JP2014500172A5 - - Google Patents
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- Publication number
- JP2014500172A5 JP2014500172A5 JP2013531909A JP2013531909A JP2014500172A5 JP 2014500172 A5 JP2014500172 A5 JP 2014500172A5 JP 2013531909 A JP2013531909 A JP 2013531909A JP 2013531909 A JP2013531909 A JP 2013531909A JP 2014500172 A5 JP2014500172 A5 JP 2014500172A5
- Authority
- JP
- Japan
- Prior art keywords
- angle
- oriented
- reinforcing fibers
- web
- base
- 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
- 239000012783 reinforcing fiber Substances 0.000 claims description 18
- 239000003351 stiffener Substances 0.000 claims description 12
- 239000000835 fiber Substances 0.000 claims description 11
- 238000005452 bending Methods 0.000 claims description 2
- 229920000049 Carbon (fiber) Polymers 0.000 claims 1
- 239000004917 carbon fiber Substances 0.000 claims 1
- 239000002131 composite material Substances 0.000 claims 1
- 239000011159 matrix material Substances 0.000 claims 1
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims 1
- 229920000642 polymer Polymers 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 6
- 239000004753 textile Substances 0.000 description 2
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US12/897,742 US8720825B2 (en) | 2005-03-31 | 2010-10-04 | Composite stiffeners for aerospace vehicles |
| US12/897,742 | 2010-10-04 | ||
| PCT/US2011/054206 WO2012047751A1 (en) | 2010-10-04 | 2011-09-30 | Composite stiffeners for aerospace vehicles |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2014500172A JP2014500172A (ja) | 2014-01-09 |
| JP2014500172A5 true JP2014500172A5 (enExample) | 2016-05-19 |
| JP6012607B2 JP6012607B2 (ja) | 2016-10-25 |
Family
ID=44801202
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2013531909A Active JP6012607B2 (ja) | 2010-10-04 | 2011-09-30 | 航空宇宙ビークルの複合材スチフナ |
Country Status (6)
| Country | Link |
|---|---|
| US (2) | US8720825B2 (enExample) |
| EP (2) | EP2625026B1 (enExample) |
| JP (1) | JP6012607B2 (enExample) |
| CN (1) | CN103038052A (enExample) |
| ES (2) | ES2673499T3 (enExample) |
| WO (1) | WO2012047751A1 (enExample) |
Families Citing this family (44)
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| US8585856B1 (en) | 2010-05-13 | 2013-11-19 | Textron Innovations Inc. | Process for fabricating aircraft parts using an integrated form |
| JP5535957B2 (ja) | 2011-02-21 | 2014-07-02 | 三菱航空機株式会社 | 翼パネルの形成方法 |
| CA3071187A1 (en) | 2011-04-15 | 2013-07-04 | JG Entrepreneurial Enterprises LLC | Transportation system including a hovering vehicle |
| DE102012001055B4 (de) * | 2012-01-20 | 2023-06-29 | Liebherr-Aerospace Lindenberg Gmbh | Bauteil |
| US9545757B1 (en) | 2012-02-08 | 2017-01-17 | Textron Innovations, Inc. | Composite lay up and method of forming |
| US9050757B1 (en) | 2012-02-08 | 2015-06-09 | Textron Innovations, Inc. | System and method for curing composites |
| US9051062B1 (en) | 2012-02-08 | 2015-06-09 | Textron Innovations, Inc. | Assembly using skeleton structure |
| US9302455B1 (en) | 2012-02-08 | 2016-04-05 | Textron Innovations, Inc. | Fast cure process |
| US9649820B1 (en) | 2012-02-08 | 2017-05-16 | Textron Innovations, Inc. | Assembly using skeleton structure |
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| US9878773B2 (en) | 2012-12-03 | 2018-01-30 | The Boeing Company | Split resistant composite laminate |
| US20140166191A1 (en) | 2012-12-14 | 2014-06-19 | Aurora Flight Sciences Corporation | Methods for combining components of varying stages of cure |
| AU2014200142B2 (en) * | 2013-01-26 | 2017-02-23 | The Boeing Company | Box structures for carrying loads and methods of making the same |
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| EP2910365B1 (en) * | 2014-02-21 | 2017-04-26 | Airbus Operations GmbH | Composite structural element and torsion box |
| WO2015142171A1 (en) * | 2014-03-17 | 2015-09-24 | Gtm Holding B.V. | Primary structure connecting element for aircraft and method for manufacturing the connecting element |
| US9533444B2 (en) * | 2014-04-09 | 2017-01-03 | Randall J. Philpot | Method for creating furniture components from composites |
| ES2661116T3 (es) * | 2014-05-30 | 2018-03-27 | Airbus Operations, S.L. | Procedimiento de fabricación de paneles de fibra de carbono reforzados con larguerillos en forma de omega |
| GB2528080A (en) * | 2014-07-08 | 2016-01-13 | Airbus Operations Ltd | Structure |
| US10099445B2 (en) | 2015-05-14 | 2018-10-16 | The Boeing Company | Systems and methods for forming composite materials |
| US10190954B2 (en) * | 2015-06-01 | 2019-01-29 | The Boeing Company | Pre-strained composite test coupons |
| EP3112254B1 (en) * | 2015-06-29 | 2020-10-14 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | Aircraft structural component adapted for absorbing and transmitting forces |
| GB201511402D0 (en) * | 2015-06-30 | 2015-08-12 | Short Brothers Plc | Repair including a chamfered bracket and a chamfered bracket component for reinforcing a damaged structural element made from composite materials |
| US10005267B1 (en) | 2015-09-22 | 2018-06-26 | Textron Innovations, Inc. | Formation of complex composite structures using laminate templates |
| DE102016210123A1 (de) * | 2016-06-08 | 2017-12-14 | Airbus Operations Gmbh | Versteifungsbauteil für eine Struktur eines Luft- oder Raumfahrzeugs, Luft- oder Raumfahrzeug, sowie Verfahren |
| US10449754B2 (en) * | 2016-06-28 | 2019-10-22 | The Boeing Company | Wrinkle reduction in formed composite laminates |
| US10227127B2 (en) * | 2016-07-26 | 2019-03-12 | Embraer S.A. | Fiber metal laminate reinforced wing spar for retractable underwing mounted landing gear assemblies |
| US10696373B2 (en) | 2016-09-13 | 2020-06-30 | The Boeing Company | Aircraft wings and aircraft including such aircraft wings |
| US20180086429A1 (en) * | 2016-09-28 | 2018-03-29 | The Boeing Company | Airfoil-Shaped Body Having Composite Base Skin with Integral Hat-Shaped Spar |
| JP6980454B2 (ja) * | 2017-08-17 | 2021-12-15 | 三菱重工業株式会社 | 複合材の設計方法、複合材の評価方法及び複合材 |
| DE102018104122A1 (de) * | 2018-02-23 | 2019-08-29 | Airbus Operations Gmbh | Verbundstrukturelement |
| US11332228B2 (en) | 2018-04-06 | 2022-05-17 | Aurora Flight Sciences Corporation | Aircraft fuselage with composite pre-form |
| US11180238B2 (en) * | 2018-11-19 | 2021-11-23 | The Boeing Company | Shear ties for aircraft wing |
| US11325688B2 (en) | 2019-05-09 | 2022-05-10 | The Boeing Company | Composite stringer and methods for forming a composite stringer |
| US11318705B2 (en) | 2019-08-26 | 2022-05-03 | The Boeing Company | Ply stackings for solid laminate stiffened panel |
| CA3138153A1 (en) * | 2021-01-28 | 2022-07-28 | The Boeing Company | Flat composite panel with tear arrestment and method of making the same |
| GB2605430A (en) * | 2021-03-31 | 2022-10-05 | Airbus Operations Ltd | Load-bearing structures |
| FR3134032B1 (fr) | 2022-04-01 | 2024-07-05 | Design Tech Centre | Panneau anti flambage, structure aéroportée intégrant de tels panneaux et procédé de fabrication correspondant |
| GB202307925D0 (en) * | 2023-05-26 | 2023-07-12 | Rolls Royce Plc | Kinetic energy absorptive composite article |
| CN116714286A (zh) * | 2023-06-16 | 2023-09-08 | 北京玻钢院复合材料有限公司 | 一种复合材料蒙皮与桁架的连接方法 |
| US12122501B1 (en) * | 2023-09-06 | 2024-10-22 | Jetzero, Inc. | Aircraft with carbon fiber material and a method of manufacture |
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| 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 |
| US7837147B2 (en) * | 2005-03-18 | 2010-11-23 | The Boeing Company | Systems and methods for reducing noise in aircraft fuselages and other structures |
| US8201371B2 (en) * | 2005-03-31 | 2012-06-19 | The Boeing Company | Composite beam chord between reinforcement plates |
| US7807249B2 (en) * | 2005-03-31 | 2010-10-05 | The Boeing Company | Composite article having reinforcing fibers oriented to suppress or delay ply splitting |
| US8444087B2 (en) * | 2005-04-28 | 2013-05-21 | The Boeing Company | Composite skin and stringer structure and method for forming the same |
| US20060222837A1 (en) * | 2005-03-31 | 2006-10-05 | The Boeing Company | Multi-axial laminate composite structures and methods of forming the same |
| US7721495B2 (en) * | 2005-03-31 | 2010-05-25 | The Boeing Company | Composite structural members and methods for forming the same |
| US20060237588A1 (en) * | 2005-03-31 | 2006-10-26 | The Boeing Company | Composite structural member having an undulating web and method for forming the same |
| US9302427B2 (en) * | 2005-03-31 | 2016-04-05 | The Boeing Company | Aeropspace structure including composite beam chord clamped between reinforcement plates |
| FR2913747B1 (fr) * | 2007-03-16 | 2009-04-24 | Messier Dowty Sa Sa | Procede de realisation de raidisseurs en materiau composite |
-
2010
- 2010-10-04 US US12/897,742 patent/US8720825B2/en active Active
-
2011
- 2011-09-30 WO PCT/US2011/054206 patent/WO2012047751A1/en not_active Ceased
- 2011-09-30 CN CN2011800371824A patent/CN103038052A/zh active Pending
- 2011-09-30 ES ES16194975.5T patent/ES2673499T3/es active Active
- 2011-09-30 ES ES11770283.7T patent/ES2623431T3/es active Active
- 2011-09-30 JP JP2013531909A patent/JP6012607B2/ja active Active
- 2011-09-30 EP EP11770283.7A patent/EP2625026B1/en active Active
- 2011-09-30 EP EP16194975.5A patent/EP3144128B1/en active Active
-
2014
- 2014-04-14 US US14/252,764 patent/US9592650B2/en active Active
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