EP0911426B1 - Production of mouldings - Google Patents

Production of mouldings Download PDF

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Publication number
EP0911426B1
EP0911426B1 EP98120105A EP98120105A EP0911426B1 EP 0911426 B1 EP0911426 B1 EP 0911426B1 EP 98120105 A EP98120105 A EP 98120105A EP 98120105 A EP98120105 A EP 98120105A EP 0911426 B1 EP0911426 B1 EP 0911426B1
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EP
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Prior art keywords
thermal spraying
gas
base body
layer
process according
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Expired - Lifetime
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EP98120105A
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German (de)
French (fr)
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EP0911426A1 (en
Inventor
Peter Dipl.-Ing. Heinrich
Heinrich Professor Dr.-Ing. Kreye
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Linde GmbH
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Linde GmbH
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    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C4/00Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/18After-treatment
    • C23C4/185Separation of the coating from the substrate
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C24/00Coating starting from inorganic powder
    • C23C24/02Coating starting from inorganic powder by application of pressure only
    • C23C24/04Impact or kinetic deposition of particles
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C4/00Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/12Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the method of spraying

Definitions

  • the invention relates to a method for producing molded parts.
  • molded parts or moldings are very different Geometry needed. The requirements for the properties of the molded parts are included differently. The production of molded parts is particularly difficult made of or with difficult to form materials.
  • EP 911424 A1 with the same priority has a method for producing Composite bodies described in which an object by thermal spraying is made from two different materials.
  • EP 911425 A1 with the same priority has a method for coating Substrate materials described by thermal spraying, in which special gases and special temperatures are used.
  • DE 195 20 885 C1 describes a method for thermal spraying Layer of a metal or a metal alloy described. With this Processes can spray layers with a thickness of 20 mm and more getting produced.
  • the spray layer can be bonded to the substrate be used. At least 60% by weight of the wettable powder particles have the Impact on the substrate at a temperature between the solidus and the liquidus temperature of the metal alloy or up to 80 ° C below the Melting temperature is.
  • the present invention is based on the object of a method for the production to show molded parts that simplify the manufacture of molded parts, cheaper or made possible at all and / or which contributes significantly to to improve the quality and properties of molded parts. In particular, should the production of molded parts from or with difficult to form materials be made possible.
  • a base body is coated by thermal spraying, a powdered filler material by means of a gas on the to be coated Surface of the base body is passed without the powder particles of the Filler material are melted in the gas jet.
  • Thermal spraying for coating knows that as process variants autogenous flame spraying or the high speed flame spraying that Arc spraying, plasma spraying, detonation spraying and that Laser spraying.
  • Thermal spray processes are essentially characterized in that they enable evenly applied coatings.
  • Coatings can be applied by varying the spray materials can be adapted to different requirements.
  • the spray materials can be processed in the form of wires, rods or as powder. With thermal In addition, thermal post-treatment can be provided for spraying.
  • An essential feature of the invention is that the powder particles of Filler material in the gas jet should not be melted.
  • the aim is to have the powder particles of the filler material in the Do not melt the gas jet (i.e. convert it completely into the liquid phase) that but is not aimed that the powder particles of the filler in Gas jet as a mixture of on and / or unmelted particles and on the other hand, composed of molten particles.
  • the statement that the powder particles of the filler material not be melted in the gas jet can be ensured that the Temperature of the gas jet below the melting point of the powder particles Filler material is.
  • the cold gas spray process has compared to conventional processes of thermal spraying has a number of advantages.
  • the thermal action and The effect of force on the surface of the substrate material is reduced, as a result unwanted changes in the material properties of the substrate material can be prevented or at least significantly reduced. You can also changes in the structure of the substrate material are largely prevented.
  • a base body can be sprayed on by a layer or a layer Coating reinforced to a desired thickness using the cold gas spraying process become.
  • Relatively thin base bodies e.g. a relatively thin walled after A molded part produced by a conventional method as a starting material be used. This body is then sprayed on same or different material on the inside and / or the outside reinforced to the necessary thickness. Special advantages can be achieved if the Base body has a smaller thickness than that by thermal spraying sprayed-on layer This variant facilitates the production of molded parts or with materials that are difficult to form.
  • Moldings made of easily plastically deformable are also suitable as base bodies Material, for example copper, aluminum or alloys containing them.
  • the Base bodies can be relatively thin, for example in the range from 0.1 to 10 mm, preferably 0.5 to 5.0 mm. After spraying a particularly heavy malleable material by means of the cold spray process can then Molded articles, for example mechanically or chemically by dissolving, be removed from the sprayed-on layer. In this case, only that Spray layer the desired molded part.
  • This method supports in particular Dimensions the production of molded parts from or with difficult to form materials.
  • a raw body according to one of the possibilities described above or produced by a combination.
  • This raw body does not have to have the desired shape of the molded part to be produced, on the contrary, e.g. consist of a flat sheet metal body.
  • the workpiece can (the coated raw or basic body or just the layer) in one or several of the known forming processes (drawing, deep drawing, rolling, pressing and the like) are processed further. This is how you finally get that desired molding.
  • the advantage of this variant is that sprayed sheets or raw bodies are very fine-grained and practically texture-free. Your deformation takes place therefore very uniform and allows higher degrees of deformation than with sheet metal were produced by annealing or rolling.
  • the gas for thermal spraying can be nitrogen, helium, Argon, neon, krypton, xenon, a gas containing hydrogen, a carbon-containing one Gas, especially carbon dioxide, oxygen, an oxygen-containing Contain gas, air, hydrogen or mixtures of the aforementioned gases.
  • gases air and / or helium known from EP 0 484 533 B1 are suitable nitrogen, argon, also for the gas carrying the powdered filler material, Neon, krypton, xenon, oxygen, a gas containing hydrogen, a carbon-containing one Gas, especially carbon dioxide, hydrogen or mixtures of the aforementioned gases and mixtures of these gases with helium.
  • the proportion of helium of the total gas can be up to 90% by volume. A helium content of 10 to 50 vol .-% observed in the gas mixture.
  • the so produced Layers adhere very well to a wide variety of substrate materials, for example on metal, metal alloys, ceramics, glass, plastics and composite materials.
  • the coatings produced using the method according to the invention are of high quality, have an extremely low porosity and possess extremely smooth spray surfaces, so that there is usually no need for reworking
  • the gases used according to the invention have a sufficient density and Speed of sound to the required high speeds of the powder particles to be able to guarantee.
  • the gas can be inert and / or reactive gases contain. With the gases mentioned is the production of very dense and special uniform coatings possible, which is also due to their hardness and distinguish strength.
  • the layers have extremely low oxide contents. They have no or at least no pronounced texture, i.e. There is none Preferred orientation of the individual grains or crystals.
  • the substrate becomes further not heated by a flame or a plasma, so no or only extreme minor changes to the base body and no distortion of workpieces due to thermal stress due to thermal spraying.
  • the gas jet can be heated to a temperature in the range between 30 and 800 ° C are, all known powdery spray materials are used can.
  • the invention is particularly suitable for wettable powders made of metals, metal alloys, Hard materials, ceramics and / or plastics.
  • the temperature of the gas jet selected between 300 and 500 ° C. These gas temperatures are particularly suitable for the use of reactive gases or reactive Gas constituents. As reactive gas or gas components are in particular Hydrogen admixtures, carbon-containing gases or nitrogenous gases mention.
  • a gas jet with a pressure of 5 to 50 bar used. Above all, working with higher gas pressures brings additional Advantages because the energy transfer in the form of kinetic energy is increased. It gas pressures in the range from 21 to 50 bar are particularly suitable. Excellent Spray results were achieved, for example, with gas pressures of around 35 bar.
  • the High pressure gas supply can, for example, by the in the German patent application DE 197 16 414.5 described method or the one described there Gas supply system can be ensured.
  • the powder particles can run at one speed can be accelerated from 300 to 1600 m / s. Suitable in the process according to the invention speeds of the powder particles between 1000 and 1600 m / s, particularly preferably between 1250 and 1600 m / s, since in this case the Energy transfer in the form of kinetic energy is particularly high.
  • the powders used in the process according to the invention preferably have Particle sizes from 1 to 100 ⁇ m.
  • the method according to the invention offers the possibility in connection with a Automation and with computer-controlled movement of the base body or Spray gun to produce molded parts particularly quickly and inexpensively (rapid prototyping).
  • a shaped sheet 1 is shown in FIG. 1 in FIG. This sheet1 is applied a layer 2 by thermal spraying using the cold gas spraying method.
  • the sheet 1 has a smaller thickness than the sprayed-on layer 2.
  • the molding obtained in this way in Figure B consists of base body 1 (sheet metal) and Spray layer 2.
  • a molded body 1 made of a copper sheet is shown in FIG. After this Applying a thermal spray layer 2 as shown in Figure B, the copper sheet 1 mechanically detached from layer 2 The molded part obtained in this way is shown in Figure C. only from the spray layer 2.
  • the initially unshaped raw body or sheet 1 from Figure A of Figure 3 is provided with a layer 2 by thermal spraying using the cold gas spraying method (Picture B).
  • the workpiece consisting of the spray layer 2 is made according to a conventional Forming process deforms and receives, as shown in Figure D, on this Way its desired shape as a molding.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Plasma & Fusion (AREA)
  • Coating By Spraying Or Casting (AREA)

Description

Die Erfindung betrifft ein Verfahren zur Herstellung von Formteilen.The invention relates to a method for producing molded parts.

In der industriellen Fertigung werden Formteile bzw. Formkörper unterschiedlichster Geometrie benötigt. Die Anforderungen an die Eigenschaften der Formteile sind dabei unterschiedlich. Besondere Schwierigkeiten bereitet die Herstellung von Formteilen aus bzw. mit schwer formbaren Werkstoffen.In industrial production, molded parts or moldings are very different Geometry needed. The requirements for the properties of the molded parts are included differently. The production of molded parts is particularly difficult made of or with difficult to form materials.

In der EP 911424 A1 mit gleichem Zeitrang ist ein Verfahren zur Herstellung von Verbundkörpern beschrieben, bei dem durch thermisches Spritzen ein Gegenstand aus zwei unterschiedlichen Werkstoffen hergestellt wird.EP 911424 A1 with the same priority has a method for producing Composite bodies described in which an object by thermal spraying is made from two different materials.

In der EP 911425 A1 mit gleichem Zeitrang ist ein Verfahren zum Beschichten von Substratwerkstoffen durch thermisches Spritzen beschrieben, bei dem spezielle Gase und spezielle Temperaturen zur Anwendung kommen.EP 911425 A1 with the same priority has a method for coating Substrate materials described by thermal spraying, in which special gases and special temperatures are used.

In der DE 195 20 885 C1 ist ein Verfahren zum thermischen Spritzen einer Schicht aus einem Metall oder einer Metallegierung beschrieben. Mit diesem Verfahren können Spritzschichten mit einer Dicke von 20 mm und mehr hergestellt werden. Die Spritzschicht kann im Verbund mit dem Substrat eingesetzt werden. Wenigstens 60 Gew-% der Spritzpulverteilchen weisen beim Auftreffen auf das Substrat eine Temperatur auf, die zwischen der Solidus- und der Liquidus-Temperatur der Metallegierung oder bis zu 80 °C unterhalb der Schmelztemperatur liegt.DE 195 20 885 C1 describes a method for thermal spraying Layer of a metal or a metal alloy described. With this Processes can spray layers with a thickness of 20 mm and more getting produced. The spray layer can be bonded to the substrate be used. At least 60% by weight of the wettable powder particles have the Impact on the substrate at a temperature between the solidus and the liquidus temperature of the metal alloy or up to 80 ° C below the Melting temperature is.

Der vorliegenden Erfindung liegt die Aufgabe zugrunde, ein Verfahren zur Herstellung von Formteilen aufzuzeigen, welches die Herstellung von Formteilen vereinfacht, verbilligt oder überhaupt erst ermöglicht und/oder welches wesentlich dazu beiträgt, die Qualität und die Eigenschaften von Formteilen zu verbessern. Insbesondere sollte die Herstellung von Formteilen aus bzw. mit schwer formbaren Werkstoffen ermöglicht werden.The present invention is based on the object of a method for the production to show molded parts that simplify the manufacture of molded parts, cheaper or made possible at all and / or which contributes significantly to to improve the quality and properties of molded parts. In particular, should the production of molded parts from or with difficult to form materials be made possible.

Die gestellte Aufgabe wird durch ein Verfahren nach den Ansprüchen gelöst Hierbei wird ein Grundkörper durch thermisches Spritzen beschichtet, wobei ein pulverförmiger Zusatzwerkstoff mittels eines Gases auf die zu beschichtende Oberfläche des Grundkörpers geleitet wird, ohne dass die Pulverpartikel des Zusatzwerkstoffes im Gasstrahl geschmolzen werden.The object is achieved by a method according to the claims a base body is coated by thermal spraying, a powdered filler material by means of a gas on the to be coated Surface of the base body is passed without the powder particles of the Filler material are melted in the gas jet.

Das thermische Spritzen zum Beschichten kennt als Verfahrensvarianten das autogene Flammspritzen oder das Hochgeschwindigkeits-Flammspritzen, das Lichtbogenspritzen, das Plasmaspritzen, das Detonationsspritzen und das Laserspritzen.Thermal spraying for coating knows that as process variants autogenous flame spraying or the high speed flame spraying that Arc spraying, plasma spraying, detonation spraying and that Laser spraying.

Thermische Spritzverfahren werden in allgemeiner Form beispielsweise in

  • Übersicht und Einführung in das "Thermische Spritzen", Peter Heinrich, Linde-Berichte aus Technik und Wissenschaft, 52/1982, Seiten 29 bis 37, oder
  • Thermisches Spritzen - Fakten und Stand der Technik, Peter Heinrich, Jahrbuch Oberflächentechnik 1992, Band 48, 1991, Seiten 304 bis 327, Metall-Verlag GmbH,
beschrieben.Thermal spray processes are in general form, for example in
  • Overview and introduction to "thermal spraying" , Peter Heinrich, Linde reports from technology and science, 52/1982, pages 29 to 37, or
  • Thermal spraying - facts and state of the art, Peter Heinrich, yearbook surface technology 1992, volume 48, 1991, pages 304 to 327, Metall-Verlag GmbH,
described.

Thermische Spritzverfahren zeichnen sich im wesentlichen dadurch aus, daß sie gleichmäßig aufgetragene Beschichtungen ermöglichen. Durch thermische Spritzverfahren aufgetragene Beschichtungen können durch Variation der Spritzmaterialien an unterschiedliche Anforderungen angepaßt werden. Die Spritzmaterialien können dabei in Form von Drähten, Stäben oder als Pulver verarbeitet werden. Beim thermischen Spritzen kann zusätzlich eine thermische Nachbehandlung vorgesehen sein.Thermal spray processes are essentially characterized in that they enable evenly applied coatings. By thermal spraying Coatings can be applied by varying the spray materials can be adapted to different requirements. The spray materials can can be processed in the form of wires, rods or as powder. With thermal In addition, thermal post-treatment can be provided for spraying.

In jüngerer Zeit wurde darüber hinaus ein weiteres thermisches Spritzverfahren entwickelt, welches auch als Kaltgasspritzen bezeichnet wird. Es handelt sich dabei um eine Art Weiterentwicklung des Hochgeschwindigkeits-Flammspritzens mit Pulver. Dieses Verfahren ist beispielsweise in der europäischen Patentschrift EP 0 484 533 B1 beschrieben. Beim Kaltgasspritzen kommt ein Zusatzwerkstoff in Pulverform zum Einsatz. Die Pulverpartikel werden beim Kaltgasspritzen jedoch nicht im Gasstrahl geschmolzen. Vielmehr liegt die Temperatur des Gasstrahles unterhalb des Schmelzpunktes der Pulverpartikel des Zusatzwerkstoffes (EP 0 484 533 B1) oder aber nur in geringem Maße oberhalb der Schmelztemperatur des Pulvers. Im Kaltgasspritzverfahren wird also ein im Vergleich zu den herkömmlichen Spritzverfahren "kaltes" bzw. ein vergleichsweise kälteres Gas verwendet. Gleichwohl wird das Gas aber ebenso wie in den herkömmlichen Verfahren erwärmt, aber lediglich auf Temperaturen unterhalb des Schmelzpunktes der Pulverpartikel des Zusatzwerkstorfes oder auf Temperaturen des Gasstrahles von 100 K bis zu 200 K oberhalb des Schmelzpunktes der Pulverpartikel des Zusatzwerkstoffes.Recently, another thermal spraying process has also been developed which is also known as cold gas spraying. It is about a kind of further development of high-speed flame spraying with powder. This method is described, for example, in European patent EP 0 484 533 B1 described. A filler material in powder form is used for cold gas spraying Commitment. However, the powder particles are not melted in a gas jet during cold gas spraying. Rather, the temperature of the gas jet is below the melting point the powder particles of the filler material (EP 0 484 533 B1) or only in slightly above the melting temperature of the powder. In the cold gas spray process becomes a "cold" or a compared to the conventional spraying process comparatively colder gas used. Nevertheless, the gas is just as in heated up to conventional methods, but only to temperatures below the melting point of the powder particles of the filler peat or at temperatures of the gas jet from 100 K to 200 K above the melting point of the powder particles of the filler material.

Ein wesentliches Merkmal der Erfindung besteht darin, daß die Pulverpartikel des Zusatzwerkstoffes im Gasstrahl nicht geschmolzen werden. Dies soll gemäß der Erfindung bedeuten, daß angestrebt wird, die Pulverpartikel des Zusatzwerkstoffes im Gasstrahl nicht aufzuschmelzen (d.h. völlig in die flüssige Phase zu wandeln), daß aber nicht angestrebt wird, daß sich die Pulverpartikel des Zusatzwerkstoffes im Gasstrahl als Mischung einerseits aus an- und/oder ungeschmolzenen Partikeln und andererseits aus geschmolzenen Partikeln zusammensetzen. Die Angabe, daß die Pulverpartikel des Zusatzwerkstoffes im Gasstrahl nicht geschmolzen werden kann dadurch sichergestellt werden, daß die Temperatur des Gasstrahles unterhalb des Schmelzpunktes der Pulverpartikel des Zusatzwerkstoffes liegt. Aber selbst bei Temperaturen des Gasstrahles von 100 K bis zu 200 K oberhalb des Schmelzpunktes der Pulverpartikel des Zusatzwerkstoffes kann aufgrund der extrem kurzen Verweilzeit der Partikel im Gasstrahl im Bereich von Millisekunden ein Schmelzen oder auch ein Anschmelzen der Pulverpartikel verhindert werden. Die Bedeutung der höheren Gastemperaturen bzw. der Vorteil der Erwärmung des Gases liegt darin, daß in heißeren Gasen die Schallgeschwindigkeit höher ist und dadurch auch die Partikelgeschwindigkeit vergleichsweise größer wird.An essential feature of the invention is that the powder particles of Filler material in the gas jet should not be melted. According to the Invention mean that the aim is to have the powder particles of the filler material in the Do not melt the gas jet (i.e. convert it completely into the liquid phase) that but is not aimed that the powder particles of the filler in Gas jet as a mixture of on and / or unmelted particles and on the other hand, composed of molten particles. The statement that the powder particles of the filler material not be melted in the gas jet can be ensured that the Temperature of the gas jet below the melting point of the powder particles Filler material is. But even at temperatures of the gas jet from 100 K to to 200 K above the melting point of the powder particles of the filler material due to the extremely short dwell time of the particles in the gas jet in the range of Milliseconds prevent the powder particles from melting or melting become. The importance of higher gas temperatures or the advantage of Heating of the gas lies in the fact that in hotter gases the speed of sound is higher and the particle speed also becomes comparatively greater as a result.

Das Kaltgasspritzverfahren besitzt gegenüber herkömmlichen Verfahren des thermischen Spritzens eine Reihe von Vorteilen. Die thermische Einwirkung und Kraftwirkung auf die Oberfläche des Substratwerkstoffes ist verringert, wodurch ungewollte Veränderungen der Materialeigenschaften des Substratwerkstoffes verhindert oder zumindest merklich verringert werden können. Ebenso können weitgehend Änderungen in der Struktur des Substratwerkstoffs unterbunden werden.The cold gas spray process has compared to conventional processes of thermal spraying has a number of advantages. The thermal action and The effect of force on the surface of the substrate material is reduced, as a result unwanted changes in the material properties of the substrate material can be prevented or at least significantly reduced. You can also changes in the structure of the substrate material are largely prevented.

Überraschenderweise wurde nun festgestellt, daß die zahlreichen verfahrenstechnischen Möglichkeiten des thermischen Spritzens nach dem Kaltgasspritzverfahren für die Herstellung von Formteilen genutzt werden können. Durch die Möglichkeiten der Verwendung unterschiedliche Pulvermaterialien und Pulvermischungen eröffnet sich eine breite Palette für die Zusammensetzung von Formteilen.Surprisingly, it has now been found that the numerous process engineering Possibilities of thermal spraying using the cold gas spraying process can be used for the production of molded parts. Through the possibilities opened the use of different powder materials and powder mixtures a wide range for the composition of molded parts.

Ein Grundkörper kann erfindungsgemäß durch Aufspritzen einer Schicht oder eines Überzugs mittels des Kaltgasspritzverfahrens auf eine gewünschte Dicke verstärkt werden. Dabei können relativ dünne Grundkörper, z.B. ein relativ dünnwandiges nach einem herkömmlichem Verfahren hergestelltes Formteil, als Ausgangsmaterial verwendet werden. Dieser Grundkörper wird anschließend durch Aufspritzen von gleichartigem oder unterschiedlichem Material auf der Innen- und/oder der Außenseite auf die notwendige Dicke verstärkt. Besondere Vorteile sind zu erzielen, wenn der Grundkörper eine geringere Dicke aufweist als die durch thermisches Spritzen aufgespritzte Schicht Diese Variante erleichtert die Herstellung von Formteilen aus bzw. mit schwer formbaren Werkstoffen.According to the invention, a base body can be sprayed on by a layer or a layer Coating reinforced to a desired thickness using the cold gas spraying process become. Relatively thin base bodies, e.g. a relatively thin walled after A molded part produced by a conventional method as a starting material be used. This body is then sprayed on same or different material on the inside and / or the outside reinforced to the necessary thickness. Special advantages can be achieved if the Base body has a smaller thickness than that by thermal spraying sprayed-on layer This variant facilitates the production of molded parts or with materials that are difficult to form.

Es eignen sich als Grundkörper auch Formkörper aus leicht plastisch verformbarem Material, beispielsweise Kupfer, Aluminium oder diese enthaltenden Legierungen. Die Grundkörper können relativ dünn sein, beispielsweise im Bereich von 0,1 bis 10 mm, vorzugsweise 0,5 bis 5,0 mm. Nach dem Aufspritzen eines insbesondere schwer formbaren Materials mittels des Kaltspritzverfahrens kann anschließend der Formkörper, beispielsweise auf mechanischem Wege oder chemisch durch Auflösen, von der aufgespritzten Schicht entfernt werden. In diesem Fall bildet allein die Spritzschicht das gewünschte Formteil. Diese Methode unterstützt in besonderem Maße die Herstellung von Formteilen aus bzw. mit schwer formbaren Werkstoffen.Moldings made of easily plastically deformable are also suitable as base bodies Material, for example copper, aluminum or alloys containing them. The Base bodies can be relatively thin, for example in the range from 0.1 to 10 mm, preferably 0.5 to 5.0 mm. After spraying a particularly heavy malleable material by means of the cold spray process can then Molded articles, for example mechanically or chemically by dissolving, be removed from the sprayed-on layer. In this case, only that Spray layer the desired molded part. This method supports in particular Dimensions the production of molded parts from or with difficult to form materials.

In einer weiteren Variante der Erfindung wird zunächst ein Rohkörper nach einem der oben beschrieben Möglichkeiten oder nach einer Kombination hergestellt. Dieser Rohkörper muß noch nicht die gewünschte Form des herzustellenden Formteils aufweisen, sondern kann im Gegenteil z.B. aus einem flachen Blechkörper bestehen. Nach dem Auftragen der Schicht durch thermisches Spritzen kann das Werkstück (der beschichtete Roh- oder Grundkörper oder nur die Schicht) in einem oder mehreren der bekannten Umformprozesse (Ziehen, Tiefziehen, Walzen, Pressen und dergleichen) weiter bearbeitet werden. Auf diese Weise erhält man schließlich das gewünschte Formteil. Der Vorteil dieser Variante liegt darin, daß gespritzte Bleche bzw. Rohkörper sehr feinkörnig und praktisch texturfrei sind. Ihre Verformung erfolgt daher sehr gleichmäßig und erlaubt höhere Verformungsgrade als bei Blechen, die durch Glühen oder Walzen hergestellt wurden.In a further variant of the invention, a raw body according to one of the possibilities described above or produced by a combination. This raw body does not have to have the desired shape of the molded part to be produced, on the contrary, e.g. consist of a flat sheet metal body. After applying the layer by thermal spraying, the workpiece can (the coated raw or basic body or just the layer) in one or several of the known forming processes (drawing, deep drawing, rolling, pressing and the like) are processed further. This is how you finally get that desired molding. The advantage of this variant is that sprayed sheets or raw bodies are very fine-grained and practically texture-free. Your deformation takes place therefore very uniform and allows higher degrees of deformation than with sheet metal were produced by annealing or rolling.

Erfindungsgemäß kann das Gas für das thermische Spritzen Stickstoff, Helium, Argon, Neon, Krypton, Xenon, ein Wasserstoff enthaltendes Gas, ein kohlenstoffhaltiges Gas, insbesondere Kohlendioxid, Sauerstoff, ein Sauerstoff enthaltendes Gas, Luft, Wasserstoff oder Mischungen der vorgenannten Gase enthalten. Neben den aus der EP 0 484 533 B1 bekannten Gasen Luft und/oder Helium eignen sich auch für das den pulverförmigen Zusatzwerkstoff tragende Gas ein Stickstoff, Argon, Neon, Krypton, Xenon, Sauerstoff, ein Wasserstoff enthaltendes Gas, ein kohlenstoffhaltiges Gas, insbesondere Kohlendioxid, Wasserstoff oder Mischungen der vorgenannten Gase und Mischungen dieser Gase mit Helium. Der Anteil des Helium am Gesamtgas kann bis zu 90 Vol.-% betragen. Bevorzugt wird ein Heliumanteil von 10 bis 50 Vol.-% im Gasgemisch eingehalten.According to the invention, the gas for thermal spraying can be nitrogen, helium, Argon, neon, krypton, xenon, a gas containing hydrogen, a carbon-containing one Gas, especially carbon dioxide, oxygen, an oxygen-containing Contain gas, air, hydrogen or mixtures of the aforementioned gases. Next The gases air and / or helium known from EP 0 484 533 B1 are suitable nitrogen, argon, also for the gas carrying the powdered filler material, Neon, krypton, xenon, oxygen, a gas containing hydrogen, a carbon-containing one Gas, especially carbon dioxide, hydrogen or mixtures of the aforementioned gases and mixtures of these gases with helium. The proportion of helium of the total gas can be up to 90% by volume. A helium content of 10 to 50 vol .-% observed in the gas mixture.

Es hat sich gezeigt, daß durch den Einsatz von unterschiedlichen Gasen zum Beschleunigen und Tragen des pulverförmigen Zusatzwerkstoffes die Flexibilität und Wirksamkeit des Verfahrens wesentlich vergrößert werden kann. Die so hergestellten Schichten haften sehr gut auf den verschiedensten Substratwerkstoffen, beispielsweise auf Metall, Metallegierungen, Keramik, Glas, Kunststoffe und Verbundwerkstoffe. Die mit dem erfindungsgemäßen Verfahren hergestellten Beschichtungen sind von hoher Güte, weisen eine außerordentlich geringe Porosität auf und besitzen extrem glatte Spritzoberflächen, so daß sich in der Regel eine Nacharbeitung erübrigt Die erfindungsgemäß eingesetzten Gase besitzen eine ausreichende Dichte und Schallgeschwindigkeit, um die erforderlichen hohen Geschwindigkeiten der Pulverpartikel gewährleisten zu können. Das Gas kann dabei inerte und/oder reaktive Gase enthalten. Mit den genannten Gasen ist die Herstellung von sehr dichten und besonders gleichmäßigen Beschichtungen möglich, welche sich außerdem durch ihre Härte und Festigkeit auszeichnen. Die Schichten weisen extrem geringe Oxidgehalte auf. Sie besitzen keine oder zumindest keine ausgeprägte Textur, d.h. es gibt keine Vorzugsorientierung der einzelnen Körner oder Kristalle. Das Substrat wird femer nicht durch eine Flamme oder ein Plasma erwärmt, so daß keine oder nur extrem geringe Veränderungen am Grundkörper und auch kein Verzug von Werkstücken durch Wärmespannungen infolge des thermischen Spritzens auftreten.It has been shown that by using different gases to accelerate and carrying the powdered filler the flexibility and Effectiveness of the process can be increased significantly. The so produced Layers adhere very well to a wide variety of substrate materials, for example on metal, metal alloys, ceramics, glass, plastics and composite materials. The coatings produced using the method according to the invention are of high quality, have an extremely low porosity and possess extremely smooth spray surfaces, so that there is usually no need for reworking The gases used according to the invention have a sufficient density and Speed of sound to the required high speeds of the powder particles to be able to guarantee. The gas can be inert and / or reactive gases contain. With the gases mentioned is the production of very dense and special uniform coatings possible, which is also due to their hardness and distinguish strength. The layers have extremely low oxide contents. They have no or at least no pronounced texture, i.e. There is none Preferred orientation of the individual grains or crystals. The substrate becomes further not heated by a flame or a plasma, so no or only extreme minor changes to the base body and no distortion of workpieces due to thermal stress due to thermal spraying.

Der Gasstrahl kann auf eine Temperatur im Bereich zwischen 30 und 800 °C erwärmt werden, wobei alle bekannten pulverförmigen Spritzmaterialien eingesetzt werden können. Die Erfindung eignet sich insbesondere für Spritzpulver aus Metallen, Metalllegierungen, Hartstoffen, Keramiken und/oder Kunststoffen.The gas jet can be heated to a temperature in the range between 30 and 800 ° C are, all known powdery spray materials are used can. The invention is particularly suitable for wettable powders made of metals, metal alloys, Hard materials, ceramics and / or plastics.

In Ausgestaltung des erfindungsgemäßen Verfahrens wird die Temperatur des Gasstrahles im Bereich zwischen 300 und 500 °C gewählt. Diese Gastemperaturen eignen sich insbesondere für den Einsatz von reaktiven Gasen oder reaktiven Gasbestandteilen. Als reaktive Gas oder Gasbestandteile sind insbesondere Wasserstoffzumischungen, kohlenstoffhaltige Gase oder stickstoffhaltige Gase zu erwähnen. In an embodiment of the method according to the invention, the temperature of the gas jet selected between 300 and 500 ° C. These gas temperatures are particularly suitable for the use of reactive gases or reactive Gas constituents. As reactive gas or gas components are in particular Hydrogen admixtures, carbon-containing gases or nitrogenous gases mention.

In Weiterbildung der Erfindung wird ein Gasstrahl mit einem Druck von 5 bis 50 bar eingesetzt. Vor allem das Arbeiten mit höheren Gasdrücken bringt zusätzliche Vorteile, da die Energieübertragung in Form von kinetischer Energie erhöht wird. Es eignen sich insbesondere Gasdrücke im Bereich von 21 bis 50 bar. Hervorragende Spritzergebnisse wurden beispielsweise mit Gasdrücken von etwa 35 bar erzielt. Die Hochdruckgasversorgung kann beispielsweise durch das in der deutschen Patentanmeldung DE 197 16 414.5 beschriebene Verfahren bzw. die dort beschriebene Gasversorgungsanlage sichergestellt werden.In a development of the invention, a gas jet with a pressure of 5 to 50 bar used. Above all, working with higher gas pressures brings additional Advantages because the energy transfer in the form of kinetic energy is increased. It gas pressures in the range from 21 to 50 bar are particularly suitable. excellent Spray results were achieved, for example, with gas pressures of around 35 bar. The High pressure gas supply can, for example, by the in the German patent application DE 197 16 414.5 described method or the one described there Gas supply system can be ensured.

Im erfindungsgemäßen Verfahren können die Pulverpartikel auf eine Geschwindigkeit von 300 bis 1600 m/s beschleunigt werden. Im erfindungsgemäßen Verfahren eignen sich dabei insbesondere Geschwindigkeiten der Pulverpartikel zwischen 1000 und 1600 m/s, besonders bevorzugt zwischen 1250 und 1600 m/s, da in diesem Fall die Energieübertragung in Form von kinetischer Energie besonders hoch ausfällt.In the process according to the invention, the powder particles can run at one speed can be accelerated from 300 to 1600 m / s. Suitable in the process according to the invention speeds of the powder particles between 1000 and 1600 m / s, particularly preferably between 1250 and 1600 m / s, since in this case the Energy transfer in the form of kinetic energy is particularly high.

Die im erfindungsgemäßen Verfahren eingesetzten Pulver besitzen bevorzugt Partikelgrößen von 1 bis 100 µm.The powders used in the process according to the invention preferably have Particle sizes from 1 to 100 µm.

Das erfindungsgemäße Verfahren bietet die Möglichkeit, in Verbindung mit einer Automatisierung und mit computergesteuerter Bewegung des Grundkörpers oder der Spritzpistole Formteile besonders rasch und kostengünstig herzustellen (rapid prototyping).The method according to the invention offers the possibility in connection with a Automation and with computer-controlled movement of the base body or Spray gun to produce molded parts particularly quickly and inexpensively (rapid prototyping).

Zur Durchführung des erfindungsgemäßen Verfahrens können alle geeigneten Vorrichtungen eingesetzt werden, insbesondere gilt dies für die in der EP 0 484 533 B1 beschriebene Vorrichtung.All suitable devices can be used to carry out the method according to the invention are used, in particular this applies to those in EP 0 484 533 B1 described device.

Besondere Vorteile gegenüber herkömmlichen Formteilen bringen folgende nach der Erfindung hergestellte Formteile mit sich:

  • Formteile, welche einen Grundkörper und eine durch thermisches Spritzen erzeugte Schicht umfassen, wobei der Grundkörper vorzugsweise eine geringere Dicke aufweist als die aufgespritzte Schicht und
  • Formteile, welche jeweils aus einer (oder auch mehreren) mittels thermischen Spritzens erzeugten Schicht bestehen.
The following molded parts produced according to the invention have particular advantages over conventional molded parts:
  • Molded parts which comprise a base body and a layer produced by thermal spraying, the base body preferably having a smaller thickness than the sprayed-on layer and
  • Molded parts, which each consist of one (or more) layer produced by thermal spraying.

Die Erfindung sowie weitere Einzelheiten der Erfindung werden im folgenden anhand von in den Zeichnungen dargestellten Ausführungsbeispielen näher erläutert.The invention and further details of the invention are described below of exemplary embodiments illustrated in the drawings.

Hierbei zeigen:

Figur 1
ein erfindungsgemäß hergestelltes Formteil aus Grundkörper und Schicht;
Figur 2
ein erfindungsgemäß hergestelltes Formteil bestehend aus der Spritzschicht;
Figur 3
ein erfindungsgemäß hergestelltes Formteil bestehend aus der Spritzschicht nach Umformung mit herkömmlichem Verfahren.
Here show:
Figure 1
a molded part made according to the invention from base body and layer;
Figure 2
a molded part made according to the invention consisting of the spray layer;
Figure 3
a molded part made according to the invention consisting of the spray layer after shaping with a conventional method.

In Figur 1 ist im Bild A eine geformtes Blech 1 dargestellt. Auf dieses Blech1 wird durch thermisches Spritzen nach dem Kaltgasspritzverfahren eine Schicht 2 aufgetragen. Das Blech 1 weist eine geringere Dicke auf als die aufgespritzte Schicht 2. Das so erhaltene Formteil in Bild B besteht aus Grundkörper 1 (Blech) und Spritzschicht 2.A shaped sheet 1 is shown in FIG. 1 in FIG. This sheet1 is applied a layer 2 by thermal spraying using the cold gas spraying method. The sheet 1 has a smaller thickness than the sprayed-on layer 2. The molding obtained in this way in Figure B consists of base body 1 (sheet metal) and Spray layer 2.

In Figur 2 ist im Bild A ein Formkörper 1 aus einem Kupferblech gezeigt. Nach dem Auftragen einer thermischen Spritzschicht 2 gemäß Bild B, wird das Kupferblech 1 mechanisch von der Schicht 2 gelöst Das so erhaltene Formteil in Bild C besteht lediglich aus der Spritzschicht 2.A molded body 1 made of a copper sheet is shown in FIG. After this Applying a thermal spray layer 2 as shown in Figure B, the copper sheet 1 mechanically detached from layer 2 The molded part obtained in this way is shown in Figure C. only from the spray layer 2.

Der zunächst ungeformte Rohkörper bzw. das Blech 1 aus Bild A von Figur 3 wird durch thermisches Spritzen nach dem Kaltgasspritzverfahren mit einer Schicht 2 versehen (Bild B). Nachdem mechanisch das Blech 1 von der Schicht 2 entfernt wurde (Bild C), wird das aus der Spritzschicht 2 bestehende Werkstück nach einem herkömmlichen Umformprozess verformt und erhält, wie in Bild D dargestellt, auf diese Weise seine gewünschte Form als Formteil.The initially unshaped raw body or sheet 1 from Figure A of Figure 3 is provided with a layer 2 by thermal spraying using the cold gas spraying method (Picture B). After the sheet 1 was mechanically removed from the layer 2 (Figure C), the workpiece consisting of the spray layer 2 is made according to a conventional Forming process deforms and receives, as shown in Figure D, on this Way its desired shape as a molding.

Claims (8)

  1. Process for producing shaped parts (1, 2; 2), in which a base body (1) is coated (2) by thermal spraying and a pulverulent additive is passed onto the surface of the base body (1) which is to be coated by means of a gas without the powder particles of the additive being melted in the gas jet and in which the base body (1) is reinforced by spray coating to a desired thickness, the base body (1) having a thickness which is less than that of the layer (2) which is sprayed on by thermal spraying.
  2. Process for producing shaped parts (1, 2; 2) according to Claim 1, characterized in that the shaped part (1, 2; 2) which is produced by thermal spraying is subjected to one or more conventional forming processes, in particular by drawing, deep drawing, rolling and/or pressing.
  3. Process according to one of Claims 1 or 2, characterized in that the base body (1), after the layer (2) has been sprayed on by thermal spraying, is removed from this layer (2).
  4. Process according to Claim 3, characterized in that the base body (1) is removed from the layer (2) by means of a mechanical treatment or chemically by dissolution.
  5. Process according to one of Claims 1 to 4, characterized in that the gas used for the thermal spraying contains nitrogen, helium, argon, neon, krypton, xenon, a hydrogen-containing gas, a carbon-containing gas, in particular carbon dioxide, oxygen, an oxygen-containing gas, air, hydrogen or mixtures of the abovementioned gases.
  6. Process according to one of Claims 1 to 5, characterized in that the temperature of the gas jet during the thermal spraying lies in the range between 30 and 800°C.
  7. Process according to one of Claims 1 to 6, characterized in that the gas jet has a pressure of from 5 to 50 bar during the thermal spraying.
  8. Process according to one of Claims 1 to 7, characterized in that the powder particles are accelerated to a velocity of 300 to 1600 m/s during the thermal spraying.
EP98120105A 1997-10-27 1998-10-23 Production of mouldings Expired - Lifetime EP0911426B1 (en)

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DE19747385A DE19747385A1 (en) 1997-10-27 1997-10-27 Manufacture of molded parts

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102009048706A1 (en) * 2009-10-08 2011-04-28 Hermle Maschinenbau Gmbh Method and device for producing a molded part by means of generative application
DE102015102908A1 (en) 2015-03-02 2016-09-08 Schuler Pressen Gmbh Process for manufacturing a molded part, molding, tool and press with a tool

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19747384A1 (en) * 1997-10-27 1999-04-29 Linde Ag Manufacture of composite bodies
DE19747386A1 (en) * 1997-10-27 1999-04-29 Linde Ag Process for the thermal coating of substrate materials
US6602545B1 (en) * 2000-07-25 2003-08-05 Ford Global Technologies, L.L.C. Method of directly making rapid prototype tooling having free-form shape
US7367488B2 (en) 2005-05-10 2008-05-06 Honeywell International, Inc. Method of repair of thin wall housings
US20080145688A1 (en) 2006-12-13 2008-06-19 H.C. Starck Inc. Method of joining tantalum clade steel structures
DE102007018211A1 (en) 2007-04-16 2008-10-23 Linde Ag Production of electron beam accelerator windows comprises applying coating to support using thermal or kinetic spraying, support then being removed from coating, which is used as window
DE102007017753A1 (en) * 2007-04-16 2008-10-23 Innovaris Gmbh & Co. Kg Production of large components by kinetic cold gas compacting of material particles
US8197894B2 (en) 2007-05-04 2012-06-12 H.C. Starck Gmbh Methods of forming sputtering targets
WO2009109016A1 (en) * 2008-03-06 2009-09-11 Commonwealth Scientific And Industrial Research Organisation Manufacture of pipes
US8246903B2 (en) * 2008-09-09 2012-08-21 H.C. Starck Inc. Dynamic dehydriding of refractory metal powders
DE102010014747A1 (en) * 2010-04-13 2011-10-13 Hermle Maschinenbau Gmbh Producing component, comprises forming base body with conventional method, layering volume body directly on base body, forming further volume body on volume body, and inserting insert such as tube between base body and the volume body
US9412568B2 (en) 2011-09-29 2016-08-09 H.C. Starck, Inc. Large-area sputtering targets
US10519552B2 (en) 2016-12-22 2019-12-31 United Technologies Corporation Deposited material structure with integrated component
US10363634B2 (en) 2016-12-22 2019-07-30 United Technologies Corporation Deposited structure with integral cooling enhancement features
US20180179639A1 (en) * 2016-12-22 2018-06-28 United Technologies Corporation Modular tooling for a deposited structure
US10907256B2 (en) 2016-12-22 2021-02-02 Raytheon Technologies Corporation Reinforcement of a deposited structure forming a metal matrix composite
US10563310B2 (en) 2016-12-22 2020-02-18 United Technologies Corporation Multi-wall deposited thin sheet structure
US10648084B2 (en) 2016-12-22 2020-05-12 United Technologies Corporation Material deposition to form a sheet structure
DE102018005363A1 (en) * 2018-07-02 2020-01-02 Technische Universität Chemnitz Process for the production of a metallic semi-finished or finished part as a composite with a functionalized surface and such a semi-finished or finished part

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0911424A1 (en) * 1997-10-27 1999-04-28 Linde Aktiengesellschaft Making of composite materials
EP0911425A1 (en) * 1997-10-27 1999-04-28 Linde Aktiengesellschaft Method for thermally coating surfaces

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE810223C (en) * 1949-04-14 1951-08-06 Deutsche Edelstahlwerke Ag Process for the production of metallic moldings
US3165570A (en) * 1962-08-22 1965-01-12 Alexander T Deutsch Refractory powder injection, process and apparatus
DE2646554C3 (en) * 1976-10-15 1980-01-10 Castolin S.A., Lausanne (Schweiz) Powder welding process for coating metallic materials
NL7908745A (en) * 1979-12-04 1981-07-01 Skf Ind Trading & Dev METHOD FOR MANUFACTURING AN ARTICLE APPLIED BY THERMAL SPRAYING AND OBJECT, IN PARTICULAR A DRILLING CHISEL, OBTAINED BY THIS METHOD
CH658045A5 (en) * 1982-05-12 1986-10-15 Castolin Sa Process for the production of glass moulds for machines for the production of hollow glass
EP0305142A1 (en) * 1987-08-28 1989-03-01 Corning Glass Works Method of forming an article of desired geometry
DE3806177A1 (en) * 1988-02-26 1989-09-07 Siemens Ag Method for applying layers of high-temperature superconducting material to substrates
EP0484533B1 (en) * 1990-05-19 1995-01-25 Anatoly Nikiforovich Papyrin Method and device for coating
WO1995007768A1 (en) * 1993-09-15 1995-03-23 Societe Europeenne De Propulsion Method for the production of composite materials or coatings and system for implementing it
DE4413306C1 (en) * 1994-04-16 1995-10-19 Daimler Benz Aerospace Ag Reinforcing a construction component
DE4427262C1 (en) * 1994-07-30 1995-03-23 Mtu Muenchen Gmbh Process and apparatus for flame spraying
DE19520885C2 (en) * 1995-06-08 1999-05-20 Daimler Benz Ag Process for the thermal spraying of layers of metal alloys or metals and its use

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0911424A1 (en) * 1997-10-27 1999-04-28 Linde Aktiengesellschaft Making of composite materials
EP0911425A1 (en) * 1997-10-27 1999-04-28 Linde Aktiengesellschaft Method for thermally coating surfaces

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102009048706A1 (en) * 2009-10-08 2011-04-28 Hermle Maschinenbau Gmbh Method and device for producing a molded part by means of generative application
DE102015102908A1 (en) 2015-03-02 2016-09-08 Schuler Pressen Gmbh Process for manufacturing a molded part, molding, tool and press with a tool
WO2016138892A1 (en) 2015-03-02 2016-09-09 Schuler Pressen Gmbh Method for producing a moulded part, moulded part, tool and press comprising a tool

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