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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)
  • Composite Materials (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (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)
  • Separation By Low-Temperature Treatments (AREA)
  • Special Wing (AREA)
  • Injection Moulding Of Plastics Or The Like (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
WO2009008903A1 (en) * 2007-01-12 2009-01-15 The Nordam Group, Inc. 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
CA2817200C (en) 2010-11-16 2019-01-08 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
ES2781182T3 (es) * 2015-11-05 2020-08-31 Airbus Operations Sl Procedimiento de fabricación de una cuaderna circundante de abertura para un fuselaje de aeronave, y cuaderna
US11235853B2 (en) * 2018-10-16 2022-02-01 Textron Innovations Inc. Aircraft windowed structure

Family Cites Families (17)

* 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
SU653169A1 (ru) * 1977-10-24 1979-03-25 Предприятие П/Я Г-4217 Судовой иллюминатор
DE3176353D1 (en) * 1981-09-30 1987-09-17 Boeing Co 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
DE10251579B4 (de) * 2002-03-08 2012-02-02 Airbus Operations Gmbh Verfahren zur Herstellung einer umlaufenden dreidimensionalen Faserverstärkungsstruktur
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
GB0213161D0 (en) * 2002-06-07 2002-07-17 Short Brothers Plc A fibre reinforced composite component
RU27049U1 (ru) * 2002-06-14 2003-01-10 Общество с органиченной ответственностью "ИФК - Джетс" Оконный модуль
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
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
JP2008500231A (ja) 2008-01-10
ATE395253T1 (de) 2008-05-15
WO2005115838A1 (en) 2005-12-08
RU2376197C2 (ru) 2009-12-20
EP1748923B1 (en) 2008-05-14
CA2564167A1 (en) 2005-12-08
CN100447050C (zh) 2008-12-31
CN1956881A (zh) 2007-05-02
US20080191095A1 (en) 2008-08-14
DE102004025378B4 (de) 2011-01-13
US7819360B2 (en) 2010-10-26
DE102004025378A1 (de) 2005-12-22
DE602005006793D1 (de) 2008-06-26
RU2006143857A (ru) 2008-06-27
EP1748923A1 (en) 2007-02-07
JP4842934B2 (ja) 2011-12-21

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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.