BRPI0816483A2 - Quadro de estrutura material compósito, notadamente para fuselagem de aeronave,e, fuselagem de aeronave - Google Patents

Quadro de estrutura material compósito, notadamente para fuselagem de aeronave,e, fuselagem de aeronave

Info

Publication number
BRPI0816483A2
BRPI0816483A2 BRPI0816483A BRPI0816483A2 BR PI0816483 A2 BRPI0816483 A2 BR PI0816483A2 BR PI0816483 A BRPI0816483 A BR PI0816483A BR PI0816483 A2 BRPI0816483 A2 BR PI0816483A2
Authority
BR
Brazil
Prior art keywords
aircraft fuselage
notably
composite material
material structure
structure frame
Prior art date
Application number
Other languages
English (en)
Inventor
Anaïs Markowski
Eric Bouchet
Denis Soula
Marie Elduayen
Original Assignee
Airbus Operations Sas
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 Operations Sas filed Critical Airbus Operations Sas
Publication of BRPI0816483A2 publication Critical patent/BRPI0816483A2/pt

Links

Classifications

    • 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
    • B29C70/06—Fibrous reinforcements only
    • B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
    • B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
    • B29C70/20—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in a single direction, e.g. roofing or other parallel fibres
    • B29C70/202—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in a single direction, e.g. roofing or other parallel fibres arranged in parallel planes or structures of fibres crossing at substantial angles, e.g. cross-moulding compound [XMC]
    • 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
    • B64C1/061—Frames
    • 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
    • B29C70/06—Fibrous reinforcements only
    • B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
    • B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
    • B29C70/20—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in a single direction, e.g. roofing or other parallel fibres
    • B29C70/205—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in a single direction, e.g. roofing or other parallel fibres the structure being shaped to form a three-dimensional configuration
    • 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
    • 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
    • B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
    • B29L2031/3076—Aircrafts
    • B29L2031/3082—Fuselages
    • 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
    • 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
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24058—Structurally defined web or sheet [e.g., overall dimension, etc.] including grain, strips, or filamentary elements in respective layers or components in angular relation
    • Y10T428/24124—Fibers

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Textile Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Moulding By Coating Moulds (AREA)
BRPI0816483 2007-09-07 2008-09-04 Quadro de estrutura material compósito, notadamente para fuselagem de aeronave,e, fuselagem de aeronave BRPI0816483A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0757431A FR2920743B1 (fr) 2007-09-07 2007-09-07 Cadre de structure en materiau composite et fuselage d'aeronef comportant un tel cadre
PCT/EP2008/061703 WO2009030731A1 (fr) 2007-09-07 2008-09-04 Cadre de structure en materiau composite et fuselage d'aeronef comportant un tel cadre

Publications (1)

Publication Number Publication Date
BRPI0816483A2 true BRPI0816483A2 (pt) 2015-03-17

Family

ID=39301300

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0816483 BRPI0816483A2 (pt) 2007-09-07 2008-09-04 Quadro de estrutura material compósito, notadamente para fuselagem de aeronave,e, fuselagem de aeronave

Country Status (9)

Country Link
US (1) US8556213B2 (pt)
EP (1) EP2185345B1 (pt)
JP (1) JP5314024B2 (pt)
CN (1) CN101795850B (pt)
BR (1) BRPI0816483A2 (pt)
CA (1) CA2698617C (pt)
FR (1) FR2920743B1 (pt)
RU (1) RU2469853C2 (pt)
WO (1) WO2009030731A1 (pt)

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DE102006026169B4 (de) * 2006-06-06 2012-06-21 Airbus Operations Gmbh Flugzeugrumpfstruktur und Verfahren zu deren Herstellung
DE102006026168A1 (de) 2006-06-06 2008-01-31 Airbus Deutschland Gmbh Flugzeugrumpfstruktur und Verfahren zu deren Herstellung
DE102006026170B4 (de) 2006-06-06 2012-06-21 Airbus Operations Gmbh Flugzeugrumpfstruktur und Verfahren zu deren Herstellung
US8038099B2 (en) * 2008-04-30 2011-10-18 The Boeing Company Bonded metal fuselage and method for making the same
US7967250B2 (en) * 2008-05-12 2011-06-28 EMBRAER—Empresa Brasileira de Aeronáutica Hybrid aircraft fuselage structural components and methods of making same
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
ES2382765B1 (es) * 2009-06-29 2013-05-03 Airbus Operations, S.L. Diseño de cuadernas de aeronave
FR2950833A1 (fr) * 2009-10-01 2011-04-08 Airbus Operations Sas Procede et dispositif pour la fabrication automatisee de preformes seches circulaires
ES2383986B1 (es) 2009-12-30 2013-05-16 Airbus Operations, S.L. Cuaderna de fuselaje de aeronave en material compuesto con alma estabilizada.
ES2384349B1 (es) 2009-12-30 2013-05-16 Airbus Operations, S.L. Cuaderna de fuselaje de aeronave en material compuesto con costillas estabilizadoras.
DE102010042186A1 (de) 2010-10-08 2012-04-12 Airbus Operations Gmbh Verbund, Luft- oder Raumfahrzeug sowie Verfahren
ES2400771B1 (es) * 2011-03-30 2014-02-14 Airbus Operations S.L. Fuselaje de aeronave con cuadernas altamente resistentes.
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
US9545757B1 (en) 2012-02-08 2017-01-17 Textron Innovations, Inc. Composite lay up and method of forming
US9289949B2 (en) * 2012-06-08 2016-03-22 The Boeing Company Optimized cross-ply orientation in composite laminates
US10099765B2 (en) 2012-08-08 2018-10-16 The Boeing Company Monolithic composite structures for vehicles
FR3000019B1 (fr) 2012-12-21 2015-01-30 Airbus Operations Sas Raidisseur de fuselage d'aeronef forme a l'aide d'une tole repliee sur elle-meme
DE102014103438A1 (de) * 2013-07-16 2015-01-22 Airbus Operations Gmbh Spritzgussverfahren zur Herstellung eines Primärstrukturverbindungselements
EP2910365B1 (en) 2014-02-21 2017-04-26 Airbus Operations GmbH Composite structural element and torsion box
WO2015142171A1 (en) * 2014-03-17 2015-09-24 Gtm Holding B.V. Primary structure connecting element for aircraft and method for manufacturing the connecting element
EP2942269B1 (en) * 2014-05-06 2018-09-26 Airbus Operations GmbH Method for manufacturing a load bearing structure and such a load bearing structure
US20160288931A1 (en) * 2015-03-31 2016-10-06 Worldvu Satellites Limited Satellite frame and method of making a satellite
FR3040014B1 (fr) * 2015-08-14 2017-09-08 Conseil & Technique Procede de fabrication d’un cadre de forme annulaire
US10005267B1 (en) 2015-09-22 2018-06-26 Textron Innovations, Inc. Formation of complex composite structures using laminate templates
EP3372396A1 (en) 2017-03-06 2018-09-12 Airbus Operations, S.L. A curved composite part and method for manufacturing thereof
DE102018104122A1 (de) 2018-02-23 2019-08-29 Airbus Operations Gmbh Verbundstrukturelement

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WO2002055289A1 (fr) * 2001-01-12 2002-07-18 Bridgestone Corporation Procede de production d'element de pneumatique et dispositif a cet effet
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JP4522796B2 (ja) * 2004-09-06 2010-08-11 本田技研工業株式会社 繊維強化複合材環状構造体の製造方法、及びその構造体からなる航空機胴体用環状フレーム
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Also Published As

Publication number Publication date
US20100308165A1 (en) 2010-12-09
CN101795850B (zh) 2013-08-07
FR2920743A1 (fr) 2009-03-13
US8556213B2 (en) 2013-10-15
WO2009030731A1 (fr) 2009-03-12
FR2920743B1 (fr) 2009-12-18
JP2010537889A (ja) 2010-12-09
RU2010113382A (ru) 2011-10-20
EP2185345A1 (fr) 2010-05-19
EP2185345B1 (fr) 2012-07-04
JP5314024B2 (ja) 2013-10-16
CA2698617A1 (fr) 2009-03-12
RU2469853C2 (ru) 2012-12-20
CA2698617C (fr) 2016-10-04
CN101795850A (zh) 2010-08-04

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Legal Events

Date Code Title Description
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]

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