JP2012520205A - 準等方性ラミネート材を用いた複合構造 - Google Patents
準等方性ラミネート材を用いた複合構造 Download PDFInfo
- Publication number
- JP2012520205A JP2012520205A JP2011554087A JP2011554087A JP2012520205A JP 2012520205 A JP2012520205 A JP 2012520205A JP 2011554087 A JP2011554087 A JP 2011554087A JP 2011554087 A JP2011554087 A JP 2011554087A JP 2012520205 A JP2012520205 A JP 2012520205A
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- Prior art keywords
- composite
- plies
- skin
- stack
- fiber
- 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.)
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Images
Classifications
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- B29C70/06—Fibrous reinforcements only
- B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
- B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
- B29C70/20—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in a single direction, e.g. roofing or other parallel fibres
- B29C70/202—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in a single direction, e.g. roofing or other parallel fibres arranged in parallel planes or structures of fibres crossing at substantial angles, e.g. cross-moulding compound [XMC]
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- B29D99/0014—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings provided with ridges or ribs, e.g. joined ribs
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- B32B5/24—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
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- B32B5/24—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
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- B64C—AEROPLANES; HELICOPTERS
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- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
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- B64C—AEROPLANES; HELICOPTERS
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- B64C2001/0054—Fuselage structures substantially made from particular materials
- B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
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- 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
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- 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.]
- Y10T428/24058—Structurally defined web or sheet [e.g., overall dimension, etc.] including grain, strips, or filamentary elements in respective layers or components in angular relation
- Y10T428/24124—Fibers
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Textile Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Laminated Bodies (AREA)
- Moulding By Coating Moulds (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
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 true JP2012520205A (ja) | 2012-09-06 |
| JP2012520205A5 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) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2021075040A (ja) * | 2019-08-26 | 2021-05-20 | ザ・ボーイング・カンパニーThe Boeing Company | 中実積層補強パネルのためのプライの積み重ね |
Families Citing this family (44)
| 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 |
| US8617694B1 (en) | 2009-03-09 | 2013-12-31 | The Boeing Company | Discretely tailored multi-zone bondline for fail-safe structural repair |
| US9492975B2 (en) | 2009-03-09 | 2016-11-15 | The Boeing Company | Structural bonded patch with tapered adhesive design |
| US8409384B2 (en) * | 2009-03-09 | 2013-04-02 | The Boeing Company | Predictable bonded rework of composite structures |
| 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 |
| 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 |
| BR112012028784A2 (pt) * | 2010-05-11 | 2016-07-19 | Saab Ab | artigo compósito que compreende partículas e método para formação de um artigo compósito |
| 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 |
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Also Published As
| Publication number | Publication date |
|---|---|
| US20100233424A1 (en) | 2010-09-16 |
| EP2406071B1 (en) | 2016-03-02 |
| EP2406071A1 (en) | 2012-01-18 |
| JP2017213900A (ja) | 2017-12-07 |
| ES2564837T3 (es) | 2016-03-29 |
| JP6162186B2 (ja) | 2017-07-12 |
| JP2016020206A (ja) | 2016-02-04 |
| WO2010104741A1 (en) | 2010-09-16 |
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