ATE292539T1 - Verfahren zum montieren von biegsamen platten auf eine offene struktur und anlage zur durchführung des verfahrens - Google Patents

Verfahren zum montieren von biegsamen platten auf eine offene struktur und anlage zur durchführung des verfahrens

Info

Publication number
ATE292539T1
ATE292539T1 AT00401949T AT00401949T ATE292539T1 AT E292539 T1 ATE292539 T1 AT E292539T1 AT 00401949 T AT00401949 T AT 00401949T AT 00401949 T AT00401949 T AT 00401949T AT E292539 T1 ATE292539 T1 AT E292539T1
Authority
AT
Austria
Prior art keywords
implementing
open structure
flexible panels
mounting flexible
panel
Prior art date
Application number
AT00401949T
Other languages
English (en)
Inventor
Jean Noel Guillou
Andre Gregoire
Original Assignee
Sonaca Sa
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 Sonaca Sa filed Critical Sonaca Sa
Application granted granted Critical
Publication of ATE292539T1 publication Critical patent/ATE292539T1/de

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/26—Construction, shape, or attachment of separate skins, e.g. panels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P19/00—Machines for simply fitting together or separating metal parts or objects, or metal and non-metal parts, whether or not involving some deformation; Tools or devices therefor so far as not provided for in other classes
    • B23P19/04—Machines for simply fitting together or separating metal parts or objects, or metal and non-metal parts, whether or not involving some deformation; Tools or devices therefor so far as not provided for in other classes for assembling or disassembling parts
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/28—Leading or trailing edges attached to primary structures, e.g. forming fixed slots
    • 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
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P2700/00—Indexing scheme relating to the articles being treated, e.g. manufactured, repaired, assembled, connected or other operations covered in the subgroups
    • B23P2700/01—Aircraft parts
    • 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
    • Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10—Methods of surface bonding and/or assembly therefor
    • Y10T156/1002—Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina
    • Y10T156/1028—Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina by bending, drawing or stretch forming sheet to assume shape of configured lamina while in contact therewith
    • Y10T156/1031—Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina by bending, drawing or stretch forming sheet to assume shape of configured lamina while in contact therewith with preshaping of lamina

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Transportation (AREA)
  • Helmets And Other Head Coverings (AREA)
  • Connection Of Plates (AREA)
  • Automatic Assembly (AREA)
  • Body Structure For Vehicles (AREA)
  • Standing Axle, Rod, Or Tube Structures Coupled By Welding, Adhesion, Or Deposition (AREA)
  • Conveying And Assembling Of Building Elements In Situ (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Roof Covering Using Slabs Or Stiff Sheets (AREA)
AT00401949T 1999-07-09 2000-07-06 Verfahren zum montieren von biegsamen platten auf eine offene struktur und anlage zur durchführung des verfahrens ATE292539T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
BE9900474A BE1012781A3 (fr) 1999-07-09 1999-07-09 Procede d'assemblage d'un panneau souple sur une structure ouverte et installation pour la mise en oeuvre de ce procede.

Publications (1)

Publication Number Publication Date
ATE292539T1 true ATE292539T1 (de) 2005-04-15

Family

ID=3891997

Family Applications (1)

Application Number Title Priority Date Filing Date
AT00401949T ATE292539T1 (de) 1999-07-09 2000-07-06 Verfahren zum montieren von biegsamen platten auf eine offene struktur und anlage zur durchführung des verfahrens

Country Status (8)

Country Link
US (1) US6551428B1 (de)
EP (1) EP1066914B1 (de)
AT (1) ATE292539T1 (de)
BE (1) BE1012781A3 (de)
BR (1) BR0002658A (de)
CA (1) CA2314162C (de)
DE (1) DE60019203T2 (de)
ES (1) ES2240028T3 (de)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US12612309B2 (en) 2020-01-08 2026-04-28 Thyssenkrupp Industrial Solutions Ag Integrated method for the commercial and industrial utilisation of calcium sulphate whilst obtaining rare earth elements from the production of phosphoric acid

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US7048174B2 (en) * 2003-08-25 2006-05-23 The Boeing Company Adaptable spring force clamping apparatus and methods
US9033328B2 (en) * 2003-10-31 2015-05-19 The Boeing Company Reconfigurable clamping system
BE1016117A3 (fr) * 2004-07-09 2006-03-07 Sonaca Sa Volet mobile de bord d'attaque d'une aile principale de la voilure d'un aeronef.
US20060080919A1 (en) * 2004-10-14 2006-04-20 Dykstra Thomas L Fabric/rail attachment process
US7748591B2 (en) * 2004-12-14 2010-07-06 The Boeing Company Pressure foot clamp for friction stir welding machine
US20060237888A1 (en) * 2005-04-22 2006-10-26 The Boeing Company Inflatable clamping systems and methods
CN101648335B (zh) * 2009-09-08 2011-10-05 南车南京浦镇车辆有限公司 轨道车辆车窗安装工艺
FR3015328B1 (fr) * 2013-12-19 2016-05-27 Aerolia Procede et systeme d'assemblage d'une pluralite de panneaux
FR3015329B1 (fr) * 2013-12-19 2016-05-20 Aerolia Procede, dispositif et systeme d'assemblage d'une pluralite de panneaux
DE102014017596B4 (de) * 2014-05-16 2025-01-30 Liebherr-Aerospace Lindenberg Gmbh Flash FAL Track II
JP2017013201A (ja) * 2015-07-03 2017-01-19 三菱重工業株式会社 位置決め装置および位置決め方法
JP2017024140A (ja) * 2015-07-27 2017-02-02 三菱重工業株式会社 位置決めシステムおよび位置決め方法
JP6650147B2 (ja) * 2016-02-02 2020-02-19 三菱重工業株式会社 航空機パネル製造方法及び航空機パネル製造システム
CN106808191B (zh) * 2016-06-07 2019-06-28 东莞理工学院 一种散热片胶钉安装贴胶一体机
GB201710385D0 (en) * 2017-06-29 2017-08-16 Airbus Operations Gmbh Aerofoil structure and method of assembly
US10669043B2 (en) * 2017-08-10 2020-06-02 Gulfstream Aerospace Corporation Fixtures for working aircraft components and methods for the same
IT201700122745A1 (it) * 2017-10-27 2019-04-27 Salver S P A Procedimento di assemblaggio di parti di un’ala aeronautica
CN108127382A (zh) * 2017-12-05 2018-06-08 北京星航机电装备有限公司 一种盖板式tps结构的装配方法
US10773830B2 (en) * 2018-04-26 2020-09-15 The Boeing Company Flexible track manufacturing system and method
GB2577279A (en) * 2018-09-19 2020-03-25 Airbus Operations Ltd A wing assembly
CN109483201B (zh) * 2018-12-29 2024-06-25 浙江联宜电机有限公司 弹簧销压装装置
US11383821B2 (en) 2019-03-22 2022-07-12 Airbus Operations Gmbh Wing leading-edge device and a wing having such a wing leading-edge device
DE102019114098A1 (de) 2019-05-27 2020-12-03 Airbus Operations Gmbh Strömungskörper für ein Luftfahrzeug mit einer massiven Hinterkantenkomponente
CN110723307B (zh) * 2019-09-30 2020-12-22 北京星航机电装备有限公司 一种用于飞行器离线换装隔热瓦粘接加载的弓形卡
DE102020100241A1 (de) 2020-01-08 2021-07-08 Thyssenkrupp Ag Verfahren zur Herstellung von Phosphorsäure und Klinkerprozess-geeigneter Kalziumsulfatqualität zur kommerziellen und industriellen Verwertung von Kalziumsulfat
CN113501138B (zh) * 2021-09-13 2021-11-30 成都飞机工业（集团）有限责任公司 一种增加飞机部件精整加工工艺刚性的方法
CN114962403B (zh) * 2022-04-22 2022-12-13 广州韩乐电器实业有限公司 一种组合式液晶电视边框与显示板组合设备

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3376184A (en) * 1965-06-11 1968-04-02 Lawrence H Egland Pressure bonding system for spanwise reinforced airfoils
US3616075A (en) * 1968-11-20 1971-10-26 American Aviat Corp Fuselage jig
US4595444A (en) 1983-11-14 1986-06-17 United Technologies Corporation Isostatic die and method for assembly of skeletal structures
US4783228A (en) * 1986-07-03 1988-11-08 Lockheed Corporation Method of bonding metal skins to internal support structures
FR2611552A1 (fr) * 1987-02-27 1988-09-09 Renault Procede pour l'assemblage automatise de pieces de tolerie notamment
US4894903A (en) * 1988-07-06 1990-01-23 The Boeing Company Assembly jig and method for making wing panels
US5425908A (en) * 1993-02-05 1995-06-20 Foamseal, Inc. Method of forming structural panel assemblies
WO1997034733A1 (en) 1996-03-22 1997-09-25 The Boeing Company Determinant spar assembly

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US12612309B2 (en) 2020-01-08 2026-04-28 Thyssenkrupp Industrial Solutions Ag Integrated method for the commercial and industrial utilisation of calcium sulphate whilst obtaining rare earth elements from the production of phosphoric acid

Also Published As

Publication number Publication date
EP1066914B1 (de) 2005-04-06
CA2314162C (fr) 2009-01-06
BE1012781A3 (fr) 2001-03-06
CA2314162A1 (fr) 2001-01-09
DE60019203T2 (de) 2006-01-26
DE60019203D1 (de) 2005-05-12
ES2240028T3 (es) 2005-10-16
EP1066914A1 (de) 2001-01-10
US6551428B1 (en) 2003-04-22
BR0002658A (pt) 2001-03-13

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