CN102356016B - 在运输工具制造中利用粘接技术接合大面积的部件的方法和装置 - Google Patents
在运输工具制造中利用粘接技术接合大面积的部件的方法和装置 Download PDFInfo
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- CN102356016B CN102356016B CN2010800124381A CN201080012438A CN102356016B CN 102356016 B CN102356016 B CN 102356016B CN 2010800124381 A CN2010800124381 A CN 2010800124381A CN 201080012438 A CN201080012438 A CN 201080012438A CN 102356016 B CN102356016 B CN 102356016B
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- 238000000034 method Methods 0.000 title claims abstract description 41
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- 238000005516 engineering process Methods 0.000 claims description 19
- 238000004519 manufacturing process Methods 0.000 claims description 15
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- 238000005259 measurement Methods 0.000 abstract 2
- 208000034189 Sclerosis Diseases 0.000 description 4
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- 241000167854 Bourreria succulenta Species 0.000 description 2
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- 239000011248 coating agent Substances 0.000 description 1
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Images
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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05C—APPARATUS FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05C11/00—Component parts, details or accessories not specifically provided for in groups B05C1/00 - B05C9/00
- B05C11/10—Storage, supply or control of liquid or other fluent material; Recovery of excess liquid or other fluent material
- B05C11/1002—Means for controlling supply, i.e. flow or pressure, of liquid or other fluent material to the applying apparatus, e.g. valves
- B05C11/1015—Means for controlling supply, i.e. flow or pressure, of liquid or other fluent material to the applying apparatus, e.g. valves responsive to a conditions of ambient medium or target, e.g. humidity, temperature ; responsive to position or movement of the coating head relative to the target
- B05C11/1021—Means for controlling supply, i.e. flow or pressure, of liquid or other fluent material to the applying apparatus, e.g. valves responsive to a conditions of ambient medium or target, e.g. humidity, temperature ; responsive to position or movement of the coating head relative to the target responsive to presence or shape of target
-
- 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
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/068—Fuselage sections
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05C—APPARATUS FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05C13/00—Means for manipulating or holding work, e.g. for separate articles
- B05C13/02—Means for manipulating or holding work, e.g. for separate articles for particular articles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05C—APPARATUS FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05C5/00—Apparatus in which liquid or other fluent material is projected, poured or allowed to flow on to the surface of the work
- B05C5/02—Apparatus in which liquid or other fluent material is projected, poured or allowed to flow on to the surface of the work the liquid or other fluent material being discharged through an outlet orifice by pressure, e.g. from an outlet device in contact or almost in contact, with the work
- B05C5/0208—Apparatus in which liquid or other fluent material is projected, poured or allowed to flow on to the surface of the work the liquid or other fluent material being discharged through an outlet orifice by pressure, e.g. from an outlet device in contact or almost in contact, with the work for applying liquid or other fluent material to separate articles
- B05C5/0212—Apparatus in which liquid or other fluent material is projected, poured or allowed to flow on to the surface of the work the liquid or other fluent material being discharged through an outlet orifice by pressure, e.g. from an outlet device in contact or almost in contact, with the work for applying liquid or other fluent material to separate articles only at particular parts of the articles
- B05C5/0216—Apparatus in which liquid or other fluent material is projected, poured or allowed to flow on to the surface of the work the liquid or other fluent material being discharged through an outlet orifice by pressure, e.g. from an outlet device in contact or almost in contact, with the work for applying liquid or other fluent material to separate articles only at particular parts of the articles by relative movement of article and outlet according to a predetermined path
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
- B62D—MOTOR VEHICLES; TRAILERS
- B62D27/00—Connections between superstructure or understructure sub-units
- B62D27/02—Connections between superstructure or understructure sub-units rigid
- B62D27/026—Connections by glue bonding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
- B62D—MOTOR VEHICLES; TRAILERS
- B62D65/00—Designing, manufacturing, e.g. assembling, facilitating disassembly, or structurally modifying motor vehicles or trailers, not otherwise provided for
- B62D65/02—Joining sub-units or components to, or positioning sub-units or components with respect to, body shell or other sub-units or components
- B62D65/024—Positioning of sub-units or components with respect to body shell or other sub-units or components
- B62D65/028—Positioning of sub-units or components with respect to body shell or other sub-units or components by determining relative positions by measurement
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Mechanical Engineering (AREA)
- Transportation (AREA)
- Adhesives Or Adhesive Processes (AREA)
- Lining Or Joining Of Plastics Or The Like (AREA)
- Automatic Assembly (AREA)
- Standing Axle, Rod, Or Tube Structures Coupled By Welding, Adhesion, Or Deposition (AREA)
Abstract
Description
Claims (13)
Applications Claiming Priority (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102009013540 | 2009-03-19 | ||
DE102009013540.5 | 2009-03-19 | ||
DE102010010686A DE102010010686A1 (de) | 2009-03-19 | 2010-03-08 | Verfahren und Vorrichtung zum klebtechnischen Fügen großflächiger Komponenten im Fahrzeugbau |
DE102010010686.0 | 2010-03-08 | ||
PCT/EP2010/053523 WO2010106129A1 (de) | 2009-03-19 | 2010-03-18 | Verfahren und vorrichtung zum klebtechnischen fügen grossflächiger komponenten im fahrzeugbau |
Publications (2)
Publication Number | Publication Date |
---|---|
CN102356016A CN102356016A (zh) | 2012-02-15 |
CN102356016B true CN102356016B (zh) | 2013-10-09 |
Family
ID=42126200
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN2010800124381A Expired - Fee Related CN102356016B (zh) | 2009-03-19 | 2010-03-18 | 在运输工具制造中利用粘接技术接合大面积的部件的方法和装置 |
Country Status (9)
Country | Link |
---|---|
US (1) | US8968500B2 (zh) |
EP (1) | EP2408656B1 (zh) |
JP (1) | JP2012520208A (zh) |
CN (1) | CN102356016B (zh) |
BR (1) | BRPI1009126A2 (zh) |
CA (1) | CA2754699A1 (zh) |
DE (1) | DE102010010686A1 (zh) |
RU (1) | RU2483989C1 (zh) |
WO (1) | WO2010106129A1 (zh) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102010010686A1 (de) | 2009-03-19 | 2011-01-05 | Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. | Verfahren und Vorrichtung zum klebtechnischen Fügen großflächiger Komponenten im Fahrzeugbau |
DE102010010685A1 (de) | 2009-03-19 | 2011-02-03 | Airbus Operations Gmbh | Verfahren zur toleranzangepassten Klebstoffapplikation im Fahrzeugbau |
CN102556366B (zh) * | 2012-02-18 | 2014-07-23 | 沈阳飞机工业(集团)有限公司 | 用于飞机部件对接的定位器底面支撑装置 |
US10046865B2 (en) * | 2013-05-09 | 2018-08-14 | The Boeing Company | Apparatus and method for installation of a frame assembly to a body |
DE202014101000U1 (de) * | 2014-03-06 | 2015-06-12 | Kuka Systems Gmbh | Fügewerkzeug und Fügeeinrichtung |
US10518483B2 (en) * | 2017-01-25 | 2019-12-31 | The Boeing Company | Compound shimming |
EP3543814A1 (de) * | 2018-03-21 | 2019-09-25 | balti ag | Verfahren zur herstellung von verbundwerkstücken, anlage und fügevorrichtung |
US11433990B2 (en) * | 2018-07-09 | 2022-09-06 | Rohr, Inc. | Active laminar flow control system with composite panel |
CN112246560B (zh) * | 2020-09-26 | 2021-08-10 | 马鞍山贺辉信息科技有限公司 | 一种用于汽车中控盒装配的涂胶压扣设备及其工作方法 |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5738749A (en) * | 1993-05-27 | 1998-04-14 | Cincinnati Milacron Inc. | Method of using a variable force compactor |
US6017484A (en) * | 1997-01-21 | 2000-01-25 | Harold P. Hale | Method for manufacture of minimum porosity, wrinkle free composite parts |
CN1826451A (zh) * | 2003-02-24 | 2006-08-30 | 贝尔直升机泰克斯特龙公司 | 用于结构蒙皮的接触加强件 |
CN101272956A (zh) * | 2005-09-22 | 2008-09-24 | 空中客车英国有限公司 | 飞行器部件的组装 |
Family Cites Families (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SU137015A1 (ru) * | 1960-05-31 | 1960-11-30 | А.Д. Аничкин | Способ прессовани изделий с клееной слоистой оболочкой и упругим заполнителем |
JPS58187479A (ja) * | 1982-04-27 | 1983-11-01 | Honda Motor Co Ltd | 可撓シ−ル材の外被材貼付方法 |
GB9825880D0 (en) | 1998-11-27 | 1999-01-20 | Rover Group | Adhesive dispensing method |
GB9926579D0 (en) | 1999-11-11 | 2000-01-12 | British Aerospace | Reinforcement of a laminated member for an aircraft |
DE10319926B4 (de) * | 2003-05-02 | 2006-09-28 | Airbus Deutschland Gmbh | Verfahren zum Ausgleichen eines Fügespaltes |
US7282107B2 (en) | 2003-08-22 | 2007-10-16 | The Boeing Company | Multiple head automated composite laminating machine for the fabrication of large barrel section components |
US7527222B2 (en) * | 2004-04-06 | 2009-05-05 | The Boeing Company | Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections |
EP1755997B1 (en) * | 2004-04-21 | 2014-11-26 | Ingersoll Machine Tools, Inc. | Automated fiber placement using multiple placement heads, replaceable creels, and replaceable placement heads |
US8515424B2 (en) | 2004-06-01 | 2013-08-20 | Qualcomm Incorporated | Connected-state radio session transfer in wireless communication systems |
US7503368B2 (en) * | 2004-11-24 | 2009-03-17 | The Boeing Company | Composite sections for aircraft fuselages and other structures, and methods and systems for manufacturing such sections |
US7410352B2 (en) * | 2005-04-13 | 2008-08-12 | The Boeing Company | Multi-ring system for fuselage barrel formation |
US20070034197A1 (en) | 2005-08-15 | 2007-02-15 | Tschech Steven E | Rapid-firing projectile launcher |
NL1030066C2 (nl) * | 2005-09-29 | 2007-03-30 | Gtm Consulting B V | Werkwijze voor het vervaardigen van een vormdeel uit een samengesteld materiaal. |
US7955548B2 (en) | 2006-04-13 | 2011-06-07 | American Gfm Corporation | Method for making three-dimensional preforms using electroluminescent devices |
JP4327839B2 (ja) | 2006-12-13 | 2009-09-09 | 本田技研工業株式会社 | アルミニウム合金製主翼の組立方法 |
FR2912680B1 (fr) * | 2007-02-21 | 2009-04-24 | Coriolis Composites Sa | Procede et dispositif de fabrication de pieces en materiau composite, en particulier de troncons de fuselage d'avion |
RU2329183C1 (ru) * | 2007-05-18 | 2008-07-20 | Общество с ограниченной ответственностью "Самара ВВВ-Авиа" | Способ сборки консоли крыла самолета |
US9034128B2 (en) | 2007-12-17 | 2015-05-19 | The Boeing Company | Fitting doublers using gap mapping |
DE102007061429B4 (de) | 2007-12-20 | 2014-08-21 | Airbus Operations Gmbh | Rumpfstruktur |
EP2334932B2 (en) | 2008-08-25 | 2024-05-01 | Vestas Wind Systems A/S | Assembly and method of preparing an assembly |
DE102010010686A1 (de) | 2009-03-19 | 2011-01-05 | Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. | Verfahren und Vorrichtung zum klebtechnischen Fügen großflächiger Komponenten im Fahrzeugbau |
DE102010010685A1 (de) | 2009-03-19 | 2011-02-03 | Airbus Operations Gmbh | Verfahren zur toleranzangepassten Klebstoffapplikation im Fahrzeugbau |
US8758538B2 (en) | 2010-05-12 | 2014-06-24 | Fives Machining Systems, Inc. | Robotic based fiber placement cell with stationary dispensing head and creel |
-
2010
- 2010-03-08 DE DE102010010686A patent/DE102010010686A1/de not_active Ceased
- 2010-03-18 CA CA2754699A patent/CA2754699A1/en not_active Abandoned
- 2010-03-18 JP JP2012500252A patent/JP2012520208A/ja active Pending
- 2010-03-18 RU RU2011139569/11A patent/RU2483989C1/ru not_active IP Right Cessation
- 2010-03-18 CN CN2010800124381A patent/CN102356016B/zh not_active Expired - Fee Related
- 2010-03-18 WO PCT/EP2010/053523 patent/WO2010106129A1/de active Application Filing
- 2010-03-18 EP EP10709522.6A patent/EP2408656B1/de active Active
- 2010-03-18 BR BRPI1009126A patent/BRPI1009126A2/pt not_active IP Right Cessation
-
2011
- 2011-08-30 US US13/221,279 patent/US8968500B2/en not_active Expired - Fee Related
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5738749A (en) * | 1993-05-27 | 1998-04-14 | Cincinnati Milacron Inc. | Method of using a variable force compactor |
US6017484A (en) * | 1997-01-21 | 2000-01-25 | Harold P. Hale | Method for manufacture of minimum porosity, wrinkle free composite parts |
CN1826451A (zh) * | 2003-02-24 | 2006-08-30 | 贝尔直升机泰克斯特龙公司 | 用于结构蒙皮的接触加强件 |
CN101272956A (zh) * | 2005-09-22 | 2008-09-24 | 空中客车英国有限公司 | 飞行器部件的组装 |
Also Published As
Publication number | Publication date |
---|---|
EP2408656B1 (de) | 2016-08-24 |
US20120043008A1 (en) | 2012-02-23 |
WO2010106129A1 (de) | 2010-09-23 |
RU2011139569A (ru) | 2013-04-27 |
JP2012520208A (ja) | 2012-09-06 |
DE102010010686A1 (de) | 2011-01-05 |
BRPI1009126A2 (pt) | 2016-03-01 |
CN102356016A (zh) | 2012-02-15 |
CA2754699A1 (en) | 2010-09-23 |
US8968500B2 (en) | 2015-03-03 |
EP2408656A1 (de) | 2012-01-25 |
RU2483989C1 (ru) | 2013-06-10 |
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SE01 | Entry into force of request for substantive examination | ||
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GR01 | Patent grant | ||
ASS | Succession or assignment of patent right |
Free format text: FORMER OWNER: AIRBUS GMBH (DE) Effective date: 20150211 Owner name: AIRBUS GMBH (DE) Free format text: FORMER OWNER: FRAUNHOFER-GESELLSCHAFT ZUR FORDERUNG DER ANGEWANDTEN FORSCHUNG E.V. Effective date: 20150211 |
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C41 | Transfer of patent application or patent right or utility model | ||
TR01 | Transfer of patent right |
Effective date of registration: 20150211 Address after: hamburg Patentee after: Airbus GMBH (DE) Address before: Munich, Germany Patentee before: Fraunhofer Application and Research Promotion Association Patentee before: Airbus GMBH (DE) |
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Granted publication date: 20131009 Termination date: 20170318 |