JP2014510879A5 - - Google Patents
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- Publication number
- JP2014510879A5 JP2014510879A5 JP2013550467A JP2013550467A JP2014510879A5 JP 2014510879 A5 JP2014510879 A5 JP 2014510879A5 JP 2013550467 A JP2013550467 A JP 2013550467A JP 2013550467 A JP2013550467 A JP 2013550467A JP 2014510879 A5 JP2014510879 A5 JP 2014510879A5
- Authority
- JP
- Japan
- Prior art keywords
- preform
- shell
- continuous
- fiber
- recess
- 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
- 239000000835 fiber Substances 0.000 claims description 34
- 239000002131 composite material Substances 0.000 claims description 27
- 238000000034 method Methods 0.000 claims description 13
- 239000003351 stiffener Substances 0.000 claims description 10
- 229920005989 resin Polymers 0.000 claims description 8
- 239000011347 resin Substances 0.000 claims description 8
- 230000002787 reinforcement Effects 0.000 claims description 7
- 238000009954 braiding Methods 0.000 claims description 5
- 239000004744 fabric Substances 0.000 claims description 4
- 239000012783 reinforcing fiber Substances 0.000 claims description 4
- 238000002347 injection Methods 0.000 claims description 2
- 239000007924 injection Substances 0.000 claims description 2
- 238000004519 manufacturing process Methods 0.000 claims description 2
- 239000002952 polymeric resin Substances 0.000 claims description 2
- 230000003014 reinforcing effect Effects 0.000 claims description 2
- 229920003002 synthetic resin Polymers 0.000 claims description 2
- 230000007704 transition Effects 0.000 claims description 2
- 235000002597 Solanum melongena Nutrition 0.000 claims 1
- 244000061458 Solanum melongena Species 0.000 claims 1
- 239000012779 reinforcing material Substances 0.000 claims 1
- 239000000463 material Substances 0.000 description 1
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US13/012,162 | 2011-01-24 | ||
| US13/012,162 US8636252B2 (en) | 2010-06-25 | 2011-01-24 | Composite structures having integrated stiffeners with smooth runouts and method of making the same |
| PCT/US2011/063658 WO2012102789A1 (en) | 2011-01-24 | 2011-12-07 | Composite structures having integrated stiffeners with smooth runouts and method of making the same |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2014510879A JP2014510879A (ja) | 2014-05-01 |
| JP2014510879A5 true JP2014510879A5 (enExample) | 2014-12-04 |
| JP6005661B2 JP6005661B2 (ja) | 2016-10-12 |
Family
ID=45418809
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2013550467A Active JP6005661B2 (ja) | 2011-01-24 | 2011-12-07 | 滑らかなランナウトを持つ一体型補剛材を有する複合構造物およびその作製方法 |
Country Status (9)
| Country | Link |
|---|---|
| US (2) | US8636252B2 (enExample) |
| EP (2) | EP3533594B1 (enExample) |
| JP (1) | JP6005661B2 (enExample) |
| KR (1) | KR101900967B1 (enExample) |
| CN (1) | CN103370185B (enExample) |
| CA (1) | CA2822577C (enExample) |
| ES (1) | ES2784175T3 (enExample) |
| PT (1) | PT2668024T (enExample) |
| WO (1) | WO2012102789A1 (enExample) |
Families Citing this family (76)
| 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 |
| DE102009060695A1 (de) * | 2009-12-29 | 2011-07-07 | Airbus Operations GmbH, 21129 | Flugzeugrumpf und Hautfeld |
| US8628717B2 (en) | 2010-06-25 | 2014-01-14 | The Boeing Company | Composite structures having integrated stiffeners and method of making the same |
| US8940213B2 (en) | 2010-06-25 | 2015-01-27 | The Boeing Company | Resin infusion of composite parts using a perforated caul sheet |
| US9682514B2 (en) | 2010-06-25 | 2017-06-20 | The Boeing Company | Method of manufacturing resin infused composite parts using a perforated caul sheet |
| 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 |
| GB201020152D0 (en) * | 2010-11-29 | 2011-01-12 | Airbus Uk Ltd | Aircraft panel structure and aircraft panel structure manufacturing method for alleviation of stress |
| SE537320C2 (sv) * | 2011-06-16 | 2015-04-07 | Bassoe Technology Ab | Borrtorn med förstyvat skal samt havsplattform |
| US8651419B2 (en) | 2011-07-18 | 2014-02-18 | The Boeing Company | Flexible truss frame and method of making the same |
| GB201120707D0 (en) | 2011-12-01 | 2012-01-11 | Airbus Operations Ltd | Leading edge structure |
| JP5991786B2 (ja) * | 2012-07-20 | 2016-09-14 | 難波プレス工業株式会社 | 補強リブ付きプレス成形品及びその製造方法 |
| ES2619478T3 (es) * | 2012-10-31 | 2017-06-26 | Airbus Operations S.L. | Larguerillo |
| GB201301766D0 (en) * | 2013-01-31 | 2013-03-20 | Airbus Operations Ltd | Structural assembly joint |
| GB201307066D0 (en) * | 2013-04-18 | 2013-05-29 | Airbus Operations Ltd | Winglet and braided composite spar |
| EP2989003A4 (en) * | 2013-04-25 | 2016-12-07 | Saab Ab | EXPIRATION OF A STAMPING ELEMENT |
| US10308343B2 (en) * | 2013-05-30 | 2019-06-04 | The Boeing Company | Composite hat stiffener |
| US9395339B2 (en) * | 2013-08-26 | 2016-07-19 | The Boeing Comapany | Apparatus for non-destructive inspection of stringers |
| US10086922B2 (en) * | 2013-11-15 | 2018-10-02 | The Boeing Company | Low stress stiffener runout in Pi bonded structure |
| US10272619B2 (en) | 2014-05-19 | 2019-04-30 | The Boeing Company | Manufacture of a resin infused one-piece composite truss structure |
| US9511540B2 (en) * | 2014-08-07 | 2016-12-06 | GM Global Technology Operations LLC | Process for securing a micro-truss structure to a panel |
| US10086534B2 (en) | 2014-10-17 | 2018-10-02 | The Boeing Company | Multifunctional mandrel end cap and method |
| US10040537B2 (en) * | 2015-01-15 | 2018-08-07 | The Boeing Company | Laminate composite wing structures |
| FR3036684B1 (fr) * | 2015-05-29 | 2019-05-10 | Stelia Aerospace | Raidisseur monobloc pour structure aeronautique |
| JP6292185B2 (ja) * | 2015-07-07 | 2018-03-14 | 株式会社豊田自動織機 | 繊維積層体、繊維積層体の製造方法、及び繊維強化複合材 |
| US9809297B2 (en) * | 2015-08-26 | 2017-11-07 | The Boeing Company | Structures containing stiffeners having transition portions |
| CN204915569U (zh) * | 2015-09-17 | 2015-12-30 | 延锋彼欧宁波汽车外饰系统有限公司 | 一种保险杠总成 |
| EP3173223A1 (en) * | 2015-11-27 | 2017-05-31 | Airbus Operations GmbH | A method for manufacturing an aircraft structure component |
| NL2015927B1 (en) * | 2015-12-08 | 2017-06-28 | Atg Europe B V | Composite grid structure. |
| US10273935B2 (en) | 2016-01-15 | 2019-04-30 | General Electric Company | Rotor blades having structural skin insert and methods of making same |
| US20170274577A1 (en) * | 2016-03-24 | 2017-09-28 | The Boeing Company | Composite structures with stiffeners and method of making the same |
| DE102016208782A1 (de) * | 2016-05-20 | 2017-11-23 | Continental Teves Ag & Co. Ohg | Verfahren zum Ummanteln einer elektrischen Einheit und elektrisches Bauelement |
| DE102016208783A1 (de) * | 2016-05-20 | 2017-11-23 | Continental Teves Ag & Co. Ohg | Verfahren zum Ummanteln einer elektrischen Einheit und elektrisches Bauelement |
| US9707898B1 (en) * | 2016-07-11 | 2017-07-18 | Ford Global Technologies, Llc | Extruded multi-layer molded running board |
| US10814602B2 (en) * | 2016-09-14 | 2020-10-27 | The Boeing Company | Method of producing cored composite parts |
| WO2018061281A1 (ja) | 2016-09-29 | 2018-04-05 | 株式会社Subaru | 複合材構造体及び複合材構造体の製造方法 |
| US10248158B2 (en) * | 2016-10-21 | 2019-04-02 | Microsoft Technology Licensing, Llc | Enclosure assembly and monitor device including same |
| US10365180B2 (en) * | 2016-12-15 | 2019-07-30 | The Boeing Company | Non-destructive leak source detection and identification for complex bagging in conjunction with flow measurement systems |
| CN107052715B (zh) * | 2017-03-30 | 2019-03-01 | 陕西飞机工业(集团)有限公司 | 一种大型机翼整体壁板数控加工方法 |
| CN108688192B (zh) * | 2017-04-12 | 2020-11-03 | 深圳市泰格尔航天航空科技有限公司 | 一种c型梁复合材料成型工装及复合材料c型梁成型方法 |
| EP3428062A1 (en) * | 2017-07-11 | 2019-01-16 | Airbus Operations GmbH | A leading edge structure for a flow control system of an aircraft |
| EP3659774B1 (en) * | 2017-07-25 | 2023-05-31 | Subaru Corporation | Composite material molding jig and composite material molding method |
| US10974806B2 (en) * | 2017-10-05 | 2021-04-13 | Gulfstream Aerospace Corporation | Unified canopies for aircraft |
| US11519291B2 (en) * | 2018-01-11 | 2022-12-06 | Raytheon Technologies Corporation | Integral stiffening rail for braided composite gas turbine engine component |
| US10669005B2 (en) | 2018-02-27 | 2020-06-02 | The Boeing Company | Solid laminate stringer |
| WO2019171683A1 (ja) * | 2018-03-05 | 2019-09-12 | 日本飛行機株式会社 | ハニカムサンドイッチ複合材の成形方法およびこれに用いる治具 |
| CN108438199A (zh) * | 2018-03-23 | 2018-08-24 | 太原科技大学 | 一种提高飞机蒙皮承载力的复合材料加强件 |
| JP6692388B2 (ja) * | 2018-06-11 | 2020-05-13 | 本田技研工業株式会社 | 車体後部構造 |
| US11433990B2 (en) * | 2018-07-09 | 2022-09-06 | Rohr, Inc. | Active laminar flow control system with composite panel |
| US11485468B2 (en) * | 2018-09-27 | 2022-11-01 | The Boeing Company | Thermoplastic multi-grid overmolded/co-consolidated aircraft fuselage structure |
| US10994823B2 (en) * | 2018-10-11 | 2021-05-04 | The Boeing Company | Beaded panels and method of forming beaded panels |
| US11052617B2 (en) | 2018-11-01 | 2021-07-06 | The Boeing Company | Fabrication of plank stringers |
| US11491750B2 (en) * | 2019-01-07 | 2022-11-08 | Varial Surf Technology, Inc. | Moldless vacuum infusion process |
| GB2581835A (en) * | 2019-03-01 | 2020-09-02 | Airbus Operations Ltd | Composite stiffener |
| CN113710446B (zh) * | 2019-04-18 | 2023-11-14 | 帝人碳纤维欧洲有限公司 | 楔形填料预成型坯 |
| 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 |
| 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 |
| 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 |
| WO2020229501A1 (en) * | 2019-05-14 | 2020-11-19 | Airbus Operations Limited | Aircraft panel assembly |
| CN110370676B (zh) * | 2019-07-11 | 2021-05-25 | 航天海鹰(镇江)特种材料有限公司 | 一种高强度软性工装实现l型加强筋与c型框结构复材制件共固化的方法 |
| US10994500B1 (en) | 2019-11-19 | 2021-05-04 | The Boeing Company | System and method for a composite panel |
| US11667371B2 (en) * | 2020-04-03 | 2023-06-06 | The Boeing Company | Composite materials having reinforced access openings |
| CA3122789C (en) * | 2020-07-29 | 2024-06-11 | The Boeing Company | Bead-stiffened movable surfaces |
| US11760463B2 (en) | 2020-07-29 | 2023-09-19 | The Boeing Company | Structure having net-area-tension joint |
| CA3120840A1 (en) | 2020-07-29 | 2022-01-29 | The Boeing Company | Wing assembly having wing joints joining outer wing structures to centerwing structure |
| US11643184B2 (en) * | 2020-07-29 | 2023-05-09 | The Boeing Company | Wing assembly having discretely stiffened composite wing panels |
| JP7426492B2 (ja) * | 2020-08-19 | 2024-02-01 | 川崎重工業株式会社 | 複合材料製パネル構造体およびその製造方法 |
| GB202015876D0 (en) * | 2020-10-07 | 2020-11-18 | Lm Wind Power As | A precured fibrous strip for a load-carrying structure for a wind turbine blade |
| CA3105549A1 (en) | 2020-10-22 | 2022-04-22 | Transtex Inc. | Ribbed aerodynamic skirt panel and assembly thereof |
| CN113199786B (zh) * | 2021-04-29 | 2023-09-26 | 上海电气风电集团股份有限公司 | 风机叶片用腹板的制造方法 |
| US11794560B2 (en) * | 2021-08-06 | 2023-10-24 | GM Global Technology Operations LLC | Composite component with integrated conduit |
| GB2612957A (en) * | 2021-11-08 | 2023-05-24 | Airbus Operations Ltd | Stiffener with core and shell |
| GB2615755A (en) * | 2022-02-15 | 2023-08-23 | Airbus Operations Ltd | Fuel tank stringer with flow passage |
| DE102022110887A1 (de) * | 2022-05-03 | 2023-11-09 | Premium Aerotec Gmbh | Verfahren zum Herstellen eines Bauteils aus einem Verbundmaterial mit lokal erhöhter DickeVerfahren zum Herstellen eines Bauteils aus einem Verbundmaterial mit lokal erhöhter Dicke |
| US11933046B1 (en) * | 2022-07-14 | 2024-03-19 | Anthony Attalla | Stiff wall panel assembly for a building structure and associated method(s) |
| US12397896B2 (en) | 2022-12-21 | 2025-08-26 | Rapidflight Holdings, Llc | Additive manufactured aircraft structure with reinforcements and method of making the same |
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| US2709973A (en) * | 1952-11-13 | 1955-06-07 | Pullman Standard Car Mfg Co | Railway car side wall |
| US3339333A (en) * | 1965-04-05 | 1967-09-05 | Metcom Products Co | Back-up tab for siding |
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| FR2922516B1 (fr) * | 2007-10-18 | 2010-04-16 | Airbus France | Eclissage de raidisseurs en omega au niveau d'une jonction circonferentielle d'un fuselage d'avion |
| DE102008059653B4 (de) * | 2008-11-28 | 2015-07-09 | Gkn Aerospace Services Ltd. | Flächiges Bauteil eines Fluggerätes und Verfahren zu dessen Herstellung |
| GB0912015D0 (en) | 2009-07-10 | 2009-08-19 | Airbus Operations Ltd | Stringer |
| ES2392236B1 (es) * | 2010-01-15 | 2013-10-09 | Airbus Operations, S.L. | Componente de aeronave con paneles rigidizados con larguerillos. |
| 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 |
| US9682514B2 (en) | 2010-06-25 | 2017-06-20 | The Boeing Company | Method of manufacturing resin infused 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 |
| US8940213B2 (en) | 2010-06-25 | 2015-01-27 | The Boeing Company | Resin infusion of composite parts using a perforated caul sheet |
| ES2398985B1 (es) * | 2011-03-14 | 2014-02-14 | Airbus Operations S.L. | Dispositivos de transferencia de carga en la terminación de un larguerillo. |
-
2011
- 2011-01-24 US US13/012,162 patent/US8636252B2/en active Active
- 2011-12-07 EP EP19170308.1A patent/EP3533594B1/en active Active
- 2011-12-07 JP JP2013550467A patent/JP6005661B2/ja active Active
- 2011-12-07 EP EP11802243.3A patent/EP2668024B1/en active Active
- 2011-12-07 PT PT118022433T patent/PT2668024T/pt unknown
- 2011-12-07 CN CN201180065886.2A patent/CN103370185B/zh active Active
- 2011-12-07 WO PCT/US2011/063658 patent/WO2012102789A1/en not_active Ceased
- 2011-12-07 KR KR1020137013813A patent/KR101900967B1/ko active Active
- 2011-12-07 CA CA2822577A patent/CA2822577C/en active Active
- 2011-12-07 ES ES11802243T patent/ES2784175T3/es active Active
-
2013
- 2013-12-27 US US14/141,433 patent/US9440402B2/en active Active
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