BRPI0813463A2 - Aperfeiçoamento em membros estruturais compósitos alongados - Google Patents
Aperfeiçoamento em membros estruturais compósitos alongadosInfo
- Publication number
- BRPI0813463A2 BRPI0813463A2 BRPI0813463-4A2A BRPI0813463A BRPI0813463A2 BR PI0813463 A2 BRPI0813463 A2 BR PI0813463A2 BR PI0813463 A BRPI0813463 A BR PI0813463A BR PI0813463 A2 BRPI0813463 A2 BR PI0813463A2
- Authority
- BR
- Brazil
- Prior art keywords
- improvement
- structural members
- composite structural
- extended composite
- extended
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/18—Spars; Ribs; Stringers
- B64C3/182—Stringers, longerons
-
- 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
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/26—Construction, shape, or attachment of separate skins, e.g. panels
-
- 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
-
- 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
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
-
- 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
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24174—Structurally defined web or sheet [e.g., overall dimension, etc.] including sheet or component perpendicular to plane of web or sheet
-
- 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
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24628—Nonplanar uniform thickness material
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GBGB0712549.5A GB0712549D0 (en) | 2007-06-29 | 2007-06-29 | Improvements in elongate composite structural members |
PCT/GB2008/050485 WO2009004364A2 (en) | 2007-06-29 | 2008-06-24 | Improvements in elongate composite structural member |
Publications (1)
Publication Number | Publication Date |
---|---|
BRPI0813463A2 true BRPI0813463A2 (pt) | 2014-12-23 |
Family
ID=38420862
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BRPI0813463-4A2A BRPI0813463A2 (pt) | 2007-06-29 | 2008-06-24 | Aperfeiçoamento em membros estruturais compósitos alongados |
Country Status (10)
Country | Link |
---|---|
US (1) | US8864076B2 (pt) |
EP (1) | EP2162351B1 (pt) |
JP (1) | JP5686287B2 (pt) |
KR (1) | KR101515051B1 (pt) |
CN (1) | CN101795937B (pt) |
BR (1) | BRPI0813463A2 (pt) |
CA (1) | CA2691165C (pt) |
GB (1) | GB0712549D0 (pt) |
RU (1) | RU2486102C2 (pt) |
WO (1) | WO2009004364A2 (pt) |
Families Citing this family (33)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB0712549D0 (en) | 2007-06-29 | 2007-08-08 | Airbus Uk Ltd | Improvements in elongate composite structural members |
GB0712552D0 (en) | 2007-06-29 | 2007-08-08 | Airbus Uk Ltd | Elongate composite structural members and improvements therein |
GB0712553D0 (en) | 2007-06-29 | 2007-08-08 | Airbus Uk Ltd | Composite panel stiffener |
GB0813146D0 (en) | 2008-07-18 | 2008-08-27 | Airbus Uk Ltd | Ramped stiffener and apparatus and method for forming the same |
GB0813161D0 (en) | 2008-07-18 | 2008-08-27 | Airbus Uk Ltd | Ramped stiffener and apparatus and method for forming the same |
GB0813149D0 (en) | 2008-07-18 | 2008-08-27 | Airbus Uk Ltd | Ramped stiffener and apparatus and method for forming the same |
ES2393102B1 (es) * | 2010-06-30 | 2013-11-21 | Airbus Operations, S.L. | Componente de aeronave con paneles rigidizados con larguerillos con dos tipos de ensanchamientos locales. |
US9266279B2 (en) | 2010-07-08 | 2016-02-23 | Orbital Atk, Inc. | Variable material stretch-forming apparatus and methods |
GB201101435D0 (en) * | 2011-01-27 | 2011-03-16 | Airbus Uk Ltd | Stringer for an aircraft wing and method of forming thereof |
ES2392233B1 (es) * | 2011-01-31 | 2013-10-09 | Airbus Operations S.L. | Revestimiento de cajón de torsión rigidizado con larguerillos no paralelos. |
US8993097B2 (en) | 2011-10-10 | 2015-03-31 | The Boeing Company | Tapered height curved composite stringers and corresponding panels |
US9352822B2 (en) * | 2012-05-30 | 2016-05-31 | The Boeing Company | Bonded composite airfoil |
EP2687436B1 (en) * | 2012-07-17 | 2016-08-31 | Airbus Operations, S.L. | Highly integrated leading edge of an aircraft lifting surface |
US8973871B2 (en) * | 2013-01-26 | 2015-03-10 | The Boeing Company | Box structures for carrying loads and methods of making the same |
GB201307066D0 (en) * | 2013-04-18 | 2013-05-29 | Airbus Operations Ltd | Winglet and braided composite spar |
US10329009B2 (en) * | 2014-09-17 | 2019-06-25 | The Boeing Company | Composite wing edge attachment and method |
US9809297B2 (en) * | 2015-08-26 | 2017-11-07 | The Boeing Company | Structures containing stiffeners having transition portions |
JP6581875B2 (ja) * | 2015-10-06 | 2019-09-25 | 三菱重工業株式会社 | 複合材の成形方法 |
US10207789B2 (en) * | 2016-08-16 | 2019-02-19 | The Boeing Company | Aircraft composite wingbox integration |
US10421528B2 (en) | 2016-08-16 | 2019-09-24 | The Boeing Company | Planked stringers that provide structural support for an aircraft wing |
GB2557274A (en) * | 2016-12-02 | 2018-06-20 | Airbus Operations Ltd | Aerofoil structure components |
CN106650045B (zh) * | 2016-12-05 | 2019-07-12 | 大连理工大学 | 一种二级箱间段结构优化设计与强度分析方法 |
CN106777617B (zh) * | 2016-12-05 | 2019-06-14 | 大连理工大学 | 一种二级箱间段结构优化设计方法 |
US10647406B2 (en) * | 2017-06-01 | 2020-05-12 | The Boeing Company | Closed-angle composite airfoil spar and method of fabricating the same |
JP7034846B2 (ja) * | 2018-06-15 | 2022-03-14 | 三菱重工業株式会社 | プリプレグ積層用成形型及びプリプレグ積層方法 |
US11312468B2 (en) * | 2018-08-08 | 2022-04-26 | The Boeing Company | Elongate structures, structural assemblies with elongate structures, and methods for supporting a structural load |
CN109484672B (zh) * | 2018-11-30 | 2024-01-16 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | 一种上墙端与壁板连接整体角盒组件 |
CN109409009A (zh) * | 2018-11-30 | 2019-03-01 | 中国航空工业集团公司沈阳飞机设计研究所 | 一种弯扭耦合机翼结构优化方法 |
CN113165281B (zh) * | 2018-12-10 | 2023-07-21 | 维斯塔斯风力系统有限公司 | 关于风力涡轮机叶片制造的改进 |
US10913215B2 (en) * | 2019-05-09 | 2021-02-09 | The Boeing Company | Composite structure having a variable gage and methods for forming a composite structure having a variable gage |
US10919256B2 (en) * | 2019-05-09 | 2021-02-16 | The Boeing Company | Composite structure having a variable gage and methods for forming a composite structure having a variable gage |
US10919260B2 (en) * | 2019-05-09 | 2021-02-16 | The Boeing Company | Composite structure having a variable gage and methods for forming a composite structure having a variable gage |
GB2615755A (en) * | 2022-02-15 | 2023-08-23 | Airbus Operations Ltd | Fuel tank stringer with flow passage |
Family Cites Families (73)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2403569A (en) * | 1943-06-16 | 1946-07-09 | Budd Edward G Mfg Co | Fabricated metal structure |
US2471490A (en) * | 1945-08-10 | 1949-05-31 | Carnegie Illinois Steel Corp | Apparatus for making structural shapes |
US2655194A (en) * | 1946-10-31 | 1953-10-13 | Einar W Nilsson | Apparatus for processing round bars and tubes |
US3355922A (en) | 1964-09-29 | 1967-12-05 | Kawasaki Steel Co | Roll forming machine |
US3519228A (en) * | 1967-09-29 | 1970-07-07 | Dow Chemical Co | Airfoil structure |
US3657911A (en) * | 1970-03-13 | 1972-04-25 | Foster Wheeler Corp | Bending machine |
NL7203324A (pt) * | 1972-03-14 | 1973-09-18 | ||
US4006617A (en) * | 1975-11-24 | 1977-02-08 | The Boeing Company | Method and apparatus for roll forming tapered structural members |
US4084029A (en) * | 1977-07-25 | 1978-04-11 | The Boeing Company | Sine wave beam web and method of manufacture |
US4331723A (en) | 1980-11-05 | 1982-05-25 | The Boeing Company | Advanced composite |
JPS5927722A (ja) | 1982-08-07 | 1984-02-14 | Shiraki Kinzoku Kogyo Kk | ロ−ル成形装置 |
JPS59179228A (ja) | 1983-03-31 | 1984-10-11 | Shiraki Kinzoku Kogyo Kk | ロ−ル成形装置 |
SU1304743A3 (ru) | 1983-07-15 | 1987-04-15 | Спи-Батиньоль (Фирма) | Способ изготовлени тонких профильных полос и устройство дл его осуществлени |
JPS61108404A (ja) | 1984-11-02 | 1986-05-27 | Nippon Steel Corp | フランジを有する形材の圧延方法 |
JPS62207637A (ja) | 1986-03-10 | 1987-09-12 | 財団法人日本航空機開発協会 | 板状構造材用補強材の成形方法およびその成形装置 |
JPS63258297A (ja) * | 1987-04-16 | 1988-10-25 | 富士重工業株式会社 | 複合材による箱形構造体の補強構造 |
JP2517634B2 (ja) * | 1987-12-21 | 1996-07-24 | 富士重工業株式会社 | 複合材料製品の成形方法 |
US5171510A (en) * | 1988-06-08 | 1992-12-15 | Aerospatiale Societe Nationale Industrielle | Method of producing a frame made of a composite material, especially for the fuselage of an aircraft |
US4913910A (en) * | 1988-06-22 | 1990-04-03 | The Boeing Company | Apparatus for forming laminate into a predetermined configuration |
US5026447A (en) * | 1989-02-10 | 1991-06-25 | Phillips Petroleum Company | Method for making variable cross section pultruded thermoplastic composite articles |
EP0395224A3 (en) | 1989-04-26 | 1991-01-02 | General Motors Corporation | A feature based method of designing automotive panels |
US5096525A (en) * | 1989-09-12 | 1992-03-17 | The Boeing Company | Apparatus and method for forming and bonding a thermoplastic part from thermoplastic blanks |
US5036688A (en) * | 1989-12-18 | 1991-08-06 | Quality Trailer Products Corporation | Fender forming system |
US5182060A (en) * | 1991-01-31 | 1993-01-26 | E. I. Du Pont De Nemours And Company | Continuous forming of composites |
US5074139A (en) * | 1991-03-04 | 1991-12-24 | Motorola, Inc. | Roll forming of semiconductor component leadframes |
JP3021077B2 (ja) | 1991-03-28 | 2000-03-15 | 富士重工業株式会社 | 複合材充填材の成形装置 |
JPH07102609B2 (ja) | 1991-08-12 | 1995-11-08 | 川崎重工業株式会社 | 繊維強化複合材の成形方法 |
AT398064B (de) * | 1992-07-01 | 1994-09-26 | Hoac Austria Flugzeugwerk Wr N | Kunststoff-verbundprofil, insbesondere flügelholm für den flugzeugbau |
JPH06226356A (ja) | 1993-01-29 | 1994-08-16 | Aisin Seiki Co Ltd | ロール成形法 |
JP3578796B2 (ja) | 1993-04-19 | 2004-10-20 | 橋本フォーミング工業株式会社 | 異形横断面形状の長尺材の製造方法および装置 |
JPH07172395A (ja) * | 1993-12-20 | 1995-07-11 | Mitsubishi Heavy Ind Ltd | 航空機のインテグラルタンク |
JP3483623B2 (ja) | 1994-07-19 | 2004-01-06 | 富士重工業株式会社 | 繊維強化プラスチック構造部材の成形方法 |
US5538589A (en) * | 1994-08-31 | 1996-07-23 | The Boeing Company | Composite stringer assembly machine |
JP2954836B2 (ja) | 1994-09-14 | 1999-09-27 | 川崎重工業株式会社 | 繊維強化樹脂系型材の成形方法 |
GB2312532B (en) | 1995-04-19 | 1998-04-22 | Honda Motor Co Ltd | Method of generating die structure data and producing a die structure |
US5729462A (en) * | 1995-08-25 | 1998-03-17 | Northrop Grumman Corporation | Method and apparatus for constructing a complex tool surface for use in an age forming process |
US7509740B2 (en) * | 2001-11-13 | 2009-03-31 | The Boeing Company | Method of manufacturing a wing |
US5820804A (en) * | 1996-06-20 | 1998-10-13 | Elmaleh; Jon | Apparatus and method for shaping an elongated member |
US5848765A (en) * | 1996-06-20 | 1998-12-15 | The Boeing Company | Reduced amplitude corrugated web spar |
JP3737581B2 (ja) | 1996-11-12 | 2006-01-18 | シロキ工業株式会社 | ロール成形装置 |
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 |
US5984511A (en) * | 1997-05-12 | 1999-11-16 | Mcdonnell Douglas Corporation | Knowledge driven composite design optimization process and system therefor |
US6375120B1 (en) * | 1997-07-14 | 2002-04-23 | Jason M. Wolnek | Method and apparatus for building a metal/composite hybrid airplane component |
AU6354499A (en) | 1998-10-23 | 2000-05-15 | Bae Systems Plc | A roll forming machine and method |
GB9828368D0 (en) * | 1998-12-22 | 1999-02-17 | British Aerospace | Forming reinforcing components |
JP3012847B1 (ja) * | 1999-03-25 | 2000-02-28 | 株式会社ジャムコ | 複合材の成形方法とその装置 |
RU2144487C1 (ru) | 1999-07-06 | 2000-01-20 | Закрытое акционерное общество "Интеллект" | Стрингер летательного аппарата |
RU2144488C1 (ru) * | 1999-07-06 | 2000-01-20 | Закрытое акционерное общество "Интеллект" | Лонжерон летательного аппарата |
US6513757B1 (en) | 1999-07-19 | 2003-02-04 | Fuji Jukogyo Kabushiki Kaisha | Wing of composite material and method of fabricating the same |
FR2804057B1 (fr) * | 2000-01-24 | 2002-09-20 | Plastic Omnium Cie | Moule a plan de joint mobile pour realiser une piece en matiere plastique et un procede utilisant un tel moule |
ES2185443B1 (es) | 2000-03-07 | 2004-09-01 | Airbus España S.L. | Procedimiento de fabricacion de piezas precuradas en material compuesto con rigidizadores aplicados en estado fresco. |
US6478922B1 (en) | 2000-06-15 | 2002-11-12 | Alliant Techsystems Inc. | Method of manufacturing a composite structure using a conformable locating aperture system |
GB0022589D0 (en) | 2000-09-14 | 2000-11-01 | Bae Systems Plc | Composite joints |
JP4639551B2 (ja) | 2001-08-10 | 2011-02-23 | 東レ株式会社 | Cfrp製スキン−ストリンガー構造部材の製造方法 |
DE10210517B3 (de) * | 2002-03-09 | 2004-01-29 | Airbus Deutschland Gmbh | Verfahren zur Herstellung eines Bauteiles in Faserverbundbauweise |
GB0207239D0 (en) * | 2002-03-27 | 2002-05-08 | Airbus Uk Ltd | Wing skin and method of manufacture thereof |
RU2219058C1 (ru) | 2002-04-22 | 2003-12-20 | ФГУП Кумертауское авиационное производственное предприятие | Способ изготовления композиционных крупногабаритных лопастей |
US6814916B2 (en) * | 2002-08-30 | 2004-11-09 | The Boeing Company | Forming method for composites |
EP1408224A1 (fr) | 2002-10-10 | 2004-04-14 | Hubert Antoine | Moteur à piston combiné à un cycle de Joule |
JP2004338465A (ja) * | 2003-05-14 | 2004-12-02 | Murata Mach Ltd | コーナーフィーラー及びコーナーフィーラーを充填した構造体及びコーナーフィーラーの製造方法 |
JP3782072B2 (ja) * | 2003-05-30 | 2006-06-07 | 川崎重工業株式会社 | 複合材型材の成形方法及び装置 |
EP1547756A1 (en) | 2003-12-24 | 2005-06-29 | Airbus UK Limited | Method of manufacturing aircraft components |
JP3862697B2 (ja) * | 2003-12-26 | 2006-12-27 | 株式会社ジャムコ | 熱硬化複合材料の成形装置 |
FR2866626B1 (fr) * | 2004-02-20 | 2006-05-19 | Airbus France | Arret de raidisseur a pentes decalees et panneau muni d'un tel arret |
WO2005105413A2 (en) | 2004-04-21 | 2005-11-10 | Ingersoll Machine Tools, Inc. | Automated forming of pre-impregnated composite structural elements |
US7469735B2 (en) * | 2005-08-03 | 2008-12-30 | The Boeing Corporation | Composite structural element fabricating device and method |
US7398586B2 (en) * | 2005-11-01 | 2008-07-15 | The Boeing Company | Methods and systems for manufacturing a family of aircraft wings and other composite structures |
US9102103B2 (en) * | 2006-02-02 | 2015-08-11 | The Boeing Company | Thermoplastic composite parts having integrated metal fittings and method of making the same |
US7575194B2 (en) * | 2006-11-30 | 2009-08-18 | The Boeing Company | Apparatuses and methods for joining composite members and other structural members in aircraft wing boxes and other structures |
ES2346834B1 (es) * | 2007-04-30 | 2011-08-17 | Airbus Operations, S.L. | Estructura de costilla para cajones de torsion de un ala o de un estabilizador de una aeronave. |
GB0712553D0 (en) | 2007-06-29 | 2007-08-08 | Airbus Uk Ltd | Composite panel stiffener |
GB0712549D0 (en) | 2007-06-29 | 2007-08-08 | Airbus Uk Ltd | Improvements in elongate composite structural members |
DE102008002117B4 (de) * | 2008-05-30 | 2013-10-31 | Airbus Operations Gmbh | Verbund und Struktur |
-
2007
- 2007-06-29 GB GBGB0712549.5A patent/GB0712549D0/en not_active Ceased
-
2008
- 2008-06-24 EP EP08762590.1A patent/EP2162351B1/en not_active Not-in-force
- 2008-06-24 BR BRPI0813463-4A2A patent/BRPI0813463A2/pt not_active IP Right Cessation
- 2008-06-24 KR KR1020107002189A patent/KR101515051B1/ko not_active IP Right Cessation
- 2008-06-24 WO PCT/GB2008/050485 patent/WO2009004364A2/en active Application Filing
- 2008-06-24 CA CA2691165A patent/CA2691165C/en not_active Expired - Fee Related
- 2008-06-24 JP JP2010514134A patent/JP5686287B2/ja not_active Expired - Fee Related
- 2008-06-24 RU RU2010102980/11A patent/RU2486102C2/ru not_active IP Right Cessation
- 2008-06-24 US US12/602,163 patent/US8864076B2/en not_active Expired - Fee Related
- 2008-06-24 CN CN2008801010484A patent/CN101795937B/zh not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
JP2010531777A (ja) | 2010-09-30 |
US20100178453A1 (en) | 2010-07-15 |
RU2486102C2 (ru) | 2013-06-27 |
CA2691165A1 (en) | 2009-01-08 |
CN101795937A (zh) | 2010-08-04 |
GB0712549D0 (en) | 2007-08-08 |
JP5686287B2 (ja) | 2015-03-18 |
EP2162351A2 (en) | 2010-03-17 |
KR20100045453A (ko) | 2010-05-03 |
CA2691165C (en) | 2016-10-04 |
KR101515051B1 (ko) | 2015-04-24 |
WO2009004364A3 (en) | 2009-05-22 |
EP2162351B1 (en) | 2014-10-15 |
RU2010102980A (ru) | 2011-08-10 |
US8864076B2 (en) | 2014-10-21 |
WO2009004364A2 (en) | 2009-01-08 |
CN101795937B (zh) | 2013-05-08 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
BRPI0813463A2 (pt) | Aperfeiçoamento em membros estruturais compósitos alongados | |
BRPI0820937A2 (pt) | Peças em material compósito eletroestrutural | |
BRPI0912585A2 (pt) | compósito acústico | |
BRPI0719715A2 (pt) | Estrutura composta | |
BRPI0918712A2 (pt) | laminado | |
FR2948598B1 (fr) | Renfort composite | |
BRPI0917195A2 (pt) | estrutura compósita curada-plana | |
BRPI0921259A2 (pt) | conjunto em conformidade com nvis | |
BRPI0908777A2 (pt) | Arco preferencial em telas compósitas | |
FI20070691A (fi) | Paneelirakenne | |
DE602008000866D1 (de) | Verbunddrehbank | |
DE602008003400D1 (de) | Wabenstruktur | |
BRPI1015045A2 (pt) | melhoramentos nos materiais compósitos. | |
BRPI0820446A2 (pt) | Recipente compósito | |
BR112012010477A2 (pt) | pilar compósito furcado | |
BR112012011362A2 (pt) | estrutura de núcleo e painel compósito | |
DE602009001201D1 (de) | Wabenstruktur | |
ES2965663T3 (es) | Mejoras en materiales compuestos | |
DE112009001284A5 (de) | Kompositstruktur | |
DK2326172T3 (da) | Antisvampemidler | |
FR2936181B1 (fr) | Panneau sandwich composite renforce | |
BRPI0914767A2 (pt) | composição de laminado compósito | |
BRPI0911641A2 (pt) | unidade estrutural | |
FR2952581B1 (fr) | Panneau en materiau composite | |
BRPI0820958A2 (pt) | Intermediário, e, composto |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
B25D | Requested change of name of applicant approved |
Owner name: AIRBUS OPERATIONS LIMITED (GB) |
|
B08F | Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette] | ||
B08K | Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette] |