JP2011520690A5 - - Google Patents
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- Publication number
- JP2011520690A5 JP2011520690A5 JP2011509724A JP2011509724A JP2011520690A5 JP 2011520690 A5 JP2011520690 A5 JP 2011520690A5 JP 2011509724 A JP2011509724 A JP 2011509724A JP 2011509724 A JP2011509724 A JP 2011509724A JP 2011520690 A5 JP2011520690 A5 JP 2011520690A5
- Authority
- JP
- Japan
- Prior art keywords
- composite
- layer
- filler
- base
- adhesive
- 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.)
- Granted
Links
- 239000002131 composite material Substances 0.000 claims description 31
- 239000010410 layer Substances 0.000 claims description 21
- 239000000945 filler Substances 0.000 claims description 18
- 239000004744 fabric Substances 0.000 claims description 14
- 239000000853 adhesive Substances 0.000 claims description 11
- 230000001070 adhesive effect Effects 0.000 claims description 11
- 238000000034 method Methods 0.000 claims description 9
- 239000000835 fiber Substances 0.000 claims description 8
- 230000002787 reinforcement Effects 0.000 claims description 8
- 239000012790 adhesive layer Substances 0.000 claims description 3
- 239000012783 reinforcing fiber Substances 0.000 claims description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 239000004593 Epoxy Substances 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 239000012779 reinforcing material Substances 0.000 description 1
- 239000011800 void material Substances 0.000 description 1
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US12/122,124 US8540833B2 (en) | 2008-05-16 | 2008-05-16 | Reinforced stiffeners and method for making the same |
| US12/122,124 | 2008-05-16 | ||
| PCT/US2009/044042 WO2009140555A2 (en) | 2008-05-16 | 2009-05-14 | Reinforced stiffeners and method for making the same |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2011520690A JP2011520690A (ja) | 2011-07-21 |
| JP2011520690A5 true JP2011520690A5 (enExample) | 2012-06-07 |
| JP5548192B2 JP5548192B2 (ja) | 2014-07-16 |
Family
ID=41171228
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2011509724A Active JP5548192B2 (ja) | 2008-05-16 | 2009-05-14 | 強化補強材を作製する方法 |
Country Status (8)
| Country | Link |
|---|---|
| US (2) | US8540833B2 (enExample) |
| EP (1) | EP2303560B1 (enExample) |
| JP (1) | JP5548192B2 (enExample) |
| KR (1) | KR101675167B1 (enExample) |
| CN (1) | CN102026798B (enExample) |
| ES (1) | ES2405583T3 (enExample) |
| RU (1) | RU2514747C2 (enExample) |
| WO (1) | WO2009140555A2 (enExample) |
Families Citing this family (77)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9586699B1 (en) | 1999-08-16 | 2017-03-07 | Smart Drilling And Completion, Inc. | Methods and apparatus for monitoring and fixing holes in composite aircraft |
| US9625361B1 (en) | 2001-08-19 | 2017-04-18 | Smart Drilling And Completion, Inc. | Methods and apparatus to prevent failures of fiber-reinforced composite materials under compressive stresses caused by fluids and gases invading microfractures in the materials |
| US8540833B2 (en) | 2008-05-16 | 2013-09-24 | The Boeing Company | Reinforced stiffeners and method for making the same |
| CA2765138A1 (en) * | 2009-06-11 | 2010-12-16 | Saab Ab | Nano-reinforced radius filler for an aircraft structure and a method of producing an aircraft structure comprising such filler |
| BRPI0924616A2 (pt) | 2009-06-11 | 2016-03-01 | Saab Ab | junta compósita para estrutura de avião |
| FR2953092B1 (fr) * | 2009-11-25 | 2011-12-16 | European Aeronautic Defence & Space Co Eads France | Raidisseur electro-structural en materiau composite |
| ES2364615B1 (es) * | 2010-02-17 | 2012-09-17 | Airbus Operations, S.L. | Proceso de fabricación de larguerillos para la estructura de una aeronave y producto obtenido. |
| DE102010003114A1 (de) * | 2010-03-22 | 2011-09-22 | Repower Systems Ag | Stegverbindung |
| GB201016279D0 (en) * | 2010-09-28 | 2010-11-10 | Airbus Operations Ltd | Stiffener run-out |
| US9140283B2 (en) * | 2010-11-12 | 2015-09-22 | Raytheon Company | Adhesively-bonded structural composite joint utilizing shoulder-centered sleeves |
| GB2486231B (en) * | 2010-12-07 | 2013-04-03 | Gkn Aerospace Services Ltd | Composite structure |
| FR2970432B1 (fr) | 2011-01-19 | 2013-02-08 | Skf Aerospace France | Ferrure multi-branche en materiau composite et procede de fabrication d'une telle ferrure multi-branche |
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| US8776375B2 (en) * | 2011-05-19 | 2014-07-15 | The Boeing Company | Aircraft structure for high capacity pull off |
| CA2837862C (en) * | 2011-06-03 | 2018-10-23 | Cytec Technology Corp. | Resin coated radius fillers and system and method of making the same |
| FR2977186B1 (fr) * | 2011-07-01 | 2014-08-22 | Daher Aerospace | Procede de renforcement local d'un panneau composite a renfort fibreux et panneau obtenu par un tel procede |
| JP6009236B2 (ja) * | 2011-08-10 | 2016-10-19 | ザ・ボーイング・カンパニーThe Boeing Company | 複合ストリンガの高能力プルオフのための垂直積層ヌードル |
| US8591685B2 (en) * | 2011-10-27 | 2013-11-26 | The Boeing Company | Method and apparatus for producing composite fillers |
| FR2984274B1 (fr) * | 2011-12-15 | 2014-06-27 | Airbus Operations Sas | Poutre securisee, en particulier cadre fort de fuselage, ainsi que fuselage d'aeronef equipe de tels cadres |
| US8703269B2 (en) | 2012-02-14 | 2014-04-22 | Gulfstream Aerospace Corporation | Reinforced composite structures for aircrafts and methods for making the same |
| US9359078B2 (en) * | 2012-03-28 | 2016-06-07 | B/E Aerospace, Inc. | Aircraft galley monument structure |
| EP2666622B1 (en) | 2012-05-22 | 2017-04-12 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | Skin-stiffener transition assembly, method of manufacture and application of said skin-stiffener transition assembly |
| US9352822B2 (en) * | 2012-05-30 | 2016-05-31 | The Boeing Company | Bonded composite airfoil |
| US8758879B2 (en) | 2012-06-24 | 2014-06-24 | The Boeing Company | Composite hat stiffener, composite hat-stiffened pressure webs, and methods of making the same |
| US9616594B2 (en) * | 2012-08-06 | 2017-04-11 | The Boeing Company | Radius fillers for composite structures, composite structures that include radius fillers, and systems and methods of forming the same |
| JP5945209B2 (ja) * | 2012-10-25 | 2016-07-05 | 株式会社Ihi | 円筒状ケース及び円筒状ケースの製造方法 |
| US9370921B2 (en) * | 2012-11-01 | 2016-06-21 | The Boeing Company | Composite radius fillers and methods of forming the same |
| US9327470B1 (en) * | 2012-12-05 | 2016-05-03 | The Boeing Company | Variable-radius laminated radius filler and system and method for manufacturing same |
| US8973871B2 (en) * | 2013-01-26 | 2015-03-10 | The Boeing Company | Box structures for carrying loads and methods of making the same |
| US9463880B2 (en) * | 2013-02-07 | 2016-10-11 | The Boeing Company | Method and system of making composite structures having gap fillers with chopped fiber material |
| US9205634B2 (en) * | 2013-05-16 | 2015-12-08 | The Boeing Company | Composite structure and method |
| CN103434638A (zh) * | 2013-09-16 | 2013-12-11 | 哈尔滨工业大学 | 复合材料机翼中梁与加强肋的混合连接方法 |
| US10144203B2 (en) * | 2013-10-03 | 2018-12-04 | The Boeing Company | Pre-formed thermoplastic filler for thermoset structure |
| CN103522555B (zh) * | 2013-10-25 | 2016-05-25 | 重庆大学 | 一种复合材料工字梁的整体成型制造方法 |
| ES2786124T3 (es) | 2013-12-27 | 2020-10-08 | Airbus Operations Sl | Método de fabricación de un elemento de refuerzo |
| US9827710B2 (en) | 2014-02-04 | 2017-11-28 | The Boeing Company | Radius filler and method of manufacturing same |
| US9566739B2 (en) * | 2014-02-18 | 2017-02-14 | The Boeing Company | Composite filler |
| US10065366B2 (en) * | 2014-05-27 | 2018-09-04 | The Boeing Company | Folded composite filler |
| US10040274B2 (en) | 2014-06-17 | 2018-08-07 | The Boeing Company | Pre-filled radius layups |
| US9475256B2 (en) * | 2014-07-10 | 2016-10-25 | The Boeing Company | Composite filler |
| US9440414B2 (en) | 2014-07-25 | 2016-09-13 | The Boeing Company | Fabric jacketed unidirectional noodle |
| US9517606B2 (en) * | 2014-08-06 | 2016-12-13 | The Boeing Company | Composite structure and method of forming thereof |
| US10232572B2 (en) * | 2014-08-27 | 2019-03-19 | The Boeing Company | Composite filler forming apparatus |
| BE1022462B1 (fr) * | 2014-09-12 | 2016-04-07 | Techspace Aero S.A. | Carter composite de compresseur basse pression de turbomachine axiale |
| US10449734B2 (en) * | 2014-09-18 | 2019-10-22 | Alenia Aermacchi S.P.A. | Methods for manufacturing elongated structural elements of composite material |
| US9592651B2 (en) * | 2014-09-30 | 2017-03-14 | The Boeing Company | Composite structures having reduced area radius fillers and methods of forming the same |
| US9637354B2 (en) | 2014-10-20 | 2017-05-02 | The Boeing Company | Devices and methods for handling radius fillers |
| US9850102B2 (en) | 2014-10-20 | 2017-12-26 | The Boeing Company | Devices and methods for handling radius fillers |
| MA40753A (fr) * | 2014-10-30 | 2017-09-06 | Lm Wp Patent Holding As | Fabrication d'une bande de cisaillement en forme de i |
| US9914549B2 (en) | 2015-02-23 | 2018-03-13 | The Boeing Company | Method, system and apparatus for assembling a composite wing skin with stiffeners |
| US10513101B2 (en) * | 2015-03-13 | 2019-12-24 | The Boeing Company | Apparatuses and methods for creating layered tape composite structures |
| JP6502719B2 (ja) * | 2015-03-26 | 2019-04-17 | 株式会社Subaru | 航空機構造体、航空機構造体の製造方法及び航空機構造体の設計情報の作成方法 |
| FR3036060B1 (fr) | 2015-05-12 | 2017-04-28 | Aircelle Sa | Piece en materiau composite comportant un raidisseur en t et procede de fabrication d'une telle piece |
| RU2595692C1 (ru) * | 2015-05-18 | 2016-08-27 | Акционерное общество "Обнинское научно-производственное предприятие "Технология" им. А.Г. Ромашина" (АО "ОНПП "Технология" им.А.Г.Ромашина") | Узел соединения конструкций из композиционных материалов |
| EP3100852B1 (en) * | 2015-06-03 | 2017-11-15 | Tusas-Türk Havacilik Ve Uzay Sanayii A.S. | A curved laminated structure |
| RU2599661C1 (ru) * | 2015-07-28 | 2016-10-10 | Акционерное общество "Обнинское научно-производственное предприятие "Технология" им. А.Г. Ромашина" | Способ изготовления композитного элемента жесткости |
| US9463864B1 (en) | 2015-07-28 | 2016-10-11 | The Boeing Company | Radius filler containing vertical ply stacks and thin plies |
| US20170029577A1 (en) | 2015-07-29 | 2017-02-02 | The Boeing Company | Noodle Comprised of a Matrix of Discontinuous Filaments |
| US20170036375A1 (en) * | 2015-08-07 | 2017-02-09 | Hexcel Corporation | Multi-sectional composite tooling |
| US9809297B2 (en) * | 2015-08-26 | 2017-11-07 | The Boeing Company | Structures containing stiffeners having transition portions |
| KR101743091B1 (ko) * | 2015-10-20 | 2017-06-02 | 주식회사 영원무역 | 원단접합 구조 및 이를 포함하는 원단가공품 |
| FR3043355B1 (fr) * | 2015-11-06 | 2017-12-22 | Safran | Procede de fabrication d'une piece en materiau composite comprenant un corps solidaire d'une ou plusieurs plates-formes |
| RU2613912C1 (ru) * | 2016-01-21 | 2017-03-22 | Владимир Александрович Грибановский | Способ изготовления усиленного элемента жесткости из композиционного материала |
| US10329030B2 (en) * | 2016-03-04 | 2019-06-25 | The Boeing Company | Conductive radius filler system and method |
| CN106182806A (zh) * | 2016-07-11 | 2016-12-07 | 威海光威复合材料股份有限公司 | 纤维增强复合材料横梁的制备方法 |
| US10668683B2 (en) * | 2016-09-15 | 2020-06-02 | The Boeing Company | Gap fillers for composite materials |
| US10046525B2 (en) | 2016-09-30 | 2018-08-14 | The Boeing Company | Advanced variable radius laminated composite radius filler |
| RU2660848C1 (ru) * | 2017-04-24 | 2018-07-10 | Владимир Александрович Грибановский | Способ изготовления усиленного элемента жёсткости из композиционного материала |
| EP3658767B1 (en) * | 2017-07-27 | 2022-12-14 | Vestas Wind Systems A/S | Web foot for a shear web |
| US10875625B2 (en) * | 2017-08-23 | 2020-12-29 | The Boeing Company | Co-cured spar and stringer center wing box |
| US10927710B2 (en) | 2018-09-26 | 2021-02-23 | Raytheon Technologies Corporation | Blade outer air seal laminate T-joint |
| US11180238B2 (en) * | 2018-11-19 | 2021-11-23 | The Boeing Company | Shear ties for aircraft wing |
| ES2906760T3 (es) * | 2019-02-19 | 2022-04-20 | Muelles Y Ballestas Hispano Alemanas Projects S L | Panel rigidizado en materiales compuestos y procedimiento de fabricación de dicho panel |
| JP7322588B2 (ja) * | 2019-08-19 | 2023-08-08 | 株式会社豊田自動織機 | 繊維構造体及び繊維強化複合材 |
| CN112895520A (zh) * | 2021-01-15 | 2021-06-04 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | 飞机舵面复合材料双向加强结构及成型方法 |
| EP4552971A1 (en) * | 2023-11-07 | 2025-05-14 | Airbus Operations, S.L.U. | Y-shaped stringers made of composite material |
| DE102024114446A1 (de) * | 2024-05-23 | 2025-11-27 | Everllence Se | Mehrstufiger Verdichter |
Family Cites Families (46)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3025208A (en) * | 1957-08-01 | 1962-03-13 | Robert F Geiger | Apparatus for metal adhesive bonding |
| US3071217A (en) * | 1960-01-15 | 1963-01-01 | Avro Aircraft Ltd | Vibration damping in sheet metal structures |
| US3578544A (en) * | 1968-01-18 | 1971-05-11 | Phillips Petroleum Co | Reinforced microporous laminates |
| US4113910A (en) * | 1977-04-27 | 1978-09-12 | Rockwell International Corporation | Composite load coupler for reinforcing composite structural joints |
| US4151031A (en) * | 1977-07-05 | 1979-04-24 | General Dynamics Corporation | Apparatus for continuously forming composite shapes |
| US4109435A (en) * | 1977-08-26 | 1978-08-29 | Rockwell International Corporation | Composite structural joint and method of fabrication thereof |
| US4331495A (en) * | 1978-01-19 | 1982-05-25 | Rockwell International Corporation | Method of fabricating a reinforced composite structure |
| US4256790A (en) * | 1978-01-19 | 1981-03-17 | Rockwell International Corporation | Reinforced composite structure and method of fabrication thereof |
| US4206895A (en) * | 1978-03-30 | 1980-06-10 | Olez Nejat A | Loop-tension joint |
| US4331723A (en) | 1980-11-05 | 1982-05-25 | The Boeing Company | Advanced composite |
| US4715560A (en) * | 1983-03-14 | 1987-12-29 | Lear Fan Limited | Composite cruciform structure for joining intersecting structural members of an airframe and the like |
| US4966802A (en) * | 1985-05-10 | 1990-10-30 | The Boeing Company | Composites made of fiber reinforced resin elements joined by adhesive |
| US4968802A (en) * | 1985-10-01 | 1990-11-06 | Eli Lilly And Company | Process of making alkoxy cycloalkanol esters of dihydrolysergic acid |
| DE3614618A1 (de) * | 1986-04-30 | 1987-11-05 | Messerschmitt Boelkow Blohm | Schalenstruktur aus faserverstaerktem kunststoff |
| US4783228A (en) * | 1986-07-03 | 1988-11-08 | Lockheed Corporation | Method of bonding metal skins to internal support structures |
| JPH0436905Y2 (enExample) * | 1987-02-03 | 1992-08-31 | ||
| JPH0790605B2 (ja) * | 1987-09-16 | 1995-10-04 | 三菱重工業株式会社 | 複合材製桁材のジョイント部補強用繊維構造体およびその製造方法 |
| US5026595A (en) | 1989-11-09 | 1991-06-25 | Techniweave, Inc. | Woven gap filler for use in the lay-up of composite plastic structural units |
| US5262595A (en) * | 1990-07-25 | 1993-11-16 | Ngk Insulators, Ltd. | Dielectric ceramic body including TiO2 dispersion in crystallized cordierite matrix phase, method of producing the same, and circuit board using the same |
| JPH05459A (ja) * | 1991-01-25 | 1993-01-08 | Hitachi Ltd | 繊維強化樹脂複合材料を用いた構造部材 |
| JP3314561B2 (ja) * | 1994-11-30 | 2002-08-12 | 松下電器産業株式会社 | スクロール圧縮機 |
| US5556496A (en) * | 1995-01-10 | 1996-09-17 | Sumerak; Joseph E. | Pultrusion method for making variable cross-section thermoset articles |
| US5556565A (en) * | 1995-06-07 | 1996-09-17 | The Boeing Company | Method for composite welding using a hybrid metal webbed composite beam |
| US5842317A (en) * | 1996-02-07 | 1998-12-01 | Mcdonnell Douglas Corporation | Crack arresting structure |
| US5833786A (en) * | 1996-05-16 | 1998-11-10 | The Boeing Company | Titanium radius filler for use in composite interfaces |
| US5639535A (en) * | 1996-06-06 | 1997-06-17 | The Boeing Company | Composite interleaving for composite interfaces |
| US5848767A (en) * | 1996-08-05 | 1998-12-15 | The Boeing Company | One piece spacecraft frame |
| JP3400399B2 (ja) * | 2000-01-11 | 2003-04-28 | 株式会社ジャムコ | Frp製h形部材の連続成形装置 |
| US6562436B2 (en) * | 2000-02-25 | 2003-05-13 | The Boeing Company | Laminated composite radius filler |
| GB0022589D0 (en) | 2000-09-14 | 2000-11-01 | Bae Systems Plc | Composite joints |
| US7052572B2 (en) * | 2001-08-01 | 2006-05-30 | Fuji Jukogyo Kabushiki Kaisha | Method for manufacturing a structure |
| US6648273B2 (en) * | 2001-10-30 | 2003-11-18 | The Boeing Company | Light weight and high strength fuselage |
| US20030175520A1 (en) * | 2002-03-13 | 2003-09-18 | Grutta James T. | Formed composite structural members and methods and apparatus for making the same |
| JP2004076805A (ja) * | 2002-08-12 | 2004-03-11 | Toyota Motor Corp | 衝撃エネルギー吸収用複合材料及び衝撃エネルギー吸収方法 |
| US20040035979A1 (en) * | 2002-08-23 | 2004-02-26 | Mccoskey William Robert | Integrally stiffened axial load carrying skin panels for primary aircraft structure and closed loop manufacturing methods for making the same |
| FR2844742B1 (fr) * | 2002-09-25 | 2005-04-29 | Pechiney Rhenalu | Feuilles composites stratifiees aluminium-fibres de verre |
| 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 |
| US7159822B2 (en) * | 2004-04-06 | 2007-01-09 | The Boeing Company | Structural panels for use in aircraft fuselages and other structures |
| US7134629B2 (en) * | 2004-04-06 | 2006-11-14 | The Boeing Company | Structural panels for use in aircraft fuselages and other structures |
| US7080805B2 (en) * | 2004-05-05 | 2006-07-25 | The Boeing Company | Stiffened structures and associated methods |
| CA2616455C (en) * | 2005-07-25 | 2016-02-09 | Tlv Co., Ltd. | Device management method, analysis system used for the device management method, analysis data structure, and maintenance inspection support apparatus used for the device management method |
| US7469735B2 (en) * | 2005-08-03 | 2008-12-30 | The Boeing Corporation | Composite structural element fabricating device and method |
| US20070095475A1 (en) * | 2005-11-01 | 2007-05-03 | L&L Products, Inc. | Adhesive material and method of using same |
| CN101394988B (zh) | 2006-03-15 | 2010-09-29 | 东丽株式会社 | 预成型体的制造方法及制造装置 |
| JP4977543B2 (ja) | 2007-07-20 | 2012-07-18 | 日本電気通信システム株式会社 | 制御装置、制御システム、制御方法及び制御プログラム |
| US8540833B2 (en) | 2008-05-16 | 2013-09-24 | The Boeing Company | Reinforced stiffeners and method for making the same |
-
2008
- 2008-05-16 US US12/122,124 patent/US8540833B2/en active Active
-
2009
- 2009-05-14 WO PCT/US2009/044042 patent/WO2009140555A2/en not_active Ceased
- 2009-05-14 ES ES09747636T patent/ES2405583T3/es active Active
- 2009-05-14 EP EP09747636A patent/EP2303560B1/en active Active
- 2009-05-14 RU RU2010149945/05A patent/RU2514747C2/ru active
- 2009-05-14 JP JP2011509724A patent/JP5548192B2/ja active Active
- 2009-05-14 CN CN2009801177612A patent/CN102026798B/zh active Active
- 2009-05-14 KR KR1020107020519A patent/KR101675167B1/ko active Active
-
2013
- 2013-06-27 US US13/928,760 patent/US9981444B2/en active Active
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