CN1950200B - 铝-纤维层压体 - Google Patents

铝-纤维层压体 Download PDF

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Publication number
CN1950200B
CN1950200B CN2005800122756A CN200580012275A CN1950200B CN 1950200 B CN1950200 B CN 1950200B CN 2005800122756 A CN2005800122756 A CN 2005800122756A CN 200580012275 A CN200580012275 A CN 200580012275A CN 1950200 B CN1950200 B CN 1950200B
Authority
CN
China
Prior art keywords
layered product
described layered
fiber
layer
metal
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.)
Expired - Fee Related
Application number
CN2005800122756A
Other languages
English (en)
Chinese (zh)
Other versions
CN1950200A (zh
Inventor
威拉德·N·韦斯特尔
A·卢·温格特
斯文·E·阿克斯特
加里·D·塔斯
爱德华·李
莫·K·索莱曼
威廉·B·格雷斯
凯·Y·布洛豪伊亚克
朱迪·S·陈
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Boeing Co
Original Assignee
Boeing Co
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Boeing Co filed Critical Boeing Co
Publication of CN1950200A publication Critical patent/CN1950200A/zh
Application granted granted Critical
Publication of CN1950200B publication Critical patent/CN1950200B/zh
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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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 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
    • B32B3/12—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 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)
CN2005800122756A 2004-02-10 2005-02-02 铝-纤维层压体 Expired - Fee Related CN1950200B (zh)

Applications Claiming Priority (3)

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
PCT/US2005/002858 WO2005110736A2 (en) 2004-02-10 2005-02-02 Aluminum-fiber laminate

Publications (2)

Publication Number Publication Date
CN1950200A CN1950200A (zh) 2007-04-18
CN1950200B true CN1950200B (zh) 2012-09-19

Family

ID=34827228

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2005800122756A Expired - Fee Related CN1950200B (zh) 2004-02-10 2005-02-02 铝-纤维层压体

Country Status (7)

Country Link
US (2) US20050175813A1 (enExample)
EP (1) EP1718459B1 (enExample)
JP (1) JP5300197B2 (enExample)
CN (1) CN1950200B (enExample)
AU (1) AU2005243765A1 (enExample)
CA (1) CA2556234C (enExample)
WO (1) WO2005110736A2 (enExample)

Families Citing this family (67)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL1030515C2 (nl) * 2005-11-24 2007-05-25 Gtm Consulting B V Laminaat uit metaalplaten en kunststof.
US20100043939A1 (en) * 2006-05-15 2010-02-25 Alcoa, Inc. Reinforced Hybrid Structures and Methods Thereof
NL2000100C2 (nl) * 2006-06-13 2007-12-14 Gtm Consulting B V Laminaat uit metaalplaten en kunststof.
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
CA2602319A1 (en) * 2006-09-25 2008-03-25 General Electric Company Blade containment system for a gas turbine engine
DE102006051989B4 (de) * 2006-11-03 2010-09-30 Airbus Deutschland Gmbh Versteifte Beplankung für ein Luft- oder Raumfahrzeug mit einem Laminat-Stringer hoher Steifigkeit
WO2008133030A1 (ja) * 2007-04-13 2008-11-06 Taisei Plas Co., Ltd. チタン合金複合体とその接合方法
JP5094849B2 (ja) * 2007-04-24 2012-12-12 大成プラス株式会社 ステンレス鋼複合体
US20090211697A1 (en) * 2007-05-15 2009-08-27 Heinimann Markus B Reinforced hybrid structures and methods thereof
KR101216800B1 (ko) * 2007-05-28 2013-01-10 다이세이 플라스 가부시끼가이샤 강재 복합체 및 그 제조 방법
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
EP2085215B1 (en) * 2008-01-29 2013-03-27 GTM Holding B.V. High-toughness fiber-metal laminate
ITMI20080886A1 (it) * 2008-05-15 2009-11-16 Alenia Aermacchi Spa Giunto per indurre elevate cadute di temperatura tra parti collegate su un velivolo
CN102186666B (zh) 2008-08-18 2015-06-24 多产研究有限责任公司 可成型的轻质复合材料
US20100078259A1 (en) * 2008-09-30 2010-04-01 Honeywell International Inc. Flowbodies and methods of forming flowbodies
NL2002289C2 (en) * 2008-12-04 2010-06-07 Gtm Holding B V Sandwich panel, support member for use in a sandwich panel and aircraft provided with such a sandwich panel.
IT1392320B1 (it) * 2008-12-09 2012-02-24 Alenia Aeronautica Spa Bordo d'attacco per ali ed impennaggi di aeromobili
CA2822748C (en) 2009-12-28 2021-06-01 Shimon Mizrahi Processes for welding composite materials and articles therefrom
CN102844178B (zh) 2010-02-15 2015-09-16 多产研究有限责任公司 可成型的轻质复合材料体系及方法
US10214827B2 (en) 2010-05-19 2019-02-26 Sanford Process Corporation Microcrystalline anodic coatings and related methods therefor
US8609254B2 (en) 2010-05-19 2013-12-17 Sanford Process Corporation Microcrystalline anodic coatings and related methods therefor
US20110300358A1 (en) * 2010-06-04 2011-12-08 The Boeing Company Shape memory alloy/fiber reinforced polymeric composite structures and method for forming
KR20120010129A (ko) 2010-07-21 2012-02-02 이와오 히시다 금속제품 표면의 가공방법
ES2541631T3 (es) * 2010-11-29 2015-07-22 Gtm-Advanced Structures B.V. Laminado de material compuesto reforzado fibra-lámina metálica
KR101093224B1 (ko) * 2010-12-14 2011-12-13 주식회사 신영 다중결합소재
TWI445483B (zh) 2010-12-23 2014-07-11 仁寶電腦工業股份有限公司 殼體結構及具有其之電子裝置
JP5779003B2 (ja) * 2011-06-09 2015-09-16 新日鉄住金マテリアルズ株式会社 鋼構造物の補強方法及び鋼構造物補強用積層材
US9090043B2 (en) * 2011-08-03 2015-07-28 The Boeing Company Molybdenum composite hybrid laminates and methods
CN104203752A (zh) 2012-03-26 2014-12-10 三菱重工业株式会社 燃料箱、主翼、航空器主体、航空器及移动体
US9233526B2 (en) 2012-08-03 2016-01-12 Productive Research Llc Composites having improved interlayer adhesion and methods thereof
JP5852255B2 (ja) * 2012-10-09 2016-02-03 三菱重工業株式会社 構造体用構造材、燃料タンク、主翼及び航空機
CN102991009B (zh) * 2012-11-16 2015-02-11 中国航空工业集团公司北京航空材料研究院 一种层间增韧的碳纤维-金属层合板
CN103009717A (zh) * 2012-11-30 2013-04-03 南京航空航天大学 一种轻质耐高温碳纤维金属混杂层板
CN103029376B (zh) * 2012-12-21 2015-12-23 官宇寰 一种金属-纤维复合层板及其制造方法
EP2759399B1 (en) * 2013-01-28 2015-05-13 GS4C S.r.L. Multilayer wall and method for forming said wall
US9253823B2 (en) 2013-02-10 2016-02-02 The Boeing Company Metal matrix composite used as a heating element
JP6113544B2 (ja) * 2013-03-26 2017-04-12 三菱重工業株式会社 燃料タンク、主翼、航空機胴体、航空機及び移動体
JP6071686B2 (ja) * 2013-03-26 2017-02-01 三菱重工業株式会社 燃料タンク、主翼、航空機胴体、航空機及び移動体
CN103332287B (zh) * 2013-06-25 2015-11-25 哈尔滨工业大学 一种承载性能好的抗皱褶可变形蒙皮
CN103342164B (zh) * 2013-06-25 2016-01-27 哈尔滨工业大学 一种便于安装和预紧的复合材料柔性可承载的变形蒙皮
EP3019705B1 (en) 2013-07-09 2019-01-30 United Technologies Corporation High-modulus coating for local stiffening of airfoil trailing edges
CA2917871A1 (en) 2013-07-09 2015-01-15 United Technologies Corporation Plated tubular lattice structure
WO2015006487A1 (en) 2013-07-09 2015-01-15 United Technologies Corporation Erosion and wear protection for composites and plated polymers
EP3019710A4 (en) 2013-07-09 2017-05-10 United Technologies Corporation Plated polymer fan
WO2015017095A2 (en) 2013-07-09 2015-02-05 United Technologies Corporation Plated polymer nosecone
US20160152005A1 (en) * 2013-07-09 2016-06-02 United Technologies Corporation Hybrid plated composite stack
US10927843B2 (en) 2013-07-09 2021-02-23 Raytheon Technologies Corporation Plated polymer compressor
CN103895315B (zh) * 2014-02-19 2016-03-02 南京航空航天大学 Glare构件的制备成形方法
ES2566630T3 (es) * 2014-07-09 2016-04-14 Hydro Aluminium Rolled Products Gmbh Componente estructural multicapa, procedimiento para su producción y uso del mismo así como sistema con un componente estructural de este tipo
CN105522788B (zh) * 2014-11-24 2017-11-21 比亚迪股份有限公司 一种纤维金属层合板及其制备方法
US10458433B2 (en) * 2015-06-17 2019-10-29 United Technologies Corporation Co-molded metallic fan case containment ring
TWM538876U (zh) * 2016-11-22 2017-04-01 Tyko Tech Co Ltd 複合材料結構
US11014337B2 (en) 2016-12-14 2021-05-25 The Boeing Company Laminate structures comprising fiber-reinforced thermoplastic prepreg plies
US11273622B2 (en) 2016-12-14 2022-03-15 The Boeing Company Stiffening elements that comprise integral current flowpaths
US11077644B2 (en) 2016-12-14 2021-08-03 The Boeing Company Material systems and methods of manufacturing material systems
US20180179990A1 (en) 2016-12-27 2018-06-28 Orbital Atk, Inc. Hybrid metal composite structures, rocket motors and multi-stage rocket motor assemblies including hybrid metal composite structures, and related methods
US10919615B2 (en) * 2017-03-29 2021-02-16 The Boeing Company Methods and apparatuses for joining titanium and titanium alloy structures to epoxy-containing compounds
JP7034849B2 (ja) * 2018-06-28 2022-03-14 三菱重工業株式会社 複合材、複合材の製造方法、及び複合材の硬化方法
CA3122507A1 (en) 2018-12-10 2020-06-18 Boston Materials, Inc. Systems and methods for carbon fiber alignment and fiber-reinforced composites
CN109483920B (zh) * 2018-12-18 2020-03-10 燕山大学 碳纤维复合材料与铝合金板材冲压连接的方法及其装置
US11338552B2 (en) 2019-02-15 2022-05-24 Productive Research Llc Composite materials, vehicle applications and methods thereof
CA3146284A1 (en) 2019-07-10 2021-01-14 Boston Materials, Inc. Systems and methods for forming short-fiber films, composites comprising thermosets, and other composites
CN111139410A (zh) * 2020-01-13 2020-05-12 嘉瑞科技（惠州）有限公司 一种纤维加强型铝合金层压复合材料及其制备方法
CN111231366B (zh) * 2020-01-14 2021-06-01 上海交通大学 Cfrp/铝合金热成形淬火时效共固化一体化成形方法
US11802415B2 (en) 2020-10-16 2023-10-31 JXR Constructors, Inc. Continuous composite structural reinforcing device and system
DE102020131895A1 (de) 2020-12-01 2022-06-02 Airbus Operations Gmbh Verfahren zum Anbringen einer Korrosionsschutzlage an einer zu schützenden Oberfläche eines Bauteils
US12428587B1 (en) 2024-09-03 2025-09-30 Boston Materials, Inc. Liquid metal compositions and methods

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0323660A1 (en) * 1987-12-31 1989-07-12 Akzo N.V. Process for manufacturing a laminate of metal sheets and filaments-reinforced synthetic layers
CN1080590A (zh) * 1992-07-03 1994-01-12 中国科学院金属研究所 维尼纶增强铝合金层压复合材料及制备方法
US5429326A (en) * 1992-07-09 1995-07-04 Structural Laminates Company Spliced laminate for aircraft fuselage

Family Cites Families (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL8100088A (nl) * 1981-01-09 1982-08-02 Tech Hogeschool Delft Afdeling Laminaat uit metalen platen en daarmede verbonden draden, alsmede werkwijzen ter vervaardiging daarvan.
NL8100087A (nl) * 1981-01-09 1982-08-02 Tech Hogeschool Delft Afdeling Laminaat uit metalen platen en daarmede verbonden draden.
US4624923A (en) * 1984-06-08 1986-11-25 Yeda Research And Development Company Limited Metal-coated polyaldehyde microspheres
US4877647A (en) * 1986-04-17 1989-10-31 Kansas State University Research Foundation Method of coating substrates with solvated clusters of metal particles
US4818481A (en) * 1987-03-09 1989-04-04 Exxon Research And Engineering Company Method of extruding aluminum-base oxide dispersion strengthened
FR2613372B1 (fr) * 1987-04-03 1989-06-09 Rhone Poulenc Chimie Particules composites polymere/metal compactes, dispersions aqueuses desdites particules, leur procede de preparation et leur application en biologie
EP0312150B1 (en) * 1987-10-14 1992-12-02 Structural Laminates Company Laminate of metal sheets and continuous filaments-reinforced thermoplastic synthetic material, as well as a process for the manufacture of such a laminate
US5160771A (en) * 1990-09-27 1992-11-03 Structural Laminates Company Joining metal-polymer-metal laminate sections
US5231412A (en) * 1990-12-24 1993-07-27 Motorola, Inc. Sleeved monopole antenna
US5578384A (en) * 1995-12-07 1996-11-26 Ticomp, Inc. Beta titanium-fiber reinforced composite laminates
US5609907A (en) * 1995-02-09 1997-03-11 The Penn State Research Foundation Self-assembled metal colloid monolayers
US5866272A (en) * 1996-01-11 1999-02-02 The Boeing Company Titanium-polymer hybrid laminates
US5869141A (en) * 1996-11-04 1999-02-09 The Boeing Company Surface pretreatment for sol coating of metals
US5958578A (en) * 1996-11-04 1999-09-28 The Boeing Company Hybrid laminate having improved metal-to-resin adhesion
JP3725279B2 (ja) * 1997-02-20 2005-12-07 Ｙｋｋ株式会社 高強度、高延性アルミニウム合金
ES2186184T3 (es) * 1997-05-28 2003-05-01 Structural Laminates Co Procedimiento para realizar un laminado y laminado obtenido mediante dicho procedimiento.
US6384798B1 (en) * 1997-09-24 2002-05-07 Magellan Corporation Quadrifilar antenna
US5963971A (en) * 1997-10-09 1999-10-05 International Business Machines Corporation Method and apparatus for handling audit requests of logical volumes in a virtual media server
US6094178A (en) * 1997-11-14 2000-07-25 Ericsson, Inc. Dual mode quadrifilar helix antenna and associated methods of operation
US6441795B1 (en) * 2000-11-29 2002-08-27 Lockheed Martin Corporation Conical horn antenna with flare break and impedance output structure
US6863971B2 (en) * 2001-03-22 2005-03-08 Cycletec Ltd. Strong durable low cost composite materials made from treated cellulose and plastic
EP1401378B1 (en) * 2001-06-12 2008-08-13 Stick Tech OY A prepreg, a composite and their uses
US6805904B2 (en) * 2002-02-20 2004-10-19 International Business Machines Corporation Process of forming a multilayer nanoparticle-containing thin film self-assembly
DE60336140D1 (de) * 2002-06-27 2011-04-07 Teijin Aramid Bv Verfahren zur herstellung von synthetisch-organischen fasern mit hoher festigkeit und/oder hohem modul aus aromatischen heterozyklischen steifen polymeren
US6902699B2 (en) * 2002-10-02 2005-06-07 The Boeing Company Method for preparing cryomilled aluminum alloys and components extruded and forged therefrom
NL1022706C2 (nl) * 2003-02-17 2004-08-19 Stichting Fmlc Laminaat uit metaalplaten en elkaar kruisende dradenlagen uit verschillende materialen in kunststof.
NL1024076C2 (nl) * 2003-08-08 2005-02-10 Stork Fokker Aesp Bv Werkwijze voor het vormen van een laminaat met een uitsparing.

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0323660A1 (en) * 1987-12-31 1989-07-12 Akzo N.V. Process for manufacturing a laminate of metal sheets and filaments-reinforced synthetic layers
CN1080590A (zh) * 1992-07-03 1994-01-12 中国科学院金属研究所 维尼纶增强铝合金层压复合材料及制备方法
US5429326A (en) * 1992-07-09 1995-07-04 Structural Laminates Company Spliced laminate for aircraft fuselage

Also Published As

Publication number Publication date
US20050175813A1 (en) 2005-08-11
CA2556234A1 (en) 2005-11-24
WO2005110736A3 (en) 2006-03-30
EP1718459B1 (en) 2017-11-22
CA2556234C (en) 2013-11-19
AU2005243765A1 (en) 2005-11-24
US20050271859A1 (en) 2005-12-08
EP1718459A2 (en) 2006-11-08
CN1950200A (zh) 2007-04-18
WO2005110736A2 (en) 2005-11-24
JP5300197B2 (ja) 2013-09-25
JP2007521995A (ja) 2007-08-09

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Granted publication date: 20120919

Termination date: 20190202