BRPI0511011A - moldura de janela para aeronave - Google Patents

moldura de janela para aeronave

Info

Publication number
BRPI0511011A
BRPI0511011A BRPI0511011-4A BRPI0511011A BRPI0511011A BR PI0511011 A BRPI0511011 A BR PI0511011A BR PI0511011 A BRPI0511011 A BR PI0511011A BR PI0511011 A BRPI0511011 A BR PI0511011A
Authority
BR
Brazil
Prior art keywords
window frame
frame
aircraft window
window
flange
Prior art date
Application number
BRPI0511011-4A
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 BRPI0511011A publication Critical patent/BRPI0511011A/pt

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
    • B29C70/46—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
    • 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
    • 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
    • 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
    • Y10T428/24074—Strand or strand-portions

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Moulding By Coating Moulds (AREA)
  • Wing Frames And Configurations (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Window Of Vehicle (AREA)
  • Injection Moulding Of Plastics Or The Like (AREA)
  • Special Wing (AREA)
  • Separation By Low-Temperature Treatments (AREA)
  • Body Structure For Vehicles (AREA)

Abstract

MOLDURA DE JANELA PARA AERONAVE. Uma moldura de janela (1) para instalação no envoltório externo de uma aeronave compreende em cada caso pelo menos um flange externo (2), um flange interno (3), e um flange vertical (4) disposto de forma perpendicular a e entre esses flanges (2, 3), onde a conexão com a estrutura da aeronave (5) é realizada através do flange externo (2) e onde o flange interno (3), um elemento de janela (7, 8) a ser retido é fixado, que é retido através do flange vertical (4). A moldura de janela (1) compreende resina reforçada com feixes de fibra dispostos de forma unidirecional (20), onde o progresso dos feixes de fibra nas três regiões do flange externo (2), do flange interno (3) e do flange vertical (4) respectivamente, segue a direção da carga mecânica. Para fabricação, uma parte semi-acabada feita de feixes de fibra dispostos de maneira unidirecional é inserida em uma ferramenta de moldagem (11), na qual, sob pressão e temperatura, a resina é injetada, e o componente feito dessa maneira é endurecido subseqüentemente na ferramenta de moldagem (11).
BRPI0511011-4A 2004-05-24 2005-05-24 moldura de janela para aeronave BRPI0511011A (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE102004025378A DE102004025378B4 (de) 2004-05-24 2004-05-24 Fensterrahmen für Flugzeuge
US60010404P 2004-08-09 2004-08-09
PCT/EP2005/005604 WO2005115838A1 (en) 2004-05-24 2005-05-24 Window frame for aircraft

Publications (1)

Publication Number Publication Date
BRPI0511011A true BRPI0511011A (pt) 2007-11-20

Family

ID=35433004

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0511011-4A BRPI0511011A (pt) 2004-05-24 2005-05-24 moldura de janela para aeronave

Country Status (10)

Country Link
US (1) US7819360B2 (pt)
EP (1) EP1748923B1 (pt)
JP (1) JP4842934B2 (pt)
CN (1) CN100447050C (pt)
AT (1) ATE395253T1 (pt)
BR (1) BRPI0511011A (pt)
CA (1) CA2564167A1 (pt)
DE (2) DE102004025378B4 (pt)
RU (1) RU2376197C2 (pt)
WO (1) WO2005115838A1 (pt)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20100096063A1 (en) * 2006-11-13 2010-04-22 Friddell S Douglas Inspectability of composite items
US7988094B2 (en) 2007-01-12 2011-08-02 Scott Ernest Ostrem Aircraft window erosion shield
US8449709B2 (en) * 2007-05-25 2013-05-28 The Boeing Company Method of fabricating fiber reinforced composite structure having stepped surface
DE102010023265A1 (de) * 2010-06-09 2011-12-15 Howaldtswerke-Deutsche Werft Gmbh Verschlusskörper zum Verschließen einer Öffnung eines Wasserfahrzeugs
US8714486B2 (en) 2010-11-16 2014-05-06 The Nordam Group, Inc. Hybrid frame co-mold manufacture
GB201206885D0 (en) * 2012-04-19 2012-06-06 Cytec Tech Corp Composite materials
EP2842865B1 (en) * 2013-08-28 2019-12-18 Airbus Operations GmbH Window panel for an airframe and method of producing same
EP3312083B1 (en) * 2015-11-05 2021-10-20 Airbus Operations, S.L.U. Forming tool for manufacturing an aperture surrounding frame for an aircraft fuselage
US11235853B2 (en) * 2018-10-16 2022-02-01 Textron Innovations Inc. Aircraft windowed structure

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3356403A (en) * 1965-01-12 1967-12-05 August B Sak Modular construction and support means therefor
US3906669A (en) * 1973-03-02 1975-09-23 Lockheed Aircraft Corp Window assembly
EP0089337B1 (en) * 1981-09-30 1987-08-12 The Boeing Company Composite structures window belt and method of making
FR2632604B1 (fr) 1988-06-08 1991-07-12 Aerospatiale Cadre en materiau composite notamment pour fuselage d'aeronef, et son procede de fabrication
US5271581A (en) * 1992-05-29 1993-12-21 Irish Michael J Window clip for aircraft
DE4234038C2 (de) 1992-10-09 1997-07-03 Daimler Benz Aerospace Airbus Schalenbauteil aus Faserverbundwerkstoff
US5496602A (en) * 1994-11-22 1996-03-05 Dow-United Technologies Composite Products, Inc. Low resin content unidirectional fiber tape
US6318035B1 (en) * 1999-06-01 2001-11-20 Lockheed Martin Corporation Window frame assembly for use in an aircraft and associated method of manufacture
GB0113916D0 (en) * 2001-06-07 2001-08-01 Bae Systems Plc Adding glass to composite bonding surfaces
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
DE10251579B4 (de) * 2002-03-08 2012-02-02 Airbus Operations Gmbh Verfahren zur Herstellung einer umlaufenden dreidimensionalen Faserverstärkungsstruktur
GB0213161D0 (en) * 2002-06-07 2002-07-17 Short Brothers Plc A fibre reinforced composite component
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
DE10250826B4 (de) * 2002-10-31 2008-05-29 Airbus Deutschland Gmbh Verfahren zur Herstellung eines dreidimensionalen Preforms
JP4309748B2 (ja) * 2003-11-25 2009-08-05 シキボウ株式会社 航空機に用いられるｆｒｐ製窓枠用のドライプリフォーム

Also Published As

Publication number Publication date
EP1748923B1 (en) 2008-05-14
CA2564167A1 (en) 2005-12-08
CN1956881A (zh) 2007-05-02
EP1748923A1 (en) 2007-02-07
DE602005006793D1 (de) 2008-06-26
RU2006143857A (ru) 2008-06-27
RU2376197C2 (ru) 2009-12-20
DE102004025378B4 (de) 2011-01-13
CN100447050C (zh) 2008-12-31
US20080191095A1 (en) 2008-08-14
WO2005115838A1 (en) 2005-12-08
DE102004025378A1 (de) 2005-12-22
JP2008500231A (ja) 2008-01-10
US7819360B2 (en) 2010-10-26
ATE395253T1 (de) 2008-05-15
JP4842934B2 (ja) 2011-12-21

Similar Documents

Publication Publication Date Title
BRPI0511009A (pt) armação de janela para aeronave
BRPI0511011A (pt) moldura de janela para aeronave
BRPI0510635A (pt) moldura de janela para aeronave
FR2911112B1 (fr) Section de fuselage pour aeronef et aeronef comprenant une telle section
BRPI0511182A (pt) estrutura de janela para aeronave
DE602007007953D1 (de) Flugzeugtür
BRPI0822588A2 (pt) método para formar um componente de pneu com múltiplas camadas
GB2444694A (en) Window assembly retaining system
WO2007042038A3 (en) A window element, a profiled pultruded panel, a system of a profiled pultruded panel and one or more fixation elements, a covering of a building or a house, a building or a house, a method of providing an outer weather resistant covering, and a building element
DE602007001960D1 (de) Gepäckraum, insbesondere abgedichteter raum für eine flugzeugkabine
BRPI0403587A (pt) Mecanismo de instalação de assento de passageiro em emenda de trilhos
GB2444668A (en) Optimal aircraft window shape for noise control
KR101268750B1 (ko) 엘리베이터 도어의 유리판 고정장치
ATE402033T1 (de) Panoramawindschutzschreibe für ein kraftfahrzeug
WO2006072749A3 (fr) Perfectionnement aux portes de cabines d’aeronefs
EP1790813A3 (de) Ecklageranordnung für Fenster, Türen oder dergleichen
ATE521781T1 (de) Verbundfensterflügel für fenster und fenstertüren mit entsprechendem stockprofil
JP5355507B2 (ja) 鉄道車両用袖仕切り構造及びその製造方法
ATE409271T1 (de) Glaswand
JP2010132423A (ja) エレベーターのドア装置
ATE479572T1 (de) Dichtung für kfz-tür oder kfz-fenster
ITTO20050909A1 (it) Profilo con strato biadesivo dotato di linguetta di distacco facilitato dello strato protettivo dello strato biadesivo stesso procedimento e dispositivi di realizzazione di tale linguetta
EP2157272A3 (en) Frame for a window, door or the like
GB2466786A (en) Glazing clip
DK1980702T3 (da) Rammekonstruktion til vinduer og/eller døre

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.