WO2005110736A2 - Aluminum-fiber laminate - Google Patents
Aluminum-fiber laminate Download PDFInfo
- Publication number
- WO2005110736A2 WO2005110736A2 PCT/US2005/002858 US2005002858W WO2005110736A2 WO 2005110736 A2 WO2005110736 A2 WO 2005110736A2 US 2005002858 W US2005002858 W US 2005002858W WO 2005110736 A2 WO2005110736 A2 WO 2005110736A2
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- laminate
- aluminum alloy
- fibers
- metallic layers
- layers
- Prior art date
Links
Classifications
-
- 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
- B32B15/00—Layered products comprising a layer of metal
- B32B15/14—Layered products comprising a layer of metal next to a fibrous or filamentary layer
-
- 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
- B32B15/00—Layered products comprising a layer of metal
- B32B15/18—Layered products comprising a layer of metal comprising iron or steel
-
- 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
- B32B15/00—Layered products comprising a layer of metal
- B32B15/20—Layered products comprising a layer of metal comprising aluminium or copper
-
- 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 form; Layered products 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 form; Layered products having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
- B32B3/12—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material characterised by a layer of regularly- arranged cells, e.g. a honeycomb structure
-
- 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
- B32B2307/00—Properties of the layers or laminate
- B32B2307/70—Other properties
- B32B2307/714—Inert, i.e. inert to chemical degradation, corrosion
-
- 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
- B32B2605/00—Vehicles
- B32B2605/18—Aircraft
-
- 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
-
- 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.]
- Y10T428/24149—Honeycomb-like
Landscapes
- Laminated Bodies (AREA)
Abstract
Description
Claims
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2006553149A JP5300197B2 (en) | 2004-02-10 | 2005-02-02 | Aluminum-fiber laminate |
CA2556234A CA2556234C (en) | 2004-02-10 | 2005-02-02 | Aluminum-fiber laminate |
CN2005800122756A CN1950200B (en) | 2004-02-10 | 2005-02-02 | Aluminum-fiber laminate |
EP05779475.2A EP1718459B1 (en) | 2004-02-10 | 2005-02-02 | Aluminum-fiber laminate |
AU2005243765A AU2005243765A1 (en) | 2004-02-10 | 2005-02-02 | Aluminum-fiber laminate |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10/775,564 US20050175813A1 (en) | 2004-02-10 | 2004-02-10 | Aluminum-fiber laminate |
US10/775,564 | 2004-02-10 |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2005110736A2 true WO2005110736A2 (en) | 2005-11-24 |
WO2005110736A3 WO2005110736A3 (en) | 2006-03-30 |
Family
ID=34827228
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US2005/002858 WO2005110736A2 (en) | 2004-02-10 | 2005-02-02 | Aluminum-fiber laminate |
Country Status (7)
Country | Link |
---|---|
US (2) | US20050175813A1 (en) |
EP (1) | EP1718459B1 (en) |
JP (1) | JP5300197B2 (en) |
CN (1) | CN1950200B (en) |
AU (1) | AU2005243765A1 (en) |
CA (1) | CA2556234C (en) |
WO (1) | WO2005110736A2 (en) |
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JP2008082332A (en) * | 2006-09-25 | 2008-04-10 | General Electric Co <Ge> | Blade containment system for gas turbine engine |
WO2008053041A1 (en) * | 2006-11-03 | 2008-05-08 | Airbus Deutschland Gmbh | Stiffened casing for an aircraft or spacecraft with a laminate stringer of high rigidity and corresponding laminate stringer |
WO2008133296A1 (en) * | 2007-04-24 | 2008-11-06 | Taisei Plas Co., Ltd. | Stainless steel complex and its manufacturing method |
EP2085215A1 (en) | 2008-01-29 | 2009-08-05 | GTM Holding B.V. | High-toughness fiber-metal laminate |
EP2143558A1 (en) * | 2007-04-13 | 2010-01-13 | Taisei Plas Co., Ltd. | Titanium alloy compound material, and its jointing method |
EP2153985A1 (en) * | 2007-05-28 | 2010-02-17 | Taisei Plas Co., Ltd. | Steel product composite and process for producing the steel product composite |
EP2409831A1 (en) * | 2010-07-21 | 2012-01-25 | Iwao Hishida | Processing Method of Metal Product Surface |
EP2965902A1 (en) * | 2014-07-09 | 2016-01-13 | Hydro Aluminium Rolled Products GmbH | Multilayer structural component, method for producing the same and use thereof, and system comprising such a structural component |
DE102020131895A1 (en) | 2020-12-01 | 2022-06-02 | Airbus Operations Gmbh | Method for applying an anti-corrosion layer to a component surface to be protected |
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NL1030515C2 (en) * | 2005-11-24 | 2007-05-25 | Gtm Consulting B V | Laminate from metal sheets and plastic. |
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US7595112B1 (en) | 2006-07-31 | 2009-09-29 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Resin infusion of layered metal/composite hybrid and resulting metal/composite hybrid laminate |
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US7851062B2 (en) * | 2007-06-04 | 2010-12-14 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Metal/fiber laminate and fabrication using a porous metal/fiber preform |
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US20100078259A1 (en) * | 2008-09-30 | 2010-04-01 | Honeywell International Inc. | Flowbodies and methods of forming flowbodies |
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US9415568B2 (en) | 2010-02-15 | 2016-08-16 | Productive Research Llc | Formable light weight composite material systems and methods |
US10214827B2 (en) | 2010-05-19 | 2019-02-26 | Sanford Process Corporation | Microcrystalline anodic coatings and related methods therefor |
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US20110300358A1 (en) * | 2010-06-04 | 2011-12-08 | The Boeing Company | Shape memory alloy/fiber reinforced polymeric composite structures and method for forming |
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EP0323660A1 (en) * | 1987-12-31 | 1989-07-12 | Akzo N.V. | Process for manufacturing a laminate of metal sheets and filaments-reinforced synthetic layers |
US5429326A (en) * | 1992-07-09 | 1995-07-04 | Structural Laminates Company | Spliced laminate for aircraft fuselage |
US6736919B1 (en) * | 1997-05-28 | 2004-05-18 | Structural Laminates Company | Method for making a laminate and laminate obtainable by said method |
WO2004071761A1 (en) * | 2003-02-17 | 2004-08-26 | Stichting Fmlc | Laminate of metal plates and intersecting fibre layers |
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2004
- 2004-02-10 US US10/775,564 patent/US20050175813A1/en not_active Abandoned
-
2005
- 2005-02-02 WO PCT/US2005/002858 patent/WO2005110736A2/en active Application Filing
- 2005-02-02 CA CA2556234A patent/CA2556234C/en not_active Expired - Fee Related
- 2005-02-02 JP JP2006553149A patent/JP5300197B2/en not_active Expired - Fee Related
- 2005-02-02 EP EP05779475.2A patent/EP1718459B1/en not_active Not-in-force
- 2005-02-02 CN CN2005800122756A patent/CN1950200B/en not_active Expired - Fee Related
- 2005-02-02 AU AU2005243765A patent/AU2005243765A1/en not_active Abandoned
- 2005-03-03 US US11/072,851 patent/US20050271859A1/en not_active Abandoned
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Cited By (21)
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JP2008082332A (en) * | 2006-09-25 | 2008-04-10 | General Electric Co <Ge> | Blade containment system for gas turbine engine |
WO2008053041A1 (en) * | 2006-11-03 | 2008-05-08 | Airbus Deutschland Gmbh | Stiffened casing for an aircraft or spacecraft with a laminate stringer of high rigidity and corresponding laminate stringer |
US8317134B2 (en) | 2006-11-03 | 2012-11-27 | Aribus Deutschland GmbH | Stiffened casing for an aircraft or spacecraft with a laminate stringer of high rigidity and corresponding laminate stringer |
JP2010508203A (en) * | 2006-11-03 | 2010-03-18 | エアバス・オペレーションズ・ゲーエムベーハー | Aircraft or spacecraft hardened enclosure with highly rigid laminated longitudinal members and corresponding laminated longitudinal members |
EP2143558A1 (en) * | 2007-04-13 | 2010-01-13 | Taisei Plas Co., Ltd. | Titanium alloy compound material, and its jointing method |
EP2143558A4 (en) * | 2007-04-13 | 2010-07-14 | Taisei Plas Co Ltd | Titanium alloy compound material, and its jointing method |
EP2141014A1 (en) * | 2007-04-24 | 2010-01-06 | Taisei Plas Co., Ltd. | Stainless steel complex and its manufacturing method |
JPWO2008133296A1 (en) * | 2007-04-24 | 2010-07-29 | 大成プラス株式会社 | Stainless steel composite and its manufacturing method |
JP5094849B2 (en) * | 2007-04-24 | 2012-12-12 | 大成プラス株式会社 | Stainless steel composite |
EP2141014A4 (en) * | 2007-04-24 | 2010-07-14 | Taisei Plas Co Ltd | Stainless steel complex and its manufacturing method |
WO2008133296A1 (en) * | 2007-04-24 | 2008-11-06 | Taisei Plas Co., Ltd. | Stainless steel complex and its manufacturing method |
EP2153985A4 (en) * | 2007-05-28 | 2010-07-14 | Taisei Plas Co Ltd | Steel product composite and process for producing the steel product composite |
EP2476549A1 (en) * | 2007-05-28 | 2012-07-18 | Taisei Plas Co., Ltd. | Steel material composite and manufacturing method thereof |
EP2153985A1 (en) * | 2007-05-28 | 2010-02-17 | Taisei Plas Co., Ltd. | Steel product composite and process for producing the steel product composite |
KR101216800B1 (en) * | 2007-05-28 | 2013-01-10 | 다이세이 플라스 가부시끼가이샤 | Steel product composite and process for producing the steel product composite |
EP2085215A1 (en) | 2008-01-29 | 2009-08-05 | GTM Holding B.V. | High-toughness fiber-metal laminate |
WO2009095381A1 (en) * | 2008-01-29 | 2009-08-06 | Gtm Holding B.V. | High toughness fiber-metal laminate |
EP2409831A1 (en) * | 2010-07-21 | 2012-01-25 | Iwao Hishida | Processing Method of Metal Product Surface |
US8961734B2 (en) | 2010-07-21 | 2015-02-24 | Iwao Hishida | Processing method of metal product surface |
EP2965902A1 (en) * | 2014-07-09 | 2016-01-13 | Hydro Aluminium Rolled Products GmbH | Multilayer structural component, method for producing the same and use thereof, and system comprising such a structural component |
DE102020131895A1 (en) | 2020-12-01 | 2022-06-02 | Airbus Operations Gmbh | Method for applying an anti-corrosion layer to a component surface to be protected |
Also Published As
Publication number | Publication date |
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JP2007521995A (en) | 2007-08-09 |
JP5300197B2 (en) | 2013-09-25 |
EP1718459A2 (en) | 2006-11-08 |
CA2556234C (en) | 2013-11-19 |
WO2005110736A3 (en) | 2006-03-30 |
US20050271859A1 (en) | 2005-12-08 |
CA2556234A1 (en) | 2005-11-24 |
US20050175813A1 (en) | 2005-08-11 |
EP1718459B1 (en) | 2017-11-22 |
AU2005243765A1 (en) | 2005-11-24 |
CN1950200A (en) | 2007-04-18 |
CN1950200B (en) | 2012-09-19 |
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