CN102317059B - 用于复合结构的可预测粘合修复的渐缩补片 - Google Patents
用于复合结构的可预测粘合修复的渐缩补片 Download PDFInfo
- Publication number
- CN102317059B CN102317059B CN201080007770.9A CN201080007770A CN102317059B CN 102317059 B CN102317059 B CN 102317059B CN 201080007770 A CN201080007770 A CN 201080007770A CN 102317059 B CN102317059 B CN 102317059B
- Authority
- CN
- China
- Prior art keywords
- patch
- composite
- tapered
- ply
- composite structure
- 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.)
- Active
Links
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C73/00—Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D
- B29C73/04—Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D using preformed elements
- B29C73/10—Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D using preformed elements using patches sealing on the surface of the article
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C73/00—Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D
- B29C73/04—Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D using preformed elements
- B29C73/14—Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D using preformed elements using elements composed of two parts joined together after having been placed one on each side of the article
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B19/00—Layered products comprising a layer of natural mineral fibres or particles, e.g. asbestos, mica
- B32B19/04—Layered products comprising a layer of natural mineral fibres or particles, e.g. asbestos, mica next to another layer of the same or of a different material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
- B32B3/10—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
- B32B3/26—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer
- B32B3/263—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer characterised by a layer having non-uniform thickness
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C73/00—Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D
- B29C73/16—Auto-repairing or self-sealing arrangements or agents
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
- B29L2031/3076—Aircrafts
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49764—Method of mechanical manufacture with testing or indicating
- Y10T29/49778—Method of mechanical manufacture with testing or indicating with aligning, guiding, or instruction
- Y10T29/4978—Assisting assembly or disassembly
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/18—Longitudinally sectional layer of three or more sections
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/20—Patched hole or depression
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/21—Circular sheet or circular blank
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24273—Structurally defined web or sheet [e.g., overall dimension, etc.] including aperture
- Y10T428/24322—Composite web or sheet
- Y10T428/24331—Composite web or sheet including nonapertured component
- Y10T428/24339—Keyed
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24479—Structurally defined web or sheet [e.g., overall dimension, etc.] including variation in thickness
- Y10T428/24488—Differential nonuniformity at margin
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24479—Structurally defined web or sheet [e.g., overall dimension, etc.] including variation in thickness
- Y10T428/24612—Composite web or sheet
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Laminated Bodies (AREA)
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 (2)
| Publication Number | Publication Date |
|---|---|
| CN102317059A CN102317059A (zh) | 2012-01-11 |
| CN102317059B true CN102317059B (zh) | 2015-11-25 |
Family
ID=42235674
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201080007770.9A Active CN102317059B (zh) | 2009-03-09 | 2010-03-04 | 用于复合结构的可预测粘合修复的渐缩补片 |
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 |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4987700A (en) * | 1988-12-13 | 1991-01-29 | The Boeing Company | Mechanical scarfing apparatus |
| CN1221864A (zh) * | 1998-12-28 | 1999-07-07 | 东营柯林清洗技术发展有限公司 | 用于在线管道修复的复合结构衬里及其压力挤涂工艺 |
| CN2385206Y (zh) * | 1999-07-13 | 2000-06-28 | 蔡志章 | 组装式翻衬法管线修复装置 |
| EP1775445A2 (en) * | 2005-10-11 | 2007-04-18 | United Technologies Corporation | Method of repair for inlet caps of turbine engines |
Family Cites Families (58)
| 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 |
| 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 |
| 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 |
| 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 |
| 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 |
| US20060029807A1 (en) * | 2004-08-04 | 2006-02-09 | Peck Scott O | Method for the design of laminated composite materials |
| US8468454B2 (en) * | 2004-08-26 | 2013-06-18 | Sony Corporation | Method and system for displaying portions of recorded media content instances |
| 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 |
| 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 |
| GB2447964B (en) * | 2007-03-29 | 2012-07-18 | Gurit Uk Ltd | Moulding material |
| 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 |
| 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
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4987700A (en) * | 1988-12-13 | 1991-01-29 | The Boeing Company | Mechanical scarfing apparatus |
| CN1221864A (zh) * | 1998-12-28 | 1999-07-07 | 东营柯林清洗技术发展有限公司 | 用于在线管道修复的复合结构衬里及其压力挤涂工艺 |
| CN2385206Y (zh) * | 1999-07-13 | 2000-06-28 | 蔡志章 | 组装式翻衬法管线修复装置 |
| EP1775445A2 (en) * | 2005-10-11 | 2007-04-18 | United Technologies Corporation | Method of repair for inlet caps of turbine engines |
Also Published As
| Publication number | Publication date |
|---|---|
| EP2406063A1 (en) | 2012-01-18 |
| WO2010104746A1 (en) | 2010-09-16 |
| US20130260077A1 (en) | 2013-10-03 |
| US20100227117A1 (en) | 2010-09-09 |
| JP5792076B2 (ja) | 2015-10-07 |
| US8540909B2 (en) | 2013-09-24 |
| CA2754624A1 (en) | 2010-09-16 |
| JP2012519615A (ja) | 2012-08-30 |
| CA2754624C (en) | 2014-09-09 |
| CN102317059A (zh) | 2012-01-11 |
| EP2406063B1 (en) | 2016-08-31 |
| US8802213B2 (en) | 2014-08-12 |
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