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FR2906008B1 - Eclisse de lisses et dispositif de jonction orbitale - Google Patents

Eclisse de lisses et dispositif de jonction orbitale

Info

Publication number
FR2906008B1
FR2906008B1 FR0653751A FR0653751A FR2906008B1 FR 2906008 B1 FR2906008 B1 FR 2906008B1 FR 0653751 A FR0653751 A FR 0653751A FR 0653751 A FR0653751 A FR 0653751A FR 2906008 B1 FR2906008 B1 FR 2906008B1
Authority
FR
France
Prior art keywords
junction device
orbital junction
chest
smooth
smooth chest
Prior art date
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 - Fee Related
Application number
FR0653751A
Other languages
English (en)
Other versions
FR2906008A1 (fr
Inventor
Cedric Meyer
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 Operations SAS
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
Priority to FR0653751A priority Critical patent/FR2906008B1/fr
Priority to US11/855,197 priority patent/US7823362B2/en
Publication of FR2906008A1 publication Critical patent/FR2906008A1/fr
Application granted granted Critical
Publication of FR2906008B1 publication Critical patent/FR2906008B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Connection Of Plates (AREA)
  • Mutual Connection Of Rods And Tubes (AREA)
FR0653751A 2006-09-15 2006-09-15 Eclisse de lisses et dispositif de jonction orbitale Expired - Fee Related FR2906008B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR0653751A FR2906008B1 (fr) 2006-09-15 2006-09-15 Eclisse de lisses et dispositif de jonction orbitale
US11/855,197 US7823362B2 (en) 2006-09-15 2007-09-14 Splice plate for stringers and orbital joining device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0653751A FR2906008B1 (fr) 2006-09-15 2006-09-15 Eclisse de lisses et dispositif de jonction orbitale

Publications (2)

Publication Number Publication Date
FR2906008A1 FR2906008A1 (fr) 2008-03-21
FR2906008B1 true FR2906008B1 (fr) 2008-11-07

Family

ID=37909365

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0653751A Expired - Fee Related FR2906008B1 (fr) 2006-09-15 2006-09-15 Eclisse de lisses et dispositif de jonction orbitale

Country Status (2)

Country Link
US (1) US7823362B2 (fr)
FR (1) FR2906008B1 (fr)

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DE102008010197B4 (de) * 2008-02-20 2012-03-22 Airbus Operations Gmbh Verfahren zum Verbinden von zwei Rumpfsektionen unter Schaffung eines Querstoßes sowie Querstoßverbindung
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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.
FR2947523B1 (fr) 2009-07-03 2011-07-22 Airbus Operations Sas Element de fuselage comportant un troncon de fuselage et des moyens de jonction
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
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DE102010053892B4 (de) * 2010-12-09 2015-01-29 Airbus Operations Gmbh Sitzverstellvorrichtung sowie Luft-oder Raumfahrzeug
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FR2970942B1 (fr) * 2011-01-28 2013-02-22 Airbus Operations Sas Raccordement des cadres de raidissage entre un fuselage d'aeronef et un caisson de voilure
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FR2976916B1 (fr) * 2011-06-27 2013-07-26 Airbus Operations Sas Dispositif et procede d'assemblage de deux troncons de fuselage d'aeronef
US8740151B1 (en) 2012-01-03 2014-06-03 The Boeing Company Adjustable splice fitting for shimless connection of structual members
DE102012202504A1 (de) * 2012-02-17 2013-08-22 Airbus Operations Gmbh Strukturbauteil für ein Luft- oder Raumfahrzeug
US8939406B2 (en) * 2012-07-02 2015-01-27 The Boeing Company Joining composite fuselage sections along window belts
EP2759467B1 (fr) * 2013-01-24 2016-10-19 Airbus Operations GmbH Cadre d'aéronef et procedé pour le montage de deux segments de fuselage
DE102013102812B4 (de) * 2013-03-19 2017-01-26 Airbus Operations Gmbh Rumpfstruktur für ein Verkehrsmittel, Verkehrsmittel und Verfahren zum Herstellen einer Rumpfstruktur für ein Verkehrsmittel
EP2781450B1 (fr) 2013-03-19 2018-05-02 Airbus Operations GmbH Système et procédé pour interconnecter des structures composites
US9096324B2 (en) * 2013-03-19 2015-08-04 The Boeing Company Joint assembly to form a sealed flow conduit
EP2799220B1 (fr) * 2013-04-30 2020-06-17 Airbus Operations S.L. Structure composite pour un avion et son procédé de fabrication
US9527572B2 (en) * 2014-06-26 2016-12-27 The Boeing Company Elongated structures and related assemblies
US9676549B2 (en) 2014-12-02 2017-06-13 Fontaine Commercial Trailer, Inc. Floor assembly for transportable refrigerated container
US9809297B2 (en) * 2015-08-26 2017-11-07 The Boeing Company Structures containing stiffeners having transition portions
CA3043302C (fr) * 2016-11-11 2020-09-29 Mitsubishi Heavy Industries, Ltd. Procede de production d'element et systeme de production d'element
CN110475715B (zh) * 2017-03-30 2023-04-04 赛峰客舱公司 侧壁面板组件
CN108639307A (zh) * 2018-06-22 2018-10-12 西安飞机工业（集团）有限责任公司 一种飞机外挂接头的连接结构
US11312468B2 (en) * 2018-08-08 2022-04-26 The Boeing Company Elongate structures, structural assemblies with elongate structures, and methods for supporting a structural load
CN109183982A (zh) * 2018-11-08 2019-01-11 张展有 一种不同功能空间区域划分组合的搭建结构
US11198497B2 (en) * 2019-06-19 2021-12-14 The Boeing Company Splice fittings that are affixed to stringers via web-installed fasteners
US10864999B1 (en) * 2019-07-18 2020-12-15 QMI, Inc. Cessna tail-cone reinforcement angle splice, installation kit, and method for installation thereof
US11724791B2 (en) * 2019-10-08 2023-08-15 The Boeing Company Enhanced design for stringer runout terminations on composite panels
FR3105165A1 (fr) * 2019-12-19 2021-06-25 Airbus Operations Élément de cadre pour fuselage d’aéronef pourvu d’ouvertures adaptées à un montage par enfilage de raidisseur.
US11524762B2 (en) * 2020-02-21 2022-12-13 The Boeing Company Fuselage structure splice
US11459124B2 (en) 2020-02-21 2022-10-04 The Boeing Company Assembly tool for fuselage structure splice
US11420718B2 (en) * 2020-03-27 2022-08-23 The Boeing Company Aircraft tail assembly
CN114308487A (zh) * 2022-01-05 2022-04-12 上海拔山自动化技术有限公司 一种多功能喷漆机器人轨道装置及其控制方法
EP4282754A1 (fr) 2022-05-24 2023-11-29 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Ensemble de fixation destiné à la fixation d'une poutre de fuseau d'empennage à un fuselage arrière d'un aéronef à voilure tournante

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US7530531B2 (en) * 2004-10-04 2009-05-12 The Boeing Company Apparatus and methods for installing an aircraft window panel

Also Published As

Publication number Publication date
US20080067289A1 (en) 2008-03-20
US7823362B2 (en) 2010-11-02
FR2906008A1 (fr) 2008-03-21

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Legal Events

Date Code Title Description
CA Change of address

Effective date: 20110916

CD Change of name or company name

Owner name: AIRBUS HOLDING, FR

Effective date: 20110916

CJ Change in legal form

Effective date: 20110916

TP Transmission of property

Owner name: AIRBUS HOLDING, FR

Effective date: 20110913

PLFP Fee payment

Year of fee payment: 11

PLFP Fee payment

Year of fee payment: 12

PLFP Fee payment

Year of fee payment: 13

PLFP Fee payment

Year of fee payment: 14

ST Notification of lapse

Effective date: 20210506