DE602007013173D1 - Verfahren und Vorrichtung zur Herstellung eines Tragflächenholmprofilelements - Google Patents
Verfahren und Vorrichtung zur Herstellung eines TragflächenholmprofilelementsInfo
- Publication number
- DE602007013173D1 DE602007013173D1 DE602007013173T DE602007013173T DE602007013173D1 DE 602007013173 D1 DE602007013173 D1 DE 602007013173D1 DE 602007013173 T DE602007013173 T DE 602007013173T DE 602007013173 T DE602007013173 T DE 602007013173T DE 602007013173 D1 DE602007013173 D1 DE 602007013173D1
- Authority
- DE
- Germany
- Prior art keywords
- protrusion
- profile element
- producing
- wing spar
- flange portion
- 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.)
- Active
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
- B29C70/34—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
- B29C70/342—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation using isostatic pressure
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
- B29C70/38—Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
- B29C70/386—Automated tape laying [ATL]
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
- B29D99/00—Subject matter not provided for in other groups of this subclass
- B29D99/0003—Producing profiled members, e.g. beams
- B29D99/0007—Producing profiled members, e.g. beams having a variable cross-section
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
- B29C70/38—Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
- B29L2031/3076—Aircrafts
- B29L2031/3085—Wings
-
- 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
- Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
- Y10T156/10—Methods of surface bonding and/or assembly therefor
- Y10T156/1002—Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina
- Y10T156/1007—Running or continuous length work
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Robotics (AREA)
- Moulding By Coating Moulds (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Extrusion Moulding Of Plastics Or The Like (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP07100884A EP1946913B1 (de) | 2007-01-22 | 2007-01-22 | Verfahren und Vorrichtung zur Herstellung eines Tragflächenholmprofilelements |
Publications (1)
Publication Number | Publication Date |
---|---|
DE602007013173D1 true DE602007013173D1 (de) | 2011-04-28 |
Family
ID=38169656
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE602007013173T Active DE602007013173D1 (de) | 2007-01-22 | 2007-01-22 | Verfahren und Vorrichtung zur Herstellung eines Tragflächenholmprofilelements |
Country Status (5)
Country | Link |
---|---|
US (1) | US20090025865A1 (de) |
EP (1) | EP1946913B1 (de) |
AT (1) | ATE501835T1 (de) |
DE (1) | DE602007013173D1 (de) |
ES (1) | ES2359090T3 (de) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB0906157D0 (en) * | 2009-04-09 | 2009-05-20 | Airbus Uk Ltd | Improved wing structure |
US8763153B2 (en) * | 2011-05-10 | 2014-06-24 | Microsoft Corporation | Presenting messages associated with locations |
US10105940B2 (en) * | 2016-04-18 | 2018-10-23 | The Boeing Company | Formation of composite laminates having one or more divergent flanges |
ES2800182T3 (es) * | 2017-07-13 | 2020-12-28 | Airbus Operations Sl | Disposición estructural de caja para una aeronave y procedimiento de fabricación de la misma |
WO2019178072A1 (en) * | 2018-03-12 | 2019-09-19 | Cytec Industries Inc. | Fabrication of three-dimensional composite structures |
US10682821B2 (en) * | 2018-05-01 | 2020-06-16 | Divergent Technologies, Inc. | Flexible tooling system and method for manufacturing of composite structures |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4351688A (en) * | 1979-12-10 | 1982-09-28 | General Dynamics Corporation | Composite tape laying machine |
US4451528A (en) * | 1981-03-30 | 1984-05-29 | Ni Industries, Inc. | Composite fiber reinforced member and method |
US4475976A (en) * | 1983-12-23 | 1984-10-09 | The Boeing Company | Method and apparatus for forming composite material articles |
US5242523A (en) * | 1992-05-14 | 1993-09-07 | The Boeing Company | Caul and method for bonding and curing intricate composite structures |
US5753164A (en) * | 1995-08-30 | 1998-05-19 | The Budd Company | Automated thermoset molding method |
JPH10258463A (ja) * | 1997-03-19 | 1998-09-29 | Fuji Heavy Ind Ltd | 複合材の小骨およびその成形方法 |
GB9828368D0 (en) | 1998-12-22 | 1999-02-17 | British Aerospace | Forming reinforcing components |
ES2205961B2 (es) * | 2001-02-13 | 2005-03-01 | Eads Construcciones Aeronauticas, S.A. | Procedimiento de fabricacion de elementos de material compuesto mediante la tecnoclogia del coencolado. |
US6758439B2 (en) * | 2002-10-22 | 2004-07-06 | The Boeing Company | Apparatuses and methods for attaching engine nacelles to aircraft |
US7534387B2 (en) * | 2004-02-25 | 2009-05-19 | The Boeing Company | Apparatus and methods for processing composite components using an elastomeric caul |
JP2006312260A (ja) * | 2005-05-09 | 2006-11-16 | Fuji Heavy Ind Ltd | プリプレグの折曲成形装置及びその折曲成形方法 |
EP1731291B1 (de) * | 2005-06-08 | 2008-09-24 | Saab Ab | Automatische Bandeauflegevorrichtung und Verfahren unter Verwendung dieser Vorrichtung |
-
2007
- 2007-01-22 DE DE602007013173T patent/DE602007013173D1/de active Active
- 2007-01-22 AT AT07100884T patent/ATE501835T1/de not_active IP Right Cessation
- 2007-01-22 EP EP07100884A patent/EP1946913B1/de active Active
- 2007-01-22 ES ES07100884T patent/ES2359090T3/es active Active
-
2008
- 2008-01-22 US US12/010,180 patent/US20090025865A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
US20090025865A1 (en) | 2009-01-29 |
ES2359090T3 (es) | 2011-05-18 |
ATE501835T1 (de) | 2011-04-15 |
EP1946913A1 (de) | 2008-07-23 |
EP1946913B1 (de) | 2011-03-16 |
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