JP2012520205A5 - - Google Patents
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- Publication number
- JP2012520205A5 JP2012520205A5 JP2011554087A JP2011554087A JP2012520205A5 JP 2012520205 A5 JP2012520205 A5 JP 2012520205A5 JP 2011554087 A JP2011554087 A JP 2011554087A JP 2011554087 A JP2011554087 A JP 2011554087A JP 2012520205 A5 JP2012520205 A5 JP 2012520205A5
- Authority
- JP
- Japan
- Prior art keywords
- skin
- frame member
- composite
- ply
- stack
- 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.)
- Pending
Links
- 239000002131 composite material Substances 0.000 claims description 20
- 238000000034 method Methods 0.000 claims description 10
- 239000000835 fiber Substances 0.000 claims description 4
- 230000008878 coupling Effects 0.000 claims description 3
- 238000010168 coupling process Methods 0.000 claims description 3
- 238000005859 coupling reaction Methods 0.000 claims description 3
- 239000003733 fiber-reinforced composite Substances 0.000 claims description 2
- 239000012783 reinforcing fiber Substances 0.000 description 1
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US12/401,541 | 2009-03-10 | ||
| US12/401,541 US20100233424A1 (en) | 2009-03-10 | 2009-03-10 | Composite structures employing quasi-isotropic laminates |
| PCT/US2010/026229 WO2010104741A1 (en) | 2009-03-10 | 2010-03-04 | Composite structures employing quasi-isotropic laminates |
Related Child Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2015172206A Division JP6162186B2 (ja) | 2009-03-10 | 2015-09-01 | 準等方性ラミネート材を用いた複合構造 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JP2012520205A JP2012520205A (ja) | 2012-09-06 |
| JP2012520205A5 true JP2012520205A5 (enExample) | 2013-03-07 |
Family
ID=42136041
Family Applications (3)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2011554087A Pending JP2012520205A (ja) | 2009-03-10 | 2010-03-04 | 準等方性ラミネート材を用いた複合構造 |
| JP2015172206A Active JP6162186B2 (ja) | 2009-03-10 | 2015-09-01 | 準等方性ラミネート材を用いた複合構造 |
| JP2017116163A Pending JP2017213900A (ja) | 2009-03-10 | 2017-06-13 | 準等方性ラミネート材を用いた複合構造 |
Family Applications After (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2015172206A Active JP6162186B2 (ja) | 2009-03-10 | 2015-09-01 | 準等方性ラミネート材を用いた複合構造 |
| JP2017116163A Pending JP2017213900A (ja) | 2009-03-10 | 2017-06-13 | 準等方性ラミネート材を用いた複合構造 |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US20100233424A1 (enExample) |
| EP (1) | EP2406071B1 (enExample) |
| JP (3) | JP2012520205A (enExample) |
| ES (1) | ES2564837T3 (enExample) |
| WO (1) | WO2010104741A1 (enExample) |
Families Citing this family (45)
| 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 |
| US9492975B2 (en) | 2009-03-09 | 2016-11-15 | The Boeing Company | Structural bonded patch with tapered adhesive design |
| US8540909B2 (en) * | 2009-03-09 | 2013-09-24 | The Boeing Company | Method of reworking an area of a composite structure containing an inconsistency |
| US8409384B2 (en) * | 2009-03-09 | 2013-04-02 | The Boeing Company | Predictable bonded rework of composite structures |
| US8617694B1 (en) | 2009-03-09 | 2013-12-31 | The Boeing Company | Discretely tailored multi-zone bondline for fail-safe structural repair |
| US8524356B1 (en) | 2009-03-09 | 2013-09-03 | The Boeing Company | Bonded patch having multiple zones of fracture toughness |
| US8449703B2 (en) * | 2009-03-09 | 2013-05-28 | The Boeing Company | Predictable bonded rework of composite structures using tailored patches |
| US8857128B2 (en) * | 2009-05-18 | 2014-10-14 | Apple Inc. | Reinforced device housing |
| US8815132B2 (en) * | 2010-01-18 | 2014-08-26 | The Boeing Company | Method of configuring a patch body |
| CA2799105A1 (en) * | 2010-05-11 | 2011-11-17 | Saab Ab | A composite article comprising particles and a method of forming a composite article |
| US8372495B2 (en) | 2010-05-26 | 2013-02-12 | Apple Inc. | Electronic device enclosure using sandwich construction |
| DE102010023496B4 (de) * | 2010-06-11 | 2017-02-23 | Airbus Operations Gmbh | Rumpfsegment eines Flugzeugs |
| US8765042B2 (en) | 2010-06-11 | 2014-07-01 | Airbus Operations Gmbh | Fuselage section of an aircraft and method for the production of the fuselage section |
| US9120272B2 (en) | 2010-07-22 | 2015-09-01 | Apple Inc. | Smooth composite structure |
| US9011623B2 (en) | 2011-03-03 | 2015-04-21 | Apple Inc. | Composite enclosure |
| EP2806418A4 (en) * | 2012-01-16 | 2015-12-16 | Nec Corp | MOBILE TERMINAL DEVICE |
| US9545757B1 (en) | 2012-02-08 | 2017-01-17 | Textron Innovations, Inc. | Composite lay up and method of forming |
| US20130280477A1 (en) * | 2012-03-26 | 2013-10-24 | Peter C. Davis | Off-angle laid scrims |
| EP2831328A4 (en) * | 2012-03-26 | 2015-12-02 | Saint Gobain Adfors Canada Ltd | FABRIC WITH ABORED ANGLES |
| US9964096B2 (en) * | 2013-01-10 | 2018-05-08 | Wei7 Llc | Triaxial fiber-reinforced composite laminate |
| US20160009368A1 (en) * | 2013-02-28 | 2016-01-14 | The Boeing Company | Composite laminated plate having reduced crossply angle |
| US10407955B2 (en) | 2013-03-13 | 2019-09-10 | Apple Inc. | Stiff fabric |
| US9314979B1 (en) | 2013-07-16 | 2016-04-19 | The Boeing Company | Trapezoidal rework patch |
| CN204608330U (zh) | 2013-12-20 | 2015-09-02 | 苹果公司 | 编织纤维带 |
| EP2910365B1 (en) * | 2014-02-21 | 2017-04-26 | Airbus Operations GmbH | Composite structural element and torsion box |
| US9850173B2 (en) | 2015-01-09 | 2017-12-26 | The Boeing Company | Hybrid sandwich ceramic matrix composite |
| DE102015010436B4 (de) * | 2015-08-14 | 2019-01-24 | Airbus Defence and Space GmbH | Wabenkern für dimensionsstabile Sandwichbauteile, dessen Verwendung, Sandwichplatte mit diesem Wabenkern und Verfahren zur Herstellung des Wabenkerns |
| US10005267B1 (en) | 2015-09-22 | 2018-06-26 | Textron Innovations, Inc. | Formation of complex composite structures using laminate templates |
| FR3061129B1 (fr) * | 2016-12-22 | 2019-05-31 | Airbus Operations | Procede de fabrication d'un module d'isolation thermophonique pour aeronef comprenant une etape de cintrage |
| RU179119U1 (ru) * | 2017-09-14 | 2018-04-26 | Российская Федерация, от имени которой выступает ФОНД ПЕРСПЕКТИВНЫХ ИССЛЕДОВАНИЙ | Устройство выхода волоконно-оптического датчика из композита |
| US10864686B2 (en) | 2017-09-25 | 2020-12-15 | Apple Inc. | Continuous carbon fiber winding for thin structural ribs |
| US11400657B2 (en) * | 2017-10-02 | 2022-08-02 | The Boeing Company | Methods of fabrication of composite repair parts and related kits |
| CN113272366A (zh) * | 2019-01-10 | 2021-08-17 | 艾维恩股份有限公司 | 具有包覆成型刚性部分的弹性柔性复合制品 |
| US11318705B2 (en) * | 2019-08-26 | 2022-05-03 | The Boeing Company | Ply stackings for solid laminate stiffened panel |
| CN114341289A (zh) | 2019-09-25 | 2022-04-12 | 3M创新有限公司 | 多相粘合剂制品及其方法 |
| EP4067033A4 (en) * | 2019-11-29 | 2023-12-20 | Toray Industries, Inc. | FIBER-REINFORCED COMPOSITE MATERIAL AND SANDWICH STRUCTURE |
| EP4067034A4 (en) * | 2019-11-29 | 2023-12-27 | Toray Industries, Inc. | FIBER REINFORCED COMPOSITE MATERIAL AND SANDWICH STRUCTURE |
| US12005682B2 (en) * | 2020-03-18 | 2024-06-11 | The Board Of Trustees Of The Leland Stanford Junior University | Composite laminate cards of finite size, tapered composite laminate structures formed from the same, and methods of manufacturing and using the same |
| US12024312B2 (en) | 2020-12-01 | 2024-07-02 | The Boeing Company | Rework part for composite structure |
| WO2022145005A1 (ja) * | 2020-12-28 | 2022-07-07 | 三菱重工業株式会社 | 繊維強化シート積層体並びに繊維強化シート積層体の製造方法及び構造体の製造方法 |
| US11969953B2 (en) * | 2022-07-26 | 2024-04-30 | The Boeing Company | Prepreg charge optimized for forming contoured composite laminate structures |
| US12049048B2 (en) | 2022-07-26 | 2024-07-30 | The Boeing Company | Method for high rate production of composite laminate structures |
| US20250083791A1 (en) * | 2023-09-07 | 2025-03-13 | Jetzero, Inc. | Dry fiber construction of a blended wing body aircraft and method of manufacture |
| US12187425B1 (en) | 2024-01-19 | 2025-01-07 | Jetzero, Inc. | Aircraft component with structural foam |
Family Cites Families (60)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3995080A (en) * | 1974-10-07 | 1976-11-30 | General Dynamics Corporation | Filament reinforced structural shapes |
| US4352707A (en) * | 1981-04-23 | 1982-10-05 | Grumman Aerospace Corporation | Composite repair apparatus |
| US4497404A (en) * | 1983-09-30 | 1985-02-05 | Lowrance William T | Protective device for a golf club |
| US4588853A (en) * | 1984-06-21 | 1986-05-13 | Roll Form Products, Inc. | Electrical trench grommet member |
| US4967799A (en) * | 1984-08-15 | 1990-11-06 | Dayco Products, Inc. | Plastic abrasion-resistant protective sleeve for hose and method of protecting hose |
| US4588626A (en) * | 1984-10-29 | 1986-05-13 | The Boeing Company | Blind-side panel repair patch |
| US5034254A (en) * | 1984-10-29 | 1991-07-23 | The Boeing Company | Blind-side panel repair patch |
| US4961799A (en) * | 1984-10-29 | 1990-10-09 | The Boeing Company | Blind-side panel repair method |
| US4820564A (en) * | 1984-10-29 | 1989-04-11 | The Boeing Company | Blind-side repair patch kit |
| US4916880A (en) * | 1986-07-21 | 1990-04-17 | The Boeing Company | Apparatus for repairing a hole in a structural wall of composite material |
| US4978404A (en) * | 1986-07-21 | 1990-12-18 | The Boeing Company | Method for repairing a hole in a structural wall of composite material |
| US4912594A (en) * | 1986-11-03 | 1990-03-27 | The Boeing Company | Integral lightning protection repair system and method for its use |
| US4824500A (en) * | 1987-11-03 | 1989-04-25 | The Dow Chemical Company | Method for repairing damaged composite articles |
| US4808253A (en) * | 1987-11-06 | 1989-02-28 | Grumman Aerospace Corporation | Method and apparatus for performing a repair on a contoured section of a composite structure |
| US4858853A (en) * | 1988-02-17 | 1989-08-22 | The Boeing Company | Bolted repair for curved surfaces |
| US5207541A (en) * | 1988-12-13 | 1993-05-04 | The Boeing Company | Scarfing apparatus |
| US5023987A (en) * | 1989-08-28 | 1991-06-18 | The Boeing Company | Strato streak flush patch |
| US5190611A (en) * | 1991-02-13 | 1993-03-02 | The Boeing Company | Bearing load restoration method for composite structures |
| JPH04341837A (ja) * | 1991-05-17 | 1992-11-27 | Ishikawajima Harima Heavy Ind Co Ltd | Frp積層板 |
| US5214307A (en) * | 1991-07-08 | 1993-05-25 | Micron Technology, Inc. | Lead frame for semiconductor devices having improved adhesive bond line control |
| US5232962A (en) * | 1991-10-09 | 1993-08-03 | Quantum Materials, Inc. | Adhesive bonding composition with bond line limiting spacer system |
| US5344515A (en) * | 1993-03-01 | 1994-09-06 | Argo-Tech Corporation | Method of making a pump housing |
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| WO1994025180A1 (en) * | 1993-05-05 | 1994-11-10 | Albany International Research Co. | Composite sandwich element |
| US5620768A (en) * | 1993-10-15 | 1997-04-15 | Pro Patch Systems, Inc. | Repair patch and method of manufacturing thereof |
| US5601676A (en) * | 1994-02-25 | 1997-02-11 | The Board Of Trustees Operating Michigan State University | Composite joining and repair |
| US5709469A (en) * | 1995-03-13 | 1998-01-20 | The United States Of America As Represented By The Secretary Of The Air Force | Process for testing integrity of bonds between epoxy patches and aircraft structural materials |
| US5626934A (en) * | 1995-10-20 | 1997-05-06 | United States Of America | Enhancing damage tolerance of adhesive bonds |
| US5868886A (en) * | 1995-12-22 | 1999-02-09 | Alston; Mark S. | Z-pin reinforced bonded composite repairs |
| US5732743A (en) * | 1996-06-14 | 1998-03-31 | Ls Technology Inc. | Method of sealing pipes |
| GB9622780D0 (en) * | 1996-11-01 | 1997-01-08 | British Aerospace | Repair of composite laminates |
| FR2763882B1 (fr) * | 1997-05-29 | 1999-08-20 | Aerospatiale | Outillage de reparation sur site d'une structure composite presentant une zone endommagee et procede correspondant |
| US5993934A (en) * | 1997-08-06 | 1999-11-30 | Eastman Kodak Company | Near zero CTE carbon fiber hybrid laminate |
| US6265333B1 (en) * | 1998-06-02 | 2001-07-24 | Board Of Regents, University Of Nebraska-Lincoln | Delamination resistant composites prepared by small diameter fiber reinforcement at ply interfaces |
| JP2001183833A (ja) * | 1999-12-27 | 2001-07-06 | Sumitomo Chem Co Ltd | レジスト組成物 |
| CN1224495C (zh) * | 2000-03-03 | 2005-10-26 | 快速科技有限公司 | 复合材料部件和金属部件的生产、成形、粘接、连接和修理系统 |
| US6472758B1 (en) * | 2000-07-20 | 2002-10-29 | Amkor Technology, Inc. | Semiconductor package including stacked semiconductor dies and bond wires |
| EP1473130B1 (en) * | 2001-12-06 | 2011-08-24 | Toray Industries, Inc. | Fiber-reinforced composite material and method for production thereof |
| US6656299B1 (en) * | 2001-12-19 | 2003-12-02 | Lockheed Martin Corporation | Method and apparatus for structural repair |
| US6761783B2 (en) * | 2002-04-09 | 2004-07-13 | The Boeing Company | Process method to repair bismaleimide (BMI) composite structures |
| US6758924B1 (en) * | 2002-04-15 | 2004-07-06 | The United States Of America As Represented By The Secretary Of The Air Force | Method of repairing cracked aircraft structures |
| NL1022706C2 (nl) * | 2003-02-17 | 2004-08-19 | Stichting Fmlc | Laminaat uit metaalplaten en elkaar kruisende dradenlagen uit verschillende materialen in kunststof. |
| US8246882B2 (en) * | 2003-05-02 | 2012-08-21 | The Boeing Company | Methods and preforms for forming composite members with interlayers formed of nonwoven, continuous materials |
| US6764754B1 (en) * | 2003-07-15 | 2004-07-20 | The Boeing Company | Composite material with improved damping characteristics and method of making same |
| US7527222B2 (en) * | 2004-04-06 | 2009-05-05 | The Boeing Company | Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections |
| JP4118264B2 (ja) * | 2004-07-15 | 2008-07-16 | 本田技研工業株式会社 | 衝撃吸収部材 |
| US20060029807A1 (en) * | 2004-08-04 | 2006-02-09 | Peck Scott O | Method for the design of laminated composite materials |
| US7325771B2 (en) * | 2004-09-23 | 2008-02-05 | The Boeing Company | Splice joints for composite aircraft fuselages and other structures |
| EP1683627A1 (en) * | 2005-01-25 | 2006-07-26 | Saab Ab | Method and apparatus for repairing a composite article |
| US8444087B2 (en) * | 2005-04-28 | 2013-05-21 | The Boeing Company | Composite skin and stringer structure and method for forming the same |
| JP2007016122A (ja) * | 2005-07-07 | 2007-01-25 | Toray Ind Inc | 炭素繊維強化複合材料 |
| US20070095457A1 (en) * | 2005-11-02 | 2007-05-03 | The Boeing Company | Fast line maintenance repair method and system for composite structures |
| US7398698B2 (en) * | 2005-11-03 | 2008-07-15 | The Boeing Company | Smart repair patch and associated method |
| US7935205B2 (en) * | 2006-06-19 | 2011-05-03 | United Technologies Corporation | Repair of composite sandwich structures |
| US7628879B2 (en) * | 2007-08-23 | 2009-12-08 | The Boeing Company | Conductive scrim embedded structural adhesive films |
| GB0721546D0 (en) * | 2007-11-01 | 2007-12-12 | Rolls Royce Plc | Composite material repair |
| US8409384B2 (en) * | 2009-03-09 | 2013-04-02 | The Boeing Company | Predictable bonded rework of composite structures |
| US8540909B2 (en) * | 2009-03-09 | 2013-09-24 | The Boeing Company | Method of reworking an area of a composite structure containing an inconsistency |
| US8449703B2 (en) * | 2009-03-09 | 2013-05-28 | The Boeing Company | Predictable bonded rework of composite structures using tailored patches |
| US8617694B1 (en) * | 2009-03-09 | 2013-12-31 | The Boeing Company | Discretely tailored multi-zone bondline for fail-safe structural repair |
-
2009
- 2009-03-10 US US12/401,541 patent/US20100233424A1/en not_active Abandoned
-
2010
- 2010-03-04 ES ES10707416.3T patent/ES2564837T3/es active Active
- 2010-03-04 WO PCT/US2010/026229 patent/WO2010104741A1/en not_active Ceased
- 2010-03-04 JP JP2011554087A patent/JP2012520205A/ja active Pending
- 2010-03-04 EP EP10707416.3A patent/EP2406071B1/en active Active
-
2015
- 2015-09-01 JP JP2015172206A patent/JP6162186B2/ja active Active
-
2017
- 2017-06-13 JP JP2017116163A patent/JP2017213900A/ja active Pending
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