ATE545582T1 - Verfahren und vorrichtung zur herstellung einer versteiften platte - Google Patents

Verfahren und vorrichtung zur herstellung einer versteiften platte

Info

Publication number
ATE545582T1
ATE545582T1 AT08750766T AT08750766T ATE545582T1 AT E545582 T1 ATE545582 T1 AT E545582T1 AT 08750766 T AT08750766 T AT 08750766T AT 08750766 T AT08750766 T AT 08750766T AT E545582 T1 ATE545582 T1 AT E545582T1
Authority
AT
Austria
Prior art keywords
stop block
base
hand
hand side
producing
Prior art date
Application number
AT08750766T
Other languages
English (en)
Inventor
Alan Minshull
Original Assignee
Airbus Operations Ltd
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 Ltd filed Critical Airbus Operations Ltd
Application granted granted Critical
Publication of ATE545582T1 publication Critical patent/ATE545582T1/de

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D39/00—Application of procedures in order to connect objects or parts, e.g. coating with sheet metal otherwise than by plating; Tube expanders
    • 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
    • B33—ADDITIVE MANUFACTURING TECHNOLOGY
    • B33Y—ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
    • B33Y80/00—Products made by additive manufacturing
    • 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
    • Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P70/00—Climate change mitigation technologies in the production process for final industrial or consumer products
    • Y02P70/50—Manufacturing or production processes characterised by the final manufactured product
    • 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
    • Y10T29/49616—Structural member making
    • Y10T29/49622—Vehicular structural member making
    • 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
    • Y10T29/49616—Structural member making
    • Y10T29/49623—Static structure, e.g., a building component
    • Y10T29/49629—Panel
    • 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
    • Y10T29/49895—Associating parts by use of aligning means [e.g., use of a drift pin or a "fixture"]
    • 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
    • Y10T29/49895—Associating parts by use of aligning means [e.g., use of a drift pin or a "fixture"]
    • Y10T29/49899—Associating parts by use of aligning means [e.g., use of a drift pin or a "fixture"] by multiple cooperating aligning means
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Transportation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Laminated Bodies (AREA)
  • Joining Of Building Structures In Genera (AREA)
  • Finishing Walls (AREA)
  • Moulding By Coating Moulds (AREA)
  • Devices For Post-Treatments, Processing, Supply, Discharge, And Other Processes (AREA)
AT08750766T 2007-05-31 2008-05-23 Verfahren und vorrichtung zur herstellung einer versteiften platte ATE545582T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GBGB0710349.2A GB0710349D0 (en) 2007-05-31 2007-05-31 Method of manufacturing a stiffened panel
PCT/GB2008/050371 WO2008146034A2 (en) 2007-05-31 2008-05-23 Method of manufacturing a stiffened panel

Publications (1)

Publication Number Publication Date
ATE545582T1 true ATE545582T1 (de) 2012-03-15

Family

ID=38289569

Family Applications (1)

Application Number Title Priority Date Filing Date
AT08750766T ATE545582T1 (de) 2007-05-31 2008-05-23 Verfahren und vorrichtung zur herstellung einer versteiften platte

Country Status (11)

Country Link
US (1) US8752294B2 (de)
EP (2) EP2148816B1 (de)
JP (1) JP5497637B2 (de)
KR (1) KR20080105960A (de)
CN (1) CN101674986B (de)
AT (1) ATE545582T1 (de)
BR (1) BRPI0812017A2 (de)
CA (1) CA2686127C (de)
GB (1) GB0710349D0 (de)
RU (1) RU2465178C2 (de)
WO (1) WO2008146034A2 (de)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0710349D0 (en) * 2007-05-31 2007-07-11 Airbus Uk Ltd Method of manufacturing a stiffened panel
US9614430B2 (en) * 2014-02-26 2017-04-04 Fsp Technology Inc. Inverting apparatus and AC power system using the same
US10052670B2 (en) * 2015-09-11 2018-08-21 Triumph Aerostructures, Llc Stringer forming device and methods of using the same
CN110860613B (zh) * 2019-11-19 2020-10-09 燕山大学 大型异型管材微铸轧增材制造的内腔近净成型装置

Family Cites Families (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS58143075U (ja) * 1982-03-16 1983-09-27 トヨタ自動車株式会社 板金部品の位置決め固定装置
DE3219151A1 (de) 1982-05-21 1983-11-24 Gross & Froelich GmbH, 7000 Stuttgart Spannvorrichtung
JPS59109587A (ja) 1982-12-16 1984-06-25 Nippon Steel Corp コ−クス炉装入炭の乾燥予熱輸送装置
JPS59109587U (ja) * 1983-01-17 1984-07-24 日産自動車株式会社 ゲ−ジプレ−ト
JPS59185093U (ja) * 1983-05-26 1984-12-08 三菱重工業株式会社 板状部材と骨材との組立治具
US5033178A (en) 1988-07-06 1991-07-23 The Boeing Company Assembly jig and method for making wing panels
US4894903A (en) 1988-07-06 1990-01-23 The Boeing Company Assembly jig and method for making wing panels
US5135695A (en) 1989-12-04 1992-08-04 Board Of Regents The University Of Texas System Positioning, focusing and monitoring of gas phase selective beam deposition
SU1777297A1 (ru) * 1990-02-12 1997-05-20 Обнинское научно-производственное объединение "Технология" Панель из композиционного материала и способ ее изготовления
US5341556A (en) * 1991-06-28 1994-08-30 The United States Of America As Represented By The Secretary Of The Air Force Method and apparatus for manufacture of reinforced panels
RU2067543C1 (ru) * 1992-04-14 1996-10-10 Акционерное общество открытого типа "Таганрогская авиация" Устройство для сборки агрегатов летательных аппаратов
US5367595A (en) 1993-07-15 1994-11-22 General Motors Corporation Fiber optic connector for connecting a fiber optic harness to an optical device
US5906863A (en) 1994-08-08 1999-05-25 Lombardi; John Methods for the preparation of reinforced three-dimensional bodies
JP3144317B2 (ja) 1996-09-12 2001-03-12 トヨタ自動車株式会社 積層製造方法
CN1051520C (zh) * 1996-10-07 2000-04-19 王新云 飞行器的预应力结构及制造方法
US6143378A (en) * 1998-05-12 2000-11-07 Sandia Corporation Energetic additive manufacturing process with feed wire
US6410105B1 (en) * 1998-06-30 2002-06-25 Jyoti Mazumder Production of overhang, undercut, and cavity structures using direct metal depostion
US6200514B1 (en) 1999-02-09 2001-03-13 Baker Hughes Incorporated Process of making a bit body and mold therefor
US6855099B2 (en) * 2001-10-31 2005-02-15 The Boeing Company Manufacturing system for aircraft structures and other large structures
US7076856B2 (en) 2002-11-14 2006-07-18 The Boeing Company Adjustable system and method for supporting and joining structural members
GB2399049B (en) 2003-03-05 2006-01-18 Stour Prec Tools Ltd Composite structural component and method
GB2405119B (en) * 2003-08-01 2007-08-01 Martin Gibbons A clamp for holding a door to be worked on
DE10342880A1 (de) 2003-09-15 2005-04-14 Trumpf Werkzeugmaschinen Gmbh + Co. Kg Substratplatte
GB0519364D0 (en) * 2005-09-22 2005-11-02 Airbus Uk Ltd Assembly of aircraft components
GB0710349D0 (en) * 2007-05-31 2007-07-11 Airbus Uk Ltd Method of manufacturing a stiffened panel

Also Published As

Publication number Publication date
EP2148816B1 (de) 2012-02-15
CN101674986B (zh) 2015-11-25
US8752294B2 (en) 2014-06-17
JP2010527847A (ja) 2010-08-19
WO2008146034A3 (en) 2009-05-07
CA2686127C (en) 2016-05-03
GB0710349D0 (en) 2007-07-11
US20100170165A1 (en) 2010-07-08
BRPI0812017A2 (pt) 2014-11-18
CA2686127A1 (en) 2008-12-04
WO2008146034A2 (en) 2008-12-04
JP5497637B2 (ja) 2014-05-21
RU2465178C2 (ru) 2012-10-27
EP2441679B1 (de) 2015-07-01
EP2148816A2 (de) 2010-02-03
EP2441679A3 (de) 2013-02-13
RU2009145627A (ru) 2011-07-10
CN101674986A (zh) 2010-03-17
EP2441679A2 (de) 2012-04-18
KR20080105960A (ko) 2008-12-04

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