TR200401102T4 - Kompozit strüktürlerin montajı - Google Patents

Kompozit strüktürlerin montajı

Info

Publication number
TR200401102T4
TR200401102T4 TR2004/01102T TR200401102T TR200401102T4 TR 200401102 T4 TR200401102 T4 TR 200401102T4 TR 2004/01102 T TR2004/01102 T TR 2004/01102T TR 200401102 T TR200401102 T TR 200401102T TR 200401102 T4 TR200401102 T4 TR 200401102T4
Authority
TR
Turkey
Prior art keywords
panel
installation
form boards
composite structures
edges
Prior art date
Application number
TR2004/01102T
Other languages
English (en)
Inventor
Eric Miller Keith
John Simmonds Robert
Original Assignee
Airbus Uk Limited
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 Uk Limited filed Critical Airbus Uk Limited
Publication of TR200401102T4 publication Critical patent/TR200401102T4/tr

Links

Classifications

    • 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
    • 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
    • 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
    • Y10T29/53—Means to assemble or disassemble
    • Y10T29/53435—Means to assemble or disassemble including assembly pallet

Landscapes

  • Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Mechanical Engineering (AREA)
  • Transportation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)
  • Laminated Bodies (AREA)
  • Moulds For Moulding Plastics Or The Like (AREA)
  • Body Structure For Vehicles (AREA)
  • Moulding By Coating Moulds (AREA)

Abstract

Bu bulusta panolarin kompozit bir strüktüre montajina iliskin bir aparat ve yöntem sunulmaktadir. Söz konusu aparat kompozit bir panoyu istenen sekle çekmek ve panoyu pano üzerindeki sonraki islemlerde bu sekilde desteklemek için en az bir sablonu olan bir kalip jigi ihtiva etmektedir ve özelligi aparatin panoyu en az bir sablona dogru çekmek için en az bir kenar kenetine sahip olmasidir.
TR2004/01102T 2000-02-08 2001-02-06 Kompozit strüktürlerin montajı TR200401102T4 (tr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GBGB0002837.3A GB0002837D0 (en) 2000-02-08 2000-02-08 Assembling composite structures

Publications (1)

Publication Number Publication Date
TR200401102T4 true TR200401102T4 (tr) 2004-06-21

Family

ID=9885143

Family Applications (1)

Application Number Title Priority Date Filing Date
TR2004/01102T TR200401102T4 (tr) 2000-02-08 2001-02-06 Kompozit strüktürlerin montajı

Country Status (11)

Country Link
US (1) US7137202B2 (tr)
EP (1) EP1254047B1 (tr)
AT (1) ATE264219T1 (tr)
AU (1) AU2001235755A1 (tr)
BR (1) BR0108166B1 (tr)
CA (1) CA2398300C (tr)
DE (1) DE60102796T2 (tr)
ES (1) ES2215123T3 (tr)
GB (1) GB0002837D0 (tr)
TR (1) TR200401102T4 (tr)
WO (1) WO2001058753A1 (tr)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
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US6779272B2 (en) * 2002-08-30 2004-08-24 The Boeing Company Single piece flow based wing assembly system
US7584947B2 (en) * 2005-05-20 2009-09-08 The Boeing Company Reconfigurable workpiece support fixture
AU2007227489A1 (en) * 2006-03-17 2007-09-27 Triumf Self-supporting multilayer films having a diamond-like carbon layer
ES2357489B1 (es) * 2008-05-19 2012-03-05 Airbus Operations, S.L. Procedimiento y útil de montaje de cajones de torsión para uso aeron�?utico.
FR2988317B1 (fr) * 2012-03-23 2014-05-09 Airbus Operations Sas Outillage d'usinage pour cadre de fuselage d'aeronef
KR101416830B1 (ko) * 2012-10-15 2014-07-08 한국항공우주산업 주식회사 항공기의 주구조물 고정용 치구
EP2756934B1 (en) * 2013-01-16 2019-09-04 Airbus Operations GmbH Apparatus and method for assembling workpieces
CN103302609B (zh) * 2013-06-24 2015-09-02 中国商用飞机有限责任公司 用于翼类前缘蒙皮修边的夹持工装
WO2015038041A1 (en) * 2013-09-11 2015-03-19 Saab Ab A fixture device for manufacture of aeronautical structures and a method for applying the device
CN103921116B (zh) * 2014-04-24 2016-05-11 浙江大学 一种飞机壁板柔性装配系统
EP3587242A1 (en) * 2018-06-28 2020-01-01 BAE SYSTEMS plc Method and apparatus for assembling aircraft airframes
US11970289B2 (en) 2018-06-28 2024-04-30 Bae Systems Plc Method and apparatus for producing shims
US11731788B2 (en) 2019-05-23 2023-08-22 Bae Systems Plc Method and apparatus for producing at least part of a structural frame of a vehicle
US11353664B1 (en) 2019-08-21 2022-06-07 Senko Advanced Components, Inc. Fiber optic connector
CN113844672B (zh) * 2020-06-28 2023-04-11 航天特种材料及工艺技术研究所 一种复合材料无人机垂尾的装配型架及其装配方法
GB2599169A (en) * 2020-09-29 2022-03-30 Airbus Operations Ltd A rigid temporary reinforcement structure
JP2023070091A (ja) * 2021-11-03 2023-05-18 ザ・ボーイング・カンパニー ワークにおける機械励起振動を減衰させるためのシステム及び方法
CN114986929A (zh) * 2022-06-01 2022-09-02 沈阳飞机工业（集团）有限公司 一种提高复合材料进气道二次胶接质量和效率的方法

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US2831522A (en) 1955-05-09 1958-04-22 Liberty Products Corp Shaped block and clamp arms for shaping plates
US3094958A (en) 1958-10-27 1963-06-25 Smith Corp A O Brazing fixture
US4527783A (en) * 1983-04-26 1985-07-09 Grumman Aerospace Corporation Universal contoured parts holding fixture
US4603466A (en) * 1984-02-17 1986-08-05 Gca Corporation Wafer chuck
US4684113A (en) * 1984-09-28 1987-08-04 The Boeing Company Universal holding fixture
US4928936A (en) * 1986-12-02 1990-05-29 Nikon Corporation Loading apparatus
JPH0292636A (ja) * 1988-09-30 1990-04-03 Wakaba Sangyo:Kk 軟質シート被覆物品の製造方法
US4995146A (en) * 1988-10-26 1991-02-26 The Boeing Company Assembly jig and method for making wing spars
US5249785A (en) * 1992-04-20 1993-10-05 Boeing Commercial Airplane Group Reconfigurable holding fixture
US5239753A (en) * 1992-10-07 1993-08-31 Stahl/Scott Fetzer Company Process for forming curved vehicle body panels
AUPN516795A0 (en) * 1995-09-01 1995-09-28 Armacel Pty Limited Layered structural article
KR100207451B1 (ko) * 1995-12-14 1999-07-15 윤종용 반도체 웨이퍼 고정장치
US6170157B1 (en) * 1996-03-22 2001-01-09 The Boeing Company Determinant spar assembly
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WO1999046079A1 (en) 1998-03-12 1999-09-16 General Electro Mechanical Corporation Flexible fixture system and method
US6672576B1 (en) * 2001-12-03 2004-01-06 United Defense Lp Apparatus for and method of utilizing vacuum in machine tool operations

Also Published As

Publication number Publication date
AU2001235755A1 (en) 2001-08-20
BR0108166B1 (pt) 2010-07-13
EP1254047A1 (en) 2002-11-06
CA2398300A1 (en) 2001-08-16
DE60102796T2 (de) 2004-08-19
DE60102796D1 (de) 2004-05-19
ATE264219T1 (de) 2004-04-15
US20030000077A1 (en) 2003-01-02
GB0002837D0 (en) 2000-03-29
CA2398300C (en) 2009-02-03
WO2001058753A1 (en) 2001-08-16
US7137202B2 (en) 2006-11-21
EP1254047B1 (en) 2004-04-14
BR0108166A (pt) 2003-02-25
ES2215123T3 (es) 2004-10-01

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