JP2013512808A5 - - Google Patents
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- Publication number
- JP2013512808A5 JP2013512808A5 JP2012543112A JP2012543112A JP2013512808A5 JP 2013512808 A5 JP2013512808 A5 JP 2013512808A5 JP 2012543112 A JP2012543112 A JP 2012543112A JP 2012543112 A JP2012543112 A JP 2012543112A JP 2013512808 A5 JP2013512808 A5 JP 2013512808A5
- Authority
- JP
- Japan
- Prior art keywords
- surrogate patch
- surrogate
- patch body
- sensor
- rework area
- 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
- 238000000034 method Methods 0.000 claims description 9
- 239000002131 composite material Substances 0.000 claims description 6
- 239000000463 material Substances 0.000 claims description 6
- 238000000157 electrochemical-induced impedance spectroscopy Methods 0.000 claims description 4
- 238000001514 detection method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US12/633,753 | 2009-12-08 | ||
| US12/633,753 US8545650B2 (en) | 2009-12-08 | 2009-12-08 | Method of repairing a composite structure |
| PCT/US2010/055684 WO2011071622A1 (en) | 2009-12-08 | 2010-11-05 | Surrogate patch for composite repair process |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2013512808A JP2013512808A (ja) | 2013-04-18 |
| JP2013512808A5 true JP2013512808A5 (enExample) | 2013-12-19 |
| JP5963169B2 JP5963169B2 (ja) | 2016-08-03 |
Family
ID=43813722
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2012543112A Active JP5963169B2 (ja) | 2009-12-08 | 2010-11-05 | 複合構造修復プロセスのサロゲートパッチ |
Country Status (11)
| Country | Link |
|---|---|
| US (2) | US8545650B2 (enExample) |
| EP (1) | EP2509777B1 (enExample) |
| JP (1) | JP5963169B2 (enExample) |
| KR (1) | KR101819760B1 (enExample) |
| CN (2) | CN107512014B (enExample) |
| BR (1) | BR112012013817B1 (enExample) |
| CA (1) | CA2783188C (enExample) |
| ES (1) | ES2555984T3 (enExample) |
| PT (1) | PT2509777E (enExample) |
| SG (1) | SG185358A1 (enExample) |
| WO (1) | WO2011071622A1 (enExample) |
Families Citing this family (47)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2953812B1 (fr) * | 2009-12-11 | 2012-09-07 | Airbus Operations Sas | Procede de reparation d'un fuselage d'aeronef |
| US8444127B2 (en) * | 2009-12-14 | 2013-05-21 | The Boeing Company | High temperature composite patch tool |
| IT1399682B1 (it) * | 2010-03-29 | 2013-04-26 | Alenia Aeronautica Spa | Procedimento e dispositivo per la riparazione di pannelli di materiale composito |
| DE102011006792B4 (de) * | 2011-04-05 | 2017-07-27 | Airbus Operations Gmbh | Verfahren zum Herstellen und Verbinden von faserverstärkten Bauteilen sowie Luft- oder Raumfahrzeug |
| 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 |
| US8844108B2 (en) * | 2011-07-12 | 2014-09-30 | The Boeing Company | Large area repair of composite aircraft |
| DE102011086453A1 (de) * | 2011-11-16 | 2013-05-16 | Wobben Properties Gmbh | Heizeinrichtung zur Reparatur oder Herstellung von Komponenten einer Windenergieanlage und Teilen davon sowie Windenergieanlage |
| DE102011122059A1 (de) * | 2011-12-22 | 2013-06-27 | Airbus Operations Gmbh | System und Verfahren zur Reparatur eines Strukturbauteils |
| FR2985213B1 (fr) * | 2011-12-28 | 2016-12-30 | Airbus Operations Sas | Panneau composite auto-raidi et procede de realisation |
| US9919388B2 (en) * | 2012-01-26 | 2018-03-20 | General Electric Company | Method for repairing a laminated article having a damaged area |
| FR2991228B1 (fr) | 2012-05-29 | 2015-03-06 | Airbus Operations Sas | Procede et dispositif de realisation d'un panneau composite auto-raidi |
| FR2999970B1 (fr) | 2012-12-20 | 2015-06-19 | Airbus Operations Sas | Procede de realisation d'une preforme textile a fibres continues par circulation d'un flux de gaz chaud a travers un ensemble fibreux |
| US20150306712A1 (en) * | 2013-01-07 | 2015-10-29 | University Of Washington Through Its Center For Commercialization | Embedded section heater for bonding composite structures, and associated apparatuses and methods |
| US9817452B2 (en) | 2013-01-11 | 2017-11-14 | The Boeing Company | System and method for thermal management guidance |
| FR3015433B1 (fr) | 2013-12-23 | 2016-02-12 | Airbus Operations Sas | Ensemble pour aeronef comprenant un mat d'accrochage integre a la nacelle et agence en partie arriere du fuselage |
| CN103770346B (zh) * | 2014-01-07 | 2016-05-04 | 杭州华聚复合材料有限公司 | 一种热塑性蜂窝板的修复方法 |
| US10583616B2 (en) | 2014-06-20 | 2020-03-10 | The Boeing Company | Forming tools and flexible ultrasonic transducer arrays |
| US10768128B2 (en) | 2014-07-22 | 2020-09-08 | The Boeing Company | Systems and methods of monitoring a thermal protection system |
| WO2016137565A1 (en) * | 2015-02-23 | 2016-09-01 | Sikorsky Aircraft Corporation | Composite repair method |
| US9945735B2 (en) * | 2015-03-26 | 2018-04-17 | The Boeing Company | System and method to monitor a thermal environment of a composite structure using a thermochromatic witness assembly |
| US9873527B2 (en) * | 2015-03-26 | 2018-01-23 | The Boeing Company | System and method to map a thermal profile of a composite structure using a thermochromatic witness assembly |
| US20160370309A1 (en) | 2015-06-22 | 2016-12-22 | The Boeing Company | Methods and systems for determining an allowable moisture content in a composite structure |
| FR3042779B1 (fr) * | 2015-10-27 | 2018-07-13 | Airbus Operations | Procede de reparation d'une structure d'aeronef a partir de plaques deformables |
| US10695993B2 (en) | 2016-01-15 | 2020-06-30 | GM Global Technology Operations LLC | In-situ polymerization of polyamides for composite part repair |
| US10288554B2 (en) * | 2016-01-27 | 2019-05-14 | The Boeing Company | Moisture detecting bleeder materials |
| US10927684B2 (en) * | 2016-02-08 | 2021-02-23 | Raytheon Technologies Corporation | Repairing a coating with a pre-configured coating patch |
| US10589477B2 (en) | 2016-05-02 | 2020-03-17 | GM Global Technology Operations LLC | Cosmetic repair of a thermoplastic carbon fiber composite |
| DE102016109121B4 (de) | 2016-05-18 | 2023-03-23 | Airbus Operations Gmbh | Mobiles Heizsystem und Heizverfahren |
| US10774648B2 (en) | 2016-10-04 | 2020-09-15 | General Electric Company | Methods and features for CMC component repairs |
| US20180147800A1 (en) * | 2016-11-30 | 2018-05-31 | The Boeing Company | Configurable Cooling Assembly and Cooling Method |
| JP6847679B2 (ja) * | 2017-01-20 | 2021-03-24 | 三菱重工業株式会社 | 複合材の修理方法 |
| US10656074B2 (en) * | 2017-05-02 | 2020-05-19 | The Boeing Company | Bondline sensors |
| US10611104B2 (en) | 2017-06-15 | 2020-04-07 | GM Global Technology Operations LLC | Heating elements for repair of molding defects for carbon fiber thermoplastic composites |
| US20190064003A1 (en) * | 2017-08-29 | 2019-02-28 | Te Wire & Cable Llc | Multipoint Temperature Profiling and Monitoring System for Composite Repair |
| DE102017122630A1 (de) * | 2017-09-28 | 2019-03-28 | Airbus Operations Gmbh | Vakuumfolie mit belüftungseigenschaften |
| DE202017105967U1 (de) * | 2017-09-29 | 2018-01-31 | Airbus Operations Gmbh | Farbbasiertes Heizsystem |
| JP7036694B2 (ja) * | 2018-09-12 | 2022-03-15 | 三菱重工業株式会社 | 修理パッチ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 |
| US11554559B2 (en) * | 2019-12-11 | 2023-01-17 | The Boeing Company | Caul plate for irregular surface |
| FR3106772B1 (fr) * | 2020-01-31 | 2022-01-28 | Ecole Nat Superieure D’Arts Et Metiers | Tapis chauffant souple pour le preformage ou la consolidation de pieces composites |
| CN111392028A (zh) * | 2020-04-13 | 2020-07-10 | 中国商用飞机有限责任公司 | 用于机翼长桁的长桁修理件以及修理机翼长桁的方法 |
| US12397516B2 (en) | 2020-12-07 | 2025-08-26 | General Electric Company | Method for repairing composite components using a support member |
| CN113877865B (zh) * | 2021-11-10 | 2022-12-09 | 段瑞 | 一种农业大棚膜内部清洗器 |
| US20240359413A1 (en) * | 2023-04-26 | 2024-10-31 | The Boeing Company | Systems and methods for composite stringer package construction and compacted stringer packages |
| CN119610737B (zh) * | 2024-12-04 | 2025-10-28 | 中建材(上海)航空技术有限公司 | 一种复合材料修复方法及修复结构 |
Family Cites Families (24)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4221962A (en) * | 1978-04-24 | 1980-09-09 | Northrop Corporation | Fiber-optic moisture sensor for composite structures |
| US4622091A (en) * | 1984-11-29 | 1986-11-11 | The Boeing Company | Resin film infusion process and apparatus |
| US4652319A (en) * | 1984-12-03 | 1987-03-24 | Hammond Russell E | Method of curing patches on contoured surfaces |
| 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 |
| GB2213596A (en) | 1988-01-07 | 1989-08-16 | Protimeter Plc | Disposable humidity sensor |
| JP2796123B2 (ja) * | 1989-05-26 | 1998-09-10 | 神鋼パンテック株式会社 | グラスライニング鋼製機器のライニングガラス層の破損局部の補修方法および装置 |
| US5145541A (en) * | 1989-07-07 | 1992-09-08 | Hexcel Corporation | Low energy cured composite repair system based on imidazole-blocked naphthyl-diisocyanates |
| US6527849B2 (en) * | 1990-06-19 | 2003-03-04 | Carolyn M. Dry | Self-repairing, reinforced matrix materials |
| US5442156A (en) * | 1991-04-09 | 1995-08-15 | The Boeing Company | Heating apparatus for composite structure repair |
| US5379689A (en) * | 1993-07-29 | 1995-01-10 | General Electric Company | Composite repair press for manufacturing and repairing a workpiece made from a composite material |
| US5833795A (en) * | 1996-09-19 | 1998-11-10 | Mcdonnell Douglas Corporation | Magnetic particle integrated adhesive and associated method of repairing a composite material product |
| US6561247B2 (en) * | 1998-06-29 | 2003-05-13 | General Electric Company | Method and apparatus for repairing a discrete damaged portion of an article surface |
| US6385836B1 (en) * | 2000-06-30 | 2002-05-14 | Lockheed Martin Corporation | Method for composite material repair |
| GB2375742A (en) | 2001-05-23 | 2002-11-27 | Monarch Vulcanising Systems Lt | Tyre repair patch |
| US6761783B2 (en) * | 2002-04-09 | 2004-07-13 | The Boeing Company | Process method to repair bismaleimide (BMI) composite structures |
| EP1504236A4 (en) * | 2002-05-15 | 2009-08-19 | Glaxo Group Ltd | MICROELECTROMECHANICAL SYSTEM AND METHOD FOR DETERMINING TEMPERATURE AND HUMIDITY PROFILES WITHIN PHARMACEUTICAL PACKAGING |
| US6976519B2 (en) * | 2002-12-11 | 2005-12-20 | Bh Thermal, Inc. | Portable curing system for use with vacuum bag repairs and the like |
| US20060027308A1 (en) * | 2004-08-05 | 2006-02-09 | Mackenzie M S | Method and apparatus for curing patches on composite structures having complex substrates |
| US20070095457A1 (en) * | 2005-11-02 | 2007-05-03 | The Boeing Company | Fast line maintenance repair method and system for composite structures |
| US8043453B2 (en) * | 2005-12-23 | 2011-10-25 | The Boeing Company | System and method for reworking composites |
| GB2440954B (en) * | 2006-08-18 | 2008-12-17 | Insensys Ltd | Structural monitoring |
| DE102007013755B4 (de) | 2007-03-22 | 2020-10-29 | Te Connectivity Germany Gmbh | Indikatorelement für einen magnetischen Drehwinkelgeber |
| SG151151A1 (en) * | 2007-09-11 | 2009-04-30 | Aircraft Plastics Australia Pt | Aircraft plastics repair |
| DE202007013755U1 (de) | 2007-10-02 | 2008-03-13 | Kiersch Composite Gmbh | Verbundwerkstoffelement |
-
2009
- 2009-12-08 US US12/633,753 patent/US8545650B2/en active Active
-
2010
- 2010-11-05 BR BR112012013817-0A patent/BR112012013817B1/pt active IP Right Grant
- 2010-11-05 SG SG2012073532A patent/SG185358A1/en unknown
- 2010-11-05 CN CN201710704803.9A patent/CN107512014B/zh active Active
- 2010-11-05 ES ES10779165.9T patent/ES2555984T3/es active Active
- 2010-11-05 CN CN201080054521.5A patent/CN102686386B/zh active Active
- 2010-11-05 EP EP10779165.9A patent/EP2509777B1/en active Active
- 2010-11-05 KR KR1020127009873A patent/KR101819760B1/ko active Active
- 2010-11-05 WO PCT/US2010/055684 patent/WO2011071622A1/en not_active Ceased
- 2010-11-05 JP JP2012543112A patent/JP5963169B2/ja active Active
- 2010-11-05 PT PT107791659T patent/PT2509777E/pt unknown
- 2010-11-05 CA CA2783188A patent/CA2783188C/en active Active
-
2013
- 2013-08-28 US US14/012,676 patent/US9381730B2/en active Active
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