ATE251571T1 - Montageverfahren - Google Patents
MontageverfahrenInfo
- Publication number
- ATE251571T1 ATE251571T1 AT01917337T AT01917337T ATE251571T1 AT E251571 T1 ATE251571 T1 AT E251571T1 AT 01917337 T AT01917337 T AT 01917337T AT 01917337 T AT01917337 T AT 01917337T AT E251571 T1 ATE251571 T1 AT E251571T1
- Authority
- AT
- Austria
- Prior art keywords
- assembly
- assembly procedure
- assembly point
- point
- location
- Prior art date
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
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23B—TURNING; BORING
- B23B2215/00—Details of workpieces
- B23B2215/04—Aircraft components
Landscapes
- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Transportation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Length Measuring Devices By Optical Means (AREA)
- Auxiliary Devices For And Details Of Packaging Control (AREA)
- Making Paper Articles (AREA)
- Diaphragms For Electromechanical Transducers (AREA)
- Drilling And Boring (AREA)
- Coupling Device And Connection With Printed Circuit (AREA)
- Magnetically Actuated Valves (AREA)
- Automatic Assembly (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GBGB0008302.2A GB0008302D0 (en) | 2000-04-06 | 2000-04-06 | Assembly method |
| PCT/GB2001/001581 WO2001076943A1 (en) | 2000-04-06 | 2001-04-06 | Assembly method |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ATE251571T1 true ATE251571T1 (de) | 2003-10-15 |
Family
ID=9889201
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AT01917337T ATE251571T1 (de) | 2000-04-06 | 2001-04-06 | Montageverfahren |
Country Status (9)
| Country | Link |
|---|---|
| US (1) | US6892160B2 (de) |
| EP (1) | EP1268276B1 (de) |
| JP (1) | JP3523237B2 (de) |
| AT (1) | ATE251571T1 (de) |
| AU (2) | AU4441701A (de) |
| DE (1) | DE60100945T2 (de) |
| ES (1) | ES2203598T3 (de) |
| GB (1) | GB0008302D0 (de) |
| WO (1) | WO2001076943A1 (de) |
Families Citing this family (22)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7384220B2 (en) * | 2004-01-06 | 2008-06-10 | The Boeing Company | Laser-guided coordination hole drilling |
| US7194326B2 (en) † | 2004-02-06 | 2007-03-20 | The Boeing Company | Methods and systems for large-scale airframe assembly |
| US20050251283A1 (en) * | 2004-04-28 | 2005-11-10 | Shovan Gerald L | Computer programed method of forming and fabricating parts into an assembly |
| GB0606079D0 (en) * | 2006-03-27 | 2006-05-03 | Airbus Uk Ltd | Aircraft component |
| US7353609B2 (en) * | 2006-05-19 | 2008-04-08 | Boeing Company | Hole location method and apparatus |
| US7500318B2 (en) * | 2006-12-08 | 2009-03-10 | Toyota Motor Engineering & Manufacturing North America, Inc. | Threaded attachment position adapter |
| RU2469924C2 (ru) * | 2007-11-29 | 2012-12-20 | Эйрбас Оперейшнс Сас | Способ монтажа крыла |
| WO2009068107A1 (en) * | 2007-11-29 | 2009-06-04 | Airbus France Sas | Method of preparing the connection between two fuselage sections of an aircraft |
| US20110119919A1 (en) * | 2009-11-23 | 2011-05-26 | The Boeing Company | Determinant Assembly System for Manufacturing Objects |
| CN102288123B (zh) * | 2011-06-27 | 2013-03-27 | 清华大学 | 一种用于焊接变形三维非接触式测量的精确定位方法 |
| DE102012209320A1 (de) * | 2012-06-01 | 2013-12-05 | Airbus Operations Gmbh | Verfahren und Lagervorrichtung zum Lagern und Ausrichten eines Bauteils |
| WO2016142907A1 (en) * | 2015-03-12 | 2016-09-15 | Bombardier Inc. | Assembly of components with datum features |
| US10275565B2 (en) | 2015-11-06 | 2019-04-30 | The Boeing Company | Advanced automated process for the wing-to-body join of an aircraft with predictive surface scanning |
| CN106652034B (zh) * | 2016-09-23 | 2020-04-28 | 江西洪都航空工业集团有限责任公司 | 蒙皮零件快速生成导孔的建模方法 |
| US10934020B2 (en) * | 2017-01-25 | 2021-03-02 | The Boeing Company | Method and system for joining structures |
| ES2859756T3 (es) | 2018-03-01 | 2021-10-04 | Aciturri Eng S L U | Procedimiento de montaje de la estructura de una aeronave y bastidor para llevar a cabo dicho procedimiento |
| US10712730B2 (en) | 2018-10-04 | 2020-07-14 | The Boeing Company | Methods of synchronizing manufacturing of a shimless assembly |
| CN111137468B (zh) * | 2019-12-20 | 2021-08-31 | 清华大学 | 多约束条件的飞机蒙皮调姿方法及系统 |
| CN111664813B (zh) * | 2020-05-15 | 2021-08-03 | 成都飞机工业(集团)有限责任公司 | 一种自由面任意孔法矢测量装置、方法及补偿方法 |
| CN112504197B (zh) * | 2020-11-09 | 2022-09-02 | 航天材料及工艺研究所 | 一种基于统一基准的多工位高效装配方法 |
| US11873072B2 (en) | 2021-01-20 | 2024-01-16 | The Boeing Company | Pressure bulkhead assembly methods and systems |
| US11845528B2 (en) | 2021-01-20 | 2023-12-19 | The Boeing Company | Pressure bulkhead assembly and method and system for making the same |
Family Cites Families (23)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5148591A (en) * | 1981-05-11 | 1992-09-22 | Sensor Adaptive Machines, Inc. | Vision target based assembly |
| FR2551860B1 (fr) * | 1983-09-08 | 1987-05-07 | Sciaky Sa | Installation pour la determination des coordonnees spatiales d'un point d'une piece, notamment pour le controle d'un outillage tel qu'un outillage de soudage de carrosserie de vehicule automobile |
| US4851905A (en) * | 1984-10-12 | 1989-07-25 | Diffracto Ltd. | Vision target fixture construction |
| US5267143A (en) * | 1984-10-12 | 1993-11-30 | Sensor Adaptive Machines, Incorporated | Vision assisted fixture construction |
| JPH0815877B2 (ja) * | 1987-12-10 | 1996-02-21 | 日産自動車株式会社 | 自動車車体の組立方法 |
| JPH0829726B2 (ja) * | 1988-07-18 | 1996-03-27 | 日産自動車株式会社 | 自動車車体の組立て方法 |
| JPH02284885A (ja) | 1989-04-27 | 1990-11-22 | Nissan Motor Co Ltd | ワーク位置決め装置の位置教示方法 |
| GB8923948D0 (en) | 1989-10-24 | 1989-12-13 | Lk Ltd | Calibration of measuring apparatus |
| IT224002Z2 (it) * | 1990-01-31 | 1995-10-05 | Comau Spa | Dispositivo per la saldatura di scocche di autoveicoli |
| IT1239874B (it) * | 1990-01-31 | 1993-11-15 | Comau Spa | Dispositivo per la saldatura laser di scocche di autoveicoli |
| FR2661758B1 (fr) | 1990-05-04 | 1992-11-27 | Aerospatiale | Procede et systeme pour la realisation d'une surface de reference plane, definie par une equation determinee, sur un bati d'assemblage d'une structure, a partir d'une surface brute. |
| US5142118A (en) * | 1991-05-14 | 1992-08-25 | Progressive Tool & Industries Co. | Laser welding unit |
| US5380978A (en) * | 1991-07-12 | 1995-01-10 | Pryor; Timothy R. | Method and apparatus for assembly of car bodies and other 3-dimensional objects |
| US5388318A (en) * | 1992-10-09 | 1995-02-14 | Laharco, Inc. | Method for defining a template for assembling a structure |
| US5560102A (en) | 1992-10-13 | 1996-10-01 | The Boeing Company | Panel and fuselage assembly |
| GB2276600B (en) | 1993-04-01 | 1996-07-31 | British Aerospace | Manufacture of aircraft wings |
| US5910894A (en) * | 1994-01-11 | 1999-06-08 | Sensor Adaptive Machines, Inc. | Sensor based assembly tooling improvements |
| US5427300A (en) * | 1994-03-22 | 1995-06-27 | Progressive Tool & Industries Co. | Apparatus for framing vehicle bodies |
| US5530549A (en) | 1994-05-24 | 1996-06-25 | Spatialmetrix Corp. | Probing retroreflector and methods of measuring surfaces therewith |
| US6314630B1 (en) | 1996-03-22 | 2001-11-13 | The Boeing Company | Determinant wing assembly |
| US5861956A (en) | 1997-05-27 | 1999-01-19 | Spatialmetrix Corporation | Retroreflector for use with tooling ball |
| US6230382B1 (en) * | 1998-05-11 | 2001-05-15 | Vought Aircraft Industries, Inc. | System and method for assembling an aircraft |
| US6510357B1 (en) * | 2000-02-25 | 2003-01-21 | Daimlerchrysler Corporation | Automated welding program for full body-in-white finite element assembly |
-
2000
- 2000-04-06 GB GBGB0008302.2A patent/GB0008302D0/en not_active Ceased
-
2001
- 2001-04-06 ES ES01917337T patent/ES2203598T3/es not_active Expired - Lifetime
- 2001-04-06 WO PCT/GB2001/001581 patent/WO2001076943A1/en not_active Ceased
- 2001-04-06 AT AT01917337T patent/ATE251571T1/de not_active IP Right Cessation
- 2001-04-06 AU AU4441701A patent/AU4441701A/xx active Pending
- 2001-04-06 JP JP2001574431A patent/JP3523237B2/ja not_active Expired - Fee Related
- 2001-04-06 AU AU2001244417A patent/AU2001244417B2/en not_active Expired - Fee Related
- 2001-04-06 US US10/089,891 patent/US6892160B2/en not_active Expired - Lifetime
- 2001-04-06 DE DE60100945T patent/DE60100945T2/de not_active Expired - Lifetime
- 2001-04-06 EP EP01917337A patent/EP1268276B1/de not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| JP3523237B2 (ja) | 2004-04-26 |
| EP1268276A1 (de) | 2003-01-02 |
| DE60100945D1 (de) | 2003-11-13 |
| EP1268276B1 (de) | 2003-10-08 |
| ES2203598T3 (es) | 2004-04-16 |
| US20030167147A1 (en) | 2003-09-04 |
| JP2003530232A (ja) | 2003-10-14 |
| US6892160B2 (en) | 2005-05-10 |
| WO2001076943A1 (en) | 2001-10-18 |
| GB0008302D0 (en) | 2000-05-24 |
| AU2001244417B2 (en) | 2005-09-08 |
| DE60100945T2 (de) | 2004-05-19 |
| AU4441701A (en) | 2001-10-23 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |