CN101873965B - 飞机机身环周接合部处的ω形加固件的拼接 - Google Patents

飞机机身环周接合部处的ω形加固件的拼接 Download PDF

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Publication number
CN101873965B
CN101873965B CN2008801119059A CN200880111905A CN101873965B CN 101873965 B CN101873965 B CN 101873965B CN 2008801119059 A CN2008801119059 A CN 2008801119059A CN 200880111905 A CN200880111905 A CN 200880111905A CN 101873965 B CN101873965 B CN 101873965B
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China
Prior art keywords
clamping plate
reinforcing member
substrate
fastening element
areal
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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
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CN2008801119059A
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English (en)
Chinese (zh)
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CN101873965A (zh
Inventor
H·卡泽纳夫
B·卡恰圭拉
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Alrbus Operations Sas
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Alrbus Operations Sas
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    • 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
    • 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

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Connection Of Plates (AREA)
  • Road Paving Structures (AREA)
  • Footwear And Its Accessory, Manufacturing Method And Apparatuses (AREA)
  • Passenger Equipment (AREA)
  • Orthopedics, Nursing, And Contraception (AREA)
CN2008801119059A 2007-10-18 2008-10-15 飞机机身环周接合部处的ω形加固件的拼接 Expired - Fee Related CN101873965B (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR0758406 2007-10-18
FR0758406A FR2922516B1 (fr) 2007-10-18 2007-10-18 Eclissage de raidisseurs en omega au niveau d'une jonction circonferentielle d'un fuselage d'avion
PCT/FR2008/051862 WO2009053645A2 (fr) 2007-10-18 2008-10-15 Eclissage de raidisseurs en oméga au niveau d'une jonction circonférentielle d'un fuselage d'avion

Publications (2)

Publication Number Publication Date
CN101873965A CN101873965A (zh) 2010-10-27
CN101873965B true CN101873965B (zh) 2013-10-23

Family

ID=39456542

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2008801119059A Expired - Fee Related CN101873965B (zh) 2007-10-18 2008-10-15 飞机机身环周接合部处的ω形加固件的拼接

Country Status (9)

Country Link
US (1) US8302909B2 (enExample)
EP (1) EP2200899B1 (enExample)
JP (1) JP5414680B2 (enExample)
CN (1) CN101873965B (enExample)
BR (1) BRPI0818031A2 (enExample)
CA (1) CA2702316C (enExample)
FR (1) FR2922516B1 (enExample)
RU (1) RU2482014C2 (enExample)
WO (1) WO2009053645A2 (enExample)

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FR2922516B1 (fr) * 2007-10-18 2010-04-16 Airbus France Eclissage de raidisseurs en omega au niveau d'une jonction circonferentielle d'un fuselage d'avion
DE102007054053A1 (de) * 2007-11-13 2009-05-20 Airbus Deutschland Gmbh Kupplungselement zur Verbindung von zwei Längsversteifungselementen
DE102008012252B4 (de) * 2008-03-03 2014-07-31 Airbus Operations Gmbh Verbund sowie Luft- oder Raumfahrzeug mit einem derartigen Verbund
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.
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
ES2384250B1 (es) * 2009-09-30 2013-05-16 Airbus Operations, S.L. Unión de elementos estructurales de aeronave.
DE102009060695A1 (de) * 2009-12-29 2011-07-07 Airbus Operations GmbH, 21129 Flugzeugrumpf und Hautfeld
ES2392236B1 (es) * 2010-01-15 2013-10-09 Airbus Operations, S.L. Componente de aeronave con paneles rigidizados con larguerillos.
US9682514B2 (en) 2010-06-25 2017-06-20 The Boeing Company Method of manufacturing resin infused composite parts using a perforated caul sheet
US8628717B2 (en) 2010-06-25 2014-01-14 The Boeing Company Composite structures having integrated stiffeners and method of making the same
US8940213B2 (en) 2010-06-25 2015-01-27 The Boeing Company Resin infusion of composite parts using a perforated caul sheet
US8636252B2 (en) 2010-06-25 2014-01-28 The Boeing Company Composite structures having integrated stiffeners with smooth runouts and method of making the same
EP2404824B1 (fr) * 2010-07-08 2015-09-09 Airbus Opérations SAS Structure d'aeronef et Procédé de réalisation d'une telle structure
US8567722B2 (en) 2010-12-15 2013-10-29 The Boeing Company Splice and associated method for joining fuselage sections
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
ES2398985B1 (es) * 2011-03-14 2014-02-14 Airbus Operations S.L. Dispositivos de transferencia de carga en la terminación de un larguerillo.
FR2976916B1 (fr) * 2011-06-27 2013-07-26 Airbus Operations Sas Dispositif et procede d'assemblage de deux troncons de fuselage d'aeronef
FR2978372B1 (fr) * 2011-07-27 2013-09-13 Airbus Operations Sas Panneau raidi pour aeronef, comprenant des raidisseurs a ames entaillees
US8684311B2 (en) * 2012-03-07 2014-04-01 The Boeing Company Bonded splice joint
FR3000018B1 (fr) * 2012-12-21 2016-12-09 Airbus Operations Sas Raidisseur de fuselage d'aeronef, son procede de fabrication, et fuselage d'aeronef equipe d'un tel raidisseur
EP2759467B1 (en) * 2013-01-24 2016-10-19 Airbus Operations GmbH Aircraft frame and method of mounting two fuselage segments
EP2781450B1 (en) 2013-03-19 2018-05-02 Airbus Operations GmbH System and method for interconnecting composite structures
US9205634B2 (en) * 2013-05-16 2015-12-08 The Boeing Company Composite structure and method
FR3006297B1 (fr) * 2013-05-29 2016-07-15 Airbus Operations Sas Procede d'assemblage de deux panneaux comportant des raidisseurs a l'aide d'eclisses et aeronef comprenant une zone de jonction amelioree entre une poutre ventrale et une barque avant
US9656319B2 (en) * 2013-11-13 2017-05-23 The Boeing Company Positioning system for electromagnetic riveting
DE102014103179B3 (de) * 2014-03-10 2015-08-06 Airbus Operations Gmbh Kupplung zur Verbindung zweier Stringer benachbarter Rumpfsektionen
CN104724276A (zh) * 2015-04-14 2015-06-24 中航沈飞民用飞机有限责任公司 一种复合材料蒙皮防侵蚀的机身环向对接结构
US10053203B2 (en) * 2015-10-13 2018-08-21 The Boeing Company Composite stiffener with integral conductive element
CN106596003B (zh) * 2016-11-29 2019-04-23 中国航空工业集团公司沈阳飞机设计研究所 一种复合材料飞机机身段充压试验方法
US10532801B2 (en) * 2017-01-17 2020-01-14 The Boeing Company Continuous insulation blanket cap strip assemblies and methods of using same
CN108032988B (zh) * 2017-10-25 2020-06-16 北京航空航天大学 一种纤维增强复合材料飞行器舱段连接结构及其制备方法
US11845236B2 (en) 2018-03-12 2023-12-19 The Boeing Company Composite structure splice and method
US10857751B2 (en) 2019-05-09 2020-12-08 The Boeing Company Composite stringer and methods for forming a composite stringer
US11198497B2 (en) * 2019-06-19 2021-12-14 The Boeing Company Splice fittings that are affixed to stringers via web-installed fasteners
US11420718B2 (en) * 2020-03-27 2022-08-23 The Boeing Company Aircraft tail 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.
US12017748B2 (en) * 2021-03-17 2024-06-25 The Boeing Company Fuselage barrel assemblies and methods of assembling fuselage barrel assemblies

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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
CN1863668A (zh) * 2003-10-07 2006-11-15 斯托克·福克Aesp公司 在包括局部加强件的层压板中的接合结构
CN1906081A (zh) * 2004-01-05 2007-01-31 空中客车德国有限公司 用于飞机中客舱的内衬板的板装置

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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
DE102007029500B4 (de) * 2007-06-25 2013-02-14 Airbus Operations Gmbh Verfahren zum Koppeln von Versteifungsprofilelementen sowie Strukturbauteil
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
FR2922516B1 (fr) * 2007-10-18 2010-04-16 Airbus France Eclissage de raidisseurs en omega au niveau d'une jonction circonferentielle d'un fuselage d'avion
DE102008012252B4 (de) * 2008-03-03 2014-07-31 Airbus Operations Gmbh Verbund sowie Luft- oder Raumfahrzeug mit einem derartigen Verbund

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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
CN1863668A (zh) * 2003-10-07 2006-11-15 斯托克·福克Aesp公司 在包括局部加强件的层压板中的接合结构
CN1906081A (zh) * 2004-01-05 2007-01-31 空中客车德国有限公司 用于飞机中客舱的内衬板的板装置

Also Published As

Publication number Publication date
RU2482014C2 (ru) 2013-05-20
FR2922516A1 (fr) 2009-04-24
FR2922516B1 (fr) 2010-04-16
WO2009053645A3 (fr) 2009-06-18
EP2200899A2 (fr) 2010-06-30
BRPI0818031A2 (pt) 2015-03-24
EP2200899B1 (fr) 2012-08-01
JP5414680B2 (ja) 2014-02-12
RU2010119710A (ru) 2011-11-27
US8302909B2 (en) 2012-11-06
JP2011500417A (ja) 2011-01-06
CA2702316A1 (fr) 2009-04-30
WO2009053645A2 (fr) 2009-04-30
CA2702316C (fr) 2015-06-16
CN101873965A (zh) 2010-10-27
US20100282905A1 (en) 2010-11-11
WO2009053645A8 (fr) 2009-12-17

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Granted publication date: 20131023

Termination date: 20191015