ATE510766T1 - Flugzeugrumpfstruktur, aus verbundmaterial hergestellter rumpf und mit einer solchen rumpfstruktur ausgerüstetes flugzeug - Google Patents

Flugzeugrumpfstruktur, aus verbundmaterial hergestellter rumpf und mit einer solchen rumpfstruktur ausgerüstetes flugzeug

Info

Publication number
ATE510766T1
ATE510766T1 AT08804876T AT08804876T ATE510766T1 AT E510766 T1 ATE510766 T1 AT E510766T1 AT 08804876 T AT08804876 T AT 08804876T AT 08804876 T AT08804876 T AT 08804876T AT E510766 T1 ATE510766 T1 AT E510766T1
Authority
AT
Austria
Prior art keywords
aircraft
fully
composite material
fuselage structure
fuselage
Prior art date
Application number
AT08804876T
Other languages
English (en)
Inventor
Guillaume Gallant
Laurent Giuseppin
Damien Aguera
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
Application granted granted Critical
Publication of ATE510766T1 publication Critical patent/ATE510766T1/de

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
    • B64C1/068—Fuselage sections
    • 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
    • B64C1/12—Construction or attachment of skin panels
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Connection Of Plates (AREA)
  • Reinforced Plastic Materials (AREA)
  • Moulding By Coating Moulds (AREA)
  • Laminated Bodies (AREA)
  • Tires In General (AREA)
AT08804876T 2007-10-08 2008-09-29 Flugzeugrumpfstruktur, aus verbundmaterial hergestellter rumpf und mit einer solchen rumpfstruktur ausgerüstetes flugzeug ATE510766T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0758132A FR2921898B1 (fr) 2007-10-08 2007-10-08 Structure de fuselage pour fuselage d'aeronef en materiau composite et aeronef equipe d'une telle structure de fuselage
PCT/EP2008/063018 WO2009047158A1 (fr) 2007-10-08 2008-09-29 Structure de fuselage pour fuselage d'aeronef en materiau composite et aeronef equipe d'une telle structure de fuselage.

Publications (1)

Publication Number Publication Date
ATE510766T1 true ATE510766T1 (de) 2011-06-15

Family

ID=39473966

Family Applications (1)

Application Number Title Priority Date Filing Date
AT08804876T ATE510766T1 (de) 2007-10-08 2008-09-29 Flugzeugrumpfstruktur, aus verbundmaterial hergestellter rumpf und mit einer solchen rumpfstruktur ausgerüstetes flugzeug

Country Status (10)

Country Link
US (1) US8550399B2 (de)
EP (1) EP2197739B1 (de)
JP (1) JP5462174B2 (de)
CN (1) CN101821161B (de)
AT (1) ATE510766T1 (de)
BR (1) BRPI0817758A2 (de)
CA (1) CA2701690A1 (de)
FR (1) FR2921898B1 (de)
RU (1) RU2473452C2 (de)
WO (1) WO2009047158A1 (de)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2952905B1 (fr) * 2009-11-20 2012-06-01 Airbus Operations Sas Dispositif d'attache de moyens raidisseurs a un element de cadre, et structure comportant un tel dispositif d'attache
JP5808111B2 (ja) 2011-02-04 2015-11-10 三菱重工業株式会社 航空機用複合材構造体、これを備えた航空機主翼および航空機胴体
FR2984845B1 (fr) * 2011-12-21 2014-07-11 Airbus Operations Sas Element de structure de fuselage d'aeronef anti deversement
RU2595354C1 (ru) * 2015-05-21 2016-08-27 Акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" Корпус гиперзвукового летательного аппарата и способ его изготовления
CN107434031A (zh) 2016-05-25 2017-12-05 空中客车简化股份公司 飞行器翼体的结构部件和包括该结构部件的飞行器
RU2694638C2 (ru) * 2017-11-09 2019-07-16 Акционерное общество Научно-производственное объединение "Опытно-конструкторское бюро имени М.П. Симонова" Кессон фюзеляжа
RU202616U1 (ru) * 2020-11-02 2021-03-01 Федеральное государственное бюджетное образовательное учреждение высшего образования "Казанский национальный исследовательский технический университет им. А.Н. Туполева - КАИ" Фюзеляж летательного аппарата из ферменного заполнителя

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2489779A1 (fr) * 1980-09-09 1982-03-12 Aerospatiale Structure de fuselage pour aeronef resistant aux ruptures longitudinales du revetement exterieur
US4502092A (en) * 1982-09-30 1985-02-26 The Boeing Company Integral lightning protection system for composite aircraft skins
FR2693976B1 (fr) * 1992-07-22 1994-09-30 Eurocopter France Structure de fuselage pour hélicoptère.
US6766984B1 (en) * 1998-07-16 2004-07-27 Icom Engineering Corporation Stiffeners for aircraft structural panels
JP4318381B2 (ja) * 2000-04-27 2009-08-19 本田技研工業株式会社 繊維強化複合材からなる胴体構造体の製造方法、及びそれにより製造される胴体構造体
EP1336469A1 (de) * 2002-02-19 2003-08-20 Alenia Aeronautica S.P.A. Verfahren zur Herstellung eines Versteifungselementes für ein Flugzeugaussenblech und mit dem Versteifungselement versehenes Aussenblech
DE102004001078B8 (de) * 2004-01-05 2013-06-13 Airbus Operations Gmbh Flugzeugrumpf
DE102004001049B4 (de) * 2004-01-05 2009-12-10 Airbus Deutschland Gmbh Isolierpaket-Anordnung zur Innenisolierung eines Flugzeugrumpfes
RU2270135C2 (ru) * 2004-03-04 2006-02-20 Карклин Андрей Михайлович Фюзеляж летательного аппарата
US7527222B2 (en) * 2004-04-06 2009-05-05 The Boeing Company Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections
FR2894869B1 (fr) * 2005-12-20 2009-10-09 Airbus France Sas Procede de fabrication d'un fuselage d'aeronef en materiau composite
US7277266B1 (en) * 2006-03-29 2007-10-02 The Boeing Company Lightning protection system for composite structure

Also Published As

Publication number Publication date
JP2010540348A (ja) 2010-12-24
WO2009047158A1 (fr) 2009-04-16
RU2473452C2 (ru) 2013-01-27
FR2921898A1 (fr) 2009-04-10
CN101821161A (zh) 2010-09-01
US20100264273A1 (en) 2010-10-21
EP2197739A1 (de) 2010-06-23
CA2701690A1 (fr) 2009-04-16
CN101821161B (zh) 2013-02-13
BRPI0817758A2 (pt) 2015-03-24
FR2921898B1 (fr) 2009-12-11
JP5462174B2 (ja) 2014-04-02
EP2197739B1 (de) 2011-05-25
US8550399B2 (en) 2013-10-08
RU2010117200A (ru) 2011-11-20

Similar Documents

Publication Publication Date Title
ATE510766T1 (de) Flugzeugrumpfstruktur, aus verbundmaterial hergestellter rumpf und mit einer solchen rumpfstruktur ausgerüstetes flugzeug
EP2487106A4 (de) Verbundstoffmaterialstruktur, sowie flugzeugtragfläche und damit ausgestatteter flugzeugrumpf
WO2012048329A3 (en) Support structure and systems including the same
WO2015047485A3 (en) Gas turbine engine cmc airfoil assembly
FR2915458B1 (fr) Assemblage de panneaux de fuselage d'un avion
WO2015080781A3 (en) Ply architecture for integral platform and damper retaining features in cmc turbine blades
GB2509279A (en) Electrical Insulator Casing
FR2914622B1 (fr) Aeronef comprenant une structure assurant les fonctions structurale et electrique
WO2012092623A3 (en) Anti-icing, de-icing, and heating configuration, integration, and power methods for aircraft, aerodynamic, and complex surfaces
EP3020072B8 (de) Flugzeug für grosse höhen mit integrierten solarzellen sowie entsprechende systeme und verfahren
EP2027012B8 (de) Heckstruktur für ein luft- oder raumfahrzeug
WO2014004900A3 (en) Benzoxazine resin composition, prepreg, and fiber-reinforced composite material
GB201101435D0 (en) Stringer for an aircraft wing and method of forming thereof
WO2009156549A3 (es) Estructura de superficie sustentadora de aeronave
EP2599719A4 (de) Flugzeuge mit einer integralen aerodynamischen konfiguration
WO2009022165A3 (en) Aircraft light unit
EP2147855A4 (de) Flugzeuganordnung und verfahren zu ihrer herstellung
DE502007000343D1 (de) Zwei-Wellen-Triebwerk für Flugzeuge mit hohem Bedarf an elektrischer Leistung
DE602007014391D1 (de) Propellerschaufelfixierung
EP2671794A4 (de) Verbundwerkstoffstruktur sowie flugzeugflügel und -rumpf damit
WO2015067891A3 (fr) Ensemble pour aeronef comprenant une ferrure fixee sur la partie extrados d'un caisson de voilure, pour le montage d'un mat d'accrochage sur ce caisson de voilure
WO2014210503A3 (en) Coatings for window surfaces to produce electricity
WO2011023396A3 (en) Aircraft having at least two electrical propulsion groups mounted at a rear portion thereof
WO2009132846A3 (de) Lagervorrichtung zur lagerung einer energie-versorgungsvorrichtung an einem strukturteil eines flugzeugs und flugzeug mit einer lagervorrichtung
WO2014155293A8 (en) Wind turbine blade root and process for manufacturing a wind turbine blade root

Legal Events

Date Code Title Description
RER Ceased as to paragraph 5 lit. 3 law introducing patent treaties