BRPI0813962A2 - Membros estruturais de compósito alongados e melhorias nestes - Google Patents
Membros estruturais de compósito alongados e melhorias nestesInfo
- Publication number
- BRPI0813962A2 BRPI0813962A2 BRPI0813962-8A2A BRPI0813962A BRPI0813962A2 BR PI0813962 A2 BRPI0813962 A2 BR PI0813962A2 BR PI0813962 A BRPI0813962 A BR PI0813962A BR PI0813962 A2 BRPI0813962 A2 BR PI0813962A2
- Authority
- BR
- Brazil
- Prior art keywords
- spar
- structural
- web
- length
- linearly
- 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
- B29C70/30—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
- B29C70/302—Details of the edges of fibre composites, e.g. edge finishing or means to avoid delamination
-
- 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
- B64C1/064—Stringers; Longerons
-
- 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
- B64C1/065—Spars
-
- 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
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/18—Spars; Ribs; Stringers
- B64C3/185—Spars
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/18—Spars; Ribs; Stringers
- B64C3/187—Ribs
-
- G—PHYSICS
- G06—COMPUTING OR CALCULATING; COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F30/00—Computer-aided design [CAD]
- G06F30/10—Geometric CAD
- G06F30/15—Vehicle, aircraft or watercraft design
-
- 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
- B29K2105/24—Condition, form or state of moulded material or of the material to be shaped crosslinked or vulcanised
- B29K2105/246—Uncured, e.g. green
-
- 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
- B64C2001/0054—Fuselage structures substantially made from particular materials
- B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- Geometry (AREA)
- Theoretical Computer Science (AREA)
- General Physics & Mathematics (AREA)
- Composite Materials (AREA)
- Chemical & Material Sciences (AREA)
- Computational Mathematics (AREA)
- Computer Hardware Design (AREA)
- Evolutionary Computation (AREA)
- General Engineering & Computer Science (AREA)
- Pure & Applied Mathematics (AREA)
- Mathematical Optimization (AREA)
- Mathematical Analysis (AREA)
- Automation & Control Theory (AREA)
- Moulding By Coating Moulds (AREA)
- Laminated Bodies (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GBGB0712552.9A GB0712552D0 (en) | 2007-06-29 | 2007-06-29 | Elongate composite structural members and improvements therein |
| PCT/GB2008/050481 WO2009004363A2 (en) | 2007-06-29 | 2008-06-24 | Elongate composite structural members and improvements therein |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BRPI0813962A2 true BRPI0813962A2 (pt) | 2015-01-06 |
Family
ID=38420865
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BRPI0813962-8A2A BRPI0813962A2 (pt) | 2007-06-29 | 2008-06-24 | Membros estruturais de compósito alongados e melhorias nestes |
Country Status (12)
| Country | Link |
|---|---|
| US (1) | US8864075B2 (pt) |
| EP (2) | EP2167379B1 (pt) |
| JP (1) | JP5686286B2 (pt) |
| KR (2) | KR101558988B1 (pt) |
| CN (1) | CN101772452B (pt) |
| AT (2) | ATE544672T1 (pt) |
| BR (1) | BRPI0813962A2 (pt) |
| CA (1) | CA2690988A1 (pt) |
| DE (1) | DE602008005884D1 (pt) |
| GB (1) | GB0712552D0 (pt) |
| RU (1) | RU2485011C2 (pt) |
| WO (1) | WO2009004363A2 (pt) |
Families Citing this family (31)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2010056164A1 (en) * | 2008-11-13 | 2010-05-20 | Saab Ab | Method of forming a composite article |
| US8074694B2 (en) * | 2009-05-28 | 2011-12-13 | The Boeing Company | Stringer transition method |
| EP2383669B1 (en) * | 2010-04-02 | 2018-07-11 | Dassault Systèmes | Design of a part modeled by parallel geodesic curves |
| GB201008186D0 (en) * | 2010-05-17 | 2010-06-30 | Airbus Operations Ltd | A structural assembly for an aircraft |
| US9682514B2 (en) | 2010-06-25 | 2017-06-20 | The Boeing Company | Method of manufacturing resin infused composite parts using a perforated caul sheet |
| US8940213B2 (en) | 2010-06-25 | 2015-01-27 | The Boeing Company | Resin infusion of composite parts using a perforated caul sheet |
| US8628717B2 (en) | 2010-06-25 | 2014-01-14 | The Boeing Company | Composite structures having integrated stiffeners and method of making the same |
| US8636252B2 (en) | 2010-06-25 | 2014-01-28 | The Boeing Company | Composite structures having integrated stiffeners with smooth runouts and method of making the same |
| US8967526B2 (en) * | 2010-08-12 | 2015-03-03 | Abe Karem | Multi-role aircraft with interchangeable mission modules |
| US9221532B2 (en) * | 2010-08-12 | 2015-12-29 | Abe Karem | Multi-role aircraft with interchangeable mission modules |
| DE102010053635B4 (de) * | 2010-12-07 | 2017-05-11 | Hero Gmbh | Verfahren zur Herstellung eines Faserverbundprodukts |
| US8993097B2 (en) * | 2011-10-10 | 2015-03-31 | The Boeing Company | Tapered height curved composite stringers and corresponding panels |
| CN103008497B (zh) * | 2012-11-06 | 2014-09-10 | 西北工业大学 | 一种框肋类钣金件复杂弯边展开方法 |
| US20150203187A1 (en) * | 2013-04-02 | 2015-07-23 | The Boeing Company | Continuously Curved Spar and Method of Manufacturing |
| GB201307066D0 (en) | 2013-04-18 | 2013-05-29 | Airbus Operations Ltd | Winglet and braided composite spar |
| DE102013011915A1 (de) * | 2013-07-17 | 2015-01-22 | Airbus Defence and Space GmbH | Veränderbares Flügelprofil |
| CN103495636B (zh) * | 2013-09-30 | 2015-09-02 | 中国航空工业集团公司北京航空制造工程研究所 | 采用柔性多点模具进行蒙皮拉形及定位的方法 |
| CN103729498B (zh) * | 2013-12-09 | 2017-06-06 | 中国航空工业集团公司西安飞机设计研究所 | 一种大型复合材料加筋壁板结构设计方法 |
| US9626460B2 (en) * | 2014-03-24 | 2017-04-18 | Siemens Prodcut Lifecycle Management Software Inc. | Method for creating accurate, updateable vertical ramps that fall on ramp geometry in transition areas of laminated composite parts |
| US20160275206A1 (en) * | 2014-05-13 | 2016-09-22 | Geodesic Sketching On Curved Surfaces | Geodesic sketching on curved surfaces |
| CN104190772B (zh) * | 2014-09-15 | 2017-02-01 | 沈阳飞机工业(集团)有限公司 | 管接钣金零件弯边展开设计方法 |
| JP6441467B2 (ja) * | 2014-09-29 | 2018-12-19 | ザ・ボーイング・カンパニーThe Boeing Company | 方向舵及び昇降舵の用途のためのキック付スパー |
| CN105511404B (zh) * | 2015-11-30 | 2017-12-19 | 中航飞机股份有限公司西安飞机分公司 | 一种具有复杂特征的双曲率长桁展开加工方法 |
| US10105940B2 (en) * | 2016-04-18 | 2018-10-23 | The Boeing Company | Formation of composite laminates having one or more divergent flanges |
| CN106709184B (zh) * | 2016-12-26 | 2020-01-14 | 中国航空工业集团公司西安飞机设计研究所 | 机翼壁板内形曲面生成方法 |
| 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 |
| US20200086970A1 (en) * | 2018-09-18 | 2020-03-19 | The Boeing Company | Composite fabric wing spar with interleaved tape cap plies |
| CN115339163B (zh) * | 2022-07-28 | 2023-10-24 | 广西师范大学 | 考虑老化效应的复合材料层合板拉伸试样及其制备方法 |
| US12533856B2 (en) * | 2023-08-30 | 2026-01-27 | The Boeing Company | Methods and tools for forming composite structures with preferable wrinkle configurations |
| US12215592B1 (en) | 2024-02-07 | 2025-02-04 | General Electric Company | Preform for making a casing structure for turbine engines |
Family Cites Families (74)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US335922A (en) * | 1886-02-09 | Wash-bowl and pump for sleeping-cars | ||
| 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 |
| 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 |
| US5119309A (en) * | 1989-04-26 | 1992-06-02 | General Motors Corporation | 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 |
| US5332178A (en) * | 1992-06-05 | 1994-07-26 | Williams International Corporation | Composite wing and manufacturing process thereof |
| 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 |
| 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 |
| US5848765A (en) * | 1996-06-20 | 1998-12-15 | The Boeing Company | Reduced amplitude corrugated web spar |
| US5820804A (en) * | 1996-06-20 | 1998-10-13 | Elmaleh; Jon | Apparatus and method for shaping an elongated member |
| 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 |
| JP3628965B2 (ja) * | 1998-10-23 | 2005-03-16 | エアバス・ユ―ケ―・リミテッド | ロール形成機械 |
| 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 |
| RU2144488C1 (ru) * | 1999-07-06 | 2000-01-20 | Закрытое акционерное общество "Интеллект" | Лонжерон летательного аппарата |
| RU2144487C1 (ru) | 1999-07-06 | 2000-01-20 | Закрытое акционерное общество "Интеллект" | Стрингер летательного аппарата |
| JP4187878B2 (ja) * | 1999-07-19 | 2008-11-26 | 富士重工業株式会社 | 航空機の複合材翼およびその製造方法 |
| 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 |
| CN2537631Y (zh) * | 2002-01-04 | 2003-02-26 | 李应奇 | 改进的适用于慢速飞机的机翼 |
| 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 |
| FR2866626B1 (fr) | 2004-02-20 | 2006-05-19 | Airbus France | Arret de raidisseur a pentes decalees et panneau muni d'un tel arret |
| DE102004018579A1 (de) * | 2004-04-16 | 2005-11-03 | Airbus Deutschland Gmbh | Verkleidung für eine Struktur eines Flugzeugs |
| WO2005105413A2 (en) | 2004-04-21 | 2005-11-10 | Ingersoll Machine Tools, Inc. | Automated forming of pre-impregnated composite structural elements |
| JP2006335049A (ja) * | 2005-06-06 | 2006-12-14 | Mitsubishi Heavy Ind Ltd | 複合材シート加工装置、複合構造材の形成方法 |
| US7469735B2 (en) * | 2005-08-03 | 2008-12-30 | The Boeing Corporation | Composite structural element fabricating device and method |
| 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. |
| GB0712549D0 (en) | 2007-06-29 | 2007-08-08 | Airbus Uk Ltd | Improvements in elongate composite structural members |
| GB0712553D0 (en) | 2007-06-29 | 2007-08-08 | Airbus Uk Ltd | Composite panel stiffener |
| JP5180606B2 (ja) * | 2008-01-29 | 2013-04-10 | 三菱重工業株式会社 | 複合材部材の製造方法及びプリプレグシートの積層体 |
-
2007
- 2007-06-29 GB GBGB0712552.9A patent/GB0712552D0/en not_active Ceased
-
2008
- 2008-06-24 EP EP08762589A patent/EP2167379B1/en not_active Not-in-force
- 2008-06-24 RU RU2010102978/11A patent/RU2485011C2/ru not_active IP Right Cessation
- 2008-06-24 DE DE602008005884T patent/DE602008005884D1/de active Active
- 2008-06-24 KR KR1020107001788A patent/KR101558988B1/ko not_active Expired - Fee Related
- 2008-06-24 JP JP2010514133A patent/JP5686286B2/ja not_active Expired - Fee Related
- 2008-06-24 WO PCT/GB2008/050481 patent/WO2009004363A2/en not_active Ceased
- 2008-06-24 KR KR1020157018001A patent/KR101558987B1/ko not_active Expired - Fee Related
- 2008-06-24 EP EP10172445A patent/EP2243702B1/en not_active Not-in-force
- 2008-06-24 US US12/602,160 patent/US8864075B2/en not_active Expired - Fee Related
- 2008-06-24 AT AT10172445T patent/ATE544672T1/de active
- 2008-06-24 CA CA2690988A patent/CA2690988A1/en not_active Abandoned
- 2008-06-24 BR BRPI0813962-8A2A patent/BRPI0813962A2/pt not_active IP Right Cessation
- 2008-06-24 AT AT08762589T patent/ATE503685T1/de not_active IP Right Cessation
- 2008-06-24 CN CN2008801020787A patent/CN101772452B/zh not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| EP2167379B1 (en) | 2011-03-30 |
| CA2690988A1 (en) | 2009-01-08 |
| KR101558988B1 (ko) | 2015-10-19 |
| RU2010102978A (ru) | 2011-08-10 |
| EP2243702A1 (en) | 2010-10-27 |
| CN101772452A (zh) | 2010-07-07 |
| JP2010531776A (ja) | 2010-09-30 |
| US20100170989A1 (en) | 2010-07-08 |
| JP5686286B2 (ja) | 2015-03-18 |
| RU2485011C2 (ru) | 2013-06-20 |
| WO2009004363A3 (en) | 2009-05-14 |
| DE602008005884D1 (de) | 2011-05-12 |
| KR20100040876A (ko) | 2010-04-21 |
| KR20150086382A (ko) | 2015-07-27 |
| ATE503685T1 (de) | 2011-04-15 |
| EP2243702B1 (en) | 2012-02-08 |
| KR101558987B1 (ko) | 2015-10-12 |
| EP2167379A2 (en) | 2010-03-31 |
| US8864075B2 (en) | 2014-10-21 |
| WO2009004363A2 (en) | 2009-01-08 |
| GB0712552D0 (en) | 2007-08-08 |
| ATE544672T1 (de) | 2012-02-15 |
| CN101772452B (zh) | 2013-05-08 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| BRPI0813962A2 (pt) | Membros estruturais de compósito alongados e melhorias nestes | |
| GB0712549D0 (en) | Improvements in elongate composite structural members | |
| GB0906952D0 (en) | Aircraft assembly and spar | |
| EP2629973A4 (en) | GRADIENT NANOPArtICLEs-CARBON allotrope POLYMER COMPOSITE | |
| WO2009004362A3 (en) | Composite panel stiffener | |
| FR2990177B1 (fr) | Element structurel de vehicule ferroviaire, du type paroi longitudinale ou plancher | |
| EP2480710A4 (en) | MULTILAYER POLYMILIC ACID FILM WITH HIGH HUMIDITY BARRIER | |
| GB0708333D0 (en) | Composite structure | |
| DE502008000121D1 (de) | Fahrgastrückhaltevorrichtung für Fahrgeschäfte | |
| BR112012012263A2 (pt) | estruturas marítimas compósitas adaptadas para cnt | |
| RU2017146000A (ru) | Селективно ослабленные растянутые пленки | |
| BR112014016414A8 (pt) | unidade de processamento de material | |
| BR112013011271A8 (pt) | dispositivo para fixar uma guitarra | |
| BR112012014894A2 (pt) | processo para a fabricação de uma folha de folha de material de múltiplas camadas , folha de material de múltiplas camadas e uso das mesmas. | |
| FR3002877B1 (fr) | Procede de fabrication d'un materiau composite multicouche, materiau composite multicouche obtenu par le procede et pieces ou structures mecaniques realisees avec ledit materiau. | |
| FR2939102B1 (fr) | Structure rigide de mat d'aeronef equipee d'une extension de nervure pour la reprise du moment selon la direction longitudinale | |
| BRPI0920099A8 (pt) | Dispositivo de tranferência destinado à transferência de uma lona de reforço, e, processo de transferência | |
| ATE549255T1 (de) | Schrumpftunnel | |
| WO2013128054A3 (es) | Estructura de refuerzo integrada en estructura interna de aeronave en material compuesto | |
| BR112013025252B8 (pt) | Método e dispositivo para detectar parâmetros de uma trama de material transversal ou circular em uma máquina de processamento de material e uso do método | |
| BR112013027790A2 (pt) | conjunto para uma nacela de aeronave | |
| ATE539915T1 (de) | Transportaufbau mit rungen | |
| EP3524339C0 (en) | METHOD FOR INCREASE THE THICKNESS OF A CARBON NANOTUBE ARC STRUCTURE | |
| BR112013004412A2 (pt) | elemento de ajuste de cinto de segurança | |
| BR112013027562A2 (pt) | Estrutura de entrada de ar para uma nacela de motor turbojato |
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] |