JP2012519615A5 - - Google Patents
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- Publication number
- JP2012519615A5 JP2012519615A5 JP2011554090A JP2011554090A JP2012519615A5 JP 2012519615 A5 JP2012519615 A5 JP 2012519615A5 JP 2011554090 A JP2011554090 A JP 2011554090A JP 2011554090 A JP2011554090 A JP 2011554090A JP 2012519615 A5 JP2012519615 A5 JP 2012519615A5
- Authority
- JP
- Japan
- Prior art keywords
- patch
- composite
- regions
- forming
- edge
- 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
- 239000002131 composite material Substances 0.000 claims description 35
- 239000012790 adhesive layer Substances 0.000 claims description 12
- 229920002430 Fibre-reinforced plastic Polymers 0.000 claims description 2
- 239000011151 fibre-reinforced plastic Substances 0.000 claims description 2
- 230000003247 decreasing effect Effects 0.000 claims 1
- 210000001503 joint Anatomy 0.000 claims 1
- 239000000853 adhesive Substances 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US12/400,561 US8540909B2 (en) | 2009-03-09 | 2009-03-09 | Method of reworking an area of a composite structure containing an inconsistency |
| US12/400,561 | 2009-03-09 | ||
| PCT/US2010/026256 WO2010104746A1 (en) | 2009-03-09 | 2010-03-04 | Tapered patch for predictable bonded rework of composite structures |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2012519615A JP2012519615A (ja) | 2012-08-30 |
| JP2012519615A5 true JP2012519615A5 (enExample) | 2013-04-04 |
| JP5792076B2 JP5792076B2 (ja) | 2015-10-07 |
Family
ID=42235674
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2011554090A Active JP5792076B2 (ja) | 2009-03-09 | 2010-03-04 | 複合構造の予測可能な結合補修のためのテーパつきパッチ |
Country Status (6)
| Country | Link |
|---|---|
| US (2) | US8540909B2 (enExample) |
| EP (1) | EP2406063B1 (enExample) |
| JP (1) | JP5792076B2 (enExample) |
| CN (1) | CN102317059B (enExample) |
| CA (1) | CA2754624C (enExample) |
| WO (1) | WO2010104746A1 (enExample) |
Families Citing this family (46)
| 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 |
| US8524356B1 (en) | 2009-03-09 | 2013-09-03 | The Boeing Company | Bonded patch having multiple zones of fracture toughness |
| 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 |
| 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 |
| US9492975B2 (en) | 2009-03-09 | 2016-11-15 | The Boeing Company | Structural bonded patch with tapered adhesive design |
| US20100233424A1 (en) * | 2009-03-10 | 2010-09-16 | The Boeing Company | Composite structures employing quasi-isotropic laminates |
| FR2953812B1 (fr) * | 2009-12-11 | 2012-09-07 | Airbus Operations Sas | Procede de reparation d'un fuselage d'aeronef |
| US8815132B2 (en) * | 2010-01-18 | 2014-08-26 | The Boeing Company | Method of configuring a patch body |
| US8752641B2 (en) * | 2010-11-30 | 2014-06-17 | United Technologies Corporation | Torque protection device for fire blanket and associated method |
| 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 |
| US9376923B2 (en) | 2011-07-13 | 2016-06-28 | Vestas Wind Systems A/S | Chordwise lay-up of fibre sheet material for turbine blades |
| 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 |
| ES2436728B2 (es) * | 2012-06-29 | 2015-04-06 | Airbus Operations S.L. | Pieza y método para la reparación de elementos longitudinales fabricados en material compuesto |
| NO336368B1 (no) | 2012-11-21 | 2015-08-10 | Flowtite Technology As | En flens, og en fremgangsmåte for å fremstille en flens |
| JP6162993B2 (ja) * | 2013-03-28 | 2017-07-12 | 三菱航空機株式会社 | 被修理部の修理方法および修理により得られた修理結果物 |
| US9314979B1 (en) | 2013-07-16 | 2016-04-19 | The Boeing Company | Trapezoidal rework patch |
| 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 |
| US20170259514A1 (en) * | 2014-10-17 | 2017-09-14 | Philmore H. Colburn, II | Repair patch for rotor blade |
| US10222353B2 (en) * | 2015-03-18 | 2019-03-05 | The Boeing Company | Method and assembly for inspecting a partially cured repair patch prior to installation |
| US10213964B2 (en) * | 2015-05-08 | 2019-02-26 | The Boeing Company | Methods and apparatus for repairing composite materials |
| US9919444B2 (en) | 2015-07-10 | 2018-03-20 | Wichita State University | System for developing composite repair patches on aircraft or other composite structures |
| GB201519877D0 (en) * | 2015-11-11 | 2015-12-23 | Short Brothers Plc | Methods and patches for repairing composite laminates |
| US10753277B2 (en) * | 2016-07-27 | 2020-08-25 | Raytheon Technologies Corporation | Inlet cap of an engine |
| JP6420857B2 (ja) * | 2017-02-09 | 2018-11-07 | 三菱重工業株式会社 | 風力発電設備、風車翼および風車翼の補強方法 |
| JP6496360B2 (ja) * | 2017-06-29 | 2019-04-03 | ファナック株式会社 | 樹脂複合板の製造方法 |
| US10737986B2 (en) * | 2017-09-19 | 2020-08-11 | General Electric Company | Methods for repairing composite cylinders |
| CN107738497B (zh) * | 2017-11-23 | 2020-04-28 | 河北工业大学 | 一种用于胶接修补的填充修补方法 |
| US11459908B2 (en) * | 2018-08-31 | 2022-10-04 | General Electric Company | CMC component including directionally controllable CMC insert and method of fabrication |
| JP7018855B2 (ja) * | 2018-09-11 | 2022-02-14 | 三菱重工業株式会社 | 修理パッチ、修理パッチの成形方法及び複合材の修理方法 |
| DK3712423T3 (da) * | 2019-03-21 | 2023-01-30 | Siemens Gamesa Renewable Energy As | Fremgangsmåde til reparation af et beskadiget bjælkedæksel af en vindmøllevinge af en vindmølle |
| WO2020232367A1 (en) * | 2019-05-15 | 2020-11-19 | DAP Products, Inc. | Patching method and apparatuses |
| US11572162B2 (en) * | 2019-05-29 | 2023-02-07 | Lockheed Martin Corporation | Securing assembly for a rotor blade |
| CN110435164B (zh) * | 2019-07-19 | 2024-05-14 | 中国工程物理研究院化工材料研究所 | 一种降低脆性材料开孔结构应力集中的方法及其结构 |
| DE102019121357A1 (de) * | 2019-08-07 | 2021-02-11 | Airbus Defence and Space GmbH | Verfahren zum Reparieren eines Faserverbundbauteils |
| CN115052740B (zh) * | 2020-03-18 | 2024-08-02 | 小利兰斯坦福大学理事会 | 有限尺寸的复合层压插片、由其形成的渐缩复合层压结构及其制造和使用方法 |
| EP4008538A1 (en) * | 2020-12-01 | 2022-06-08 | The Boeing Company | Rework part for composite structure |
| US12397516B2 (en) | 2020-12-07 | 2025-08-26 | General Electric Company | Method for repairing composite components using a support member |
| JP2023132234A (ja) * | 2022-03-10 | 2023-09-22 | 株式会社Subaru | 繊維強化樹脂接合構造体 |
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| US8524356B1 (en) * | 2009-03-09 | 2013-09-03 | The Boeing Company | Bonded patch having multiple zones of fracture toughness |
| 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 |
| US8409384B2 (en) * | 2009-03-09 | 2013-04-02 | The Boeing Company | Predictable bonded rework of composite structures |
| US20100233424A1 (en) | 2009-03-10 | 2010-09-16 | The Boeing Company | Composite structures employing quasi-isotropic laminates |
-
2009
- 2009-03-09 US US12/400,561 patent/US8540909B2/en active Active
-
2010
- 2010-03-04 EP EP10708066.5A patent/EP2406063B1/en active Active
- 2010-03-04 WO PCT/US2010/026256 patent/WO2010104746A1/en not_active Ceased
- 2010-03-04 CA CA2754624A patent/CA2754624C/en active Active
- 2010-03-04 CN CN201080007770.9A patent/CN102317059B/zh active Active
- 2010-03-04 JP JP2011554090A patent/JP5792076B2/ja active Active
-
2013
- 2013-05-27 US US13/902,855 patent/US8802213B2/en active Active
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