BRPI0402616A - Estrutura de construção leve - Google Patents

Estrutura de construção leve

Info

Publication number
BRPI0402616A
BRPI0402616A BRPI0402616A BRPI0402616A BR PI0402616 A BRPI0402616 A BR PI0402616A BR PI0402616 A BRPI0402616 A BR PI0402616A BR PI0402616 A BRPI0402616 A BR PI0402616A
Authority
BR
Brazil
Prior art keywords
adhesive
fibres
lightweight structure
reinforced
aid
Prior art date
Application number
Other languages
English (en)
Inventor
Hans-Juergen Schmidt
Alexei Vichniakov
Original Assignee
Airbus Gmbh
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 Airbus Gmbh filed Critical Airbus Gmbh
Publication of BRPI0402616A publication Critical patent/BRPI0402616A/pt
Publication of BRPI0402616B1 publication Critical patent/BRPI0402616B1/pt

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
    • B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B15/08—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
    • 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
    • B32B15/02—Layer formed of wires, e.g. mesh
    • 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
    • B32B3/14—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 face layer formed of separate pieces of material which are juxtaposed side-by-side
    • 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
    • B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
    • B32B7/04—Interconnection of layers
    • B32B7/12—Interconnection of layers using interposed adhesives or interposed materials with bonding properties
    • 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
    • B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
    • B32B2260/02—Composition of the impregnated, bonded or embedded layer
    • B32B2260/021—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
    • B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/02—Synthetic macromolecular fibres
    • B32B2262/0261—Polyamide fibres
    • B32B2262/0269—Aromatic polyamide fibres
    • 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
    • B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/10—Inorganic fibres
    • 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
    • B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/10—Inorganic fibres
    • B32B2262/101—Glass fibres
    • 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
    • B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/10—Inorganic fibres
    • B32B2262/106—Carbon fibres, e.g. graphite fibres
    • 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
    • B32B2305/00—Condition, form or state of the layers or laminate
    • B32B2305/08—Reinforcements
    • 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
    • B32B2311/00—Metals, their alloys or their compounds
    • B32B2311/18—Titanium
    • 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
    • Y10T428/249921—Web or sheet containing structurally defined element or component
    • Y10T428/249924—Noninterengaged fiber-containing paper-free web or sheet which is not of specified porosity

Landscapes

  • Laminated Bodies (AREA)
  • Rod-Shaped Construction Members (AREA)

Abstract

"ESTRUTURA DE CONSTRUçãO LEVE". A presente invenção refere-se a uma estrutura de construção leve que consiste em um revestimento externo bem como em uma estrutura de reforço montada no dito revestimento e unida a ele por colagem, assim como em uma camada adicional, reforçada por fibras, aplicada também por colagem, entre o revestimento externo e a estrutura de reforço. As fibras são integradas, antes ou depois do processo de colagem, em uma matriz de material sintético e podem ser posicionadas tanto de maneira unidimensional ou ser unidas a estruturas tecidas de maneira bidimensional.
BRPI0402616 2003-07-08 2004-07-06 estrutura de construÇço leve BRPI0402616B1 (pt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE10330708 2003-07-08

Publications (2)

Publication Number Publication Date
BRPI0402616A true BRPI0402616A (pt) 2005-05-17
BRPI0402616B1 BRPI0402616B1 (pt) 2013-07-02

Family

ID=33441649

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0402616 BRPI0402616B1 (pt) 2003-07-08 2004-07-06 estrutura de construÇço leve

Country Status (7)

Country Link
US (1) US7753312B2 (pt)
EP (1) EP1495859B1 (pt)
AT (1) ATE406998T1 (pt)
BR (1) BRPI0402616B1 (pt)
CA (1) CA2473350C (pt)
DE (1) DE502004007968D1 (pt)
RU (1) RU2352464C2 (pt)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10238460B3 (de) * 2002-08-22 2004-03-11 Airbus Deutschland Gmbh Leichtbaustruktur aus dünnen Metallblechlagen
EP1495858B1 (de) * 2003-07-08 2019-08-07 Airbus Operations GmbH Leichtbaustruktur aus metallischen schichtwerkstoffen
DE10360808B4 (de) * 2003-12-19 2005-10-27 Airbus Deutschland Gmbh Faserverstärkter metallischer Verbundwerkstoff
DE102006007428A1 (de) * 2006-02-17 2007-08-30 Airbus Deutschland Gmbh Verstärkungsmaterial zur lokalen Verstärkung eines mit einem Verbundmaterial gebildeten Bauteils sowie Verfahren
US20080000577A1 (en) * 2006-06-07 2008-01-03 Airbus Deutschland Gmbh Adhesive bonding arrangement for adhesively bonding two structural elements and method for producing an adhesive bond between two structural elements
KR101093224B1 (ko) * 2010-12-14 2011-12-13 주식회사 신영 다중결합소재
US10730252B2 (en) * 2015-03-23 2020-08-04 Khalifa University of Science and Technology Lightweight composite single-skin sandwich lattice structures
US11338899B2 (en) * 2018-04-05 2022-05-24 The Boeing Company Joint for a metal airplane skin using metal matrix composite
EP3702263A1 (en) * 2019-02-28 2020-09-02 Airbus Operations GmbH Aircraft structure for flow control
US11549391B2 (en) 2021-03-22 2023-01-10 General Electric Company Component formed from hybrid material

Family Cites Families (96)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1775386A (en) * 1928-05-02 1930-09-09 Blondin Joseph Aircraft supporting and controlling surface
US3058704A (en) * 1958-01-16 1962-10-16 Johnson & Johnson Laminated adhesive sheeting for aircraft
US3071217A (en) * 1960-01-15 1963-01-01 Avro Aircraft Ltd Vibration damping in sheet metal structures
US3401025A (en) * 1965-05-03 1968-09-10 Boeing Co Bonded article comprising two metallic members joined by an intermediate layer
US3490983A (en) * 1965-05-17 1970-01-20 Hitco Fiber reinforced structures and methods of making the same
US3416756A (en) * 1966-08-03 1968-12-17 Dow Chemical Co Airfoil structure
US3768760A (en) * 1970-10-30 1973-10-30 Hercules Inc Graphite fiber composite covering employing multi-directional
US3700517A (en) * 1970-11-24 1972-10-24 Us Army Method for arresting propagating fractures in stressed-skin monocoque type of construction
US3779487A (en) * 1971-04-19 1973-12-18 L Ashton Light weight contoured load carrying structure
US3885071A (en) * 1972-08-10 1975-05-20 Lockheed Aircraft Corp Fiber-reinforced epoxy composite joints
US4015035A (en) * 1972-08-10 1977-03-29 Lockheed Aircraft Corporation Method of forming fiber-reinforced epoxy composite joints, and product thereof
US3771748A (en) * 1972-10-10 1973-11-13 I M Ind Kynock Ltd Structures
US3995081A (en) * 1974-10-07 1976-11-30 General Dynamics Corporation Composite structural beams and method
US4086378A (en) * 1975-02-20 1978-04-25 Mcdonnell Douglas Corporation Stiffened composite structural member and method of fabrication
US4052523A (en) * 1976-09-14 1977-10-04 The United States Of America As Represented By The National Aeronautics And Space Administration Composite sandwich lattice structure
US4269884A (en) * 1979-10-10 1981-05-26 Allied Chemical Corporation Fiber reinforced multi-ply stampable thermoplastic sheet
SU901372A1 (ru) 1980-02-05 1982-01-30 Предприятие П/Я В-8570 Асбестова пр жа
NL8100087A (nl) * 1981-01-09 1982-08-02 Tech Hogeschool Delft Afdeling Laminaat uit metalen platen en daarmede verbonden draden.
US4411380A (en) * 1981-06-30 1983-10-25 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Metal matrix composite structural panel construction
JPS6199655A (ja) * 1984-10-18 1986-05-17 Toyota Motor Corp 鉱物繊維強化金属複合材料
DE3614618A1 (de) * 1986-04-30 1987-11-05 Messerschmitt Boelkow Blohm Schalenstruktur aus faserverstaerktem kunststoff
US5151311A (en) * 1987-11-02 1992-09-29 Grumman Aerospace Corporation Acoustic attenuating liner and method of making same
SU1526076A1 (ru) 1987-12-14 1992-01-30 Институт Механики Полимеров Ан Латвсср Пространственно-армированный композиционный материал и устройство дл его изготовлени
US5641366A (en) * 1988-01-20 1997-06-24 Loral Vought Systems Corporation Method for forming fiber-reinforced composite
US5200256A (en) * 1989-01-23 1993-04-06 Dunbar C R Composite lightweight bullet proof panel for use on vessels, aircraft and the like
US5106668A (en) * 1989-06-07 1992-04-21 Hexcel Corporation Multi-layer honeycomb structure
EP0414110A3 (en) * 1989-08-21 1992-04-08 The B.F. Goodrich Company Compression molded flame retardant and high impact strength ultra high molecular weight polyethylene composition
US5251849A (en) * 1989-12-26 1993-10-12 Florida International University For Board Of Regents Strain reduced airplane skin
US5223067A (en) * 1990-02-28 1993-06-29 Fuji Jukogyo Kabushiki Kaisha Method of fabricating aircraft fuselage structure
US5087511A (en) * 1990-08-31 1992-02-11 General Electric Company Composite element having a variable density core
FR2668470B1 (fr) * 1990-10-29 1992-12-24 Saint Gobain Isover Procede et dispositif de production de fibres par centrifugation interne et application au fibrage de certains verres.
US6086975A (en) * 1991-01-16 2000-07-11 The Boeing Company Lighting protection for electrically conductive or insulating skin and core for honeycomb structure
GB9101354D0 (en) * 1991-01-22 1991-03-06 Short Brothers Plc Noise attentuation panel
GB2253185A (en) 1991-03-01 1992-09-02 Secr Defence Reinforced alloy laminates
US5352529A (en) * 1991-05-13 1994-10-04 Auto-Air Composites, Inc. Lightweight thrust vectoring panel
RU2100498C1 (ru) 1992-04-03 1997-12-27 Дсм Н.В. Слой из нетканого материала, слоистая структура (варианты), способ изготовления слоя из нетканого материала
NL9200625A (nl) * 1992-04-03 1993-11-01 Dsm Nv Niet-geweven uit polyolefinevezels bestaande laag voor toepassing in een gelaagde antiballistische structuur.
US5242523A (en) * 1992-05-14 1993-09-07 The Boeing Company Caul and method for bonding and curing intricate composite structures
AT398064B (de) * 1992-07-01 1994-09-26 Hoac Austria Flugzeugwerk Wr N Kunststoff-verbundprofil, insbesondere flügelholm für den flugzeugbau
DE4322108C2 (de) * 1992-07-03 2001-08-09 Toyoda Gosei Kk Verstärkte Polypropylenharzmischung und daraus hergestellte Radkappe
US5429326A (en) * 1992-07-09 1995-07-04 Structural Laminates Company Spliced laminate for aircraft fuselage
US5599874A (en) * 1993-08-25 1997-02-04 Caterpillar Inc. Thermoplastic polyurethane elastomer based on a hydroxyl terminated polyol, an aromatic chain extender and 1,5 naphthalene diisocyanate
US5451377A (en) * 1993-09-29 1995-09-19 Rockwell International Corp. Composite structures and methods of manufacturing such structures
US5578384A (en) * 1995-12-07 1996-11-26 Ticomp, Inc. Beta titanium-fiber reinforced composite laminates
FR2719553B1 (fr) * 1994-05-04 1996-07-26 Eurocopter France Dispositif anti-couple à rotor arrière et stator redresseur carénés pour hélicoptère.
US5520532A (en) * 1994-08-01 1996-05-28 United Technologies Corporation Molding assembly for forming airfoil structures
US5622733A (en) * 1994-10-04 1997-04-22 Rockwell International Corporation Tooling for the fabrication of composite hollow crown-stiffened skins and panels
US5667866A (en) * 1995-05-02 1997-09-16 The Nordam Group, Inc. Multi-layered, unbalanced sandwich panel
US6025048A (en) * 1995-06-29 2000-02-15 The Regents Of The University Of California Hybrid ceramic matrix composite laminates
US5866272A (en) * 1996-01-11 1999-02-02 The Boeing Company Titanium-polymer hybrid laminates
US5895699A (en) * 1996-03-15 1999-04-20 The Boeing Company Tiedown ply for reducing core crush in composite honeycomb sandwich structure
EP0883484A1 (en) * 1996-01-11 1998-12-16 The Boeing Company Composite honeycomb sandwich structure
RU2102227C1 (ru) 1996-01-22 1998-01-20 Акционерное общество открытого типа "Фибробетон" Многослойный строительный элемент и способ его изготовления
US5902756A (en) * 1996-07-25 1999-05-11 Northrop Grumman Corporation Ceramic matrix composites with integrated topcoat layers
US5804278A (en) * 1997-01-03 1998-09-08 Fixtures Manufacturing Corporation Laminated panel construction with honeycomb grid core
US5851647A (en) * 1997-02-14 1998-12-22 Hollingsworth & Vose Company Nonwoven metal and glass
US6641893B1 (en) * 1997-03-14 2003-11-04 Massachusetts Institute Of Technology Functionally-graded materials and the engineering of tribological resistance at surfaces
JPH10258463A (ja) * 1997-03-19 1998-09-29 Fuji Heavy Ind Ltd 複合材の小骨およびその成形方法
US5919177A (en) * 1997-03-28 1999-07-06 Kimberly-Clark Worldwide, Inc. Permeable fiber-like film coated nonwoven
US6736919B1 (en) 1997-05-28 2004-05-18 Structural Laminates Company Method for making a laminate and laminate obtainable by said method
KR100217487B1 (ko) * 1997-06-03 1999-09-01 맹섭 골프채의 헤드커버
US6105902A (en) * 1997-07-15 2000-08-22 Mcdonnell Douglas Corporation Aircraft fuselage and method of forming same
US6458309B1 (en) * 1998-06-01 2002-10-01 Rohr, Inc. Method for fabricating an advanced composite aerostructure article having an integral co-cured fly away hollow mandrel
JP2000043796A (ja) * 1998-07-30 2000-02-15 Japan Aircraft Development Corp 複合材の翼形構造およびその成形方法
US6230465B1 (en) * 1998-08-04 2001-05-15 Oldcastle Precast, Inc. Precast concrete structural modules
DE19844035C1 (de) * 1998-09-25 1999-11-25 Daimler Chrysler Aerospace Schalenbauteil für ein Flugzeug und Verfahren zur Herstellung
US6190484B1 (en) * 1999-02-19 2001-02-20 Kari Appa Monolithic composite wing manufacturing process
DE19924909C1 (de) * 1999-05-31 2000-06-21 Daimler Chrysler Ag Metallisches Schalenbauteil
US6889937B2 (en) * 1999-11-18 2005-05-10 Rocky Mountain Composites, Inc. Single piece co-cure composite wing
US6655633B1 (en) * 2000-01-21 2003-12-02 W. Cullen Chapman, Jr. Tubular members integrated to form a structure
DE10007995C2 (de) * 2000-02-22 2002-03-07 Airbus Gmbh Strukturbauteil, insbesondere für ein Flugzeug und Verfahren zur Herstellung eines Strukturbauteils
JP4416900B2 (ja) * 2000-03-10 2010-02-17 富士重工業株式会社 複合材パネルおよびその製造方法
JP4318381B2 (ja) * 2000-04-27 2009-08-19 本田技研工業株式会社 繊維強化複合材からなる胴体構造体の製造方法、及びそれにより製造される胴体構造体
DE10031510A1 (de) * 2000-06-28 2002-01-17 Airbus Gmbh Strukturbauteil für ein Flugzeug
US6712315B2 (en) * 2000-11-30 2004-03-30 Airbus Deutschland Gmbh Metal structural component for an aircraft, with resistance to crack propagation
US7226559B2 (en) * 2000-12-08 2007-06-05 Toyota Motor Sales, U.S.A., Inc. Method for molding structures
RU2192493C2 (ru) 2000-12-19 2002-11-10 Государственное предприятие Всероссийский научно-исследовательский институт авиационных материалов Сплав на основе титана и изделие, выполненное из него
JP4526698B2 (ja) * 2000-12-22 2010-08-18 富士重工業株式会社 複合材成形品及びその製造方法
US7124797B2 (en) * 2001-03-02 2006-10-24 Toyota Motor Sales, Usa, Inc. Filament winding apparatus and methods of winding filament
SE519185C2 (sv) * 2001-06-07 2003-01-28 Saab Ab Flygplanspanel
GB0113916D0 (en) * 2001-06-07 2001-08-01 Bae Systems Plc Adding glass to composite bonding surfaces
JP4574086B2 (ja) * 2001-09-03 2010-11-04 富士重工業株式会社 複合材翼の製造方法および複合材翼
GB0122050D0 (en) * 2001-09-13 2001-10-31 Bae Systems Plc Composite material structure
US6648273B2 (en) * 2001-10-30 2003-11-18 The Boeing Company Light weight and high strength fuselage
US6825137B2 (en) * 2001-12-19 2004-11-30 Telair International Incorporated Lightweight ballistic resistant rigid structural panel
EP1336469A1 (en) * 2002-02-19 2003-08-20 Alenia Aeronautica S.P.A. Methods of manufacturing a stiffening element for an aircraft skin panel and a skin panel provided with the stiffening element
US6779830B2 (en) * 2002-04-09 2004-08-24 Ford Global Technologies, Llc Anti-intrusion beam for a vehicle door assembly
US7204951B2 (en) * 2002-07-30 2007-04-17 Rocky Mountain Composites, Inc. Method of assembling a single piece co-cured structure
DE10238460B3 (de) 2002-08-22 2004-03-11 Airbus Deutschland Gmbh Leichtbaustruktur aus dünnen Metallblechlagen
US20040035979A1 (en) * 2002-08-23 2004-02-26 Mccoskey William Robert Integrally stiffened axial load carrying skin panels for primary aircraft structure and closed loop manufacturing methods for making the same
US7093470B2 (en) * 2002-09-24 2006-08-22 The Boeing Company Methods of making integrally stiffened axial load carrying skin panels for primary aircraft structure and fuel tank structures
EP1495858B1 (de) * 2003-07-08 2019-08-07 Airbus Operations GmbH Leichtbaustruktur aus metallischen schichtwerkstoffen
DE10360808B4 (de) * 2003-12-19 2005-10-27 Airbus Deutschland Gmbh Faserverstärkter metallischer Verbundwerkstoff
US7481398B2 (en) * 2004-02-25 2009-01-27 Airbus Deutschland Gmbh Intercostal for aircraft
EP1666354B1 (de) * 2004-12-01 2010-09-29 Airbus Operations GmbH Strukturbauteil, Verfahren zum Herstellen eines Strukturbauteils und Verwendung eines Strukturbauteils für eine Flugzeugschale
US7255916B2 (en) * 2005-01-04 2007-08-14 Airbus Deutschland Gmbh Metallic layer material, reinforced with basalt fibers, as well as products made thereof

Also Published As

Publication number Publication date
BRPI0402616B1 (pt) 2013-07-02
US7753312B2 (en) 2010-07-13
ATE406998T1 (de) 2008-09-15
EP1495859A1 (de) 2005-01-12
RU2352464C2 (ru) 2009-04-20
RU2004120841A (ru) 2006-01-10
CA2473350C (en) 2011-11-29
DE502004007968D1 (de) 2008-10-16
CA2473350A1 (en) 2005-01-08
US20050112347A1 (en) 2005-05-26
EP1495859B1 (de) 2008-09-03

Similar Documents

Publication Publication Date Title
DE502006002968D1 (de) Faserverbund-Werkstoff und Verfahren zu dessen Herstellung
DE502005007872D1 (de) Kunststoff-Verbundscheibe für die Fahrzeugverscheibung
TW200621499A (en) Sandwich structure and integrated molding using the same
ATE339344T1 (de) Verbesserte konstruktionsverstärkung
ATE517134T1 (de) Zwei-komponenten klebstoff
DE502005005367D1 (de) Holzwerkstoffplatte sowie ein Verfahren zum Herstellen einer Holzwerkstoffplatte
AU2006289279A1 (en) Reinforcing body made of fibre-reinforced plastic
BRPI0402616A (pt) Estrutura de construção leve
PL1863629T3 (pl) Sposób produkcji części kompozytowych wzmocnionych włóknami
WO2008127812A3 (en) Sign post comprising composite material
JP2005506217A5 (pt)
BRPI0518219A (pt) artigo adesivo, métodos de ligação, e de aumento da rigidez de um substrato, uso de um artigo adesivo, e, método de produção de um artigo adesivo
BRPI0602465A (pt) material de reforço composto isolado
ATE452024T1 (de) Verbundbauteil für eine fahrzeugkarosserie, insbesondere ein fahrzeugdach, sowie herstellungsverfahren dafür
FR2902689B1 (fr) Panneau raidi a raidisseurs composites a sensibilite aux chocs diminuee
BRPI0506501A (pt) processo de fabricação de uma armação à base de fibras e armação à base de fibras
DE60025973D1 (de) Formteil sowie Verfahren zu seiner Herstellung
DE50204958D1 (de) Natursteinplatte und verfahren zur herstellung
DE502004004996D1 (de) Verbundbauteil, sowie Verfahren zu dessen Herstellung
ATE348230T1 (de) Leichtbauelement mit fliesen und verfahren zu dessen herstellung
WO2003093098A3 (en) Boat hull construction
ATE324495T1 (de) Verstärkte rohrstrukturen
DE50301416D1 (de) Verbundmaterial
WO2004067817A3 (en) Fiber and resin composite reinforcement
HUP0600053A2 (en) Construction element, especially sandwich-panel, as well as method of producing this kind of construction element

Legal Events

Date Code Title Description
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 06/07/2004, OBSERVADAS AS CONDICOES LEGAIS.

B21F Lapse acc. art. 78, item iv - on non-payment of the annual fees in time
B24J Lapse because of non-payment of annual fees (definitively: art 78 iv lpi, resolution 113/2013 art. 12)