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DE3622781A1 - Multilayer system - Google Patents

Multilayer system

Info

Publication number
DE3622781A1
DE3622781A1 DE19863622781 DE3622781A DE3622781A1 DE 3622781 A1 DE3622781 A1 DE 3622781A1 DE 19863622781 DE19863622781 DE 19863622781 DE 3622781 A DE3622781 A DE 3622781A DE 3622781 A1 DE3622781 A1 DE 3622781A1
Authority
DE
Germany
Prior art keywords
layer system
metal
plated
titanium
knitted fabric
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.)
Granted
Application number
DE19863622781
Other languages
German (de)
Other versions
DE3622781C2 (en
Inventor
Alfred Buck
Erich A Dolderer
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.)
BUCK, ALFRED, 7407 ROTTENBURG, DE
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to DE19863622781 priority Critical patent/DE3622781A1/en
Publication of DE3622781A1 publication Critical patent/DE3622781A1/en
Application granted granted Critical
Publication of DE3622781C2 publication Critical patent/DE3622781C2/de
Granted legal-status Critical Current

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
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K1/00—Soldering, e.g. brazing, or unsoldering
    • B23K1/19—Soldering, e.g. brazing, or unsoldering taking account of the properties of the materials to be soldered
    • 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
    • B32B5/022—Non-woven fabric
    • 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
    • B32B5/024—Woven fabric
    • 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
    • B32B5/026—Knitted fabric
    • 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
    • B32B9/00—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00
    • B32B9/005—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising one layer of ceramic material, e.g. porcelain, ceramic tile
    • 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
    • B32B9/00—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00
    • B32B9/04—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising such particular substance as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B9/041—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising such particular substance as the main or only constituent of a layer, which is next to another layer of the same or of a different material of metal
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B37/00—Joining burned ceramic articles with other burned ceramic articles or other articles by heating
    • C04B37/02—Joining burned ceramic articles with other burned ceramic articles or other articles by heating with metallic articles
    • C04B37/023—Joining burned ceramic articles with other burned ceramic articles or other articles by heating with metallic articles characterised by the interlayer used
    • C04B37/026—Joining burned ceramic articles with other burned ceramic articles or other articles by heating with metallic articles characterised by the interlayer used consisting of metals or metal salts
    • 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
    • B32B2262/105—Ceramic 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
    • B32B2305/10—Fibres of continuous length
    • B32B2305/18—Fabrics, textiles
    • B32B2305/186—Knitted fabrics
    • 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
    • B32B2305/10—Fibres of continuous length
    • B32B2305/18—Fabrics, textiles
    • B32B2305/188—Woven fabrics
    • 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
    • B32B2305/10—Fibres of continuous length
    • B32B2305/20—Fibres of continuous length in the form of a non-woven mat
    • 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
    • B32B2307/30—Properties of the layers or laminate having particular thermal properties
    • B32B2307/306—Resistant to heat
    • 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
    • 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
    • B32B2315/00—Other materials containing non-metallic inorganic compounds not provided for in groups B32B2311/00 - B32B2313/04
    • B32B2315/02—Ceramics
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
    • C04B2237/02—Aspects relating to interlayers, e.g. used to join ceramic articles with other articles by heating
    • C04B2237/12—Metallic interlayers
    • C04B2237/122—Metallic interlayers based on refractory metals
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
    • C04B2237/30—Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
    • C04B2237/32—Ceramic
    • C04B2237/38—Fiber or whisker reinforced
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
    • C04B2237/30—Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
    • C04B2237/40—Metallic
    • C04B2237/403—Refractory metals
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
    • C04B2237/50—Processing aspects relating to ceramic laminates or to the joining of ceramic articles with other articles by heating
    • C04B2237/59—Aspects relating to the structure of the interlayer
    • C04B2237/592—Aspects relating to the structure of the interlayer whereby the interlayer is not continuous, e.g. not the whole surface of the smallest substrate is covered by the interlayer
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
    • C04B2237/50—Processing aspects relating to ceramic laminates or to the joining of ceramic articles with other articles by heating
    • C04B2237/76—Forming laminates or joined articles comprising at least one member in the form other than a sheet or disc, e.g. two tubes or a tube and a sheet or disc

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Ceramic Engineering (AREA)
  • Textile Engineering (AREA)
  • Materials Engineering (AREA)
  • Structural Engineering (AREA)
  • Organic Chemistry (AREA)
  • Mechanical Engineering (AREA)
  • Ceramic Products (AREA)
  • Laminated Bodies (AREA)

Abstract

A process is described by means of which non-woven fabrics, meshes, woven and knitted fabrics produced from ceramic fibres can be connected by hard soldering to a metallic, hard-solderable material.

Description

Der Einsatz neuer keramischer Hochtemperatur-Faserwerk­ stoffe welche zu Gelegen, Geflechten, Geweben und Ge­ stricken verarbeitet werden nimmt ständig zu.The use of new ceramic high-temperature fiber plants fabrics which are used for fabrics, braids, fabrics and fabrics knitting processed is constantly increasing.

Die daraus hergestellten Erzeugnisse werden zusammen mit Harzen zu Bauelementen verarbeitet. Die Harze haben eine Temperaturbeständigkeit derzeit von max. +300°C. Unter diesen Umständen kann die hohe Temperaturbeständigkeit der keramischen Fasern nicht annähernd ausgenützt werden.The products made from it are together with Resins processed into components. The resins have one Temperature resistance currently of max. + 300 ° C. Under these circumstances can the high temperature resistance the ceramic fibers are not used anywhere.

Anhand eines Systems Titan - keramisches Gestricke wird beispielhaft ein Verfahren beschrieben, wie zwei so un­ terschiedliche Werkstoffe verbunden werden können.Using a titanium - ceramic knitted fabric system an example of a method described as two so un different materials can be connected.

Reines Titan hat einen Schmelzpunkt von 1668°C und eig­ net sich infolge seiner geringen Dichte besonders gut wenn auf geringes Gewicht eines solchen Verbund-Werktoffs Wert gelegt wird.Pure titanium has a melting point of 1668 ° C and proper net is particularly good due to its low density if on the light weight of such a composite material Value is placed.

Bauteile aus Titan lassen sich nach dem Hartlöt-Verfahren verbinden. Diese Eigenschaft wird dazu verwendet kerami­ sche Faser-Werkstoffe mit Titan zu verbinden. Dies ist auch auf andere hartlötbare Werkstoffe anwendbar.Titanium components can be brazed connect. This property is used for kerami connecting fiber materials with titanium. This is also applicable to other brazeable materials.

Um eine Verbindung beider Werkstoffe herzustellen können zwei Verfahren zur Anwendung kommen.To be able to connect both materials two methods are used.

Es kommt ein sgt. plattiertes Gestricke zum Einsatz. Beim Stricken wird eine Faser aus keramischem Werkstoff und gleichzeitig ein Titandraht zugeführt. Es entsteht ein Gestricke welches einseitig mit Titan plattiert ist.There is a sgt. plated knitted fabrics for use. At the A fiber made of ceramic material and at the same time a titanium wire is fed. It arises Knitted fabric which is plated on one side with titanium.

Ein weiteres Verfahren arbeitet mit einer Beschichtung ei­ nes Gestrickes aus Keramikfaser mit einem metallischen Werkstoff. Besonders gut eignet sich hierfür das Sputtern. Nach diesem Verfahren wird je nach apparativem Aufbau eine Seite des Gestrickes bevorzugt metallisiert.Another method works with a coating knitted fabric made of ceramic fiber with a metallic Material. Sputtering is particularly suitable for this. According to this method, a Side of the knitted fabric preferably metallized.

Beim einseitigen Metallisieren ist es vorteilhaft ein Dop­ pelgestricke zu verwenden. Bei gleichem Garn und gleicher Maschenbildung verdoppelt sich die Dicke des Gestricks.When metallizing on one side it is advantageous to use a dop to use furs. With the same yarn and the same Stitching doubles the thickness of the knitted fabric.

Das Titanbauelement, beispielsweise ein Titanblech und die beschichtete Seite des Faserelements bzw. die mit Titan plattierte Seite des Gestrickes werden im Schutzgaslöt­ ofen miteinander unter Zugabe eines geeigneten Hartlots verlötet. The titanium component, for example a titanium sheet and the coated side of the fiber element or the one with titanium plated side of the knitted fabric are soldered in protective gas oven with the addition of a suitable brazing alloy soldered.  

Beim Hartlöten wird nur die äußerste metallische oder metallisierte Gestrickeschicht mit dem Titanblech hart verlötet. Trotzdem wird die Elastizität und Reckbarkeit des Gestrickes auf ein Minimum reduziert.When brazing, only the outermost metallic or metallized knitted layer with the titanium sheet hard soldered. Nevertheless, the elasticity and stretchability of the knitted fabric reduced to a minimum.

Speziell beim Doppelgestrick bleibt die schlechte Wärme­ leitfähigkeit erhalten.The bad warmth remains especially with the double knitted fabric maintain conductivity.

Falls beide Teile dreidimensional verformt werden sollen muß dies vor dem Lötvorgang geschehen. Vor dem Löten wer­ den die verformten Teile gefügt, positioniert und unter Verwendung einer entsprechend ausgebildeten Lötvorrich­ tung verlötet.If both parts are to be deformed three-dimensionally this must be done before the soldering process. Who before soldering which the deformed parts are joined, positioned and under Use an appropriately trained soldering iron tung soldered.

Mittels des vorgeschlagenen Verfahrens lassen sich auch Mehrschicht-Systeme aus mehr wie zwei Lagen herstellen.The proposed method can also be used Manufacture multi-layer systems from more than two layers.

Unter Anwendung einer solchen Verbindungstechnik ist es möglich, einerseits die Festigkeit eines Metalles auszu­ nützen und andererseits die schlechte Wärmeleitfähigkeit eines solchen Metall-Keramikgestricks zu optimieren.It is using such a connection technique possible, on the one hand, to establish the strength of a metal benefit and on the other hand the poor thermal conductivity to optimize such a metal-ceramic knitted fabric.

Claims (4)

1. Mehrschicht-System bestend aus einem hartlötbaren Metall und einem Faserwerkstoff hoher Teperaturbeständigkeit dadurch gekennzeichnet, daß der Faserwerkstoff mit einem hartlötbaren Metall beschichtet wird, so daß zwischen den beiden Werkstoffen eine Lötverbindung hergestellt werden kann.1. Multi-layer system consisting of a brazeable metal and a fiber material of high temperature resistance, characterized in that the fiber material is coated with a brazeable metal, so that a solder connection can be made between the two materials. 2. Mehrschicht-System nach Anspruch 1, dadurch gekennzeichnet, daß ein Doppelgestrick verwendet wird wobei nur eine Seite mit Metall beschichtet wird.2. Multi-layer system according to claim 1, characterized in that a double knit is used only one side is coated with metal. 3. Mehrschicht-System nach Anspruch 1, dadurch gekennzeichnet, daß beim Stricken eines hochtempera­ turfesten Werkstoffs (Garn) einseitig ein lötbarer Draht aufplattiert wird so daß die aufplattierte metallische Seite mittels Hartlöten mit dem metallischen Basiswerkstoff ver­ bunden werden kann.3. Multi-layer system according to claim 1, characterized in that when knitting a high temperature solid material (yarn) a solderable wire on one side is plated so that the plated metal side by means of brazing with the metallic base material can be bound. 4. Mehrschicht-System nach Anspruch 1, 2 u. 3, dadurch gekennzeichnet, daß beide Bauelemente vor dem Hart­ löten verformt werden und erst nach der Verformung mittels einer Vorrichtung vor dem Hartlöten gegeneinander positio­ niert werden, und anschließend die Hartlötverbindung herge­ stellt wird.4. Multi-layer system according to claim 1, 2 u. 3, characterized in that both components before the hard soldering are deformed and only after the deformation by means of a device before brazing against each other positio be kidney, and then the braze joint is posed.
DE19863622781 1986-07-07 1986-07-07 Multilayer system Granted DE3622781A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE19863622781 DE3622781A1 (en) 1986-07-07 1986-07-07 Multilayer system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19863622781 DE3622781A1 (en) 1986-07-07 1986-07-07 Multilayer system

Publications (2)

Publication Number Publication Date
DE3622781A1 true DE3622781A1 (en) 1988-01-28
DE3622781C2 DE3622781C2 (en) 1990-07-26

Family

ID=6304578

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19863622781 Granted DE3622781A1 (en) 1986-07-07 1986-07-07 Multilayer system

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Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0375589A1 (en) * 1988-12-20 1990-06-27 United Technologies Corporation Method of attaching ceramic fiber arrays to metallic substrates
EP1312467A1 (en) * 2001-11-16 2003-05-21 EADS Deutschland GmbH Metal fibre reinforced composite material and method of making
FR2846905A1 (en) * 2002-11-09 2004-05-14 Haver & Boecker Thin composite material comprises base material layer in shape of sheet metal plate and at least one metallic material layer
NL1023175C2 (en) * 2003-04-14 2004-10-18 H & St Heat & Surface Treat B Fibre reinforced composite for e.g. aircraft or vehicles, comprises fibrous core and upper layer bonded together by solder material layer
US8540842B2 (en) 2008-08-18 2013-09-24 Productive Research Llc Formable light weight composites
US8796580B2 (en) 2009-12-28 2014-08-05 Productive Research Processes for welding composite materials and articles therefrom
US9005768B2 (en) 2011-02-21 2015-04-14 Productive Research Composite materials including regions differing in properties and methods
US9115264B2 (en) 2010-02-15 2015-08-25 Productive Research Llc Delamination resistant, weldable and formable light weight composites
US9233526B2 (en) 2012-08-03 2016-01-12 Productive Research Llc Composites having improved interlayer adhesion and methods thereof
EP2980289A1 (en) * 2014-07-28 2016-02-03 The Boeing Company Multi-material integrated knit thermal protection for industrial applications
EP3106556A1 (en) * 2015-06-16 2016-12-21 The Boeing Company Single-layer ceramic-based knit fabric for high temperature bulb seals
US10337130B2 (en) 2016-02-01 2019-07-02 The Boeing Company Metal alloy knit fabric for high temperature insulating materials
US11338552B2 (en) 2019-02-15 2022-05-24 Productive Research Llc Composite materials, vehicle applications and methods thereof

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102014203872A1 (en) * 2014-03-04 2015-09-10 Bayerische Motoren Werke Aktiengesellschaft Process for producing a flat semifinished product and fiber-reinforced semifinished product

Citations (2)

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Publication number Priority date Publication date Assignee Title
DE3032627A1 (en) * 1979-08-29 1981-03-12 Sumitomo Chemical Co HEAT-RESISTANT ELASTIC MATERIAL MADE OF FIBER-REINFORCED METAL COMPOSITE.
DE3000171A1 (en) * 1980-01-04 1981-07-09 Vereinigte Aluminium-Werke Ag, 5300 Bonn FIBER REINFORCED COMPOSITE AND METHOD FOR THE PRODUCTION THEREOF

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3032627A1 (en) * 1979-08-29 1981-03-12 Sumitomo Chemical Co HEAT-RESISTANT ELASTIC MATERIAL MADE OF FIBER-REINFORCED METAL COMPOSITE.
DE3000171A1 (en) * 1980-01-04 1981-07-09 Vereinigte Aluminium-Werke Ag, 5300 Bonn FIBER REINFORCED COMPOSITE AND METHOD FOR THE PRODUCTION THEREOF

Cited By (36)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU623954B2 (en) * 1988-12-20 1992-05-28 United Technologies Corporation Method of attaching ceramic fiber arrays to metallic substrates
EP0375589A1 (en) * 1988-12-20 1990-06-27 United Technologies Corporation Method of attaching ceramic fiber arrays to metallic substrates
US6861156B2 (en) 2001-11-16 2005-03-01 Eads Deutschland Gmbh Metal fiber-reinforced composite material as well as a method for its production
EP1312467A1 (en) * 2001-11-16 2003-05-21 EADS Deutschland GmbH Metal fibre reinforced composite material and method of making
FR2846905A1 (en) * 2002-11-09 2004-05-14 Haver & Boecker Thin composite material comprises base material layer in shape of sheet metal plate and at least one metallic material layer
DE10252157A1 (en) * 2002-11-09 2004-06-03 Haver & Boecker Flat composite material and method of manufacture
DE10252157B4 (en) * 2002-11-09 2012-11-22 Haver & Boecker Sheet composite material and method of manufacture
NL1023175C2 (en) * 2003-04-14 2004-10-18 H & St Heat & Surface Treat B Fibre reinforced composite for e.g. aircraft or vehicles, comprises fibrous core and upper layer bonded together by solder material layer
US8540842B2 (en) 2008-08-18 2013-09-24 Productive Research Llc Formable light weight composites
US9889634B2 (en) 2008-08-18 2018-02-13 Productive Research Llc Formable light weight composites
US9434134B2 (en) 2008-08-18 2016-09-06 Productive Research Llc Formable light weight composites
US8796580B2 (en) 2009-12-28 2014-08-05 Productive Research Processes for welding composite materials and articles therefrom
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