JP2015189082A5 - - Google Patents
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- JP2015189082A5 JP2015189082A5 JP2014067920A JP2014067920A JP2015189082A5 JP 2015189082 A5 JP2015189082 A5 JP 2015189082A5 JP 2014067920 A JP2014067920 A JP 2014067920A JP 2014067920 A JP2014067920 A JP 2014067920A JP 2015189082 A5 JP2015189082 A5 JP 2015189082A5
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Priority Applications (8)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2014067920A JP6309324B2 (ja) | 2014-03-28 | 2014-03-28 | 複合材構造体、これを備えた航空機翼および航空機胴体、並びに複合材構造体の製造方法 |
| PCT/JP2015/057786 WO2015146690A1 (ja) | 2014-03-28 | 2015-03-17 | 複合材構造体、これを備えた航空機翼および航空機胴体、並びに複合材構造体の製造方法 |
| EP15770101.2A EP3103623B1 (en) | 2014-03-28 | 2015-03-17 | Composite material structure, aircraft wing and aircraft fuselage provided with same, and method for manufacturing composite material structure |
| BR112016020521-9A BR112016020521A2 (pt) | 2014-03-28 | 2015-03-17 | Estrutura de material compósito, asa de avião e fuselagem de avião dotadas da mesma e método para fabricação de estrutura de material compósito |
| RU2016135195A RU2645500C1 (ru) | 2014-03-28 | 2015-03-17 | Конструкция из композиционного материала и содержащие ее крыло летательного аппарата и фюзеляж летательного аппарата, способ изготовления конструкции из композиционного материала |
| US15/117,895 US10137664B2 (en) | 2014-03-28 | 2015-03-17 | Composite material structure, aircraft wing and aircraft fuselage provided with same, and method for manufacturing composite material structure |
| CN201580009194.4A CN106029346B (zh) | 2014-03-28 | 2015-03-17 | 复合材料构造体、具有该复合材料构造体的航空机机翼及航空机机身、以及复合材料构造体的制造方法 |
| CA2940463A CA2940463C (en) | 2014-03-28 | 2015-03-17 | Composite material structure, aircraft wing and aircraft fuselage provided with same, and method for manufacturing composite material structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2014067920A JP6309324B2 (ja) | 2014-03-28 | 2014-03-28 | 複合材構造体、これを備えた航空機翼および航空機胴体、並びに複合材構造体の製造方法 |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2015189082A JP2015189082A (ja) | 2015-11-02 |
| JP2015189082A5 true JP2015189082A5 (enExample) | 2016-09-08 |
| JP6309324B2 JP6309324B2 (ja) | 2018-04-11 |
Family
ID=54195213
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2014067920A Active JP6309324B2 (ja) | 2014-03-28 | 2014-03-28 | 複合材構造体、これを備えた航空機翼および航空機胴体、並びに複合材構造体の製造方法 |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US10137664B2 (enExample) |
| EP (1) | EP3103623B1 (enExample) |
| JP (1) | JP6309324B2 (enExample) |
| CN (1) | CN106029346B (enExample) |
| BR (1) | BR112016020521A2 (enExample) |
| CA (1) | CA2940463C (enExample) |
| RU (1) | RU2645500C1 (enExample) |
| WO (1) | WO2015146690A1 (enExample) |
Families Citing this family (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102016100191A1 (de) * | 2016-01-06 | 2017-07-06 | Wobben Properties Gmbh | Faserverbundbauteil und Strukturbauteil sowie Herstellungsverfahren |
| US10843788B2 (en) * | 2017-06-29 | 2020-11-24 | Textron Innovations Inc. | Damping structures for tiltrotor aircraft wings |
| FR3068912B1 (fr) * | 2017-07-11 | 2019-08-23 | Faurecia Automotive Industrie | Procede de fabrication d'une piece d'equipement de vehicule automobile et piece d'equipement associee |
| WO2019118881A1 (en) * | 2017-12-15 | 2019-06-20 | Stc.Unm | Gradually recruited fiber reinforced polymer (frp) composite |
| JP7112950B2 (ja) * | 2018-12-05 | 2022-08-04 | 三菱重工業株式会社 | 複合材の設計方法および複合材 |
| JP7198701B2 (ja) * | 2019-03-27 | 2023-01-04 | 日産自動車株式会社 | 繊維強化プラスチック複合材、繊維強化プラスチックプリフォーム、及び繊維強化プラスチック中間基材 |
| JP7390144B2 (ja) * | 2019-09-24 | 2023-12-01 | 三菱重工業株式会社 | 複合材の継手部材及び継手構造体 |
| GB2623100A (en) * | 2022-10-06 | 2024-04-10 | Bae Systems Plc | Aircraft wings |
| GB2638210A (en) * | 2024-02-15 | 2025-08-20 | Airbus Operations Ltd | Composite structure |
Family Cites Families (29)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5989842A (ja) * | 1982-11-12 | 1984-05-24 | Nhk Spring Co Ltd | Frp製ばね板 |
| DE3718676A1 (de) | 1987-06-04 | 1988-12-22 | Mtu Muenchen Gmbh | Formkoerper und verfahren zu seiner herstellung |
| NL8702487A (nl) * | 1987-10-19 | 1989-05-16 | Dsm Resins Bv | Werkwijze voor de vervaardiging van persprodukten. |
| JPH01263030A (ja) * | 1988-04-15 | 1989-10-19 | Agency Of Ind Science & Technol | 複合材のファスナ継手 |
| JPH0462038A (ja) | 1990-06-25 | 1992-02-27 | Ryobi Ltd | 積層管およびその製造方法 |
| JPH0489326A (ja) | 1990-07-31 | 1992-03-23 | Matsushita Electric Ind Co Ltd | 光学ガラス成形体とその製造方法とその製造装置 |
| JPH04334696A (ja) | 1991-05-09 | 1992-11-20 | Mitsubishi Heavy Ind Ltd | 複合材製補強パネル |
| MX9206033A (es) * | 1991-10-22 | 1993-05-01 | Univ Brigham Young | Amortiguamiento mejorado en estructuras compuestas a traves de acoplamiento por esfuerzo. |
| DE4234038C2 (de) * | 1992-10-09 | 1997-07-03 | Daimler Benz Aerospace Airbus | Schalenbauteil aus Faserverbundwerkstoff |
| FR2699499B1 (fr) * | 1992-12-23 | 1995-03-10 | Eurocopter France | Pale en composite thermoplastique, notamment pour rotor arrière caréné d'hélicoptère, et son procédé de fabrication avec étape d'injection. |
| US5771680A (en) * | 1995-12-21 | 1998-06-30 | General Electric Company | Stiffened composite structures and method of making thereof |
| US20020028332A1 (en) * | 1996-10-09 | 2002-03-07 | Pratt William F. | Wavy composite tubular structures |
| US7906191B2 (en) * | 1997-11-14 | 2011-03-15 | William F. Pratt | Wavy composite structures |
| DE29813901U1 (de) * | 1998-07-23 | 1999-02-04 | Inst Konstruktion Und Verbundb | Verbundbauteil |
| RU2185964C1 (ru) * | 2001-01-19 | 2002-07-27 | Государственное предприятие "Всероссийский научно-исследовательский институт авиационных материалов" | Слоистый композиционный материал и изделие, выполненное из него |
| GB0117804D0 (en) * | 2001-07-21 | 2001-09-12 | Bae Systems Plc | Aircraft structural components |
| DE10153875A1 (de) * | 2001-11-02 | 2003-05-15 | Bpw Bergische Achsen Kg | Bauteil in langgestreckter Bauweise aus einem Faser-Kunststoff-Verbund |
| US9302427B2 (en) | 2005-03-31 | 2016-04-05 | The Boeing Company | Aeropspace structure including composite beam chord clamped between reinforcement plates |
| DE102007019305A1 (de) * | 2007-04-24 | 2008-11-06 | Airbus Deutschland Gmbh | Befestigungsanordnung zum Befestigen eines Bauteils an einem Flugzeugrumpf, Flugzeug und Verfahren zum Fertigen einer Befestigungsanordnung |
| DE102008008386A1 (de) * | 2008-02-09 | 2009-08-13 | Airbus Deutschland Gmbh | Verfahren zur Herstellung eines FVW-Bauteils |
| JP5167953B2 (ja) | 2008-05-27 | 2013-03-21 | 東レ株式会社 | 積層基材、繊維強化プラスチック、およびそれらの製造方法 |
| JP5308533B2 (ja) * | 2009-10-08 | 2013-10-09 | 三菱重工業株式会社 | 複合材構造体、これを備えた航空機主翼および航空機胴体 |
| JP2011084008A (ja) | 2009-10-16 | 2011-04-28 | Toyota Motor Corp | Frp積層体の成形方法 |
| BR112013010337A2 (pt) | 2011-02-04 | 2016-08-02 | Mitsubishi Heavy Ind Ltd | estrutura de material compósito, e asa de aeronave e fuselagem providas da mesma |
| JP5808111B2 (ja) | 2011-02-04 | 2015-11-10 | 三菱重工業株式会社 | 航空機用複合材構造体、これを備えた航空機主翼および航空機胴体 |
| US8616500B2 (en) * | 2011-03-04 | 2013-12-31 | The Boeing Company | Diamond shaped window for composite and/or metallic airframe |
| JP6004669B2 (ja) * | 2012-02-29 | 2016-10-12 | 三菱重工業株式会社 | 複合材構造体、これを備えた航空機翼および航空機胴体、並びに複合材構造体の製造方法 |
| US9289949B2 (en) * | 2012-06-08 | 2016-03-22 | The Boeing Company | Optimized cross-ply orientation in composite laminates |
| DE102012221404A1 (de) * | 2012-11-22 | 2014-06-05 | Bayerische Motoren Werke Aktiengesellschaft | Aus einem Faserverbund bestehende Komponente, insbesondere für das Fahrwerk eines Kraftfahrzeuges |
-
2014
- 2014-03-28 JP JP2014067920A patent/JP6309324B2/ja active Active
-
2015
- 2015-03-17 CA CA2940463A patent/CA2940463C/en active Active
- 2015-03-17 EP EP15770101.2A patent/EP3103623B1/en active Active
- 2015-03-17 WO PCT/JP2015/057786 patent/WO2015146690A1/ja not_active Ceased
- 2015-03-17 CN CN201580009194.4A patent/CN106029346B/zh not_active Expired - Fee Related
- 2015-03-17 US US15/117,895 patent/US10137664B2/en active Active
- 2015-03-17 RU RU2016135195A patent/RU2645500C1/ru active
- 2015-03-17 BR BR112016020521-9A patent/BR112016020521A2/pt not_active IP Right Cessation
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