JP2012519614A5 - - Google Patents
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- Publication number
- JP2012519614A5 JP2012519614A5 JP2011554089A JP2011554089A JP2012519614A5 JP 2012519614 A5 JP2012519614 A5 JP 2012519614A5 JP 2011554089 A JP2011554089 A JP 2011554089A JP 2011554089 A JP2011554089 A JP 2011554089A JP 2012519614 A5 JP2012519614 A5 JP 2012519614A5
- Authority
- JP
- Japan
- Prior art keywords
- region
- patch
- laminated
- plies
- regions
- 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
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US12/400,519 US8449703B2 (en) | 2009-03-09 | 2009-03-09 | Predictable bonded rework of composite structures using tailored patches |
| US12/400,519 | 2009-03-09 | ||
| PCT/US2010/026252 WO2010104745A1 (en) | 2009-03-09 | 2010-03-04 | Predictable bonded rework of composite structures using tailored patches |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2012519614A JP2012519614A (ja) | 2012-08-30 |
| JP2012519614A5 true JP2012519614A5 (enExample) | 2013-04-04 |
| JP5852887B2 JP5852887B2 (ja) | 2016-02-03 |
Family
ID=42235656
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2011554089A Active JP5852887B2 (ja) | 2009-03-09 | 2010-03-04 | 適合させたパッチを用いた複合構造の予測可能な結合補修 |
Country Status (6)
| Country | Link |
|---|---|
| US (2) | US8449703B2 (enExample) |
| EP (1) | EP2406062B1 (enExample) |
| JP (1) | JP5852887B2 (enExample) |
| CN (1) | CN102317058B (enExample) |
| CA (1) | CA2754750C (enExample) |
| WO (1) | WO2010104745A1 (enExample) |
Families Citing this family (28)
| 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 |
| US8409384B2 (en) * | 2009-03-09 | 2013-04-02 | The Boeing Company | Predictable bonded rework of composite structures |
| US8449703B2 (en) * | 2009-03-09 | 2013-05-28 | The Boeing Company | Predictable bonded rework of composite structures using tailored patches |
| US9492975B2 (en) | 2009-03-09 | 2016-11-15 | The Boeing Company | Structural bonded patch with tapered adhesive design |
| US8524356B1 (en) | 2009-03-09 | 2013-09-03 | The Boeing Company | Bonded patch having multiple zones of fracture toughness |
| US8617694B1 (en) | 2009-03-09 | 2013-12-31 | The Boeing Company | Discretely tailored multi-zone bondline for fail-safe structural repair |
| US8540909B2 (en) * | 2009-03-09 | 2013-09-24 | The Boeing Company | Method of reworking an area of a composite structure containing an inconsistency |
| US20100233424A1 (en) * | 2009-03-10 | 2010-09-16 | The Boeing Company | Composite structures employing quasi-isotropic laminates |
| US8815132B2 (en) * | 2010-01-18 | 2014-08-26 | The Boeing Company | Method of configuring a patch body |
| US8720278B1 (en) | 2011-05-05 | 2014-05-13 | The Boeing Company | Method of detecting inconsistencies in composite structures and stress sensitive coatings used therein |
| US9085052B1 (en) | 2011-05-05 | 2015-07-21 | The Boeing Company | Structural repair having optical witness and method of monitoring repair performance |
| 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 |
| US8960604B1 (en) | 2011-09-07 | 2015-02-24 | The Boeing Company | Composite fuselage system with composite fuselage sections |
| US8895130B2 (en) | 2011-10-07 | 2014-11-25 | The Boeing Company | Peel-resistant mechanism for use in bonding components |
| US9314979B1 (en) | 2013-07-16 | 2016-04-19 | The Boeing Company | Trapezoidal rework patch |
| US20150185128A1 (en) * | 2013-12-26 | 2015-07-02 | The Boeing Company | Detection and Assessment of Damage to Composite Structure |
| US9518907B2 (en) | 2014-01-16 | 2016-12-13 | The Boeing Company | Methods and apparatus to determine integrity of composite structures |
| WO2015167630A1 (en) * | 2014-05-01 | 2015-11-05 | The Boeing Company | Structural bonded patch with tapered adhesive design |
| US10768128B2 (en) | 2014-07-22 | 2020-09-08 | The Boeing Company | Systems and methods of monitoring a thermal protection system |
| FR3042779B1 (fr) * | 2015-10-27 | 2018-07-13 | Airbus Operations | Procede de reparation d'une structure d'aeronef a partir de plaques deformables |
| US10288554B2 (en) * | 2016-01-27 | 2019-05-14 | The Boeing Company | Moisture detecting bleeder materials |
| US10710352B2 (en) | 2017-07-11 | 2020-07-14 | The Boeing Company | Structural pre-cured repair patch for repair to highly loaded primary and secondary structural components |
| DE202017105967U1 (de) * | 2017-09-29 | 2018-01-31 | Airbus Operations Gmbh | Farbbasiertes Heizsystem |
| JP7065052B2 (ja) * | 2019-03-14 | 2022-05-11 | 三菱重工業株式会社 | フィッティング方法及び修理方法 |
| AU2020204380A1 (en) | 2019-11-27 | 2021-06-10 | University Of Southern Queensland | A method and patch for defect repair |
| EP4008538A1 (en) | 2020-12-01 | 2022-06-08 | The Boeing Company | Rework part for composite structure |
| CN118178730A (zh) * | 2024-03-27 | 2024-06-14 | 上海茂摩生物科技有限公司 | 真皮脱细胞基质补片及其制备方法和应用 |
Family Cites Families (62)
| 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 |
| US4820564A (en) * | 1984-10-29 | 1989-04-11 | The Boeing Company | Blind-side repair patch kit |
| 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 |
| US4588626A (en) * | 1984-10-29 | 1986-05-13 | The Boeing Company | Blind-side panel repair patch |
| US4978404A (en) * | 1986-07-21 | 1990-12-18 | The Boeing Company | Method for repairing a hole in a structural wall of composite material |
| US4916880A (en) * | 1986-07-21 | 1990-04-17 | The Boeing Company | Apparatus 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 |
| US5618606A (en) | 1989-09-18 | 1997-04-08 | Rockwell International Corporation | Process for bonding staged composites with a cobonded staged adhesive and article |
| US5190611A (en) * | 1991-02-13 | 1993-03-02 | The Boeing Company | Bearing load restoration method for composite structures |
| 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 |
| US5374388A (en) | 1993-04-22 | 1994-12-20 | Lockheed Corporation | Method of forming contoured repair patches |
| 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 |
| CN2407933Y (zh) * | 1999-11-29 | 2000-11-29 | 捷安特(中国)有限公司 | 单向纤维补强贴片 |
| JP2001183833A (ja) | 1999-12-27 | 2001-07-06 | Sumitomo Chem Co Ltd | レジスト組成物 |
| BR0108968B1 (pt) | 2000-03-03 | 2012-10-02 | método para unir componentes compósitos e sistema para consertar componentes compósitos e para unir componentes. | |
| US6472758B1 (en) * | 2000-07-20 | 2002-10-29 | Amkor Technology, Inc. | Semiconductor package including stacked semiconductor dies and bond wires |
| US20030047268A1 (en) | 2001-08-23 | 2003-03-13 | Korchnak Gregory J. | Method for repairing fuel tanks |
| US7208220B2 (en) | 2001-12-06 | 2007-04-24 | 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 |
| JP4118264B2 (ja) * | 2004-07-15 | 2008-07-16 | 本田技研工業株式会社 | 衝撃吸収部材 |
| US20060059828A1 (en) * | 2004-07-29 | 2006-03-23 | Stevenson James F | Repair method for noise suppression structure |
| 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 |
| US7419556B2 (en) | 2005-10-11 | 2008-09-02 | United Technologies Corporation | Method of repair for inlet caps of turbine engines |
| 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 |
| US20080233346A1 (en) | 2007-03-23 | 2008-09-25 | United Technologies Corporation | Repair of a composite sandwich structure having a perforated skin |
| 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 |
| CN101357524A (zh) * | 2008-02-18 | 2009-02-04 | 江其超 | 防裂的裂缝修补材料的生产方法 |
| US20100117117A1 (en) | 2008-11-10 | 2010-05-13 | Infineon Technologies Ag | Vertical IGBT Device |
| US8449703B2 (en) * | 2009-03-09 | 2013-05-28 | The Boeing Company | Predictable bonded rework of composite structures using tailored patches |
| 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 |
| US20100233424A1 (en) | 2009-03-10 | 2010-09-16 | The Boeing Company | Composite structures employing quasi-isotropic laminates |
-
2009
- 2009-03-09 US US12/400,519 patent/US8449703B2/en active Active
-
2010
- 2010-03-04 WO PCT/US2010/026252 patent/WO2010104745A1/en not_active Ceased
- 2010-03-04 EP EP10708065.7A patent/EP2406062B1/en active Active
- 2010-03-04 CA CA2754750A patent/CA2754750C/en active Active
- 2010-03-04 JP JP2011554089A patent/JP5852887B2/ja active Active
- 2010-03-04 CN CN201080007769.6A patent/CN102317058B/zh active Active
-
2013
- 2013-05-26 US US13/902,816 patent/US8828515B2/en active Active
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