ATE555009T1 - Flugzeugaufbau mit versteifungskantenverbindungen - Google Patents

Flugzeugaufbau mit versteifungskantenverbindungen

Info

Publication number
ATE555009T1
ATE555009T1 AT08839251T AT08839251T ATE555009T1 AT E555009 T1 ATE555009 T1 AT E555009T1 AT 08839251 T AT08839251 T AT 08839251T AT 08839251 T AT08839251 T AT 08839251T AT E555009 T1 ATE555009 T1 AT E555009T1
Authority
AT
Austria
Prior art keywords
stiffeners
aircraft structure
panels
interrupted
junction
Prior art date
Application number
AT08839251T
Other languages
English (en)
Inventor
Helene Cazeneuve
Bruno Cacciaguerra
Jean Claude Lacombe
David Andissac
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 ATE555009T1 publication Critical patent/ATE555009T1/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
    • B64C1/064—Stringers; Longerons
    • 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
    • B64C1/069—Joining arrangements therefor
    • 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)
  • Moulding By Coating Moulds (AREA)
  • Laminated Bodies (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Tires In General (AREA)
  • Connection Of Plates (AREA)
  • Braking Arrangements (AREA)
  • Gasket Seals (AREA)
AT08839251T 2007-10-18 2008-09-12 Flugzeugaufbau mit versteifungskantenverbindungen ATE555009T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0758423A FR2922518B1 (fr) 2007-10-18 2007-10-18 Structure d'avion comportant des jonctions d'arrets de raidisseurs
PCT/FR2008/051631 WO2009050358A2 (fr) 2007-10-18 2008-09-12 Structure d'avion comportant des jonctions d'arrêts de raidisseur

Publications (1)

Publication Number Publication Date
ATE555009T1 true ATE555009T1 (de) 2012-05-15

Family

ID=39473882

Family Applications (1)

Application Number Title Priority Date Filing Date
AT08839251T ATE555009T1 (de) 2007-10-18 2008-09-12 Flugzeugaufbau mit versteifungskantenverbindungen

Country Status (10)

Country Link
US (1) US8215584B2 (de)
EP (1) EP2209711B1 (de)
JP (1) JP5250039B2 (de)
CN (1) CN101903238B (de)
AT (1) ATE555009T1 (de)
BR (1) BRPI0817838A2 (de)
CA (1) CA2702908C (de)
FR (1) FR2922518B1 (de)
RU (1) RU2433064C1 (de)
WO (1) WO2009050358A2 (de)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2922518B1 (fr) * 2007-10-18 2010-04-23 Airbus France Structure d'avion comportant des jonctions d'arrets de raidisseurs
FR2947522B1 (fr) * 2009-07-03 2011-07-01 Airbus Operations Sas Element de fuselage comportant un troncon de fuselage et des moyens de jonction, portion de fuselage, fuselage et aeronef
ES2392236B1 (es) * 2010-01-15 2013-10-09 Airbus Operations, S.L. Componente de aeronave con paneles rigidizados con larguerillos.
DE102010013370B8 (de) 2010-03-30 2013-12-12 Eads Deutschland Gmbh Wandbauteil für ein Luftfahrzeug
EP2404824B1 (de) * 2010-07-08 2015-09-09 Airbus Opérations SAS Luftfahrzeugstruktur und Herstellungsverfahren für eine solche Struktur
US8567722B2 (en) * 2010-12-15 2013-10-29 The Boeing Company Splice and associated method for joining fuselage sections
FR2976916B1 (fr) * 2011-06-27 2013-07-26 Airbus Operations Sas Dispositif et procede d'assemblage de deux troncons de fuselage d'aeronef
FR2984845B1 (fr) * 2011-12-21 2014-07-11 Airbus Operations Sas Element de structure de fuselage d'aeronef anti deversement
US8960606B2 (en) * 2012-10-31 2015-02-24 The Boeing Company Circumference splice for joining shell structures
EP2799220B1 (de) * 2013-04-30 2020-06-17 Airbus Operations S.L. Verbundstruktur für ein Flugzeug und Herstellungsverfahren dafür
US10421528B2 (en) 2016-08-16 2019-09-24 The Boeing Company Planked stringers that provide structural support for an aircraft wing
US10207789B2 (en) * 2016-08-16 2019-02-19 The Boeing Company Aircraft composite wingbox integration
GB2571911A (en) * 2017-12-21 2019-09-18 Airbus Operations Gmbh A Stiffener for an Aircraft Assembly
US20200122816A1 (en) * 2018-10-22 2020-04-23 The Boeing Company Bulkhead joint assembly
FR3114574A1 (fr) * 2020-09-30 2022-04-01 Airbus Operations Élément d’interface pour connecter deux tronçons de fuselage d’aéronef avec un nombre réduit de pièces.

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU1519121A1 (ru) * 1988-03-28 1996-05-20 Д.Л. Мемнонов Салон пассажирского самолета
US5518208A (en) * 1993-12-28 1996-05-21 The Boeing Company Optimum aircraft body frame to body skin shear tie installation pattern for body skin/stringer circumferential splices
RU2191716C2 (ru) * 1999-04-27 2002-10-27 Открытое акционерное общество Таганрогский авиационный научно-технический комплекс им. Г.М.Бериева Салон летательного аппарата
US7134629B2 (en) * 2004-04-06 2006-11-14 The Boeing Company Structural panels for use in aircraft fuselages and other structures
US7325771B2 (en) * 2004-09-23 2008-02-05 The Boeing Company Splice joints for composite aircraft fuselages and other structures
US20060248854A1 (en) * 2005-05-05 2006-11-09 Bartley-Cho Jonathan D Thermally insulated structure - tapered joint concept
FR2922517B1 (fr) * 2007-10-18 2010-04-23 Airbus France Avion comportant des jonctions d'arrets de raidisseurs et procede de fabrication d'un tel avion
FR2922518B1 (fr) * 2007-10-18 2010-04-23 Airbus France Structure d'avion comportant des jonctions d'arrets de raidisseurs
DE102008012252B4 (de) * 2008-03-03 2014-07-31 Airbus Operations Gmbh Verbund sowie Luft- oder Raumfahrzeug mit einem derartigen Verbund

Also Published As

Publication number Publication date
FR2922518B1 (fr) 2010-04-23
CA2702908A1 (fr) 2009-04-23
BRPI0817838A2 (pt) 2015-03-31
US20100264272A1 (en) 2010-10-21
EP2209711A2 (de) 2010-07-28
US8215584B2 (en) 2012-07-10
JP5250039B2 (ja) 2013-07-31
CN101903238B (zh) 2014-02-19
RU2433064C1 (ru) 2011-11-10
CA2702908C (fr) 2013-01-08
EP2209711B1 (de) 2012-04-25
WO2009050358A3 (fr) 2009-06-11
WO2009050358A2 (fr) 2009-04-23
FR2922518A1 (fr) 2009-04-24
JP2011500416A (ja) 2011-01-06
CN101903238A (zh) 2010-12-01

Similar Documents

Publication Publication Date Title
ATE555009T1 (de) Flugzeugaufbau mit versteifungskantenverbindungen
WO2020243364A3 (en) A novel aircraft design using tandem wings and a distributed propulsion system
RU2427500C2 (ru) Соединение обшивки и стыковой накладки конструкции летательного аппарата, конструкция летательного аппарата, крыло и способ изготовления соединения обшивки и стыковой накладки конструкции летательного аппарата
FR2915178B1 (fr) Attache d'un caisson de mat sur une voilure, pincant un panneau lateral du caisson
GB201000878D0 (en) Sandwich panel
EA200901189A1 (ru) Летательный аппарат
RU2013149494A (ru) Вертикально встроенные стрингеры
BR112022000323A2 (pt) Estrutura de fuselagem de uma aeronave e método para fabricar a mesma
WO2009050357A3 (fr) Avion comportant des jonctions d'arrêts de raidisseurs et procédé de fabrication d'un tel avion
BR112012001714A2 (pt) "estrutura de material compósito, asa principal de aeronave, e, fuselagem de aeronave"
GB0717690D0 (en) Wind turbine blade
WO2011001081A3 (fr) Encadrement d'une ouverture menagee dans un fuselage d'aeronef
WO2009137893A3 (en) Hybrid aircraft fuselage structural components and methods of making same
FR2958418B1 (fr) Systeme de gestion de vol d'un aeronef sans pilote a bord de l'aeronef
BRPI0818031A2 (pt) Junção de enrijecedores em ômega no nível de uma junção circunferencial de uma fuselagem de avião
BR112014020090A8 (pt) Aeronave para decolagem e aterrissagem vertical com duas disposições de asa
WO2012001206A3 (es) Estructura interna de aeronave en material compuesto
DE602007011896D1 (de) Ausfallsichere steuerflächentropfenverbindung
BR112012018357A2 (pt) transportador para acomodar uma pluralidade de recipientes, blanqueta para formar um transportador para acomodar uma pluralidade de recipientes, e método para formar um transportador
GB2605197B (en) Aircraft wing with trailing edge panel
EP2671792A4 (de) Verbundwerkstoffstruktur sowie flugzeugflügel und -rumpf damit
DE602006006865D1 (de) Flugzeug mit zentraler stromlinienverkleidung, die den druck auf die flügelstrukturen mittels lokaler geometrischer verformungen einstellt
BR112015008250A2 (pt) método e equipamento para moldagem de roupa íntima descartável e ajustável com aspecto de cueca/calcinha com painel frontal totalmente seccionado com linha de enfraquecimento
BRPI0817758A2 (pt) Estrutura de fuselagem para fuselagem de aeronave de material compósito, e, aeronave
GB2585484B (en) Aircraft with two front wing attachments, each having at least one vertical linking element