FR2489779B1 - - Google Patents

Info

Publication number
FR2489779B1
FR2489779B1 FR8019439A FR8019439A FR2489779B1 FR 2489779 B1 FR2489779 B1 FR 2489779B1 FR 8019439 A FR8019439 A FR 8019439A FR 8019439 A FR8019439 A FR 8019439A FR 2489779 B1 FR2489779 B1 FR 2489779B1
Authority
FR
France
Legal status (The legal status 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 status listed.)
Expired
Application number
FR8019439A
Other languages
French (fr)
Other versions
FR2489779A1 (fr
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Group SAS
Original Assignee
Airbus Group 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 Group SAS filed Critical Airbus Group SAS
Priority to FR8019439A priority Critical patent/FR2489779A1/fr
Priority to EP81401343A priority patent/EP0048191B1/fr
Priority to DE8181401343T priority patent/DE3162301D1/de
Publication of FR2489779A1 publication Critical patent/FR2489779A1/fr
Application granted granted Critical
Publication of FR2489779B1 publication Critical patent/FR2489779B1/fr
Granted legal-status Critical Current

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
    • 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
    • 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
    • B64C2001/0081—Fuselage structures substantially made from particular materials from metallic materials

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Tires In General (AREA)
  • Automatic Assembly (AREA)
  • Connection Of Plates (AREA)
FR8019439A 1980-09-09 1980-09-09 Structure de fuselage pour aeronef resistant aux ruptures longitudinales du revetement exterieur Granted FR2489779A1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR8019439A FR2489779A1 (fr) 1980-09-09 1980-09-09 Structure de fuselage pour aeronef resistant aux ruptures longitudinales du revetement exterieur
EP81401343A EP0048191B1 (fr) 1980-09-09 1981-08-26 Structure de fuselage pour aéronef résistant aux ruptures longitudinales du revêtement extérieur
DE8181401343T DE3162301D1 (en) 1980-09-09 1981-08-26 Airship fuselage structure resistant to longitudinal cracks of the skin

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8019439A FR2489779A1 (fr) 1980-09-09 1980-09-09 Structure de fuselage pour aeronef resistant aux ruptures longitudinales du revetement exterieur

Publications (2)

Publication Number Publication Date
FR2489779A1 FR2489779A1 (fr) 1982-03-12
FR2489779B1 true FR2489779B1 (OSRAM) 1984-03-09

Family

ID=9245773

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8019439A Granted FR2489779A1 (fr) 1980-09-09 1980-09-09 Structure de fuselage pour aeronef resistant aux ruptures longitudinales du revetement exterieur

Country Status (3)

Country Link
EP (1) EP0048191B1 (OSRAM)
DE (1) DE3162301D1 (OSRAM)
FR (1) FR2489779A1 (OSRAM)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4671470A (en) * 1985-07-15 1987-06-09 Beech Aircraft Corporation Method for fastening aircraft frame elements to sandwich skin panels covering same using woven fiber connectors
DE3614618A1 (de) * 1986-04-30 1987-11-05 Messerschmitt Boelkow Blohm Schalenstruktur aus faserverstaerktem kunststoff
GB8711886D0 (en) * 1987-05-20 1987-06-24 Westland Group Plc Joints
US5560102A (en) * 1992-10-13 1996-10-01 The Boeing Company Panel and fuselage assembly
DE19534031C1 (de) * 1995-09-14 1997-01-30 Dornier Luftfahrt Anordnung zur Verbindung der Außenhaut der Oberschale mit der Außenhaut der Unterschale eines Flugzeugrumpfes
GB0606079D0 (en) 2006-03-27 2006-05-03 Airbus Uk Ltd Aircraft component
FR2906008B1 (fr) 2006-09-15 2008-11-07 Airbus France Sa Eclisse de lisses et dispositif de jonction orbitale
FR2921898B1 (fr) 2007-10-08 2009-12-11 Airbus France Structure de fuselage pour fuselage d'aeronef en materiau composite et aeronef equipe d'une telle structure de fuselage
DE102007054053A1 (de) * 2007-11-13 2009-05-20 Airbus Deutschland Gmbh Kupplungselement zur Verbindung von zwei Längsversteifungselementen
DE102008044229A1 (de) 2008-12-01 2010-06-10 Airbus Deutschland Gmbh Schalenbauteil für ein Luft- oder Raumfahrzeug
ES2382765B1 (es) * 2009-06-29 2013-05-03 Airbus Operations, S.L. Diseño de cuadernas de aeronave
DE102009033444A1 (de) * 2009-07-16 2011-01-27 Airbus Operations Gmbh Schalensegment zur Herstellung einer Rumpfzellensektion für eine Rumpfzelle eines Flugzeugs
FR2977296B1 (fr) * 2011-06-28 2013-08-02 Airbus Operations Sas Procede de liaison entre pieces se chevauchant sur plusieurs plans et application a un panneau de fuselage d'aeronef
RU2518381C1 (ru) * 2013-02-01 2014-06-10 Общество с ограниченной ответственностью ОКБ "АТЛАНТ" Дирижабль жесткой конструкции
FR3009352B1 (fr) 2013-08-01 2016-01-01 Airbus Operations Sas Outillage pour le maintien simultane de plusieurs clips de fixation contre un element de cadre de fuselage d'aeronef
FR3009274A1 (fr) 2013-08-01 2015-02-06 Airbus Operations Sas Element de cadre de fuselage d'aeronef integrant des languettes pour la fixation de raidisseurs
FR3009351B1 (fr) 2013-08-01 2015-08-07 Airbus Operations Sas Outillage pour le maintien simultane de plusieurs clips de fixation contre un element de cadre de fuselage d'aeronef
EP4112444A1 (en) * 2021-06-30 2023-01-04 Airbus Operations GmbH Structural system for an aircraft for installation of equipment

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1497155A (en) * 1975-12-22 1978-01-05 Secr Defence Structures

Also Published As

Publication number Publication date
EP0048191B1 (fr) 1984-02-15
FR2489779A1 (fr) 1982-03-12
DE3162301D1 (en) 1984-03-22
EP0048191A1 (fr) 1982-03-24

Similar Documents

Publication Publication Date Title
FR2473180B1 (OSRAM)
DE3152593A1 (OSRAM)
FR2473578B1 (OSRAM)
CH655632B (OSRAM)
FR2473575B1 (OSRAM)
DE3153460A1 (OSRAM)
FR2473151B1 (OSRAM)
FR2473394B1 (OSRAM)
DE3152509T1 (OSRAM)
CH655684B (OSRAM)
CH660829GA3 (OSRAM)
DE3153254A1 (OSRAM)
FR2473031B1 (OSRAM)
FR2473519B1 (OSRAM)
DE3153680A1 (OSRAM)
FR2473488B1 (OSRAM)
CH655411B (OSRAM)
CH647640GA3 (OSRAM)
DE3050629A1 (OSRAM)
CH655674B (OSRAM)
FR2473437B1 (OSRAM)
FR2473595B1 (OSRAM)
FR2472923B1 (OSRAM)
FR2473304B1 (OSRAM)
FR2473338B1 (OSRAM)

Legal Events

Date Code Title Description
ST Notification of lapse