NL8100087A - Laminaat uit metalen platen en daarmede verbonden draden. - Google Patents

Laminaat uit metalen platen en daarmede verbonden draden. Download PDF

Info

Publication number
NL8100087A
NL8100087A NL8100087A NL8100087A NL8100087A NL 8100087 A NL8100087 A NL 8100087A NL 8100087 A NL8100087 A NL 8100087A NL 8100087 A NL8100087 A NL 8100087A NL 8100087 A NL8100087 A NL 8100087A
Authority
NL
Netherlands
Prior art keywords
laminate according
metal plates
threads
laminate
aluminum
Prior art date
Application number
NL8100087A
Other languages
English (en)
Dutch (nl)
Original Assignee
Tech Hogeschool Delft Afdeling
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=19836834&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=NL8100087(A) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Tech Hogeschool Delft Afdeling filed Critical Tech Hogeschool Delft Afdeling
Priority to NL8100087A priority Critical patent/NL8100087A/nl
Priority to DE8282200014T priority patent/DE3267655D1/de
Priority to EP82200014A priority patent/EP0056289B1/de
Priority to JP57001106A priority patent/JPS57137148A/ja
Priority to IE36/82A priority patent/IE53179B1/en
Priority to AT82200014T priority patent/ATE16778T1/de
Publication of NL8100087A publication Critical patent/NL8100087A/nl
Priority to US06/533,883 priority patent/US4500589A/en

Links

Classifications

    • 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
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/06—Fibrous reinforcements only
    • B29C70/08—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers
    • B29C70/088—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers and with one or more layers of non-plastics material or non-specified material, e.g. supports
    • 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
    • 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
    • B32B15/14—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
    • B32B5/00—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
    • B32B5/02—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 structural features of a fibrous or filamentary layer
    • B32B5/04—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 structural features of a fibrous or filamentary layer characterised by a layer being specifically extensible by reason of its structure or arrangement, e.g. by reason of the chemical nature of the fibres or filaments
    • 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
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/12—Construction or attachment of skin panels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • 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
    • B29K2277/00—Use of PA, i.e. polyamides, e.g. polyesteramides or derivatives thereof, as reinforcement
    • B29K2277/10—Aromatic polyamides [Polyaramides] or derivatives thereof
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • 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
    • B29K2705/00—Use of metals, their alloys or their compounds, for preformed parts, e.g. for inserts
    • B29K2705/02—Aluminium
    • 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
    • B32B2307/00—Properties of the layers or laminate
    • B32B2307/50—Properties of the layers or laminate having particular mechanical properties
    • B32B2307/51—Elastic
    • 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
    • B32B2307/50—Properties of the layers or laminate having particular mechanical properties
    • B32B2307/54—Yield strength; Tensile strength
    • 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
    • B32B2311/24—Aluminium
    • 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
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0081—Fuselage structures substantially made from particular materials from metallic materials
    • 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
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S428/00—Stock material or miscellaneous articles
    • Y10S428/902—High modulus filament or fiber
    • 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
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S428/00—Stock material or miscellaneous articles
    • Y10S428/91—Product with molecular orientation
    • 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.]
    • Y10T428/24942—Structurally defined web or sheet [e.g., overall dimension, etc.] including components having same physical characteristic in differing degree
    • Y10T428/2495—Thickness [relative or absolute]
    • 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.]
    • Y10T428/24942—Structurally defined web or sheet [e.g., overall dimension, etc.] including components having same physical characteristic in differing degree
    • Y10T428/2495—Thickness [relative or absolute]
    • Y10T428/24967—Absolute thicknesses specified
    • 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.]
    • Y10T428/24942—Structurally defined web or sheet [e.g., overall dimension, etc.] including components having same physical characteristic in differing degree
    • Y10T428/2495—Thickness [relative or absolute]
    • Y10T428/24967—Absolute thicknesses specified
    • Y10T428/24975—No layer or component greater than 5 mils thick
    • 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
    • Y10T428/31504—Composite [nonstructural laminate]
    • Y10T428/31511—Of epoxy ether
    • Y10T428/31515—As intermediate layer
    • Y10T428/31522—Next to metal
    • 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
    • Y10T428/31504—Composite [nonstructural laminate]
    • Y10T428/31511—Of epoxy ether
    • Y10T428/31529—Next to metal
    • 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
    • Y10T428/31504—Composite [nonstructural laminate]
    • Y10T428/31551—Of polyamidoester [polyurethane, polyisocyanate, polycarbamate, etc.]
    • Y10T428/31605—Next to free metal
    • 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
    • Y10T428/31504—Composite [nonstructural laminate]
    • Y10T428/31678—Of metal
    • Y10T428/31681—Next to polyester, polyamide or polyimide [e.g., alkyd, glue, or nylon, etc.]
    • 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
    • Y10T428/31504—Composite [nonstructural laminate]
    • Y10T428/31725—Of polyamide
    • 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
    • Y10T442/00—Fabric [woven, knitted, or nonwoven textile or cloth, etc.]
    • Y10T442/30—Woven fabric [i.e., woven strand or strip material]
    • Y10T442/3382—Including a free metal or alloy constituent
    • Y10T442/3415—Preformed metallic film or foil or sheet [film or foil or sheet had structural integrity prior to association with the woven fabric]
    • Y10T442/3423—Plural metallic films or foils or sheets

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Laminated Bodies (AREA)
NL8100087A 1981-01-09 1981-01-09 Laminaat uit metalen platen en daarmede verbonden draden. NL8100087A (nl)

Priority Applications (7)

Application Number Priority Date Filing Date Title
NL8100087A NL8100087A (nl) 1981-01-09 1981-01-09 Laminaat uit metalen platen en daarmede verbonden draden.
DE8282200014T DE3267655D1 (en) 1981-01-09 1982-01-08 Laminate of aluminium sheet material and aramid fibres
EP82200014A EP0056289B1 (de) 1981-01-09 1982-01-08 Schichtstoff aus Aluminiumschichten und Polyaramidfasern
JP57001106A JPS57137148A (en) 1981-01-09 1982-01-08 Laminate of aluminum material and alamide fiber
IE36/82A IE53179B1 (en) 1981-01-09 1982-01-08 Laminate of aluminium sheet material and aramid fibres
AT82200014T ATE16778T1 (de) 1981-01-09 1982-01-08 Schichtstoff aus aluminiumschichten und polyaramidfasern.
US06/533,883 US4500589A (en) 1981-01-09 1983-09-20 Laminate of aluminum sheet material and aramid fibers

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
NL8100087 1981-01-09
NL8100087A NL8100087A (nl) 1981-01-09 1981-01-09 Laminaat uit metalen platen en daarmede verbonden draden.

Publications (1)

Publication Number Publication Date
NL8100087A true NL8100087A (nl) 1982-08-02

Family

ID=19836834

Family Applications (1)

Application Number Title Priority Date Filing Date
NL8100087A NL8100087A (nl) 1981-01-09 1981-01-09 Laminaat uit metalen platen en daarmede verbonden draden.

Country Status (7)

Country Link
US (1) US4500589A (de)
EP (1) EP0056289B1 (de)
JP (1) JPS57137148A (de)
AT (1) ATE16778T1 (de)
DE (1) DE3267655D1 (de)
IE (1) IE53179B1 (de)
NL (1) NL8100087A (de)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0312151A1 (de) * 1987-10-14 1989-04-19 Akzo N.V. Schichtstoff aus Metallschichten und aus durchgehendem faserverstärktem synthetischem Material
RU2641744C1 (ru) * 2017-03-02 2018-01-22 Федеральное государственное унитарное предприятие "Всероссийский научно-исследовательский институт авиационных материалов" (ФГУП "ВИАМ") Слоистый гибридный композиционный материал и изделие, выполненное из него
WO2023119127A1 (en) 2021-12-22 2023-06-29 Jan Verhaeghe A fibre-metal composite panel comprising a fibre-reinforced thermoplastic panel and a metal plate, and a method for manufacturing it

Families Citing this family (75)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2164293A (en) * 1984-08-31 1986-03-19 Motoplat Import resistant fuel tanks
JPS62162022U (de) * 1986-04-07 1987-10-15
US4888247A (en) * 1986-08-27 1989-12-19 General Electric Company Low-thermal-expansion, heat conducting laminates having layers of metal and reinforced polymer matrix composite
US4803105A (en) * 1987-02-13 1989-02-07 Essex Specialty Products, Inc. Reinforcing sheet for the reinforcement of panel and method of reinforcing panel
ATE82903T1 (de) * 1987-10-14 1992-12-15 Structural Laminates Co Schichtstoff aus metallschichten und aus durchgehendem,faserverstaerkten,synthetischen,th rmoplastischen material und verfahren zu seiner herstellung.
DE3872858T2 (de) * 1987-12-31 1993-01-14 Structural Laminates Co Zusammengestelltes laminat aus metallschichten und mit fortlaufenden faeden verstaerkte kunststoffschichten.
US5030488A (en) * 1988-11-23 1991-07-09 Chemical And Polymer Technology, Inc. Laminates, panels and means for joining them
KR100191983B1 (ko) * 1989-05-30 1999-06-15 레그랜드 지.윌리엄 열차단 라미네이트 및 이의 제조방법
US5082886A (en) * 1989-08-28 1992-01-21 General Electric Company Low compression set, oil and fuel resistant, liquid injection moldable, silicone rubber
US6604708B1 (en) * 1989-12-26 2003-08-12 The Boeing Company Carbon brake wear for aircraft
DK0439046T3 (da) 1990-01-22 1993-12-27 Atd Corp Måtte med køleplade og termisk isolerende områder
EP0473843B1 (de) * 1990-09-05 1995-07-26 Fokker Aircraft B.V. Laminat für gebogene Struktur und Verfahren zu ihrer Herstellung
US5227216A (en) * 1991-03-25 1993-07-13 Mcdonnell Douglas Corporation Fiber/metal laminate
US5429326A (en) * 1992-07-09 1995-07-04 Structural Laminates Company Spliced laminate for aircraft fuselage
US5567535A (en) * 1992-11-18 1996-10-22 Mcdonnell Douglas Corporation Fiber/metal laminate splice
US6194081B1 (en) 1993-10-18 2001-02-27 Ticomp. Inc. Beta titanium-composite laminate
US5906550A (en) * 1993-10-18 1999-05-25 Ticomp, Inc. Sports bat having multilayered shell
US5733390A (en) * 1993-10-18 1998-03-31 Ticomp, Inc. Carbon-titanium composites
US5578384A (en) * 1995-12-07 1996-11-26 Ticomp, Inc. Beta titanium-fiber reinforced composite laminates
US6565959B1 (en) * 1994-03-04 2003-05-20 Daniel A. Tingley Use of synthetic fibers in a glueline to increase resistance to sag in wood and wood composite structures
US5744228A (en) * 1994-03-04 1998-04-28 Tingley; Daniel A. Use of synthetic fibers in a glueline to increase resistance to sag in wood and wood composite structures
US5700347A (en) * 1996-01-11 1997-12-23 The Boeing Company Thermoplastic multi-tape application head
US5651850A (en) * 1996-01-11 1997-07-29 The Boeing Company Method of fabricating hybrid composite structures
US5866272A (en) * 1996-01-11 1999-02-02 The Boeing Company Titanium-polymer hybrid laminates
ATE226512T1 (de) 1997-05-28 2002-11-15 Structural Laminates Co Verfahren zur herstellung eines mehrschichtwerkstoffes und ein mehrschichtwerkstoff der mit diesem verfahren herzustellen ist
US6039832A (en) * 1998-02-27 2000-03-21 The Boeing Company Thermoplastic titanium honeycomb panel
NL1011516C2 (nl) * 1999-03-10 2000-09-12 Adprotech B V Laminaat uit metaallagen die met een vezelversterkte hechtingsmiddellaag zijn verbonden.
US6075701A (en) * 1999-05-14 2000-06-13 Hughes Electronics Corporation Electronic structure having an embedded pyrolytic graphite heat sink material
SE0101129L (sv) * 2001-03-30 2002-08-06 Saab Ab Metallkompositlaminat samt sätt att framställa detsamma
US6648273B2 (en) 2001-10-30 2003-11-18 The Boeing Company Light weight and high strength fuselage
DE10238460B3 (de) * 2002-08-22 2004-03-11 Airbus Deutschland Gmbh Leichtbaustruktur aus dünnen Metallblechlagen
FR2844742B1 (fr) 2002-09-25 2005-04-29 Pechiney Rhenalu Feuilles composites stratifiees aluminium-fibres de verre
US7192501B2 (en) * 2002-10-29 2007-03-20 The Boeing Company Method for improving crack resistance in fiber-metal-laminate structures
EP1495858B1 (de) * 2003-07-08 2019-08-07 Airbus Operations GmbH Leichtbaustruktur aus metallischen schichtwerkstoffen
ATE406998T1 (de) * 2003-07-08 2008-09-15 Airbus Gmbh Leichtbaustruktur
US6851649B1 (en) 2003-08-14 2005-02-08 The Boeing Company Methods and systems for controlling wheel brakes on aircraft and other vehicles
DE10360808B4 (de) * 2003-12-19 2005-10-27 Airbus Deutschland Gmbh Faserverstärkter metallischer Verbundwerkstoff
US20050175813A1 (en) * 2004-02-10 2005-08-11 Wingert A. L. Aluminum-fiber laminate
FR2876655B1 (fr) * 2004-10-19 2008-05-30 Faurecia Interieur Ind Snc Traverse pour vehicule automobile, et vehicule automobile correspondant
US7281684B2 (en) * 2005-02-23 2007-10-16 The Boeing Company Systems and methods for braking aircraft, including braking intermediate main gears and differential braking
EP1728623A1 (de) * 2005-06-03 2006-12-06 Pedro Lloveras Calvo Mehrschicht Aluminium-Textil Laminat
NL1030029C2 (nl) * 2005-09-26 2007-03-27 Gtm Consulting B V Werkwijze en inrichting voor het verlijmen van componenten tot een samengesteld vormdeel.
NL1030066C2 (nl) * 2005-09-29 2007-03-30 Gtm Consulting B V Werkwijze voor het vervaardigen van een vormdeel uit een samengesteld materiaal.
US7446064B2 (en) * 2006-03-01 2008-11-04 Alcoa Inc. Impact resistant building panels
EP2021238A2 (de) * 2006-05-15 2009-02-11 Alcoa Inc. Verstärkte hybridstrukturen und verfahren dafür
DE102006023210B4 (de) 2006-05-17 2012-12-13 Airbus Operations Gmbh Verfahren zum Herstellen einer Laminatstruktur, Laminatstruktur und deren Verwendung
US8011165B2 (en) * 2006-06-07 2011-09-06 Integritect Consulting, Inc. Composite assembly with saturated bonding mass and process of reinforced attachment
NL2000100C2 (nl) * 2006-06-13 2007-12-14 Gtm Consulting B V Laminaat uit metaalplaten en kunststof.
NL2000232C2 (nl) * 2006-09-12 2008-03-13 Gtm Consulting B V Huidpaneel voor een vliegtuigromp.
US7690164B2 (en) * 2006-12-05 2010-04-06 Lockheed Martin Corporation System, method, and apparatus for structural lug formed from a combination of metal and composite laminate materials
JP5094839B2 (ja) * 2007-03-12 2012-12-12 大成プラス株式会社 アルミニウム合金複合体
US20090211697A1 (en) * 2007-05-15 2009-08-27 Heinimann Markus B Reinforced hybrid structures and methods thereof
EP2085215B1 (de) 2008-01-29 2013-03-27 GTM Holding B.V. Hochfeste Fasermetallbeschichtung
DE102008062860A1 (de) 2008-12-23 2010-07-01 Universität Bremen Schichtverbundwerkstoff, Verfahren zu dessen Herstellung und Verwendung desselben
CA2816509C (en) * 2010-11-12 2016-02-23 Bell Helicopter Textron Inc. Composite rotor blade having weighted material for mass balancing
ES2541631T3 (es) 2010-11-29 2015-07-22 Gtm-Advanced Structures B.V. Laminado de material compuesto reforzado fibra-lámina metálica
DE102011006032A1 (de) * 2011-03-24 2012-09-27 Airbus Operations Gmbh Verfahren zur Herstellung eines Strukturbauteils sowie Strukturbauteil
DE102011054909A1 (de) * 2011-10-28 2013-05-02 Benteler Automobiltechnik Gmbh Verfahren zur Herstellung eines Kraftfahrzeugbauteils sowie nach dem Verfahren hergestelltes Kraftfahrzeugbauteil
NL2007683C2 (en) * 2011-10-31 2013-05-06 Gtm Advanced Products B V Improved fiber-metal laminate.
DE102012003734A1 (de) 2012-02-28 2013-08-29 Deutsches Zentrum für Luft- und Raumfahrt e.V. Verfahren zur Herstellung eines Bauteils aus einem Hybridlaminat
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
EP2868469A1 (de) * 2013-10-31 2015-05-06 Alcoa Architectural Products SAS Doppelbogen-Aluminiumtafel und Verfahren zur Herstellung davon
KR101429727B1 (ko) * 2014-02-20 2014-08-14 (주)오토젠 하이브리드 복합소재를 이용한 히트 프로텍터의 제조방법
EP2942280A1 (de) * 2014-05-07 2015-11-11 BAE Systems PLC Flüssigspeichersystem
PL3140195T3 (pl) * 2014-05-07 2018-10-31 Bae Systems Plc System przechowywania cieczy
GB2528541A (en) 2014-05-07 2016-01-27 Bae Systems Plc Liquid storage system
GB2528540B (en) 2014-05-07 2016-08-03 Bae Systems Plc Fuel storage system comprising outer and inner tanks
EP2942281A1 (de) * 2014-05-07 2015-11-11 BAE Systems PLC Flüssigkeitsspeicherbehälter
US10640226B2 (en) 2014-05-07 2020-05-05 Bae Systems Plc Liquid storage system
US10189576B2 (en) 2014-05-07 2019-01-29 Bae Systems Plc Liquid storage tank
FR3021255B1 (fr) * 2014-05-21 2016-05-13 Renault Sa Portiere renforcee de vehicule automobile
NL2012889B1 (en) 2014-05-26 2016-05-03 Gtm Advanced Products B V Laminate of a metal sheet and an adhesive layer bonded thereto.
NL2017062B1 (nl) * 2016-06-28 2018-01-05 Fokker Aerostructures Bv Werkwijze voor het vervaardigen van een paneel met verdikking
GB2582148A (en) * 2019-03-12 2020-09-16 Airbus Operations Ltd Impact resistant panels
EP4238758A1 (de) 2022-03-04 2023-09-06 Inegi - Instituto de Ciência e Inovação em Engenharia Mecânica e Engenharia Industrial Verbundstoffrahmen aus verstärkungsthermoplastbasiertem faser-metall-laminat und herstellungsverfahren dafür

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB635823A (en) * 1945-06-01 1950-04-19 Ernest Platton King Improved method of manufacturing composite metal-fibrous structures
US3189054A (en) * 1961-06-23 1965-06-15 Aerojet General Co Laminate structure of alternate layers of metal and glass fiber tapes
US3321019A (en) * 1965-10-22 1967-05-23 United Aircraft Corp Fiberglass blade
GB1303301A (de) * 1970-02-13 1973-01-17
JPS5045372U (de) * 1973-08-22 1975-05-07
US4035694A (en) * 1974-01-07 1977-07-12 Minnesota Mining And Manufacturing Company Metal-clad dielectric sheeting
JPS51149699A (en) * 1975-06-14 1976-12-22 Kawasaki Heavy Ind Ltd Rotar y wing
FR2322190A1 (fr) * 1975-08-27 1977-03-25 Aerospatiale Procede de liaison par collage
US4029838A (en) * 1975-09-24 1977-06-14 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Hybrid composite laminate structures
JPS54123941A (en) * 1978-03-18 1979-09-26 Nippon Columbia Electroacoustic converter vibrator
US4369222A (en) * 1978-12-22 1983-01-18 Monsanto Company Metal-thermoplastic-metal laminates
EP0013146B1 (de) * 1978-12-22 1982-01-20 Monsanto Company Metall-Thermoplast-Metall-Verbundgebilde und Verfahren zur Herstellung solcher Verbundgebilde
JPS55122002A (en) * 1979-03-13 1980-09-19 Kuramoto Sangyo Kk Fabric for heat and fire resistant protectzng wear

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0312151A1 (de) * 1987-10-14 1989-04-19 Akzo N.V. Schichtstoff aus Metallschichten und aus durchgehendem faserverstärktem synthetischem Material
US5039571A (en) * 1987-10-14 1991-08-13 Akzo Nv Metal-resin laminate reinforced with S2-glass fibres
RU2641744C1 (ru) * 2017-03-02 2018-01-22 Федеральное государственное унитарное предприятие "Всероссийский научно-исследовательский институт авиационных материалов" (ФГУП "ВИАМ") Слоистый гибридный композиционный материал и изделие, выполненное из него
WO2023119127A1 (en) 2021-12-22 2023-06-29 Jan Verhaeghe A fibre-metal composite panel comprising a fibre-reinforced thermoplastic panel and a metal plate, and a method for manufacturing it
BE1030072A1 (nl) 2021-12-22 2023-07-14 Roeve Koen De Een vezel-metaal composiet paneel omvattend een vezelversterkt thermoplastisch paneel en een metalen plaat en werkwijze voor de vervaardiging ervan

Also Published As

Publication number Publication date
IE820036L (en) 1982-07-09
US4500589A (en) 1985-02-19
IE53179B1 (en) 1988-08-17
DE3267655D1 (en) 1986-01-16
EP0056289B1 (de) 1985-12-04
EP0056289A1 (de) 1982-07-21
JPH0226581B2 (de) 1990-06-11
JPS57137148A (en) 1982-08-24
ATE16778T1 (de) 1985-12-15

Similar Documents

Publication Publication Date Title
NL8100087A (nl) Laminaat uit metalen platen en daarmede verbonden draden.
NL8100088A (nl) Laminaat uit metalen platen en daarmede verbonden draden, alsmede werkwijzen ter vervaardiging daarvan.
JP3212605B2 (ja) 航空機の胴体用の積層パネル
JP2640262B2 (ja) 金属シート及び連続的フィラメント強化合成層の複合ラミネート
JP2660563B2 (ja) 金属シート及び連続ガラスフィラメントで強化された合成材料のラミネート
US5227216A (en) Fiber/metal laminate
EP0312150B1 (de) Schichtstoff aus Metallschichten und aus durchgehendem,faserverstärkten,synthetischen,thermoplastischen Material und Verfahren zu seiner Herstellung
Salman Effects of jute fibre content on the mechanical and dynamic mechanical properties of the composites in structural applications
NL1022706C2 (nl) Laminaat uit metaalplaten en elkaar kruisende dradenlagen uit verschillende materialen in kunststof.
JP2909211B2 (ja) 強化アロイラミネート
US5087503A (en) Composite constant stress beam with gradient fiber distribution
Gussenhoven et al. Fatigue behavior of reinforced concrete beams strengthened with different FRP laminate configurations
EP0323660A1 (de) Verfahren zum Herstellen eines Laminates aus Metallschichten und mit Fäden verstärkte Kunststoffschichten
US5194111A (en) Composite constant stress beam with gradient fiber distribution
Droździel et al. Low-velocity impact resistance of thin-ply in comparison with conventional aluminium-carbon laminates
JP2009538250A (ja) 強化ハイブリッドの構造とその製造方法
US20080292853A1 (en) Composite Laminated Material and Article Made Thereof
JP6552837B2 (ja) 鋼構造物の補強方法及び鋼構造物補強用積層材
NL1029088C2 (nl) Vezel-metaal laminaten en constructies voorzien daarvan.
Salman Defence Technology
Abdulrahman UV radiation effect on static and dynamic behavior of fiber reinforced Composite plates
Neagoe Flexural Performance of Reinforced Concrete Beams Strengthened with Composite Materials
Nguyen-Hoa Prévision de la rupture des composites polyester/tissus de verre= Prediction of failure in polyester reinforced by woven glass fabrics.

Legal Events

Date Code Title Description
A1B A search report has been drawn up
A85 Still pending on 85-01-01
BV The patent application has lapsed