BRPI0511009A - armação de janela para aeronave - Google Patents

armação de janela para aeronave

Info

Publication number
BRPI0511009A
BRPI0511009A BRPI0511009-2A BRPI0511009A BRPI0511009A BR PI0511009 A BRPI0511009 A BR PI0511009A BR PI0511009 A BRPI0511009 A BR PI0511009A BR PI0511009 A BRPI0511009 A BR PI0511009A
Authority
BR
Brazil
Prior art keywords
window frame
frame
aircraft window
window
flange
Prior art date
Application number
BRPI0511009-2A
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 BRPI0511009A publication Critical patent/BRPI0511009A/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
    • 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

Abstract

ARMAçãO DE JANELA PARA AERONAVE. Uma armação de janela (1) para instalação no revestimento externo (5) de uma aeronave compreende pelo menos um flange externo (2), um flange interno (3) e um flange vertical (4) disposto em sentido perpendicular a e entre estes flanges, pelo que a 1igação com a estrutura da aeronave ocorre por meio do flange externo (2) e pelo que é fixado no flange interno (3) o elemento de janela a ser retido, que é retido por meio do flange vertical (4). A armação de janela (1) compreende uma resina reforçada com peças semi-acabadas de uma trama de fibras, pelo que a progressão das camadas de trama nas três regiões do flange externo, do flange interno e do flange vertical, respectivamente, segue a direção de carga mecânica. Para a fabricação, uma peça semi-acabada (10) fabricada a partir de uma trama reforçada (20, 21, 22) é inserida em uma ferramenta de moldagem (11), na qual, sob pressão e temperatura, a resina é injetada, e o componente fabricado desta maneira é endurecido em seguida na ferramenta de moldagem.
BRPI0511009-2A 2004-05-24 2005-05-24 armação de janela para aeronave BRPI0511009A (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE102004025380A DE102004025380B4 (de) 2004-05-24 2004-05-24 Fensterrahmen für Flugzeuge
US60010104P 2004-08-09 2004-08-09
PCT/EP2005/005605 WO2005115839A1 (en) 2004-05-24 2005-05-24 Window frame for aircraft

Publications (1)

Publication Number Publication Date
BRPI0511009A true BRPI0511009A (pt) 2007-11-20

Family

ID=35433005

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0511009-2A BRPI0511009A (pt) 2004-05-24 2005-05-24 armação de janela para aeronave

Country Status (10)

Country Link
US (1) US20080054122A1 (pt)
EP (1) EP1748924B1 (pt)
JP (1) JP2008500232A (pt)
CN (1) CN100447051C (pt)
AT (1) ATE425080T1 (pt)
BR (1) BRPI0511009A (pt)
CA (1) CA2565495A1 (pt)
DE (2) DE102004025380B4 (pt)
RU (1) RU2376196C2 (pt)
WO (1) WO2005115839A1 (pt)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7249943B2 (en) 2003-08-01 2007-07-31 Alliant Techsystems Inc. Apparatus for forming composite stiffeners and reinforcing structures
US20100096063A1 (en) * 2006-11-13 2010-04-22 Friddell S Douglas Inspectability of composite items
CA2675274C (en) * 2007-01-12 2015-10-27 The Nordam Group, Inc. Aircraft window erosion shield
FR2920743B1 (fr) * 2007-09-07 2009-12-18 Airbus France Cadre de structure en materiau composite et fuselage d'aeronef comportant un tel cadre
DE102008008386A1 (de) 2008-02-09 2009-08-13 Airbus Deutschland Gmbh Verfahren zur Herstellung eines FVW-Bauteils
US8709576B2 (en) 2008-11-21 2014-04-29 Airbus Operations (Sas) Curved structural part made of composite material and a process for manufacturing such a part
US8969223B2 (en) * 2009-10-01 2015-03-03 Albany Engineered Composites, Inc. Woven preform, composite, and method of making thereof
US9662841B2 (en) 2009-11-10 2017-05-30 Orbital Atk, Inc. Radially extending composite structures
US8282757B2 (en) 2009-11-10 2012-10-09 Alliant Techsystems Inc. Automated composite annular structure forming
WO2012078179A1 (en) 2010-11-16 2012-06-14 The Nordam Group, Inc. Hybrid frame co-mold manufacture
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

Family Cites Families (18)

* 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
US3788162A (en) * 1972-05-31 1974-01-29 Univ Johns Hopkins Pseudo-isotropic filament disk structures
US3906669A (en) * 1973-03-02 1975-09-23 Lockheed Aircraft Corp Window assembly
FR2421056A1 (fr) * 1978-03-29 1979-10-26 Europ Propulsion Texture tridimensionnelle annulaire utilisable notamment comme renfort
WO1983001237A1 (en) * 1981-09-30 1983-04-14 Whitener, Philip, Charles Composite structures window belt and method of making
US5077110A (en) * 1988-10-19 1991-12-31 E. I. Du Pont De Nemours And Company Apparatus and method for shaping fiber reinforced resin matrix materials and product thereof
US6641893B1 (en) * 1997-03-14 2003-11-04 Massachusetts Institute Of Technology Functionally-graded materials and the engineering of tribological resistance at surfaces
AT404925B (de) * 1997-07-25 1999-03-25 Fischer Adv Components Gmbh Fenstereinheit für flugzeugkabinen
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
EP1342554B1 (de) * 2002-03-08 2010-02-03 Airbus Deutschland GmbH Verfahren zum Herstellen textiler Vorformlinge aus textilen Halbzeugen
DE10251579B4 (de) * 2002-03-08 2012-02-02 Airbus Operations Gmbh Verfahren zur Herstellung einer umlaufenden dreidimensionalen Faserverstärkungsstruktur
US7014806B2 (en) * 2002-03-08 2006-03-21 Airbus Deutschland Gmbh Method for producing a three-dimensional fiber reinforced ring frame component
GB0213161D0 (en) * 2002-06-07 2002-07-17 Short Brothers Plc A fibre reinforced composite component
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
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
DE102006044093B4 (de) * 2006-09-20 2009-01-22 Airbus Deutschland Gmbh Scheibenersatz zum Ausfüllen eines Fensterrahmens

Also Published As

Publication number Publication date
CN1956883A (zh) 2007-05-02
DE102004025380A1 (de) 2005-12-22
RU2006143333A (ru) 2008-06-27
CN100447051C (zh) 2008-12-31
ATE425080T1 (de) 2009-03-15
RU2376196C2 (ru) 2009-12-20
EP1748924A1 (en) 2007-02-07
CA2565495A1 (en) 2005-12-08
DE102004025380B4 (de) 2011-01-13
DE602005013211D1 (de) 2009-04-23
JP2008500232A (ja) 2008-01-10
WO2005115839B1 (en) 2006-01-12
EP1748924B1 (en) 2009-03-11
US20080054122A1 (en) 2008-03-06
WO2005115839A1 (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.