BRPI0511182A - estrutura de janela para aeronave - Google Patents

estrutura de janela para aeronave

Info

Publication number
BRPI0511182A
BRPI0511182A BRPI0511182-0A BRPI0511182A BRPI0511182A BR PI0511182 A BRPI0511182 A BR PI0511182A BR PI0511182 A BRPI0511182 A BR PI0511182A BR PI0511182 A BRPI0511182 A BR PI0511182A
Authority
BR
Brazil
Prior art keywords
window frame
flange
aircraft window
holder units
outer flange
Prior art date
Application number
BRPI0511182-0A
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 BRPI0511182A publication Critical patent/BRPI0511182A/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

Abstract

ESTRUTURA DE JANELA PARA AERONAVE. Uma estrutura de janela (1) para instalação no invólucro exterior (5) de uma aeronave, estrutura esta que compreende pelo menos um flange externo (2), um flange interno (3), e um flange vertical (4) disposto perpendicular a e entre estes flanges, um flange vertical é fixado a um elemento de janela (7, 8) a ser preso. Este é fixado em sua posição por meio de uma pluralidade de elementos prendedores (10) distribuídos em eqüidistância sobre a periferia da estrutura de janela (1), os elementos prendedores (10) são conectados ao flange externo (2) da estrutura de janela. Cada um dos elementos prendedores (10) compreende uma chapa de base (11) com um pino (12) disposto perpendicular à superfície de chapa, assim como um grampo prendedor (13) que pode ser colocado em encaixe por ajuste de força com o pino (12). As superfícies externas do pino são providas com uma estrutura do tipo dente de serra, a qual é colocada em encaixe com os elementos de aperto (15) em forma de gancho formados de maneira flexível sobre o grampo prendedor (13) e sobre os quais um elemento de trava em forma de anel (14) se desloca. Os elementos prendedores (10) compreendem um material termoplástico que pode ser provido com fibras de reforço e são feitas por meio de fundição sob pressão. Antes da instalação da estrutura de janela (1) na aeronave, as chapas de base (11) dos elementos prendedores (10) são aderidas ao flange externo (2) da estrutura de janela (1), e, após a montagem, são rebitadas com estes elementos prendedores ao invólucro exterior (5) da aeronave.
BRPI0511182-0A 2004-05-24 2005-05-24 estrutura de janela para aeronave BRPI0511182A (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE102004025375A DE102004025375B4 (de) 2004-05-24 2004-05-24 Fensterrahmen für Flugzeuge
US60011104P 2004-08-09 2004-08-09
PCT/EP2005/005607 WO2005115840A1 (en) 2004-05-24 2005-05-24 Window frame for aircraft

Publications (1)

Publication Number Publication Date
BRPI0511182A true BRPI0511182A (pt) 2007-12-04

Family

ID=35433001

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0511182-0A BRPI0511182A (pt) 2004-05-24 2005-05-24 estrutura de janela para aeronave

Country Status (10)

Country Link
US (1) US7905452B2 (pt)
EP (1) EP1748926B1 (pt)
JP (1) JP4825799B2 (pt)
CN (1) CN100431920C (pt)
AT (1) ATE427882T1 (pt)
BR (1) BRPI0511182A (pt)
CA (1) CA2564781A1 (pt)
DE (1) DE102004025375B4 (pt)
RU (1) RU2378153C2 (pt)
WO (1) WO2005115840A1 (pt)

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US20080078876A1 (en) * 2006-08-15 2008-04-03 Baggette Phillip D Composite resin window frame constructions for airplanes
EP1932757B1 (en) * 2006-12-15 2016-10-26 Airbus Deutschland GmbH Bonded aluminium window frame on fibre metal laminate fuselage skin
US20080169380A1 (en) 2007-01-12 2008-07-17 The Nordam Group, Inc. Composite aircraft window frame
JP4969268B2 (ja) * 2007-02-19 2012-07-04 三菱重工業株式会社 航空機用窓材およびその製造方法
US7823833B2 (en) 2007-03-05 2010-11-02 The Boeing Company Window installation method and apparatus
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
FR2961485B1 (fr) * 2010-06-22 2013-03-29 Airbus Operations Sas Dispositif de fixation de systemes pour aeronef, destine a etre notamment utilise au niveau d'un hublot
CN101979229A (zh) * 2010-08-27 2011-02-23 国营江北机械厂 脆性复合陶瓷材料柔性装夹加工方法
EP2640919A4 (en) 2010-11-16 2018-01-10 The Nordam Group, Inc. Hybrid frame co-mold manufacture
US8616500B2 (en) * 2011-03-04 2013-12-31 The Boeing Company Diamond shaped window for composite and/or metallic airframe
EP2842865B1 (en) 2013-08-28 2019-12-18 Airbus Operations GmbH Window panel for an airframe and method of producing same
WO2016201087A1 (en) * 2015-06-09 2016-12-15 Gentex Corporation Retention of an electro-optic window assembly
US11407486B2 (en) * 2019-11-14 2022-08-09 The Boeing Company Window clamp system for a vehicle
DE102020000356B4 (de) * 2020-01-22 2021-08-12 Diehl Aviation Laupheim Gmbh Fenstereinheit für ein Flugzeug, Flugzeug mit der Fenstereinheit sowie Verfahren zur Montage der Fenstereinheit

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Publication number Priority date Publication date Assignee Title
US4364595A (en) * 1980-10-06 1982-12-21 Donnelly Mirrors, Inc. Vehicle window assembly
WO1983001237A1 (en) * 1981-09-30 1983-04-14 Whitener, Philip, Charles Composite structures window belt and method of making
US4793108A (en) * 1983-03-01 1988-12-27 The Boeing Company Enclosed interlayer plastic laminated window
DE3627536A1 (de) * 1986-08-13 1988-02-25 Ver Glaswerke Gmbh Fuer die direktverklebung vorgesehene glasscheibe, insbesondere autoglasscheibe
US4739955A (en) 1986-09-30 1988-04-26 The Boeing Company Aircraft cabin panel and insulation retainer with integrated use as a spacer-isolator
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Also Published As

Publication number Publication date
ATE427882T1 (de) 2009-04-15
US7905452B2 (en) 2011-03-15
WO2005115840A1 (en) 2005-12-08
EP1748926B1 (en) 2009-04-08
CN1956882A (zh) 2007-05-02
CN100431920C (zh) 2008-11-12
RU2378153C2 (ru) 2010-01-10
DE102004025375A1 (de) 2005-12-22
JP4825799B2 (ja) 2011-11-30
US20070075187A1 (en) 2007-04-05
CA2564781A1 (en) 2005-12-08
RU2006143335A (ru) 2008-06-27
DE102004025375B4 (de) 2010-01-28
EP1748926A1 (en) 2007-02-07
JP2008500234A (ja) 2008-01-10

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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 AO NAO RECOLHIMENTO DA 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.