[go: up one dir, main page]

FR3009351B1 - Outillage pour le maintien simultane de plusieurs clips de fixation contre un element de cadre de fuselage d'aeronef - Google Patents

Outillage pour le maintien simultane de plusieurs clips de fixation contre un element de cadre de fuselage d'aeronef

Info

Publication number
FR3009351B1
FR3009351B1 FR1357672A FR1357672A FR3009351B1 FR 3009351 B1 FR3009351 B1 FR 3009351B1 FR 1357672 A FR1357672 A FR 1357672A FR 1357672 A FR1357672 A FR 1357672A FR 3009351 B1 FR3009351 B1 FR 3009351B1
Authority
FR
France
Prior art keywords
tooling
frame element
aircraft fuselage
fuselage frame
fastening clips
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
FR1357672A
Other languages
English (en)
Other versions
FR3009351A1 (fr
Inventor
Yannick Marin
Damien Guilloteau
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 FR1357672A priority Critical patent/FR3009351B1/fr
Priority to US14/448,779 priority patent/US9527606B2/en
Priority to CN201410378489.6A priority patent/CN104339290B/zh
Publication of FR3009351A1 publication Critical patent/FR3009351A1/fr
Application granted granted Critical
Publication of FR3009351B1 publication Critical patent/FR3009351B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/10—Manufacturing or assembling aircraft, e.g. jigs 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
    • B64C1/061—Frames
    • 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
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49826—Assembling or joining
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/53—Means to assemble or disassemble
    • Y10T29/53978—Means to assemble or disassemble including means to relatively position plural work parts

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Transportation (AREA)
  • Automatic Assembly (AREA)
FR1357672A 2013-08-01 2013-08-01 Outillage pour le maintien simultane de plusieurs clips de fixation contre un element de cadre de fuselage d'aeronef Expired - Fee Related FR3009351B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1357672A FR3009351B1 (fr) 2013-08-01 2013-08-01 Outillage pour le maintien simultane de plusieurs clips de fixation contre un element de cadre de fuselage d'aeronef
US14/448,779 US9527606B2 (en) 2013-08-01 2014-07-31 Tool to hold several mounting clamps simultaneously against an aircraft fuselage frame element
CN201410378489.6A CN104339290B (zh) 2013-08-01 2014-08-01 将数个安装夹具同时保持在飞行器机身框架元件上的工具

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1357672A FR3009351B1 (fr) 2013-08-01 2013-08-01 Outillage pour le maintien simultane de plusieurs clips de fixation contre un element de cadre de fuselage d'aeronef

Publications (2)

Publication Number Publication Date
FR3009351A1 FR3009351A1 (fr) 2015-02-06
FR3009351B1 true FR3009351B1 (fr) 2015-08-07

Family

ID=49237471

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1357672A Expired - Fee Related FR3009351B1 (fr) 2013-08-01 2013-08-01 Outillage pour le maintien simultane de plusieurs clips de fixation contre un element de cadre de fuselage d'aeronef

Country Status (3)

Country Link
US (1) US9527606B2 (fr)
CN (1) CN104339290B (fr)
FR (1) FR3009351B1 (fr)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
FR3061054B1 (fr) * 2016-12-22 2019-06-14 Airbus Operations Dispositif de guidage adapte pour se positionner sur une surface a double rayon de courbure
US10520933B2 (en) * 2018-04-13 2019-12-31 The Boeing Company System and method for removing a workpiece from a manufacturing fixture
CN109605103A (zh) * 2018-12-13 2019-04-12 上海航天设备制造总厂有限公司 一种用于角片双边定位的装置
CN111531495A (zh) * 2020-05-15 2020-08-14 沈阳飞机工业（集团）有限公司 复材t或工型长桁间距控制的方法
CN111451970B (zh) * 2020-05-19 2025-04-01 西安臻航智能装备科技有限公司 飞机长桁自动锁紧装置及自动锁紧方法
CN111776245B (zh) * 2020-06-12 2023-09-05 陕西飞机工业（集团）有限公司 一种卡板及卡板的安装方法
CN115540791B (zh) * 2022-12-01 2023-03-14 成都市鸿侠科技有限责任公司 一种飞机蒙皮外形精度检测装置

Family Cites Families (65)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2620008A (en) * 1948-12-07 1952-12-02 Logan L Mallard Deformable means for interlocking machine elements
US2680497A (en) 1950-04-24 1954-06-08 Bernard C Miller Gang of grease fitting caps
US3036521A (en) 1958-07-28 1962-05-29 Go Oil Well Services Inc Bore hole perforating apparatus
US3177915A (en) * 1961-01-16 1965-04-13 Fleur George La Trim fastener and strip
US3165968A (en) * 1962-07-23 1965-01-19 Edgar P Anstett Synthetic plastic nailing strip
FR1345076A (fr) 1962-10-24 1963-12-06 Sud Aviation Perfectionnement aux structures à revêtement mince renforcé par des éléments longitudinaux et transversaux
US3241658A (en) * 1964-11-19 1966-03-22 Bechik Products Inc Plastic handles in bundle form
US3467417A (en) * 1966-11-09 1969-09-16 Standard Pressed Steel Co Fastener unit
US3648749A (en) 1970-02-05 1972-03-14 Central Screw Co Fastener assembly with locking capabilities
US3999659A (en) * 1970-03-23 1976-12-28 Maclean-Fogg Lock Nut Company Pierce nuts in strip form
US3704507A (en) * 1970-03-23 1972-12-05 Mac Lean Fogg Lock Nut Co Method of fabricating and attaching pierce nuts to a panel
US3711931A (en) * 1971-04-01 1973-01-23 Multifastener Corp Method of forming fastener strip
US3967528A (en) * 1974-04-05 1976-07-06 The United States Of America As Represented By The Secretary Of The Navy Bomb rack sway bolt assembly
US4310132A (en) 1978-02-16 1982-01-12 Nasa Fuselage structure using advanced technology fiber reinforced composites
US4310964A (en) * 1979-01-02 1982-01-19 The Boeing Company Method and apparatus for the automated assembly of major subassemblies
US4203204A (en) * 1979-01-02 1980-05-20 The Boeing Company Apparatus for the automated assembly of major subassemblies
FR2489779A1 (fr) 1980-09-09 1982-03-12 Aerospatiale Structure de fuselage pour aeronef resistant aux ruptures longitudinales du revetement exterieur
GB2101506B (en) * 1981-06-18 1985-05-30 Tekron Licensing Bv Workbench vices
US4412820A (en) 1982-04-30 1983-11-01 Modcom, Inc. Orthodontic tension-applying apparatus
US4946386A (en) 1988-06-09 1990-08-07 Ormco Corporation Orthodontic O-ring dispenser and method of making
US4995146A (en) * 1988-10-26 1991-02-26 The Boeing Company Assembly jig and method for making wing spars
US5116178A (en) * 1989-03-16 1992-05-26 General Electric Company Safety cable for fasteners
US5105515A (en) * 1990-11-16 1992-04-21 The Boeing Company Wing spar assembly jig with adjustable clamp assemblies
US5142764A (en) * 1990-11-28 1992-09-01 The United States Of America As Represented By The Secretary Of The Air Force Method for tack-free positioning of aircraft components for subsequent fastening
US5242523A (en) 1992-05-14 1993-09-07 The Boeing Company Caul and method for bonding and curing intricate composite structures
US5273426A (en) 1992-06-25 1993-12-28 Dragan William B Transformable orthodontic O-ring dispenser
US5477596A (en) * 1992-12-23 1995-12-26 The Boeing Company Stringer/clip placement and drilling
US5596859A (en) 1994-09-20 1997-01-28 Horton; Jim W. Metal wall stud
US5632583A (en) 1995-07-18 1997-05-27 Schneider; William A. Split bolt ring
US5775514A (en) * 1997-02-28 1998-07-07 Lin; Jack Screw band
US6141848A (en) * 1997-06-28 2000-11-07 The Boeing Company Contoured stringer/clip drilling
US6210084B1 (en) * 1997-11-26 2001-04-03 The Boeing Company Pressure foot assembly for clamping a joint
US6158666A (en) * 1997-11-26 2000-12-12 Banks; David P. Vacuum fastened guide and method for supporting tooling on a component
US6073326A (en) * 1998-11-24 2000-06-13 The Boeing Company Lap splice mini-riveter system
US6134940A (en) * 1997-11-26 2000-10-24 The Boeing Company Angular bucking bar
US6088897A (en) * 1998-11-24 2000-07-18 The Boeing Company Bucking bar end-effector for upsetting a rivet
US6332299B1 (en) 1999-02-05 2001-12-25 Stewart, Iii Kenneth G. Connector for multiple member frame systems
EP1223002B1 (fr) * 2001-01-16 2004-04-14 Airbus Deutschland GmbH Dispositif de retenue pour maintenir en position des structures de grande dimension
US6708821B2 (en) * 2002-08-21 2004-03-23 Illinois Tool Works Inc. Fastener collation strip and debris exhaust mechanism
US6889414B2 (en) * 2003-05-27 2005-05-10 General Motors Corporation Reusable retainer and assembly
US20070246876A1 (en) * 2006-04-21 2007-10-25 The Boeing Company Reconfigurable Low-Profile Pneumatic Edge-Clamp Systems and Methods
DE102006051457B4 (de) 2006-10-31 2012-04-12 Airbus Operations Gmbh Versteifungselement für ein Luft- oder Raumfahrzeug und Verfahren zum Herstellen desselben
US8910908B2 (en) 2006-10-31 2014-12-16 Airbus Operations Gmbh Two-piece stiffening element
US7735780B2 (en) * 2007-12-20 2010-06-15 L-3 Communications Integrated Systems, L.P. Aircraft stringer clip and related methods
DE102008012252B4 (de) 2008-03-03 2014-07-31 Airbus Operations Gmbh Verbund sowie Luft- oder Raumfahrzeug mit einem derartigen Verbund
WO2009120964A2 (fr) 2008-03-27 2009-10-01 The General Hospital Corporation Cytométrie en flux in vivo fondée sur l’autofluorescence cellulaire
AT508169A1 (de) 2009-04-16 2010-11-15 Facc Ag Spant und verfahren zur herstellung eines solchen spants
DE102009019337B4 (de) 2009-04-30 2015-05-13 Airbus Operations Gmbh Modulare Haltevorrichtung für innerhalb eines Flugzeugrumpfs verlegte Anbauteile
US8181949B2 (en) * 2009-05-25 2012-05-22 Yi-Po Hung Micro-adjustable parallel bench vise
US8235634B2 (en) * 2009-07-27 2012-08-07 Ortronics, Inc. Cage nut assembly
CN201496349U (zh) * 2009-08-31 2010-06-02 中国建筑西南设计研究院有限公司 一种隐藏式卡环连接系统
CN102019592B (zh) * 2009-09-10 2012-07-04 中国航空工业集团公司北京航空制造工程研究所 一种大尺寸复合材料加筋壁板成形的定位装置
DE102009056999B4 (de) 2009-12-04 2014-08-21 Eads Deutschland Gmbh Versteifungsstruktur für Hautfeld und Flugzeug
US8510952B2 (en) * 2010-07-15 2013-08-20 The Boeing Company Agile manufacturing apparatus and method for high throughput
ES2400771B1 (es) 2011-03-30 2014-02-14 Airbus Operations S.L. Fuselaje de aeronave con cuadernas altamente resistentes.
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
EP2565117B1 (fr) * 2011-08-29 2013-12-11 Airbus Operations (S.A.S.) Élément de raidissement pour avion
GB2495075A (en) 2011-09-14 2013-04-03 Simon Bullivant Coupling assembly and method for coupling reinforcing bars used in concrete blocks in an end to end relationship
CN202592246U (zh) * 2012-04-27 2012-12-12 西安飞机工业（集团）有限责任公司 一种飞机长桁的定位机构
US8720730B2 (en) 2012-08-02 2014-05-13 Douglas Bodden, JR. Lid saver and method
US8784028B2 (en) 2012-10-16 2014-07-22 Northrop Grumman Systems Corporation Tethered fastening device
GB2510170B (en) * 2013-01-28 2015-10-14 Business Lines Ltd Security device for connecting together adjacent wheel nut covers
FR3007735B1 (fr) 2013-06-28 2015-08-07 Airbus Operations Sas Liaison d'un element de fuselage d'aeronef et d'un cadre par une entretoise et une cale
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

Also Published As

Publication number Publication date
FR3009351A1 (fr) 2015-02-06
CN104339290A (zh) 2015-02-11
CN104339290B (zh) 2017-09-26
US9527606B2 (en) 2016-12-27
US20150040369A1 (en) 2015-02-12

Similar Documents

Publication Publication Date Title
FR3009352B1 (fr) Outillage pour le maintien simultane de plusieurs clips de fixation contre un element de cadre de fuselage d'aeronef
FR3009351B1 (fr) Outillage pour le maintien simultane de plusieurs clips de fixation contre un element de cadre de fuselage d'aeronef
IL283542B (en) Method and device for functional imaging of the brain
IL255961B (en) Anti-cd40 antibodies and uses thereof
EP3380000A4 (fr) Procédés et systèmes destinés à fournir des stimuli au cerveau
DK3326606T3 (en) Methods for fixing hair and skin
ZA201505860B (en) Methods for the synthesis of sphingomyelins and dihydrosphingomyelins
IL244405A0 (en) System and method for sorting
HUE044954T2 (hu) Elektroretinográfiás (ERG) rendszer pszichiátriai rendellenességek felmérésére
GB2580816B (en) Integrated manifold system
IL242943A0 (en) A process for the preparation of abiraterone and its intermediates
EP3051176A4 (fr) Matériau d'amortissement de vibrations et procédé de fixation de matériau d'amortissement de vibrations
SG11201705748SA (en) Anti-glycoprotein antibodies and uses thereof
PT3265039T (pt) Suporte de membro e sistema de fixação do suporte de membro
FR3039511B1 (fr) Rechauffage pour equipement aeronautique d'aeronef
EP3114967A4 (fr) Structure de fixation de revêtement et siège de véhicule
PL3586016T3 (pl) Przyrząd mocujący i zespół mocujący
PL3277658T3 (pl) Sposób i system do syntezy biodiesla
SG11201510230PA (en) Aircraft capable of passing from the aerial domain to the spatial domain and method for automatically adapting the configuration of same
SG11201907112RA (en) Fastening structure and fastening method
SG11201907113SA (en) Fastening structure and fastening method
FR2993240B1 (fr) Structure d'aeronef, et procede de montage associe
GB201618423D0 (en) Methods for fixing hair and skin
GB201522797D0 (en) Method and system for adjusting the maximum duartion of time-critical functions
PL3582317T3 (pl) Niestandardowy moduł bms i sposób jego projektowania

Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 4

PLFP Fee payment

Year of fee payment: 5

PLFP Fee payment

Year of fee payment: 6

PLFP Fee payment

Year of fee payment: 7

ST Notification of lapse

Effective date: 20210405