ES2194645T3 - Procedimiento y dispositivo para fabricar un componente tridimensional de grandes dimensiones. - Google Patents
Procedimiento y dispositivo para fabricar un componente tridimensional de grandes dimensiones.Info
- Publication number
- ES2194645T3 ES2194645T3 ES00111628T ES00111628T ES2194645T3 ES 2194645 T3 ES2194645 T3 ES 2194645T3 ES 00111628 T ES00111628 T ES 00111628T ES 00111628 T ES00111628 T ES 00111628T ES 2194645 T3 ES2194645 T3 ES 2194645T3
- Authority
- ES
- Spain
- Prior art keywords
- component
- partial section
- dimensional
- hull
- support
- 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 - Lifetime
Links
- 238000004519 manufacturing process Methods 0.000 title abstract 3
- 238000000034 method Methods 0.000 title abstract 2
Classifications
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- 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
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
- B21J15/00—Riveting
- B21J15/10—Riveting machines
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
- B21J15/00—Riveting
- B21J15/10—Riveting machines
- B21J15/14—Riveting machines specially adapted for riveting specific articles, e.g. brake lining machines
- B21J15/142—Aerospace structures
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- 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
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- 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
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- 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
- B64C2001/0018—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like comprising two decks adapted for carrying passengers only
- B64C2001/0027—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like comprising two decks adapted for carrying passengers only arranged one above the other
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- 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
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- 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
- Y10T29/49764—Method of mechanical manufacture with testing or indicating
- Y10T29/49778—Method of mechanical manufacture with testing or indicating with aligning, guiding, or instruction
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- 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
- Y10T29/49764—Method of mechanical manufacture with testing or indicating
- Y10T29/49778—Method of mechanical manufacture with testing or indicating with aligning, guiding, or instruction
- Y10T29/4978—Assisting assembly or disassembly
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- 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
- Y10T29/4981—Utilizing transitory attached element or associated separate material
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- 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
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- 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"]
- Y10T29/49901—Sequentially associating parts on stationary aligning means
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- 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
- Y10T29/49904—Assembling a subassembly, then assembling with a second subassembly
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- 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
- Y10T29/49998—Work holding
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- 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
- Y10T29/51—Plural diverse manufacturing apparatus including means for metal shaping or assembling
- Y10T29/5176—Plural diverse manufacturing apparatus including means for metal shaping or assembling including machining means
- Y10T29/5177—Plural diverse manufacturing apparatus including means for metal shaping or assembling including machining means and work-holder for assembly
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- 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
- Y10T29/53004—Means to assemble or disassemble with means to regulate operation by use of templet, tape, card or other replaceable information supply
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- 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
- Y10T29/53039—Means to assemble or disassemble with control means energized in response to activator stimulated by condition sensor
- Y10T29/53061—Responsive to work or work-related machine element
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- 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
- Y10T29/53087—Means to assemble or disassemble with signal, scale, illuminator, or optical viewer
- Y10T29/53091—Means to assemble or disassemble with signal, scale, illuminator, or optical viewer for work-holder for assembly or disassembly
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- 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
- Y10T29/53313—Means to interrelatedly feed plural work parts from plural sources without manual intervention
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- 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
- Y10T29/53909—Means comprising hand manipulatable tool
- Y10T29/53943—Hand gripper for direct push or pull
- Y10T29/53952—Tube sleeve or ferrule applying or removing
- Y10T29/53957—Thread-tapping grip
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- 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
- Y10T29/53961—Means to assemble or disassemble with work-holder for assembly
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Transportation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Automatic Assembly (AREA)
- Moulding By Coating Moulds (AREA)
Abstract
Procedimiento para la fabricación de un componente tridimensional de grandes dimensiones, especialmente un fuselaje de avión configurado de forma de tonel de un avión (14) de gran capacidad, enel que el componente de grandes dimensiones está compuesto de componentes (4, 5, 8, 10) unidos, en forma de casco y preferiblemente reforzados mediante elementos que soportan cargas, como largueros y cuadernas, y en su espacio interior presenta una o varias rejillas (2, 3) de suelo en forma de planchas, que se extienden en la dirección longitudinal del componente de grandes dimensiones, así como desde una de sus paredes laterales a la pared lateral opuesta, utilizándose una rejilla (2, 3) de suelo que actúa conjuntamente con un soporte (1) central como punto de partida para el montaje de los componentes (4, 5, 8, 10), y con lo que el componente tridimensional de grandes dimensiones, al que se hace referencia como a una sección, se compone de como mínimo dos secciones parciales alineadas una junto a laotra con costuras transversales, caracterizado porque para la fabricación de la primera sección parcial: - se sujeta mecánicamente de forma fija con ayuda de elementos tensores, como mínimo una rejilla (2, 3) de suelo en la superficie de un soporte (1) central longitudinal y colocado con sus extremos frontales, y - los componentes (4, 5, 8, 10) en forma de casco que presentan una rigidez propia definida se posicionan unos detrás de los otros alrededor del soporte (1) central por medio de un sistema (6, 7, 9) portador controlado por ordenador y a continuación se unen de forma mecánica, de tal manera que primero se unen mecánicamente los cascos (4, 5) laterales opuestos entre sí con la o las rejilla/s (2, 3) del suelo, y luego el casco (8) inferior o el casco (10) superior se unen uno detrás del otro a los cascos (4, 5) laterales, y porque, por medio de costuras transversales, se une a la primera sección parcial terminada una segunda sección parcial fabricada de la misma manera, y a esta segunda sección parcial, en casos dados, otras secciones parciales contiguas fabricadas de la misma manera hasta que se termina el componente (14) de grandes dimensiones.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE19929471A DE19929471C1 (de) | 1999-06-26 | 1999-06-26 | Verfahren und Vorrichtung zur Herstellung eines dreidimensionalen Großbauteiles |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ES2194645T3 true ES2194645T3 (es) | 2003-12-01 |
Family
ID=7912756
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| ES00111628T Expired - Lifetime ES2194645T3 (es) | 1999-06-26 | 2000-05-31 | Procedimiento y dispositivo para fabricar un componente tridimensional de grandes dimensiones. |
Country Status (4)
| Country | Link |
|---|---|
| US (2) | US6408517B1 (es) |
| EP (1) | EP1063166B1 (es) |
| DE (2) | DE19929471C1 (es) |
| ES (1) | ES2194645T3 (es) |
Families Citing this family (71)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2821778B1 (fr) * | 2001-03-07 | 2004-11-19 | S O C O A Soc De Conception Co | Procede d'assemblage automatisee de structures volumineuses notamment aeronautiques, dispositifs et produit logiciel permettant de le mettre en oeuvre |
| US6691392B2 (en) * | 2001-05-16 | 2004-02-17 | Utica Enterprises, Inc. | Method and apparatus for assembling exterior automotive vehicle body components onto an automotive vehicle body |
| DE10146442B4 (de) * | 2001-09-20 | 2005-01-27 | Thyssenkrupp Automotive Ag | Vorrichtung zum Verbindung von zwei oder mehr Bauteilen mittels Nieten |
| FR2863673B1 (fr) * | 2003-12-10 | 2006-03-10 | Airbus France | Dispositif d'assemblage par rivetage de plusieurs elements et procede d'assemblage de panneaux notamment de fuselage d'aeronef a l'aide dudit dispositif |
| US20060010689A1 (en) * | 2004-07-14 | 2006-01-19 | Ali Salour | Automated drill process for two-diameter holes in multi-layer variable thickness composite materials |
| FR2877916B1 (fr) * | 2004-11-15 | 2008-04-25 | Airbus France Sas | Cadre de structure de fuselage d'aeronef |
| DE102004056287A1 (de) * | 2004-11-22 | 2006-05-24 | Airbus Deutschland Gmbh | Vorrichtung und Verfahren zur Fertigung von Sektionen für Verkehrsmittel, insbesondere für Luftfahrzeuge |
| DE102004056286B4 (de) * | 2004-11-22 | 2015-12-24 | Airbus Operations Gmbh | Vorrichtung und Verfahren zum form- und/oder abmessungsunabhängigen Zusammenfügen und Heften von mehreren Einzelkomponenten zur Bildung von eigensteifen, transportfähigen Sektionen für Verkehrsmittel, insbesondere für Luftfahrzeuge |
| US20060185143A1 (en) * | 2004-11-22 | 2006-08-24 | Airbus Deutschland Gmbh | Method and device for manufacturing sections for transportation systems |
| DE102004056285B4 (de) * | 2004-11-22 | 2010-08-26 | Airbus Deutschland Gmbh | Vorrichtung mit mindestens zwei Knickarmrobotern zur form- und/oder abmessungsunabhängigen Verbindung von Einzelkomponenten zur Bildung von Sektionen für Luftfahrzeuge |
| DE102004056284B4 (de) * | 2004-11-22 | 2010-08-26 | Airbus Deutschland Gmbh | Vorrichtung zum Transport von Bauteilen für Verkehrsmittel |
| US7850374B2 (en) * | 2005-01-14 | 2010-12-14 | Avago Technologies Fiber Ip (Singapore) Pte. Ltd. | Optical transmitter module with an integrated lens and method for making the module |
| US20060277751A1 (en) * | 2005-05-09 | 2006-12-14 | The Boeing Company | Rotating internal support apparatus and method for large hollow structures |
| US7596843B2 (en) * | 2005-06-16 | 2009-10-06 | The Boeing Company | Rotating internal support apparatus and method for large hollow structures |
| US7926694B2 (en) * | 2005-10-14 | 2011-04-19 | Enrique Franco | Apparatus for vertically manufacturing poles and columns |
| DE102005054869A1 (de) * | 2005-11-17 | 2007-05-31 | Airbus Deutschland Gmbh | Verfahren zur Herstellung einer Rumpfzelle eines Luftfahrzeugs |
| DE102006015642B4 (de) * | 2006-03-29 | 2009-12-31 | Ima Materialforschung Und Anwendungstechnik Gmbh | Prüfvorrichtung für Rumpfschalen |
| DE102006025930B4 (de) * | 2006-06-02 | 2008-09-11 | Airbus Deutschland Gmbh | Rumpfstruktur und Verfahren zur Herstellung einer Rumpfstruktur |
| JP4954283B2 (ja) | 2006-06-28 | 2012-06-13 | エアバス オペレーションズ ゲーエムベーハー | 航空機胴体の組立構造 |
| DE102006060360B8 (de) * | 2006-12-20 | 2010-09-30 | Airbus Deutschland Gmbh | Rumpfsektion zur Bildung einer Rumpfzelle eines Flugzeugs |
| US7849729B2 (en) * | 2006-12-22 | 2010-12-14 | The Boeing Company | Leak detection in vacuum bags |
| CN100491202C (zh) * | 2007-04-12 | 2009-05-27 | 沈阳飞机工业(集团)有限公司 | 数字化装配有空间复合角度定位器工装的方法 |
| US9770871B2 (en) | 2007-05-22 | 2017-09-26 | The Boeing Company | Method and apparatus for layup placement |
| US8568551B2 (en) * | 2007-05-22 | 2013-10-29 | The Boeing Company | Pre-patterned layup kit and method of manufacture |
| DE102007028918A1 (de) * | 2007-06-22 | 2009-01-02 | Airbus Deutschland Gmbh | Verfahren zur Herstellung einer Rumpfzelle eines Flugzeugs sowie Vorrichtung |
| US8936695B2 (en) | 2007-07-28 | 2015-01-20 | The Boeing Company | Method for forming and applying composite layups having complex geometries |
| US8333864B2 (en) | 2008-09-30 | 2012-12-18 | The Boeing Company | Compaction of prepreg plies on composite laminate structures |
| US8707766B2 (en) | 2010-04-21 | 2014-04-29 | The Boeing Company | Leak detection in vacuum bags |
| DE102007044387B4 (de) * | 2007-09-18 | 2010-07-15 | Airbus Deutschland Gmbh | Verfahren zur Herstellung einer Rumpfzelle eines Flugzeugs |
| US8916010B2 (en) | 2007-12-07 | 2014-12-23 | The Boeing Company | Composite manufacturing method |
| US8752293B2 (en) | 2007-12-07 | 2014-06-17 | The Boeing Company | Method of fabricating structures using composite modules and structures made thereby |
| DE102008044262B4 (de) | 2008-12-02 | 2019-12-12 | Airbus Operations Gmbh | Vorrichtung und Verfahren zum Eintakten von Strukturbauteilen in einen Bauplatz |
| US8468674B2 (en) * | 2008-12-02 | 2013-06-25 | Airbus Operations Gmbh | Device and method for supplying structural components to an assembly zone |
| ES2376098B1 (es) * | 2009-07-24 | 2013-02-04 | Airbus Operations S.L. | Procedimiento de ensamblaje de secciones de fuselaje de una aeronave. |
| DE102011005632B4 (de) * | 2011-03-16 | 2013-09-19 | Siemens Aktiengesellschaft | Aufbaustand zum Zusammenfügen von Wagenkasten-Baugruppen |
| US8914979B2 (en) * | 2011-07-21 | 2014-12-23 | Spirit AcroSystems, Inc. | System and method for assembling aircraft components |
| CN102950458A (zh) * | 2011-08-24 | 2013-03-06 | 上海福伊特水电设备有限公司 | 混流式转轮叶片三维空间定位装配工装 |
| US9090357B2 (en) * | 2011-12-15 | 2015-07-28 | The Boeing Company | Method of assembling panelized aircraft fuselages |
| CN102794728B (zh) * | 2012-08-22 | 2014-07-02 | 浙江大学 | 一种球头自适应入位锁紧装置及其方法 |
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| US9880694B2 (en) | 2013-05-09 | 2018-01-30 | The Boeing Company | Shop order status visualization system |
| US9612725B1 (en) | 2013-02-28 | 2017-04-04 | The Boeing Company | Nonconformance visualization system |
| US9292180B2 (en) | 2013-02-28 | 2016-03-22 | The Boeing Company | Locator system for three-dimensional visualization |
| US10067650B2 (en) | 2013-06-20 | 2018-09-04 | The Boeing Company | Aircraft comparison system with synchronized displays |
| US20140298216A1 (en) | 2013-03-28 | 2014-10-02 | The Boeing Company | Visualization of an Object Using a Visual Query System |
| US10416857B2 (en) | 2013-05-09 | 2019-09-17 | The Boeing Company | Serial number control visualization system |
| US9604319B2 (en) * | 2013-08-13 | 2017-03-28 | The Boeing Company | Method for processing curved sheets using magnetic clamping members |
| DE102013110684A1 (de) * | 2013-09-26 | 2015-03-26 | Airbus Operations Gmbh | Verfahren zum Montieren eines Flugzeugrumpfs und Rumpffertigungsstation |
| FR3020347B1 (fr) * | 2014-04-28 | 2016-05-20 | Airbus Operations Sas | Procede d'assemblage d'une partie arriere d'aeronef |
| US9937549B2 (en) | 2014-07-09 | 2018-04-10 | The Boeing Company | Two-stage riveting |
| US9555587B2 (en) * | 2014-08-13 | 2017-01-31 | The Boeing Company | Composite layup tools for aircraft fuselage barrels, methods of assembling the layup tools, and aircraft fuselage barrel sections formed utilizing the layup tools |
| EP2985232A1 (en) * | 2014-08-13 | 2016-02-17 | Airbus Operations GmbH | Method for assembling an aircraft fuselage |
| DE102014111747B4 (de) * | 2014-08-18 | 2021-11-04 | Airbus Operations Gmbh | Bearbeitungsvorrichtung zur Montage von Luftfahrzeugen |
| DE102014116560A1 (de) * | 2014-11-12 | 2016-05-12 | Airbus Operations Gmbh | Verfahren und Vorrichtung zum Befestigen eines Luftfahrzeug- oder Raumfahrzeug-Bauteils an einer Rumpfsektion eines Luftfahrzeugs oder Raumfahrzeugs |
| JP6523693B2 (ja) | 2015-01-28 | 2019-06-05 | 三菱重工業株式会社 | 航空機部品位置決め装置、航空機組立システム及び航空機組立方法 |
| FR3035075B1 (fr) * | 2015-04-20 | 2018-08-17 | Airbus Operations | Ensemble d'outillage pour l'integration d'une partie centrale d'aeronef, procede associe et aeronef ainsi integre |
| JP6563271B2 (ja) * | 2015-08-03 | 2019-08-21 | 三菱重工業株式会社 | 組立体製造装置及び組立体製造方法 |
| JP6629001B2 (ja) | 2015-08-03 | 2020-01-15 | 三菱重工業株式会社 | 組立体製造装置及び組立体製造方法 |
| CN105539876B (zh) * | 2015-12-14 | 2018-12-18 | 浙江日发航空数字装备有限责任公司 | 飞机装配用调姿球头装置 |
| 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 |
| US10685147B2 (en) | 2016-02-29 | 2020-06-16 | The Boeing Company | Non-conformance mapping and visualization |
| FR3072656B1 (fr) * | 2017-10-24 | 2019-11-08 | Airbus | Systeme d’outillage destine a la manipulation d’au moins un module superieur et /ou au moins un module inferieur. |
| FR3086268A1 (fr) * | 2018-09-25 | 2020-03-27 | Airbus Operations | Procede d’assemblage d’un troncon de fuselage d’aeronef a partir de deux parties superieure et inferieure superposees, support de montage polyvalent, outillage et unite de production de troncons de fuselage pour la mise en œuvre dudit procede |
| CN114056595B (zh) * | 2020-08-04 | 2024-01-23 | 上海飞机制造有限公司 | 数控定位器应力释放装置及对接调姿系统 |
| US11597044B2 (en) | 2020-11-18 | 2023-03-07 | The Boeing Company | Composite assembly for unhardened fuselage components |
| FR3138122A1 (fr) | 2022-07-25 | 2024-01-26 | Airbus Operations | Système de transport de grille de plancher de cabine d’aéronef en vue d’un assemblage d’un corps de fuselage d’aéronef et procédé de calibration dudit système de transport. |
| EP4311782B1 (fr) * | 2022-07-25 | 2025-10-29 | Airbus Operations SAS | Système de manipulation d'une coque latérale d'un aéronef en vue d'un assemblage d'un corps de fuselage de l'aéronef et procédé d'assemblage d'un corps de fuselage d'un aéronef |
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| US2117435A (en) * | 1937-05-20 | 1938-05-17 | Clifford B Langstroth | Machine for use in manufacturing boiler shells |
| US2370083A (en) * | 1942-04-13 | 1945-02-20 | Cons Aircraft Corp | Method of assembling airplane fuselages and the like |
| US2378043A (en) * | 1942-10-24 | 1945-06-12 | Ford Motor Co | Method of airframe assembly |
| US2374894A (en) * | 1943-06-16 | 1945-05-01 | Ford Motor Co | Method and apparatus for assembling aircraft fuselages |
| US2391510A (en) * | 1944-05-13 | 1945-12-25 | Ford Motor Co | Mating fixture |
| US2594586A (en) * | 1948-11-15 | 1952-04-29 | Edo Corp | Shipping container |
| US2928535A (en) * | 1953-07-14 | 1960-03-15 | Walter A Simmons | Shock-resisting support for storing and shipping engines and the like equipment containing destructible components |
| US3194525A (en) * | 1964-02-07 | 1965-07-13 | James E Webb | Supporting and protecting device |
| US3612484A (en) * | 1969-01-06 | 1971-10-12 | Nat Steel Erecting Corp | Apparatus for lifting and transporting disabled aircraft |
| US4259776A (en) * | 1978-08-09 | 1981-04-07 | Airships International Inc. | Method of assembly of airship hull |
| US4371108A (en) * | 1980-08-09 | 1983-02-01 | Stephen Roggendorff | Methods of manufacturing large tubular columns |
| US4462535A (en) * | 1981-04-23 | 1984-07-31 | Amca International Corporation | Apparatus and process for manufacture of tunnel tubes |
| SE447708B (sv) * | 1983-10-21 | 1986-12-08 | Atlas Copco Ab | Anordning for sammanfogning medelst nitning av tva eller flera sektioner ingaende i en konstruktion bestaende av skivformiga element |
| US5560102A (en) * | 1992-10-13 | 1996-10-01 | The Boeing Company | Panel and fuselage assembly |
| FR2702982B1 (fr) * | 1993-03-23 | 1995-06-30 | Aerospatiale | Dispositif de positionnement d'un support d'outils ou analogues sur la face externe d'une structure tubulaire, notamment un fuselage d'aeronef. |
| US5645389A (en) * | 1995-11-30 | 1997-07-08 | Stanley Aviation Corporation | Shipping frame from fan section of aircraft engine |
| US6230382B1 (en) * | 1998-05-11 | 2001-05-15 | Vought Aircraft Industries, Inc. | System and method for assembling an aircraft |
| US6170141B1 (en) * | 1998-09-25 | 2001-01-09 | Stanley Aviation Corporation | Shipping system for jet aircraft engine and method of installing and removing jet aircraft engine |
| ES2169620B1 (es) * | 1999-01-22 | 2003-11-01 | Torres Ingenieria De Procesos | Util para el montaje de secciones del fuselaje de aeronaves. |
-
1999
- 1999-06-26 DE DE19929471A patent/DE19929471C1/de not_active Expired - Fee Related
-
2000
- 2000-05-31 DE DE50001766T patent/DE50001766D1/de not_active Expired - Lifetime
- 2000-05-31 EP EP00111628A patent/EP1063166B1/de not_active Expired - Lifetime
- 2000-05-31 ES ES00111628T patent/ES2194645T3/es not_active Expired - Lifetime
- 2000-06-26 US US09/603,870 patent/US6408517B1/en not_active Expired - Lifetime
-
2001
- 2001-07-31 US US09/919,388 patent/US6481096B2/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| US20010054228A1 (en) | 2001-12-27 |
| US6408517B1 (en) | 2002-06-25 |
| DE19929471C1 (de) | 2001-01-18 |
| EP1063166B1 (de) | 2003-04-16 |
| DE50001766D1 (de) | 2003-05-22 |
| EP1063166A1 (de) | 2000-12-27 |
| US6481096B2 (en) | 2002-11-19 |
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