BRPI0619125B1 - porta de cabine pressurizada para aeronave de material composto de fibra - Google Patents

porta de cabine pressurizada para aeronave de material composto de fibra Download PDF

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Publication number
BRPI0619125B1
BRPI0619125B1 BRPI0619125A BRPI0619125A BRPI0619125B1 BR PI0619125 B1 BRPI0619125 B1 BR PI0619125B1 BR PI0619125 A BRPI0619125 A BR PI0619125A BR PI0619125 A BRPI0619125 A BR PI0619125A BR PI0619125 B1 BRPI0619125 B1 BR PI0619125B1
Authority
BR
Brazil
Prior art keywords
pressurized cabin
composite material
cabin door
fiber composite
door
Prior art date
Application number
BRPI0619125A
Other languages
English (en)
Inventor
Schmiedel Patrik
Hänsch Peter
Müller Reinhard
Braun Richard
Original Assignee
Airbus Helicopters Deutschland GmbH
Eurocopter Deutschland
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 Helicopters Deutschland GmbH, Eurocopter Deutschland filed Critical Airbus Helicopters Deutschland GmbH
Publication of BRPI0619125A2 publication Critical patent/BRPI0619125A2/pt
Publication of BRPI0619125B1 publication Critical patent/BRPI0619125B1/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
    • B64C1/1407—Doors; surrounding frames
    • B64C1/1461—Structures of doors or surrounding 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Laminated Bodies (AREA)
  • Moulding By Coating Moulds (AREA)
  • Body Structure For Vehicles (AREA)
  • Securing Of Glass Panes Or The Like (AREA)

Abstract

porta de cabine pressurizada para aeronave de material composto de fibra. a presente invenção refere-se a porta de cabine pressurizada para aeronave com uma direção de altura (x), de largura (y) e de profundidade (z) compreendendo: uma unidade integral de estrutura de porta (2) constituída de material composto de fibra, que apresenta uma película externa (4) e uma armação de porta disposta sobre o lado interno da película externa (4), armação esta que possui como elementos essenciais de sustentação suportes de borda (6a, 6b) e suportes longitudinais (8a-8f) correndo em direção da largura (y), que se estendem entre os suportes de borda (6a, 6b), sendo que os espaços intermediários da armação de porta (2a), que estão delimitados pelo lado interno da película externa (4), pelos suportes de borda (6a, 6b) e pelos suportes longitudinais (8a-8f), estão projetados abertos na direção do lado interno da porta.
BRPI0619125A 2005-12-02 2006-12-01 porta de cabine pressurizada para aeronave de material composto de fibra BRPI0619125B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE102005057907.8 2005-12-02
DE102005057907A DE102005057907B4 (de) 2005-12-02 2005-12-02 Luftfahrzeug-Druckkabinentür aus Faserverbundwerkstoff
PCT/DE2006/002138 WO2007062641A2 (de) 2005-12-02 2006-12-01 Luftfahrzeug-druckkabinentür aus faserverbundwerkstoff

Publications (2)

Publication Number Publication Date
BRPI0619125A2 BRPI0619125A2 (pt) 2011-09-13
BRPI0619125B1 true BRPI0619125B1 (pt) 2020-04-28

Family

ID=37734870

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0619125A BRPI0619125B1 (pt) 2005-12-02 2006-12-01 porta de cabine pressurizada para aeronave de material composto de fibra

Country Status (9)

Country Link
US (1) US9168996B2 (pt)
EP (1) EP1957360B1 (pt)
JP (1) JP4943449B2 (pt)
CN (1) CN101321664B (pt)
BR (1) BRPI0619125B1 (pt)
CA (1) CA2632264C (pt)
DE (1) DE102005057907B4 (pt)
RU (1) RU2415051C2 (pt)
WO (1) WO2007062641A2 (pt)

Families Citing this family (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2927686B1 (fr) * 2008-02-20 2010-10-08 Eads Socata Panneau composite monolithique auto-raidi et pivotant, notamment pour une partie mobile d'aeronef.
FR2928620B1 (fr) * 2008-03-14 2012-02-03 Latecoere Panneau ouvrant d'aeronef, notamment une porte de cabine d'avion
DE102009060876A1 (de) * 2009-12-30 2011-07-14 IMA Materialforschung und Anwendungstechnik GmbH, 01109 Luft- oder Raumfahrzeughülle
DE102010014265B4 (de) * 2010-04-08 2013-01-31 Deutsches Zentrum für Luft- und Raumfahrt e.V. Türrahmenanordnung mit einer Tür für einen Rumpf insbesondere für Luft- oder Raumfahrzeuge
EP2415662B1 (en) 2010-08-02 2012-07-18 Eurocopter Deutschland GmbH Fuselage structure made of composite material
EP2554471B1 (en) * 2011-08-01 2013-10-23 Eurocopter Deutschland GmbH Loads interface, particularly a loads interface of an aircraft structure
EP2554472B1 (en) * 2011-08-01 2013-12-11 Eurocopter Deutschland GmbH Loads interface, particularly a loads interface for a plug type aircraft door
US8434591B2 (en) * 2011-09-21 2013-05-07 Robert Bosch Gmbh Acoustic barrier
ES2645628T3 (es) * 2011-12-01 2017-12-07 Airbus Operations S.L. Cuaderna altamente cargada de un fuselaje de aeronave con un alma con estructura de celosía
EP2703282B1 (en) * 2012-08-31 2017-11-15 Airbus Operations GmbH System and method for equalizing an overpressure in the interior of an aircraft cabin
IL223443A (en) 2012-12-04 2014-06-30 Elbit Systems Cyclone Ltd Buildings from composite materials with integral composite connectors and manufacturing methods
CN106892084A (zh) * 2017-02-04 2017-06-27 江苏恒神股份有限公司 一种飞机用碳纤维舱门结构
FR3081828B1 (fr) 2018-06-02 2021-04-16 Latecoere Porte de cabine pressurisee d'aeronef a structure formee de poutres
US11167836B2 (en) * 2018-06-21 2021-11-09 Sierra Nevada Corporation Devices and methods to attach composite core to a surrounding structure
CN109484614A (zh) * 2018-12-18 2019-03-19 中航沈飞民用飞机有限责任公司 一种复合材料结构的增压舱门
US11426951B2 (en) 2019-01-02 2022-08-30 The Boeing Company Expandable bladders as tooling for composite parts
FR3093500B1 (fr) 2019-03-06 2021-07-02 Latecoere Porte de cabine pressurisée d’aéronef à armature intérieure de reprise d’efforts
US11414205B2 (en) * 2019-06-16 2022-08-16 The Boeing Company Fuel containment system
US11298892B2 (en) 2019-07-01 2022-04-12 The Boeing Company Expandable tooling systems and methods
FR3103782B1 (fr) 2019-12-02 2024-03-15 Latecoere Porte de cabine pressurisée d’aéronef à structure formée de poutres à section évolutive
US11548607B2 (en) * 2019-12-16 2023-01-10 The Boeing Company Longitudinal beam joint for a pressure deck assembly
US11872776B2 (en) 2019-12-19 2024-01-16 The Boeing Company Methods for recovering expanded polymer tooling
FR3109364B1 (fr) * 2020-04-17 2022-04-08 Latecoere Procédé de fabrication d’une porte d’aéronef monolithique par matriçage et usinage
FR3121628B1 (fr) 2021-04-13 2023-04-21 Conseil & Technique Procédé de fabrication d’un dispositif de cloison en matériau composite, dispositif de cloison obtenu, et éléments constitutifs d’aéronef utilisant un tel dispositif de cloison.
DE102021117594B4 (de) 2021-07-07 2023-05-17 Deutsches Zentrum für Luft- und Raumfahrt e.V. Außenverkleidung für Flugobjekte sowie Verfahren zu dessen Herstellung
FR3128894B1 (fr) 2021-11-09 2024-03-01 Latecoere Procédé de fabrication d’une structure composite monobloc et structure en bassine réalisée à partir de ce procédé.
FR3134336A1 (fr) 2022-04-07 2023-10-13 Latecoere Procédé de fabrication d’une structure composite monobloc hybride et porte réalisée à partir du procédé.

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US4557440A (en) * 1983-08-18 1985-12-10 The Boeing Company Movable panel with compound curvature and method of making same
DE3614618A1 (de) * 1986-04-30 1987-11-05 Messerschmitt Boelkow Blohm Schalenstruktur aus faserverstaerktem kunststoff
US5242523A (en) 1992-05-14 1993-09-07 The Boeing Company Caul and method for bonding and curing intricate composite structures
JP3839080B2 (ja) * 1995-06-21 2006-11-01 富士重工業株式会社 繊維強化複合材の構造体及びその製造方法
DE19529476C2 (de) 1995-08-11 2000-08-10 Deutsch Zentr Luft & Raumfahrt Flügel mit schubsteifen Flügelschalen aus Faserverbundwerkstoffen für Luftfahrzeuge
US5931415A (en) * 1997-05-09 1999-08-03 The Boeing Company Plug-type overwing emergency exit door assembly
AU2001262912A1 (en) * 2000-02-25 2001-09-03 The Boeing Company Laminated composite radius filler
DE10035349C1 (de) * 2000-07-20 2001-09-27 Eurocopter Deutschland Flugzeugtür
DE10035334B4 (de) 2000-07-20 2007-11-29 Eurocopter Deutschland Gmbh Flugzeugtür und eine Außenhaut einer Flugzeugtür
DE10037307B4 (de) * 2000-07-28 2004-02-05 Honsel Gmbh & Co Kg Strukturelement für ein Flugzeug, insbesondere Flugzeugtür
JP4526698B2 (ja) * 2000-12-22 2010-08-18 富士重工業株式会社 複合材成形品及びその製造方法
ES2205961B2 (es) 2001-02-13 2005-03-01 Eads Construcciones Aeronauticas, S.A. Procedimiento de fabricacion de elementos de material compuesto mediante la tecnoclogia del coencolado.
DE10109638B4 (de) * 2001-03-01 2009-07-30 Eurocopter Deutschland Gmbh Druckbelastbare Außenhaut einer Flugzeugtür
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Also Published As

Publication number Publication date
JP2009517269A (ja) 2009-04-30
RU2008126460A (ru) 2010-01-20
RU2415051C2 (ru) 2011-03-27
CA2632264C (en) 2012-09-18
CN101321664B (zh) 2011-01-12
US20090078826A1 (en) 2009-03-26
CA2632264A1 (en) 2007-06-07
EP1957360B1 (de) 2011-07-27
US9168996B2 (en) 2015-10-27
BRPI0619125A2 (pt) 2011-09-13
CN101321664A (zh) 2008-12-10
DE102005057907A1 (de) 2007-07-12
DE102005057907B4 (de) 2012-03-22
WO2007062641A2 (de) 2007-06-07
WO2007062641A3 (de) 2007-07-12
JP4943449B2 (ja) 2012-05-30
EP1957360A2 (de) 2008-08-20

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Legal Events

Date Code Title Description
B25D Requested change of name of applicant approved

Owner name: AIRBUS HELICOPTERS DEUTSCHLAND GMBH (DE)

B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B06A Patent application procedure suspended [chapter 6.1 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 10 (DEZ) ANOS CONTADOS A PARTIR DE 28/04/2020, OBSERVADAS AS CONDICOES LEGAIS.

B21F Lapse acc. art. 78, item iv - on non-payment of the annual fees in time

Free format text: REFERENTE A 16A ANUIDADE.

B24J Lapse because of non-payment of annual fees (definitively: art 78 iv lpi, resolution 113/2013 art. 12)

Free format text: EM VIRTUDE DA EXTINCAO PUBLICADA NA RPI 2699 DE 27-09-2022 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDA A EXTINCAO DA PATENTE E SEUS CERTIFICADOS, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.