BRPI0506667A - fuselagem - Google Patents

fuselagem

Info

Publication number
BRPI0506667A
BRPI0506667A BRPI0506667-0A BRPI0506667A BRPI0506667A BR PI0506667 A BRPI0506667 A BR PI0506667A BR PI0506667 A BRPI0506667 A BR PI0506667A BR PI0506667 A BRPI0506667 A BR PI0506667A
Authority
BR
Brazil
Prior art keywords
fuselage
aircraft
exterior skin
metallic material
semi
Prior art date
Application number
BRPI0506667-0A
Other languages
English (en)
Inventor
Rainer Mueller
Peter Turanski
Wilko Oestereich
Thorsten Reinelt
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
Priority claimed from DE200410001078 external-priority patent/DE102004001078B8/de
Application filed by Airbus Gmbh filed Critical Airbus Gmbh
Publication of BRPI0506667A publication Critical patent/BRPI0506667A/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
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/066—Interior liners
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B15/08—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
    • 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
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
    • 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
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0081—Fuselage structures substantially made from particular materials from metallic materials
    • 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)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Devices For Conveying Motion By Means Of Endless Flexible Members (AREA)

Abstract

FUSELAGEM A fuselagem é concebida de tal modo a impedir o espalhamento das chamas produzidas por um fonte de fogo e ação na fuselagem de foram do meio físico da aeronave. O conceito da fuselagem considera materiais ou combinações de materiais, que vão mal propiciar que a proteção da área da cabine de uma aeronave (em pouso de emergência) seja violada por chamas espalhando-se de fora do meio físico da aeronave, o que pode facilitar uma evacuação de passageiros da aeronave. Uma fuselagem de aeronave, cuja estrutura da fuselagem, além de outros elementos estruturais, que são componentes do contraventamento de resistência mecânica da fuselagem e ajudam a absorver suas forças, abrange uma crosta externa (2), consistindo de vários respectivos materiais, que são projetados para serem resistente a cisalhamento, e incorporados como um elemento de suporte no contraventamento de resistência mecânica (6, 7, 8), para absorver e transferir as forças e torques agindo nele. A crosta externa (2) é produzida de um material semi-acabado incombustível, consistindo de um material não metálico ou um material metálico incombustível, em que o material semi-acabado pode ser moldado por processamento adicional. Também, a crosta externa pode ser produzida por um material semi-acabado, combinando um material não metálico e um material metálico, em que o produto crosta externa produzido é um material híbrido, que pode ser moldado e unido por processamento adicional.
BRPI0506667-0A 2004-01-05 2005-01-05 fuselagem BRPI0506667A (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE200410001078 DE102004001078B8 (de) 2004-01-05 2004-01-05 Flugzeugrumpf
US60010504P 2004-08-09 2004-08-09
PCT/EP2005/000038 WO2005068289A2 (en) 2004-01-05 2005-01-05 Fuselage

Publications (1)

Publication Number Publication Date
BRPI0506667A true BRPI0506667A (pt) 2007-05-15

Family

ID=34796599

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0506667-0A BRPI0506667A (pt) 2004-01-05 2005-01-05 fuselagem

Country Status (9)

Country Link
US (1) US20070023572A1 (pt)
EP (1) EP1701881B1 (pt)
JP (1) JP5021315B2 (pt)
AT (1) ATE424346T1 (pt)
BR (1) BRPI0506667A (pt)
CA (1) CA2548369A1 (pt)
DE (1) DE602005013059D1 (pt)
RU (1) RU2384462C2 (pt)
WO (1) WO2005068289A2 (pt)

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* Cited by examiner, † Cited by third party
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DE102005060958A1 (de) * 2005-12-20 2007-06-21 Airbus Deutschland Gmbh Schutzvorrichtung
ES2329324B1 (es) * 2007-03-30 2010-09-06 Airbus España, S.L. Borde de ataque de aeronave de material compuesto reforzado.
DE102007018753B4 (de) * 2007-04-20 2012-11-08 Airbus Operations Gmbh Brandschutzraum für Flugzeugpassagiere mit Hilfe von Rumpfbehäutung aus Faser-Metall-Laminaten
US8678267B2 (en) * 2008-10-10 2014-03-25 The Boeing Company System and method for integrally forming a stiffener with a fiber metal laminate
DE102010053569B4 (de) * 2010-12-06 2012-07-26 Airbus Operations Gmbh Verfahren zur Reparatur eines Flugzeugstrukturbauteils
EP2871046A1 (en) 2013-11-06 2015-05-13 Airbus Operations GmbH Connecting port arrangement for use in an apparatus for producing a composite material component
DE102013226739A1 (de) 2013-12-19 2015-06-25 Airbus Operations Gmbh Formwerkzeug, Formgebungseinrichtung und Verfahren zum Verformen eines Verstärkungsfasern enthaltenden Halbzeugs
DE102013226730A1 (de) 2013-12-19 2015-07-09 Airbus Operations Gmbh Imprägnierwerkzeug und Verfahren zum kontinuierlichen Imprägnieren eines Verstärkungsfasermaterials mit einem Kunststoffmaterial
DE102013226753A1 (de) 2013-12-19 2015-06-25 Airbus Operations Gmbh Vorrichtung und Verfahren zur kontinuierlichen Fertigung von Strukturbauteilen aus faserverstärkten Verbundmaterialien sowie Formwerkzeugset
DE102014215935A1 (de) 2014-08-12 2016-02-18 Airbus Operations Gmbh Vorrichtung und Verfahren zur Fertigung von Bauteilen aus einem faserverstärkten Verbundmaterial
US9845158B2 (en) * 2014-10-17 2017-12-19 X Development Llc Aircraft battery containment pods
EP3042747B1 (en) 2015-01-12 2018-03-14 Airbus Operations GmbH Forming apparatus and method for forming a semi-finished product comprising reinforcement fibres
DE102015211670A1 (de) 2015-06-24 2016-12-29 Airbus Operations Gmbh Verfahren und Vorrichtung zur Serienfertigung von Bauteilen aus einem faserverstärkten Verbundmaterial
RU2708862C1 (ru) * 2019-01-18 2019-12-11 Публичное акционерное общество "Авиационная холдинговая компания "Сухой" Способ изготовления детали и деталь из гибридного композиционного материала

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FR1215912A (fr) * 1958-11-22 1960-04-21 Bronzavia Sa Matériau en feuilles, susceptible de servir d'écran de protection contre les flammes
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Also Published As

Publication number Publication date
EP1701881B1 (en) 2009-03-04
RU2006127021A (ru) 2008-02-27
JP5021315B2 (ja) 2012-09-05
WO2005068289A2 (en) 2005-07-28
DE602005013059D1 (de) 2009-04-16
RU2384462C2 (ru) 2010-03-20
JP2007517711A (ja) 2007-07-05
CA2548369A1 (en) 2005-07-28
WO2005068289A3 (en) 2005-12-01
ATE424346T1 (de) 2009-03-15
EP1701881A2 (en) 2006-09-20
US20070023572A1 (en) 2007-02-01

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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

B09A Decision: intention to grant [chapter 9.1 patent gazette]
B11D Dismissal acc. art. 38, par 2 of ipl - failure to pay fee after grant in time