканая заготовка, композитный материал, и способ их изготовления |
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 |
US8714486B2 (en) | 2010-11-16 | 2014-05-06 | 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 |
US20230286637A1 (en) * | 2022-03-09 | 2023-09-14 | 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 |
Family Cites Families (11)
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 |
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 |
US7014806B2 (en) * | 2002-03-08 | 2006-03-21 | Airbus Deutschland Gmbh | Method for producing a three-dimensional fiber reinforced ring frame component |
US6736352B2 (en) * | 2002-06-25 | 2004-05-18 | The Boeing Company | Aircraft windows and associated methods for installation |
EP1529865B1 (en) * | 2002-08-12 | 2009-01-28 | Shikibo Ltd. | Preform precursor for fiber-reinforced composite material, preform for fiber-reinforced composite material, and method of manufacturing the precursor and the preform |
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 |
-
2004
- 2004-05-24 DE DE102004025381.1A patent/DE102004025381B4/de not_active Expired - Fee Related
-
2005
- 2005-05-24 BR BRPI0511162-5A patent/BRPI0511162A/pt not_active IP Right Cessation
- 2005-05-24 CN CN200580016811XA patent/CN1956837B/zh active Active
- 2005-05-24 US US11/597,351 patent/US8096506B2/en active Active
- 2005-05-24 JP JP2007517109A patent/JP2008500233A/ja active Pending
- 2005-05-24 CA CA002563574A patent/CA2563574A1/en not_active Abandoned
- 2005-05-24 EP EP05742702A patent/EP1748879A1/en not_active Ceased
- 2005-05-24 RU RU2006140137/12A patent/RU2006140137A/ru not_active Application Discontinuation
- 2005-05-24 WO PCT/EP2005/005606 patent/WO2005115728A1/en not_active Application Discontinuation
Also Published As
Publication number | Publication date |
---|---|
US20080197237A1 (en) | 2008-08-21 |
CA2563574A1 (en) | 2005-12-08 |
RU2006140137A (ru) | 2008-05-20 |
DE102004025381B4 (de) | 2014-01-23 |
US8096506B2 (en) | 2012-01-17 |
JP2008500233A (ja) | 2008-01-10 |
EP1748879A1 (en) | 2007-02-07 |
DE102004025381A1 (de) | 2005-12-22 |
CN1956837A (zh) | 2007-05-02 |
CN1956837B (zh) | 2011-04-27 |
WO2005115728A1 (en) | 2005-12-08 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
BRPI0511162A (pt) | método para fazer moldura de janela | |
BRPI0914181A2 (pt) | método de fabricação de painel de vídeo | |
BRPI0600165A (pt) | processo de produção de um pneumático | |
BRPI0510635A (pt) | moldura de janela para aeronave | |
EP2112292B1 (de) | Dichtelement | |
BRPI0518077A (pt) | processo de fabricação de uma estrutura destinada à obtenção de um documento de segurança e/ou de valor ou para o aumento de segurança de um artigo e respectiva estrutura | |
BRPI0616452B8 (pt) | quinolinas e seu uso terapêutico | |
NO150021C (no) | Innretning for temporaer eller permanent tillukking av en kroppskanal eller et kroppshulrom | |
BRPI0706617A8 (pt) | Método para formar uma célula de combustível, sistema para formar uma célula de combustível, e, conjunto de eletrodo de membrana | |
BRPI0718450A8 (pt) | Método para testar a integridade de uma porção de corpo de tubulação flexível, método para ventilar uma região anular disposta entre uma camada de barreira e uma camada de vedação interna de uma porção de corpo de tubulação flexível e tubulação flexível | |
BRPI0705741A (pt) | dispositivo de bloco silenciador, procedimento e aparelho de fabricaçao | |
ATE380104T1 (de) | Faser-polymer-verbundstoff-(fpc)-material | |
BR112018076472A2 (pt) | lâmina de turbina eólica com juntas de cola melhoradas e método relacionado | |
BR112014030672A2 (pt) | método e montagem para reforçar e/ou revestir material poroso, método para ancorar um elemento de união e montagem para reforçar material poroso | |
BRPI0915802B8 (pt) | processo para produção de um filme diretamente em forma alveolar | |
BRPI0801556A2 (pt) | processo e dispositivo para o fechamento controlado de pelo menos um clipe em torno de uma seÇço de tranÇado sem material de enchimento entre duas seÇÕes de material de enchimento envolvidas por um invàlucro | |
BR112018001961A2 (pt) | composição, uso de uma composição, e, processos para produção de uma composição e de um artigo. | |
BR112012014352A2 (pt) | material de endurecimento de polímero termoplástico, e, método para fabricar uma parte de compósito | |
BR112017016276A2 (pt) | minerais engenheirados para uso como cargas de policarbonato e métodos de utilizá-los para reforçar policarbonatos | |
BR0113753A (pt) | Método para reforçar uma estrutura metálica existente | |
BR112015024403A2 (pt) | unidade que compreende uma placa de forma de concreto que inclui um abrigo e um elemento de reparo e método de reparo de uma placa de forma de concreto | |
BRPI0715735A2 (pt) | mÉtodo para administrar pelo menos um substÂncia que atua como agente de tratamento em material de planta, e, dispositivo para administrar pelo menos uma substÂncia em material de planta | |
BRPI0602188A (pt) | conjunto de cilindro para compressor e método de montagem para o mesmo | |
BR112013020094A2 (pt) | estrutura ferroviária e método de montagem | |
BR112017020692A2 (pt) | gaxeta laminada para vedação entre duas superfícies opostas, e método de fabricação de uma gaxeta laminada para vedação entre duas superfícies opostas |
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. |