BRPI0821246A2 - Método e dispositivo para produção de componentes estruturais em formato de tubo - Google Patents
Método e dispositivo para produção de componentes estruturais em formato de tuboInfo
- Publication number
- BRPI0821246A2 BRPI0821246A2 BRPI0821246-5A BRPI0821246A BRPI0821246A2 BR PI0821246 A2 BRPI0821246 A2 BR PI0821246A2 BR PI0821246 A BRPI0821246 A BR PI0821246A BR PI0821246 A2 BRPI0821246 A2 BR PI0821246A2
- Authority
- BR
- Brazil
- Prior art keywords
- structural components
- shaped structural
- producing pipe
- producing
- pipe
- Prior art date
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
- B29C70/40—Shaping or impregnating by compression not applied
- B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
- B29C70/46—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
- B29C70/48—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs and impregnating the reinforcements in the closed mould, e.g. resin transfer moulding [RTM], e.g. by vacuum
-
- 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
- B29C33/00—Moulds or cores; Details thereof or accessories therefor
- B29C33/44—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles
- B29C33/48—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles with means for collapsing or disassembling
- B29C33/50—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles with means for collapsing or disassembling elastic or flexible
- B29C33/505—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles with means for collapsing or disassembling elastic or flexible cores or mandrels, e.g. inflatable
-
- 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
- B29C70/345—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 matched moulds
-
- 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
- B29C70/36—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 impregnating by casting, e.g. vacuum casting
-
- 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
- B29C70/40—Shaping or impregnating by compression not applied
- B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
- B29C70/44—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
- B29C70/443—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding and impregnating by vacuum or injection
-
- 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
- B29C70/40—Shaping or impregnating by compression not applied
- B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
- B29C70/44—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
- B29C70/446—Moulding structures having an axis of symmetry or at least one channel, e.g. tubular structures, frames
-
- 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
- B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
- B29C70/541—Positioning reinforcements in a mould, e.g. using clamping means for the reinforcement
-
- 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
- B29D23/00—Producing tubular articles
- B29D23/001—Pipes; Pipe joints
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B30—PRESSES
- B30B—PRESSES IN GENERAL
- B30B5/00—Presses characterised by the use of pressing means other than those mentioned in the preceding groups
- B30B5/02—Presses characterised by the use of pressing means other than those mentioned in the preceding groups wherein the pressing means is in the form of a flexible element, e.g. diaphragm, urged by fluid pressure
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
- B29K2105/06—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
- B29K2105/08—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns
- B29K2105/0872—Prepregs
- B29K2105/089—Prepregs fabric
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2307/00—Use of elements other than metals as reinforcement
- B29K2307/04—Carbon
-
- 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
- B29L2023/00—Tubular articles
- B29L2023/22—Tubes or pipes, i.e. rigid
-
- 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
- B29L2031/3082—Fuselages
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Moulding By Coating Moulds (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US749207P | 2007-12-13 | 2007-12-13 | |
DE102007060029A DE102007060029A1 (de) | 2007-12-13 | 2007-12-13 | Verfahren und Vorrichtung zur Herstellung röhrenförmiger Strukturbauteile |
PCT/EP2008/065355 WO2009074419A1 (de) | 2007-12-13 | 2008-11-12 | Verfahren und vorrichtung zur herstellung röhrenförmiger strukturbauteile |
Publications (1)
Publication Number | Publication Date |
---|---|
BRPI0821246A2 true BRPI0821246A2 (pt) | 2015-06-16 |
Family
ID=40679895
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BRPI0821246-5A BRPI0821246A2 (pt) | 2007-12-13 | 2008-11-12 | Método e dispositivo para produção de componentes estruturais em formato de tubo |
Country Status (9)
Country | Link |
---|---|
US (3) | US20100276069A1 (pt) |
EP (1) | EP2229273B1 (pt) |
JP (1) | JP2011506136A (pt) |
CN (1) | CN101896329B (pt) |
BR (1) | BRPI0821246A2 (pt) |
CA (1) | CA2707802A1 (pt) |
DE (1) | DE102007060029A1 (pt) |
RU (1) | RU2488488C2 (pt) |
WO (1) | WO2009074419A1 (pt) |
Families Citing this family (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8529818B2 (en) * | 2009-09-30 | 2013-09-10 | General Electric Company | Automated fiber placement in female mold |
DE102009057009B4 (de) * | 2009-12-04 | 2015-01-08 | Airbus Defence and Space GmbH | Vorrichtung und Verfahren zur Herstellung eines schalenförmigen Verbundbauteils |
DE102009056978A1 (de) * | 2009-12-07 | 2011-06-09 | Airbus Operations Gmbh | Vorrichtung und Verfahren zur Herstellung einer aus einem Faserverbundwerkstoff bestehenden Rumpfschale für ein Luftfahrzeug |
DE102010043415B4 (de) | 2010-11-04 | 2015-04-09 | Airbus Operations Gmbh | Verfahren zum Herstellen eines hohlen Bauteils sowie Vorrichtung |
DE102010051739B3 (de) | 2010-11-19 | 2011-12-29 | Siempelkamp Maschinen- Und Anlagenbau Gmbh & Co. Kg | Verfahren und Vorrichtung zum Herstellen von zylindrischen Großstrukturen |
DE102011119226A1 (de) * | 2011-11-22 | 2013-05-23 | Daimler Ag | Verfahren zum Herstellen eines Hohlprofilssowie Hohlprofilbauteil |
EP2626194A1 (en) * | 2012-02-07 | 2013-08-14 | Siemens Aktiengesellschaft | Method of manufacturing a turbine blade, system for manufacturing a turbine blade and intermediate member for manufacturing a turbine blade |
ITTO20120317A1 (it) | 2012-04-12 | 2013-10-13 | Alenia Aermacchi Spa | Procedimento per la fabbricazione di barili integrali di fusoliera in materiale composito |
DE102012010271B4 (de) | 2012-05-25 | 2017-10-12 | Premium Aerotec Gmbh | Verfahren zur Herstellung eines Faserverbundbauteils mittels eines Vakuumaufbaues |
DE102012210043A1 (de) * | 2012-06-14 | 2013-12-19 | Airbus Operations Gmbh | Verfahren und Vorrichtung zur Herstellung einer Leichtbaustruktur sowie Leichtbaustruktur |
JP6214300B2 (ja) | 2012-10-29 | 2017-10-18 | キヤノン株式会社 | 定着用部材の製造方法及び製造装置 |
DE102012112939A1 (de) | 2012-12-21 | 2014-06-26 | Leichtbau-Zentrum Sachsen Gmbh | Vorrichtung und Verfahren zur Infiltration einer Faserpreform |
DE102013205089A1 (de) * | 2013-03-22 | 2014-09-25 | Supertex Composites Gmbh | Verfahren und Herstellungssystem zur Herstellung eines faserverstärkten Strukturbauteils |
DE102013209143A1 (de) * | 2013-05-16 | 2014-11-20 | Zf Friedrichshafen Ag | Verfahren zum Herstellen eines rotationssymmetrischen Faser-Kunststoff-Verbund-Bauteils, Vorrichtung zur Durchführung eines derartigen Verfahrens und rotationssym-metrisches Faser-Kunststoff-Verbund-Bauteil |
DE102014217039A1 (de) * | 2014-08-27 | 2016-03-03 | Bayerische Motoren Werke Aktiengesellschaft | Verfahren für die Herstellung eines mit wenigstens einem Verstärkungsschott verstärkten geschlossenen Hohlprofils aus Faserverbundmaterial |
DE102014217486A1 (de) * | 2014-09-02 | 2016-03-03 | Bayerische Motoren Werke Aktiengesellschaft | Verfahren zum Herstellen von FKV-Bauteilen mit lokaler Verstärkung |
CN104494160B (zh) * | 2014-11-25 | 2017-01-25 | 中联重科股份有限公司 | 折叠臂架、纤维增强树脂基复合材料臂节及其制造方法 |
EP3271127B1 (en) * | 2015-03-17 | 2020-11-18 | President and Fellows of Harvard College | Method for automated membrane fabrication |
EP3312083B1 (en) * | 2015-11-05 | 2021-10-20 | Airbus Operations, S.L.U. | Forming tool for manufacturing an aperture surrounding frame for an aircraft fuselage |
US10689087B2 (en) | 2016-08-02 | 2020-06-23 | The Boeing Company | Tubular structure and a method of manufacturing thereof |
GB2555089A (en) * | 2016-10-11 | 2018-04-25 | Jaguar Land Rover Ltd | A Method of moulding a composite structure |
WO2019021537A1 (ja) * | 2017-07-25 | 2019-01-31 | 株式会社Subaru | 複合材成形治具及び複合材成形方法 |
US10520933B2 (en) | 2018-04-13 | 2019-12-31 | The Boeing Company | System and method for removing a workpiece from a manufacturing fixture |
US11523750B2 (en) | 2018-08-06 | 2022-12-13 | Biosense Webster (Israel) Ltd. | Assessing tissue contact with catheter using pairs of electrodes and common reference ground established using designed circuit-board capacitance |
DE102019007784B4 (de) * | 2019-11-09 | 2021-07-01 | Diehl Aviation Laupheim Gmbh | Hohlkanal-Herstellung im Sandwich-Panel mit Platzhalter und Sandwich-Panel |
Family Cites Families (23)
Publication number | Priority date | Publication date | Assignee | Title |
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US2739350A (en) * | 1952-01-28 | 1956-03-27 | Northrop Aircraft Inc | Method and means of molding |
US2815534A (en) * | 1954-07-12 | 1957-12-10 | Ising George Earl | Process for making a closed one-piece reinforced plastic tank |
US2995781A (en) * | 1957-11-19 | 1961-08-15 | Clarence L Sipler | Method of making tubular conduits |
US3049901A (en) * | 1960-04-01 | 1962-08-21 | Singer Fidelity Inc | Flexible hose |
DE3923416A1 (de) * | 1989-07-12 | 1991-01-24 | Mecron Med Prod Gmbh | Verfahren zur herstellung eines ein hohlprofil aufweisenden koerpers |
JP2935722B2 (ja) * | 1990-02-28 | 1999-08-16 | 富士重工業株式会社 | 航空機の胴体構造およびその成形方法 |
CA2056224A1 (en) * | 1990-12-19 | 1992-06-20 | Terry Martin Boustead | Conformal composite molding |
FR2704898B1 (fr) | 1993-05-03 | 1995-08-04 | Drillflex | Structure tubulaire de preforme ou de matrice pour le tubage d'un puits. |
FR2769866B1 (fr) * | 1997-10-20 | 2000-01-14 | Sarma | Procede de moulage, moule de fabrication d'une piece globalement cylindrique a profil creux en matiere composite et piece obtenue grace a ce procede |
DE19803909A1 (de) | 1998-02-02 | 1999-08-05 | Ver Foerderung Inst Kunststoff | Verfahren zur Herstellung von endlosfaserverstärkten Hohlkörpern im Harzinjektionsverfahren |
KR20010075455A (ko) * | 1998-09-30 | 2001-08-09 | 히라이 가쯔히꼬 | 중공 단면을 갖는 섬유 강화 수지 구조체 및 그의 제조 방법 |
JP4346143B2 (ja) * | 1999-02-24 | 2009-10-21 | 社団法人日本航空宇宙工業会 | 複合樹脂製品の成形方法及びその装置 |
DE19913079A1 (de) * | 1999-03-23 | 2000-09-28 | Bayerische Motoren Werke Ag | Bauteil aus einem thermoplastischen Faserverbundwerkstoff und Verfahren zu dessen Herstellung |
US6510961B1 (en) * | 1999-04-14 | 2003-01-28 | A&P Technology | Integrally-reinforced braided tubular structure and method of producing the same |
RU2156397C1 (ru) * | 1999-06-30 | 2000-09-20 | Государственное предприятие "Производственное объединение "Авангард" | Способ ремонта трубопровода (варианты) |
US7204951B2 (en) * | 2002-07-30 | 2007-04-17 | Rocky Mountain Composites, Inc. | Method of assembling a single piece co-cured structure |
US20080289743A1 (en) * | 2003-05-02 | 2008-11-27 | Tsotsis Thomas K | Highly porous interlayers to toughen liquid-molded fabric-based composites |
US20040219855A1 (en) * | 2003-05-02 | 2004-11-04 | Tsotsis Thomas K. | Highly porous interlayers to toughen liquid-molded fabric-based composites |
DE102004006615B4 (de) * | 2004-02-10 | 2016-03-31 | Airbus Helicopters Deutschland GmbH | Verfahren zur Herstellung eines Faserverbundwerkstoff-Hohlbauteils sowie Zwischenprodukt dafür |
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 |
JP4826176B2 (ja) * | 2005-08-31 | 2011-11-30 | 東レ株式会社 | 強化繊維プリフォームおよびrtm成形方法 |
US7824171B2 (en) * | 2005-10-31 | 2010-11-02 | The Boeing Company | Corner-consolidating inflatable apparatus and method for manufacturing composite structures |
CN101711211A (zh) * | 2007-01-30 | 2010-05-19 | 空客运营有限公司 | 用于飞行器机身的复合材料结构及其制造方法 |
-
2007
- 2007-12-13 DE DE102007060029A patent/DE102007060029A1/de not_active Ceased
-
2008
- 2008-11-12 RU RU2010122662/05A patent/RU2488488C2/ru not_active IP Right Cessation
- 2008-11-12 EP EP08860048.1A patent/EP2229273B1/de not_active Not-in-force
- 2008-11-12 CA CA2707802A patent/CA2707802A1/en not_active Abandoned
- 2008-11-12 CN CN200880120453.0A patent/CN101896329B/zh not_active Expired - Fee Related
- 2008-11-12 BR BRPI0821246-5A patent/BRPI0821246A2/pt not_active IP Right Cessation
- 2008-11-12 JP JP2010537352A patent/JP2011506136A/ja active Pending
- 2008-11-12 WO PCT/EP2008/065355 patent/WO2009074419A1/de active Application Filing
-
2010
- 2010-06-04 US US12/794,487 patent/US20100276069A1/en not_active Abandoned
-
2014
- 2014-05-23 US US14/285,704 patent/US9180628B2/en not_active Expired - Fee Related
-
2015
- 2015-10-30 US US14/928,389 patent/US20160129647A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
RU2010122662A (ru) | 2012-01-20 |
US20160129647A1 (en) | 2016-05-12 |
RU2488488C2 (ru) | 2013-07-27 |
WO2009074419A1 (de) | 2009-06-18 |
CN101896329A (zh) | 2010-11-24 |
EP2229273A1 (de) | 2010-09-22 |
EP2229273B1 (de) | 2016-01-27 |
US20100276069A1 (en) | 2010-11-04 |
JP2011506136A (ja) | 2011-03-03 |
CN101896329B (zh) | 2014-04-09 |
US9180628B2 (en) | 2015-11-10 |
DE102007060029A1 (de) | 2009-06-18 |
US20140346715A1 (en) | 2014-11-27 |
CA2707802A1 (en) | 2009-06-18 |
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