BRPI0506601A - disposição de acondicionamento de isolamento para isolar a parte interna de uma fuselagem de aeronave - Google Patents

disposição de acondicionamento de isolamento para isolar a parte interna de uma fuselagem de aeronave

Info

Publication number
BRPI0506601A
BRPI0506601A BRPI0506601-8A BRPI0506601A BRPI0506601A BR PI0506601 A BRPI0506601 A BR PI0506601A BR PI0506601 A BRPI0506601 A BR PI0506601A BR PI0506601 A BRPI0506601 A BR PI0506601A
Authority
BR
Brazil
Prior art keywords
insulation
fuselage
aircraft
section
packages
Prior art date
Application number
BRPI0506601-8A
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 DE200410001049 external-priority patent/DE102004001049B4/de
Application filed by Airbus Gmbh filed Critical Airbus Gmbh
Publication of BRPI0506601A publication Critical patent/BRPI0506601A/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
    • B64C1/40—Sound or heat insulation, e.g. using insulation blankets
    • A—HUMAN NECESSITIES
    • A62—LIFE-SAVING; FIRE-FIGHTING
    • A62C—FIRE-FIGHTING
    • A62C2/00—Fire prevention or containment
    • A62C2/06—Physical fire-barriers
    • A—HUMAN NECESSITIES
    • A62—LIFE-SAVING; FIRE-FIGHTING
    • A62C—FIRE-FIGHTING
    • A62C3/00—Fire prevention, containment or extinguishing specially adapted for particular objects or places
    • A62C3/07—Fire prevention, containment or extinguishing specially adapted for particular objects or places in vehicles, e.g. in road vehicles
    • A62C3/08—Fire prevention, containment or extinguishing specially adapted for particular objects or places in vehicles, e.g. in road vehicles in aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D25/00—Emergency apparatus or devices, not otherwise provided for

Landscapes

  • Business, Economics & Management (AREA)
  • Emergency Management (AREA)
  • Engineering & Computer Science (AREA)
  • Health & Medical Sciences (AREA)
  • Public Health (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Thermal Insulation (AREA)
  • Insulating Bodies (AREA)
  • Packages (AREA)

Abstract

DISPOSIçãO DE ACONDICIONAMENTO DE ISOLAMENTO PARA ISOLAR A PARTE INTERNA DE UMA FUSELAGEM DE AERONAVE Acedita-se que projeto e a fixação de um acondicionamento de isolamento, de acordo com uma modalidade exemplificativa, que pode ser instalado próximo à estrutura da fuselagem, protejam a região da cabine de uma aeronave contra fogo, cujas chamas agem no acondicionamento de isolamento da parte externa de fora do meio físico da aeronave, facilitando,desse modo, claramente, a evacuação dos passageiros do veículo. A disposição do acondionamento de isolamento pode compreender vários acondionamentos de isolamento da fuselagem(19 - 22) de uma forma alongada. Esses acondicionamentos podem unir a estrutura da fuselagem da aeronave na direção do eixo longitudinal (9) da aeronave. Pode unir longitudinalmente uma superfície de suporte (31a) das longarinas de reforço (31), que são presas na fuselagem da aeronave, ou unir longitudinalmente uma área intena (33a) de um painel de crosta externa, e são fixadas em ambas as partes laterais longitudinais das nervuras (32). Além do mais, esses acondicionamentos de isolamento (19 - 22) podem ser encerrados completamente por uma folha incombustível (11), que é disposta em um espaço encerrado pelo revestimento interno e pelos painéis da crosta externa. O projeto de um acondicionamento de isolamento da fuselagem pode ser implementado com isolamento incombustível de uma maior seção transversal e/ou uma camada de barreira incombustível de uma menor seção transversal, que são é ou são dispostos dentro do acondicionamento de isolamento da fuselagem, individualmente ou em combinação.Nessa disposição, o isolamento ou a camada de barreira se estende próximo ou adjacente a uma região de parede interna da parede da folha. Como uma alternativa, apenas esse isolamento que, na extremidade longitudinal do acondicionamento de isolamento da fuselagem, continua para fora com uma seção terminal de isolamento plana,é presa fora da, e adjacente à, circunferência da folha (11) do acondicionamento da fuselagem (19 - 22). A dita seção terminal de isolamento é presa em uma região de fixação de nervuras, que é disposta abaixo das respectivas partes laterais longitudinais (32) e próxima à longarina de reforço (31) por meio de elementos de fixação inconbustíveis (4, 13).
BRPI0506601-8A 2004-01-05 2005-01-05 disposição de acondicionamento de isolamento para isolar a parte interna de uma fuselagem de aeronave BRPI0506601A (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE200410001049 DE102004001049B4 (de) 2004-01-05 2004-01-05 Isolierpaket-Anordnung zur Innenisolierung eines Flugzeugrumpfes
US60010604P 2004-08-09 2004-08-09
PCT/EP2005/000044 WO2005068290A1 (en) 2004-01-05 2005-01-05 Insulation package arrangement for insulating the interior of an aircraft fuselage

Publications (1)

Publication Number Publication Date
BRPI0506601A true BRPI0506601A (pt) 2007-05-02

Family

ID=34796598

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0506601-8A BRPI0506601A (pt) 2004-01-05 2005-01-05 disposição de acondicionamento de isolamento para isolar a parte interna de uma fuselagem de aeronave

Country Status (7)

Country Link
US (1) US8011619B2 (pt)
EP (1) EP1701883A1 (pt)
JP (1) JP5021316B2 (pt)
BR (1) BRPI0506601A (pt)
CA (1) CA2548115C (pt)
RU (1) RU2373109C2 (pt)
WO (1) WO2005068290A1 (pt)

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US7419124B2 (en) * 2004-03-08 2008-09-02 Airbus Deutschland Gmbh Multi-purpose mount for securing insulation and holding cables
US7278608B2 (en) * 2005-06-27 2007-10-09 Johns Manville Reinforced insulation product and system suitable for use in an aircraft
US7374132B2 (en) * 2005-08-23 2008-05-20 Johns Manville Insulation product and system suitable for use in an aircraft
US7367527B2 (en) * 2005-08-23 2008-05-06 Johns Manville Reinforced insulation product and system suitable for use in an aircraft
DE102006023209A1 (de) * 2006-05-17 2007-11-22 Airbus Deutschland Gmbh Isolierung einer Flugzeugrumpfstruktur
FR2904804B1 (fr) * 2006-08-14 2009-04-10 Airbus France Sas Dispositif d'attache combinee de fixation de matelas d'isolation et d'equipements pour aeronefs
DE102007003276B4 (de) * 2007-01-23 2013-11-28 Airbus Operations Gmbh Luft- und Raumfahrzeug mit einem CFK-Bauteil und einem Metallbauteil, wobei das CFK-Bauteil und das Metallbauteil über wenigstens ein Verbindungselement mit einem Verbindungsabschnitt miteinander verbunden sind
DE102007018753B4 (de) * 2007-04-20 2012-11-08 Airbus Operations Gmbh Brandschutzraum für Flugzeugpassagiere mit Hilfe von Rumpfbehäutung aus Faser-Metall-Laminaten
FR2936219B1 (fr) 2008-09-23 2010-09-17 Airbus France Structure de fuselage pour fixation combinee de matelas d'isolation et d'equipements, aeronef incorporant une telle structure.
FR2961477B1 (fr) 2010-06-22 2012-08-03 Airbus Operations Sas Matelas isolant pour aeronef et ensemble integrant un tel matelas
US9017789B2 (en) * 2010-10-12 2015-04-28 Amsafe Bridport Limited Insulation assemblies for engine housings and associated methods of use and manufacture
US20120128959A1 (en) 2010-11-19 2012-05-24 Fernando Joseph A Fire barrier layer and fire barrier film laminate
US9676168B2 (en) 2010-11-19 2017-06-13 Lamart Corporation Fire barrier layer and fire barrier film laminate
DE102010052671B4 (de) * 2010-11-26 2017-03-23 Airbus Operations Gmbh Isolierungsanordnung mit Ventilationsöffnungen für Luftfahrzeuge
DE102011087286A1 (de) 2011-08-03 2013-02-07 Bayerische Motoren Werke Aktiengesellschaft Verbindungselement
US9132910B2 (en) * 2012-02-14 2015-09-15 Gulfstream Aerospace Corporation Method for attaching a component to an internal portion of an aircraft fuselage
US8985517B2 (en) * 2012-10-26 2015-03-24 Textron Innovations Inc. Passive cooling of transmission using mast mounted heat pipes
US10059427B2 (en) 2014-03-25 2018-08-28 Gulfstream Aerospace Corporation Over-frame blanket assemblies and methods of installation in fuselage assemblies
US9725154B2 (en) * 2014-05-13 2017-08-08 The Boeing Company Method and apparatus for reducing structural vibration and noise
JP6535167B2 (ja) 2015-01-21 2019-06-26 三菱航空機株式会社 航空機、および胴体の冷却構造
US10023286B2 (en) * 2015-11-19 2018-07-17 The Boeing Company Aircraft bay blankets that provide enhanced drainage features
US10604224B2 (en) * 2016-01-12 2020-03-31 The Boeing Company Aircraft bay blankets that provide enhanced drainage features
US9988137B2 (en) * 2016-03-29 2018-06-05 The Boeing Company Methods and apparatus for forming and installing insulation blankets in a vehicle compartment
US10787303B2 (en) 2016-05-29 2020-09-29 Cellulose Material Solutions, LLC Packaging insulation products and methods of making and using same
US11078007B2 (en) 2016-06-27 2021-08-03 Cellulose Material Solutions, LLC Thermoplastic packaging insulation products and methods of making and using same
FR3059062B1 (fr) * 2016-11-22 2019-07-19 Airbus Operations Entretoise auto-perforante pour un matelas d'isolation d'aeronef, procede de pose de ladite entretoise et matelas d'isolation d'aeronef equipe de ladite entretoise
US10532801B2 (en) * 2017-01-17 2020-01-14 The Boeing Company Continuous insulation blanket cap strip assemblies and methods of using same
US10814954B2 (en) * 2017-01-17 2020-10-27 The Boeing Company Insulation system
US10988230B2 (en) * 2017-06-19 2021-04-27 The Boeing Company Passive moisture management bladder in an aircraft
CN113978696B (zh) * 2021-11-08 2024-04-09 湖北航天技术研究院总体设计所 一种航天器及其热阻式端头帽安装结构

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Also Published As

Publication number Publication date
JP2007517713A (ja) 2007-07-05
RU2373109C2 (ru) 2009-11-20
JP5021316B2 (ja) 2012-09-05
CA2548115C (en) 2013-02-26
US20060284014A1 (en) 2006-12-21
RU2006127019A (ru) 2008-02-27
US8011619B2 (en) 2011-09-06
EP1701883A1 (en) 2006-09-20
WO2005068290A1 (en) 2005-07-28
CA2548115A1 (en) 2005-07-28

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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

B07A Application suspended after technical examination (opinion) [chapter 7.1 patent gazette]
B09B Patent application refused [chapter 9.2 patent gazette]
B09B Patent application refused [chapter 9.2 patent gazette]